Axisymmetric convergent/divergent nozzle with external flaps

Fluid sprinkling – spraying – and diffusing – Reaction motor discharge nozzle with jacketed or hollow... – With subsequent mixing in main discharge stream in or...

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23926517, 23926533, 23926541, B64C 1502

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active

053640292

ABSTRACT:
The gas turbine engine nozzle has fifteen divergent flaps (18) secured to fifteen convergent flaps (14). Five external flaps (30), are each of a "V" shape, and surround the divergent flaps. The position of all flaps is adjustable (22) for varying the nozzle configuration. Arms (46,48) of the external flaps overlap, being parallel at the maximum overlap. The external flaps are slidably secured to the divergent flaps and move therewith.

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