Hybrid ice-protection system for use on roughness-sensitive airfoils
    1.
    发明授权
    Hybrid ice-protection system for use on roughness-sensitive airfoils 失效
    用于粗糙度敏感翼型的混合冰保护系统

    公开(公告)号:US5921502A

    公开(公告)日:1999-07-13

    申请号:US665914

    申请日:1996-06-19

    IPC分类号: B64D15/00 B64D15/04 B64D15/16

    CPC分类号: B64D15/16 B64D15/163

    摘要: An electro-thermal or hot gas anti-icer of the "running-wet" type is mounted at the leading edge of an airfoil. Mechanical de-icers are mounted on the surfaces aft of the anti-icer. The mechanical de-icers throw off ice without creating runback water, thereby eliminating runback refreeze ridges caused by a known hybrid ice-protection system. Advantageously, the de-icers are of a type in which the airfoil has a semi-rigid skin that forms an aerodynamic surface of the airfoil, and in which there is at least one mechanical actuator for flexing the skin.

    摘要翻译: “跑步湿式”类型的电热或热气体防冰器安装在翼型的前缘。 机械除冰器安装在防冰板后面的表面上。 机械除冰器在不产生回流水的情况下扔冰,从而消除由已知的混合防冰系统引起的回流重冰脊。 有利地,除冰器是其中翼型件具有半刚性皮肤的类型,其形成翼型件的空气动力学表面,并且其中存在至少一个用于使皮肤弯曲的机械致动器。