ROCKET ENGINE NOZZLE EXTENDING ADAPTER Russian patent published in 2010 - IPC F02K9/97 

Abstract RU 2386847 C1

FIELD: engines and pumps.

SUBSTANCE: proposed adapter comprises stationary cowl made from composite carbon-carbon material, extending adapter and adapter locks arranged on cowl outer surface. Cowl outer surface has metal load-carrying ring fitted via heatproof insert thereon. Outer surface of aforesaid ring carries damping and sealing elements, as well as locking units. Heatproof insert represents as continuation of cowl flow section in the zone it interacts with extending adapter. Load-carrying ring has cuts in the area it is attached to cowl.

EFFECT: higher reliability at impact and lateral loads.

2 cl, 1 dwg

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RU 2 386 847 C1

Authors

Sokolovskij Mikhail Ivanovich

Bondarenko Sergej Aleksandrovich

Krylov Aleksandr Dmitrievich

Suchenkov Dmitrij Dmitrievich

Chmykhov Aleksandr Anatol'Evich

Dates

2010-04-20Published

2008-09-11Filed