发明名称 2000 Series alloys with enhanced damage tolerance performance for aerospace applications
摘要 The invention provides a 2000 series aluminum alloy having enhanced damage tolerance, the alloy consisting essentially of about 3.0-4.0 wt % copper; about 0.4-1.1 wt % magnesium; up to about 0.8 wt % silver; up to about 1.0 wt % Zn; up to about 0.25 wt % Zr; up to about 0.9 wt % Mn; up to about 0.5 wt % Fe; and up to about 0.5 wt % Si, the balance substantially aluminum, incidental impurities and elements, said copper and magnesium present in a ratio of about 3.6-5 parts copper to about 1 part magnesium. The alloy is suitable for use in wrought or cast products including those used in aerospace applications, particularly sheet or plate structural members, extrusions and forgings, and provides an improved combination of strength and damage tolerance.
申请公布号 US2006011272(A1) 申请公布日期 2006.01.19
申请号 US20040893003 申请日期 2004.07.15
申请人 LIN JEN C;NEWMAN JOHN M;MAGNUSEN PAUL E;BRAY GARY H 发明人 LIN JEN C.;NEWMAN JOHN M.;MAGNUSEN PAUL E.;BRAY GARY H.
分类号 C22C21/12 主分类号 C22C21/12
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