To provide an aerial vehicle that is efficient in flight and that can take off and land vertically.SOLUTION: A flight control apparatus for fixed-wing aircraft includes a first port wing 115 and first starboard wing 120, a first port swash plate 145 coupled between a first port rotor 155 and a first port electric motor 135 that is coupled to the first port wing 115, and a first starboard swash plate 150 coupled between a first starboard rotor 130 and a first starboard electric motor 140 that is coupled to the first starboard wing 120.SELECTED DRAWING: Figure 3A

    【課題】飛行時に効率がよく、かつ垂直に離着陸できる航空機を提供する。【解決手段】固定翼機の飛行制御装置が、第1の左翼115および第1の右翼120と、第1の左ロータ155と第1の左翼115に連結された第1の左電気モータ135との間に連結された第1の左スワッシュプレート145と、第1の右ロータ130と第1の右翼120に連結された第1の右電気モータ140との間に連結された第1の右スワッシュプレート150と、を有する。【選択図】図3A


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    Titel :

    VERTICAL TAKEOFF AND LANDING (VTOL) AIR VEHICLE


    Weitere Titelangaben:

    垂直離着陸(VTOL)航空機



    Erscheinungsdatum :

    13.06.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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