This angle-of-attack sensor, in particular for an aircraft, of the type including a sensor body (11) on which a wind vane (12) is mounted movable in rotation by a flow, is characterized in that the wind vane (12) includes at least one deflector (13, 14) extending from the leading edge of this wind vane over at least part of the intrados and/or extrados thereof.
Angle-of-attack sensor, in particular for an aircraft
2024-09-19
Patent
Electronic Resource
English
IGNORING TURBULENCE AIRCRAFT AND AIRCRAFT ATTACK ANGLE CHANGE SENSOR
European Patent Office | 2020
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