SYNERGETIC NOISE ABSORPTION AND ANTI-ICING FOR AIRCRAFTS
    1.
    发明公开
    SYNERGETIC NOISE ABSORPTION AND ANTI-ICING FOR AIRCRAFTS 审中-公开
    ENTEISUNGFÜRFLUGZEUGE的SYNERGISTISCHEGERÄUSCHABSORPTION

    公开(公告)号:EP3135587A1

    公开(公告)日:2017-03-01

    申请号:EP16176603.5

    申请日:2016-06-28

    IPC分类号: B64D15/12 B64D29/00 B64D33/02

    摘要: Systems and methods are provided for an inductive coil anti-icing and noise absorption system. In certain versions, the inductive coil anti-icing and noise absorption system may include an inductive coil and a skin. The inductive coil may generate electromagnetic fields and may electromagnetically couple with the skin. The skin, upon electromagnetically coupling with the inductive coil, may increase in temperature and the increase in temperature may melt or prevent the formation of ice on the skin. The skin or a portion of the skin may be porous and may allow incorporation of a sound absorbing liner. The sound absorbing liner may attenuate noise generated by the aircraft (e.g., noise generated by the aircraft engine). Certain versions may include a plurality of inductive coils and a plurality of skins.

    摘要翻译: 为感应线圈防冰和噪声吸收系统提供了系统和方法。 在某些版本中,感应线圈防冰和噪声吸收系统可以包括感应线圈和皮肤。 感应线圈可以产生电磁场并且可以与皮肤电磁耦合。 皮肤在与感应线圈电磁耦合时可能会升高温度,并且温度升高可能会熔化或防止皮肤上形成冰。 皮肤或皮肤的一部分可以是多孔的,并且可以允许结合吸音衬垫。 吸音衬垫可以衰减飞行器产生的噪音(例如飞机发动机产生的噪音)。 某些版本可以包括多个感应线圈和多个皮肤。