A fuel system (200) for a hydrogen fuelled aircraft propulsion system (103) comprises a tank (104) configured to store hydrogen, a first inductor (436a-c) provided within the tank (104) and configured to heat hydrogen fuel within the tank (104), and a second inductor (432a-c) provided externally to the tank (104), and configured to induce a current in the first inductor (436a-c).


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    Title :

    GAS TURBINE ENGINE


    Additional title:

    GASTURBINENTRIEBWERK
    MOTEUR À TURBINE À GAZ


    Contributors:

    Publication date :

    2025-05-07


    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



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