Fluid sprinkling – spraying – and diffusing – Reaction motor discharge nozzle – With means controlling amount – shape or direction of...
Patent
1986-10-31
1988-08-02
Kashnikow, Andres
Fluid sprinkling, spraying, and diffusing
Reaction motor discharge nozzle
With means controlling amount, shape or direction of...
23926535, 74750R, B64D 3304
Patent
active
047609648
ABSTRACT:
In order to enhance performance of an aircraft while at the same time utilizing redundant aircraft hydraulic power in an efficient manner, an actuator system for a nozzle flap of an aircraft engine is provided. The actuator system includes a power drive unit in operatively associated relation with drive transmitting gearing at a single location together with an actuator driven by the power drive unit through the drive transmitting gearing, and the actuator includes output drive gearing operatively associated with the nozzle flap for driving the nozzle flap at spaced apart locations. With this arrangement, the nozzle flap is driven at spaced apart locations by the power drive unit from a single location through the actuator to permit downsizing of components with consequent weight reduction to achieve enhanced performance.
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"Geared Rotary Hydraulic Actuators for the General Electric A9/Vectoring Flap Demonstrator Engine Program" A Document (Proposal E 2951-P1, vol. 1 Tech RFP 790-04305-1) of Sandstrand Aviation Mech Unit, Rockford Ill.
Kashnikow Andres
Sundstrand Corporation
Weldon Kevin P.
LandOfFree
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