The disclosure relates to a flight control system comprising at least one hydraulic servo actuator, wherein the servo actuator includes a two-stage electrohydraulic servo valve, wherein the servo valve comprises a pilot stage in which the control current is translated into a hydraulic control pressure, and a power stage in which a valve slide is moved in response to the control pressure in order to adjust the throughflow direction and throughflow cross-section of the valve. The disclosure furthermore relates to an aircraft comprising such a flight control system.
Flight control system comprising a hydraulic servo actuator
2023-09-26
Patent
Electronic Resource
English
FLIGHT CONTROL SYSTEM COMPRISING A HYDRAULIC SERVO ACTUATOR
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