In accordance with at least one aspect of this disclosure, a system (100), includes a fuel line (106) defining a fuel inlet (110) and a fuel outlet (112), configured to provide fuel from a fuel tank (102) to an engine (104). A boost pump (108), including a boost impeller (114), is disposed in the fuel line (106) configured to drive fuel from the fuel inlet (110) to the fuel outlet (112) and operatively connected to the boost pump (108) via a drive shaft (119). The system includes a fluid line (118) defining a fluid inlet (120) and a fluid outlet (122), configured to provide fluid from a fluid source (124) to a fluid destination(126). A fluid turbine (128) is disposed in the fluid line (118) configured to alter a pressure of the fuel line (106) between the fuel inlet (110) and the fuel outlet (112).


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    Titel :

    VARIABLE SPEED HYDRAULIC MOTOR DRIVEN FUEL SYSTEMS


    Weitere Titelangaben:

    MIT EINEM HYDRAULIKMOTOR ANGETRIEBENE KRAFTSTOFFSYSTEME MIT VARIABLER GESCHWINDIGKEIT
    SYSTÈMES DE CARBURANT ENTRAÎNÉS PAR MOTEUR HYDRAULIQUE À VITESSE VARIABLE


    Beteiligte:
    GOY EDWARD W (Autor:in)

    Erscheinungsdatum :

    06.03.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT





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