A pitot tube (10) includes an outer tube (28) extending from a first tube end (62) to second tube end (64). The second tube end (64) defines a tip portion (36) of the pitot tube (10). A tube sleeve (30) is located inside of the outer tube (28) and defines a tube passage (34) extending from the first tube end (62) to the second tube end (64). A heating element is located between the outer tube (28) and the tube sleeve (30). The heating element is isolated from airflow into the tube passage (34). A method of forming a pitot tube (10) includes installing a heating element to an outer surface of a tube sleeve (30), the tube sleeve (30) defining a tube passage (34) of the pitot tube (10). The tube sleeve (30) is secured in an outer tube (28) such that the heating element is between the tube sleeve (30) and the outer tube (28) and is isolated from airflow through the tube passage (34).


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    Title :

    PITOT TUBE HEATER ASSEMBLY


    Additional title:

    STAUDRUCKSONDENHEIZERANORDNUNG
    ENSEMBLE DE CHAUFFAGE DE TUBE DE PITOT


    Contributors:

    Publication date :

    2024-07-24


    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



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