AA 7010 Aluminum Alloy
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العائلة: Aluminum Alloy
Zinc Alloy (Al-Zn). AA designation 7010.
تقييمات الأداء
Performance Radar
| خاصية | Rating |
|---|---|
| Strength | 6 / 10 |
| Corrosion Res. | 6 / 10 |
| Lightweight | 9 / 10 |
| Machinability | 8 / 10 |
| Affordability | 7 / 10 |
| Heat Res. | 4 / 10 |
التركيب
الخصائص الميكانيكية
| مقاومة الشد | 528.0 MPa |
| حد الخضوع | 480.0 MPa |
| الاستطالة | 12.0% |
| الصلابة (روكويل) |
التركيب الكيميائي
| العنصر | النسبة المئوية (%) |
|---|---|
| Al | 89,47 |
| Cr | 0,05 |
| Cu | 1,69 |
| Fe | 0,09 |
| Mg | 2,35 |
| Mn | 0,05 |
| Si | 0,075 |
| Ti | 0,05 |
| Zn | 6,26 |
| Zr | 0,14 |
أين تشتري AA 7010 Aluminum Alloy
قد تكسب الروابط عمولة دون أي تكلفة إضافية عليك.
الوصف
AA 7010 is a high-strength aerospace aluminum-zinc-magnesium-copper alloy (~6.2% Zn, 2.3% Mg, 1.7% Cu) with zirconium addition to control grain structure, providing excellent combinations of strength, toughness, and resistance to stress corrosion cracking in thick plate. It is formulated specifically for thick structural plate where 7075 would exhibit reduced properties, and is typically used in T7651 or T7351 temper. Primary applications include aircraft upper wing skins, fuselage frames, spars, and heavy structural bulkheads.