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Magnesium-lithium alloy, method of manufacturing magnesium-lithium alloy, aircraft part, and method of manufacturing aircraft part

机译:镁锂合金,镁锂合金的制造方法,飞机零件以及飞机零件的制造方法

摘要

According to one implementation, a magnesium-lithium alloy in which at least lithium is added to magnesium is manufactured by giving a strain to a magnesium-lithium alloy workpiece, after a solution treatment, and progressing an aging of the magnesium-lithium alloy workpiece without a heat treatment. The strain is given by a cold working. The aging is progressed after giving the strain. Further, according to one implementation, an aircraft part includes the above-mentioned magnesium-lithium alloy as a material. Further, according to one implementation, a method of manufacturing an aircraft part includes processing the above-mentioned magnesium-lithium alloy.
机译:根据一种实施方式,通过在固溶处理后对镁锂合金工件施加应变,并使镁锂合金工件在不经过固溶处理的情况下进行时效,来制造其中至少向锂中添加了锂的镁锂合金。热处理。应变是通过冷加工产生的。施加应变后,老化得以进行。此外,根据一种实施方式,飞机部件包括上述镁-锂合金作为材料。此外,根据一种实施方式,一种制造飞机部件的方法包括处理上述镁-锂合金。

著录项

  • 公开/公告号US10752981B2

    专利类型

  • 公开/公告日2020-08-25

    原文格式PDF

  • 申请/专利权人 FUJI JUKOGYO KABUSHIKI KAISHA;

    申请/专利号US201615062507

  • 发明设计人 AYAKO MIURA;

    申请日2016-03-07

  • 分类号C22F1/06;C22C23;B62D29;

  • 国家 US

  • 入库时间 2022-08-21 11:30:41

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