The present invention relates to a multicopter provided with a parallel hybrid propulsion system, which includes: a first propeller (62) receiving rotating force from a first rotating shaft (31) which is output of an engine (21); a second rotating shaft (32) to which the rotating force of the first rotating shaft (31) is transmitted; a second propeller (63) receiving the rotating force from the second rotating shaft (32); a power generator (90) generating energy by the output of the engine (21); and a propeller supplied with the energy from the power generator. According to the present invention, a plurality of frames can be folded to increase space utilization.

    본 발명은 엔진(21)의 출력인 제1 회전축(31)으로 부터 회전력을 제공 받는 제1 프로펠러(62); 상기 제1 회전축(31)의 회전력이 전달되는 제2 회전축(32); 상기 제2 회전축(32)으로 부터 회전력을 전달받는 제2 프로펠러(63); 상기 엔진(21)의 출력에 의해 에너지를 생성하는 발전기(90); 및 상기 발전기로부터 에너지를 공급받는 프로펠러를 포함하는 것을 특징으로 하는 병렬 하이브리드 추진 시스템을 구비한 멀티콥터에 관한 것이다.


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    Title :

    A multi copter with parallel hybrid propulsion system


    Additional title:

    병렬 하이브리드 추진 시스템을 구비한 멀티콥터


    Contributors:
    LEE JE WON (author)

    Publication date :

    2020-04-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

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



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