Articulated plug nozzle

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

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B64C 1502, B64D 3304

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active

040435083

ABSTRACT:
A propulsion nozzle having a substantially axial nozzle shroud and an articulated plug mounted in spacial relation therewith to form a motive fluid flow path having a throat therebetween. The plug is articulative to permit the throat of the nozzle to be disposed, as required, in a position at the downstream end of the shroud or at a position upstream of the downstream end without translating either the shroud or the plug.

REFERENCES:
patent: 3237864 (1966-03-01), Taylor et al.
patent: 3261164 (1966-07-01), Tumicki
patent: 3295555 (1967-01-01), James et al.
patent: 3352494 (1967-11-01), Colville et al.
patent: 3391869 (1968-07-01), Glass
patent: 3612402 (1971-10-01), Timms et al.
patent: 3774868 (1973-11-01), Goetz
D180-19106-1, Cavanagh et al., "Design Feasibility Study or An Airframe Integrated Nozzle Concept," The Boeing Company, Nov. 1975.
(R74AEG452) Dusa et al., Turbine Engine Exhaust Nozzle Performance Investigation, Phase I Interim Report, The Boeing Company, May 1974.

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