发明名称 ELEMENT DE STRUCTURE D'AVION EN ALLIAGE A1-CU-MG
摘要 <p>Weldable product, notably rolled, drawn or forged, is made in an alloy with the following composition (by weight %): (a) Cu: 3.8 - 4.3; (b) Mg: 1.25 - 1.45; (c) Mn: 0.2 - 0.5; (d) Zn: 0.4 - 1.3; (e) Fe less than 0.15; (f) Si less than 0.15; (g) Zr at most 0.05; (h) Ag less than 0.01; (i) other elements each less than 0.05 and less than 0.15 in total; (j) remainder Al; (k) treated by putting into solution, tempering and cold drawing, with a permanent deformation of between 0.5 and 15 %, and preferably of between 1.5 and 3.5 %. The cold drawing is achieved by controlled traction and/or cold transformation, such as rolling or drawing. Independent claims are also included for: (i) a plated sheet of this alloy; (ii) an aircraft structural element of this alloy; (iii) a method for the fabrication of a weldable product of this alloy.</p>
申请公布号 FR2842212(B1) 申请公布日期 2004.08.13
申请号 FR20020008737 申请日期 2002.07.11
申请人 PECHINEY RHENALU 发明人 WARNER TIMOTHY;DIF RONAN;BES BERNARD;RIBES HERVE
分类号 C22C21/16;C22C21/18;C22F1/057;(IPC1-7):C22C21/16;B64C1/12 主分类号 C22C21/16
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