ACTUATOR ASSEMBLIES

Actuator assemblies with a casing having an elongated body defining an interior with a longitudinal axis and an open end providing access to the interior, a main piston having at least a portion slidably received within the interior through the open end for sliding axial movement relative to the lon...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	THOMPSON CALVIN SCOTT, PFAFF BRADLEY LYNN, OZANICH BRENT MICHAEL
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COSMONAUTICS DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLUID-PRESSURE ACTUATORS FLUID-PRESSURE ACTUATORS, e.g. SERVO-MOTORS FLYING SUITS HEATING HELICOPTERS HYDRAULICS OR PNEUMATICS IN GENERAL LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	Actuator assemblies with a casing having an elongated body defining an interior with a longitudinal axis and an open end providing access to the interior, a main piston having at least a portion slidably received within the interior through the open end for sliding axial movement relative to the longitudinal axis between a retracted position and an extended position and a lock segment mounted to a portion of the main piston such that sliding movement of the lock segment moves the lock segment radially, relative to the longitudinal axis, between a locked position and an unlocked position.