본 발명은 항공기의 동력 제공 시스템 및 이의 제어 방법에 관한 것으로, 본 발명의 실시 예에 의한 항공기의 동력 제공 시스템은 전기 에너지를 생성하는 연료전지, 연료전지가 생성한 전압을 제1 출력단을 통해서 항공기 구동을 위한 제1 모터부에 제공하고, 미리 설정된 구동 모드에 따라 연료전지와의 연결이 스위칭되는 컨버터부, 제2 출력단을 통해서 항공기 구동을 위한 제2 모터부에 전압을 제공하며, 제2 출력단이 상기 연료전지의 출력 노드에 연결되는 배터리 및 구동 모드에 따라 연료전지와 컨버터부와의 연결을 제어하는 프로세서를 포함할 수 있다.

    A power supply system for an aircraft and a control method thereof are provided. The power supply system of the aircraft includes a fuel cell configured to generate electrical energy, a converter device configured to supply a voltage generated by the fuel cell to a first motor device for driving the aircraft through a first output terminal and switch a connection with the fuel cell depending on a predetermined driving mode, a battery configured to supply the voltage to a second motor device for driving the aircraft through a second output terminal, the second output terminal being connected with an output node of the fuel cell, and a processor configure to control a connection between the fuel cell and the converter device depending on the driving mode.


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    Titel :

    POWER SUPPLY SYSTEM OF AIRCRAFT AND CONTROLLING METHOD THEREOF


    Weitere Titelangaben:

    항공기의 동력 제공 시스템 및 이의 제어 방법


    Beteiligte:
    KIM JONG PIL (Autor:in) / LEE WOO YOUNG (Autor:in) / LEE HEE KWANG (Autor:in) / LEE JUNG HYUN (Autor:in) / CHANG SAE KWON (Autor:in) / KIM MI JIN (Autor:in)

    Erscheinungsdatum :

    2024-05-21


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H01M Verfahren oder Mittel, z.B. Batterien, für die direkte Umwandlung von chemischer in elektrische Energie , PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY



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