A primary structural assembly for an aircraft outside-skin heat exchanger, the assembly comprising an outer-skin portion which defines an outer shape of the aircraft and forms a portion of a hull of the aircraft, wherein the outer-skin portion comprises at least one recess, a thermal-transfer fluid connection which is designed to convey a thermal-transfer fluid into the recess, a component which closes the recess, and at least one retaining element which is arranged in or on the recess and is configured to hold the component closing the recess, in the recess. Further, an aircraft including such a primary structural assembly and a method for attaching the aircraft outside-skin heat exchanger are disclosed.


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    Titel :

    PRIMARY STRUCTURAL ASSEMBLY FOR AN AIRCRAFT OUTSIDE-SKIN HEAT EXCHANGER, AIRCRAFT HAVING A PRIMIARY STRUCTURAL ASSEMBLY, AND METHOD FOR ATTACHING AN AIRCRAFT OUTSIDE-SKIN HEAT EXCHANGER


    Beteiligte:
    PIESKER MARKUS (Autor:in)

    Erscheinungsdatum :

    30.06.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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





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