The present invention includes: an engine mounted on an aircraft; a generator installed to be driven by a power of the engine; a compressor installed to be driven by the engine or generator; a battery provided to store electricity generated by the generator; a power distributor provided to distribute the electricity generated by the generator to the battery and a main propulsion unit; and at least one nozzle device provided to eject the high-pressure gas provided from the compressor to the outside of a fuselage, thereby capable of improving safety and flight performance of an aircraft.

    본 발명은 비행체에 탑재된 엔진; 상기 엔진의 동력으로 구동될 수 있도록 설치된 제너레이터; 상기 엔진 또는 제너레이터에 의해 구동될 수 있도록 설치된 압축기; 상기 제너레이터에서 발전된 전기를 저장할 수 있도록 구비된 배터리; 상기 제너레이터에서 발전된 전기를 상기 배터리와 메인 추진 장치로 배분할 수 있도록 구비된 전력분배기; 상기 압축기에서 제공되는 고압가스를 동체의 외부로 분출시킬 수 있도록 구비된 적어도 하나 이상의 노즐장치를 포함하여 구성된다.


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    Title :

    AUXILIARY PROPULSION DEVICE FOR AIRCRAFT


    Additional title:

    비행체의 보조 추진 장치


    Contributors:
    JUNG WOO SUK (author) / KIM GWI TAEK (author) / JEON YOON CHEOL (author) / CHO HYUN KI (author)

    Publication date :

    2022-07-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B05B Sprühvorrichtungen , SPRAYING APPARATUS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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