The invention relates to a force application device for a control stick of an aircraft, said control stick comprising a control lever that is connected to at least one motor comprising a drive shaft that can be rotated about an axis, the force application device comprising: a first pin connected to the shaft, a housing, an electromagnet, a movable actuator comprising a magnetic material, a coupling device comprising an input gear connected to the housing and an output gear comprising a second pin, and means for clamping the first pin and the second pin which comprise a first tooth and a second tooth, said device having an operating configuration in which the electromagnet is active and the output gear is positioned at a distance from the input gear, and a blocking configuration in which the electromagnet is inactive and the gears are meshed.
FORCE APPLICATION DEVICE FOR A CONTROL STICK OF AN AIRCRAFT
31.03.2022
Patent
Elektronische Ressource
Englisch
FORCE APPLICATION DEVICE FOR AN AIRCRAFT CONTROL STICK
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