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.
Methods and apparatus for detecting airflow control surface skew conditions
27.11.2018
Patent
Elektronische Ressource
Englisch
METHODS AND APPARATUS FOR DETECTING AIRFLOW CONTROL SURFACE SKEW CONDITIONS
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