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Blade and method for reloading an abradable coating

机译:用于重新加载可磨损涂层的叶片和方法

摘要

The invention relates to a blade (16), in particular a fan blade, for resurfacing an abradable coating (26) on an internal surface of a turbine engine case (18) intended to surround the blade. The comprises a root (20) and an airfoil (24) having a tip opposite the root, said root comprising a housing (32) for the storage or passage of a polymerisable refill resin. The airfoil comprises longitudinal channels (34), the first ends of said channels being connected to the housing and the opposite ends opening at the aforementioned tip.
机译:本发明涉及一种叶片( 16 ),特别是风扇叶片,用于在涡轮发动机壳体的内表面上重新锻造可磨蚀的涂层( 26 )( 18 )旨在围绕刀片。包括具有与根部相对的尖端的根( 20 )和翼型( 24 / b>),所述根包括壳体( 32

著录项

  • 公开/公告号US10982560B2

    专利类型

  • 公开/公告日2021-04-20

    原文格式PDF

  • 申请/专利权人 SAFRAN AIRCRAFT ENGINES;

    申请/专利号US201716092733

  • 发明设计人 MICHAEL ISEMENE;ALEXANDRE BRANCO;

    申请日2017-04-10

  • 分类号F01D11/12;F01D5/14;F01D5/20;F01D5/30;

  • 国家 US

  • 入库时间 2022-08-24 18:17:25

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