An aircraft propulsion system includes at least two gas turbine engines and a bottoming cycle system where a working fluid is circulated within a closed circuit that includes a bottoming compressor section and a bottoming turbine section. Each of the at least two gas turbine engines include a primary heat exchanger for communicating thermal energy into the working fluid of the bottoming cycle.


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    Title :

    SHARED CRYOGENIC BOTTOMING CYCLE


    Contributors:

    Publication date :

    2024-10-31


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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    EVANS BRANDON M / TERWILLIGER NEIL J | European Patent Office | 2024

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    Organic Rankine Bottoming Cycle

    Doyle,E. / ThermoElectron,US | Automotive engineering | 1976


    Bottoming-Cycle fuer Nutzfahrzeuge

    Henkel, G. / Struck, W. / Moetz, K. | Tema Archive | 1985