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公开(公告)号:US20200165707A1
公开(公告)日:2020-05-28
申请号:US16619419
申请日:2018-06-05
Applicant: CONSTELLIUM ISSOIRE
Inventor: Ricky WHELCHEL , Mathieu REVIL-BAUDARD , Philippe JARRY , Bernard BES , Fanny MAS
Abstract: An aluminium alloy comprising lithium with improved mechanical strength and toughness. The invention relates to a 2XXX wrought alloy product comprising from 0.05 to 1.9% by weight of Li and from 0.005 to 0.045% by weight of Cr and/or of V. The invention also relates to an as-cast 2XXX alloy product comprising from 0.05 to 1.9% by weight of Li and from 0.005 to 0.045% by weight of Cr and/or of V. Finally, the invention relates to an aircraft structure element, preferably a lower surface or upper surface element, the skin and stiffeners of which originate from the same starting material, a spar or a rib, comprising a wrought product.