Products name:
7075 is one of the highest strength aluminum alloys available Its strength-to weight ratio is excellent and it is ideally used for highly stressed parts. It may be formed in the annealed condition and subsequently heat treated. Spot or flash welding can be used, although arc and gas welding are not recommended. It is available in the clad ('Alclad") form to improve the corrosion resistance with the over-all high strength being only moderately affected. Applications: Used where highest strength is needed.
7000 series aircraft aluminum advantage
- 1. Reduce the fuel consumption
- 2. Improve the flight speed,
- 3. Increase the loading capacity
- 4. Reduce the airplane body weight ,with lightweight
Aluminum alloy sheet 7075 t7651 Product character:
- High strength,
- Excellent machining performance
- With heat treatment
Aluminum alloy sheet AA7075 t7651 Application :
- Tooling aluminum plates
- Machining fixtures, computer & electronics, mould cooling
- Plastic injection mold
- Aircraft structure
Product Description:
| Product Name | 7000 Series aluminum alloy sheet 7075 t7651 for Aircraft structure |
| Alloy | 7075 |
| Temper | T7651 |
| Thickness | 6.0-200 mm |
| Width | 800-4000 mm |
| Length | 1000~24000 |
| Surface | Be free from Oil Stain, Dent, Inclusion, Scratches, Stain, Oxide Discoloration, Breaks, Corrosion, Roll Marks, Dirt Streaks and other defect which will interfere with use. |
7000 series Chemical Composition (Standard:SAE AMS 4078)
| Alloy | Si | Fe | Cu | Mn | Mg | Cr | Zn | Zr | Ti | Standard |
| 7075 | 0.40 | 0.50 | 1.2-2.0 | 0.30 | 2.1-2.9 | 0.18-0.28 | 5.1-6.1 | 0.05 | 0.20 | En573 |
| 7475 | 0.10 | 0.12 | 1.2-1.9 | 0.06 | 1.9-2.6 | 0.18-0.25 | 5.2-6.2 | 0.05 | 0.06 | En573 |
| 7050 | 0.12 | 0.15 | 2.0-2.6 | 0.10 | 1.9-2.6 | 0.04 | 5.7-6.7 | 0.08-0.15 | 0.06 | En573 |
| 7B50 | 0.12 | 0.15 | 1.8-2.6 | 0.10 | 2.0-2.8 | 0.04 | 6.0-7.0 | 0.08-0.16 | 0.10 | - |
| 7A55 | 0.10 | 0.10 | 1.8-2.5 | 0.05 | 1.8-2.8 | 0.04 | 7.5-8.5 | 0.08-0.20 | 0.1-0.25 | |
7000 Series Mechanical properties (Standard SAE AMS 4078)
| Alloy | Temper | Typical Thickness | Tensile Strength | Yield Strength | Elongation | Standard |
| 7075 | T651 | 6.0~225.0 | 570 | 495 | 10 | SAE AMS 4045 |
| 7075 | T7651 | 6.0~150.0 | 500 | 420 | 10 | SAE AMS 4078 |
| 7475 | T7651 | 6.0~50.0 | 510 | 435 | 10 | SAE AMS 4089 |
| 7050 | T7451 | 6.0~225.0 | 530 | 460 | 10 | SAE AMS 4050 |
| 7050 | T7651 | 6.0~100.0 | 550 | 480 | 10 | SAE AMS 4201 |
| 7B50 | T6151 | 6.0~50.0 | 600 | 550 | 12 | ----- |
| 7B50 | T7751 | 6.0~100.0 | 590 | 540 | 10 | ----- |
| 7A55 | T7751 | 6.0~50.0 | 635 | 605 | 10 | ----- |
FAQ:
Q1: What's your payment term?
A: T/T 30% ,L/C at sight
Q2: Can you provide A4 sample FOR test?
A: Yes,we can.
Q4: Can we visit your factory with business trip ?
Yes ,You can .
Q5: Can you cut into small specification ?
A: Yes,we can cuting as per your specification request
Q6: May we have your MTC for material ?
A: Yes,we can
7075 t7651 Aluminum Plate :
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