An integrated propulsion system according to an example of the present disclosure includes, among other things, a fan section, a gas turbine engine, a geared architecture, a nacelle assembly and a mounting assembly. The nacelle assembly includes a fan nacelle and an aft nacelle, the fan nacelle arranged at least partially about a fan and the engine, and the fan nacelle arranged at least partially about a core cowling to define a bypass flow path.


    Access

    Download


    Export, share and cite



    Title :

    PROPULSION SYSTEM ARRANGEMENT FOR TURBOFAN GAS TURBINE ENGINE


    Contributors:

    Publication date :

    2022-02-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / 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 / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



    Propulsion system arrangement for turbofan gas turbine engine

    ECKETT CHRISTOPHER A / SUCIU GABRIEL L | European Patent Office | 2023

    Free access

    Propulsion system arrangement for turbofan gas turbine engine

    ECKETT CHRISTOPHER A / SUCIU GABRIEL L | European Patent Office | 2021

    Free access

    PROPULSION SYSTEM ARRANGEMENT FOR TURBOFAN GAS TURBINE ENGINE

    ECKETT CHRISTOPHER A / SUCIU GABRIEL L | European Patent Office | 2020

    Free access

    Propulsion system arrangement for turbofan gas turbine engine

    ECKETT CHRISTOPHER A / SUCIU GABRIEL L | European Patent Office | 2018

    Free access

    PROPULSION SYSTEM ARRANGEMENT FOR TURBOFAN GAS TURBINE ENGINE

    ECKETT CHRISTOPHER A / SUCIU GABRIEL L | European Patent Office | 2018

    Free access