Nozzle hydraulic actuator ring with cooling flow
AssigneeDowty Defence and Air Systems Limited
InventorGerald W. Pickard
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AssigneeDowty Defence and Air Systems Limited
InventorGerald W. Pickard
Estimating the term…
A hydraulic actuator system, for use in an aircraft, and in which the servo fluid supply to the system is used to provide for the operation and cooling of the system. The system comprises a hydraulically operated piston mechanism including at least one hydraulically operated piston, a servo vluid input to the system, which is connected in a ring main to a first side of the hydraulically operated piston, a servo fluid output from the system, which is connected in a ring main to a second side of the hydraulically operated piston, a variable restrictor arrangement which provides an interface between the servo fluid input ring main and the servo fluid output ring main, and a restrictor arrangement positioned in the servo fluid output side of the system. The position of the piston of the hydraulic piston and the adjustment thereof, are controlled by the restriction applied on the system by the variable restrictor arrangement.
A hydraulic actuator system in which the servo fluid supply to the system is used to provide for the operation and cooling of the system, comprises:
Dependencies are inferred from the claim text.