본 발명에 따른 엔진-배터리 하이브리드 추진시스템은 전류를 발생시켜 출력시키는 발전부; 상기 발전부에서 발생시킨 전류를 정류하는 정류부; 상기 발전부의 전류 발생을 제어하는 상기 시동 발전기 제어부; 상기 정류부의 출력단에 연결되어, 정류되어 입력되는 DC 전류를 충전하는 배터리; 및 상기 배터리의 전원으로 구동되는 각종 로드;를 포함하여, 엔진-배터리 하이브리드 추진시스템을 적용함으로써 항공기 시스템에 배터리 단독 시스템에 비해 오랜 시간 전원을 공급할 수 있는 효과가 있다

    According to the present invention, an engine-battery hybrid propulsion system includes: a generation unit generating an electric current to output the same; a commutating unit commutating the electric current generated from the generation unit; a starting generator control unit controlling generation of the electric current of the generation unit; a battery connected to an output terminal of the commutating unit and charging a commutated and inputted DC current; and various loads driven by power of the battery, thereby supplying power to an aircraft system for a longer time than a battery independence system by applying the engine-battery hybrid propulsion system.


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    Titel :

    - HYBRID GASOLINE-ELECTRIC PROPULSION SYSTEM


    Weitere Titelangaben:

    엔진-배터리 하이브리드 추진시스템


    Erscheinungsdatum :

    2019-07-12


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

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



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