Divergent flap actuation system for two-dimensional convergent -

Fluid sprinkling – spraying – and diffusing – Reaction motor discharge nozzle – With means controlling amount – shape or direction of...

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23926537, 74104, B64C 1502

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active

051020505

ABSTRACT:
A pair of linear actuators is disposed within a gas turbojet engine exhaust nozzle for actuating a pivotable truss frame which in turn actuates a divergent flap. One end of each actuator is pivotally mounted to a fixed structural support within the exhaust nozzle while the other end of each actuator is pivotally mounted to the truss frame. Rollers mounted to the truss frame transmit actuation forces from the actuators to the divergent flap without transmitting parasitic actuation loads to the divergent flap.

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