PURPOSE: To provide a multicopter which can stably fly for a long time, and further, which has a high safety such that situation of crashing thereof due to battery exhaustion and so on can be avoided.CONSTITUTION: In a multicopter, propellers are divided into driving one and controlling one, the driving propeller is rotated by an engine, and electricity generated in a power generator by use of power from the engine is stored. The multicopter has a drive mechanism in which a motor for the flight controlling propeller is driven by said electricity, whereby the multicopter can stably fly for a long time, and further, the multicopter can be safely dropped by the flight controlling propeller even if the engine stops.

    【目的】 安定的に長時間飛行させることができ、かつまた、電池切れなどによる墜落の事態を避けることができる安全性の高いマルチコプターを目的とする。【構成】 マルチコプターにおいて、プロペラを駆動用と制御用に分け、エンジンにより駆動用プロペラを回転させ、また、エンジンからの動力を用いて発電機で発電した電気を蓄電し、この電力により飛行制御用のプロペラのモーターを駆動させることにより、安定的に長時間飛行させることができ、かつまた、エンジンが停止しても飛行制御用プロペラで安全に降下できる駆動機構を有する。


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    Title :

    ENGINE MOTOR HYBRID DRIVE MULTICOPTER


    Additional title:

    エンジンモーターハイブリッド駆動マルチコプター


    Contributors:

    Publication date :

    2017-08-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

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



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