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2A02 T6 Aircraft Aerospace Aviation Aluminum Forgings
2A02 T6 Aircraft Aerospace Aviation Aluminum Forgings

2A02 T6 Aircraft Aerospace Aviation Aluminum Forgings

China 2A02 T6 Aircraft Aerospace Aviation Aluminum Forgings, Find details about China 2A02 T6 Aircraft Aluminum Forgings, 2A02 T6 Aerospace Aluminum Forgings from 2A02 T6 Aircraft Aerospace Aviation Aluminum Forgings

Model NO.
2A02
Surface Treatment
Zinc/Chrome Plating,Anodizing
Forging Tolerance
+/-0.2mm
Standard
ANSI
Certification
CE, ISO 9001:2008
Service
OEM ODM
Trademark
Chalco Aluminum
Transport Package
Export Standard Wooden Pallet or as Your Requsts
Specification
According to Customer Requirement
Origin
Henan China
HS Code
7218100000
Model NO.
2A02
Surface Treatment
Zinc/Chrome Plating,Anodizing
Forging Tolerance
+/-0.2mm
Standard
ANSI
Certification
CE, ISO 9001:2008
Service
OEM ODM
Trademark
Chalco Aluminum
Transport Package
Export Standard Wooden Pallet or as Your Requsts
Specification
According to Customer Requirement
Origin
Henan China
HS Code
7218100000
2A02 T6 Aircraft Aerospace Aviation Aluminum Forgings
 
Chemical Composition of 2A02 Aircraft Aerospace Aluminum Bar Forgings
AlloySiFeCuMnMgCrNiZnTiZrOthersAl
EachTotal
2A020.300.302.6~3.20.45~0.72.0~2.4--0.100.15-0.050.15Remainder
2A02 Aircraft Aerospace Aluminum Bar Forgings is a kind of alloy with high strength in hard aluminum. It is characterized by high strength at normal temperature and high thermal strength, which belongs to heat-resistant hard aluminum. The alloy has high plasticity during hot deformation. It has a tendency to form coarse grain ring in extruded semi-finished products, which can be strengthened by heat treatment and used in quenching and artificial aging. Compared with 2A70 and 2A80 heat-resistant forging aluminum, the corrosion stability is better, but it has the tendency of stress corrosion cracking, and the weldability is better than that of 2A70, and the machinability is good.
AlloyAlloy SeriesMain Features
2A02Al-Cu-MnThe heat treatment strengthened alloy, Al-Cu-Mg system, has high strength and plasticity, high heat resistance and corrosion resistance in artificial aging. It is used to manufacture aero turbojet axial compressor blades and other parts at 200 --300ºC.
 
Technical StandardTypeD/mmTemperDirectionRm/MpaRp0.2/MpaA/%HBS
Not less than
GB/T 3191Extruded aluminum barAll DiametersT6L43027510-
GJB 2054
HB 5202		Extruded aluminum bar≤240T6L43027510-
GJB 2351
HB 5204		ForgingsFollow the contractT6L39025510100


 
Mechanical Properties of 2A02 T6 Alloy Extruded Strip (30 x 130mm) at Different Temperatures
Temperatures/ºCRm/MpaRp0.01/MpaRp0.2/MpaA10/%Z/%
2049127432513.021.2
10047124728815.622.8
15042826829616.128.7
20037422827416.133.4
25023612816816.966.6
3001719411221.575.9
350108255927.685.6
 
Typical Mechanical Properties of 2A06 T6 Alloy Bar at Room Temperature
Specs d/mmRm/MpaRp0.2/MpaA10/%
Min.Max.AverageMin.Max.AverageMin.Max.Average
31500545514.5305430360.2102015.3
33500570525.3335440366.3111815.1
36495555522.4335380358.4112015.5
Typical Mechanical Properties of 2A02 T6 Alloy strip and Die Forgings at Room Temperature
TypeSpecs/mmDirectionRm/MpaRp02/MpaA10/%
Extruded stripShape 60×110L51033817.5

 

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