A servocontrol for controlling the position of a moving part of an aircraft includes a piloting device configured to control a power device according to a displacement control, the piloting device including a piloting unit further including a set of electronic, mechanical and/or hydraulic accessories in fluidic communication with the hydraulic cylinder and a body delimiting a network of tubular cavities fluidically connecting the electronic, mechanical and/or hydraulic accessories. The body includes an external surface, at least a first coupling portion between the network and a hydraulic cylinder and at least a second coupling portion between the network and the hydraulic cylinder and a neutral axis being defined for each tubular cavity. The neutral axis of at least one tubular cavity is curved.
SERVOCONTROL FOR CONTROLLING THE POSITION OF A MOVING PART OF AN AIRCRAFT
2024-07-18
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
European Patent Office | 2024
|NTRS | 1978
|European Patent Office | 2015
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