A gas generator has at least one compressor rotor, at least one gas generator turbine rotor and a combustion section. A fan drive turbine is positioned downstream of a path of the products of combustion having passed over the at least one gas generator turbine rotor. The fan drive turbine drives a shaft and the shaft engages gears to drive at least three fan rotors.


    Access

    Download


    Export, share and cite



    Title :

    GAS TURBINE ENGINE WITH DISTRIBUTED FANS



    Publication date :

    2017-10-26


    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



    GAS TURBINE ENGINE WITH DISTRIBUTED FANS

    SUCIU GABRIEL L / MCCUNE MICHAEL E / CHANDLER JESSE M et al. | European Patent Office | 2022

    Free access

    Gas turbine engine with distributed fans

    SUCIU GABRIEL L / MCCUNE MICHAEL E / CHANDLER JESSE M et al. | European Patent Office | 2020

    Free access

    Gas turbine engine with distributed fans

    SUCIU GABRIEL L / MCCUNE MICHAEL E / CHANDLER JESSE M et al. | European Patent Office | 2017

    Free access

    Gas turbine engine with embedded distributed fans

    SUCIU GABRIEL L / EPSTEIN ALAN H / LORD WESLEY K et al. | European Patent Office | 2017

    Free access

    GAS TURBINE ENGINE WITH EMBEDDED DISTRIBUTED FANS

    SUCIU GABRIEL L / EPSTEIN ALAN H / LORD WESLEY K et al. | European Patent Office | 2015

    Free access