To provide systems and methods that allow improved bus bars.SOLUTION: A resistive heating circuit for a heated or ice-protected aircraft structure includes a flexible dielectric substrate, a resistive heating element supported by the substrate, and a bus bar. The bus bar is electrically connected to the resistive heating element and includes a conductive ink printed onto the substrate such that the bus bar and resistive heating element flex freely with the heated or ice-protected aircraft structure. Heated or ice-protected aircraft structures and methods of making resistive heating circuits for heated or ice-protected aircraft structures are also described.SELECTED DRAWING: Figure 1

    【課題】 改善されたバスバーを可能にするシステム及び方法を提供する。【解決手段】 加熱または防氷航空機構造のための抵抗加熱回路が、可撓性誘電体基板と、基板によって支持される抵抗加熱素子と、バスバーと、を含む。バスバー及び抵抗加熱素子が、加熱または防氷航空機構造とともに自由に曲がるように、バスバーは、抵抗加熱素子に電気的に接続され、基板上にプリントされた導電性インクを含む。加熱または防氷航空機構造、及び加熱または防氷航空機構造のための抵抗加熱回路を作成する方法もまた、説明される。【選択図】図1


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    Title :

    RESISTIVE HEATING CIRCUIT, HEATED OR ICE-PROTECTED AIRCRAFT STRUCTURES AND METHODS OF MAKING RESISTIVE HEATING CIRCUITS


    Additional title:

    抵抗加熱回路、加熱または防氷航空機構造、および抵抗加熱回路の作成方法


    Contributors:

    Publication date :

    2020-04-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H05B ELECTRIC HEATING , Elektrische Heizung



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