An aircraft hybrid propulsion system (5) comprises an internal combustion engine (10), an electric motor (28) a propulsor (12) and a combining gearbox (36). The internal combustion engine (10) is coupled to a first input (62) of the combining gearbox (36), the electric motor (28) is coupled to a second input (64) of the combining gearbox (36), and the propulsor (12) is coupled to an output (68) of the combining gearbox (36), such that the propulsor (12) is driveable in use by either or both of the internal combustion engine(10) and the electric motor (28). Each of the internal combustion engine (10) and the electric motor (28) is coupled to its respective input by a respective clutch (50, 52).


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    Title :

    AIRCRAFT HYBRID PROPULSION SYSTEM


    Additional title:

    HYBRIDANTRIEBSSYSTEM FÜR FLUGZEUGE
    SYSTÈME DE PROPULSION HYBRIDE D'AÉRONEF


    Contributors:

    Publication date :

    2023-01-04


    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 / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02K JET-PROPULSION PLANTS , Strahltriebwerke



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