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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    Titel :

    AIRCRAFT SKIN HEAT EXCHANGER


    Weitere Titelangaben:

    FLUGZEUGHAUTWÄRMETAUSCHER
    ÉCHANGEUR DE CHALEUR DE LA PEAU D'UN AÉRONEF


    Beteiligte:
    SOBANSKI JON E (Autor:in) / HANRAHAN PAUL R (Autor:in)

    Erscheinungsdatum :

    2023-08-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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