The present invention discloses a hybrid propulsion system. The present invention comprises: a gas turbine engine; a main driving unit selectively connected to an output shaft of the gas turbine engine to provide a driving force; and a control unit that calculates a required torque according to an external signal, controls at least one of the gas turbine engine and the main driving unit according to the required torque, and compares a maximum output of the gas turbine engine with a preset value at the maximum output of the gas turbine engine to determine whether the gas turbine engine has a failure. Embodiments of the present invention are to provide a hybrid propulsion system. Embodiments of the present invention can check the state of the gas turbine engine when the hybrid propulsion system is used. Embodiments of the present invention can monitor the operation of a hybrid propulsion system, thereby capable of finding an exact maintenance time point.

    본 발명은 하이브리드 추진시스템을 개시한다. 본 발명은, 가스터빈 엔진과, 선택적으로 상기 가스터빈 엔진의 출력축과 연결되어 구동력을 제공하는 메인구동부와, 외부 신호에 따라 필요한 요구토크를 산출하며, 상기 요구토크에 따라 상기 가스터빈 엔진 및 상기 메인구동부 중 적어도 하나를 제어하며, 상기 가스터빈 엔진의 최대출력 시 상기 가스터빈 엔진의 최대출력과 기 설정된 값을 비교하여 상기 가스터빈 엔진의 고장 유무를 판별하는 제어부를 포함한다.


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    Title :

    Hybrid propulsion system


    Additional title:

    하이브리드 추진시스템


    Contributors:

    Publication date :

    2021-09-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen



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