An aircraft airflow sensor including a vane assembly configured to sense a direction of local airflow outside an aircraft, at least one port arranged on the vane assembly, and at least one transducer arranged with the vane assembly configured to measure a pressure within the vane assembly. The at least one transducer being in fluid communication with the at least one port. The aircraft airflow sensor also includes a shaft configured to rotatably hold the vane assembly and allow rotational movement of the vane assembly.
AIRCRAFT AIRFLOW SENSOR HAVING A VANE WITH INTEGRATED PRESSURE TRANSDUCERS
2021-04-01
Patent
Electronic Resource
English
AIRCRAFT AIRFLOW SENSOR HAVING A VANE WITH INTEGRATED PRESSURE TRANSDUCERS
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