TURBINE COMPRESSOR BLADE TIP RESISTANT TO METAL TRANSFER
    1.
    发明申请
    TURBINE COMPRESSOR BLADE TIP RESISTANT TO METAL TRANSFER 审中-公开
    涡轮压缩机叶片对金属转移的抵抗力

    公开(公告)号:WO2014042724A3

    公开(公告)日:2014-06-05

    申请号:PCT/US2013045148

    申请日:2013-06-11

    Abstract: A gas turbine engine having an engine casing extending circumferentially about an engine centerline axis; and a compressor section, a combustor section, and a turbine section within said engine casing. At least one of said compressor section and said turbine section includes at least one airfoil and at least one seal member adjacent to the at least one airfoil, wherein a tip of the at least one airfoil is metal having a thin film ceramic coating and the at least one seal member is coated with an abrasive.

    Abstract translation: 一种燃气涡轮发动机,具有围绕发动机中心线轴线周向延伸的发动机壳体; 以及在所述发动机壳体内的压缩机部分,燃烧器部分和涡轮部分。 所述压缩机部分和所述涡轮机部分中的至少一个包括至少一个翼型件和与所述至少一个翼型件相邻的至少一个密封件,其中所述至少一个翼型件的末端是具有薄膜陶瓷涂层的金属, 至少一个密封件涂覆有磨料。

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