The aircraft powerplant (22) includes an injector (74) and a fuel system (100) configured to deliver fuel to the injector (74). The fuel system (100) includes a first tank (114), a first circuit (106) and a second circuit (108) arranged in parallel with the first circuit (106) between the first tank (114) and the injector (74). The second circuit (108) includes a second tank. The fuel is directed from the first tank (114) to the injector (74) during a first mode through the first circuit (106) and independent of the second circuit (108). The fuel is directed from the second tank to the injector (74) during a second mode through the second circuit (108) and independent of the first circuit (106).


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    Titel :

    AIRCRAFT FUEL SYSTEM WITH REMOVABLE FUEL TANK


    Weitere Titelangaben:

    FLUGZEUGKRAFTSTOFFSYSTEM MIT ABNEHMBAREM KRAFTSTOFFTANK
    SYSTÈME DE CARBURANT D'AÉRONEF AVEC RÉSERVOIR DE CARBURANT AMOVIBLE


    Beteiligte:

    Erscheinungsdatum :

    18.09.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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