首页> 外国专利> ALUMINUM-MAGNESIUM ALLOY WITH HIGH CONTENT IN MAGNESIUM, RESISTANT TO CORROSION, IN PARTICULAR FOR APPLICATION IN AERONAUTICS.

ALUMINUM-MAGNESIUM ALLOY WITH HIGH CONTENT IN MAGNESIUM, RESISTANT TO CORROSION, IN PARTICULAR FOR APPLICATION IN AERONAUTICS.

机译:铝镁合金,镁含量高,耐腐蚀,特别适用于航空领域。

摘要

Magnesium-aluminum alloy with high magnesium content, weldable, resistant to corrosion, which contains a ternary aluminum-scandium-zirconium phase, composed of 5-6% by weight of magnesium (Mg), 0.05-0 , 15% by weight of zirconium (Zr), 0.05-0, 12% by weight of manganese (Mn), 0.01-0, 2% by weight of titanium, 0.05-0, 5% by weight of one or several elements of the group consisting of scandium (Sc), terbium (Tb) and lanthanides, especially cerium (Ce), where at least the scandium (Sc), 0, 1-0, 2% by weight of copper (Cu) and / or 0, 1-0, 4% by weight of zinc (Zn) as well as the rest of aluminum (Al) and unavoidable impurities with a maximum of 0.1% by weight of silicon (Si) .
机译:镁含量高,可焊接,耐腐蚀的镁铝合金,包含三元铝-scan-锆相,其中镁含量为5-6%(重量),镁含量为0.05-0、15%(重量) (Zr),0.05-0,按重量计12%的锰(Mn),0.01-0,按重量计2%的钛,0.05-0,按重量计5%的一种或几种of(Sc ),ter(Tb)和镧系元素,尤其是铈(Ce),其中至少((Sc),0、1-0、2%重量的铜(Cu)和/或0、1-0、4%重量的锌(Zn)以及其余的铝(Al)和不可避免的杂质,其最大含量为硅(Si)的0.1%。

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