To provide a manned aircraft as new means of moving.SOLUTION: A hybrid manned aircraft of the present invention comprises: an engine; a motor; a first rotary wing unit for generating an aerodynamic lift using the engine; a second rotary wing unit for generating at least a thrust in the front-back direction using the motor; and a control unit for controlling the engine and the motor. In this way, the separation between the rotary wing unit for lift and the rotary wing unit for thrust can achieve an efficient structure of the aircraft according to the power needed.SELECTED DRAWING: Figure 1

    【課題】新たな移動手段としての有人飛行体を提供すること。【解決手段】本発明によるハイブリッド有人飛行体は、エンジン及びモータと、エンジンによって揚力を発生させる第1回転翼部と、モータによって少なくとも前後方向の推進力を発生させる第2回転翼部と、エンジン及びモータを制御する制御部と、を備えている。このように、浮上用の回転翼部と推進用の回転翼部とを分離したことから必要とされる力に応じた効率的な構造とすることができる。【選択図】図1


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    Title :

    HYBRID MANNED AIRCRAFT


    Additional title:

    ハイブリッド有人飛行体


    Contributors:

    Publication date :

    2021-05-13


    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 / H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung



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