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).


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    Title :

    FRAMED HEAT EXCHANGER FOR AIRCRAFT PROPULSION SYSTEM


    Additional title:

    WÄRMETAUSCHER MIT RAHMENSTRUKTUR FÜR EIN FLUGZEUGANTRIEBSSYSTEM
    ÉCHANGEUR DE CHALEUR AVEC CADRE DE SUPPORT POUR SYSTÈME DE PROPULSION D'AÉRONEF


    Contributors:

    Publication date :

    2025-07-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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