The invention relates to a method for recovering fuel vapors from a fuel tank of an aircraft, the aircraft comprising: a fuel tank; a wing having an upper surface and a lower surface; and an opening in the lower surface of the wing. The method includes: coupling an inlet of a vapor recovery system to an opening; capturing fuel vapor flowing out of the opening from the fuel tank through an inlet of the vapor recovery system; and collecting the captured fuel vapor in a vapor storage tank of the vapor recovery system.

    本发明涉及一种从飞行器的燃料箱中回收燃料蒸气的方法,该飞行器包括:燃料箱;机翼,该机翼具有上表面和下表面;以及开口,该开口在机翼的下表面中。该方法包括:将蒸气回收系统的入口联接至开口;通过蒸气回收系统的入口捕获来自燃料箱的从开口流出的燃料蒸气;以及将捕获的燃料蒸气收集在蒸气回收系统的蒸气储存箱中。


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    Titel :

    Recovery of fuel vapors from aircraft fuel tanks


    Weitere Titelangaben:

    从飞行器燃料箱中回收燃料蒸气


    Beteiligte:
    GARDE MATTHEW (Autor:in) / FALLON ADAM (Autor:in)

    Erscheinungsdatum :

    22.03.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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    Freier Zugriff

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    Freier Zugriff