A pressure measurement probe for an aircraft, includes a pressure sensor board comprising an electronic board equipped with a pressure sensor provided with an air inlet, the electronic board further comprising at least four fixing points distributed on a circle at regular angular intervals and configured to allow the sensor board to be fixed in the pressure measurement probe in such a way as to have, when the aircraft is on the ground, a pressure sensor air inlet that is directed downward and an angular offset less than or equal to 45° between the axis of the air inlet of the pressure sensor and the vertical, irrespective of the position of the probe on the aircraft.


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    Titel :

    PRESSURE MEASUREMENT PROBE COMPRISING A PRESSURE SENSOR BOARD


    Beteiligte:
    HODOT ROMAIN (Autor:in) / CAUCHARD LILIAN (Autor:in)

    Erscheinungsdatum :

    29.08.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    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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