Disclosed is an electric pedal control device for an aircraft, the device comprising several pedal transmission assemblies, each of the pedal transmission assemblies comprising an electric motor (1), an elastic connector (3), a transmission mechanism, an angular displacement sensor (5), and a pedal, wherein the angular displacement sensor (5) is configured to acquire rotational position information about the pedal; transmission mechanism revolute pairs (6) of the transmission mechanisms in the pedal transmission assemblies are connected via a mechanical connecting rod mechanism (7) to effect linkage; and a controller of the electric pedal control device is configured to receive the rotational position information, and to control, according to the rotational position information, the electric motors (1) to dampen the elastic connectors (3). The electric pedal control device can simplify the transmission mechanism while reducing the volume, and it is easy to maintain, and has high reconfigurability when encountering a single point of failure, thereby helping to increase the dispatch rate.
ELECTRIC PEDAL CONTROL DEVICE FOR AIRCRAFT
ELEKTRISCHE PEDALSTEUERUNGSVORRICHTUNG FÜR FLUGZEUGE
DISPOSITIF DE COMMANDE DE PÉDALE ÉLECTRIQUE POUR AÉRONEF
2023-01-11
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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