Application: | Transportation Tools, Door & Window, Heat Sink, Deck, Aircraft Plate Welding Parts, Tankers, Oxyge |
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Certification: | ISO9001, ASTM, GB, SGS |
Technique: | Hot Rolled |
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Thickness:0.2-600mm
Width:200-2200mm
Length:Under 6000mm normally or customized
Weight:0.5-7.0 tons per pallet or customized
Temper:various Temper (HO-H321)
Surface treatment:mill finished and silvery aluminum plain color
7000 | Al-Zn-Mg-Cu belongs to super-hard aluminum. Such alloys are the highest strength aluminum alloy at room temperature, after solution treatment and aging, its strength reaches 680MPa, its specific strength has been equivalent to superhardness steel, hence the name superhard aluminum, mainly used for aircraft stress Structure |
7005 | Extruded material for the manufacture of welded structures that require both high strength and high fracture toughness, such as trusses, rods, containers for transportation vehicles; large heat exchangers, and the ability to be soldered Of the components; can also be used to make sports equipment such as tennis rackets and softball bats |
7039 | Frozen containers, cryogenic equipment and storage tanks, fire pressure equipment, military equipment, armor plates, missile installations |
7049 | Parts for forging the same static strength as the 7079-T6 alloy but also requiring a high resistance to stress corrosion cracking, such as aircraft and missile components - landing gear cylinders and extrusions. Fatigue properties of the parts are roughly the same as for the 7075-T6 alloy, with slightly higher toughness |
7050 | Aircraft structural plate, extrusion, free forgings and die forgings. The requirements for the manufacture of such parts are: anti-spalling corrosion, stress corrosion cracking resistance, fracture toughness and fatigue resistance are high |
7072 | 7072 air conditioner aluminum foil and thin strip; 2219,3003,3004,5050,5052,5154,6061,7075,7475,7178 alloy sheet and pipe cladding. |
7075 | For the manufacture of aircraft structures and futures He requested high strength, high corrosion resistance of high-stress structural parts, mold manufacturing |
7175 | High strength structural for forged aircraft. T736 material has a good overall performance, that is, strength, anti-spalling corrosion and stress corrosion cracking resistance, fracture toughness, fatigue strength are high |
7178 | For the manufacture of aerospace components require high compressive yield strength components |
7475 | Fuselage with aluminum package and aluminum sheet, wing skeletons, stringers and so on. Other parts should have both high strength and high fracture toughness |
7A04 | Aircraft skin, screws, and force components such as beams stringers, bulkheads, ribs, landing gear and so on |
PRODUCT
NAME |
ALLOYS NUMBER | TEMPER |
THICKNESS
(MM) |
WIDTH
(MM) |
LENGTH
(MM) |
APPLICATION |
Aluminum sheet/ Plate
|
7005
7A04 7A09 7050 7075 |
O,T3,T4,T6,T651,T8611 | 0.5-600 | 800-2600 | 800-8000 | Golf head, mold, aircraft landing gear and other |
Chemical Composition % | ||||||||||||
Alloy No. | Si | Fe | Cu | Mn | Mg | Cr | Ni | Zn | V | Ti | Zr | Al |
1050 | 0.25 | 0.4 | 0.05 | 0.05 | 0.05 | - | - | 0.05 | 0.05 | 0.03 | - | Remainder |
1060 | 0.25 | 0.35 | 0.05 | 0.03 | 0.03 | - | - | 0.05 | 0.05 | 0.03 | - | Remainder |
1070 | 0.2 | 0.25 | 0.04 | 0.03 | 0.03 | - | - | 0.04 | 0.05 | 0.03 | - | Remainder |
1100 | 0.45 | 0.35 | 0.05-0.20 | 0.03 | - | - | - | 0.01 | 0.05 | - | - | Remainder |
2014 | 0.50-1.20 | 0.7 | 3.9-5.0 | 0.4-1.2 | 0.2-0.8 | 0.1 | - | 0.25 | - | 0.15 | - | Remainder |
2017 | 0.20-0.80 | 0.7 | 3.5-4.5 | 0.40-1.0 | 0.4-0.8 | 0.1 | - | 0.25 | - | 0.15 | - | Remainder |
2024 | 0.5 | 0.5 | 3.8-4.9 | 0.3-0.9 | 1.2-1.8 | 0.1 | - | 0.25 | - | 0.15 | - | Remainder |
3003 | 0.6 | 0.7 | 0.05-0.20 | 1.0-1.5 | - | - | - | 0.1 | - | - | - | Remainder |
3004 | 0.3 | 0.7 | 0.25 | 1.0-1.5 | 0.8-1.3 | - | - | 0.25 | - | - | - | Remainder |
3105 | 0.6 | 0.7 | 0.3 | 0.3-0.8 | 0.2-0.8 | 0.2 | - | 0.4 | - | 0.1 | - | Remainder |
5005 | 0.3 | 0.7 | 0.2 | 0.2 | 0.5-1.1 | 0.1 | - | 0.25 | - | - | - | Remainder |
5052 | 0.25 | 0.4 | 0.1 | 0.1 | 2.2-2.8 | 0.15-0.35 | - | 0.1 | - | - | - | Remainder |
5083 | 0.4 | 0.4 | 0.1 | 0.40-1.0 | 4.0-4.9 | 0.05-0.25 | - | 0.25 | - | 0.15 | - | Remainder |
5086 | 0.4 | 0.5 | 0.1 | 0.2-0.7 | 3.5-4.5 | 0.05-0.25 | - | 0.25 | - | 0.15 | - | Remainder |
5182 | 0.2 | 0.35 | 0.15 | 0.2-0.5 | 4.0-5.0 | 0.1 | - | 0.25 | - | 0.1 | - | Remainder |
5754 | 0.4 | 0.4 | 0.1 | 0.5 | 2.6-3.6 | 0.3 | - | 0.2 | 0.1-0.6Mn+Zn | 0.15 | - | Remainder |
6061 | 0.4-0.8 | 0.7 | 0.15-0.40 | 0.15 | 0.8-1.2 | 0.04-0.35 | - | 0.25 | - | 0.15 | - | Remainder |
6063 | 0.2-0.6 | 0.35 | 0.1 | 0.1 | 0.45-0.90 | 0.1 | - | 0.1 | - | 0.1 | - | Remainder |
6082 | 0.7-1.3 | 0.5 | 0.1 | 0.4-1.0 | 0.6-1.2 | 0.25 | - | 0.2 | - | 0.1 | - | Remainder |
7005 | 0.35 | 0.4 | 0.1 | 0.2-0.7 | 1.0-1.8 | 0.06-0.20 | - | 4.0-5.0 | - | 0.01-0.06 | 0.08-0.20 | Remainder |
7075 | 0.4 | 0.5 | 1.2-2.0 | 0.3 | 2.1-2.9 | 0.18-0.28 | - | 5.1-6.1 | - | 0.2 | - | Remainder |
7175 | 0.15 | 0.2 | 1.2-2.0 | 0.1 | 2.1-2.9 | 0.18-0.28 | - | 5.1-6.1 | - | 0.1 | - | Remainder |
8011 | 0.50-0.90 | 0.6-1.0 | 0.1 | 0.2 | 0.05 | 0.05 | - | 0.1 | - | 0.08 | - | Remainder |
8021 | 0.15 | 1.2-1.7 | 0.05 | - | - | - | - | - | - | - | - | Remainder |
8079 | 0.05-0.3 | 0.7-1.3 | 0.05 | - | - | - | - | 0.1 | - | - | - | Remainder |
Mechanical Property | |||
Alloy | Tensile Strength(MPa) | Yield Strength(MPa) | Elongation(%) |
7005 T4 | ≥324 | ≥215 | ≥11 |
7005 T5 | ≥345 | ≥305 | ≥9 |
7005 T6 | ≥350 | ≥290 | ≥8 |
Product Properties
7005 aluminum alloy, the United States deformed aluminum and aluminum alloys. 7005 strength is higher than 7003 alloy, good welding performance, heat treatment can be strengthened. 7005 aluminum alloy extrusion material, often used in the manufacture of welded structures that require both high strength and high fracture toughness, such as trusses, rods, containers for transport vehicles; large heat exchangers, and cannot be carried out after welding Solid-melt processing components; can also be used to manufacture sports equipment such as tennis rackets and softball bats.
Performance
1. High strength heat treatable alloy.
2. Good mechanical properties.
3. Usability is good.
4. Easy to process, good wear resistance.
5.T7351 condition enhances corrosion resistance
6. High-strength materials for high-pressure structural parts.
Packaging
1) Packaging Detail:
Plate/coil is placed to the iron or wooden pallet ,wrapped by water-proof craft paper perfectly , then fixed by iron narrow belt well .
2) Port:Qingdao port or other main port in China
3) Container:20ft GP:5898mm(Length)x2352mm(Width)x2393mm(High) , loading 18~25 tons .
40ft GP:12032mm(Length)x2352mm(Width)x2393mm(High) , loading 20~28 tons.
Certificate
Factory imagine
FAQ
A: We are factory and we can provide competitive price
A: Generally it is 10-15 days if the goods are in stock. Or it is 15-25 days if the goods are not in stock, it is according to quantity and standard.
A:We have strict quality control system .We can Visit Our factory is the best way to know each other more. And we also will attach some relevant photos via email to show our office and products for you.
A:Generally speaking, the MOQ is 3 metric ton per size, if your quantity is small , we can supply you from our stock .
A: Yes, we could offer the sample for free charge but the cost of freight is by receiver ,normally
A:T/T ,D/D,L/C at sight,Acceptance L/C,Deferred Payment L/C and so on