The present invention relates to a liquid fuel tank applied to an aircraft, and more specifically, the liquid fuel tank comprises a porous screen formed of a tube having a hollow center formed in the longitudinal direction inside the liquid fuel tank, and collecting liquid fuel while blocking gas, and a vane for guiding the liquid fuel inside the liquid fuel tank to an outlet. Therefore, the liquid fuel tank allows the liquid fuel to be transferred by blocking the gas without being affected by gravity and without cutting off the fuel.

    본 발명은 비행체에 적용되는 액체 연료 탱크에 관한 것으로, 보다 상세하게는 액체 연료 탱크는 액체 연료 탱크 내부에서 길이방향으로 중심부에 중공이 형성된 튜브로 이루어져 기체는 차단하고 액체 연료는 포집하는 다공성 스크린, 및 상기 액체 연료 탱크 내부에서 액체 연료를 출구로 안내하는 베인을 포함함으로써, 중력에 영향을 받지 않고 연료의 단절이 없이 기체를 차단하여 액체 연료 이송이 가능하다.


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    Titel :

    LIQUID FUEL TANK


    Weitere Titelangaben:

    액체 연료 탱크


    Beteiligte:
    PARK JEONG BAE (Autor:in)

    Erscheinungsdatum :

    04.08.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64G Raumfahrt , COSMONAUTICS



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