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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:US11976347B2
公开(公告)日:2024-05-07
申请号:US16627970
申请日:2018-06-28
Applicant: CONSTELLIUM ISSOIRE
Inventor: Ricky Whelchel , Erembert Nizery , Diana Koschel , Jean-Christophe Ehrstrom , Alireza Arbab
Abstract: The invention concerns an extruded, rolled and/or forged aluminum-based alloy product having a thickness of at least 25 mm comprising (in weight %): Zn 6.70-7.40; Mg 1.50-1.80; Cu 2.20-2.60, with a Cu to Mg ratio of at least 1.30; Zr 0.04-0.14; Mn 0-0.5; Ti 0-0.15; V 0-0.15; Cr 0-0.25; Fe 0-0.15; Si 0-0.15; impurities ≤0.05 each and ≤0.15 total. The invention also concerns a method of making such a product. Products according to the invention are particularly advantageous because they exhibit simultaneously a low sensitivity to environmentally assisted cracking under conditions of high stress and humid environment, high strength and high toughness properties.
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33.
公开(公告)号:US20240035137A1
公开(公告)日:2024-02-01
申请号:US18254386
申请日:2021-12-16
Applicant: CONSTELLIUM ISSOIRE
Inventor: Melanie OLLAT , Jean-Christophe EHRSTROM
Abstract: A method for thermomechanical treatment of wrought products made of a 2000 series aluminum alloy comprising, in % by weight, Cu 3.5-5.8; Mg 0.2-1.5; Mn≤0.9; Fe≤0.15; Si≤0.15; Zr≤0.25; Ag≤0.8; Zn≤0.8; Ti 0.02-0.15; unavoidable impurities≤0.05 each and ≤0.15 total; remainder aluminum, enabling an improvement in the resistance to corrosion under stress. It includes a tempering consisting of two sequences. The first sequence is defined by a maximum temperature T1max comprised between 130° C. and 180° C. and by a hold time at a temperature comprised between 130° C. and 180° C. which equates to an equivalent duration t1eq160+ C. calculated at 160° C. comprised between 10 h and 80 h. The second sequence is defined by a temperature T2° C.(t) lower than T1max and a hold time t2 at a temperature comprised between 100° C. and 130° C., which equates to an equivalent time t2eq160° C. calculated at 160° C. such that t2eq160° comprised between 0.3% and 15% of the equivalent duration t1eq160° calculated for the first sequence.
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34.
公开(公告)号:US20230220530A1
公开(公告)日:2023-07-13
申请号:US18000322
申请日:2021-05-31
Applicant: CONSTELLIUM ISSOIRE
Inventor: Pablo LORENZINO , Lukasz DOLEGA
Abstract: The invention relates to the use of a wrought aluminum alloy in a T8 temper with the following composition, in wt %, Cu: 3.6-4.4; Mg: 1.2-1.4; Mn: 0.5-0.8; Zr:≤0.15; Ti: 0.01-0.15; Si≤0.20; Fe≤0.20; Zn≤0.25 other elements
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公开(公告)号:US20220389557A1
公开(公告)日:2022-12-08
申请号:US17765345
申请日:2020-09-29
Applicant: CONSTELLIUM ISSOIRE , CONSTELLIUM VALAIS SA (LTD)
Inventor: Sylvie ARSENE , Petar RATCHEV , Nicolas CALABRETTO , Christophe JAQUEROD
Abstract: The present invention relates to plates with a thickness of between 8 and 50 mm and made from aluminum alloy with a composition, as % by weight, Si: 0.7-1.3; Mg: 0.6-1.2; Mn: 0.65-1.0; Fe: 0.05-0.35; at least one element selected from Cr: 0.1-0.3 and Zr: 0.06-0.15; Ti
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公开(公告)号:US20210396636A1
公开(公告)日:2021-12-23
申请号:US17421355
申请日:2019-12-19
Applicant: CONSTELLIUM ISSOIRE
Inventor: Pablo LORENZINO , Nicolas BAYONA-CARRILLO
Abstract: The invention involves a method for testing a damage tolerance property in an aluminum alloy part with the following steps: measure at least one property representative of a the part's tensile strength; use the property measured in step a) as input datum (xi) of a neural network estimator; estimate, using the estimator, the representative property of the part's tensile strength; the method being characterized in that it includes: consideration of an acceptance threshold and comparison of the property estimated at step c) to the acceptance threshold, taking into account a confidence interval; based on the comparison: consider that the part passes the test; or consider that the part does not pass the test.
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37.
公开(公告)号:US20210016869A1
公开(公告)日:2021-01-21
申请号:US17061055
申请日:2020-10-01
Applicant: CONSTELLIUM ISSOIRE
Inventor: Nicolas BAYONA-CARRILLO
Abstract: The invention relates to a method for manufacturing a laminated or forged material, the thickness of which is 14 to 100 mm. The materials according to the invention are particularly suitable for manufacturing airplane underwing elements.
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公开(公告)号:US20200032378A1
公开(公告)日:2020-01-30
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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公开(公告)号:US10400312B2
公开(公告)日:2019-09-03
申请号:US15025147
申请日:2014-09-26
Applicant: CONSTELLIUM ISSOIRE
Inventor: Bernard Bes
Abstract: The invention relates to a rolled product with state T351, having thickness of between 15 and 50 mm, made from aluminum alloy having the following composition, in % by weight, Cu: 3.85-4.15; Mg: 0.95-1.25; Mn: 0.45-0.57; Zr: 0.09-0.16; Ti: 0.005-0.1; Fe:
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公开(公告)号:US20190136356A1
公开(公告)日:2019-05-09
申请号:US16213328
申请日:2018-12-07
Applicant: Constellium Issoire
Inventor: Fabrice HEYMES , Frank EBERL , Gaelle POUGET
Abstract: The present invention relates to extruded, rolled and/or forged products. Also provided are methods of making such products based on aluminum alloy wherein a liquid metal bath is prepared comprising 2.0 to 3.5% by weight of Cu, 1.4 to 1.8% by weight of Li, 0.1 to 0.5% by weight of Ag, 0.1 to 1.0% by weight of Mg, 0.05 to 0.18% by weight of Zr, 0.2 to 0.6% by weight of Mn and at least one element selected from Cr, Sc, Hf and Ti, the quantity of said element selected, being 0.05 to 0.3% by weight for Cr and for Sc, 0.05 to 0.5% by weight for Hf and 0.01 to 0.15% by weight for Ti, the remainder being aluminum and inevitable impurities. The products and methods of the present invention offer an advantageous compromise between static mechanical strength and damage tolerance and are useful in aeronautical design.
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