发明名称 |
DAMAGE TOLERANT ALUMINUM ALLOY SHEET FOR AIRCRAFT SKIN |
摘要 |
Disclosed is a method of producing a sheet product having improved levels of toughness and fatigue crack growth resistance while maintaining high strength, comprising providing a body of an aluminum base alloy containing 9.0 to 4.5 wt.% Cu, 1.2 to 1.5 wt.% Mg, 0.4 to 0.6 wt.% Mn, 0.12 wt.% max. Fe, 0.05 wt.% max. Si, the remainder aluminum, incidental elements and impurities and heating a body of the alloy to above 910.degree.F to dissolve soluble constituents. Thereafter, the body is hot rolled in the range of about 600 to 900.degree.F, solution heat treated for a time of less than about 15 minutes at a solution heat treating temperature, and rapidly cooled and naturally aged to provide a sheet product with improved levels of fatigue crack growth resistance while maintaining high strength.
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申请公布号 |
CA2049840(A1) |
申请公布日期 |
1992.02.28 |
申请号 |
CA19912049840 |
申请日期 |
1991.08.26 |
申请人 |
COLVIN, EDWARD L.;PETIT, JOCELYN I.;WESTERLUND, ROBERT W. |
发明人 |
COLVIN, EDWARD L.;PETIT, JOCELYN I.;WESTERLUND, ROBERT W. |
分类号 |
C22C21/12;B32B15/01;C22C21/16;C22F1/00;C22F1/057;(IPC1-7):C22F1/057 |
主分类号 |
C22C21/12 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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