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 4.0 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 DEG F to dissolve soluble constituents. Thereafter, the body is hot rolled in the range of about 600 to 900 DEG 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. <IMAGE>
申请公布号 AU8270491(A) 申请公布日期 1992.03.05
申请号 AU19910082704 申请日期 1991.08.26
申请人 ALUMINUM COMPANY OF AMERICA 发明人 EDWARD L. COLVIN;JOCELYN I. PETIT;ROBERT W. WESTERLUND
分类号 C22C21/12;B32B15/01;C22C21/16;C22F1/00;C22F1/057 主分类号 C22C21/12
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