The present disclosure relates to an airframe assembly 2' comprising an airframe support structure 50 defining an engine void 52 and configured to support a gas turbine engine 10 along an engine axis 9 of the engine void 52; a thermal enclosure 20 configured to surround the gas turbine within the engine void; a heat exchange channel 70 formed between an outer flow-bounding wall of the engine void and an inner wall defined by the thermal enclosure, configured to convey a cooling flow through the engine void outside of the thermal enclosure for the gas turbine engine; and a heat exchanger 76 mounted to the airframe support structure for heat exchange between the cooling flow and a working fluid provided to the heat exchanger.


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    Title :

    AIRFRAME ASSEMBLY


    Additional title:

    TRIEBWERKSEINHAUSUNG
    ENSEMBLE CELLULE D'AÉRONEF


    Contributors:

    Publication date :

    2025-02-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



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