A gas turbine engine (10, 100) includes a shaft (104) having a first air compressor (102) coupled thereto, a combustor (14) positioned to receive compressed air from the first compressor (102), and a power source (122) coupled to the shaft (104), the power source powered by a working fluid other than the compressed air (102).


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    Title :

    GAS TURBINE ENGINE DRIVEN BY SUPERCRITICAL POWER GENERATION SYSTEM


    Additional title:

    VON EINEM ÜBERKRITISCHEN STROMERZEUGUNGSSYSTEM ANGETRIEBENER GASTURBINENMOTOR
    MOTEUR À TURBINE À GAZ ENTRAÎNÉ PAR UN SYSTÈME DE GÉNÉRATION DE PUISSANCE SUPERCRITIQUE


    Contributors:

    Publication date :

    2020-03-11


    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 / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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