An aircraft fuel tank ventilation system, comprising a refrigerative dehumidifying device having a refrigerating element in contact with air flowing between a vent open to the atmosphere and a fuel tank. Also, a method of dehumidifying air introduced into an aircraft fuel tank via the ventilation system, the method comprising directing atmospheric air from the vent into contact with the refrigerating element, and cooling the refrigerating element so as to remove water vapor from the air flowing from the vent towards the fuel tank by condensation.


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    Titel :

    Aircraft fuel tank ventilation


    Beteiligte:
    LAM JOSEPH K-W (Autor:in) / TICHBORNE FRANKLIN (Autor:in) / MASTERS SIMON (Autor:in) / PARMENTER DAVID (Autor:in)

    Erscheinungsdatum :

    15.12.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F25D REFRIGERATORS , Kühlschränke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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