An aircraft airflow sensor probe includes an airflow assembly or a cone assembly configured to sense a direction of local airflow outside an aircraft; a shaft configured to rotatably hold the assembly and allow rotational movement of the assembly; and a motor connected to the shaft and configured to generate a torque to damp the rotational movement of the shaft as well as the assembly. The sensor probe further includes an angle of attack processor configured to control the motor to generate the torque to damp the rotational movement of the shaft as well as the assembly and a sensor configured to sense a position of the assembly and provide the position of the assembly to the angle of attack processor. An aircraft airflow sensor process is disclosed as well.


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    Titel :

    AIRCRAFT AIRFLOW SENSOR PROBE AND PROCESS OF IMPLEMENTING AN AIRCRAFT SENSOR PROBE


    Weitere Titelangaben:

    FLUGZEUGLUFTSTROMSENSORSONDE UND VERFAHREN ZUR IMPLEMENTIERUNG EINER FLUGZEUGSENSORSONDE
    SONDE DE CAPTEUR DE FLUX D'AIR D'AÉRONEF ET PROCÉDÉ DE MISE EN OEUVRE D'UNE SONDE DE CAPTEUR D'AÉRONEF


    Beteiligte:
    LANG CHARLES (Autor:in) / SCHULZ EDGARD (Autor:in) / LARKIN JASON (Autor:in) / TURNER DWIGHT (Autor:in)

    Erscheinungsdatum :

    2023-04-05


    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 / G01F Messen des Volumens, des Durchflussvolumens, des Massendurchflusses oder des Füllstandes , MEASURING VOLUME, VOLUME FLOW, MASS FLOW, OR LIQUID LEVEL



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