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2 259 933

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IPC

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Application

2004126514/11, 2004-09-02

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Start date

2004-09-02

(22)

Actual filing date

2004-09-02

(45)

Published

2005-09-10

(72)

Inventor

Aktov V.V.Burak B.K.Vatolin V.V.Gusev A.N.Ishchenko V.V.Krysanov I.N.Mashkov V.A.Pravidlo M.N.Sokolovskij G.A.Sukhov L.V.

(73)

Holder

Federal'Noe Gosudarstvennoe Unitarnoe Predprijatie Mashinostroitel'Noe Konstruktorskoe Bjuro Im. I.I. Toropova"

AVIATION CATAPULT Russian patent published in 2005 - IPC

Abstract RU 2259933 C1

FIELD: aeronautical engineering; systems of suspension of missiles and forced separation of them from flying vehicle.

SUBSTANCE: proposed device includes body with units for suspension from aircraft. Arranged in said body are ejection mechanisms, locking mechanism and on-board connector mechanism, as well as front and rear escape levers and electric automatic units. Axle of articulation attachment of front escape lever is located in upper part of body and actuator rod is secured on it. Missile lug suspension units are revolving. Front suspension unit is made in form of carriage connected with body by means of rod and provided with guides engageable with front lug of missile. Rear suspension unit is made in form of locking mechanism. Front escape lever has projection in its center part which is directed towards actuator and is used for articulation of this lever with actuator body by means of rigid rod. Device may be provided with additional suspension unit in form of slide block. Actuator has cylinder and rod with electric valve mounted inside its cavity. In initial state, rod cavity and under-piston cavity of cylinder are filled with compressed gas.

EFFECT: reduced mass; enhanced reliability of separation of missiles of large length-to-diameter ratio.

3 cl, 8 dwg

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RU 2 259 933 C1

Authors

Aktov V.V.

Burak B.K.

Vatolin V.V.

Gusev A.N.

Ishchenko V.V.

Krysanov I.N.

Mashkov V.A.

Pravidlo M.N.

Sokolovskij G.A.

Sukhov L.V.

Dates

2005-09-10—Published

2004-09-02—Filed