An example gas turbine engine (20) includes a propulsor assembly (62) including at least a fan module (66) and a fan drive turbine module (68); a gas generator assembly (64) including at least a compressor section (52), a combustor (56) in fluid communication with the compressor section (52), and a turbine in fluid communication with the combustor (56); and a geared architecture (48) driven by the fan drive turbine module (68) for rotating a fan (42) of the fan module (66). A weight of the fan module (66) and the fan drive turbine module (68) is less than about 40% of a total weight (EngTOT) of a gas turbine engine (20).


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    Title :

    GEARED TURBINE ENGINE WITH RELATIVELY LIGHTWEIGHT PROPULSOR MODULE


    Additional title:

    GETRIEBETURBINENMOTOR MIT RELATIV LEICHTEM PROPULSOR-MODUL
    MOTEUR À TURBINE À ENGRENAGES COMPRENANT UN MODULE PROPULSEUR RELATIVEMENT LÉGER


    Contributors:

    Publication date :

    2020-04-22


    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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