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1.
公开(公告)号:US11174535B2
公开(公告)日:2021-11-16
申请号:US15515891
申请日:2015-10-01
Applicant: CONSTELLIUM ISSOIRE
Inventor: Juliette Chevy , Bernard Bes , Frank Eberl
Abstract: The invention relates to a plate with a thickness of 0.5 to 9 mm with an essentially recrystallized granular structure, made from an alloy based on aluminum, comprising 2.8 to 3.2% by weight Cu, 0.5 to 0.8% by weight Li, 0.1 to 0.3% by weight Ag, 0.2 to 0.7% by weight Mg, 0.2 to 0.6% by weight Mn, 0.01 to 0.15% by weight Ti, a quantity of Zn below 0.2% by weight, a quantity of Fe and Si of less than or equal to 0.1% by weight each, and unavoidable impurities to a proportion of less than or equal to 0.05% by weight each and 0.15% by weight in total, said plate being obtained by a method comprising casting, homogenization, hot rolling and optionally cold rolling, solution heat treatment, quenching and aging. The plates according to the invention are advantageous in particular for the manufacture of aircraft fuselage panels.
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公开(公告)号:US12065720B2
公开(公告)日:2024-08-20
申请号:US17284373
申请日:2019-10-07
Applicant: CONSTELLIUM ISSOIRE
Inventor: Juliette Chevy , Jean-Christophe Ehrstrom , Pablo Lorenzino
Abstract: The invention relates to a thin metal sheet which is made of an alloy based on substantially recrystallized aluminum and which has a thickness of 0.25 to 12 mm, the alloy comprising, in percent by weight, Cu 3.4-4.0; Mg 0.5-0.8; Mn 0.1-0.7; Fe #0.15; Si #0.15; Zr #0.04; Ag #0.65; Zn #0.5; inevitable impurities #0.05 each and #0.15 in total, the remainder consisting of aluminum. The invention also relates to a process for manufacturing such a metal sheet and to the use thereof as a fuselage panel or sheet metal for the production of composite products such as fiber metal laminates (FML) for wing or fuselage applications in the aeronautical industry.
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公开(公告)号:US11667997B2
公开(公告)日:2023-06-06
申请号:US16603703
申请日:2018-04-09
Applicant: CONSTELLIUM ISSOIRE
Inventor: Juliette Chevy , Philippe Jarry , Soizic Blais , Alireza Arbab
Abstract: The invention relates to a product made of an aluminium-based alloy comprising, by wt. %, Cu: 2.4-3.2; Li: 1.6-2.3; Mg: 0.3-0.9; Mn: 0.2-0.6; Zr: 0.12-0.18; such that Zr≥−0.06 *Li+0.242; Zn:
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