HYDRAULIC ACTUATION SYSTEM

There is provided an hydraulic actuation system (10) for an aircraft, the hydraulic actuation system (10) includes an actuator (A), a primary actuation arrangement (100) to provide hydraulic fluid to control the actuator (A), wherein the hydraulic actuation system (10) is configured to detect a faul...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	Marger, Thibaut, Lassalle, Julien
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT AVIATION BLASTING COSMONAUTICS DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR FLUID-PRESSURE ACTUATORS FLUID-PRESSURE ACTUATORS, e.g. SERVO-MOTORS HEATING HELICOPTERS HYDRAULICS OR PNEUMATICS IN GENERAL LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	There is provided an hydraulic actuation system (10) for an aircraft, the hydraulic actuation system (10) includes an actuator (A), a primary actuation arrangement (100) to provide hydraulic fluid to control the actuator (A), wherein the hydraulic actuation system (10) is configured to detect a fault in the actuator (A). The hydraulic actuation system (10) also includes a secondary actuation arrangement (200) to provide hydraulic fluid to control the actuator (A) in response to a detection of a fault in the actuator (A).