An aircraft system is provided that includes a first turbine engine, a second turbine engine and an electrical system. The electrical system includes a clutch, a first electric machine and a second electric machine electrically coupled to the first electric machine. The first electric machine is mechanically coupled to a first rotating assembly of the first turbine engine. The second electric machine is mechanically coupled to a second rotating assembly of the second turbine engine through the clutch.


    Access

    Download


    Export, share and cite



    Title :

    AIRCRAFT POWERPLANT WITH BOOSTED GAS TURBINE ENGINE


    Contributors:

    Publication date :

    2024-12-12


    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 / H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES



    Aircraft powerplant with boosted gas turbine engine

    HANRAHAN PAUL R / KUPRATIS DANIEL B | European Patent Office | 2025

    Free access

    AIRCRAFT POWERPLANT WITH BOOSTED GAS TURBINE ENGINE

    HANRAHAN PAUL R / KUPRATIS DANIEL B | European Patent Office | 2023

    Free access

    Aircraft powerplant

    BRADBROOK STEPHEN JOHN | European Patent Office | 2017

    Free access

    Aircraft Powerplant Trends

    Mead, George J. | SAE Technical Papers | 1937


    Flex coupler for hybrid gas turbine engine powerplant

    MENHEERE DAVID | European Patent Office | 2025

    Free access