发明名称 produto laminado em liga de alumínio-lítio para aplicações aeronáuticas
摘要 <p>The present invention is directed to a substantially unrecrystallized rolled aluminum alloy product, obtained from a plate with a thickness of at least 30 mm, comprising 2.2 to 3.9 wt. % Cu, 0.7 to 2.1 wt. % Li, 0.2 to 0.8 wt. % Mg, 0.2 to 0.5 wt. % Mn, 0.04 to 0.18 wt. % Zr, less than 0.05 wt. % Zn, and optionally 0.1 to 0.5 wt. % Ag, remainder aluminum and unavoidable impurities having a low propensity to crack branching during L-S a fatigue test. A product of the invention has a crack deviation angle Theta of at least 20° under a maximum equivalent stress intensity factor Keff max of 10 MPa √m for a S-L cracked test sample under a mixed mode I and mode II loading wherein the angle Psi between a plane perpendicular to the initial crack direction and the load direction is 75°</p>
申请公布号 BRPI0821569(A2) 申请公布日期 2015.09.08
申请号 BR2008PI21569 申请日期 2008.12.19
申请人 ALCAN RHENALU 发明人 ARMELLE DANIELOU;JEAN-CHRISTOPHE EHRSTROM
分类号 C22C21/12;C22F1/057 主分类号 C22C21/12
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