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.


    Access

    Download


    Export, share and cite



    Title :

    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


    Contributors:

    Publication date :

    2022-06-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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





    AIRCRAFT SKIN HEAT EXCHANGER

    SOBANSKI JON E / HANRAHAN PAUL R | European Patent Office | 2023

    Free access

    AIRCRAFT SKIN HEAT EXCHANGER

    SOBANSKI JON E / HANRAHAN PAUL R | European Patent Office | 2023

    Free access

    Aircraft skin heat exchanger

    SOBANSKI JON E / HANRAHAN PAUL R | European Patent Office | 2024

    Free access