To provide an electrically-driven rotary-wing aircraft having improved safety during a flight.SOLUTION: An electrically-driven rotary-wing aircraft has an electrical driving part including a first motor, a first battery that has a first battery unit to be attached thereto in detachable manner and supplies the first motor with power from the first battery unit, and a second battery that has a second battery unit to be attached thereto in detachable manner and supplies the first motor with power from the second battery unit. The first and second batteries are disposed away from each other.SELECTED DRAWING: Figure 1

    【課題】飛行中の安全性が向上された電動回転翼航空機を提供すること。【解決手段】電動回転翼航空機は、第1のモーターを含む電動部と、第1のバッテリーユニットが着脱可能に装着され、第1のモーターに第1のバッテリーユニットから電力を供給する第1のバッテリー部と、第2のバッテリーユニットが着脱可能に装着され、第1のモーターに第2のバッテリーユニットから電力を供給する第2のバッテリー部と、を含み、第1のバッテリー部と第2のバッテリー部とは、離間した位置に配置されている。【選択図】図1


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    Title :

    ELECTRICALLY-DRIVEN ROTARY-WING AIRCRAFT


    Additional title:

    電動回転翼航空機


    Contributors:

    Publication date :

    2022-04-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

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



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