A hybrid drone of the present invention directly drives an electric motor (115) by power of power generators (100, 102) generating the power from a drive of a gasoline engine (103) to drive a propeller (116) and provides a power control unit (106) to adjust power distribution between the power generators (100, 102) and an electronic transmission (118) and a charging battery (111), charge the power in the charging battery (111) in accordance with a flight situation, and drive the electric motor (115) by the power of the charging battery (111) in case of an emergency.
본 발명은 가솔린엔진(103)의 구동으로부터 전력을 생산하는 발전기(100)(102)의 전력으로 전기모터(115)를 직접 구동하여 프로펠러(116)를 구동시키고, 파워 컨트롤 유닛(106)을 제공하여 상기 발전기(100)(102)와 전자 변속기(118)와 충전식 배터리(111)사이의 전력배분을 조정하고 비행상황에 맞추어 충전식 배터리(111)에 충전을 하고 비상상황에 충전식 배터리(111)의 전력으로 전기모터(115)를 구동한다.
Hybrid drone
하이브리드 드론
2020-10-28
Patent
Electronic Resource
Korean
IPC: | B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01N GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL , Schalldämpfer oder Auspuffvorrichtungen für Gase von Kraft- und Arbeitsmaschinen oder von Kraftmaschinen allgemein / F02B INTERNAL-COMBUSTION PISTON ENGINES , Brennkraftmaschinen mit innerer Verbrennung mit Verdrängerwirkung / F02D CONTROLLING COMBUSTION ENGINES , Steuern oder Regeln von Brennkraftmaschinen |