The invention discloses an aircraft refueling system and an aircraft comprising the same. The aircraft refueling system comprises a refueling connector (1) and an oil tank assembly (3) connected with the refueling connector (1) through a pipeline (2), and further comprises a stop valve (4) arranged in the pipeline (2) between the refueling connector (1) and the oil tank assembly (3), and the stop valve (4) is electrically connected with a refueling control panel and controlled by the refueling control panel. The stop valve (4) is used for switching on or off the pipeline (2). In the aircraft refueling system, the stop valve is arranged in the pipeline between the refueling connector and the oil tank assembly, electrically connected with the refueling control panel, controlled by the refueling control panel and used for switching on or off the pipeline. Control is achieved through the stop valve, the problem that the number of components of the aircraft refueling system is large is solved, and compared with the prior art, control is easy, and the weight is small.


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    Titel :

    Aircraft refueling system and aircraft comprising same


    Beteiligte:
    ZHAO PING AN (Autor:in) / WANG XIAOYANG (Autor:in) / ZHAO YAZHENG (Autor:in) / REN ZHONG (Autor:in)

    Erscheinungsdatum :

    04.11.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    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



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