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2 546 792

(13)

(51)

IPC

F42B10/62(2006-01-01)

F16C19/50(2006-01-01)

(21) (22)

Application

2013133007/11, 2013-07-16

(24)

Start date

2013-07-16

(22)

Actual filing date

2013-07-16

(45)

Published

2015-04-10

(72)

Inventor

Shevchenko Valerij VladimirovichShestakov Sergej AleksandrovichZemskov Vjacheslav AleksandrovichDergachev Aleksandr Anatol'Evich

(73)

Holder

Rossijskaja Federatsija, Ot Imeni Kotoroj Vystupaet Ministerstvo Oborony Rossijskoj FederatsiiOtkrytoe Aktsionernoe Obshchestvo Korporatsija Ob"Edinenie Mashinostroenija"

ROCKET STEERING DRIVE UNIT Russian patent published in 2015 - IPC F42B10/62 F16C19/50

Abstract RU 2546792 C2

FIELD: transport.

SUBSTANCE: invention relates to supersonic rocket airfoil control devices. Proposed unit consists of the shaft fitted in the case to turn therein, airfoil rigidly fitted on said shaft, steering unit, rollers and separators rigidly interconnected and fitted in rocket body. Steering unit rod is articulated with lever. Circular cavity composed by groove of the shaft and conical rolling paths on said rings house rollers arranged so that every next roller is perpendicular to previous one. Separator is arranged between said rollers.

EFFECT: operation at notable aerodynamic loads.

2 dwg

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RU 2 546 792 C2

Authors

Shevchenko Valerij Vladimirovich

Shestakov Sergej Aleksandrovich

Zemskov Vjacheslav Aleksandrovich

Dergachev Aleksandr Anatol'Evich

Dates

2015-04-10—Published

2013-07-16—Filed