A propulsion system includes a gas turbine engine, an electric motor system having a motor drive electrically connected to the electric machine and an electric motor electrically connected to the motor drive where the electric motor drives a propulsion unit, an electric machine rotatably attached to the gas turbine engine and electrically connected to the electric motor system, an energy storage system having bi-directional electrical connections with the electric motor system and the electric machine, and an Rankine cycle system in communication with the gas turbine engine for recovering waste heat from the gas turbine engine.


    Access

    Download


    Export, share and cite



    Title :

    HYBRID ELECTRIC AIRCRAFT WITH RANKINE CYCLE HEAT RECOVERY SYSTEM


    Contributors:

    Publication date :

    2017-10-12


    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 / F01K STEAM ENGINE PLANTS , Dampfkraftanlagen / H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES



    HYBRID ELECTRIC AIRCRAFT WITH RANKINE CYCLE HEAT RECOVERY SYSTEM

    HIMMELMANN RICHARD A / TONGUE STEPHEN E | European Patent Office | 2017

    Free access

    Integrated waste heat recovery system with rankine cycle

    Smague, Pascal / Leduc, Pierre | Tema Archive | 2013


    Integrated waste heat recovery system with Rankine cycle

    Smague,P. / Leduc,P. / Inst.Francais du Petrole,FR | Automotive engineering | 2013


    Development status:Binary Rankine cycle waste heat recovery system

    Rhinehart,H.L. / Ketler.C.P. / Rose,R.K. et al. | Automotive engineering | 1977


    Review of Rankine Cycle Systems Components for Hybrid Engines Waste Heat Recovery

    Hanna, Alister / Rouaud, Cedric / McCullough, Geoffrey et al. | SAE Technical Papers | 2012