Aerospace Cylinders and Actuators 製品 パーカーより

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Aerospace Cylinders and Actuators ( 1 - 11 / 11 )
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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.

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.

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.

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.

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.

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.

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.

Powerful and reliable control for applications such as thrust reversers, doors, and steering. Operating in both 3,000 psi and 5,000 psi hydraulic systems, our actuator systems provide the force needed to move objects up to 35,000 lbs.

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.

Control and vary the position of bypass air valves within the engine. During normal operation, the actuators are modulated according to the FADEC control signal. The actuator provides a position feedback signal to the FADEC.

Mechanically positions the inlet guide vanes when commanded by the full authority digital engine control (FADEC). During normal operation, the actuators are modulated according to the FADEC based upon feedback from the master’s LVDT signal.

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パーカー・ハネフィン日本株式会社
東京都港区白金台3-2-10
白金台ビル2F
〒108-0071
電話 03-6408-3901(営業本部)
FAX  03-5449-7202