• 6A02 Aircraft Aerospace Aluminum Extrusions Section for Aviation
  • 6A02 Aircraft Aerospace Aluminum Extrusions Section for Aviation
  • 6A02 Aircraft Aerospace Aluminum Extrusions Section for Aviation
  • 6A02 Aircraft Aerospace Aluminum Extrusions Section for Aviation
  • 6A02 Aircraft Aerospace Aluminum Extrusions Section for Aviation
  • 6A02 Aircraft Aerospace Aluminum Extrusions Section for Aviation

6A02 Aircraft Aerospace Aluminum Extrusions Section for Aviation

Type: Transport Aluminium Profile, Industrial Aluminium Profile, Aviation
Shape: Round/Flat/Angle/Square/ Hexagon
Grade: 6000 Series
Temper: T6/T62
Alloy: Alloy
Surface Finishing: Anodized,Electrophoresis,Powder/PVDF Coated.
Samples:
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Customization:
Diamond Member Since 2018

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Basic Info.

Model NO.
6A02
Alloying Ingredient
6A02
Certification
ISO, En755 GB5237-2008 Astmb221 DIN
Extrusion Machine
1000-4000 Tons, 35 Press Lines.
Transport Package
Export Standard Wooden Pallet or as Your Requsts
Specification
According to Customer Requirement
Trademark
Chalco Aluminum
Origin
Henan China
HS Code
7604210000
Production Capacity
4000mt/Month

Product Description

6A02 Aircraft Aerospace Aluminum Extrusions Section for Aviation  

6A02 alloy is suitable for manufacturing aircraft and engine parts with high requirements for plasticity and corrosion resistance in cold and hot state, helicopter blades and complex shape profiles and forgings. Working temperature range of parts 70~50 ºC.
The processing of6A02 Aluminum plate bar profile tube forgings in the cold and hot state, in the hot working temperature range high plasticity, forging and forging temperature of 470~380 ºC alloy can be used. For spot welding, seam welding and argon arc welding, gas welding, friction stir welding quality, good performance.
Chemical Composition of 6A02Alloy
Alloy Si Fe Cu Mn Mg Zn   Ti Others Al
Each Total
6A02 1.2 0.5 0..2~0.6 0.15~0.35 0.45~0.9 0.2 - - 0.05 0.15 Remainder
 
Calibration mechanical strength of 6A02 6A02 Aluminum plate bar profile tube forgings
Technical Standard Type Test Temper δ  or d/mm Tension Stregnth Rm/Mpa Rp0.2/Mpa A/%
YS/T 213
YS/T 214
Aluminum sheet O 0.35~5.0 ≤147 - 20
>0.5~10.0 147 - 15
T4 0.3~0.6 196 - 18
>0.6~3.0 196 - 20
3.0~5.0 196 - 18
>5.0~10.0 177 - 16
T6 0.3~5.0 294 - 10
>5.0~10.0 294 - 8
GB/T 3880 Aluminum sheet O 0.5~4.5 ≤145 - 21
>4.5~10.0 145 - 16
T62 0.5~4.5 295 - 11
>4.5~10.0 295 - 8
T4 0.5~0.8 195 - 19
>0.8~2.9 195 - 21
>2.9~4.5 195 - 19
>4.5~10.0 195 - 17
GB/T 3880 Aluminum sheet T6 0.5~4.5 295 - 11
>4.5 295 - 8
T62 4.5~12.5 305 - 12
>12.5 295 - 8
>25.0 295 - 7
>40.0 285 - 6
T42 4.5~12.5 175 - 17
>12.5 175 - 14
>25.0 165 - 12
>40.0 165 - 10
GJB 2053 Aluminum sheet
O
1.0~4.0 ≤147 - 20
T4 1.0~3.0 196 - 20
>3.0 196 - 18
T6 1.0~4.0 295 - 10
GJB 2662 Aluminum palte O 4~5 147 - 2
>5 147 - 15
T4 4~5 196 - 18
>5 176 - 16
T6 4~5 295 - 10
>5 295 - 8
T4 7~25 178 - 14
>25 167 - 12
>40 167 - 10
T6 7~25 295 - 7
>25 285 - 6
>40 275 - 6
GB/T 3191 Extruded aluminum bar rod T6, T62 ≤150 295 - 12
GJB 2054 Extruded aluminum bar rod T6 5~150 295 - 12
>150 280 - 12
HB 5202 Extruded aluminum bar rod T6 240 294 - 12
GB/T 3191 High strength extruded aluminum bar rod T62,T6 20~120 305 - 8
GJB 2054 T6 20~150 305 - 8
GJB 2507 Extruded aluminum profile T4 All the thickness 177 - 14
T6 All the thickness 294 - 10
GB/T 4437 Aluminum tube O All the thickness 147 - 17
T4 All the thickness 206 - 14
T6 All the thickness 294 - 8
GJB 2381 O All the thickness 147 - 17
T4 All the thickness 205 - 14
T6 25~120 295 - 8
>120 275 - 8
GJB 2379
 
Cold drawn aluminum tube O All the size ≤147 - 17
T4 All the size 206 -
-
14
T6 All the size 304 - 8
 
Technical Standard Type Temper L LT ST HB
Rm/Mpa Rp0.2/Mpa A5/% Rm/Mpa Rp0.2/Mpa A5/% Rm/Mpa A5/%
HB 5204 
GJB 2351
Free forgings T6 275 - 10 -       - -            - - 85
272 - 11 - - - - - 85
Die forgings T6 295 215 12 265 - 4 - - 85
295 215 12 265 - 4 - - 85

 

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