An assembly is provided for an aircraft. This aircraft assembly includes an airframe structure (178), a turbine engine (22) and a heat exchanger (26). The turbine engine (22) is mounted to the airframe structure (178). The heat exchanger (26) is mounted to the airframe structure (178) independent of the turbine engine (22). The heat exchanger (26) extends axially along and circumferentially about the turbine engine (22).
FRAMED HEAT EXCHANGER FOR AIRCRAFT PROPULSION SYSTEM
WÄRMETAUSCHER MIT RAHMENSTRUKTUR FÜR EIN FLUGZEUGANTRIEBSSYSTEM
ÉCHANGEUR DE CHALEUR AVEC CADRE DE SUPPORT POUR SYSTÈME DE PROPULSION D'AÉRONEF
23.07.2025
Patent
Elektronische Ressource
Englisch
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