ROCKET ENGINE ROTARY NOZZLE Russian patent published in 2010 - IPC F02K9/84 

Abstract RU 2403427 C2

FIELD: engines and pumps.

SUBSTANCE: proposed nozzle comprises stationary part, rotary part arranged on the engine elastic support hinge, baffle made on stationary part with gap in rotary part and heat protecting element. The latter represents an elastic ring formed by spiral coils of heatproof material, for example wound on rubber cord to roll in recesses made in the baffle and nozzle rotary part.

EFFECT: reliable heat protection of elastic support hinge with no deterioration of operating characteristics.

1 dwg

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RU 2 403 427 C2

Authors

Mokhova Svetlana Veniaminovna

Krylov Aleksandr Dmitrievich

Gavrjusova Lada Aleksandrovna

Bondarenko Sergej Aleksandrovich

Dates

2010-11-10Published

2008-10-20Filed