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热词
    • 4. 发明授权
    • High strength and high rigidity aluminum-based alloy
    • 高强度高刚性铝基合金
    • US06017403A
    • 2000-01-25
    • US601949
    • 1996-02-15
    • Tsuyoshi MasumotoAkihisa InoueYuma Horio
    • Tsuyoshi MasumotoAkihisa InoueYuma Horio
    • C22C21/00
    • C22C21/00
    • An aluminum-based alloy having the general formula Al.sub.x L.sub.y M.sub.z (wherein L is Mn or Cr; M is Ni, Co, and/or Cu; and x, y, and z, representing a composition ratio in atomic percentages, satisfy the relationships x+y+z=100, 75.ltoreq.x.ltoreq.95, 2.ltoreq.y.ltoreq.15, and 0.5.ltoreq.z.ltoreq.10) having a metallographic structure comprising a quasi-crystalline phase possesses high strength and high rigidity. In order to enhance the ductility and toughness of the aluminum-based alloy, the atomic percentage of M may be further limited to 0.5.ltoreq.z.ltoreq.4, and more preferably to 0.5.ltoreq.z.ltoreq.3. The aluminum-based alloy is useful as a structural material for aircraft, vehicles and ships, and for engine parts; as material for sashes, roofing materials, and exterior materials for use in construction; or as materials for use in marine equipment, nuclear reactors, and the like.
    • 具有通式AlxLyMz(其中L是Mn或Cr; M是Ni,Co和/或Cu;和表示原子百分比的组成比的x,y和z)的铝基合金满足关系x + 具有包含准结晶相的金相组织的y + z = 100,75,或者= x,y = x,z = 100,75