A hybrid electric gas turbine engine includes a fan section having a fan, a turbine section having a turbine drivably connected to the fan through a main shaft that extends along a central longitudinal axis, a gas generating core extending along a first axis that is radially offset from the central longitudinal axis, and an electric motor drivably connected to the main shaft, wherein the electric motor is colinear with the main shaft.


    Access

    Download


    Export, share and cite



    Title :

    Systems and methods for hybrid electric turbine engines


    Contributors:

    Publication date :

    2022-12-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    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 / F02K JET-PROPULSION PLANTS , Strahltriebwerke



    SYSTEMS AND METHODS FOR HYBRID ELECTRIC GAS TURBINE ENGINES

    KUPRATIS DANIEL / ROBERGE GARY | European Patent Office | 2022

    Free access

    SYSTEMS AND METHODS FOR HYBRID ELECTRIC GAS TURBINE ENGINES

    KUPRATIS DANIEL / ROBERGE GARY | European Patent Office | 2021

    Free access

    Systems and methods for hybrid electric gas turbine engines

    KUPRATIS DANIEL / ROBERGE GARY | European Patent Office | 2022

    Free access

    HYBRID ELECTRIC POWER FOR TURBINE ENGINES HAVING HYDROGEN FUEL SYSTEMS

    HOLLEY BRIAN M / STAUBACH JOSEPH B / MULDOON MARC J et al. | European Patent Office | 2024

    Free access