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HIGH DUCTILITY AL-LI-ZR ALLOY

机译:high ductility AL-l i-ZR alloy

摘要

PURPOSE:To obtain the Al-Li alloy which is light in weight and having high ductility by adding B, C, N, P and S to an Al-Li-Zr alloy. CONSTITUTION:An alloy contg., by weight, 1.00 to 4.00% Li, 0.01 to 0.20% Zr and one or more kinds among 0.002 to 1.0% B, 0.01 to 1.0% C, 0.01 to 1.0% N, 0.001 to 1.0% P and 0.001 to 1.0% S and the balance Al with inevitable impurities is prepd. In this way, the Al-Li alloy having increased elongation without deteriorating the tensile strength can be used as an aircraft material.
机译:目的:通过向Al-Li-Zr合金中添加B,C,N,P和S,获得重量轻,延展性高的Al-Li合金。组成:一种合金,按重量计包含1.00至4.00%Li,0.01至0.20%Zr和0.002至1.0%B,0.01至1.0%C,0.01至1.0%N,0.001至1.0%P中的一种或多种S为0.001〜1.0%,余量为Al,不可避免地含有杂质。以此方式,具有增加的伸长率而不会降低拉伸强度的Al-Li合金可以用作飞机材料。

著录项

  • 公开/公告号JPH0310040A

    专利类型

  • 公开/公告日1991-01-17

    原文格式PDF

  • 申请/专利权人 SUMITOMO LIGHT METAL IND LTD;

    申请/专利号JP19890143010

  • 发明设计人 KAWABATA TAKESHI;

    申请日1989-06-07

  • 分类号C22C21/00;H01L21/60;

  • 国家 JP

  • 入库时间 2022-08-22 06:05:09

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