Aluminum alloy and it's usage in industry

Aluminum alloys

Aluminum is the thirteenth element of the periodic table, denoted by the symbol (Al). Aluminum is white, soft, non-magnetic and conductive. Aluminum is the third most abundant element in the earth’s crust (after oxygen and silicon).

About 8% of the earth’s crust is made of the most commonly used metal, aluminum. Aluminum alloys are one of the most diverse alloys that have many usages due to their light weight and high durability.

Today, due to the great potential and usages of aluminum metal in the production of various types of metal parts and the growing expansion of industries that use this metal as a parent metal in the supply of raw materials. The market for alloy aluminum has also become wider and wider.

Aluminum as a parent metal has the unique property of combining special chemical elements to show more pronounced coordinates and capabilities than other metals. The price of aluminum metal in the Iranian market varies depending on the type of alloy. In order to obtain the desired properties and characteristics, aluminum alloying operations are usually performed during the melting and casting process.

Certain types of aluminum are formed with the main property of aluminum, which usually contains 90-96% aluminum, and in addition has one or more other elements that have been added to aluminum to improve its properties.

Alloy aluminum usually includes several minor alloying elements in addition to the main alloying elements, which have a small amount but have a great impact on their properties.

Definition of alloying

In general, the word alloying means adding one or more elements or combinations of them to aluminum to achieve a specific set of properties. The change of properties due to the addition of these elements depending on the type of base element and the alloying elements added can be exclusively dependent on an element or a combination of added elements.

Since the strength and hardness of aluminum is always less than its alloy types, aluminum alloy is generally used in industry and pure aluminum is usually used in more special usages.

The reason for the expansion of this industry

According to extensive research conducted by researchers in the field of materials and metallurgy, aluminum metal is the best known metal in the world for obtaining various alloys due to maintaining its basic properties during alloying and improving its quality coordinates.

Aluminum alloys in different categories can cover a variety of industries. Many researches have been done in this field, most of which indicate that in the initial studies of materials for the production of various parts, the first channel to obtain the best raw materials is definitely to refer to the information of aluminum alloy, because most likely one of them as materials. The initial fabrication of the part passes the initial tests.

Specifications and features of aluminum alloy

Corrosion resistance

One of the characteristics of aluminum in its pure form is corrosion resistance. Attention increases.

Many aluminum alloy grades have high levels of atmospheric and chemical corrosion resistance due to the natural formation of the oxide layer adhering to the surface. This feature is more pronounced in 1xxx, 3xxx, 5xxx and 6xxx series alloys, which we will explain in the following.

Capability in thermal conductivity

Aluminum alloys have a very high thermal conductivity and due to the fact that they melt at a lower temperature than steel, but in the presence of fire, the temperature of aluminum alloy rises at a much slower speed.

Capability in electrical conductivity

Aluminum and some alloy aluminum have a very high electrical conductivity and in this respect are among the second most conductive metals after copper. One of the main reasons for the high approach of the electrical and electronics industries is their capability and its more affordable price than copper.

Appropriate ratio of strength to weight

Aluminum does not show much change in weight after alloying, in other words, the high strength of aluminum alloy relative to its weight is one of the main factors in its selection compared to other metals. Low density aluminum is suitable for making engineering alloys.

Although their strength is not as high as that of steels, the strength-to-weight ratio is high, and for this reason commercial aluminum alloys abound. The strength of most of these alloys can be increased by hard deposition or hot work.

Resistance to failure

By alloying, the level of failure resistance in alloy aluminum is significantly increased or their so-called toughness is increased. Many aluminum alloys are tough and are used in usages that require brittle fracture resistance and crack growth.

Very high workability

Aluminum alloy after the alloying process shows a very high flexibility and ability to work, that both by extrusion process and by a variety of machining and cnc machining can be achieved very precise specialized parts. Basically, one of the features of aluminum is that by making it alloy and obtaining different types of aluminum alloy, the amount of workability in this metal can be increased.

High connectivity

Aluminum alloys can be bonded to other surfaces by extensive bonding methods such as welding, soldering, riveting and even gluing and nailing.

Recyclability

Aluminum alloys have a very, very low percentage of non-recyclable castings, and the production residue of each category can be easily recovered using the process of melting and re-casting, and after recycling, materials of the same quality can be obtained.

Aluminum alloy groups

In general, aluminum alloys are divided into two categories in terms of production method, with climbing alloys accounting for more than 80% of the total volume of aluminum alloys used.

Alloys wrought

Rolling alloys according to the standard ( Associatian Aluminum ) AA are divided into eight groups 1xxx to 8xxx depending on the type of constituent metals; Workable aluminum alloys are alloys that are mechanically shaped to the desired shape.

Some of these alloys can be reinforced by special heat treatment and others are not heat treatable. Workable alloys are divided into eight groups based on their main alloying element, and each of the alloys in each group is named by the AA (Aluminum Society) with a four-digit number .

Alloys Casting

Aluminum are alloys that are molded into the desired shape. These alloys are also some heat treatable and some non-heat treatable. Each of these alloys is named by AA with a four-digit number placed between the fourth and third digits to the left of a dot .

Types of aluminum alloys

Aluminum – copper alloy

Its brand name is Dur Aluminum . The hardness of this alloy reaches a maximum despite 5.7% copper. Silicon and magnesium alloying elements are sometimes used. Duralumin is widely used in lightweight structures and the aircraft industry.

The corrosion resistance of doraluminins is lower than that of aluminum. They often protect the duralumin surface with a thin coating of commercial pure rolled aluminum. Sometimes the C code is introduced.

Aluminum – magnesium alloy

Its brand name is Alumag . The amount of magnesium is less than 10%. The main property of alumag is its good corrosion resistance. As the amount of magnesium increases by more than 10%, its corrosion resistance decreases sharply.

The main usage of these alloys is due to their good corrosion resistance, high lightness and indirectly good polishing ability and maintaining this polish in them. For this reason, amalgam alloys are used in architectural and decorative works. Manganese and silicon alloys are sometimes used. Sometimes introduced with the code G.

Aluminum – silicon alloys

Their brand is Alpax . Increasing silicon without greatly reducing its ductility increases the castability of aluminum and at the same time increases its mechanical strength. This alloy has 12 to 13% silicon and its hardness can be increased by heat treatment.

Sometimes 7% silicon and 3% magnesium are used. It is used in the preparation of oil tanks for internal combustion engines, washing machine parts, radiators and electrical appliances. Sometimes the code S is introduced.

Tin ( Sn )

This element effectively improves the anti-friction property, so it is useful in bearing usages. Cast alloys may contain up to 25% tin. Increasing the amount of tin improves the machining properties and affects the hard deposition action in some alloys.

Lead (Pb)

The presence of lead and its properties in amounts of more than 0.1% improves the machining properties.

Iron (Fe)

This element improves the resistance to hot cracks and reduces the adhesion of the piece to the mold in injection molding. Increasing its percentage reduces the formability. It may also react with other elements added to the melt to form complex intermetallic compounds or sludge.

Manganese (Mn)

This element is used in small amounts to control the destructive effect of iron in brittle phases. It contains about half a percent of iron. Manganese is used as an alloying element in workable alloy compounds.

Chromium ‬ (Cr)

The addition of chromium causes intermetallic compounds, and because these compounds have very little solubility in the solid state, they prevent grain growth. Chromium in some alloys improves corrosion resistance and in higher amounts increases the sensitivity to rapid cooling.

Nickel (Ni)

This element together with copper increases the resistance to high temperature and also reduces the coefficient of thermal expansion.

Phosphorus (P)

This element causes germination and refining of the primary silicon phase in hyperrotective aluminum-silicon alloys.

Titanium (Ti)

This element is used to fine-tune the structure in cast aluminum alloys. Titanium is usually used in small quantities.

Strontium (Sr)

This element is used to modify aluminum-silicon eutectic alloys.

Series of aluminum alloys

Aluminum alloys are one of the most diverse alloys that have many usages due to their light weight and high durability. Aluminum alloys are divided into 8 general series, which include 1000, 2000, 3000, 4000, 5000, 5000, 7000 and 8000 serie

Alloy aluminum alloy in brief
Series or category	Major composition
1xx.x	Aluminum is almost pure
2xx.x	Aluminum and copper alloy
3xx.x	Aluminum contains copper, silicon and a little magnesium
4xx.x	Silicon aluminum
5xx.x	Aluminum and magnesium alloy
6xx.x	Alloys with a combination of magnesium, silicon and aluminum
7xx.x	Alloys with a combination of zinc, aluminum and magnesium
8xx.x	Aluminum alloy with less conventional elements such as tin and lithium

1000 series of aluminum alloys

The 1000 series aluminum alloys contain at least 99% aluminum . This series of aluminum alloys has very high corrosion resistance, high electrical and thermal conductivity, machining acceptance, relatively low mechanical properties and weldability.

Also, this series of alloys are soft and are used in works such as making foil packages for food, electrical connections and welding wires

Properties and usage of 1050 aluminum alloy :

In naming 1xxx series aluminum alloys, the last two digits represent the percentage of purity of the alloy. In fact, 1050 is an alloy with 99.5% aluminum. This alloy is also known as AA1050A, S1B and A91050.

1000 series alloys do not have very high strength due to the lack of alloying elements. Naturally, 1050 is no exception to this rule and its yield strength is only about 85MPa. This alloy is one of the series of heat treatment alloys and its strengthening is done through hard strain operation.

Due to its low mechanical strength, 1050 aluminum alloy has good ductility and is easily formed by the process of stretching, rolling and extrusion. But this alloy does not have good machining capability.

Aluminum is inherently corrosion-resistant metal. As soon as the metal is exposed to air, it oxidizes to form a thin, sticky, dense layer that prevents corrosion. This layer is so strong that it only dissolves in strong acids and bases such as chlorine and some hydroxides. It is said that this protective layer can withstand pH solutions between 4.5 and 5.8. If the protective layer of the alloy is damaged by wear, a thin layer forms again and protects the alloy against corrosion.

In terms of welding capability, 1050 has a good weldability and can be welded with most arc and gas welding methods. For welding 1050 aluminum on its own or an alloy of the same subgroup, it is recommended to use 1100 filler welding wires. Is.

Physical properties of 1050 aluminum alloy :

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Mechanical properties of 1050 aluminum:

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Chemical composition of 1050 aluminum alloy:

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1050 alloy usages

Aluminum 1050 is an alloy with a very shiny surface, high purity and low strength. This alloy has high electrical and thermal conductivity. Therefore, it can be a good option for parts with these features, including:

Electrical conductor components such as power cords and sheaths
Reflective pages
Food industry containers
Architectural flashes
Chemical plant equipment
Properties and usages of 1060 aluminum alloy

Usages properties of 1060 aluminum alloy with chemical elements is suitable for making chemical industry equipment with the best use. Aluminum alloys are known for their high corrosion resistance properties. These alloys are sensitive to high temperatures and experience increased resistance to ground temperatures. Aluminum is a good low temperature alloy. 1060 low-strength aluminum alloy and pure aluminum alloy with suitable corrosion resistance properties.

Chemical composition of aluminum alloy 1060

Alloy name

Ingredients ( weight percentage )

considerations

Other elements

AL%

1060

V<0.05

Each

Total

Min 99.6

<0.35

<0.25

<0.03

–

<0.05

<0.03

–

Physical properties of 1060 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
1060	69	26	646	657	900	23.6	2.750	27.8	234	62

SPECIFICATIONS	METRIC	IMPERIAL
Density	2.7 g/cm³	0.0975 lb/in³
melting point	649°C	1200°

Typical mechanical properties of 1060 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase	Hardship	shear strength	Fatigue strength
O	69	28	43	19	48	21
H12	83	76	16	23	55	28
H14	97	90	12	26	62	34
H16	110	103	8	30	69	45
H18	131	124	6	35	76	45

PROPERTIES	METRIC	IMPERIAL
Elastic modulus	70-80 GPa	10152-11603 ksi
Poisson’s ratio	0.33	0.33

Other characteristics Properties and usages of 1060 aluminum alloy

ASTM B209	ASTM B210	ASTM B211	ASTM B221
ASTM B241	ASTM B345	ASTM B361	ASTM B404
ASTM B548	SAE J454	ASTM B483	ASTM B234

How to make and heat treatment of aluminum alloy 1060

hard working

1060 aluminum alloy hardens only due to cold. Tempers H18, H16, H14 and H12 are determined based on the amount of work transferred to this alloy.

Anil

1060 aluminum alloy can be annealed at 343 degrees Celsius (650 degrees Fahrenheit) and then cooled in air.

Welding

Standard commercial methods can be used for 1060 aluminum. In this welding process, whenever necessary, it must be AL 1060. Good results can be obtained from the resistance welding process of this alloy through trial and error.

forming

Aluminum 1060 can be formed between 510 and 371 degrees Celsius (950 to 700 degrees Fahrenheit).

forming

1060 Aluminum can be formed perfectly with hot and cold work with special techniques.

Machining

Aluminum 1060 is graded with relatively poor machining, especially in soft and smooth conditions. The use of high-speed lubricants or instrumentation or carbide is recommended for this alloy. Some cuts of this alloy can also be dried.

Anil

Aluminum 1060 does not harden using heat treatment and can be annealed after the cold process.

Heating

Aluminum / aluminum alloy 1060 can be heated between 482 and 260 degrees Celsius (900 to 500 degrees Fahrenheit).

Properties and usage of 1060 aluminum alloy

In cases where good corrosion resistance and ductility are required and do not require high strength, this alloy is used.
Aluminum 1060 is widely used in the manufacture of railway tank cars and chemical equipment.
One of the most common uses of this alloy is to make equipment and consumables in chemical processes. The annealing temperature of this alloy is 345 degrees Celsius.

Properties and usage of 1100 aluminum alloy

Aluminum sheets 1100, pure alloys or 1000 series alloys are alloys that are at least 99% pure aluminum. The most common 1000 series alloy is this alloy (1100 alloy). This alloy is commercially called pure aluminum. Aluminum alloy 1100 is soft and malleable and also has high workability and is very suitable for usages including severe shaping. Because in the process of forming, the 1100 aluminum sheet hardens more slowly.

Alloy 1100 is the most weldable aluminum alloy and has a tensile strength of about 85% of the 3003 alloy and has a significantly lower tensile strength than the 6061 alloy. Its initial form is usually in the form of a plate or wire, and its properties are not temperature dependent. Of all the aluminum alloys, this is the mechanically strongest alloy.

Chemical composition of 1100 aluminum alloy

Alloy name	Ingredients (weight percentage)							considerations	Other elements		AL%
1100	Si+Fe	Cu	Mn	Mg	Cr	Zn	Ti	Be<0.0008	Each	Total	Min 99
1100	<1	0.05-0.2	<0.05	–	–	<0.1	–	Be<0.0008	<0.05	<0.15	Min 99

Physical properties of 1100 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
o – 1100	69	26	643	657	904	23.6	2.71	29.2	222	59
H18 – 1100	69	26	643	657	904	23.6	2.71	30.2	218	57

Mechanical properties of 1100 aluminum

Type of heat treatment	Tensile strength	Surrender strength	Increase the length of the sample with a thickness of 0.062 inches	Increase the sample length by 0.5 inches	Hardship	shear strength	Fatigue strength
O	90	34	35	45	23	62	34
H12	110	103	12	28	28	69	41
H14	124	117	9	32	32	76	48
H16	145	138	6	38	38	83	62
H18	165	152	5	44	44	90	62

usage of 1100 aluminum sheet

This type of aluminum sheet can be used as an excellent thermal conductor in various industries. Of course, it should be noted that it is also very suitable for conducting electric current.
Although light weight, it shows high strength and durability.
It is resistant to corrosion and has the ability to weld as well as bond with glue.

The main usages of this alloy in industries :

General worksheet
Low pressure panels
Light bulbs
car tag
Heat Exchangers
food plates
Light reflectors

Properties and usages of 1145 aluminum alloy

This alloy is used in the manufacture of packaging foil, heat exchangers and also in insulation. Aluminum is very durable due to its corrosion resistance. They are sensitive to high temperatures in the range of 200 to 250 degrees Celsius (392 to 482 degrees Fahrenheit). High temperatures tend to reduce the strength of these alloys. However, the strength of aluminum alloys can be increased and converted to low temperature alloys.

Chemical composition of aluminum alloy 1145

AN ITEM	CONTENT (%)
Aluminum, Al	99.45 (min)
Copper, Cu	0.05
Manganese, Mn	0.05
Magnesium, Mg	0.05
Zinc, Zn	0.05
Titanium, Ti	0.03
Silicon, Si + Iron, Fe	Remainder

Physical characteristics of aluminum alloy 1145

SPECIFICATION	METRIC	IMPERIAL
Density	2.6-2.8 g/cm³	0.0939-0.1011 lb/in³

Mechanical properties of 1145 aluminum alloy

SPECIFICATION	METRIC	IMPERIAL
Elastic modulus	70-80 GPa	10152-11603 ksi
Poisson’s ratio	0.33	0.33

Thermal properties of 1145 aluminum alloy

PROPERTIES	Conditions	TREATMENT	T (ºC)
Thermal conductivity	227 W / mK	H18	25

The equivalent materials of 1145 aluminum alloy are as follows

AMS 4011
ASTM B373
ASTM B479
QQ A-1876

Manufacture and heat treatment of aluminum alloy 1145

Machining of aluminum alloy 1145

1145 Aluminum Alloy is a difficult alloy for the machine. Machining on the H16, 18 or 19 is a little easier using the cooler, softer mode.

Alloy aluminum structure 1145

Aluminum 1145 has excellent forming quality and can be easily formed using all common forming methods.

Welding of aluminum alloy 1145

The 1145 aluminum alloy welding capability is excellent in commercial methods such as TIG or MIG welding.

Heat treatment of aluminum alloy 1145

Aluminum 1145 is not a heat curable alloy that hardens with cold.

Cold work of aluminum alloy 1145

1145 aluminum alloy works easily in the cold. Very comfortable and soft, such as annealing, H12, 14, 16. It is much more difficult with obsessive-compulsive disorder, but it is still possible.

Heat treatment of aluminum alloy 1145

This can be done at 343 ° C (650 ° F) for a reasonable amount of time and then cooled.

Hardening of aluminum alloy 1145

Alloy 1145 hardens only with cold.

Properties and usage of aluminum alloy 1199

This ultra-pure grade with excellent anodizing, soldering and welding capabilities. Aluminum alloy 1199 has the highest purity of aluminum and the lowest amount of alloy. Aluminum is one of the most important metals due to its many properties. It is used in several fields such as automotive, aerospace, marine and engineering.

Because it is abundantly available, it is relatively cheaper than many metals. Aluminum 1199 is a malleable alloy with good corrosion resistance.

Chemical composition of aluminum alloy 1199

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

1199

V<0.005Ga<0.005

Each

Total

Min 99.99

<0.006

<0.002

<0.006

–

<0.006

<0.002

–

Physical properties of aluminum alloy 1199

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
1199	62	25	660	660	900	23.6	2.705	26.7	243	64.5

PROPERTIES	METRIC	IMPERIAL
Density	2.70 g/cm³	0.0975 lb/in³
Melting point	660°C	1220°F

Typical mechanical properties of aluminum alloy 1199

Tensile strength	Surrender strength	Percentage increase	Hardship	Percentage reduction in cold rolling process
45	10	50	15	Annealed
59	57	40	–	10
77	75	15	–	20
96	91	11	–	40
110	105	6	–	60
120	115	5	27	75

PROPERTIES	METRIC	IMPERIAL
Tensile strength	115 MPa	16700 psi
Yield strength	110 MPa	16000 psi
Poisson’s ratio	0.33	0.33
Elastic modulus	62 GPa	8990 ksi
Shear modulus	25 GPa	3630 ksi
Elongation at break (@thickness 1.60 mm/0.0630 in)	5%	5%
Shear strength	74 MPa	10700 psi
Hardness, Brinell (@load 500 kg with 10.0 mm ball)	31	31

Thermal properties of aluminum 1199

SPECIFICATIONS	CONDITIONS
T (°C)	TREATMENT
Electrical conductivity	243 W / mK	25	O

Properties and usage of aluminum alloy 1199

This alloy is known as ultra-pure aluminum and is used in vapor deposition coatings on surfaces of light reflectors, electrolytic capacitor foil, and chemical equipment.

Other properties of this alloy include low machinability, corrosion resistance, excellent anodizing effect, high welding and soldering capability and excellent workability.

Usages of aluminum 1199

Food industry utensils and foils
Heat Exchangers
Packaging foils
Chemical transmission equipment

Properties and usage of 1200 aluminum alloy

Usage Properties 1200 high purity aluminum alloy is used in the production of sheets, foils, wire and.. 1000 series aluminum has a purity of 99% (minimum). Aluminum 1200 is a malleable alloy that has high thermal conductivity and good reflectivity and corrosion resistance.

Chemical composition of aluminum alloy 1200

Alloy name	Ingredients (weight percentage)							consideration	Other elements		AL%
1200	Fe+Si	Cu	Mn	Mg	Cr	Zn	Ti	–	Each	Total	Min 99
1200	<1	<0.05	<0.05	–	–	<0.01	<0.05	–	<0.05	<0.15	Min 99

ELEMENT	CONTENT (%)
Aluminum, Al	≥ 99
Silicon, Si + Iron, Fe	≤ 1
Zinc, Zn	≤ 0.10
Copper, Cu	≤ 0.050
Titanium, Ti	≤ 0.050
Manganese, Mn	≤ 0.050
Other (each)	≤ 0.050
Other (total)	≤ 0.15

Physical properties of 1200 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
1200-O	69	25.9	645	657	898	23.4	2.71	29.5	225	58.5

PROPERTIES	METRIC	IMPERIAL
Density	2.70 g/cm³	0.0975 lb/in³

Typical mechanical properties of 1200 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase	Hardship
O	90	40	40	23

PROPERTIES	METRIC	IMPERIAL
Tensile strength	70 – 105 MPa	10152-15228 psi

Aluminum equivalent alloys 1200

Al 99.0
Alcoa-102
BA 99.0%
Star-99.2
Duricilium-T (99.0%)
Hiduminium-1C.

Welding of aluminum alloy 1200

Aluminum 1200 can be easily welded with MIG and TIG methods. The most common filler metals are aluminum 1050 and 4043. Inert gas welding is more suitable than gas welding or resistance. Because the product is stronger and more resistant to corrosion. This alloy has very good performance.

Properties and usage of 1200 aluminum alloy

Good corrosion resistance, good workability, high heat transfer, surface smoothness and slightly better weldability than 1050A alloy are some of the properties of this alloy.
This alloy is used in the form of sheets, foils, wires and profiles in car license plates, identification plates, kitchen utensils, packaging foils, car decorative items, heat exchangers, radiators, as well as construction, chemical and food industries.
Construction and gable
Equipment and containers for food and chemical industries
Ship structure
Bottle cap
Car
Furniture and lighting
Sound boards
Conductive material

Properties and usage of aluminum alloy 1350

This alloy has good conductivity and is used in the electronics industry. 1000 series alloys such as 1350 aluminum have special usages in many industries. 1350 alloy is primarily used in the manufacture of electrical conductors and the temperature -H111 shows the highest electrical conductivity in all grades of extruded aluminum conductor, using IACS or 61.0%.

1350 Aluminum Alloy is a high alloy aluminum alloy (silicon, iron, copper, manganese and other elements). 1350 alloy is very conductive and has good ductility and leads to its use in electronics and other usages.

Properties and usage of aluminum alloy 1350

The following typical properties are not approved. Because in most cases they are calculated on average and are for different sizes and production methods and may not exactly represent any particular product or size. Although this data is certified by international standards and is a reliable source, it must be evaluated and tested before any use.

Chemical composition of aluminum alloy 1350

Alloy name	Ingredients (weight percentage)							consideration	Other elements		AL%
1350	Si+Fe	Cu	Mn	Mg	Cr	Zn	Ti	B<0.05Ga<0.03	Each	Total	Min 99.5
1350	<1	<3.3-4.6	<0.5-1	<0.4-1.8	<0.1	<0.8	<0.2	B<0.05Ga<0.03	<0.03	<0.1	Min 99.5

Physical properties of aluminum alloy 1350

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
1350-O	69	–	646	657	900	23.6	2.705	27.9	234	61.8
1350-H19	69	–	646	657	900	23.6	2.705	28.2	230	61

Typical mechanical properties of aluminum alloy 1350

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase
O	83	28	55
H12	97	83	62
H14	110	97	69
H16	124	110	76
H19	186	165	103

Standard alloys of aluminum alloy 1350

Generally 1000 series of aluminum alloys are produced at this standard temperature :

F :There is no special control over thermal conditions and there are no restrictions on mechanical properties.
O – Annealing : Used for products that are resistant to the lowest temperatures.
H111 & H112 : Hardens the pressure using the extrusion process.

Properties and usage of aluminum alloy 1350

This alloy is known as the Aluminum (EC) brand for the electrical industry and is used to make sheets, wires, rods, tubes, extruded profiles, transmission lines, bus bars, bus conductors (high pressure fittings), belts and tape for transformers. High pressure and… is used.

Due to its high purity of 99.5% or more of aluminum, 1350 is a component of “EC” or “Conduct Electric” alloys. 1350 alloy is used in a number of electrical and other industries due to its high conductivity and ductility.

2000 series of aluminum alloys

The 2000 series of aluminum alloys consists of two main elements, aluminum and copper, along with other alloying elements. The characteristics of this series of alloys include high strength, high hardness, good weldability, high fracture resistance and low casting capability. These properties can be improved by adding alloying elements such as magnesium and silver

The 2000 series of aluminum alloys can be used in the aerospace industry, aircraft and spacecraft construction, truck construction, and rivets or screws in various parts

Properties and usages of aluminum alloy 2007

Properties and usages of 2007 aluminum alloy mostly include excellent machining of this grade of aluminum.

Chemical composition of aluminum alloy 2007

Alloy name	Ingredients (weight percentage)							consideration	Other elements		AL%
2007	Fe+Si	Cu	Mn	Mg	Cr	Zn	Ti	Pb : 0.8-1.2Bi<0.2

Ni<0.2

Sn<0.2

EachTotalRem<1<3.3-4.6<0.5-1<0.4-1.8<0.1<0.8<0.2–<0.3

Physical properties of aluminum alloy 2007

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
2007-T3, T4	72.5	27.3	510	640	856	23	2.85	51	130	34

Typical mechanical properties of 2007 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase	Hardship
T3	460	360	11	115
T4	97	83	62	–

Properties and usages of aluminum alloy 2007

This alloy has excellent machining properties, very high cutting speed, low corrosion resistance, high toughness and strength and very high heat treating properties.

It is used in various machined components, screws, fittings and various parts, and can be produced in different shapes of pipes, sheets, wires, tubes and..

Properties and usages of aluminum alloy 2011

Properties and usages of aluminum alloy 2011 offers this alloy for extrusion of various sections with good machinability.

Aluminum alloys have strong corrosion resistance. These alloys are considered as suitable low temperature alloys. Because their resistance increases when exposed to ground temperature, they lose some of their resistance when exposed to high temperatures.

Aluminum alloys are sensitive to high temperatures between 200 and 250 degrees Celsius (392 and 482 degrees).

Chemical composition of aluminum alloy 2011

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

2011

Pb : 0.2-0.6

Each

Total

Rem

<0.4

<0.7

<5-6

–

<0.3

–

<0.05

<0.15

ELEMENT	CONTENT (%)
Aluminum, Al	93.7
Copper, Cu	5.5
Bismuth, Bi	0.4
Lead, Pb	0.4

Physical properties of aluminum alloy 2011

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
2011-T3, T4	70	26	541	638	864	23.1	2.82	44	152	39
2011-T8	70	26	541	638	864	23.1	2.82	38	173	45

PROPERTIES	METRIC	IMPERIAL
Density	2.82 g/cm³	0.1018 lb/in³

Typical mechanical properties of 2011 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	shear strength	Percentage increase	Hardship
T3	379	296	221	15	95
T4	407	310	241	12	100

PROPERTIES	METRIC	IMPERIAL
Elastic modulus	70-80 GPa	10152-11603 ksi
Poisson’s ratio	0.33	0.33

The aluminum alloy equivalents of 2011 are :

ASTM B210
ASTM B211
DIN 3.1056
QQ A-225/3
SAE J454

Manufacture and heat treatment of aluminum alloy 2011

Heating

Aluminum 2011 is stored for 2 to 3 hours at 413 degrees Celsius (775 degrees Fahrenheit) and then cooled to 100 degrees Celsius (50 degrees Fahrenheit) at 260 degrees Celsius (500 degrees) per hour in a controlled manner. Fahrenheit) and eventually cools in the air.

Welding

Welding is not recommended for 2011 aluminum.

Forming

The 2011 aluminum alloy can be heated between 288 and 482 degrees Celsius (550 and 900 degrees Fahrenheit).

shaping

Conventional methods are used to shape, bend and shape the 2011 aluminum alloy. This alloy has hardened after cooling due to the increase in strength.

Machining

2011 Aluminum Alloy is a machining alloy. High speed steel tools and carbide tools can be used for this alloy. Applause angles should have a cutting edge of 32 degrees and 15 degrees to the right. Light cutting can be dried and heavy cutting can be done using oils.

Heat treatment

The 2011 aluminum alloy is used to achieve optimum strength at 510 ° C (950 ° F). After complete heat treatment, this alloy is cooled with water and works as desired. Finally, it is heated at 160 degrees Celsius (320 degrees Fahrenheit) for 15 hours and then cooled in air.

Temper

The 2011 aluminum alloy hardens at 510 degrees Celsius (950 degrees Fahrenheit) and then the water is extinguished. The alloy can also be heated to 160 degrees Celsius (320 degrees Fahrenheit) for 14 hours after heating the solution to produce the temperature of T8.

hard working

Aluminum 2011 hardens for 3 hours at 510 degrees Celsius (950 degrees Fahrenheit) and then cools with water.

Properties and usages of alloy 2011

Aluminum 2011 is used in the manufacture of machine parts, screw machine products, pipe fittings, pipe branches, hose parts. This alloy is used in the manufacture of rods, wires, pipes and extruded profiles, stretched pipes, rebars, and also in cases that require good machining properties and strength.

Properties and usages of aluminum alloy 2014

Properties and usages of aluminum alloy 2014 include strong corrosion resistance and high electrical conductivity, and therefore it is widely used for the production of industrial sections, plates and sheets. The strength of these alloys increases at lower temperatures, and when these alloys are exposed to high temperatures, their strength is lost.

Aluminum alloys are suitable for low temperatures and are sensitive to high temperatures in the range of 200 to 250 degrees Celsius (392-482 ° F).

Chemical composition of aluminum alloy 2014

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

2014

–

Each

Total

Rem

<0.5-1.2

<0.7

<3.9-5

0.4-1.2

0.2-0.8

<0.1

<0.25

<0.15

<0.05

<0.15

Alclad 2014Coating with 6006

0.2-0.6

<0.35

0.15-0.3

0.05-0.2

0.45-0.9

<0.1

–

<0.05

<0.15

Rem

Physical specifications of aluminum alloy 2014

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
2014-O	72.4	28	507	638	–	22.5	2.8	34	192	50
2014-T6	72.4	28	507	638	–	23.4	2.8	43	155	40

Mechanical properties of aluminum alloy 2014

Alloy name	Type of heat treatment	Tensile strength	Surrender strength	Increase the sample length by 0.5 inches	Hardship	shear strength	Fatigue strength
2014	O	186	97	125	18	45	90
	T4	427	290	260	20	105	140
	T6	483	414	240	13	135	125
Alclad 2014	O	172	69	125	21	–	–
	T3	434	276	255	20	–	–
	T4	421	255	255	22	–	–
	T6	469	414	285	10	–	–

Alloy heat treatment conditions 2014 | Alclad 2014

To perform T6 operations for products such as plates, wires, rods, sheets should be stored at 160 degrees Celsius for about 18 hours. Forged parts need to be stored at 171 ° C for 10 hours. The dissolution temperature of this alloy is 502 degrees Celsius and its annealing temperature is 413 degrees Celsius.

Other characteristics of aluminum alloy 2014

Materials similar to aluminum alloy 2014 are listed in the table below.

ASTM B210	ASTM B211	ASTM B221	ASTM B241	ASTM B247
ASTM BB241	DIN 3.1255	MIL T-15089	QQ A-200/2	QQ A-225/4
QQ A-250/4	QQ A-367	SAE J454

Annealing aluminum alloy 2014

Aluminum alloy 2014 can be neutralized at 413 degrees Celsius (775 degrees Fahrenheit) for 2 to 3 hours. The alloy is then cooled between 10 and 260 degrees Celsius (50 and 500 degrees Fahrenheit) every hour, followed by cooling.

2014 aluminum alloy welding

Gas consumption arc method is recommended for 2014 aluminum alloy. Solid rods or 2017 alloy or 2014 alloy are used in the welding process. Fixturing is set to a minimum of strength because the alloy breaks during the welding process.

Forging aluminum alloy 2014

Aluminum 2014 alloy can be forged between 399 and 454 degrees Celsius (750-850 ° F).

Forming of aluminum alloy 2014

Conventional methods are used to form the 2014 aluminum alloy. The forming process is performed in T3 or T4 and a narrow bending radius is not recommended for this welding process.

Machining feature of aluminum alloy 2014

Aluminum alloy 2014 has the ability to operate in neutral conditions and the use of kerosene or oil for this machining process is recommended. The use of a 20-degree roller, a 10-degree smoothing and a 15-degree high roller are essential for cutting and turning.

Heat treatment of aluminum alloy 2014

Aluminum Alloy 2014 The alloy is heated to 502 ° C (935 ° F) and then cooled. As a result of this heat treatment, a temperature of T4 is produced.

Hardening of aluminum alloy 2014

The alloy is cured by heat treatment at 502 ° C (935 ° F). The alloy is then diluted with water to produce T4 heat.

Excess cold work after the hardening process of this alloy, causes the temperature to rise. T6511 and T6510 are produced by heat treatment at 160 ° C (320 ° F).

Asage of aluminum alloy 2014 / Alclad 2014

This alloy is used for usages that require high strength and hardness at high temperatures, for example, the following :

Extruded profiles
Heavy forging sheets and parts
Widely used in aircraft parts such as wheels, fittings and main aircraft structures
Various parts in military and defense industries
Car suspension parts
Truck frame
Rods
the wire
Pipe

Properties and usages of 2024 aluminum alloy

Production of extruded sheets, rods, wires, pipes and profiles, aircraft fuselage and… are some of the usages of this aluminum alloy. Aluminum alloys have corrosion resistant properties. These alloys are sensitive to high temperatures between 200 and 250 ° C (392-482 ° F).

The strength increases when these alloys are exposed to low temperatures and high temperatures, and the strength is lost when these alloys are exposed to high temperatures. Good aluminum alloys are low temperature alloys.

Chemical composition of aluminum alloy 2024

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

2024

–

Each

Total

Rem

<0.05

<0.5

<3.8-4.9

0.3-0.9

1.2-1.8

<0.1

<0.25

<0.15

<0.05

<0.15

Alclad 2024

Coating with 1230

Si + Fe
<0.7<0.1<0.05<0.05–<0.1<0.03–<0.05<0.15Rem

Physical properties of 2024 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
2024-O	72.4	28	502	638	875	22.9	2.77	34	190	50
2024-T3,502 T36, T351, T361, T4	72.4	28	502	638	875	23.8	2.77	57	120	30
2024-T861, T851, T81, T6	72.4	28	502	875	238	2.77	2.77	45	151	38

Mechanical properties of 2024 aluminum alloy

Alloy name	Type of heat treatment	Tensile strength	Surrender strength	Percentage increase	shear strength	Fatigue strength
2024	O	185	75	20	47	90
	T3	485	345	18	120	140
	T4, T351	470	325	20	120	140
	T361	495	395	13	130	125
Alclad 2024	O	180	75	20	–	–
	T3	450	310	18	–	–
	T4, T351	440	290	19	–	–
	T361	460	365	11	–	–
	T81	450	365	6	–	–
	T861	485	455	6	–	–

Thermal treatment conditions of Alclad 2024 / Alclad 2024 The annealing temperature of this alloy is 413° C and its dissolution temperature is 493° C. To perform aging operation,T6 or T8 should be stored at 191° C for 8-16 hours.

Other characteristics of 2024 aluminum alloy

The equivalent materials of 2024 aluminum alloy are given in the table below :

AMS 4037	AMS 4120	AMS 4192	AMS 7223	ASTM B209
ASTM B210	ASTM B211	ASTM B221	ASTM B241	ASTM B316
ASTM F467	ASTM F468	DIN 3.1355	MIL B-6812	QQ A-430
MIL T-50777	QQ A-200/3	QQ A-225/6	QQ A-250/4	MIL T-15089
SAE J454	QQ WW-T-700/3

How to produce and heat treatment of aluminum alloy 2024

Alloying aluminum alloy 2024

Aluminum 2024 alloy is cooled from a temperature of between 399 and 427 ° C (750 and 800 F) for about 2 hours and then slowly cooled in a furnace. This alloy can be cooled between cold operations with a temperature of 343 ° C (650 F) 2 hours after the alloy has cooled in air.

Common methods are used to work aluminum 2024 aluminum alloy. Suitable for a sheet that is 1/4’s thick, or a bend radius thinner than 1/2 to 1 times the thickness. Ductility in annealing conditions is best suited for this alloy. Radius bends five to six times the thickness are suitable for T3

Welding aluminum alloy 2024

In order to weld 2024 aluminum alloy, the arc method of inert gas electrodes or resistance welding is used. In general, welding of any kind is not recommended for 2024 aluminum due to the reduction of corrosion resistance due to welding heat.

Forming of aluminum alloy 2024

Aluminum 2024 alloy can be forged, but a reasonable corrosion resistance must be maintained using subsequent operating heat. Conventional methods are used to form 2024 aluminum alloys. Hot forming is not recommended for this alloy.

Machining of aluminum alloy 2024

2024 alloy has good machining properties in thermal conditions. This alloy also has good machining properties in freezing conditions. Oil lubricants should be used in the machining process.

Heat treatment of aluminum alloy 2024

The 2024 alloy has a hard sex and is strengthened during the heat treatment process. Condition T6 When the alloy is heated to 493 ° C (920 F) and then cooled to 190 ° C (375 F) for 10 h and cooled in air. Condition T4 When the alloy is heated to 493 ° C (920 F) and then cold water is cooled and finally aged at room temperature.

Edging Aluminum Alloy 2024

Condition T6 is achieved by heating the 2024 aluminum alloy to 493 ° C (920 F), then cooling the water, reheating it to 190 ° C (375 F), and finally cooling the alloy in air.

Condition T4 is obtained by heating the alloy to 493 ° C (920 F) and then cooling the cold water. Edging eventually occurs at room temperature.

Usage of 2024 aluminum alloy

This alloy is used in the form of extruded sheets, rods, wires, pipes and profiles for making pipes, aircraft structures, rivets, screws and various other structural usages.

Properties and usage of aluminum alloy 2030

Aluminum alloy 2030 is made specifically for machining usages. This alloy is famous for its excellent machining properties and short chips. Among aluminum alloys for high-speed automatic lathes, 2030 and 2007 have the highest mechanical properties.

This alloy is chosen most of the time when we need to have a good combination of machinability and mechanical properties. In addition, 2030 has low resistance to corrosion. Therefore, it is recommended to use the protective anodizing of the final products.

Properties and usage of 2030 aluminum alloy

Usage Aluminum with 2030 copper alloy Despite the mechanical properties, screws, studs, washers, flanges and parts that require high mechanical properties such as cylinders and hydraulic pistons are made.

The main usages of this alloy :

Bolt
String rods

Chemical compounds of aluminum alloy 2030

CHEMICAL ELEMENTS	Si	Fe	Cu	Mn	Mg	Cr	Zn	Ti	Al
MIN	–	–	3.3	0.2	0.5	–	–	–	–
MAX	0.8	0.7	4.5	1	1.3	0.1	0.5	0.2	Rest

Aluminum 2030 (AlCu4PbMg, A92030)

Aluminum 2030 is a 2000 series aluminum alloy: the main additive is copper alloy and is formulated for pre-formed products. By European standards, it is given as EN AW-2030. AlCu4PbMg is the chemical name for EN. A92030 is a UNS number. In addition, the name AFNOR (French) is A-U4Pb.

International standards for aluminum alloy 2030

USA	SPAIN	FRANCE	GERMANY	GB	SWEDEN	SWITZERLAND	CANADA	ITALY
AA	A	AFNOR	DIN (1712-1725)	BS	SIS	VSM	ALCAN	UNI
2030	L-3121	A-U4Pb	AlCuMgPb	2L25	4335	200	–

Aluminum alloy heat treatment conditions 2030

Baking : 380 ° C to 420 ° C for 1 to 2 hours. Slow cooling
Placement in solution : 475 º C ± 5 ° C
Cooling in cold water (maximum 70 degrees Celsius)
Maturity : T3 / T4 states, at least 4 days at 20 ° C
To obtain parts : 380 ° C to 460 ° C

2030 Aluminum Alloy Alloys

2007 (AlCu4PbMgMn, 3.1645, A92007) Aluminum	2017A (AlCu4MgSi(A), 3.1325, H14) Aluminum
2024 (AlCu4Mg1, 3.1355, 2L97, A92024) Aluminum	2017 (AlCu4MgSi, A92017) Aluminum
2014 (AlCu4SiMg, 3.1255, A92014) Aluminum	2124 (2124-T851, AlCu4Mg1(A), 3.1354) Aluminum

Properties and usage of aluminum alloy 2036

Aluminum is about one-third the weight of steel, copper, iron, or brass . This metal is non-toxic, non-weldable, non-combustible and non-magnetic. 2036 aluminum alloy is made of aluminum. It is a strong hardware alloy with copper which is the main element of the alloy.

Chemical composition of aluminum alloy 2036

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

2036

–

Each

Total

Rem

<0.5

<2.2

0.1-0.4

0.3-0.6

<0.1

<0.25

<0.15

<0.05

<0.15

Mechanical properties of 2036 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase	Hardship
T4 for sheets with a thickness of 0.64 – 3.18 mm	290-340	160-195	20-24	80

Physical properties of aluminum alloy 2036

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
2036-O	70.3	–	554	649	882	23.4	2.75	33.2	198	52
2036-T4	70.3	–	554	649	882	23.4	2.75	42.1	159	41

Thermal properties of aluminum alloy 2036

The thermal properties of 2036 aluminum alloy are presented below.

PROPERTIES	CONDITIONS
T (°C)	TREATMENT
Thermal conductivity	۱۹۸ W / mK	۲۵	O

Heat treatment conditions of 2036 alloy for annealing, this alloy should be kept at 385 for 2-3 hours. The dissolution temperature of this alloy is 499 degrees Celsius.

2036 alloy usages

Used as a sheet for car panels. Due to the sensitivity to cracking and also the reduction of mechanical properties and corrosion during welding, the welding ability of this alloy under shielding gas is limited, but in the manufacture of car parts using resistance welding, good quality can be achieved in production.

Properties and usage of aluminum alloy 2048

Properties and usages Aluminum alloy 2048 with its chemical composition, suitable physical and mechanical properties has made it possible to manufacture parts and structures of military equipment. Aluminum 2048 is an alloy with good corrosion resistance.

Chemical composition of aluminum alloy 2048

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

2048

–

Each

Total

Rem

<0.15

<0.2

2.8-3.8

0.2-0.6

1.2-1.8

–

<0.25

<0.1

<0.05

<0.15

Physical properties of 2048 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
2048-T851	72	–	–	–	926	23.5	2.75	40.3	159	42

Typical mechanical properties of 2048 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase	Elastic modulus
25	457	416	8	70.3
120	414	392	13	68.3
175	354	338	14	64
260	234	219	10	57

Properties and usage of aluminum alloy 2048

It is used in the form of sheets and plates for the construction of components and structures in the aerospace industry and military equipment.

Properties and usage of aluminum alloy 2090

Grade 2090 aluminum is used to make aircraft parts. Pure aluminum is a shiny white silver metal. The distinctive feature of this metal is its light weight. Although aluminum alloys are strong, they can be easily worked. Because it is very soft and flexible. Aluminum Alloy 2090 is an alloy made with heat capability that can be easily welded.

Chemical composition of aluminum alloy 2090

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

2090

Zr : 0.08-0.15Li : 1.9-2.6

Each

Total

Rem

<0.1

<0.12

2.4-3

<0.05

<0.25

<0.05

<0.1

<0.15

<0.05

<0.15

Physical properties of 2090 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
2090-T81	76	–	560	650	1203	23.6	2.59	–	84-92	17-19

Typical mechanical properties of 2090 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase
T81	517	470	3

Thermal properties of aluminum alloy 2090

The thermal properties of 2090-T83 aluminum are tabulated below.

PROPERTIES	METRIC	IMPERIAL
Thermal expansion co-efficient (@20-100°C/68-212°F)	m/m°C	13.1 µin/in°F
Thermal conductivity	88 W/mK	611 BTU in/hr.ft².°F

Properties and usage of aluminum alloy 2090

Aluminum 2090 is mainly used in areas where high strength such as aircraft parts are required.

Usages of aluminum 2090

This alloy is used in the manufacture of sheets, forged and extruded parts, aerial structures, aircraft main structures and reservoir structures operating at sub-zero temperatures. The fuselage of passenger and warplanes and items that require a lot of modification are other uses of this alloy.

Some aircraft parts made of 2090-T83 aluminum alloy :

Aircraft fittings and bolts
The edges of the wings and nose
Large body structures

Properties and usage of aluminum alloy 2124

Properties and usage Aluminum 2124 alloy is suitable for construction in the fuselage due to the mechanical and physical properties of this grade. Aluminum alloys have strong corrosion resistance properties. These alloys are defined as low temperature alloys with high electrical conductivity.

Aluminum alloys resist exposure to groundwater and lose their strength when exposed to high temperatures. Aluminum alloys are sensitive to high temperatures ranging from 200 to 250 degrees Celsius (392 and 482 degrees Fahrenheit).

Chemical composition of aluminum alloy 2124

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

2124

–

Each

Total

Rem

<0.2

<0.3

3.8-4.9

0.3-0.9

1.2-1.8

<0.1

<0.25

<0.15

<0.05

<0.15

ELEMENT	CONTENT (%)
Aluminum, Al	93.50
Copper, Cu	4.4
Magnesium, Mg	1.5
Manganese, Mn	0.6

Physical properties of aluminum alloy 2124

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
2124-O	72	–	502	638	882	22.9	2.77	34.5	191	50
2124-T851	72	–	502	638	882	22.9	2.77	44.2	152	39

PROPERTIES	METRIC	IMPERIAL
Density	2.6-2.8 g/cm³	0.0939-0.1011lb/in³
Melting point	510°C	950°F

Typical mechanical properties of aluminum alloy 2124

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase
-296	705	620	10
-28	505	470	8
25	485	450	8
100	455	420	9
230	325	395	15

PROPERTIES	METRIC	IMPERIAL
Elastic modulus	70-80 GPa	10152-11603 ksi
Poisson’s ratio	0.33	0.33

Alloy heat treatment conditions 2124

The dissolution temperature of the alloy is 493 degrees Celsius, the annealing temperature is 413 degrees Celsius and the aging temperature is 191 degrees Celsius.

Aluminum alloy 2124-T851

Zr + Ti limit of maximum 0.20% may be used with this alloy only for extruded products, but only if the supplier or manufacturer and the buyer agree with each other.

This agreement may be indicated, for example, by reference to a standard, letter or other device indicating the Zr + Ti limit. The reported aluminum content is calculated as the residue.

Component	Wt. %
Al	91.2 – 94.7
Cr	Max 0.1
Cu	3.8 – 4.9
Fe	Max 0.3
Si	Max 0.2
Ti	Max 0.15
Zn	Max 0.25
Mg	1.2– 1.8
Mn	0.3– 0.9
Other, each	Max 0.05
Other, total	Max 0.15

Equivalent materials of 2124 aluminum alloy are :

AMS 4221
ASTM B209
QQ A-250/29
QQ A250/9

Other properties of aluminum alloy usage 2124

Anil

Aluminum alloy 2124 is annealed at 413 ° C (775 ° F) for 2 to 3 hours. The alloys are then cooled to 10 ° C (50 ° F) per hour to 260 ° C (500 ° F) and finally cooled in air.

Welding

Resistance welding is recommended for 2124 aluminum alloy. Arc welding and gas welding are not recommended for this alloy.

Forming

Aluminum alloy 2124 can be made and created.

shaping

Aluminum alloy 2124 can be formed in a limited way and extreme cold temperature is not recommended for this alloy.

Machining

Conventional methods are used for the machining process of 2124 aluminum alloy.

Heat treatment of aluminum alloy 2124

Aluminum alloy 2124 can be dissolved at 493 ° C (920 ° F) and then quenched. Temperature T 851 When hardening is done for 12 hours at 190 degrees Celsius (375 degrees Fahrenheit) followed by air cooling.

Harden

Aluminum alloy 2124 is cured for 12 hours at 190 ° C (375 ° F) and then cooled in air.

Temper

Temper for aluminum alloy 2124 is when it is done at 190 ° C (375 ° F) for about 12 hours and is alloy and then cooled in air.

Usage of aluminum alloy 2124

They are used in the form of sheets with a thickness of 1.5 to 6 inches for use in aircraft structures.

Properties and usage of 2218 aluminum alloy

Aluminum Alloy 2218 is an alloy in the family of copper-aluminum from the 2000 series. This alloy is one of the most complex grades of the 2000 series, with a minimum weight of 88.4% aluminum. Unlike most copper-aluminum alloys, the 2218 is a high-performance alloy with a relatively low strength of 255 MPa in terms of 2000 series alloy strength.

Despite being an alloy, it has the same corrosion and oxidation resistance as marine 5000 series alloys. Although 2218 is a malleable alloy, it can be used in casting due to its granular structure and is precisely machined after casting. Welding or glue is easy to use.

To increase tensile strength at workability cost, 2218 alloy can be heat refined with the highest grades being F, T61, T71 and T72. Alternative names for alloy are 2218, A2218 and A92218 .

Chemical composition of aluminum alloy 2218

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

2218

Ni : 1.7-2.3

Each

Total

Rem

<0.9

<0.1

3.5-4.5

<0.2

1.2-1.8

<0.1

<0.25

–

<0.05

<0.15

Physical properties of aluminum alloy 2218

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
2218-T61	74.4	27.5	532	635	871	22.4	2.8	45	148	38
2218-T72	74.4	27.5	532	635	871	22.4	2.8	43	155	40

Typical mechanical properties of 2218 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase	Hardship
T61	407	303	13	115
T71	345	276	11	105
T72	331	255	11	95

Properties and usage of aluminum alloy 2218

Proper performance, thermal conductivity and subsequent stability allow the 2218 alloy to be exposed to thermal shocks whenever high-precision parts are exposed. (Especially piston engine cylinders and cylinder heads)

Usages of aluminum 2218

The following are examples of usages of this alloy.

Forged parts
Diesel engines and aircraft pistons
Aircraft cylinder head
Compressor rims
Jet engine blades

Properties and usage of aluminum alloy 2219

This alloy is used to build the bodies of tanks and aircraft. Aluminum Alloy 2219 is an alloy in the copper-aluminum family made from the 2000 series. Aluminum-copper alloys have high strength. But they are generally harder to resist than corrosion and welding than other types of aluminum alloys.

The strength of these alloys decreases when exposed to temperatures of about 200 to 250 ° C. However, their strength can increase at low temperatures. For less corrosion resistance, 2219 aluminum can be found in a pure alloy such as 1050. This alloy is usually used by extrusion and is not used in casting.

Chemical composition of aluminum alloy 2219

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

2219

–

Each

Total

Rem

<0.2

<0.3

5.8-6.8

0.2-0.4

<0.02

–

<0.1

0.002-0.1

<0.05

<0.15

2219
Coating with 7072

<0.7

<0.1

–

0.8-1.3

–

<0.05

<0.15

Rem

Physical properties of 2219 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase
O	172	76	18
T42	359	186	20
T31,T351	359	248	17
T37	393	317	11
T62	414	290	10
T81,T851	455	352	10
T87	476	393	10

PROPERTIES	METRIC	IMPERIAL
Density	2.6-2.8 g/cm3	0.0939- 0.101lb/in³
Melting point	510°C	950°F

Typical mechanical properties of 2219 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
O-2219	73.8	–	543	643	864	22.5	2.84	39	170	44
2219-T31,T37	73.8	–	543	643	864	22.5	2.84	62	116	28
2219-T62,T81,T87	73.8	–	543	643	864	22.5	2.84	57	130	35

PROPERTIES	METRIC	IMPERIAL
Tensile strength	170 MPa	24656 ksi
Yield strength	76 MPa	1022 ksi
Fatigue strength	105 MPa	15229
Elastic modulus	70-80 GPa	10153-11603 ksi
Poisson’s ratio	0.33	0.33
Elongation	18%	18%

Thermal properties of aluminum 2219

PROPERTIES	CONDITIONS
T (ºC)	TREATMENT
Thermal conductivity	170 W / mK	25

Other standards equivalent to 2219 aluminum alloy

Alternative standard names include AlCu6Mn and A92219 , which are described in the following standards:

ASTM B 209 : Standard specifications for aluminum sheets and plates
ASTM B 211 : Standard specifications for aluminum and round sections, rods and wires
ASTM B 221 : Standard specifications for aluminum alloy extruded rods, rods, wires, profiles and pipes
ISO 6361 : Aluminum sheets, straps and plates

Other titles of 2219 Aluminum Alloy include :

AMS 4066	ASTM B211	ASTM B247	MIL A-46808	QQ A-367
AMS 4068	ASTM B221	ASTM B316	MIL A-8920	QQ A-430
ASTM B209	ASTM B241	MIL A-46118	QQ A-250\30	SAE J454

Features of construction and operation of aluminum 2219

Aluminum 2219 can be machined in annealed mode. In heating conditions, this alloy is very difficult to machine. Oil base lubrication is used for machining operations.

shaping

Aluminum 2219 can be formed using conventional techniques.

Welding

To prevent cracking, 2219 aluminum alloy can be welded with great care using welding and gas welding techniques. This process proposed heat treatment in order to maintain the corrosion resistance of this alloy.

Heating

Aluminum 2219 can be heated to 538 degrees Celsius (1000 degrees Celsius) and then immersed in cold water.

Forming

To maintain the corrosion resistance property, 2219 aluminum alloy can be used.

Anil

Aluminum 2219 is annealed at a sufficient time at 538 degrees Celsius (1000 degrees Celsius) and then immersed in cold water.

Temper

Aluminum 2219 can age at 190 degrees Celsius (375 degrees Celsius) for various periods of time after cooking and cooking.

Forging

For forging, it can be tempered for 190 hours at 190 degrees Celsius (375 degrees Fahrenheit) and sheet or plate forms can be tempered at 190 degrees Celsius (375 degrees Celsius) for 36 hours, followed by cooling. Do something in the air.

Properties and usage of aluminum alloy 2219

Aluminum alloy 2219 in particular has a high resistance to breakage, is weldable and is resistant to cracking and stress. Therefore, it is widely used in the skin of supersonic aircraft and structural members. The standard space shuttle weight tank is also made of 2219 alloy. Aluminum 2219 is suitable for making structural parts that are used in high strength welding and high temperature usages.

Usages of aluminum 2219

This alloy is used to build the body of fuel tanks, structural components and shells of supersonic aircraft and.. The welding ability of this alloy is very high and it is suitable for parts that work in the temperature range of -269 degrees Celsius. This alloy has a high fracture toughness and with T8 operation, its crack resistance due to stress corrosion increases.

Properties and usage of 2319 aluminum alloy

Properties and usages Aluminum alloy 2319 with high copper composition is used for high strength aircraft welding wire and truck body usages. 2319 Aluminum Alloy is a malleable alloy that has excellent resistance to cracking and stresses.

This is a filler alloy made for use with 2219 aluminum. Aluminum alloy 2319 has higher strength and better flexibility than 4000 aluminum filler alloys when welding 2000 aluminum alloys. It should not be used for welding 5000 series aluminum alloys. Aluminum 2319 is an aluminum alloy that mainly contains copper (5.8-6.8%) as an alloying element.

It also contains .20% silicon, 0.0% iron, 40.0% manganese 40%, 0.02% magnesium, 0.10% zinc, 0.10-0% titanium. 20%, titanium 0.05-0.15% vanadium, 0.10-0.25% zirconium, 0.0003003% beryllium (in arc welding electrodes) and trace elements up to 0.15%.

The density of 2319 aluminum is 2840 kg / m3. This alloy was first registered in the United States in 1958.

Chemical composition of aluminum alloy 2319

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

2319

Zr : 0.1-0.25V : 0.05-0.150.0008 > Be

Each

Total

Rem

<0.2

<0.3

5.8-6.8

0.2-0.4

<0.02

–

<0.1

0.1-0.2

<0.05

<0.15

Physical properties of 2319 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
O-2319	–	–	543	643	864	22.5	2.83	39	170	44

Mechanical properties of aluminum alloy 2319

The table below shows the physical properties of 2319 aluminum.

PROPERTIES	METRIC	IMPERIAL
Poisson’s ratio	0.33	0.33
Elastic modulus	70-80 GPa	10152-11603ksi

Thermal properties of 2319 aluminum

PROPERTIES	CONDITIONS
T (°C)	TREATMENT
Thermal conductivity	170 W / mK	۲۵	–

The equivalent materials of 2319 aluminum alloy are listed below :

AMS 4191D
AWS A5.10.92
ER 2319
R 2319

Properties and usage of aluminum alloy 2319

This alloy is used to make welding electrodes and fillers for welding metals of alloy 2219. The annealing temperature of this alloy is 413 degrees Celsius. 2319 Aluminum Alloy is used as a welding wire for high strength structural aircraft and truck fuselage usages. This alloy is used to make welding electrodes and fillers for welding metals of alloy 2219. The annealing temperature of this alloy is 413 degrees Celsius.

Properties and usage of aluminum alloy 2618

Properties and usages Aluminum Alloy 2618 is a high-strength aluminum alloy containing copper and magnesium that is used to produce extruded and industrial climbing parts. Aluminum has high flexibility and corrosion resistance. At low temperatures, their resistance can increase. However, their resistance can be reduced at high temperatures of about 200-250 ° C.

Aluminum Alloy 2618A is a high-strength aluminum alloy containing copper and magnesium. Alloy 2618 has good machining and has a fair resistance to weather conditions.

Chemical composition of aluminum alloy 2618

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

2618

Ni : 0.9-1.2

Each

Total

Rem

0.1-0.25

0.9-1.3

1.9-2.7

–

1.3-1.8

–

<0.1

0.04-0.1

<0.05

<0.15

Physical properties of 2618 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
T61-2618	74.4	28	549	638	875	22.3	2.76	47	146	37

Typical mechanical properties of 2618 aluminum alloy

Percentage increase	Surrender strength	Tensile strength	Temperature
12	421	538	-196
10	372	441	-28
10	372	441	25
10	372	427	100
50	62	90	260

Thermal properties of 2618 aluminum alloy

The thermal properties of 2618 aluminum are given in the table below.

SPECIFICATION	METRIC	CONDITIONS
Thermal conductivity (25 ° C / 77 ° F) with T61 treatment	146 W / mK	1013 BTU / hr.ft². ° F

How to make and heat treatment of aluminum 2618

Machining

Aluminum 2618 has good machining properties. It can be operated in heating conditions.

shaping

Aluminum 2618 has the ability to form with hot and cold temperatures.

Welding

Aluminum 2618 can be welded using various methods. Welding is not done using conventional fusion welding methods. Because the heat generated by these methods can be harmful to this alloy.

Heat treatment

Aluminum 2618 can be operated for a sufficient time at 530 ° C (985 ° C) and then immersed in water.

Forming

Aluminum 2618 operates at 372 to 522 degrees Celsius (700 to 970 degrees Celsius).

Heatability

Aluminum 2618 can be operated by heating at 350 to 372 degrees Celsius (660 to 700 degrees Celsius).

Anil

Annealing of 2618 aluminum can be done at 385 ° C (725 ° C) for 4 hours. It can then be gently cooled in the oven.

Temper

Aluminum 2618 can be tempered at 527 ° C (980 ° C) for 24 hours and then immersed in boiling water. The heat treatment process can be repeated at 199 ° C (390 ° C) for 20 hours, followed by cooling in air.

Properties and usages of 2618 aluminum alloy

2618A Aluminum Alloy (2618 Aluminum) is available in plates, strips, rods, sheets, forgings and tubes.
2618A Aluminum (2618 Aluminum) Alloy is commonly used in aerospace and defense components.
This aluminum is mainly used in the manufacture of aircraft engines.

Usages of 2618 aluminum alloy

This material is commonly used for pistons and rotating parts of aircraft due to its ability to work in higher temperature usages. Forging parts, pistons and aircraft engine rotating parts that operate at high temperatures are some of the usages of this alloy.

3000 series of aluminum alloys

The 3000 series aluminum alloy is composed of two main elements, aluminum and manganese, which are stronger than the 1000 aluminum alloy series. This series of aluminum alloys has properties that can be called high tensile strength, high ductility, excellent corrosion resistance, high plastic area and good weldability.

This series of alloys can be used in the manufacture of food cans, in the manufacture of vehicle radiators, in the manufacture of chemical equipment and in the manufacture of roofs.

Properties and usage of 3003 aluminum alloy

Aluminum alloy 3003, which is one of the most widely used types of aluminum. This alloy is from the series of 3000 alloys, all of which use manganese as their main alloying element, and is considered one of the best all-purpose aluminum alloys.

3003 is an alloy in the 3000 series aluminum family and is made mostly of manganese. Like other manganese-aluminum alloys, the 3003 is an all-purpose alloy with moderate strength, good performance and good corrosion resistance. Products are usually rolled and extruded with this alloy. Aluminum alloys have high flexibility and corrosion resistance. The strength of this alloy can be increased by cooling .

Alloy 3004 is commonly used in the manufacture of beverage cans. The use of this alloy is due to the thin thickness of the can. It can be made thinner by adding 1% magnesium.

Chemical composition of aluminum alloy 3003

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

3003

–

Each

Total

Rem

<0.6

<0.7

0.05-0.2

1-1.5

–

<0.1

–

<0.05

<0.15

3003

Coating with 7072

<0.7

<0.1

–

<0.05

<0.15

Rem

Physical properties of 3003 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
3003-O	70	25	643	645	893	23.2	2.73	34	193	50
3003-H12	70	25	643	645	893	23.2	2.73	41	163	42
3003-H14	70	25	643	645	893	23.2	2.73	42	159	41
3003-H18	70	25	643	645	893	23.2	2.73	43.1	155	40

Aluminum alloys vary depending on the type and percentage of their alloying elements. Alloys with <4% alloying elements are called “workable alloys”. While those up to 22% are “cast” alloys. Type 3003 aluminum is an aluminum alloy with a nominal content of 0.12% copper, 1.2% manganese and 98.6% Al.

Note that these percentages vary slightly depending on how the aluminum alloy is made, and other impurities are in normal amounts.

Aluminum is relatively simple in composition, mainly because only a certain amount of manganese can be successfully added to aluminum (1.5 ~ M manganese) to make an alloy. The density of 3003 aluminum is 2.73 grams per cubic centimeter (0.0986 pounds per inch).

Typical mechanical properties of 3003 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase	Hardship	shear strength	Fatigue strength
O	110	42	30-40	28	76	48
H12	130	125	10-20	35	83	55
H14	180	145	8-16	40	97	62
H16	175	175	5-14	47	105	69
H18	200	185	4-10	55	110	69

When determining 3003 aluminum, certain criteria such as ultimate strength, shear strength, modulus of elasticity and shear modulus must be known. As previously explained, all mechanical values are taken from 3003-H18 aluminum alloy. But its strength values vary slightly based on the hardening process. The expected efficiencies and strengths are necessary to determine the aluminum analysis and show the maximum stress at certain points in the deformation process.

Tensile strength for 3003 aluminum alloys is 186 MPa (27000 psi) and final strength 200 MPa (29000 psi), which makes 3003 aluminum a relatively strong material. More performance strength is used. Because it defines the maximum amount of stress before deformation, which is a necessary limitation for static usages such as structures, architecture, etc.

3003 aluminum sheet shear strength

3003 Aluminum alloy is usually cut from sheet metal, especially for cases subject to shear stresses. As the scissor blades approach, two opposing forces increase along the flat surface of the paper, and the shear forces deform or “cut” the paper. Cutting sheet metal works the same way as cutting paper, but with much heavier machines than scissors and aluminum foil instead of paper.

Measuring the tensile strength of a material against shear strength is called shear strength, and it is very valuable to know alloys that can be used as sheet metal such as 3003 aluminum. For 3003 aluminum alloy, the shear strength is 110 MPa (16,000 psi), which means that it can be easily cut to any shape.

The response of matter to specific stresses (or forces at some points) is defined by its elastic modulus and shear modulus. These values are calculated from experimental stress tests, where increasing stress and its physical effect on a piece of alloy are recorded on the stress-strain curve.

The modulus of elasticity and the shear modulus are just the slope of these diagrams in the elastic region, or the region where the aluminum piece deforms permanently (think of it as a rubber band, where the material returns to its original state).

This slope is a measure of a material’s resistance to deformation and can be useful for a general understanding of a material’s strength. For 3003 aluminum, the modulus of elasticity and shear modulus is 68.9 GPa (10,000 ksi) and 25 GPa 3630 (ksi).

Thermal properties of 3003 aluminum

The thermal properties of 3003 aluminum alloy are given in the table below.

PROPERTIES	CONDITIONS
T (ºC)	TREATMENT
Thermal expansion co-efficient	۲۳٫۲ (۱۰^-۶/ºC)	۲۰-۱۰۰	–
Thermal conductivity	۱۶۲ W / mK	۲۵	H12

Equivalent names of aluminum 3003

Other names equivalent to 3003 aluminum are listed in the table below.

ASME SFA5.3 (E3003)	ASTM B234	ASTM B345	AWS A5.3 (E3003)	QQ A-200/1
ASTM B209	ASTM B241	ASTM B404	MIL A-52174	QQ A-225/2
ASTM B210	ASTM B247	ASTM B483	MIL E-15597 (MIL-3003)	QQ A-250/2
ASTM B211	ASTM B313	ASTM B491	MIL P-25995	QQ A-430
ASTM B221	ASTM B316	ASTM B547	MIL S-12875	QQ WW-T-700/2
SAE J454

Manufacture and heat treatment of aluminum 3003

Machining

Aluminum 3003 has good machining properties.

Formation

Aluminum 3003 can be modeled using conventional heating method or cold working method.

Welding

Aluminum 3003 has good welding.

Heat treatment

Aluminum 3003 does not respond to heat treatment and is not suitable for this purpose.

Forming

Aluminum 3003 can be formed at a temperature of 260 to 510 degrees Celsius (500 to 950 degrees Celsius).

Heating

Aluminum 3003 heats up at 260 to 510 degrees Celsius (500 to 950 degrees Fahrenheit).

Cooling

Aluminum 3003 can be cooled using all conventional techniques.

Anil

3003 aluminum alloy is annealed at 413 ° C (775 ° C).

Properties and usage of 3003 aluminum alloy

The body of soda cans, storage and handling equipment for chemicals, building structures, fluorescent lamp bodies, and also in similar cases where good ductility and higher strength than 3003 alloy is required, this alloy is used. Alklad 3004 is used in the construction of side guards of water canals and coating and roofing industries.

Usages of Aluminum Alloy 3003

Aluminum 3003 is used in factories, chemical equipment and general metal work. Also used in making the following:

Cooking utensils
Pressure Vessels
Ice cube trays
Gas lines
Garage doors
Refrigerator panels
Heat Exchangers
Gasoline tanks
Storage tanks
All kinds of stretched and rotated parts

Properties and usage of 3004 aluminum alloy

Aluminum alloys have high corrosion resistance. Their strength decreases when exposed to high temperatures. However, their strength can increase at groundwater temperatures. Aluminum Alloy / Aluminum 3004 Alloy contains manganese and magnesium .

3004 Aluminum Alloy An alloy made in the manganese aluminum family (3000 or 3XX series). This is similar to the 3003 alloy, except for the addition of approximately 1. magnesium. It is usually rolled and extruded. But it is not normally fake. Not used as a wrought alloy in casting.

Alloy 3004 is commonly used in the manufacture of beverage cans. This is done to meet the need for thinner gauges available in cans. In this way, it partially replaces its previous 3003 alloy in the manufacture of beverage cans. Existing stock of magnesium, which strengthens the solid solution, can make existing stocks thinner.

Chemical composition of aluminum alloy 3004

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

3004

–

Each

Total

Rem

<0.3

<0.7

<0.25

1-1.5

0.8-1.3

–

<0.25

–

<0.05

<0.15

3004
Coating with 7072

<0.7

<0.1

–

0.8-1.3

–

<0.05

<0.15

Rem

Physical properties of 3004 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
3004-O	70	25	629	654	893	23.2	2.72	41	162	42

Typical mechanical properties of 3004 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase	Hardship	shear strength	Fatigue strength
O	180	69	20-25	45	110	97
H32	218	170	10-17	52	115	105
H34	240	200	9-12	63	125	105
H36	260	230	۵-۹	70	140	110
H38	285	250	4-6	77	145	110

Other titles and names of Aluminum Alloy 3004

Alternative names include 3,526 and A93004. 3004 Aluminum and its various temperatures are discussed in the following standards:

ASTM B 209 : Standard specifications of aluminum and aluminum-alloy sheets and plates
ASTM B 221 : Standard Specifications for Aluminum and Aluminum – Alloy of Extruded Rods, Rods, Wires, Profiles and Tubes
ASTM B 547 : Standard Specifications of Aluminum and Aluminum Tube – Alloy and Round Tube Electric Arc
ISO 6361 : Sheets, strips and plates are made of aluminum and aluminum.
ASTM B221
ASTM B313
ASTM B548
SAE J454

Manufacture and heat treatment of aluminum 3004

Machining

Aluminum / aluminum alloy 3004 has good machinability in terms of hardness. Oil lubricant is used for machining operations.

Shaping

Aluminum 3004 can be formed using conventional hot or cold working methods.

Welding

Aluminum 3004 can be welded using TIG or MIG welding techniques.

Heat treatment

Aluminum 3004 is not a heat treatable alloy.

Forming

Aluminum 3004 is formed at different temperatures from 372 to 510 degrees Celsius (700 to 950 degrees Celsius).

Heating

Aluminum 3004 is heated to 260 to 483 degrees Celsius (500 to 900 degrees Celsius).

Cooling

Aluminum / Aluminum 3004 Alloy can be cooled up to 75% by reducing conventional area using conventional techniques. If it is cold beyond 75% area reduction, this process should be followed after the operation.

Anil

Aluminum 3004 is annealed at 344 ° C (650 ° C) and then cooled in air.

Properties and usage of 3004 aluminum alloy

Aluminum 3004 is used in worksheets. It is also used in the construction of storage tanks.

Properties and usage of 3005 aluminum alloy

Aluminum alloy 3005 belongs to the 3000 series aluminum, which is mainly composed of the element manganese as other alloys. This is a common alloy with rust resistance. The most common use of 3000 series aluminum or manganese aluminum alloy, which are 3003, 3004, 3005, 3103 and 3105 alloys are used in large quantities in the construction industry.

3000 series aluminum has good elongation, corrosion resistance, good processing performance and can be melted and rolled according to different needs. 3000 series aluminum alloys offer a wide range of mechanical properties with excellent corrosion resistance, welding and ductility.

Chemical composition of aluminum alloy 3005

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

3005

–

Each

Total

Rem

<0.6

<0.7

<0.3

1-1.5

0.2-0.6

<0.1

<0.25

<0.1

<0.05

<0.15

Physical Properties of Aluminum Alloy 3005

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
3005-O	69.5	26.2	635	655	891	23.1	2.73	34	190	50.5

Typical mechanical properties of 3005 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase
O	135	60	29

Thermal properties of aluminum 3005

Thermal properties of 3005-T14 aluminum alloy are shown in the table below.

PROPERTIES	METRIC	IMPERIAL
Thermal expansion co-efficient (@20-100°C/68-212°F)	m/m°C	13.3µin/in°F
Thermal conductivity	160W / mK	1110BTU in/hr.ft².°F

Heat treatment of aluminum 3005

Heat treatment of 3005 aluminum sheet has :

Properties and usage of aluminum alloy 3005

3005 aluminum alloy has high strength and good corrosion resistance. Common 3005 aluminum alloy products include :

Aluminum sheet 3005
Aluminum coil 3005
Aluminum strap 3005

Aluminum sheet 3005 is not only used in air conditioning, refrigerators, vehicles and other humid environments. Non-ferrous aluminum is also commonly used in building materials.

Usages of aluminum alloy 3005

3005 aluminum alloy has the ability to form, weldability and corrosion resistance. Used for processing parts that require good ductility, high corrosion resistance, good weldability, or both properties and higher strength than 1000 series aluminum alloys.

Kitchenware
Food and chemical processing storage devices
Liquid tanks
Various pressure vessels and pipes for general processing
Public radiators
Furniture
False Ceiling
Insulation

Properties and usages of 3103 aluminum alloy

Aluminum is a soft and light metal that has good electrical conductivity and also has sound absorption, stress absorption and anti-corrosion properties. Aluminum 3103 is not a brittle alloy with the possibility of heat treatment, but it has very good welding capability.

Chemical composition of aluminum alloy 3103

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

3103

Zr + Ti <0.1

Each

Total

Rem

<0.5

<0.7

<0.1

0.9-1.5

<0.3

<0.1

<0.2

–

<0.05

<0.15

Physical properties of 3103 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
3103-O	69.5	26.1	640	655	892	23.1	2.73	34	190	50.5

Typical mechanical properties of 3103 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase	Hardship	shear strength
O	105	45	24	29	70

Thermal properties of aluminum 3103

The thermal properties of 3103 aluminum are shown in the table below.

PROPERTIES	METRIC	IMPERIAL
Thermal conductivity	160W / mK	1109BTU in/hr.ft².°F

Equivalent materials of aluminum alloy 3103 are listed below :

Alcoa-190
BA 60
BS N3
Aluman-100
GB-3S alkane

How to make aluminum 3103

Weldability – Gas : Very good
Weldability – Arc : Very good
Weldability – Resistance : Good
Capability : Very good
Efficiency – Cold : Good
Machineability : Acceptable
Welding capability : 3103 alloy has very good welding capability
Aluminum 3103 has good performance against cold.
It has excellent soldering ability.
The performance of this alloy is acceptable.

Alloy naming

Aluminum 3103 conforms to the following standard specifications and specifications but is not a direct equivalent: ISO Al Mn1.

Types of production

Alloy 3103-H14 is usually made of sheet metal.

Types of heat treatment

The most common aluminum for 3103 aluminum are: H14 – Hard work by hard rolling does not anneal after spinning.

Properties and usage of 3103 aluminum alloy

Type 3003 aluminum is the most popular aluminum alloy due to its medium strength, good performance and good corrosion resistance. This material is excellent in many usages and is known as a “general use” alloy. For this reason, not all 3003 aluminum usages can be covered, but some common uses include:

Heat Exchangers
Weather condition evaporators
Aircraft and military parts
Radiators for motor vehicles
Freezer body
office Equipment
Pipes and plumbing
Pressure Vessels
fuel tanks
Chemical equipment
Properties and usage of 3105 aluminum alloy

Aluminum alloy 3105 has 98% pure aluminum. It has high corrosion resistance and good weldability and workability.

Chemical composition of aluminum alloy 3105

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

3105

–

Each

Total

Rem

<0.6

<0.7

<0.3

0.3-0.8

0.2-0.8

<0.2

<0.4

<0.1

<0.05

<0.15

Physical properties of 3105 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
3105-O	69	25	638	657	897	23.6	2.71	38.3	173	45

Mechanical properties of 3105 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	shear strength	Percentage increase
O	115	55	83	24
H12	150	130	97	7
H14	170	150	105	5
H16	195	170	110	4
H18	215	195	115	3
H25	180	160	105	8

Typical mechanical properties of 3105 alloy sheet These properties are typically described and are obtained in different modes of production, for example, stretched sheet or extruded tube or changes in it in different thicknesses.

Thermal properties of aluminum 3105

The thermal properties of 3105 aluminum alloy are given in the table below .

PROPERTIES	METRIC	IMPERIAL
Thermal conductivity (@25°C/77°F)	173W / mK	1201BTU in/hr.ft².°F

Another name for the equivalent of 3105 aluminum is ASTM B209 . Aluminum alloy 3105 has moderate properties for machining. However, machining it can be enhanced at harder tempers than heating conditions. Oil lubricants are used to machine this alloy.

Formation of 3105 aluminum alloy

This alloy has good shape forming properties. It is recommended that the bending radius be heated to a thickness of up to 2 tons at H12, H14 and H16. A bending radius of 2 to 7 tons should be used for H18 cooling.

Welding of aluminum alloy 3105

This alloy has good weldability properties and can be welded using arc welding.

Aluminum annealing

Aluminum 3105 alloy is cooled to 344 ° C (650 F) and then cooled in air.

usage of 3105 aluminum alloy

This alloy is used in the construction of awnings and window sills, movable sheets, capsule bodies, water studs, bottle caps and.. Its annealing temperature is 343 degrees Celsius.

4000 series of aluminum alloys

4000 series of aluminum alloys consist of two main elements, aluminum and silicon, which have a low melting point, which makes these alloys can be used in casting

The characteristics of this series of aluminum alloys include their heat resistance (by adding Mg element to it, this property can be added to some extent), medium strength and corrosion resistance. This series of alloys can be used as welding and soldering wires

Properties and usage of 4032 aluminum alloy

Properties and usages of 4032 aluminum alloy in the manufacture of forging parts, pistons and other high temperature parts. Aluminum alloys are known to be highly resistant to corrosion. These alloys are sensitive to high temperatures between 200 and 250 degrees Celsius (392 and 482 degrees Celsius) and tend to lose some of their strength.

However, the strength of aluminum alloys can be increased at low temperatures, making them ideal low-temperature alloys. Aluminum alloy 4032 is a flexible alloy.

Chemical composition of aluminum alloy 4032

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

4032

Ni : 0.05-1.3

Each

Total

Rem

11-13.5

0.5-1.3

–

0.8-1.3

<0.1

<0.25

–

<0.05

<0.15

Physical properties of 4032 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
4032-O	70	26	532	571	864	19.5	2.68	43.1	155	40
4032-T6	70	26	532	571	864	19.5	2.68	47.9	141	36

Typical mechanical properties of 4032 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	shear strength	Percentage increase	Hardship
-100	415	325	–	10	–
-300	385	315	–	9	–
25	380	315	110	9	120
100	345	300	–	9	–
200	90	62	–	30	–
300	38	24	–	70	–
400	21	12	–	90	–

Thermal properties of 4032 aluminum alloy

The thermal properties of 4032 aluminum alloy can be seen in the table below.

PROPERTIES	CONDITIONS
T (ºC)	TREATMENT
Thermal conductivity	155W / mK	25	O
Thermal expansion	19.4 x 10^-6/ºC	20-100	–

Equivalent names of aluminum 4032

ASTM B247
QQ A-367
SAE J454

Manufacturing and heat treatment of 4032 aluminum alloy

Machining

The efficiency of 4032 aluminum alloy is reasonable in terms of price. Machining should be done using lubricating oils.

Shaping

Aluminum 4032 is a forged alloy and can be formed using hot die forging.

Welding

Aluminum 4032 is weldable and the recommended method is the inert gas arc welding method. Gas welding method is not suitable.

Heat treatment

Heat treatment of 4032 aluminum solution at 510 ° C (950 ° F) for 1 to 12 hours depending on the thickness of the section.

forging

Since 4032 aluminum alloy is a forging alloy, forging can be easily done in the range of 510 to 371 ° C to 950 to 700 degrees.

Cooling

4032 aluminum alloy is not suitable for this.

Anil

To ensure complete heating, 4032 aluminum can be made at 413 ° C (775 ° C) and then the alloy can be controlled in a controlled manner at 10 ° C (50 ° F to 204 ° C (400 ° C). Finally, it is eventually cooled by air.

Temper

Aluminum 4032 is cooled with cold water by heating the solution to 510 ° C (950 ° C), heating to 171 ° C (340 ° F) for 10 hours, and finally cooling the air to tempe ( T6 degrees Celsius).

Properties and usages of 4032 aluminum alloy

Aluminum 4032 is widely used in the manufacture of pistons. This alloy is used in the manufacture of forging parts, pistons and other parts used at high temperatures, where shrinkage and expansion are important properties. For hot work, this alloy should be brought to a temperature of 480-316 degrees Celsius.

Properties and usage of 4043 aluminum alloy

This alloy is used in the preparation of metal fillers for welding and welding of casting and rolling alloys. Aluminum is used in several different industries and its list is growing every year. Aluminum alloy 4043 is a malleable and malleable alloy with good corrosion resistance.

Chemical composition of aluminum alloy 4043

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

4043

–

Each

Total

Rem

4.5

<0.8

<0.3

<0.05

–

<0.1

<0.2

<0.05

<0.15

Physical properties of 4043 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
4043-O	–	–	575	630	962	22	2.668	41	–	42

Typical mechanical properties of 4043 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Wire diameter (mm)	Percentage increase
H16	205	180	5	1.7
H14	170	165	3.2	1.3
H18	285	270	1.6	0.5
H16	200	185	1.2	0.4
O	130	50	5	25
O	115	55	3.2	31
O	145	65	1.6	22
O	110	55	1.2	29

Thermal properties of 4043 aluminum

The thermal properties of 4043 aluminum alloy can be seen in the table below :

PROPERTIES	METRIC	IMPERIAL
Thermal expansion co-efficient (average over 20-100°C/68-212°F)	m/m°C	12.3µin/in°F
Thermal conductivity	163W / mK	1130BTU in/hr.ft².°F

Other names equivalent to 4043 aluminum

BS N21
MIL-W-6712
Alcan GB-33S
Duricilium-FD
star-Si-050
AWCO-45

Properties and usages of 4043 aluminum alloy

The general usage of this alloy is in the preparation of welding metal fillers for welding all types of casting and rolling alloys, except alloys containing high magnesium. The annealing temperature of this alloy is 350 degrees Celsius.

5000 series of aluminum alloys

The 5000 series aluminum alloys have two main elements, aluminum and magnesium , which can increase the hardness of this series of aluminum alloys by performing cold plastic deformation processes

Features of this series of aluminum alloys include high strength, high corrosion resistance, good weldability, resistance to very low temperatures even near absolute zero, high resistance in environments including SO2, HNO3, H2SO4 and H3PO4, Noted softness and low density

This series of aluminum alloys can be used in the construction of fuel and food tanks, electrical connections, construction of missile parts, construction of hulls of boats and ships, and so on

Properties and usage of 5005 aluminum alloy

Aluminum alloy 5005 has a nominal magnesium content of 0.8%. It has medium strength, good weldability and good corrosion resistance in marine atmospheres.
It also has low density and excellent thermal conductivity for all common aluminum alloys. This alloy is the most common type of aluminum in the form of sheets and plates . Aluminum Alloy 5005 is a magnesium alloy that can be hardened by cooling.

Chemical composition of aluminum alloy 5005

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

5005

–

Each

Total

Rem

<0.3

<0.7

<0.3

<0.2

0.5-1.1

<0.1

<0.25

–

<0.05

<0.15

Physical properties of 5005 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
5005-O	68.2	25.9	632	652	900	23.7	2.7	33.2	205	52

Typical mechanical properties of 5005 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase (1) and (2)	Hardship	shear strength
O	124	41	25	28	76
H12	138	131	10	–	97
H14	159	152	6	–	97
H16	179	172	5	–	103
H18	200	193	4	–	116
H32	138	117	11	36	97
H34	159	138	8	41	97
H36	179	165	6	46	103
H38	200	180	5	51	110

Corrosion resistance of 5005 aluminum alloy

Corrosion resistance 5005 has a high resistance to general corrosion and other aluminum alloys do not. It also has higher resistance to the low alkaline conditions common in 5000 series alloys. Corrosion resistance in weather conditions 5005 is similar to 3003.

When anodized to improve corrosion resistance, it is clearer at 5005 than 3003 and gives a better color architecture with 6063 extrusion. Because aluminum is a reactive metal, it can corrode faster when electrically exposed to most other metals. Predicting galvanic corrosion is complex.

Welding of aluminum alloy 5005

Welding 5005 can be welded with standard methods. It is often welded with GTAW (TIG) or GMAW (MIG). To prevent contamination and weld porosity, aluminum must be very dry and clean. Weld filler metals 1100, 4043 or 4047 are used. 4043 has a high tolerance. The gas shield must be dry and free of hydrogen.

Properties and usages of 5005 aluminum alloy

Aluminum 5005 can be prepared by conventional methods. To prevent thermal distortion, the workpiece must be machined at high speed with high lubrication. Sharp tools are essential. High speed steel or tungsten carbide may be used. The cuts must be deep and continuous and have a high cutting speed. Some of the usages of this alloy include the following:

building industry
General sheets
High strength foil
Properties and usage of 5050 aluminum alloy

5050 Aluminum is a 5000 series aluminum alloy. In addition, its main alloy is magnesium and is formulated for initial formation in various products. In European standards, it is given as EN AW-5050. A95050 is a UNS number. In addition, the chemical determination of EN AlMg is 1.5 (C).

Aluminum alloys have excellent corrosion resistance. They are sensitive to high temperatures of 200 to 250 degrees Celsius (392 to 482 degrees Fahrenheit) and can lose some of their strength. However, the strength of aluminum alloys can be increased at very low temperatures, making them ideal low-temperature alloys.

Chemical composition of 5050 aluminum alloy

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

5050

–

Each

Total

Rem

<0.4

<0.7

<0.2

<0.1

1.1-1.8

<0.1

<0.25

–

<0.05

<0.15

Physical properties of 5050 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
5050-H38, O	68.9	25.9	627	652	900	23.8	2.7	34	191	50

Typical mechanical properties of 5050 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase	Hardship	shear strength	Fatigue strength
O	145	55	24	36	105	83
H32	170	145	9	46	115	90
H34	190	165	8	53	123	90
H36	205	180	7	58	130	97
H38	220	200	6	63	138	97

The equivalent materials of 5050 aluminum alloy are as follows :

ASTM B209
ASTM B210
ASTM B313
ASTM B483
ASTM B547
ASTM B548
SAE J454

Production and heat treatment of 5050 aluminum

Machining

The efficiency of 5050 aluminum is very suitable, especially in annealing conditions. However, under cooling conditions, the machining capability is much better than the annealed material. Lubricants should be used when machining.

Shaping

The ductility of 5050 aluminum alloy in the form of annealed or H32 is excellent.

Welding

Welding of these alloys can be done easily using all methods.

Heating

Heating can be done in 5050 aluminum alloy at 371 to 204 degrees Celsius (700 to 400 degrees Celsius).

Cooling

The cooling capacity of 5050 aluminum alloy is excellent, especially in the cooling form.

Anilling

Aluminum 5050 can be made at a suitable time with 343 degrees Celsius (650 degrees Fahrenheit) to ensure complete heating and then cooled in air.

Properties and usage of 5050 aluminum alloy

Aluminum 5050 is widely used in the manufacture of coil sheets, refrigerators and appliances.

Properties and usage of 5052 aluminum alloy

Aluminum alloys have strong corrosion resistance. They are sensitive to high temperatures between 200 and 250 ° C (392-482 ° F) and may lose some of their strength. However, the strength and rigidity of this aluminum alloy can be increased at lower temperatures and they are referred to as desirable alloys at low temperatures. Aluminum 5052 Alloy is a heat-removable alloy with good corrosion resistance, especially to brine.

Chemical composition of aluminum alloy 5052

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

5052

–

Each

Total

Rem

<0.25

<0.4

<0.1

2.2-2.8

0.15-0.35

<0.1

–

<0.05

<0.15

Physical properties of aluminum alloy 5052

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
5052-H38, O	69.3	25.9	607	649	900	23.8	2.68	49.3	137	35

Mechanical properties of aluminum alloy 5052

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase		Hardship	shear strength	Fatigue strength
Type of heat treatment	Tensile strength	Surrender strength	Diameter 1.6 mm	Diameter 12.5 mm	Hardship	shear strength	Fatigue strength
O	195	90	25	27	47	125	110
H32	230	195	12	16	60	140	115
H34	260	215	10	12	68	145	125
H36	275	240	8	9	73	160	130
H38	290	255	7	7	77	165	140

Typical mechanical properties of 5052 alloy These properties are typically described and are obtained in different modes of production, for example, stretched sheet or extruded tube or changes in it in different thicknesses.

Mechanical properties of 5052 aluminum sheet

Type of heat treatment	Tensile strength (ksi)	Efficiency (ksi)	Stretching ٪ in 2 “	Minimum bending radius (90 degree cold formation)
5052-O	25-31	9.5	19	0
5052-H32	31-38	23	7	1T
5052-H34	34-41	26	6	1.2 1T

Alloy heat treatment conditions 5052

The annealing temperature of this alloy is 343 degrees Celsius without maintenance at this temperature and its working temperature is 510-260 degrees Celsius.

PROPERTIES	CONDITIONS
T (ºC)	TREATMENT
Thermal conductivity	137W / mK	25	H38
Thermal expansion	23.8 x 10^-6/°C	20-100	–

Other designations of aluminum alloy 5052

AMS 4004	AMS 4017	AMS 4175	AMS 4178	AMS 4348	ASTM B209
ASTM B210	ASTM B211	ASTM B221	ASTM B234	ASTM B241	ASTM B313
ASTM B316	ASTM B404	ASTM B483	ASTM B547	ASTM B548	MIL C-26094
MIL G-18014	MIL S-12875	QQ A-225/7	QQ A-250/8	QQ A-430	QQ WW-T-700/4

Production conditions and heat treatment

Machining 5052

Aluminum Alloy 5052 is excellent and versatile. This alloy can be easily used in hard dough than in neutral form and its quality is better. Except for very small reductions, all other machining must be done using oil lubricants.

Shaping of aluminum alloy 5052

Aluminum 5052 alloy can be easily formed at room temperature. However, continuous ceramic work tends to reduce the ductility of the alloy.

Welding conditions of aluminum alloy 5052

Welding can be easily done on aluminum / aluminum 5052 using conventional methods. If a filler bar is needed, 5356 aluminum should be used as a filler. The most suitable welding methods are arc welding with tungsten or consumable gas electrode.

Conditions for forging aluminum alloy 5052

Aluminum 5052 can range from 510 ° C (950 ° F) to 260 ° C (500 ° F).

Analyzing conditions of aluminum alloy 5052

Aluminum 5052 can be cooled to 343 ° C (650 ° F) and then cooled by air.

Usage of 5052 aluminum alloy

This alloy is used in the following cases as well as in cases where corrosion resistance with good ductility, high weldability and medium static strength is required.

Manufacture of aircraft oil and fuel pipes
Fuel tanks
Marine usages and transportation
sheet
Street lighting lamps
Wire and rivet
Properties and usage of 5056 aluminum alloy

This alloy is used to produce sheets and wires. 5056 Aluminum is a 5000 series aluminum alloy, its main alloy is magnesium and is formulated to produce a variety of products. 5056 is the name of the Aluminum Association (AA) for this material. In European standards, it is given as EN AW-5056. A95056 is a UNS number. This material can have the highest flexibility and the highest tensile strength among 5000 series alloys.

Chemical composition of aluminum alloy 5056

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

5056

–

Each

Total

Rem

<0.3

<0.4

<0.5

0.05-0.2

4.5-5.6

<0.2

<0.1

–

<0.05

<0.15

the cover

–

<0.5

<0.1

–

1-1.5

0.15-0.35

1.6-2.4

–

<0.05

<0.15

Rem

Mechanical properties of 5056 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase		Hardship	shear strength	Fatigue strength
			۱	۲
O	290	152	35		65	179	138
H18	434	407	10		105	234	152
H38	414	345	15		100	221	152

Similar alloys 5056

5088 : O, AlMg5Mn0.4
5182 : AlMg4.5Mn0.4, A95182
5082 : AlMg4.5, 3.3345
5083 : AlMg4.5Mn0.7, 3.3547, N8, A95083
5019 : AlMg5, 3.3555, A95019
5456 : AlMg5Mn1, A95456

Properties and usage of aluminum alloy 5056

This alloy is used to make consumable rivets for magnesium alloys, cable covers, rivets, zippers and wires with high corrosion resistance. Alklad wire is also widely used in the manufacture of insect repellent plates and other functions where similar wires with good corrosion resistance are required.

Properties and usage of 5083 aluminum alloy

Aluminum 5083 is known for exceptional performance in harsh environments. Aluminum 5083 is highly resistant to seawater and industrial chemical environments. Aluminum 5083 also has exceptional post-welding strength. This alloy has the highest strength of non-refractory alloys but is not recommended for use at temperatures above 65 ° C.

Chemical composition of aluminum alloy 5083

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

5083

–

Each

Total

Rem

<0.4

<0.1

0.4-1

4-4.9

0.05-0.25

<0.25

–

<0.05

<0.15

Mechanical properties of aluminum alloy 5083

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase
O	290	145	22
H112	303	193	16
H116	317	228	16
H321	317	228	16
H32,H232	324	248	10
H34,H343	345	283	9

Mechanical properties for 5083 Soft O / H111 aluminum alloy

BS EN 485-2:2008 PLATE 6.3MM TO 80MM
PROPERTY	VALUE
Proof Stress	115 Min MPa
Tensile Strength	270-345 MPa
Hardness Brinell	75HB

Mechanical properties for 5083 Soft O / H111 aluminum alloy

BS EN 485-2:2008 PLATE 80MM TO 120MM
PROPERTY	VALUE
Proof Stress	110Min MPa
Tensile Strength	260Min MPa
Hardness Brinell	70HB
Elongation A	12Min%

Mechanical properties for 5083 H32 aluminum alloy

BS EN 485-2:2008 SHEET 0.2MM TO 6.00MM
PROPERTY	VALUE
Proof Stress	215Min MPa
Tensile Strength	305-380MPa
Hardness Brinell	89HB

Physical properties of aluminum alloy 5083

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
5083-F	70.3	26.4	574	638	900	24.2	2.66	59.5	120	29

Physical properties of 5083 aluminum

PROPERTY	VALUE
Density	2650kg/m³
Melting Point	570°C
Modulus of Elasticity	72GPa
Electrical Resistivity	0.058×10^-6 Ω.m
Thermal Conductivity	121W/m.K
Thermal Expansion	25×10^-6 /K

Naming of alloys

Al Mg4.5Mn0.7
AlMg4.5Mn
GM41
A95083

Manufacture of 5083 aluminum alloy

Welding conditions of aluminum alloy 5083

When welding 5083 aluminum to itself or another alloy of the same subgroup, the recommended filler metal is 5183. Other suitable fillers are 5356 and 5556.

5083 aluminum production method

This table shows how the 5083 alloy reacts.

PROCESS	RATING
Workability – Cold	Average
Machinability	Poor
Weldability – Gas	Average
Weldability – Arc	Excellent
Weldability – Resistance	Excellent
Brazability	Poor
Solderability	Poor

Alloy heat treatment conditions 5083

The annealing temperature of this alloy is 413 degrees Celsius without maintenance at this temperature and its working temperature is 482-316 degrees Celsius.

Temper Aluminum 5083

The most common materials for 5083 aluminum are :

O
H111 – Some work hardening by shaping processes, but less is required.
H32

Usages of aluminum 5083

Shipbuilding
Rail wagons
Car body
Truck body
Pressure Vessels

In air, marine, automotive, television towers, pressure vessels that have not been heat-welded, as well as in vehicles, space military components, plates, and in cases where corrosion resistance is required with moderate strength, this alloy Used. This alloy is also used to make parts that need to work at low temperatures.

Properties and usage of 5086 aluminum alloy

5086 is an alloy of aluminum, which is primarily composed of magnesium. It is not reinforced by heat, but by stronger strain or cold mechanical work. Because heat treatment does not severely affect strength, the 5086 can be easily welded and retains much of its mechanical strength. Good results with good welding and corrosion properties in seawater make the 5086 very popular for ship runways, boats and yachts.

Aluminum alloys have high corrosion resistance and electrical conductivity properties. These alloys are sensitive to high temperatures between 200 and 250 degrees Celsius (392 and 482 degrees Celsius) and tend to lose their strength. This alloy performs well at low temperatures and withstands very low temperatures. 5086 Aluminum Alloy is a high strength structural alloy.

Chemical composition of aluminum alloy 5086

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

5086

–

Each

Total

Rem

<0.4

<0.5

–

0.2-0.7

3.5-4.5

–

<0.25

<0.15

<0.05

<0.15

Physical properties of 5086 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
5086-F	71	26.4	585	640	900	23.8	2.66	56	127	31

Typical mechanical properties of 5086 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase
O	260	115	22
H116,H32	290	205	12
H34	335	225	10
H112	270	130	14

Other names equivalent to 5086 aluminum

ASTM B209	ASTM B210	ASTM B221	ASTM B241	ASTM B313
ASTM B345	ASTM B361	ASTM B547	ASTM B548	MIL C-26094
MIL S-24149/2	QQ A-200/5	QQ A-250/7	SAE J454	QQ WW-T-700/5

How to make and heat treatment of aluminum 5086

Anil

Aluminum 5086 is annealed at 343 ° C (650 ° C) and then cooled in air.

Cooling

Aluminum 5086 has excellent performance characteristics at O temperature and lower temperatures 38 H38 and H36.

Welding

Conventional methods are suitable for welding 5086 aluminum / aluminum alloy. Excellent results can be obtained when electric arc welding is used for this alloy.

Shaping

Aluminum 5086 has excellent forming properties at temperature O and less properties at temperatures H38 and H36.

Machining

Aluminum 5086 has good machining properties in H38, H36 and H34.

hard working

Aluminum 5086 can only be hardened by cooling.

Heat treatment

The thermal properties of 5086 aluminum alloy are given in the table below.

PROPERTIES	CONDITIONS
T (ºC)	TREATMENT
Thermal expansion	23.9 (10^-6/ºC)	20-100	–
Thermal conductivity	127 (W / mK)	25	All

Properties and usages of 5086 aluminum alloy

Aluminum 5086 is used in missile components, non-welded pressure vessels, aerosols, television towers, drilling rigs, transportation equipment, tanks and offshore components. This alloy is used in the manufacture of various parts in the aerospace, marine and automotive industries, parts used in the refrigeration industry and parts that operate at low temperatures.

TV antennas, means of transportation, as well as items that require good welding capability and corrosion resistance with medium strength, are other uses of this alloy.

Properties and usages of 5154 aluminum alloy

Aluminum Alloy 5154 is an alloy in the magnesium aluminum family (5000 or 5xx series). As a magnesium-aluminum alloy, it combines medium to high strength with excellent welding. Aluminum 5154 is commonly used in welded structures such as pressure vessels and ships. As a malleable alloy, it can be produced by rolling and extrusion but is not suitable for casting.

Aluminum alloys have strong corrosion resistance. These alloys are sensitive to high temperatures between 200 and 250 degrees Celsius (392 and 482 degrees Celsius) and tend to lose some of their strength. However, the strength of aluminum alloys can be increased at sub-zero temperatures, making them ideal low-temperature alloys.

Alternative names of alloy 5154

Alternative names 5154 include AlMg3.5, N5 and A95154. The alloy and its various temperatures are covered under the following standards :

ASTM B 209 : Standard specifications for aluminum sheets and plates
ASTM B 210 : Standard specifications for extruded seamless pipes
ASTM B 211 : Standard specifications for wire, round and aluminum wire
ASTM B 221 : Standard specifications for aluminum alloy extruded rods, rods, wires, profiles and pipes
ASTM B 547 : Standard specifications for aluminum pipes and rounds
ISO 6361 : Sheets, belts and plates

Chemical composition of aluminum alloy 5154

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

5154

–

Each

Total

Rem

<0.25

<0.4

<0.1

3.1-3.9

0.15-0.35

<0.2

<0.05

<0.15

Physical properties of aluminum alloy 5154

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
5154-F	69.3	25.9	593	643	900	23.9	2.66	53.9	127	32

Typical mechanical properties of 5154 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase	Hardship	shear strength	Fatigue strength
O	240	117	27	58	152	117
H32	270	207	15	67	152	124
H34	290	228	13	73	165	131
H36	310	248	12	78	179	138
H38	330	269	10	80	193	145
H119	240	117	۲۵	63	–	117

Properties and usage of aluminum alloy 5154

This alloy is used in the construction of welded structures, storage and storage tanks, pressure vessels, offshore structures and material handling tanks. Aluminum 5154 is widely used in the construction of welded structures, storage tanks and pressure vessels. It is also used in salt water service.

Properties and usages of 5182 aluminum alloy

5000 series aluminum alloys are mainly used as sheets or plates, but they can also be produced by extrusion. Aluminum alloy 5182 is a flexible alloy with good corrosion resistance. Welding capability and corrosion resistance of 5182 aluminum alloy are considered desirable.

Chemical composition of aluminum alloy 5182

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

5182

–

Each

Total

Rem

<0.2

<0.35

<0.15

0.2-0.5

4-5

<0.1

<0.25

<0.2

<0.05

<0.15

Physical properties of aluminum alloy 5182

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
5182-F	69.6	26.5	577	638	904	24.1	2.65	55.6	123	31

Properties and usage of aluminum alloy 5182

This alloy is used to make sheets for the body of tanks and containers, panels and reinforcing components in cars, as well as reinforcing members of the base and cantilever parts of the car. Its annealing temperature is 343 degrees Celsius and its working temperature is 510-260 degrees Celsius.

Usages of 5182 aluminum alloy

5182 Aluminum alloy is widely used to make car bodies and brackets due to its strength, flexibility and weldability.

Properties and usages of 5252 aluminum alloy

Aluminum 5252 is a 5000 series aluminum alloy. The main additive is magnesium alloy and is formulated into extrusion products for initial forming. 5252 is the name of the Aluminum Association (AA) for this material. In European standards, it is given as EN AW-5252. A95252 is a UNS number. In addition, the chemical name is EN AlMg2,5 (B).

Chemical composition of aluminum alloy 5252

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

5252

–

Each

Total

Rem

<0.08

<0.1

2.2-2.8

–

<0.05

–

<0.05

<0.15

Physical properties of aluminum alloy 5252

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
5252-F	68.3	–	607	649	900	23.8	2.67	49	138	35

Typical mechanical properties of 5252 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase	Hardship
H25	235	170	11	68
H28,H38	283	240	5	75

Heat treatment conditions of alloy 5252

For annealing, the temperature of this alloy should be raised to 343 degrees Celsius. The work is done on this alloy at a temperature of 510-260 degrees Celsius. The main design features of this is a non-heat-treatable aluminum and magnesium alloy. However, this alloy has moderate strength and also has resistance to atmospheric corrosion as well as excellent ease of construction.

Machining capability

The machining of the AL 5252 is relatively poor compared to other aluminum alloys. The desire to be “chewing gum” is difficult to achieve a good ending. The use of lubricants is recommended during machining.

Shaping

Whether hot or cold, this alloy is excellent.

Welding

All commercial welding methods may be used for this alloy. TIG and / or MIG welding methods are preferred. Soldering is not recommended.

Heat treatment

AL 5252 does not respond to heat treatment. Other than annealing to relieve cold pressure – see “annealing”.

Heating

If necessary, hot work can be easily done in the range of 900 to 500 Fahrenheit.

Anil

Annealing, if required, can be performed at a maximum temperature of 650 ° C, followed by air cooling.

Harden

Cooling hardens (strengthens) this alloy in the form of H. It cannot be hardened by heat treatment.

Usages of aluminum alloy 5252

This alloy is used in automotive and decorative usages that require higher strength properties than other decorative alloys. Glossy and clean surface can be achieved by immersion or anodizing. Products that are commonly used in the manufacture of home appliances and car decorations are made of sheets or sections with this alloy.

Properties and usages of 5254 aluminum alloy

Aluminum is a good low temperature alloy with high electrical conductivity and strong corrosion resistance properties. These alloys are sensitive to high temperatures between 200 and 250 degrees Celsius (392 to 482 degrees Fahrenheit). Aluminum alloys gain strength when exposed to sub-zero temperatures and lose their strength when exposed to high temperatures.

Aluminum 5254 is a 5000 series aluminum alloy. The main additive is magnesium alloy and is formulated into extrusion products for initial forming. 5254 is the name of the Aluminum Association (AA) for this material. In European standards, it is given as EN AW-5254. A95254 is a UNS number.

Chemical composition of aluminum alloy 5254

Alloy name	Ingredients (weight percentage)							consideration	Other elements		AL%
5254	Fe+Si	Cu	Mn	Mg	Cr	Zn	Ti	–	Each	Total	Rem
5254	<0.45	<0.05	<0.01	3.1-3.9	0.15-0.35	<0.2	<0.05	–	<0.05	<0.15	Rem

Physical properties of aluminum alloy 5254

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
5254	69.6	–	593	643	900	24	2.66	54	127	32

Typical mechanical properties of 5254 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase	Hardship	shear strength	Fatigue strength
O	240	115	27	58	150	115
H32	270	205	15	67	150	125
H34	290	230	13	73	165	130
H36	310	250	12	78	180	140
H38	330	270	10	80	195	145
H112	240	115	25	63	–	115

Heat treatment conditions of 5254 alloy : The annealing temperature of this alloy is 343 degrees Celsius without maintenance at this temperature and its working temperature is 510-260 degrees Celsius.

Properties and usages of aluminum alloy 5254

This type of alloy is used for rolling aluminum sheets with different specifications for different usages. In addition, like 5052 alloy, it can be used for extruding sections.

Usages of aluminum alloy 5254

Aluminum alloy 5254 is used in storage tanks for chemicals and hydrogen peroxide.

Properties and usage of aluminum alloy 5356

Aluminum alloy 5356 is an alloy from the magnesium aluminum family (5000 or 5xxx series). Unlike most aluminum and magnesium alloys, this raw material is used as a filler for welding. This grade is one of the most popular aluminum filler alloys along with 4043 alloy. Aluminum 5356 alloy has a relatively high strength but is more vulnerable to cracking. It is a better filler when welding round or butt 6061 aluminum alloy or placing anodized parts.

Chemical composition of aluminum alloy 5356

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

5356

–

Each

Total

Rem

<0.25

<0.4

<0.1

0.05-0.2

4.4-5.5

0.05-0.2

<0.1

0.06-0.2

<0.05

<0.15

To better understand the analysis and ingredients of 5356 alloy, see the following chart :

Physical properties of 5356 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
5356-O	–	–	574	638	904	24.2	2.64	59.4	116	29

Typical mechanical properties of aluminum alloy 5356

BASE ALLOY	UTS (KSI)	UYS (KSI)	ELONG (%)	UTS (KSI)	UYS (KSI)	ELONG (%)
6061-T6-T651	45	40	12	30	19	11
-T6	35	31	12	20	12	12
7005-T6-T63	54	46	12	46	30	10
7039-T64	65	55	13	44	25	13

Parameters of GMAW type aluminum 5356

WIRE DIAMETER	RANGE		BASE MATERIAL THICKNESS	SUGGESTED		WIRE FEED	GAS FLOW	CONSUMPTION FT OF WELD ۱۰۰
INCHES	AMPS	VOLTS	INCHES	AMPS	VOLTS	IPM	CFH	POUNDS
0.030	60-170	13-24	0.062	90	۲۱	350	35	1.5
			0.094	100	۲۲	560		1.8
			0.125	120	۲۲	670		2
			0.187	140	23	780		4
0.035	70-180	15-26	0.062	100	21	350	35	1.5
			0.125	130	22	420		2
			0.250	170	23	640		6
0.047	140-260	20-29	0.094	100	22	150	45	1.8
			0.125	150	23	220		2
			0.250	190	24	320		6
			0.375	220	25	400		16
0.062	190-350	25-30	0.250	200	23	200	55	6
			0.375	230	24	220		16
			0.500	260	26	270		30
			0.750	280	27	300		50
			1.000	300	28	320		105
0.094	280-400	26-31	>1.000	350	30	180	60	+150

Heat treatment conditions of alloy 5356

The annealing temperature of this alloy is 343 degrees Celsius without the need for maintenance at this temperature and its hot working temperature is 510-260 degrees Celsius.

Properties and usage of 5356 aluminum alloy

The 5XXX alloy base material, welded with AL5356, has a chemical for boiling more than 3.% magnesium and a temperature of more than 150 degrees is sensitive to cracking. This alloy is suitable for grades 5050, 5052, 5083, 5086, 5356, 5454 and 5456.

Usages of aluminum grade 5356

This alloy is used to make electrodes and welding fillers for alloys that contain high magnesium. (Above three percent magnesium) is used.

Properties and usage of 5454 aluminum alloy

Aluminum alloys have high corrosion resistance. These alloys are good alloys at low temperatures. Aluminum alloys are sensitive to high temperatures between 200 and 250 ° C (392 and 482). The strength of these alloys increases when exposed to sub-zero temperatures and the resistance to high temperatures decreases.

Chemical composition of aluminum alloy 5454

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

5454

–

Each

Total

Rem

<0.25

<0.4

<0.1

0.05-0.1

2.4-3

0.05-0.2

<0.25

<0.2

<0.05

<0.15

Physical properties of 5454 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
5454-T	69.6	–	602	646	900	23.7	2.68	51	134	34

Typical mechanical properties of 5454 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase	Hardship	shear strength
O	250	117	22	62	159
H32	275	207	10	73	165
H34	305	241	10	81	179
H36	340	276	8	–	–
H38	370	310	8	–	–
H111	260	179	14	70	159
H112	250	124	18	62	159
H311	260	179	18	70	159

Types of heat treatment of aluminum 5454

The most common 5454 aluminum temperaments are shown below :

O : Soft
H111 : Some work is done by shaping hardened processes but is less than required for H11.
H22 : The piece is hardened by rolling and then annealed to a hard quarter.
H32 : The product is hardened by rolling and then stabilized by heat treatment at low temperatures up to a quarter hard.

Equivalent names of 5454 aluminum standards

ASTM B209
ASTM B221
ASTM B234
ASTM B241
ASTM B404
ASTM B547
ASTM B548
QQ A-200/6
QQ A250 / 10
SAE J454

Fabrication and heat treatment of 5454 aluminum alloy

Annealing

Aluminum 5454 can be annealed only at 343 ° C (maximum 650 ° C) if you need to relieve cold work stress. After heating enough, the alloy eventually cools in air.

Cooling

Aluminum 5454 is able to cool using conventional methods. This alloy can be worked in any of H-32, H-34, H-111 or in cold working conditions.

Welding

Aluminum 5454 is capable of welding with all welding methods.

Blacksmithing

Aluminum 5454 can be heated.

Machining capability

Machining of 5454 aluminum is rated as average to poor. Machining operations for this alloy are recommended when the alloy is in H-34 condition. Oil lubricants can be used in the machining process.

Heating

Aluminum 5454 can be heated in the temperature range of 371 to 204 degrees Celsius (700 to 400 degrees Celsius).

Work Hardening

Aluminum 5454 is hardened only by cold work.

Properties and usage of 5454 aluminum alloy

The strength of medium to high alloy is similar to 5754 with good strength in the temperature range of 65 to 170 degrees Celsius. It has high fatigue power. Not suitable for complex or fine extrusion. 5454 aluminum alloy has excellent corrosion resistance. Especially against seawater and general environmental conditions

Usages of aluminum alloy 5454

The body of various equipment in the road transport industry
Pressure tanks, containers, boilers
Manufacture of refrigeration equipment
Columns, beams and masts of the sea
Properties and usage of 5456 aluminum alloy

Aluminum alloys are highly resistant to corrosion. They are sensitive to high temperatures between 200 and 250 degrees Celsius (392 to 482 degrees Celsius) and can lose some of their strength. However, the strength of aluminum alloys can be increased at sub-zero temperatures. 5456 aluminum alloy has good strength and is useful for making structures due to its weldable properties.

Chemical composition of aluminum alloy 5456

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

5456

–

Each

Total

Rem

<0.25

<0.4

<0.1

0.5-1

4.7-5.5

0.05-0.2

<0.25

<0.2

<0.05

<0.15

The equivalent materials of 5456 aluminum alloy are as follows :

ASTM B209
ASTM B210
ASTM B221
ASTM B241
ASTM B548
MIL S-24149/2
QQ A-200/7
QQ A250/9
SAE J454

Physical properties of 5456 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
5456-F	70.3	–	571	638	900	23.9	2.66	59.5	116	29

Typical mechanical properties of 5456 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase
O	310	159	24
H111	324	228	18
H112	310	165	22

Heat treatment conditions of 5456 alloy

The annealing temperature of this alloy is 343 degrees Celsius without maintenance at this temperature and its working temperature is 510-260 degrees Celsius.

Machining capability

5456 aluminum alloy has poor machinability. If machining, oil and carbide lubricants should be used.

Shaping

The ductility of 5456 aluminum alloy is more difficult than other aluminum alloys. It should not be too cold.

Welding

Arc welding is preferred for 5456 aluminum alloy. Therefore, it has useful structural usages. Gas welding can also be used but the results are not as good as arc welding.

Heating

The 5456 aluminum alloy can be preheated to 218 ° C (425 ° C). This will help you work out the effects of high stress on completely cold shapes.

Cooling

Aluminum alloy 5456 has a good cold working capacity, but you should avoid excessive work due to cold (reduction of more than 20%). Because when the temperature reaches 66 degrees Celsius (150 degrees Fahrenheit), it causes stress cracking.

Annealing

Annealing of 5456 aluminum alloy can be done at 343 ° C (maximum 650 ° C). This should be followed by air cooling.

Work hardening

5456 aluminum alloy can only be hardened by cold (limited) work.

Properties and usages of 5456 aluminum alloy

Marine industries
High strength welded structures
Pressure Vessels
This alloy is also used in storage tanks.
Properties and usage of 5457 aluminum alloy

Aluminum alloys are highly resistant to corrosion. They are sensitive to high temperatures between 200 and 250 degrees Celsius (392 to 482 degrees Celsius) and tend to lose some of their strength. However, the strength of aluminum alloys can increase at sub-zero temperatures. Therefore, they are suitable for low temperatures.

Aluminum 5457 is a 5000 series aluminum alloy. The main additive is magnesium alloy and is formulated into extrusion products for initial forming. In European standards, it is given as EN AW-5457. A95457 is a UNS number.

5457-H25 Aluminum
5457-H28 Aluminum
5457-H38 Aluminum
5457-O Aluminum

Chemical composition of aluminum alloy 5457

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

5457

V<0.05

Each

Total

Rem

<0.08

<0.1

<0.2

0.15-0.45

0.08-1.2

–

<0.05

–

<0.03

<0.1

Physical properties of 5457 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
5457-F	68.2	25.9	629	645	900	23.7	2.69	37.5	177	46

Typical mechanical properties of 5457 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase	Hardship	shear strength
O	130	50	22	32	85
H25	180	160	12	48	110
H28,H38	2055	185	6	55	125

Properties and usages of 5457 aluminum alloy

The most important usage of this alloy is in decorative and anodized parts in cars.

Properties and usage of 5652 aluminum alloy

5000 series aluminum alloys have excellent corrosion resistance and welding ability. Aluminum alloy 5652 is made of working alloys. Aluminum 5652 is a 5000 series aluminum alloy. The main additive is magnesium alloy and is formulated for pre-formed products. 5652 is the name of the Aluminum Association (AA) for this material. By European standards, it is referred to as EN AW-5652. A95652 is a UNS number.

Chemical composition of aluminum alloy 5652

Alloy name	Ingredients (weight percentage)							consideration	Other elements		AL%
5652	Fe+Si	Cu	Mn	Mg	Cr	Zn	Ti	–	Each	Total	Rem
5652	<0.4	<0.04	<0.01	2.2-2.8	0.15-0.35	<0.1	–	–	<0.05	<0.15	Rem

Among the aluminum alloys used, the composition of 5652 aluminum is significant due to its relatively high amount of magnesium. Magnesium is hardenable and increases through heat treatment and hard mechanisms. It also increases susceptibility to intergranular corrosion.

Physical properties of aluminum alloy 5652

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
5652	68.2	25.9	607	649	900	23.8	2.68	49	137	35

Typical mechanical properties of 5652 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase	Hardship	shear strength	Fatigue strength
O	195	90	25	47	124	110
H32	230	195	12	60	138	117
H34	260	215	10	68	145	124
H36	275	240	8	73	158	131
H38	290	255	7	77	165	138

Alloys equivalent to 5652

5052 AlMg2.5, 3.3523, A95052) Aluminum)	5021 Aluminum
5052 AlMg2Mn0.3, 3.3525, N4, A95251) Aluminum)	5251 (AlMg2Mn0.3, 3.3525, N4)
5051 A (AlMg2(B), 3.3326) AluminumAluminum	5049 (AlMg2Mn0.8, 3.3527, A95049)

Heat treatment conditions of alloy 5652

Annealing of this alloy at a temperature of 343 degrees Celsius, without the need to maintain at this temperature and its hot work is done at a temperature of 510-260 degrees Celsius.

Properties and usages of 5652 aluminum alloy

This alloy is used to make storage tanks for hydrogen peroxide as well as other chemicals.

Properties and usage of 5657 aluminum alloy

Aluminum alloys have high corrosion resistance. They are sensitive to high temperatures between 200 and 250 degrees Celsius (392 to 482 degrees Celsius) and may lose some of their strength. Aluminum Alloy 5657 is an alloy with heat treatment capability and medium strength.

Chemical composition of aluminum alloy 5657

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

5657

V<0.05Ga<0.03

Each

Total

Rem

<0.08

<0.1

<0.03

0.06-0.1

–

<0.05

–

<0.02

<0.05

Physical properties of aluminum alloy 5657

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
5657	68.2	25.9	638	657	900	23.7	2.69	32	–	54

Typical mechanical properties of 5657 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase	Hardship
H25	160	140	12	40
H28,H38	195	165	7	50

The equivalent materials of 5657 aluminum alloy are as follows :

ASTM B209
SAE J454

Manufacture and heat treatment of 5657 aluminum alloy

Machining capability

5657 aluminum alloy turning is evaluated as good. This alloy can meet the rat’s expectations as soon as it becomes the final product. Apart from very little machining, machining should be done using oil lubricants.

Shaping

With the formation of 5657 aluminum alloy using conventional methods, hot and cold forming is easily done. However, in more difficult conditions, working in the cold is quite difficult.

Welding

5657 alloy can be welded using conventional methods. Widely used methods are electric arc and gas welding.
It is suitable to use AL 5457, AL 5056 or AL5052 as a welding filler metal. This alloy can also be joined together by welding. However, this requires special processes and experimental evaluation.

Forging

5657 aluminum alloy can be forged.

Heating

Heating can be easily done on 5657 aluminum alloy in the temperature range of 371 to 232 degrees Celsius (700 to 450 degrees Celsius).

Cooling

Aluminum 5657 alloy can be cooled by conventional methods.

Annealing

Annealing is mainly done to obtain O using a refrigerant. This process is performed at a temperature of 413 degrees Celsius (775 degrees Celsius) and the air is cooled. Annealing can be done at 238 ° C (460 ° C) for 3 hours followed by air cooling.

work hardening

Aluminum 5657 only hardens with cold work.

Properties and usage of 5657 aluminum alloy

5657 Aluminum Alloy is widely used in the manufacture of home appliances with anodized coating.

6000 series of aluminum alloys

The 6000 series of aluminum alloys are composed of the main alloying elements of aluminum, magnesium and silicon . Features of this series of alloys include medium strength, high softness, high corrosion resistance in marine environments, good weldability and high ductility

This series of aluminum alloys can be used in the automotive, shipbuilding, recycling, construction, architecture and bridge industries

Properties and usages of 6005 aluminum alloy

The 6005 / 6005A alloy has properties between 6061 and 6082 alloys and can sometimes be used instead with these alloys. But 6005 / 6005A has better extrusion specifications. It has a better mill surface, but it is difficult to produce complex thin-walled shapes at 6005 / 6005A.

Chemical composition of aluminum alloy 6005

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

6005

–

Each

Total

Rem

0.6-0.9

<0.35

<0.1

0.4-0.6

<0.1

<0.05

<0.15

Physical Properties of Aluminum Alloy 6005

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
6005-T5	69	–	607	645	–	23.4	2.7	40	167	49

Typical mechanical properties of aluminum alloy 6005

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase	Hardship
T1	172	103	16	–
T5	262	241	8-10	95

Mechanical properties of 6005 T6 aluminum alloy

PROPERTY	SIZE
Density	215 Min MPa
Tensile strength	260 Min MPa
Hardness (Brinell)	85 HB
Elongation	8 Min%

Aluminum alloy 6005 also complies with the following specifications and standards :

A96005
AlSiMg
AlSiMg

Manufacture of aluminum alloy 6005

Welding

The 6005 / 6005A welding capability is excellent. 4043 alloy welding wire is recommended unless the desired piece is 7XXX series alloy, in which case 5356 wire is the recommended option.

temper

As 6005 / 6005A is usually supplied as a tube or extruded. Its most common temperament is T5. This temperament indicates that the material has been cooled from high temperatures for the forming process and then artificially aged.

Properties and usages of 6005 aluminum alloy

6005 and 6005A are used in complex extrusion and products that require more strength than 6060 and 6063.

Pipes for home furniture
Rail and bus transportation structures
Columns, platforms and pipelines
Portable folding ladders
Properties and usage of aluminum alloy 6009

Interest in aluminum alloys and aluminum joining the automotive industry has grown significantly over the past few years, resulting in fuel savings, air pollution, and safety requirements. Alcoa 6009-T4 and 6010-T4 alloys were introduced and introduced in 1976 to enhance the attractiveness of aluminum for body sheet components. Aluminum alloy 6009 is a good alloy with good corrosion resistance.

Chemical composition of aluminum alloy 6009

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

6009

–

Each

Total

Rem

0.6-1

<0.5

0.15-0.6

0.2-0.8

0.4-0.8

<0.1

<0.25

<0.1

<0.05

<0.15

Physical Properties of Aluminum Alloy 6009

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
6009-O	69	25.4	560	650	897	23.4	2.71	31.9	205	54
6009-T4	69	25.4	560	650	897	23.4	2.71	39.2	172	44
6009-T6	69	25.4	560	650	897	23.4	2.71	36.7	180	47

Typical mechanical properties of 6009 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase
T4	234	131	24
T6	345	324	12

Properties and usage of Aluminum Alloy 6009

Aluminum is the best choice for steel to build light and fuel efficient vehicles. Several aluminum alloys are provided to cover the car body. These alloys have good ductility under the received conditions and superior tensile strength (T6) that can be achieved during production periods.

In addition, 6009/6010 alloys provide improved welding properties through a combination of better metallurgical properties and low and uniform surface strength. The weldability, workability and corrosion resistance of this alloy are very good and it has a good anodizing effect. It is used as a sheet in the body of cars.

Properties and usage of 6010 aluminum alloy

Aluminum alloys are known for their high corrosion resistance. They are sensitive to high temperatures and can lose some of their strength.
However, the strength of aluminum alloys can be improved at sub-zero temperatures. Therefore, they are known as suitable alloys in low pressure.

Chemical composition of aluminum alloy 6010

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

6010

–

Each

Total

Rem

0.8-1.2

<0.5

0.15-0.6

0.2-0.8

0.8-1

<0.1

<0.25

<0.1

<0.05

<0.15

Physical properties of 6010 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
6010-O	69	25.4	585	649	897	24.1	2.7	32.5	202	53
6010-T4	69	25.4	585	649	897	24.1	2.7	44.2	151	39
6010-T6	69	25.4	585	649	897	24.1	2.7	39.2	180	44

Typical mechanical properties of 6010 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase
T4	296	186	23
T6	386	372	11

Heat treatment properties of 6010 aluminum alloy

Properties		T (°C)	Treatment
Thermal conductivity	202 W / mK	25	–

Typical mechanical properties of car body sheet made of 6010 alloy

These properties are typically stated and are produced in different modes of production, for example stretched sheet or extruded tube or in different thicknesses.

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase
T4	296	186	23
T6	386	372	11

Heat treatment conditions of 6010 aluminum alloy

Temperature (Celsius)	Type of heat treatment
566	Liquidation
177	T6
413	Anilling

Properties and usages of 6010 aluminum alloy

The most common use of this alloy is in the form of sheets in the car body .

Properties and usage of 6061 aluminum alloy

6061 aluminum alloy is sensitive to high temperature. This alloy tends to lose some of its strength when exposed to high temperatures of around 200-250 ° C. However, their strength can be increased at lower temperatures. They also have good corrosion resistance. 6061 Aluminum Alloy is the most available and heat usable alloy.

Chemical composition of aluminum alloy 6061

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

6061

–

Each

Total

Rem

0.4-0.8

<0.7

0.15-0.4

<0.15

0.8-1.2

0.04-0.35

<0.25

<0.15

<0.05

<0.15

Alclad 6061Coating with 7072

Si + Fe
0.7>

<0.1

–

0.8-1.3

–

<0.05

<0.15

Rem

Physical properties of 6061 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
6061-O	68.3	–	582	652	896	23.6	2.7	37	180	47
6061-T4, T451	68.3	–	582	652	896	23.6	2.7	43	154	40
6061-T6,T651	68.3	–	582	652	896	23.6	2.7	40	167	43

Mechanical properties of 6061 aluminum alloy

Alloy name	Type of heat treatment	Tensile strength	Surrender strength	Percentage increase		Hardship	shear strength	Fatigue strength
Alloy name	Type of heat treatment	Tensile strength	Surrender strength	Diameter 1.6 mm	Diameter 1.6 mm	Hardship	shear strength	Fatigue strength
2024	O	۱۲۴	۵۵	۲۵	۳۰	۳۰	۸۳	۶۲
	T4, T451	۲۴۱	۱۴۵	۲۲	۲۵	۶۵	۱۶۵	۷
	T6,T651	۳۱۰	۲۷۶	۱۲	۱۷	۹۵	۲۰۷	۹۷
Alclad 2024	O	۱۱۷	۴۸	۲۵	–	–	۷۶	–
	T4, T451	۲۲۸	۱۳۱	۲۲	–	–	۱۵۲	–
	T6,T651	۲۹۰	۲۵۵	۱۲	–	–	۱۸۶	–

Heat treatment of 6061 aluminum alloy

PROPERTIES	CONDITIONS
T (ºC)	TREATMENT
Thermal expansion co-efficient	23.4 (10^-6/ºC)	20-100	–
Thermal conductivity	180 W / mK	25	–

Other characteristics: Other criteria equivalent to 6061 aluminum alloy are listed in the table below.

AMS 4117	ASTM B247	ASTM B429	DIN 3.3211	MIL G-18014	QQ A-200/8
ASTM B209	ASTM B307	ASTM B483	MIL A-12545	MIL G-18015	QQ A-225/8
ASTM B210	ASTM B313	ASTM B547	MIL A-22771	MIL P-25995	QQ A-250/11
ASTM B211	ASTM B316	ASTM B548	MIL F-17132A	MIL T-7081	QQ A-367
ASTM B221	ASTM B345	ASTM B632	MIL F-18280	MIL W-23351	QQ A-430
ASTM B234	ASTM B361	ASTM F467	MIL F-39000	MIL W-85	QQ WW-T-700/6
ASTM B241	ASTM B404	ASTM F468	MIL F-3922	QQ A-200/16	SAE J454

Manufacture and heat treatment of 6061 aluminum

Machining of alloy 6061

Aluminum 6061 has good machining alloy in harder T 4 and T6. This alloy can be machined in annealing mode.

Forming of aluminum alloy 6061

Aluminum 6061 can be easily formed and work in hot conditions. It has standard methods for doing bending, design and other methods.

Welding of aluminum alloy 6061

Aluminum 6061 has excellent weldability. Thin sections can be welded using the tungsten arc welding technique. Heavier parts can be welded using an electric arc welding method. PVC 4043 wire can be used to achieve a good result, but it affects the properties of T6.

Heat treatment of aluminum 6061

Aluminum 6061 alloy is heated to a temperature of 533 ° C (990 F) for a sufficient time after drying in water. The sediment hardening process can be performed at 160 ° C (320 ° F) for 18 hours followed by cooling. This process is repeated again at 177 ° C (350 F) for 8 hours and then cooled in air.

Annealing

Aluminum 6061 alloy can be made at 775 degrees Fahrenheit for 2 to 3 hours and then by controlled cooling at 10 to 260 degrees Celsius (50 to 500 F) per hour and air cooling.

Aging

Aging of aluminum 6061 alloy can be done at 177 ° C (350 F) for 8 hours. It is then cooled in air.

Usage of 6061 aluminum alloy

This alloy in the form of sheets, profiles, seamless pipes, rods, extruded pipes, in the construction of small boat hulls, trucks, buildings, home appliances, rigs, pipelines (hydraulic systems for oil and gas and condensers) And is used where strong, weldable and corrosion-resistant structures are required.

Properties and usages of 6063 aluminum alloy

6063 Aluminum Alloy is a medium strength alloy commonly referred to as an architectural or structural alloy. This alloy is commonly used in complex extruders. It has a good full surface, high corrosion resistance, is easily suitable for welding and can be easily anodized. Normally available as T6 mode, in T4 mode it has a good formula.

Usage of 6063 aluminum alloy

building industry
extrusion
window frame
Door
Store fittings
Irrigation pipes

Properties and usage of alloy 6063

Good welding capability, corrosion resistance and very good anodizing effect and medium machining capability are the characteristics of this alloy. In the form of wires, rods, pipes, railings, extruded sections and profiles in the construction of doors and windows, building parts, kitchen appliances, irrigation pipes, corrugated sheets for roofing, extruded architectural parts and false ceilings, truck floors and Trailer used.

Determination of 6063 aluminum alloy

6063 / 6063A aluminum alloy also complies with the following specifications and standards:

AA6063	Al Mg0.7Si
GS10	AlMgSi0.5
A-GS	3.32206
ASTM B210	ASTM B221
ASTM B241 (Pipe- Seamless)	ASTM B345 (Pipe- Seamless)
ASTM B361	ASTM B429
ASTM B483	ASTM B491
MIL G-18014	MIL G-18015
MIL P-25995	MIL W-85
QQ A-200/9	SAE J454
UNS A96063	HE19

Chemical composition of aluminum alloy 6063

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

6063

–

Each

Total

Rem

0.2-0.6

<0.35

<0.1

0.45-0.9

<0.1

<0.05

<0.15

Tempers for 6063 aluminum alloy

The most common chemicals for 6063 aluminum are :

Annealed ceramic alloys

T4 – Heat solution looks natural
T6 – Heat treatment and solution solution

Physical properties of 6063 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
6063-O	68.3	25.8	615	655	900	23.4	2.69	30	126	58
6063-T1	68.3	25.8	615	655	900	23.4	2.69	35	112	50
6063-T5	68.3	25.8	615	655	900	23.4	2.69	32	121	55
6063-T6,T83	68.3	25.8	615	655	900	23.4	2.69	33	116	53

Mechanical properties of 6063 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase	Hardship	shear strength
O	150	83	18	43	96.5
T4, T451	360	207	18	90	200
T6,T651	395	359	12	120	234

Mechanical properties for 6063 T4 aluminum alloy :

BS EN 755-2:2008 EXTRUDED ROD AND BAR UP TO 150MM DIA OR A/F
PROPERTY	VALUE
Proof Stress	90 Min MPa
Tensile Strength	150 Min MPa
Elongation A50 mm	10 Min%
Hardness Brinell	50 HB
Elongation A	12 Min%

Mechanical properties for 6063 T6 aluminum alloy :

TO BS EN 755-2: 2008 ROD & BAR UP TO 150MM DIA. & A/F
PROPERTY	VALUE
Proof Stress	170 Min MPa
Tensile Strength	215 Min MPa
Elongation A50 mm	8 Min%
Hardness Brinell	75 HB
Elongation A	10 Min%

Mechanical properties for 6063 T6 aluminum alloy :

TO BS EN 755-2: 2008 ROD & BAR 150MM TO 200MM DIA. & A/F
PROPERTY	VALUE
Proof Stress	160 Min MPa
Tensile Strength	195 Min MPa
Hardness Brinell	75 HB
Elongation A	10 Min%

Mechanical properties for 6063 T6 aluminum alloy :

BS EN 755-2:2008 PROFILES UP TO 10MM WALL THICKNESS
PROPERTY	VALUE
Proof Stress	170 Min MPa
Tensile Strength	215 Min MPa
Elongation A50 mm	6 Min%
Hardness Brinell	75 HB
Elongation A	8 Min%

Mechanical properties for 6063 T6 aluminum alloy :

BS EN 755-2:2008 PROFILES 10MM TO 25MM WALL THICKNESS
PROPERTY	VALUE
Proof Stress	160 Min MPa
Tensile Strength	195 Min MPa
Elongation A50 mm	6 Min%
Hardness Brinell	75 HB
Elongation A	8 Min%

Mechanical properties of 6063A aluminum

Mechanical properties for 6063A T4 aluminum :

BS EN 755-2:2008 ROD AND BAR UP TO 150MM DIA. & A/F
PROPERTY	VALUE
Proof Stress	90 Min MPa
Tensile Strength	150 Min MPa
Elongation A50 mm	10 Min%
Hardness Brinell	50 HB
Elongation A	12 Min%

Mechanical properties for 6063A T4 aluminum :

BS EN 755-2:2008 BAR 150MM TO 200MM DIA. & A/F
PROPERTY	VALUE
Proof Stress	90 Min MPa
Tensile Strength	140 Min MPa
Hardness Brinell	50 HB
Elongation A	10 Min%

Mechanical properties for 6063A T4 aluminum :

BS EN 755-2:2008 TUBE UP TO 10MM WALL THICKNESS
PROPERTY	VALUE
Proof Stress	90 Min MPa
Tensile Strength	150 Min MPa
Elongation A50 mm	10 Min%
Hardness Brinell	50 HB
Elongation A	12 Min%

Mechanical properties for 6063A T4 aluminum :

BS EN 755-2:2008 TUBE 10MM TO 25MM WALL THICKNESS
PROPERTY	VALUE
Proof Stress	90 Min MPa
Tensile Strength	140 Min MPa
Elongation A50 mm	8 Min%
Hardness Brinell	50 HB
Elongation A	10 Min%

Mechanical properties for 6063A T4 aluminum :

BS EN 755-2:2008 PROFILES UP TO 25MM WALL THICKNESS
PROPERTY	VALUE
Proof Stress	90 Min MPa
Tensile Strength	150 Min MPa
Elongation A50 mm	10 Min%
Hardness Brinell	50 HB
Elongation A	12 Min%

Mechanical properties for 6063A T6 aluminum :

BS EN 755-2:2008 ROD AND BAR UP TO 150MM DIA. & A/F
PROPERTY	VALUE
Proof Stress	190 Min MPa
Tensile Strength	230 Min MPa
Elongation A50 mm	5 Min%
Hardness Brinell	80 HB
Elongation A	7 Min%

Mechanical properties for 6063A T6 aluminum :

BS EN 755-2:2008 BAR 150MM TO 200MM DIA. & A/F
PROPERTY	VALUE
Proof Stress	160 Min MPa
Tensile Strength	220 Min MPa
Hardness Brinell	80 HB
Elongation A	7 Min%

Mechanical properties for 6063A T6 aluminum :

BS EN 755-2:2008 TUBE UP TO 25MM WALL THICKNESS
PROPERTY	VALUE
Proof Stress	190 Min MPa
Tensile Strength	230 Min MPa
Elongation A50 mm	5 Min%
Hardness Brinell	80 HB
Elongation A	7 Min%

Mechanical properties for 6063A T6 aluminum :

BS EN 755-2:2008 PROFILES UP TO 10MM WALL THICKNESS
PROPERTY	VALUE
Proof Stress	190 Min MPa
Tensile Strength	230 Min MPa
Elongation A50 mm	5 Min%
Hardness Brinell	80 HB
Elongation A	7 Min%

Mechanical properties for 6063A T6 aluminum :

BS EN 755-2:2008 PROFILES 10MM TO 25MM WALL THICKNESS
PROPERTY	VALUE
Proof Stress	180 Min MPa
Tensile Strength	220 Min MPa
Elongation A50 mm	4 Min%
Hardness Brinell	80 HB
Elongation A	5 Min%

Physical properties of 6063 aluminum

PROPERTY	VALUE
Density	2700 kg/m³
Melting Point	600°C
Modulus of Elasticity	69.5 GPa
Electrical Resistivity	0.035×10^-6 Ω.m
Thermal Conductivity	200 W/m.K
Thermal Expansion	23.5 x 10^-6 /K

Production and manufacturing conditions of 6063 aluminum

Medium machining
Weldability – Excellent gas
Weldability – Excellent arc
Weldability – excellent resistance
Suitable for soldering

Welding conditions of aluminum 6063

6063 is suitable for all common welding methods.
The welding wire should usually be 5183 alloy or 4043 alloy.
Use 4043 alloy when maximum electrical conductivity is required.
Use 5346 alloy for resistance and conductivity and compensate for the weld size to compensate for lower electrical conductivity.

Aluminum extrusion 6063 from alum metal is available in the following forms with purity of T6 :

Quadrilateral or quadrangular
Your cans are empty
Studs
Corner with equal and unequal edge
Straps
Pipe

Aluminum alloy 6063A is a type of 6063 aluminum with more strength but has good surface properties and good anodizing absorber.

Properties and usage of 6066 aluminum alloy

Aluminum 6066 is an aluminum alloy of the 6000 series: there is a significant alloy with magnesium and silicon, and its alloy is formulated for the initial form of wrought iron products. 6066 is the name of the Aluminum Association (AA) for this material. In European standards, it is given as EN AW-6066 . A96066 is a UNS number .

Chemical composition of aluminum alloy 6066

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

6066

–

Each

Total

Rem

0.9-1.8

<0.5

0.7-1.2

0.6-1.1

0.8-1.4

0.4

0.25

<0.2

<0.05

<0.15

Similar alloys 6066

6070 (A96070) Aluminum	6013 (AlMg1Si0.8CuMn, A96013) Aluminum
6110A (AlMg0.9Si0.9MnCu) Aluminum	6110 (6110-T9, A96110) Aluminum
6182 (AlSi1MgZr, A96182) Aluminum	515.0 (515.0-F) Cast Aluminum

Physical properties of 6066 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
6066-O	69	–	563	648	887	23.2	2.71	43	147	40
6066-T6	69	–	563	648	887	23.2	2.71	47	147	37

Typical mechanical properties of 6066 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase	Hardship	shear strength
O	150	83	18	43	96.5
T4, T451	360	207	18	90	200
T6,T651	395	359	12	120	234

6066 alloy heat treatment conditions

Time (hours)	Temperature (Celsius)	Type of heat treatment
–	530	Liquidation
2-3	415	Anilling
8	175	Aging

Other equivalent specifications of 6066 aluminum alloy include ASTM B221.

Anodizing optimization conditions for 6066 aluminum alloy

The AA anodizing process has been performed industrially to improve corrosion resistance. In research, various factors such as (electrolyte concentration, temperature and voltage) affect the thickness and hardness during anodizing AA6066 in sulfuric acid.

Process factors have been modified using the Taguchi method through Experimental Design (DOE). Taguchi method consists of a set of orthogonal factors, signal to sound ratio (S / N), analysis of variance (ANOVA) which was used to determine the optimal level of conditions for anodizing of 6066 aluminum alloy and effect analysis.

Thickness and hardness It was found that the most effective factor in thickness and microhardness is the concentration of electrolyte. The optimization test was performed by Taguchi optimization test and the optimal conditions were determined.

Finally, anodizing was performed on the aluminum sample under optimal conditions and then scanned by SEM. The thickness and micro-hardness obtained under optimal conditions were 25μm and 640Hv, respectively.

Properties and usages of 6066 aluminum alloy

The selection of aluminum alloys suitable for specific usages includes tensile strength, density, softness, ductility, performance, welding ability, corrosion resistance and so on. 6066 aluminum alloy is used in forging and extrusion for welded structures. Extruded or forged parts for structures that are welded together.

Properties and usage of 6070 aluminum alloy

Aluminum 6070 is a 6000 series aluminum alloy. There are significant compounds of this alloy with magnesium and silicon and it is formulated for the initial forming of the processed products. 6070 is the name of the Aluminum Association (AA) for this material. By European standards, it is referred to as EN AW-6070 . A96070 is a UNS number.

Aluminum alloys are very sensitive to high temperatures. When exposed to sub-zero temperatures, their strength can be increased. They have high corrosion resistance and flexibility. Aluminum is a silvery white metal that is very versatile and can be cast in any known shape. Aluminum can be combined with a wide range of elements – copper, magnesium, manganese, silicon and zinc to form aluminum alloys.

Aluminum alloys are known for their high corrosion resistance. They are sensitive to high temperatures and can lose some of their strength. However, the strength of aluminum alloys can be improved at sub-zero temperatures. Aluminum alloy 6010 is made of working alloys .

Chemical composition of 6070 aluminum alloy

Among the aluminum alloys used, the 6070 aluminum alloy is notable for its relatively high amount of silicon (Si). Silicon is used to increase strength at the cost of ductility. It also reduces the melting temperature and increases the fluidity of the alloy.

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

6070

–

Each

Total

Rem

1-1.7

<0.5

0.15-0.4

0.4-1

0.5-1.2

<0.1

<0.25

<0.15

<0.05

<0.15

Physical properties of 6070 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
6070-T6	68	–	566	649	891	–	2.71	39	172	44

Typical mechanical properties of 6070 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase	Hardship	shear strength	Fatigue strength
O	145	69	20	35	97	62
T4	317	172	20	90	206	90
T6	379	352	10	120	234	97

Properties and usages of 6070 aluminum alloy

6070 aluminum alloy is used in the construction of pipelines and heavy welded structures. Welded and busy structures, pipelines, extruded structural parts for cars are examples of usages of this alloy.

Properties and usage of 6101 aluminum alloy

6101-T6 Aluminum 6101 is aluminum in T6 tempera. To achieve this degree, the metal is heat-refined and artificially aged until it meets the requirements of standard mechanical properties. Alloy 6101 Workable alloy is heatable. Alloy 6101 is suitable for usages including medium strength and maximum electrical conductivity.

This alloy is similar to the 6063 alloy but with minor chemical changes that increase the electrical conductivity and have a better usage in this field than the 6063. Aluminum alloy 6101 has good mechanical strength and high electrical conductivity. Although it has less conductivity than 1350 alloy, but it has more resistance. It can be used in making rods, structural profiles, seamless pipes.

Chemical composition of aluminum alloy 6101

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

6101

B<0.06

Each

Total

Rem

0.3-0.7

<0.5

<0.1

<0.3

0.35-0.8

<0.03

<0.1

–

<0.03

<0.1

Physical properties of 6101 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
6101-T6	68.9	–	621	654	895	23.5	2.69	30.2	218	57

Typical mechanical properties of 6101 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase	Hardship	shear strength
-196	296	228	24	–	–
-80	248	207	20	–	–
25	221	193	19	71	138
100	193	172	20	–	–
260	33	23	80	–	–

Heat treatment conditions of alloy 6101

Type of heat treatment	Temperature (Celsius)	Time (hours)
Liquidation	510	1
Old age	117	6-8
Worker	260-510	–

Other items that are equivalent to 6101 aluminum alloy are :

ASTM B317
SAE J454

How to make and heat treatment of aluminum alloy 6101

Machining capability

Aluminum alloy 6101 has good machinability. An oil-based lubricant is used for machining operations. Carbide steel tools can be used to machine this alloy.

Shaping

Aluminum alloy 6101 can be formed using conventional methods.

Welding

Aluminum alloy 6101 can be welded using all standard welding methods. Gas arc welding method is the best method for welding this alloy. The strength of subsequent parts decreases when welding under thermal conditions.

Operating heat

Aluminum alloy 6101 does not react to heat treatment. However, heat treatment can be done by annealing and aging.

Cooling

Aluminum alloy 6101 can be worked in aging or cold baking conditions.

Annealing

Aluminum alloy 6101 is cooled at 413 ° C (775 ° C) for 3 hours and then controlled cooling at 10 to 260 ° C (50-500 ° C) per hour in air. The stress annealing process can be performed after working at 344 ° C (650 ° C) followed by cooling in air.

Aging

Aluminum alloy 6101 can be aged at different temperatures and times based on the finished temperament. For example, T6 can be stored at 177 ° C (350 ° C) for 20 hours, T61 at 227 ° C (440 ° C) for 6 hours, and T63 at 194 ° C (380 ° C) for 19 hours. This is followed by air cooling.

Work hardening

Aluminum alloy 6101 hardens due to cold and aging.

Properties and usages of 6101 aluminum alloy

High strength load buses, conductors, heatsinks and… are examples of usages of this alloy.

Properties and usages of 6151 aluminum alloy

Aluminum alloys are good alloys at low temperatures. Because when they are exposed to sub-zero temperatures, they gain power. They have high electrical conductivity and corrosion resistance properties. These alloys lose their strength when exposed to high temperatures. Aluminum alloys are sensitive to high temperatures between 200 and 250 degrees Celsius (392 to 482 degrees Celsius).

Aluminum 6151 is a 6000 series aluminum alloy. There is a significant alloy with magnesium and silicon, and the alloy is formulated for initial forging wrought iron products. 6151 is the name of the Aluminum Association (AA) for this material. In European standards, it is given as EN AW-6151. In addition, UNS A96151 is another one .

This alloy has been used since 1928. But it only received its standard name in 1954. This alloy can have the lowest ductility among 6000 series alloys.

Chemical composition of aluminum alloy 6151

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

6151

–

Each

Total

Rem

0.6-1.2

<0.1

<0.35

<0.2

0.45-0.8

0.15-0.35

<0.25

<0.15

Among the alloys used, the 6151 aluminum alloy is significant due to its relatively high amounts of silicon (Si) and magnesium (magnesium). Silicon is used to increase strength at the cost of ductility. It also reduces the melting temperature and increases the fluidity of the alloy. Magnesium increases the hardening capability through heat treatment and pressure hardening mechanisms. It also increases susceptibility to intergranular corrosion.

Physical properties of aluminum alloy 6151

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
6151-O	–	–	۵۸۸	۶۴۹	۸۹۵	۲۳	۲٫۷	۳۲	۲۰۵	۵۴
6151-T4	–	–	۵۸۸	۶۴۹	۸۹۵	۲۳	۲٫۷	۴۱	۱۶۳	۴۲
6151-T6	–	–	۵۸۸	۶۴۹	۸۹۵	۲۳	۲٫۷	۳۸	۱۷۵	۴۵

Typical mechanical properties of 6151 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase
-196	295	345	20
-28	240	310	17
24	330	298	17
100	295	275	17
260	45	34	50

Alloy heat treatment conditions 6151

Type of heat treatment	Temperature (Celsius)	Time	How to cool
Anilling	413	2-3 hours	It cools to 260 degrees Celsius at 270 degrees Celsius per hour.
Liquidation	510-525	4 minutes	Ordinary parts in cold water, complex and forged parts in water 65 alb 100 ° C
Aging	165-175	8-12 hours	in the air
Heating	260-480	–	–

Similar alloys 6151

6061 (AlMg1SiCu, 3.3214, H20, A96061) Aluminum	6081 (6081-T6, AlSi0.9MgMn) Aluminum
6351 (AlSi1Mg0.5Mn, A96351) Aluminum	6016 (AlSi1.2Mg0.4, A96016) Aluminum
6005 A (AlSiMg(A), 3.3210) Aluminum	6008 (AlSiMgV, A96008) Aluminum

Properties and usage of aluminum alloy 6151

Aluminum alloy 6151 is used to make forged parts and engine and machine components and items that require forging, good strength and corrosion resistance.

Properties and usages of 6201 aluminum alloy

Aluminum alloys are known for their high corrosion resistance. They are sensitive to high temperatures between 200 and 250 degrees Celsius (392 to 482 degrees Celsius). However, the strength of aluminum alloys can be increased at sub-zero temperatures. Aluminum alloy 6201 is made of working alloys.

Chemical composition of aluminum alloy 6201

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

6201

B<0.06

Each

Total

Rem

0.5-0.95

<0.5

<0.1

<0.03

0.6-0.9

<0.03

<0.1

–

<0.03

<0.1

Physical properties of 6201 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
6201-T81	–	–	607	654	865	23.4	2.69	32	205	54

Typical mechanical properties of 6201 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase
T81	330	310	6

Alloy heat treatment conditions 6201

Type of heat treatment	Temperature (Celsius)	Time (hours)
Liquidation	510	–
Aging	150	4

Properties and usage of aluminum alloy 6201

This alloy is used in the manufacture of rods and wires for high-strength electrical conductors.

Properties and usage of 6205 aluminum alloy

6205 Aluminum Alloy is a good alloy with good corrosion resistance.

Chemical composition of aluminum alloy 6205

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

6205

Zr : 0.05-0.15

Each

Total

Rem

0.6-0.9

<0.7

<0.2

0.05-0.15

0.4-0.6

0.05-0.15

<0.25

<0.15

<0.05

<0.15

Physical properties of 6205 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
6205-T1	–	–	613	645	900	23	2.7	37	172	45
6205-T5	–	–	613	645	900	23	2.7	35	188	49

Heat treatment conditions of alloy 6205

Type of heat treatment	Temperature (Celsius)	Time (hours)
Liquidation	527	–
Aging	177	6

Properties and usage of 6205 aluminum alloy

This alloy is used in the manufacture of sheets, plates and extruded parts that require high impact strength.

Properties and usages of 6262 aluminum alloy

Aluminum alloy 6262 is a heat-treatable and machining alloy. It also has good mechanical strength and corrosion resistance.

Chemical composition of aluminum alloy 6262

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

6262

Bi : 0.4-0.7Pb : 0.4-0.7

Each

Total

Rem

0.4-0.8

<0.7

0.15-0.4

<0.15

0.8-1.2

0.04-0.15

<0.25

<0.15

<0.05

<0.15

Physical properties of aluminum alloy 6262

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
6262-T9	–	–	582	652	–	23.4	2.71	39	172	44

Typical mechanical properties of 6262 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase	Hardship	shear strength
6262-T651	310	276	17	–	–
6242-T9	400	379	10	120	241

The equivalent standards for the 6262 aluminum alloy are :

ASTM B210
ASTM B211
ASTM B221
ASTM B467
ASTM B483
QQ A-225/10
SAE J454

Manufacture and heat treatment of 6262 aluminum alloy

Machining capability

Aluminum alloy 6262 is added with lead and bismuth to improve its machining characteristics. It can be easily lubricated using carbide. Oil lubricant is used for heavy cuts.

Shaping

Aluminum alloy 6262 can be deformed using conventional methods.

Welding

Aluminum alloy 6262 has good welding capability. It can be welded using the soldering process.

Heat treatment

Aluminum alloy 6262 is subjected to heat treatment by aging.

Cooling

The cooling capacity of 6262 aluminum alloy varies with temperature in many common conditions. T6511, T6510, T6 and T651 have medium working capacity in cold. Temper T9 has poor working capacity in cold.

Annealing

Aluminum alloy 6262 is annealed at 538 ° C (1000 ° C) for a sufficient time and then cooled in hot water.

Aging

Aging of 6262 aluminum alloy can be done at a temperature of 340 to 350 degrees for a maximum of 8 to 12 hours to obtain different temperaments. For example: Templates T6 and T62 age for 8 hours to form a cold rod or rod and extrude shapes for 12 hours. Temper T4 and T42 are caused by natural aging at room temperature.

Work hardening

Aluminum alloy 6262 can be hardened by cooling or a combination of aging and cooling.

Alloy heat treatment conditions 6262

Type of heat treatment	Temperature (Celsius)	Time (hours)
Anilling	415	2-4
Liquidation	540	8-12
Aging	170	8-12

The most common temperars for 6262 aluminum alloy are :

T6 – The solution is subjected to heat treatment and artificial aging.
T9 – The solution works under heat treatment, artificial aging and cold.

Properties and usage of aluminum alloy 6262

This alloy is used in the production of screw machines with high stresses that require more corrosion resistance than the 2011 and 2017 alloys. This alloy is used in the manufacture of fittings, nuts, couplings, screw machine products and camera parts.

Usages of aluminum 6262

Bolt fittings
Camera parts
coupling
Marine connections
Hardware fittings and decorative accessories
Oil line fittings
Valves and valve parts
Properties and usages of 6351 aluminum alloy

Aluminum alloys lose their strength when exposed to temperatures of about 200-250 ° C, however, their resistance increases at sub-zero temperatures and they have a high resistance to corrosion.

Chemical composition of aluminum alloy 6351

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

6351

–

Each

Total

Rem

0.7-1.3

<0.5

<0.1

0.4-0.8

–

<0.2

<0.05

<0.15

Aluminum equivalent alloys 6351

Other 6351 aluminum alloys include ASTM B221.

Physical properties of aluminum alloy 6351

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
6351-T6	–	–	555	650	–	32.4	2.71	38	213	46

Typical mechanical properties of 6351 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase	Hardship	shear strength	Fatigue strength
T4	248	152	20	–	–	–
T6	310	283	14	95	200	90
T54	207	138	10	–	–	–

Alloy heat treatment conditions 6351

Type of heat treatment	Temperature (Celsius)	Time (hours)
Anilling	350	4
Liquidation	505	–
Aging	170	6

Properties and usage of aluminum alloy 6351

This alloy is used to make extruded parts used in cars, trains, tubes and pipes to irrigate and move oil and gasoline.

Properties and usage of 6463 aluminum alloy

Aluminum alloy 6463 is a medium strength alloy. This alloy is often known as a decorative alloy for use in decoration and can be anodized and polished to enhance this usage. Anodized, this alloy gives high quality luster, has good machining and is malleable.

Due to its radiance, it is very suitable for the decoration industry and is also used in decorating home appliances, showcases, lighting systems and industrial sizes. The very polished and smooth properties of this alloy are also suitable for use in car trims. The given properties are common and should only be used to compare alloys. Actual values depend on the specifications of the section.

Chemical composition of aluminum alloy 6463

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

6463

–

Each

Total

Rem

0.2-0.6

<0.05

<0.2

<0.05

0.45-0.9

–

<0.05

–

<0.05

<0.15

Physical properties of aluminum alloy 6463

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
6463-T1	–	–	621	654	–	23.4	2.69	34	192	50
6463-T5	–	–	621	654	–	23.4	2.69	31	209	55
6463-T6	–	–	621	654	–	23.4	2.69	33	201	53

Alloys similar to aluminum alloy 6463

Other equivalent specifications of 6463 aluminum alloy include ASTM B221.

Manufacture and heat treatment of 6463 aluminum alloy

Forming	Good
Machining	Good
Welding	Good
Soldering	Good
Anodized coating	Good
Glossy anodizing	very good
Heat treatment	0 F T4 T5 T6

Properties and usage of aluminum alloy 6463

6463 aluminum alloy is mostly used in the manufacture of extruded sections of the decoration and construction industry. 6463 aluminum alloy is commonly used as anodized and extruded or sheet in the lighting industry. This makes this alloy suitable for shop fittings and trims. It is also used for home interiors such as kitchens and bathrooms.

Usages of aluminum alloy 6463

This alloy is used in construction and architecture industries and is used as extruded parts in the automotive industry due to its good appearance and anodized appearance.

7000 series of aluminum alloys

The 7000 series of aluminum alloys are composed of two main elements, aluminum and zinc along with other alloying elements. This series of aluminum alloys has more strength and fatigue resistance than other series of aluminum alloys and also their corrosion resistance and weldability are lower than other aluminum alloys

This series of aluminum alloys is widely used in the aerospace industry. Especially used in parts that require high fatigue resistance

Properties and usage of 7005 aluminum alloy

Aluminum alloy 7005 belongs to the copper-free 7000 series aluminum alloys (Al-Zn-Mg). The main elements of the alloy :

Zinc (close to 4.5)
Magnesium (about 1.4)

Aluminum alloy 7005 hardens like heat 6061 alloy by heat treatment. However, unlike the 6061 alloy, which requires relatively fast and compressed water cooling during heat treatment, the 7005 alloy is sufficient for cooling air.

7005 is an aluminum alloy used in high-strength structures such as bicycles, does not require much heating due to its relative ease of welding. This alloy has a final tensile strength of 350 MPa, a fatigue strength of 150 MPa and a density of 2.78 g / cm³ compared to the final tensile strength of 310 MPa and a fatigue strength of 96.5 MPa and a density of 2.70 g / cm³.

Various forms of AL 7005 include :

۷۰۰۵-O
۷۰۰۵-T5
۷۰۰۵-T53
-T6

Chemical composition of aluminum alloy 7005

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

7005

Zr : 0.08-0.2

Each

Total

Rem

<0.35

<0.4

<0.1

0.2-0.7

1-1.8

0.06-0.2

4-5

0.01-0.06

<0.05

<0.15

Physical properties of 7005 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
7005-O	71	26.9	604	643	875	23.1	2.78	40.1	166	43
7005-T53	71	26.9	604	643	875	23.1	2.78	45.4	148	38
7005-T5	71	26.9	604	643	875	23.1	2.78	49.3	137	35

Typical mechanical properties of 7005 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase	shear strength
O	193	83	20	117
T53	393	345	15	221
T6,T63,T6351	372	317	12	214

Other similar standards for 7005 alloy

The equivalent material is 70000 ASTM B221 aluminum alloy.

Heat treatment conditions of alloy 7005

Annealing temperature 343 ° C, dissolution temperature 399 ° C, for T53 heat treatment, the piece is quenched from the working temperature, then 72 hours naturally aged at room temperature, then in two stages, for 8 hours at 110-110 ° C. Celsius and then stored for 16 hours at 155-145 degrees Celsius.

Properties and usages of 7005 aluminum alloy

Extruded building structures such as frames, scaffolding, chassis frames, truck door reinforcement columns, trailers and fast vehicles, as well as in cases where high-solder components with high strength and fracture toughness are required. Like large heat exchangers, this alloy is used. Sports equipment such as tennis rackets and softball sticks are also made of this alloy.

Properties and usage of 7049 aluminum alloy

Aluminum alloys have excellent corrosion resistance. They are sensitive to high temperatures in the range of 200 to 250 degrees Celsius (392 to 482 degrees Fahrenheit) and can lose some of their strength. However, the strength of aluminum alloys can be increased at sub-zero temperatures. 7049 aluminum alloy has excellent resistance to cracking and stress.

Chemical composition of aluminum alloy 7049

Among the alloys used, the combination of 7049 aluminum is significant due to its relatively high amounts of zinc and copper. Zinc is used to achieve a significant increase in strength by increasing the susceptibility to cracking under pressure. This includes limiting weldability. Copper is used to improve strength. This is to reduce corrosion resistance and weldability.

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

7049

–

Each

Total

Rem

<0.25

<0.35

1.2-1.9

<0.2

2-2.9

0.1-0.22

7.2-8.2

<0.1

<0.05

<0.15

Physical properties of 7049 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
7049	70	27.6	477	627	960	23.4	2.82	43	154	38

Typical mechanical properties of 7049 aluminum alloy

The table below shows the mechanical properties of 7049 aluminum.

Mechanical properties	the amount of
The power of proof	517 MPa
Performance power	448 MPa
Shear strength	303 MPa
Elongation A50 mm	%12
Modulus of elasticity	71.7 GPa

Manufacture and heat treatment of 7049 aluminum alloy

Machining capability

Machining of 7049 aluminum alloy is especially evaluated in good heat treatment mode. But lubricants should be used when machining.

Shaping

Ductility of 7049 aluminum alloy is done by hot forming.

Heat treatment

Heat treatment of the solution can be performed on 7049 aluminum alloy at 468 ° C (875 ° F) for a certain period of time to ensure complete heating. This is then done by cutting off the water. Alloy 7049 can be aged after heat treatment.

Modeability

7049 aluminum alloy is formed from 438 degrees Celsius (820 degrees Fahrenheit) to 382 degrees Celsius (720 degrees Fahrenheit).

Heating

7049 aluminum alloy can be heated from 438 degrees Celsius (820 degrees Fahrenheit) to 382 degrees Celsius (720 degrees Fahrenheit).

Aging

Aging or hardening of the sediment can be done for 7049 aluminum alloy in a two-step heat treatment process.

Step 1 : Allow the product to stay at room temperature, then cool for 12 hours at 121 ° C (250 ° F) and finally cool.
Step 2 : A 14-hour aging process is performed at 160 degrees Celsius (320 degrees Fahrenheit) followed by air cooling for 14 hours.

Properties and usages of 7049 aluminum alloy

7049 aluminum alloy is mainly used in structural forging, especially in the missile or aerospace industries.

Usages of 7049 aluminum alloy

Forged joints in aircraft and missiles, extruded profiles, landing gear cylinders , as well as in cases where static strength equal to forged parts of 7079-T6 alloy and resistant to stress corrosion are required, of these Alloy is used. The fatigue properties of this alloy are equal to 7075-T6 alloy, but the toughness (toughness) of this alloy is higher.

Properties and usage of 7050 aluminum alloy

Aluminum alloy 7050 is a heat-treatable alloy. It has high strength, strong mechanical resistance and corrosion and pressure resistance. 7050 aluminum alloy used in aerospace industry, which has high strength, corrosion resistance and pressure. This alloy is especially suitable for heavy plate usages (thickness 3 “to 6”) because it has a lower subsidence sensitivity and retains strength in thicker sections. Therefore, 7050 aluminum is in aerospace for various uses such as body structure and wing shell.

The 7050 aluminum plate is available in two temperaments :

T7651 or AMS 4201 has the highest resistance with peeling corrosion resistance and medium SCC resistance.
The T7451 or AMS 4050 provides better SCC resistance and excellent peeling resistance at slightly lower resistance levels.

7050 Alloy Aluminum Plates are the main option for aerospace usages, especially in the 3-6 inch thickness range. Corrosion resistance properties are better than older 7075 alloy.

Because it is less sensitive to aerospace alloys, this alloy retains its strength properties in thicker sections while maintaining crack resistance and compressive strength. AMS 4050 is usually associated with 7050, although different manufacturers require their own specifications for their products.

Chemical composition of aluminum alloy 7050

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

7050

Zr : 0.08-0.15

Each

Total

Rem

<0.12

<0.15

2-2.6

<0.1

1.9-2.9

<0.04

5.7-6.7

<0.06

<0.05

<0.15

Other equivalent standards for 7050 aluminum alloy are :

AMS 4108
AMS 4201
ASTM B247
ASTM B316
QQ A-430

Physical properties of 7050 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
7050-O	70.3	26.9	524	635	860	23.5	2.83	36.7	180	47
7050-T736,T73651	70.3	26.9	524	635	860	23.5	2.83	42.6	157	40.5
7050-T76,T7651	70.3	26.9	524	635	860	23.5	2.83	43.6	154	39.5

Typical mechanical properties of 7050 aluminum alloy

Type of heat treatment	piece type	Tensile strength	Surrender strength	Percentage increase
T73652	sheet	510	455	11
T73652	Forged piece	524	455	15

Manufacturing conditions and heat treatment of 7050 alloy

Heat treatment

The annealing temperature of this alloy is 413 degrees Celsius, the dissolution temperature is 477 degrees Celsius and its aging temperature is 177-121 degrees Celsius.

Shaping

7050 aluminum alloy can be formed under temperature or heat treatment conditions.

Welding

7050 aluminum should not be welded to prevent cracking and porosity. The weld bond produced will be weaker than the base metal. Different methods for welding this alloy are not preferred.

Cooling

7050 Aluminum Alloy can be cooled using conventional cooling methods.

Aging

Aluminum alloy 7050 is aged using two-stage heat treatment. It is heated at 122 degrees Celsius (250 degrees Fahrenheit) for 3 to 6 hours. It is reheated to 163 ° C (325 ° F) for 15 hours and then cooled in air.

Harden

7050 aluminum alloy can be hardened by heat treatment.

Properties and usage of 7050 aluminum alloy

7050 Aluminum Alloy is mainly used in the construction of aircraft and other structures. This alloy is used to make plates, extruded parts, hand forged or molded parts used in aircraft construction, parts that require high strength with resistance to corrosion and scaling, crack resistance due to stress corrosion, high fracture toughness and Resistant to fatigue, used.

Properties and usages of 7072 aluminum alloy

Aluminum alloys have high corrosion resistance. They lose their power when exposed to very high temperatures.

Chemical composition of aluminum alloy 7072

Alloy name	Ingredients (weight percentage)							consideration	Other elements		AL%
7072	Fe+Si	Cu	Mn	Mg	Cr	Zn	Ti	–	Each	Total	Rem
7072	<0.7	<0.1	<0.1	<0.1	–	0.8-1.3	–	–	<0.05	<0.15	Rem

Other equivalent standards for 7072 aluminum alloy are :

ASTM B209
ASTM B221
ASTM B234
ASTM B241
ASTM B313
ASTM B345
ASTM B404
ASTM B547

Physical properties of 7072 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
7072-O	68	–	641	657	893	23.6	2.72	28.7	227	60

Typical mechanical properties of 7072 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase
O	55-90	<21	15-20
H14	97-131	<83	1-3
H18	min131	–	1-2
H19	min145	–	1
H25	107-148	<83	2-3
H111,H211	62-97	<41	12

Properties and usages of 7072 aluminum alloy

This alloy can be used as a corrosion protection coating for Alklad sheets, plates and tubes whose base metal is alloy 2219, 3003, 3004, 5050, 5052, 5154, 6061, 7075, 7475 and 7178. The annealing temperature of this alloy is 343 degrees Celsius.

Properties and usage of 7075 aluminum alloy

Aluminum alloys have strong corrosion resistance. At lower temperatures, their strength increases, so they become a desirable low-temperature alloy. Their strength decreases if they are exposed to very high temperatures. Aluminum 7075 has high strength.

Chemical composition of aluminum alloy 7075

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

7075

–

Each

Total

Rem

<0.4

<0.5

1.2-2

<0.3

2.1-2.9

0.18-0.28

5.1-6.1

<0.2

<0.05

<0.15

Alclad 7075Coating with 7072

<0.7

<0.1

–

0.8-1.3

–

<0.05

<0.15

Rem

Physical properties of 7075 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
T6,T651,T652	71	26.9	477	635	960	23.4	2.8	52.2	130	33
,T7352,T73,T7351	71	26.9	477	635	960	23.4	2.8	43.1	155	40
7050-T76,T7651	71	26.9	477	635	960	23.4	2.8	44.8	150	38.5

Mechanical properties of 7075 aluminum alloy

Alloy name	Type of heat treatment	Tensile strength	Surrender strength	Percentage increase	Hardship	shear strength
7075	O	228	103	17	60	152
	T6,T651	572	503	11	150	317
	T73	503	343	–	–	–
Alclad 7075	O	221	97	17	–	–
Alclad 7075	T6,T651	524	462	11	–	–

Heat treatment conditions of 7075 alloy

The annealing temperature of this alloy is 413 ° C, the dissolution temperature is 462-482 (depending on the type and size of the part) and its tempering temperature for T6 operation is 121 ° C.

T7 tempering is two-step :

The first step is to bring the piece to a temperature of 107 degrees Celsius
In the second stage, the piece is heated to a temperature of 166 to 177 degrees Celsius (depending on the piece).

Other characteristics Other criteria equivalent to 7075 aluminum are :

AMS 4044	ASTM B209	ASTM B468	QQ A-200/15
AMS 4045	ASTM B210	DMS 2233	QQ A-225/9
AMS 4049	ASTM B211	MIL A-12545	QQ A-250/13
AMS 4131	ASTM B221	MIL A-22771	QQ A-250/24
AMS 4147	ASTM B241	MIL F-18280	QQ A-367
AMS 4154	ASTM B247	MIL F-5509	QQ A-430
AMS 4323	ASTM B316	QQ A-200/11	QQ WW-T-700/7
SAE J454

Heat treatment and production method of 7075 aluminum

Aluminum 7075 alloy can be machined under annealing conditions. Oil lubricants are used for machining operations.

Forming aluminum 7075

Aluminum 7075 alloy can be formed under heating conditions. In case of any problem, it can be heated to 94 to 122 degrees Celsius (200 to 250 F).

How to weld 7075 aluminum

Aluminum 7075 alloy can be welded using resistance welding method. Gas welding method is not suitable for welding this alloy. Arc welding should also be avoided, as it weakens the corrosion resistance of this alloy.

Heat treatment

Aluminum 7075 alloy is evaporated for 2 hours at 900 F and then heated with cooling humidity and relative humidity.

Forging

Aluminum 7075 alloy is forged at 372 to 483 degrees Celsius (700 to 900 F).

Analyzing

Aluminum 7075 alloy is neutralized for 3 hours at 413 ° C (775 ° F) and then by controlled cooling at 10 to 260 ° C (50 to 500 ° F) per hour and air cooled, It is heated.

Aging

Aluminum alloy 7075 can be obtained at a temperature of 122 ° C (250 F) for 24 hours to obtain a purity of T 6. Cooling T 73 can be at a temperature of 108 ° C (225 F) for 8 hours and at a temperature of 163 ° C Heat at 32 ° C for 24 hours.

Usage of 7075 aluminum alloy

Very high strength, very good anodizing effect, relatively good ductility and medium corrosion resistance are the features of this alloy. This alloy is used to make items that require very high strength and medium corrosion resistance.

sheet
wire
Rods
billet
Pipe
Aircraft structural components
The body of individual weapons
Properties and usages of 7175 aluminum alloy

These alloys are sensitive to high temperatures between 200 and 250 ° C (392-482 ° F). Aluminum alloys gain strength when exposed to low temperatures, and their strength is lost when exposed to high temperatures.

Chemical composition of aluminum alloy 7175

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

7175

–

Each

Total

Rem

<0.15

<0.2

1.2-2

<0.1

2.1-2.9

0.18-0.28

5.1-6.1

<1.1

<0.05

<0.15

Physical properties of 7175 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
7175-O	72	–	–	635	864	23.4	2.8	37.5	177	46
۷۱۷۵-T66	72	–	–	635	864	23.4	2.8	47.9	142	36
7175-T736,T73652	72	–	–	635	864	23.4	2.8	43.1	155	40

Mechanical properties of aluminum alloy 7175

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase	Hardship	shear strength	Fatigue strength
T66	593	524	11	150	324	159
T736	524	455	11	145	290	159

Alloy heat treatment conditions 7175

Annealing temperature of 413 degrees Celsius, dissolution temperature of 516 degrees Celsius, it is better to cool first to 485-477 degrees Celsius and then quench. The aging temperature of this alloy is 177-121 degrees Celsius.

PROPERTIES	CONDITIONS
T (°C)	TREATMENT
Thermal conductivity	177 (W / mK)	25	O

Production conditions of aluminum alloy 7175

Machining : It is easily possible to make parts from 7175 aluminum. This alloy can be heated. They can also be resisted by heat treatment.
Edging : Aluminum 7175 is a hard alloy.

7175 alloy usages

This alloy is used to make forged parts that require very high strength, such as aircraft components. T736 heat treatment on this alloy increases the tensile strength, corrosion resistance, scaling resistance, corrosion resistance, fatigue resistance of the part and also increases the toughness of the alloy.

Properties and usage of 7475 aluminum alloy

Aluminum alloys are sensitive to high temperatures between 200 and 250 degrees Celsius (392 to 482 degrees Fahrenheit).

Chemical composition of aluminum alloy 7475

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

7475

–

Each

Total

Rem

<0.1

<0.12

1-2

<0.06

1.9-2.6

0.18-0.25

5.2-6.2

<0.06

<0.05

<0.15

Physical properties of 7475 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
7475-O	70	27	–	635	865	23.4	2.8	37.5	177	46
7475-T61,T651	70	27	–	635	865	23.4	2.8	47.9	142	36
7475-T7351	70	27	–	635	865	23.4	2.8	43.1	155	40

Typical mechanical properties of 7475 aluminum alloy

Type of heat treatment	piece type	Tensile strength	Surrender strength	Percentage increase
T61	Sheet with a thickness of 0.04 – 0.249 inches	552	496	12
T761	Sheet with a thickness of 0.04 – 0.249 inches	524	462	12

How to make and heat treatment of 7475 alloy

Anilling

The annealing temperature of this alloy is 413 degrees Celsius and its dissolution temperature is 516 degrees Celsius. But it is better to warm and store it at 477-466 degrees Celsius first.
The aging temperature of 7475 aluminum alloy is 177-121 degrees Celsius.

Cooling

Common methods are used for cooling 7475 aluminum alloy under annealing conditions.

Welding

Aluminum 7475 is not usually welded.

Shaping

Aluminum 7475 alloy can be formed using conventional methods. This alloy can be easily formed in annealing conditions compared to heat treated conditions in which the alloy has more springs due to its strength.

Machining capability

7475 aluminum alloy has good machining specifications in annealing conditions. Oil-based lubricants can be used during machining of this alloy.

Heat treatment

Aluminum alloy 7475 can be heat treated.

Heat treatment conditions of 7475 aluminum alloy

The heat treatment characteristics of 7475 aluminum are given in the table below.

Specifications		T (ºC)	Type
Thermal conductivity	177 (W/m-K)	25	O

Properties and usages of 7475 aluminum alloy

7475 aluminum alloy can be used in aircraft fuselage and many other structures. Coated sheets and plates used in the fuselage, wing shells and wing parts of the aircraft and the retaining wall between the hot part of the engine and the rear of the aircraft, as well as other usages that require a combination of very high strength and high fracture toughness are some of the uses of this alloy. Are considered.

8000 series of aluminum alloys

The 8000 series of aluminum alloys include alloys that are not included in the previous series of aluminum alloys and mostly contain Fe, Ni, Li, Sn, Si and Ce alloying elements. This series of alloys can be used in nuclear power plants, food industry, automotive bearings, conductors and..

Some of the features of this series of aluminum alloys are as follows

Al-Fe-Ni : Has high strength and electrical conductivity

Al-Li : Has high strength and stiffness while having a low density

Al-Sn : Has high strength and corrosion resistance

Al-Fe-Si : High ductility, softness and conductivity and etc

Industries in which aluminum alloy is in greater demand

Almost all known industries in the world today need aluminum alloy and it is not possible to demarcate this field, but the main industries that use them are:

Automotive industry
aerospace Industries
Marine industries
Oil and gas and petrochemicals
Rail transport industry
Electricity and telecommunications industry
Canning and packaging industries
building industry
Properties and usage of 8090 aluminum alloy

Aluminum is a soft and light metal. It can be alloyed with elements such as manganese, magnesium, silicon, copper and lithium. Aluminum manufacturers began making aluminum-lithium alloys in the 1970s. 8090 Aluminum Alloy is a lithium-based alloy. Adding lithium to aluminum helps reduce density and increase hardness. Aluminum-lithium alloys can have excellent compositions and strength.

Chemical composition of aluminum alloy 8090

Alloy name

Ingredients (weight percentage)

consideration

Other elements

AL%

8090

Li : 2.2-2.7Zr : 0.04-0.16

Each

Total

Rem

<0.2

<0.3

1-1.6

<0.1

0.6-1.3

<0.1

<0.25

<0.1

<0.05

<0.15

Physical properties of 8090 aluminum alloy

Type of heat treatment	Tensile elastic modulus	Shear elastic modulus	rigid limit	melted limit	Specific Heat	Linear thermal expansion coefficient at a temperature of 100-20 degrees	Density	electrical resistance	Thermal conductivity	Electrical conductivity
8090-T6	77	–	600	655	930	21.4	2.55	–	93.5	17

Typical mechanical properties of 8090 aluminum alloy

Type of heat treatment	Tensile strength	Surrender strength	Percentage increase
T6	480	400	4.5

Heat treatment properties of 8090 aluminum alloy

The heat treatment properties of 8090-T8151 aluminum alloy are given in the table below.

SPECIFICATIONS	METRIC	IMPERIAL
Thermal expansion coefficient (@ 20-100 ° C / 68-212 ° F)	m/m°C	11.9 µin/in°F
Thermal conductivity	95.3 W / mK	661 BTU in/hr.ft².°F

Properties and usage of 8090 aluminum alloy

Aluminum 8090 is mainly used as an advanced material for aerospace technology and to minimize the weight of military weapons and defense systems. In cases where the stresses on the part are high and the specific gravity is very low, such as the main parts and the aircraft actuator, this alloy is used.

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Aluminum alloys

Definition of alloying

The reason for the expansion of this industry

Specifications and features of aluminum alloy

Corrosion resistance

Capability in thermal conductivity

Capability in electrical conductivity

Appropriate ratio of strength to weight

Resistance to failure

Very high workability

High connectivity

Recyclability

Aluminum alloy groups

Alloys wrought

Alloys Casting

Types of aluminum alloys

Aluminum – copper alloy

Aluminum – magnesium alloy

Aluminum – silicon alloys

Tin ( Sn )

Lead (Pb)

Iron (Fe)

Manganese (Mn)

Chromium ‬ (Cr)

Nickel (Ni)

Phosphorus (P)

Titanium (Ti)

Strontium (Sr)

Series of aluminum alloys

Alloy aluminum alloy in brief

1000 series of aluminum alloys

Properties and usage of 1050 aluminum alloy :

Physical properties of 1050 aluminum alloy :

Mechanical properties of 1050 aluminum:

Chemical composition of 1050 aluminum alloy:

1050 alloy usages

Properties and usages of 1060 aluminum alloy

Chemical composition of aluminum alloy 1060

Physical properties of 1060 aluminum alloy

Typical mechanical properties of 1060 aluminum alloy

Other characteristics Properties and usages of 1060 aluminum alloy

How to make and heat treatment of aluminum alloy 1060

Properties and usage of 1060 aluminum alloy

Properties and usage of 1100 aluminum alloy

Chemical composition of 1100 aluminum alloy

Physical properties of 1100 aluminum alloy

Mechanical properties of 1100 aluminum

usage of 1100 aluminum sheet

Properties and usages of 1145 aluminum alloy

Chemical composition of aluminum alloy 1145

Physical characteristics of aluminum alloy 1145

Mechanical properties of 1145 aluminum alloy

Thermal properties of 1145 aluminum alloy

The equivalent materials of 1145 aluminum alloy are as follows

Manufacture and heat treatment of aluminum alloy 1145

Properties and usage of aluminum alloy 1199

Chemical composition of aluminum alloy 1199

Physical properties of aluminum alloy 1199

Typical mechanical properties of aluminum alloy 1199

Thermal properties of aluminum 1199

Properties and usage of aluminum alloy 1199

Usages of aluminum 1199

Properties and usage of 1200 aluminum alloy

Chemical composition of aluminum alloy 1200

Physical properties of 1200 aluminum alloy

Typical mechanical properties of 1200 aluminum alloy

Aluminum equivalent alloys 1200

Welding of aluminum alloy 1200

Properties and usage of 1200 aluminum alloy

Properties and usage of aluminum alloy 1350

Properties and usage of aluminum alloy 1350

Chemical composition of aluminum alloy 1350

Physical properties of aluminum alloy 1350

Typical mechanical properties of aluminum alloy 1350

Standard alloys of aluminum alloy 1350

Properties and usage of aluminum alloy 1350

2000 series of aluminum alloys

Properties and usages of aluminum alloy 2007

Chemical composition of aluminum alloy 2007

Physical properties of aluminum alloy 2007