To provide a tail-sitter-type electric aircraft configured so that stability of a posture of the aircraft in a rotary wing mode can be improved and wiring leading to an electric motor and a connection part thereof can be suppressed from being damaged.SOLUTION: A tail sitter-type electric aircraft 10 is equipped with first propellers 4 that can generate lifting power required for the aircraft to take off and land in a rotary wing mode in which a nose of the aircraft is pointed upward, in which a plurality of second propellers 9 that can generate thrust force in directions different from each other, in a substantially horizontal direction in the rotary wing mode are provided at side surfaces of the aircraft.SELECTED DRAWING: Figure 1

    【課題】回転翼モードにおける機体の姿勢の安定性を向上させると共に、電気モータへ繋がる配線やその接続部が破損することを抑制できるテイルシッター型電動航空機を提供する。【解決手段】機首を上方へ向けた回転翼モードで離着陸するために必要な揚力を発生させることができる第1プロペラ4を備えるテイルシッター型電動航空機10であって、互いに異なる方向へ向かう推力を回転翼モードで略水平な方向へ向かって発生させることができる複数の第2プロペラ9が、機体の側面に設けられている。【選択図】図1


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    Title :

    TAIL-SITTER-TYPE ELECTRIC AIRCRAFT


    Additional title:

    テイルシッター型電動航空機


    Contributors:

    Publication date :

    2022-07-21


    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 / H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES



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