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HEATABLE FLOOR PANEL AND FLOOR HEATING SYSTEM FOR AN AIRCRAFT

机译:飞机的可加热地板面板和地板加热系统

摘要

A heatable floor panel for an aircraft, with a supporting level, a heat-generating level and a heat-conducting level. The heat-generating level comprises a fiber composite layer with fibers and with a matrix surrounding the fibers. The fibers are at least partially formed as conducting fiber, and the conducting fibers are formed as carbon fibers with an electrically insulating coating. The conducting fibers integrated in the floor panel in order to conduct a heating current through them. Due to the electrically insulating coating of the conducting fibers, leakage currents are avoided. The carbon fibers serve not only as heating elements, but, at the same time, also as reinforcing fibers of the fiber composite layer or of the floor panel.
机译:用于飞机的可加热地板面板,具有支撑水平,发热水平和导热水平。发热层包括具有纤维和围绕纤维的基质的纤维复合层。纤维至少部分地形成为导电纤维,并且导电纤维形成为具有电绝缘涂层的碳纤维。导电纤维集成在地板中,以便通过它们传导热电流。由于导电纤维的电绝缘涂层,避免了泄漏电流。碳纤维不仅用作加热元件,而且同时还用作纤维复合材料层或地板的增强纤维。

著录项

  • 公开/公告号US2019309960A1

    专利类型

  • 公开/公告日2019-10-10

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS GMBH;

    申请/专利号US201916359486

  • 发明设计人 MATTHIAS HEGENBART;PETER LINDE;

    申请日2019-03-20

  • 分类号F24D13/02;B64C1/18;

  • 国家 US

  • 入库时间 2022-08-21 12:07:14

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