TURBOJET ADJUSTABLE NOZZLE Russian patent published in 2014 - IPC F02K1/80 

Abstract RU 2529283 C1

FIELD: engines and pumps.

SUBSTANCE: proposed nozzle comprises fixed casing with spherical end and moving casing with seal fitted to turn relative to crosswise axis of the nozzle. Said seal is composed of segments fitted in place to displace radially spring loaded to fixed casing spherical end. Ledges are made at ends of adjacent segments for contact between them over inner mating surfaces.

EFFECT: modular design, optimum arrangement relative to spherical end, positive and negative angles of nozzle turns, simplified assembly, reliable tightness and reparability.

2 cl, 4 dwg

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RU 2 529 283 C1

Authors

Gusev Pavel Nikitovich

Pyrkov Sergej Nikolaevich

Dates

2014-09-27Published

2013-04-18Filed