TURBINE ENGINE COMPRISING AN ACTUATOR AND AIRCRAFT COMPRISING SUCH A TURBINE ENGINE, AND CORRESPONDING ACTUATION METHOD

原文（中文）

This actuator comprises a cylinder comprising a rod provided with a piston defining first and second chambers, first and second fluid lines fluidly connected to the first chamber, a resilient return means configured to exert a force on the piston, the first fluid line comprising a calibrated port, the actuator comprising a servo-valve fluidly connected to the second fluid line, a cross-sectional area of the servo-valve being greater than or equal to ten times a cross-sectional area of the calibrated port or the head loss in the first fluid line being greater than or equal to ten times the head loss in the second fluid line.