PROBLEM TO BE SOLVED: To provide a solid state power controller for an aircraft.SOLUTION: The invention relates to a solid state power controller 100 for an aircraft. The solid state power controller includes a solid state switching device for conduction of an electrical power output bus 160, a control unit 120 for controlling the solid state switching device, and a current sensing circuit 150 for monitoring current flowing in the electrical power output bus. The current sensing circuit includes a sensing fuse 140 to realize a simplified, more reliable solid state power controller.

    【課題】航空機用の固体電力制御装置を提供する。【解決手段】航空機用の固体電力制御装置100に関する。固体電力制御装置は、電力出力バス160を導通させるための固体スイッチング装置と、固体スイッチング装置を制御するための制御ユニット120と、電力出力バスを流れる電流を監視するための電流検出回路150とを備える。電流検出回路は、単純化された、より信頼性の高い固体電力制御装置を実現する検出ヒューズ140を含む。【選択図】図2


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    Title :

    SOLID STATE POWER CONTROLLER FOR AIRCRAFT


    Additional title:

    航空機用の固体電力制御装置


    Contributors:

    Publication date :

    2015-07-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H02H EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS , Schutzschaltungsanordnungen




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