Aircraft propulsion systems and aircraft having such propulsion systems are described. An aircraft propulsion system (200) includes a fan (202), a motor (206) operably connected to the fan by a drive shaft (204), and an aircraft power generation system (208) operably coupled to the motor to drive rotation of the fan through the drive shaft, wherein the aircraft power generation system comprises a fuel cell configured to generate at least 1 MW of electrical power.


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    Title :

    HYDROGEN PROPULSION SYSTEMS FOR AIRCRAFT


    Additional title:

    WASSERSTOFFANTRIEBSSYSTEME FÜR FLUGZEUGE
    SYSTÈMES DE PROPULSION À HYDROGÈNE POUR AÉRONEF


    Contributors:

    Publication date :

    2023-09-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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