发明名称 Aluminium-copper-lithium sheet with high toughness for airplane fuselage
摘要 <p>The production of an aluminum alloy sheet with elevated tenacity and mechanical strength comprises: (A) preparing a bath of molten metal in which the copper and lithium contents are controlled; (B) casting a plate from the molten metal; (C) homogenizing the plate at 490-530 o>C for 5-60 hours; (D) rolling the plate to form a sheet with a thickness of 0.8-12 mm; (E) putting into solution and tempering the sheet; (F) the controlled drawing of the sheet with a permanent deformation of 1-5 %; and (G) tempering the sheet at 140-170 o>C for 5-30 hours. Independent claims are also included for the following: (1) a rolled, extrudes and/or forged product of this Al alloy; (2) an Al alloy sheet; and (3) structural elements fabricated from the product.</p>
申请公布号 EP2017361(A1) 申请公布日期 2009.01.21
申请号 EP20080018130 申请日期 2006.06.02
申请人 ALCAN RHENALU 发明人 BES, BERNARD;RIBES, HERVE;SIGLI, CHRISTOPHE;WARNER, TIMOTHY
分类号 C22C21/12;B64C1/00;C22F1/057 主分类号 C22C21/12
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