PROBLEM TO BE SOLVED: To reduce, in a flight vehicle having both rotor blades and a fixed wing, the difficulty of attitude control and piloting in transition between a level flight and vertical taking-off and landing, as compared with a conventionally-proposed flight vehicle combining a fixed wind type flight vehicle and a rotary blade type flight vehicle, and preferably, simplify the structure and movable parts of the flight vehicle having both rotor blades and a fixed wing.SOLUTION: A flight vehicle comprises an air frame 10 on which three or more rotor blades 20a-20c are installed, a main wing 30 pivotably supported on the air frame, and a control part 50 for controlling the relative inclination of the main wing to the air frame.SELECTED DRAWING: Figure 1

    【課題】回転翼と固定翼の双方を備える飛行体において、従来提案されてきた固定翼式飛行体と回転翼式飛行体を組み合わせた飛行体に比べて、水平飛行と垂直離着陸との間で遷移させる際の姿勢制御や操縦の難しさを緩和する。また、望ましくは、回転翼と固定翼の双方を備える飛行体の構造や可動部の簡素化を図る。【解決手段】3以上の回転翼20a〜20cが取り付けられた機体10と、前記機体に軸支された主翼30と、前記機体に対する相対的な前記主翼の傾きを制御する制御部50と、を備えることを特徴とする飛行体。【選択図】図1


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    Titel :

    FLIGHT VEHICLE, MODIFICATION KIT, CONTROL METHOD AND CONTROL PROGRAM


    Weitere Titelangaben:

    飛行体、改造キット、制御方法及び制御プログラム


    Beteiligte:
    HAYAMA KIYOTERU (Autor:in) / IRIE HIROKI (Autor:in)

    Erscheinungsdatum :

    2018-02-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge






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    UNMANNED FLIGHT VEHICLE, FLIGHT CONTROL METHOD, AND FLIGHT CONTROL PROGRAM

    KUHARA SHUNSUKE | Europäisches Patentamt | 2017

    Freier Zugriff