AA 7010 Aluminum Alloy
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ファミリー: Aluminum Alloy
Zinc Alloy (Al-Zn). AA designation 7010.
性能評価
Performance Radar
| 特性 | Rating |
|---|---|
| Strength | 6 / 10 |
| Corrosion Res. | 6 / 10 |
| Lightweight | 9 / 10 |
| Machinability | 8 / 10 |
| Affordability | 7 / 10 |
| Heat Res. | 4 / 10 |
組成
機械的特性
| 引張強度 | 528.0 MPa |
| 降伏強度 | 480.0 MPa |
| 伸び | 12.0% |
| 硬度（ロックウェル） |
化学組成
| 元素 | 割合 (%) |
|---|---|
| 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 |
購入先 AA 7010 Aluminum Alloy
リンクから手数料が発生する場合がありますが、追加費用はかかりません。
説明
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.