发明名称 High-damage tolerant alloy product in particular for aerospace applications
摘要 The invention relates to an aluminium alloy wrought product with high strength and fracture toughness and high fatigue resistance and low fatigue crack growth rate, and having a composition for the alloy comprising, in weight %, about 0.3 to 1.0% magnesium (Mg), about 4.4 to 5.5% copper (Cu), about 0 to 0.20% iron (Fe), about 0 to 0.20% silicon (Si), about 0 to 0.40% zinc (Zn), and Mn in a range 0.15 to 0.8 as a dispersoids forming element in combination with one or more of dispersoids forming elements selected from the group consisting of: (Zr, Sc, Cr, Hf, Ag, Ti, V), in ranges of: about 0 to 0.5% zirconium (Zr), about 0 to 0.7% scandium (Sc), about 0 to 0.4% chromium (Cr), about 0 to 0.3% hafnium (Hf), about 0 to 0.4% titanium (Ti), about 0 to 1.0% silver (Ag), the balance being aluminium (Al) and other incidental elements, and whereby there is a limitation of the Cu-Mg content such that -1.1[Mg]+5.38<=[Cu]<=5.5. The invention further relates to a method of manufacturing such a product.
申请公布号 US2005081965(A1) 申请公布日期 2005.04.21
申请号 US20040855560 申请日期 2004.05.28
申请人 BENEDICTUS RINZE;KEIDEL CHRISTIAN J.;HEINZ ALFRED L.;HARGARTER HINRICH J.W. 发明人 BENEDICTUS RINZE;KEIDEL CHRISTIAN J.;HEINZ ALFRED L.;HARGARTER HINRICH J.W.
分类号 B64C1/12;B64C3/26;C22C21/12;C22C21/14;C22C21/16;C22C21/18;C22F1/057;(IPC1-7):C22C21/16 主分类号 B64C1/12
代理机构 代理人
主权项
地址