An aircraft propulsion system includes a core engine, a first bottoming cycle and a second bottoming cycle that utilize different working fluids having different critical temperatures such that each of the bottoming cycles have different heat absorption capabilities.


    Access

    Download


    Export, share and cite



    Title :

    STACKED CRYOGENIC BOTTOMING CYCLES


    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



    SHARED CRYOGENIC BOTTOMING CYCLE

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

    Free access

    CRYOGENIC ASSISTED BOTTOMING CYCLE

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

    Free access

    MULTIPLE HEAT SOURCE CRYOGENIC BOTTOMING CYCLE SEQUENCING AND ROUTING

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

    Free access


    Bottoming out

    Online Contents | 1996