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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    Titel :

    SHARED CRYOGENIC BOTTOMING CYCLE


    Beteiligte:

    Erscheinungsdatum :

    31.10.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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    Bottoming-Cycle fuer Nutzfahrzeuge

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