首页> 外国专利> New quenched and stretched aluminum-copper-magnesium alloy product, for aircraft wing intrados skin and wing or fuselage intrados strut manufacture has a large plastic deformation range

New quenched and stretched aluminum-copper-magnesium alloy product, for aircraft wing intrados skin and wing or fuselage intrados strut manufacture has a large plastic deformation range

机译:新的淬火和拉伸铝铜镁合金产品,用于飞机机翼内腔蒙皮以及机翼或机身内腔内支杆的制造,具有较大的塑性变形范围

摘要

A quenched and stretched wrought aluminum-copper-magnesium alloy product, having a specified composition and having a large plastic deformation range, is new. A rolled, extruded or forged AlCuMg alloy product, which has been solution treated, quenched and cold stretched and which is used for manufacture of aircraft structural elements, contains (by wt.) less than 0.15% Fe, less than 0.15% Si, 3.8-4.4(preferably 4.0-4.3)% Cu, 1-1.5% Mg, 0.5-0.8% Mn, 0.08-0.15% Zr and less than 0.05% each (less than 0.15% total) of other elements and has a Rm(L)/R0.2(L) ratio of greater than 1.25, preferably greater than 1.30. An Independent claim is also included for a process for producing the above product
机译:具有特定成分且塑性变形范围大的淬火拉伸铝-铜-镁合金锻造产品是新的。经过固溶处理,淬火和冷拉伸并用于制造飞机结构元件的轧制,挤压或锻造AlCuMg合金产品,其含量(按重量计)小于0.15%的铁,小于0.15%的硅,3.8 -4.4(最好是4.0-4.3)%的Cu,1-1.5%的Mg,0.5-0.8%的Mn,0.08-0.15%的Zr和其他元素各自小于0.05%(总量小于0.15%),并且具有Rm(L /R0.2(L)之比大于1.25,优选大于1.30。还包括针对上述产品的生产过程的独立权利要求

著录项

  • 公开/公告号FR2789405A1

    专利类型

  • 公开/公告日2000-08-11

    原文格式PDF

  • 申请/专利权人 PECHINEY RHENALU;

    申请/专利号FR19990001468

  • 申请日1999-02-04

  • 分类号C22C21/16;C22F1/057;

  • 国家 FR

  • 入库时间 2022-08-22 01:39:38

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