2A02 T6 Aircraft Aerospace Aviation Aluminum Forgings

Product Details
Customization: Available
Processing Object: Metal
Molding Style: Hot Forging
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Registered Capital
3000000 RMB
Plant Area
101~500 square meters
  • 2A02 T6 Aircraft Aerospace Aviation Aluminum Forgings
  • 2A02 T6 Aircraft Aerospace Aviation Aluminum Forgings
  • 2A02 T6 Aircraft Aerospace Aviation Aluminum Forgings
  • 2A02 T6 Aircraft Aerospace Aviation Aluminum Forgings
  • 2A02 T6 Aircraft Aerospace Aviation Aluminum Forgings
  • 2A02 T6 Aircraft Aerospace Aviation Aluminum Forgings
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Overview

Basic Info.

Model NO.
2A02
Molding Technics
Gravity Casting
Application
Aviation
Material
Aluminium
Heat Treatment
Quenching
Surface Treatment
Zinc/Chrome Plating,Anodizing
Forging Tolerance
+/-0.2mm
Standard
ANSI
Certification
CE, ISO 9001:2008
Service
OEM ODM
Transport Package
Export Standard Wooden Pallet or as Your Requsts
Specification
According to Customer Requirement
Trademark
Chalco Aluminum
Origin
Henan China
HS Code
7218100000
Production Capacity
5000pieces/Month

Product Description

2A02 T6 Aircraft Aerospace Aviation Aluminum Forgings
 
Chemical Composition of 2A02 Aircraft Aerospace Aluminum Bar Forgings
Alloy Si Fe Cu Mn Mg Cr Ni Zn Ti Zr Others Al
Each Total
2A02 0.30 0.30 2.6~3.2 0.45~0.7 2.0~2.4 - - 0.10 0.15 - 0.05 0.15 Remainder
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.
Alloy Alloy Series Main Features
2A02 Al-Cu-Mn The 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 Standard Type D/mm Temper Direction Rm/Mpa Rp0.2/Mpa A/% HBS
Not less than
GB/T 3191 Extruded aluminum bar All Diameters T6 L 430 275 10 -
GJB 2054
HB 5202
Extruded aluminum bar ≤240 T6 L 430 275 10 -
GJB 2351
HB 5204
Forgings Follow the contract T6 L 390 255 10 100


 
Mechanical Properties of 2A02 T6 Alloy Extruded Strip (30 x 130mm) at Different Temperatures
Temperatures/ºC Rm/Mpa Rp0.01/Mpa Rp0.2/Mpa A10/% Z/%
20 491 274 325 13.0 21.2
100 471 247 288 15.6 22.8
150 428 268 296 16.1 28.7
200 374 228 274 16.1 33.4
250 236 128 168 16.9 66.6
300 171 94 112 21.5 75.9
350 108 25 59 27.6 85.6
 
Typical Mechanical Properties of 2A06 T6 Alloy Bar at Room Temperature
Specs d/mm Rm/Mpa Rp0.2/Mpa A10/%
Min. Max. Average Min. Max. Average Min. Max. Average
31 500 545 514.5 305 430 360.2 10 20 15.3
33 500 570 525.3 335 440 366.3 11 18 15.1
36 495 555 522.4 335 380 358.4 11 20 15.5
Typical Mechanical Properties of 2A02 T6 Alloy strip and Die Forgings at Room Temperature
Type Specs/mm Direction Rm/Mpa Rp02/Mpa A10/%
Extruded strip Shape 60×110 L 510 338 17.5
Detailed Photos

2A02 T6 Aircraft Aerospace Aviation Aluminum Forgings2A02 T6 Aircraft Aerospace Aviation Aluminum Forgings2A02 T6 Aircraft Aerospace Aviation Aluminum Forgings2A02 T6 Aircraft Aerospace Aviation Aluminum Forgings2A02 T6 Aircraft Aerospace Aviation Aluminum Forgings


 

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