Triebwerkseinhausung

Details

Veröffentlichungs-Nr.

EP4506262

Aktenzeichen

EP24187695

Anmeldetag

10. Juli 2024

Veröffentlichung

12. Februar 2025

Rechtsraum

EP

IPC

B64D33/08F01D25/26B64D27/14B64D27/10// B64D33/10

Abstract

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.

Anmelder

Firma

Rolls-Royce plc

Land

🇬🇧 Großbritannien

Fachgebiete