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Pneumatic de-icer having improved aerodynamic characteristics

机译:具有改善的空气动力学特性的气动除冰器

摘要

A de-icer for attachment to an airfoil subject to impingement by an airstream. The airstream induces a stagnation line near the leading edge of the airfoil. The de-icer has inflatable passages that are parallel to the airstream overlying the airfoil on one side of the stagnation line, and inflatable passages that are parallel to the leading edge overlying the airfoil on the other side of the stagnation line. The de-icer maintains the aerodynamic characteristics of the airfoil during de-icer inflation. A method of manufacturing the de-icer is also provided.
机译:附着在机翼上的除冰剂,会受到气流的撞击。气流在机翼前缘附近产生停滞线。除冰器具有与在滞止线的一侧上覆盖翼型的气流平行的充气通道,以及与在滞止线的另一侧覆盖翼型的前缘平行的充气通道。除冰器在除冰器充气期间保持翼型的空气动力学特性。还提供了一种制造除冰器的方法。

著录项

  • 公开/公告号EP0658478B1

    专利类型

  • 公开/公告日1999-09-22

    原文格式PDF

  • 申请/专利权人 GOODRICH CO B F;

    申请/专利号EP19940111812

  • 发明设计人 ELY DUAIN NORVAN;MACARCHENIA JOSEPH HENRY;

    申请日1994-07-29

  • 分类号B64D15/16;

  • 国家 EP

  • 入库时间 2022-08-22 02:20:15

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