Servoactuadores hidráulicos

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Servoactuadores hidráulicos

Servoactuadores hidráulicos

Energy-saving intelligent hydraulic actuator PQCS2 series that integrates control valves and hydraulic devices. It has a built-in load and measurement sensor. It can be operated only with a dedicated controller, electrical wiring, and parameter settings.
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Parker Aerospace fly-by-wire primary and secondary flight control actuators have been tested, proven, and trusted in commercial and military applications for decades, providing highly reliable, fault-tolerant, and precise position-control solutions.
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Parker Aerospace designs and manufactures electrohydrostatic actuation (EHA) systems that use electric power for aircraft flight control-surface actuation that results in reduced aircraft weight, efficient power consumption, and improved maintainability.
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Electric backup hydraulic actuation systems operate as a conventional electrohydraulic servoactuator when normal aircraft hydraulic system is available and as an electrohydrostatic actuator upon loss of the aircraft hydraulic system.
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Our linear and rotary electromechanical actuators (EMAs) offer a safe and reliable means to control primary and secondary aircraft control surfaces, based on pilot or autopilot commands. Our EMAs include the latest in electronics and motor control.
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The Parker Aerospace electromechanical transcowl locking system (TLS) is designed to lock thrust reverser actuation systems out of operational mode during flight, totally independent of the hydraulic system.
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Our horizontal stabilizer trim actuators offer a safe and reliable means to control the position of the aircraft horizontal stabilizer surface to attain commanded pitch position during take-off, cruise, and landing.
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Our missile control actuation systems (CAS) precisely position control surfaces, providing flight control in response to guidance commands. Our broad CAS pedigree offers a low risk and reliable means of control with efficient power usage and packaging.
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Parker’s mechanical input actuators provide a safe and reliable means of translating mechanical input signals from the pilot into hydraulically-powered output motion for primary and secondary flight control surface positioning and control.
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687PDC
687PDC