Active trim system of a flight control system of an aircraft, for transmitting a tactile feeling to a pilot of the aircraft in response to a manoeuvre, the active trim system comprising:- a manual control member (6),- an elastic deformation means (1),- a reversible actuator (2) comprising a rod (5) and a motor (3) located parallel to the elastic deformation means (1) and being movable by the motor (3) and by the motion of the manual control member (6),- an intermediate linkage member (4) linked to the manual control member (6) located between:- the manual control member (6), and- the elastic deformation means (1) and the reversible actuator (2),- a controller configured to:- move the reversible actuator (2) to a predetermined zero position, and- to provide stiffness against a displacement of the intermediate linkage member (4).
ACTIVE TRIM SYSTEM OF A FLIGHT CONTROL SYSTEM OF AN AIRCRAFT
2025-05-28
Patent
Electronic Resource
Spanish
IPC: | B64C AEROPLANES , Flugzeuge |
Active trim system of a flight control system of an aircraft
European Patent Office | 2025
|ACTIVE TRIM SYSTEM OF A FLIGHT CONTROL SYSTEM OF AN AIRCRAFT
European Patent Office | 2025
|ACTIVE TRIM SYSTEM OF A FLIGHT CONTROL SYSTEM OF AN AIRCRAFT
European Patent Office | 2024
|AIAA | 2003
|