AA 7010 Aluminum Alloy
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กลุ่ม: Aluminum Alloy
Zinc Alloy (Al-Zn). AA designation 7010.
การให้คะแนนประสิทธิภาพ
Performance Radar
| สมบัติ | Rating |
|---|---|
| Strength | 6 / 10 |
| Corrosion Res. | 6 / 10 |
| Lightweight | 9 / 10 |
| Machinability | 8 / 10 |
| Affordability | 7 / 10 |
| Heat Res. | 4 / 10 |
องค์ประกอบ
สมบัติทางกล
| ความแข็งแรงแรงดึง | 528.0 MPa |
| ความแข็งแรงจุดคราก | 480.0 MPa |
| การยืดตัว | 12.0% |
| ความแข็ง (ร็อกเวลล์) |
องค์ประกอบทางเคมี
| ธาตุ | เปอร์เซ็นต์ (%) |
|---|---|
| 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 |
ซื้อได้ที่ไหน AA 7010 Aluminum Alloy
ลิงก์อาจได้รับค่าคอมมิชชันโดยไม่มีค่าใช้จ่ายเพิ่มเติมสำหรับคุณ
คำอธิบาย
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.