An assembly is provided for an aircraft. The aircraft assembly includes a rotating structure, a geartrain, a propulsor rotor and an electric machine. The rotating structure includes a turbine rotor. The geartrain includes a sun gear, a ring gear, a plurality of intermediate gears and a carrier. The sun gear is rotatably driven by the rotating structure. Each of the intermediate gears is between and meshed with the sun gear and the ring gear. Each of the intermediate gears is rotatably mounted to the carrier. The propulsor rotor is rotatably driven by the carrier. The electric machine is coupled to the ring gear.


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    Title :

    SELECTIVE POWER DISTRIBUTION FOR AN AIRCRAFT PROPULSION SYSTEM


    Contributors:

    Publication date :

    2023-11-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    Selective power distribution for an aircraft propulsion system

    HANRAHAN PAUL R | European Patent Office | 2024

    Free access

    SELECTIVE POWER DISTRIBUTION FOR AN AIRCRAFT PROPULSION SYSTEM

    HANRAHAN PAUL R | European Patent Office | 2023

    Free access

    SELECTIVE POWER DISTRIBUTION FOR AN AIRCRAFT PROPULSION SYSTEM

    HANRAHAN PAUL R | European Patent Office | 2023

    Free access

    Selective power distribution for an aircraft propulsion system

    HANRAHAN PAUL R | European Patent Office | 2024

    Free access

    SELECTIVE POWER DISTRIBUTION FOR AN AIRCRAFT PROPULSION SYSTEM

    HANRAHAN PAUL R | European Patent Office | 2024

    Free access