An electromechanical device for actuating a movable flight control surface having a skin hinged to a structure of an aircraft about a pivot axis, the device including: at least two electric motors for causing the skin to pivot about the pivot axis; a power circuit and a control circuit for powering and controlling each of the motors; and a device for limiting opposing forces exerted by the two electric motors.
ELECTROMECHANICAL ACTUATOR FOR A MOVABLE FLIGHT SURFACE
2020-03-19
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
ELECTROMECHANICAL DRIVE OF FLIGHT CONTROL MOVABLE SURFACE
European Patent Office | 2019
|Electromechanical flight control actuator
NTRS | 1979
Electromechanical flight control actuator
Tema Archive | 1976
Electromechanical flight control actuator
NTRS | 1976