The invention relates to a force application device for a control stick of an aircraft, said stick comprising a control lever that is connected to a motor comprising a drive shaft, said device having: a first pin connected to the drive shaft, a housing, a second pin secured to the housing, an electromagnet secured in relation to the housing, a movable actuator which comprises a magnetic material such that said actuator can be displaced depending on a supply of current of the electromagnet, 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 actuator separates the teeth away from the first pin and the second pin, and a blocking configuration in which the electromagnet is inactive, with the first tooth and the second tooth coming into contact with the first pin and the second pin.
Force application device for a control stick of an aircraft
2022-04-26
Patent
Electronic Resource
English
Force application device for a control stick of an aircraft
European Patent Office | 2024
|FORCE APPLICATION DEVICE FOR A CONTROL STICK OF AN AIRCRAFT
European Patent Office | 2022
|FORCE APPLICATION DEVICE FOR A CONTROL STICK OF AN AIRCRAFT
European Patent Office | 2022
|