To provide a self-standing type flight device of which a pay load and a continuous flight time can be largely assured, and of which a position attitude at the time of flight can be accurately adjusted.SOLUTION: A self-standing type flight device 10 comprises: a main rotor 14A and the like which gives a main thrust; a sub-rotor 15A and the like which performs attitude control; an engine 30 which generates energy for rotation of the main rotor 14A and the like and the sub-rotor 15A and the like; and an arithmetic control device which controls rotation of the sub-rotor 15A and the like. Further, the main rotor 14A and the like is rotated in such manner that the same is drivingly connected with the engine 30, and on the other hand, the sub-rotor 15A and the like is rotated by a motor which is driven by electric power generated from an electric generator 16A and the like which is operated by the engine 30. Further, when performing attitude control for inclining an airframe, the arithmetic control device increases an output distribution ratio of the sub-rotor 15A compared to the time when performing hovering.SELECTED DRAWING: Figure 1

    【課題】ペイロードおよび連続飛行時間を大きく確保すると共に、飛行時に於ける位置姿勢の調整を正確に行うことができる自立型飛行装置を提供する。【解決手段】本発明の自立型飛行装置10は、主推力を与えるメインロータ14A等と、姿勢制御を行うサブロータ15A等と、メインロータ14A等およびサブロータ15A等が回転するためのエネルギを発生するエンジン30と、サブロータ15A等の回転を制御する演算制御装置と、を具備する。また、メインロータ14A等は、エンジン30と駆動的に接続されることで回転する一方、サブロータ15A等は、エンジン30により運転される発電機16A等から発生する電力により駆動するモータにより回転する。更に、演算制御装置は、機体を傾斜させる姿勢制御を行う際には、ホバリングを行う際よりも、サブロータ15Aの出力配分比を大きくする。【選択図】図1


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    Title :

    ENGINE-MOUNTED SELF-STANDING TYPE FLIGHT DEVICE


    Additional title:

    エンジン搭載自立型飛行装置


    Contributors:

    Publication date :

    2021-02-18


    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



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