PRODUCTION OF ROCKET ENGINE BODY Russian patent published in 2015 - IPC F02K9/34 

Abstract RU 2566206 C1

FIELD: weapons and ammunition.

SUBSTANCE: in production, plies of fibrous material with binder are wound with the help of appropriate tooling, thermal processing and binder solidification are performed to remove said tooling. Said tooling consists of several parts and is shaped to inner surfaces of two cases facing each other by outlet diameters of cones and is assembled with two end parts including the elements of connection with engine front bottoms. Winding is executed by pseudo tape composed of crossed reinforcing fibres wound off the spinning swivel and enveloping the edge bundles. During winding, pseudo tape edge bundles are laid in circular turns in the area of end parts. After solidification, cases are cut at joint of both cones. Thereafter, tooling parts are disassembled to withdraw cases with wound end elements.

EFFECT: higher reliability, lower labour input.

3 cl, 3 dwg

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RU 2 566 206 C1

Authors

Rapoport Anatolij Tsezarevich

Syskov Jurij Mikhajlovich

Dates

2015-10-20Published

2014-06-23Filed