To provide a technique for transporting an electric vertical takeoff and landing aircraft.SOLUTION: An electric vertical takeoff and landing aircraft 100, 100a to 100d comprises: a plurality of electric drive systems 10 having a plurality of rotary wings 30 and a motor 111 for rotationally driving each rotary wing; an airframe 20 on which the plurality of rotary wings and electric drive systems are located; and a connection part 29, CP1 to CP4, CPb, CPc, CPd1, CPd2 which is provided on at least one of an upper side and a lower side of the airframe, and is connected to other machine which is other electric vertical takeoff and landing aircraft.SELECTED DRAWING: Figure 4

    【課題】電動垂直離着陸機を運搬するための技術を提供する。【解決手段】電動垂直離着陸機100、100a〜100dは、複数の回転翼30と各回転翼を回転駆動させるモータ111を有する複数の電駆動システム10と、複数の回転翼と電駆動システムとが配置された機体20と、機体における上方側と下方側とのうちの少なくとも一方に設けられ、他の電動垂直離着陸機である他機と連結するための連結部29、CP1〜CP4、CPb、CPc、CPd1、CPd2と、を備える。【選択図】図4


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    Titel :

    ELECTRIC VERTICAL TAKEOFF AND LANDING AIRCRAFT


    Weitere Titelangaben:

    電動垂直離着陸機


    Beteiligte:
    IWAKAWA AKIRA (Autor:in) / HASHIMOTO MARIKO (Autor:in) / SUGITA SHUN (Autor:in) / TAKEMURA YUICHI (Autor:in)

    Erscheinungsdatum :

    01.03.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

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