An assembly is provided for an aircraft. This aircraft assembly includes an airframe structure, a turbine engine and a heat exchanger. The turbine engine is mounted to the airframe structure. The heat exchanger is mounted to the airframe structure independent of the turbine engine. The heat exchanger extends axially along and circumferentially about the turbine engine.
FRAMED HEAT EXCHANGER FOR AIRCRAFT PROPULSION SYSTEM
24.07.2025
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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