A hydraulic system of an aircraft, the system comprising at least one servo-control, each servo-control comprising at least one cylinder together with a drive rod and a piston arranged in each cylinder. Between each cylinder of servo-control and the drive rod of that servo-control, at least one servo-control presents main sealing means with controlled leakage allowing a hydraulic fluid to leak out from the cylinder, the hydraulic system further comprising at least one enclosure, each cylinder of the servo-control being arranged inside the enclosure so that the fluid is collected in the enclosure.
AIRCRAFT HYDRAULIC SYSTEM COMPRISING AT LEAST ONE SERVO-CONTROL, AND AN ASSOCIATED ROTOR AND AIRCRAFT
2015-10-22
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
European Patent Office | 2016
|Hydraulic servo actuation system and method for aircraft
European Patent Office | 2024
|European Patent Office | 2024
|