首页> 外国专利> Porous high temp abradable seal - for gas turbine engines, comprises sintered iron, nickel or cobalt alloy

Porous high temp abradable seal - for gas turbine engines, comprises sintered iron, nickel or cobalt alloy

机译:多孔高温耐磨密封件-用于燃气轮机,包括烧结铁,镍或钴合金

摘要

A porous high temp. member, having an improved combination of oxidation and erosion resistance, controlled thermal conductivity and low elevated temp. flow stress which provides, upon rubbing contact with another member, a compliant base and a flowed continuous facing, comprises metallurgical bonded, metallographically distinguishable alloy powder particles in the size range of about +140 to -270 US Standard Sieve mesh. The alloy has the compsn. (by wt.) 15-35% Cr, 8-20% Al, up to 5% of one or more of Y, Hf and rare earth elements, balance Fe, Co and/or Ni. The member has 65-90% theoretical density.
机译:多孔的高温。该构件具有改进的抗氧化和抗侵蚀性,受控的导热性和较低的高温组合。在与另一构件摩擦接触时提供顺应性基底和流动的连续面层的流动应力包括尺寸为约+140至-270美国标准筛网的冶金结合的,金相学上可区分的合金粉末颗粒。合金具有成分。 (按重量计)15-35%的Cr,8-20%的Al,最多5%的Y,Hf和稀土元素中的一种或多种,​​其余为Fe,Co和/或Ni。成员具有65-90%的理论密度。

著录项

  • 公开/公告号IT1062508B

    专利类型

  • 公开/公告日1984-10-20

    原文格式PDF

  • 申请/专利权人 GENERAL ELECTRIC COMPANY;

    申请/专利号IT19760026213

  • 发明设计人

    申请日1976-08-11

  • 分类号F02C;

  • 国家 IT

  • 入库时间 2022-08-22 09:10:45

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