An aircraft sensor includes a housing, a strut connected to and extending from a top of the housing, and a probe extending from the strut. The strut includes a flange extending radially outward from a bottom portion of the strut and a body extending from a top of the flange. The strut also includes a bore extending into the strut body and having a closed end positioned in the body. The strut also includes a vent shaft fluidly connected to the bore and including an outlet.


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    Title :

    AIRCRAFT SENSOR WITH VENTED BORES IN A STRUT


    Contributors:

    Publication date :

    2025-03-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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