An aircraft heat exchanger system (20) according to an exemplary embodiment of this disclosure, among other possible things includes a first heat exchanger assembly (26) that is disposed in an inlet duct assembly (38), and a skin heat exchanger assembly (28) in thermal communication with an outer surface (40) of an aircraft structure (22). The skin heat exchanger (28) is in fluid communication with the first heat exchanger (26) such that a working fluid (32) is communicated therebetween.


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    Title :

    AIRCRAFT SKIN HEAT EXCHANGER


    Additional title:

    FLUGZEUGHAUTWÄRMETAUSCHER
    ÉCHANGEUR DE CHALEUR DE LA PEAU D'UN AÉRONEF


    Contributors:

    Publication date :

    2023-08-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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