A servo-control having at least one movable cylinder that includes a hydraulic directional control valve. The hydraulic valve includes a control shaft that is rotatable about a longitudinal axis, the control shaft being connected to a distributor slide. The servo-control including a stationary abutment member secured to a cylinder and an input lever situated outside the cylinder. The input lever is connected to the control shaft and includes a stop portion arranged in the abutment member. The servo-control includes movement means for moving the input lever longitudinally, a first abutment surface of the abutment member limiting a travel amplitude of the stop portion when the input lever is in a first position.
Servo-control and an aircraft having such a servo-control
2017-08-15
Patent
Elektronische Ressource
Englisch
SERVO-CONTROL AND AN AIRCRAFT HAVING SUCH A SERVO-CONTROL
Europäisches Patentamt | 2016
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