A conditioning system for an aircraft including a fuel conduit which receives a liquid fuel, an evaporator and a heater which heat the liquid fuel to convert the fuel to a gas fuel supplied to an engine on the aircraft, the evaporator transfers heat from a hot working fluid to the liquid fuel and the heater converts energy into heat applied to the liquid fuel, and a heat recovery circuit which circulates the working fluid through the evaporator and a heat exchanger in a hot exhaust gas stream generated by the engine.


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    Title :

    FUEL CONDITIONING SYSTEM



    Publication date :

    2024-07-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    Fuel conditioning system

    CASADO MONTERO CARLOS / CALDERON GOMEZ PABLO MANUEL / ZAMARRO MARTIN MARIA CRUZ et al. | European Patent Office | 2024

    Free access

    FUEL CONDITIONING SYSTEM

    CASADO MONTERO CARLOS / CALDERON GOMEZ PABLO MANUEL / ZAMARRO MARTIN MARIA CRUZ et al. | European Patent Office | 2024

    Free access

    FUEL CONDITIONING SYSTEM

    CASADO MONTERO CARLOS / CALDERÓN GÓMEZ PABLO MANUEL / ZAMARRO MARTÍN MARÍA CRUZ et al. | European Patent Office | 2024

    Free access