Servo-control and an aircraft having such a servo-control
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United States of America Patent
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Aug 15, 2017
Grant Date -
Jul 7, 2016
app pub date -
Jan 6, 2016
filing date -
Jan 6, 2015
priority date (Note) -
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status (Latency Note)
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Abstract
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.
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