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.
AIRFRAME ASSEMBLY
TRIEBWERKSEINHAUSUNG
ENSEMBLE CELLULE D'AÉRONEF
2025-02-12
Patent
Electronic Resource
English