发明名称 ALUMINUM-COPPER-LITHIUM ALLOY PRODUCT FOR A LOWER WING SKIN ELEMENT WITH IMPROVED PROPERTIES
摘要 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.
申请公布号 US2016368589(A1) 申请公布日期 2016.12.22
申请号 US201415100768 申请日期 2014.12.02
申请人 CONSTELLIUM ISSOIRE 发明人 BAYONA-CARRILLO Nicolas
分类号 B64C3/26;B21J1/00;C22F1/057;B21B3/00;C22C21/16;C22C21/14 主分类号 B64C3/26
代理机构 代理人
主权项 1. Method of manufacturing a rolled or forged product in which: (a) a slab of alloy is cast, of composition, as a percentage by weight, Cu: 1.8-2.6 Li: 1.3-1.8 Mg: 0.1-0.5 Mn: 0.1-0.5 and Zr<0.05 or Mn<0.05 and Zr 0.10-0.16 Ag: 0-0.5 Zn<0.20 Ti: 0.01-0.15 Fe: <0.1 Si: ≦0.1 other elements <0.05 each and <0.15 total, the remainder aluminum with a density less than 2.670 g/cm3, (b) said slab is homogenized at 480 to 540° C. for 5 to 60 hours, (c) said slab is hot worked by rolling and/or forging, the hot working conditions being such when the manganese content is 0.1 to 0.5% by weight and the zirconium content is less than 0.05% by weight the final hot working temperature is at least 400° C. or when the manganese content is less than 0.05% by weight and the zirconium content is between 0.10 and 0.16% by weight the final hot working temperature is at the most 400° C. to obtain a rolled and/or forged product having a thickness of between 14 and 100 mm, (d) said product is solution-heat treated at 490 to 530° C. for 15 minutes to 8 hours, (e) quench said product with water, (f) said product undergoes controlled stretching with a permanent deformation of 1 to 6%, (g) said product is artificially aged by heat treatment at 120 to 170° C. for 5 minutes to 100 hours.
地址 Issoire FR