首页> 外国专利> RESISTIVE HEATING CIRCUIT, AIRCRAFT STRUCTURE HEATED OR PROTECTED AGAINST ICE, AND METHOD FOR MANUFACTURING A RESISTIVE HEATING CIRCUIT.

RESISTIVE HEATING CIRCUIT, AIRCRAFT STRUCTURE HEATED OR PROTECTED AGAINST ICE, AND METHOD FOR MANUFACTURING A RESISTIVE HEATING CIRCUIT.

机译:电阻加热电路,针对冰的加热或保护的飞机结构,以及制造电阻加热电路的方法。

摘要

a resistive heating circuit for a heated or frost-protected aircraft structure includes a flexible dielectric substrate, a resistive heating element supported by the substrate and a busbar. the busbar is electrically connected to the resistive heating element and includes a conductive ink printed on the substrate, so that the busbar and the resistive heating element flex freely with the aircraft's structure heated or protected against frost. aircraft structures heated or protected against ice and methods of manufacturing resistive heating circuits for aircraft structures heated or protected against ice are also described.
机译:一种用于加热的或防霜的飞机结构的电阻加热电路,包括柔性介电基板,由该基板支撑的电阻加热元件和母线。母线电连接到电阻加热元件,并包括印刷在基板上的导电油墨,以便母线和电阻加热元件在飞机结构受热或防霜冻时自由弯曲。还描述了被加热或被防冰的飞机结构以及制造被加热或被防冰的飞机结构的电阻加热电路的方法。

著录项

  • 公开/公告号BR102019021677A2

    专利类型

  • 公开/公告日2020-05-26

    原文格式PDF

  • 申请/专利权人 GOODRICH CORPORATION;

    申请/专利号BR20191021677

  • 发明设计人 BRAD HARTZLER;

    申请日2019-10-15

  • 分类号B64F5/27;

  • 国家 BR

  • 入库时间 2022-08-21 11:18:31

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