7A04 T6 Aircraft Aerospace Extruded Aluminum Profiles for Aviation

Product Details
Customization: Available
Type: Transport Aluminium Profile, Industrial Aluminium Profile, Aviation
Shape: Round/Flat/Angle/Square/ Hexagon
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Registered Capital
3000000 RMB
Plant Area
101~500 square meters
  • 7A04 T6 Aircraft Aerospace Extruded Aluminum Profiles for Aviation
  • 7A04 T6 Aircraft Aerospace Extruded Aluminum Profiles for Aviation
  • 7A04 T6 Aircraft Aerospace Extruded Aluminum Profiles for Aviation
  • 7A04 T6 Aircraft Aerospace Extruded Aluminum Profiles for Aviation
  • 7A04 T6 Aircraft Aerospace Extruded Aluminum Profiles for Aviation
  • 7A04 T6 Aircraft Aerospace Extruded Aluminum Profiles for Aviation
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Overview

Basic Info.

Model NO.
7A04
Grade
7000 Series
Temper
T6
Alloy
Alloy
Surface Finishing
Anodized,Electrophoresis,Powder/PVDF Coated.
Alloying Ingredient
7A04
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

7A04 T6 Aircraft Aerospace Extruded Aluminum Profiles for Aviation  

7A04 Aluminum alloy sheet plate profile forgings
7A04 aluminum alloy sheet plate profile forgings is a heat treatment and strengthening alloy of Al-Zn-Mg-Cu system. Its strength is higher than that of hard aluminum. It is characterized by its yield strength close to tensile strength and plasticity, and its sensitivity to stress concentration is strong, especially when subjected to vibration load and repeated static load. Therefore, the design of parts, the manufacturing process and the assembly process need to strictly avoid the stress concentration and the formation of additional stress. The heat resistance of the alloy is poor, and it will soften rapidly when the temperature is higher than 125, and the stress corrosion resistance of thick and thick parts is poor in short and transverse.

The main stress parts of 7A04 alloy aluminum alloy sheet plate profile forgings is widely used in aircraft structures, such as beams and stringers, bulkheads, ribs, skin, joints, undercarriage parts etc.. It can produce all kinds of semi-finished products, such as plate, strip, section, bar, wall, pipe, wire, free forgings and die forgings.
Chemical composition of 7A04 alloy
Alloy Si Fe Cu Mn Mg Cr Ni Zn Ti Zr Others Al
Each Total
7A04 0.50 0.50 1.4~2.0 0.20~0.60 1.8~2.8 0.15~0.25 - 5.0~7.0 - - 0.05 0.15 Remainder
 
Alloy Alloy series Mean features σb  Value/MPa Working temperature/ºC
7A04 B95(Russia) The yield strength to tensile strength, low ductility, sensitivity to stress concentration effects, especially the repeated static load under vibration load and the situation is more obvious, therefore need to strictly avoid stress concentration factor and the formation of additional stress in parts of the design, manufacture and assembly process. The short transverse stress corrosion resistance of the thick and large parts of the alloy is poor. There are mainly plate and extrusion parts.
                  480~570
<125
Physical Property of 7A04 Aluminum alloy sheet plate profile forgings
Alloy Type Temper δ size/mm Direction σb/MPa σp 0.2/MPa δ % Standard
7A04


Aluminum
Plate
T6 1.0~2.5 LT 480 410 7 GJB 2053-1994
>2.5 LT 490 420 7
T9 2.0~4.0 LT 520 450 7
T6 7.0~10.0 L 490 410 6 GJB 2662-1996
>10~25 L 490 410 4
>25~40 L 490 410 3
Extruded aluminum profile T6 7.0~10.0 L 490 370 7 GJB 2054-1994
>10~25 L 530 400 6
Extruded aluminum profile T6 ≤10 L 510 460 6 GJB 2057-1995
>10~20 L 530 460 6
>20~40 L 560 460 6
>40 L 570 490 6
Free forgings T6 Weight≤30KG L 510 420 6 GJB 2351-1995
Weight>30KG L 510 420 5
Die forgings T6 Weight≤30KG L 530 440 6
Weight>30KG L 430 440 6
                   
 
Alloy Temper Aircraft type Application parts and typical parts
7A04 Aluminum plate:  T6,T9
Aluminum forgings:T6
Aluminum profile: T6
Y8, Y12 Skin, wall board, all kinds of beams (backlog, forgings), frame, fin, long truss, joint, landing gear and so on.
 
Chemical Composition of 7A04 Alloy
Alloy Si Fe Cu Mn Mg Cr Ni Zn Ti Zr Others Al
Each Total
7B04 0.10 0.25 1.4~2.0 0.20~0.60 1.8~2.8 0.15~0.25 - 5.0~6.5 - - 0.05 0.15 Remainder

7B04 aluminum alloy sheet profile forgings 

7B04 alloy is further purified and developed on the basis of long term use of 7A04 alloy. That is to improve its fracture toughness properties by controlling Fe and Si impurity elements. 7B04 alloy has been used in T6 state for a long time, and its strength is high. The characteristic is that the yield strength is close to the mild tensile, low plasticity and poor stress corrosion resistance.
7B04 aluminum alloy sheet profile forgings is a relatively mature high purity aluminum alloy in China. It is a large aluminum alloy used on  aircraft in China. Parts of the machine account for 60% of the total aluminum alloy consumption, and the consumption of the single machine is about 20t, which achieves stable batch supply. Varieties include plates, thick plates, profiles, extruded panels, bars and forgings. The successful application of 7B04 alloy to  aircraft provides valuable experience for the promotion of domestic new materials in  civil aircraft.
Alloy Alloy Series Main Features σb Value/MPa Working Temperature/ºC
7B04 B95(Russia) The fracture toughness of 7A04 alloy is higher than that of 7A04 alloy by 10%~15%. The main varieties are sheet, profile, extruded wall plate and bar, forgings and so on. There are three kinds of T6, T73 and T74 in use. The ingot of this alloy is more difficult than 7A04 alloy. It is suitable for hot forming, such as rolling, extrusion, forging and so on. It can make all kinds of parts of size and shape.
                  440~590
<125
 
Mechanical properties of 7B04 aluminum alloy
Alloy Type Temper δ  Size/mm σb/MPa σp 0.2/MPa δ % KIC or KC Standard
7B04


Aluminum sheet
T6 0.5~1.9 480 400 7 - 11-CL-027B
>1.9~6.0 490 410 7
>6.0~10.5 490 410 6
T74 0.5~1.9 450~530 380~470 8
>1.9~4.5 460~540 380~470 8
>4.5~6.0 480~560 400~490 8
>6.0~10.5 470~550 390~480 8
T73 0.5~1.9 430~530 345~420 8
>1.9~4.5 440~510 355~430 8
>4.5~10.5 450~520 375~450 8
0-T6 0.5~1.0 470 390 7
>1.0~6.0 480 400 6
>6.0~10.5 480 400 6
Aluminum Skin plate T6B 0.5~1.9 480 400 7 - 11-CL-026B
>1.9~6.0 490 400 7
>6.0~10.5 490 410 6
T74B 0.5~1.9 450~530 380~460 8
>1.9~4.5 460~540 380~460 8
>4.5~6.0 480~560 400~480 8
>6.0~10.5 470~550 390~470 8
T73B 0.5~1.9 430~550 345~420 8
>1.9~6.0 440~510 355~430 8
>6.0~10.5 450~520 375~450 8
T62B 0.5~1.9 470 390 7
>1.9~6.0 480 400 7
>6.0~10.5 480 400 6
pre-stretching aluminum plate T651 11~25 530 460 7 -
  1. CL-029B
   SWA/S1201-2002
26~50 530 460 6
51~60 520 440 5
61~80 490 420 4
T7451 11~50 490~560 420~500 7
51~60 470~540 380~460 6
61~85 460~530 365~440 6
T7351 11~50 470~540 400~480 7
51~60 450~520 365~440 6
61~85 440~510 345~420 6
Extruded Aluminum bar rod H112--T6 10~28 560 480 6 11-CL-031B
>28~150 570 490 6
>150~250 560 490 6
>250~300 550 480 6
T6 10~50 560 480 6
>50~100 570 490 6
Extruded aluminum profile H112--T6 ≤5 510 460   11-CL-028B
>5~10 520 470  
>10~75 540 480  
>75~112 540 470  
>112~125 520 450  
O--T6 ≤5 510 460  
>5~10 520 470  
>10~75 540 480  
>75~112 540 470  
>112~125 520 450  
T6 ≤5 510 460  
>5~10 530 480  
>10~75 550 490  
>75~112 550 480  
>112~125 530 460  
T74 ≤75 510~590 450~530  
>75~125 490~590 420~530  
T73 ≤5 460~530 390~460  
>5~40 480~550 420~490  
>40~75 470~540 400~470  
>75~125 460~530 390~460  
Extruded wallboard T6 All L:540 490 7 11-CL-030B
LT:510 - 6
T742 All 500~570 430~500 8
Die forgings T6 ≤75 L:510 430 6 L-T: 31.0
T-L: 21.7
S-L:18.6
 
LT:450 - 4
ST:410 - 3
>75~150 L:510 430 6
LT:450 - 4
ST:410 - 2
Free forgings T6 ≤75 L:490 410 6 -
LT:440 - 3
ST:390 - 2
>75~150 L:490 410 5
LT:440 - 3
ST:390 - 2
Die forgings T74 ≤75 L:490~580 430~520 6  
LT:460~540 410~490 4
ST:450~520 400~470 2
>75~100 L:480~570 420~510 6
LT:460~540 410~490 4
ST:450~520 390~470 2
Free forgings T74 ≤75 L:480~570 410~490 6  
LT:460~540 400~480 4
ST:450~520 390~470 2
>75~100 L:470~560 400~480 6
LT:460~540 390~470 4
ST:440~520 390~470 2
>100~125 L:450~540 390~470 6
LT:440~520 370~450 3
ST:420~500 380~460 2
Die forgings T73 ≤75 L:450~540 380~470 7 L-T: 35.7
T-L: 26.4
S-L:21.7
LT:440~520 370~450 5
ST:420~500 - 3
>75~100 L:440~530 370~460 7  
                   
 
Alloy Temper Aircraft Models Application parts and typical parts
7B04 Aluminum sheet:  T6,T74,T73,T6B,T74B,T73B,T62B.
Aluminum plate:T651,T7451,T7351
Aluminum profile: T6,T74,T73,T6,T742
Aluminum forgings:T6,T74,T73
Y8, Y12 Skin, wall board, all kinds of beams (backlog, forgings), frame, fin, long truss, joint, landing gear and so on.
Detailed Photos

7A04 T6 Aircraft Aerospace Extruded Aluminum Profiles for Aviation7A04 T6 Aircraft Aerospace Extruded Aluminum Profiles for Aviation7A04 T6 Aircraft Aerospace Extruded Aluminum Profiles for Aviation7A04 T6 Aircraft Aerospace Extruded Aluminum Profiles for Aviation7A04 T6 Aircraft Aerospace Extruded Aluminum Profiles for Aviation7A04 T6 Aircraft Aerospace Extruded Aluminum Profiles for Aviation


 

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