PROBLEM TO BE SOLVED: To reduce the weight of an electric aircraft.SOLUTION: The present invention provides an electric aircraft comprising a plurality of rotary wings, a motor that rotates each of the rotary wings, a support shaft that supports each rotary wing and motor, a motor control unit that controls the rotation of each motor, a plurality of power supply lines that supply each pair of motors with power, and a plurality of battery modules each connected to a power supply line.SELECTED DRAWING: Figure 5

    【課題】電動式航空機を軽量化する。【解決手段】複数の回転翼と、回転翼をそれぞれ回転させるモータと、回転翼およびモータをそれぞれ支持する支持軸と、モータの回転を制御するモータ制御部と、モータの対毎に電力を供給する複数の電力供給ラインと、電力供給ライン毎に接続される複数のバッテリモジュールとを備えた電動式航空機である。【選択図】図5


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    Title :

    ELECTRIC AIRCRAFT AND POWER SUPPLY DEVICE


    Additional title:

    電動式航空機および電源装置


    Contributors:

    Publication date :

    2016-12-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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