An aircraft sensor includes a housing (12), a strut (14) connected to and extending from a top of the housing (12), and a probe (16) extending from the strut (14). The strut (14) includes a flange (18) extending radially outward from a bottom portion of the strut (14) and a body (20) extending from a top of the flange (18). The strut (14) also includes a bore (24) extending into the strut body (20) and having a closed end positioned in the body (20). The strut (14) also includes a vent shaft (28) fluidly connected to the bore (24) and including an outlet.


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    Title :

    AIRCRAFT SENSOR WITH VENTED BORES IN A STRUT


    Additional title:

    FLUGZEUGSENSOR MIT BELÜFTETEN BOHRUNGEN IN EINER STREBE
    CAPTEUR D'AVION AVEC DES ORIFICES VENTILÉS DANS UNE ENTRETOISE


    Contributors:

    Publication date :

    2025-04-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G01P MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION OR SHOCK , Messen der Linear- oder Winkelgeschwindigkeit, der Beschleunigung, der Verzögerung oder des Stoßes / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G01D MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE , Anzeigen oder Aufzeichnen in Verbindung mit Messen allgemein / G01K MEASURING TEMPERATURE , Messen der Temperatur



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