发明名称 High toughness plate alloy for aerospace applications
摘要 The present invention is directed to highly controlled alloy composition relationship of a high purity Al-Mg-Cu alloy within the 2000 series aluminum alloys as defined by the Aluminum Association, wherein significant improvements are revealed in fracture toughness through plane strain, fracture toughness through plane stress, fatigue life, and fatigue crack growth resistance.
申请公布号 US6576071(B2) 申请公布日期 2003.06.10
申请号 US20020072365 申请日期 2002.02.07
申请人 ALCOA INC. 发明人 LIU JOHN;WESTERLUND ROBERT W.;BRAY GARY H.;THOM TERRENCE N.;CHAKRABARTI DHRUBA J.
分类号 C22C21/12;C22C21/16;C22F1/057;(IPC1-7):C22C21/06 主分类号 C22C21/12
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