Methods and apparatus for detecting airflow control surface skew conditions are disclosed herein. An example apparatus includes an aircraft wing, a support linkage, and a flap coupled to the aircraft wing via the support linkage. The example apparatus includes a sensor coupled to the flap at a location proximate to the support linkage. The sensor is configured to generate vibration data for the location. The example apparatus includes a detector communicatively coupled to the sensor. The detector is to detect a skew condition of the flap based on the vibration data.


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    Titel :

    METHOD AND APPARATUS FOR DETECTING AIRFLOW CONTROL SURFACE SKEW CONDITIONS


    Weitere Titelangaben:

    VERFAHREN UND VORRICHTUNG ZUR ERKENNUNG EINER SCHIEFLUFTSTROMSTEUERUNGSFLÄCHE
    PROCÉDÉ ET DISPOSITIF DE DÉTECTION DE DÉCALAGE D'UNE SURFACE DE RÉGULATION D'ÉCOULEMENT D'AIR


    Beteiligte:

    Erscheinungsdatum :

    30.09.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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