Hybrid propulsion engines for aircraft are described herein. An example hybrid propulsion engine includes a propulsor and a gas turbine engine having a first drive shaft (218). The hybrid propulsion engine also includes an electric motor having a second drive shaft (220), and the propulsor is coupled to the second drive shaft (220). The hybrid propulsion engine further includes a clutch coupled between the first drive shaft (218) and the second drive shaft (220) to enable the gas turbine engine to drive the propulsor, via the clutch, during a first mode of operation and to enable the electric motor to drive the propulsor during a second mode of operation.


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    Title :

    HYBRID PROPULSION ENGINES FOR AIRCRAFT


    Additional title:

    HYBRIDANTRIEBSMOTOREN FÜR FLUGZEUGE
    MOTEURS À PROPULSION HYBRIDE POUR AÉRONEF


    Contributors:

    Publication date :

    2023-08-16


    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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