A self-disengaging pitot tube cover which is a longitudinally segmented substantially cylindrical structure constituted by at least two separable segments where separation of at least two segments is controlled by temperature sensing and effected by a fusible link holding two adjacent segments together; so that the separated segments lose hold on the pitot tube, when a particular temperature of the pitot tube is reached.


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    Titel :

    System for ensuring failsafe operation of pitot tube covers for multiple types of pitot tubes


    Beteiligte:

    Erscheinungsdatum :

    29.08.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G01P MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION OR SHOCK , Messen der Linear- oder Winkelgeschwindigkeit, der Beschleunigung, der Verzögerung oder des Stoßes



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