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An electrothermal heater of thermally conductive, electrically insulating polymer material

机译:导热,电绝缘聚合物材料的电热加热器

摘要

It is to be thermally conductive films, composite materials, the films, and an electrothermal heating devices is disclosed, the films include. The films a polymer and a sufficient concentration of hexagonal boron nitride, in order to provide appropriate heat transfer properties, and they have a high thermal conductivity, peel strength and resistance to. The films may be thermoset polymers, thermoplastic polymers or mixtures thereof, and they can also be electrically conductive materials, reinforcing materials, such as, for example, glass fiber material, carbon fibers, metal braiding 4 and the like, and thermally conductive fillers, such as, for example, aluminum oxide, aluminum nitride and the like. The films can be enclosed in composite materials. The films can be used as part of a layer structure (100) are used, and they can be essentially in the case of any use can be used, for example at different locations in the aircraft, where a heater is desirable, including the outer skins of the engine pods, wing of the aircraft, heated floor panels and the like. The electrothermal heating devices provide a more uniform heat and a more rapid heat than the current resistance heating devices, which is made of metal foils are formed, which adhere to an adhesive film.
机译:将是导热膜,复合材料,膜,并且公开了一种电热加热装置,所述膜包括。该膜为聚合物和足够浓度的六方氮化硼,以提供适当的传热性能,并且它们具有高的热导率,剥离强度和耐热性。膜可以是热固性聚合物,热塑性聚合物或其混合物,并且它们也可以是导电材料,增强材料,例如玻璃纤维材料,碳纤维,金属编织物4等,以及导热填料,例如氧化铝,氮化铝等。可以将薄膜封装在复合材料中。所述膜可以用作所使用的层结构(100)的一部分,并且它们基本上可以在任何用途的情况下使用,例如在飞机上需要加热器的不同位置,包括外部发动机舱的外壳,飞机机翼,加热的地板等。与形成于金属箔上的电流电阻加热装置相比,电热加热装置提供更均匀的热量和更快的热量,所述电流电阻加热装置由金属箔制成,该金属箔粘附在粘合膜上。

著录项

  • 公开/公告号DE102007061548A1

    专利类型

  • 公开/公告日2008-07-10

    原文格式PDF

  • 申请/专利权人

    申请/专利号DE20071061548

  • 发明设计人

    申请日2007-12-20

  • 分类号C08K3/38;C08K3/04;C08K3/08;C08K7/00;C08J5/18;B64D15/12;

  • 国家 DE

  • 入库时间 2022-08-21 19:49:09

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