| 摘要 |
The invention relates to a system for opening and closing a door (50) to the bay (20) of the landing gear (30) of an aircraft (10) with extensive freedom in positioning. According to the invention, the means of connection (60, 70, 81, 82) between the landing gear (30) and the door (50) comprise a first system forming a cylinder actuator (60) mounted on the gear (30) and a second system forming a cylinder actuator (70) mounted on the door (50), the two actuator-forming systems (60, 70) being linked together by at least one fluidic communication means (81, 82) so that actuation of the first actuator-forming system (60) causes actuation of the second actuator-forming system (70). |
