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2 168 051

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IPC

(21) (22)

Application

99113493/06, 1999-06-21

(24)

Start date

1999-06-21

(22)

Actual filing date

1999-06-21

(45)

Published

2001-05-27

(72)

Inventor

Gritsenko E.A.Anisimov V.S.Koz'Min Ju.P.Korotov M.V.Vorob'Ev Ju.A.

(73)

Holder

Otkrytoe Aktsionernoe Obshchestvo Samarskij Nauchno-Tekhnicheskij Kompleks Im. N.D. Kuznetsova

GAS TURBINE DRIVE OF LIQUID-PROPELLANT ROCKET ENGINE Russian patent published in 2001 - IPC

Abstract RU 2168051 C2

FIELD: aircraft engineering. SUBSTANCE: gas turbine drive of liquid propellant rocket engine has generator and nozzle assembly installed before turbine and including outer shell. Nozzle assembly has hollow fairing connected with outer shell by radial posts. It is arranged inside housing of gas generator along its longitudinal axis and is secured in housing by means of splines and threaded ring. Gas generator has cooling jacket. Ring space is formed between outer shell and gas generator housing. EFFECT: reduced overall dimensions and weight of gas generator, improved reliability in operation and stability of burning process in gas flow. 2 cl, 1 dwg

Similar patents RU2168051C2

Title	Year	Author	Number
LIQUID-PROPELLANT ROCKET ENGINE GAS GENERATOR	1999	Gritsenko E.A. Anisimov V.S. Koz'Min Ju.P. Korotov M.V. Plastinin V.E.	RU2179256C2
LIQUID-PROPELLANT ROCKET ENGINE	1999	Gritsenko E.A. Anisimov V.S. Kharlamov R.V. Danil'Chenko V.P. Baryshevskij V.A. Mikhajlov S.V. Savchenko V.P. Chikalov V.G.	RU2168049C2
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RU 2 168 051 C2

Authors

Gritsenko E.A.

Anisimov V.S.

Koz'Min Ju.P.

Korotov M.V.

Vorob'Ev Ju.A.

Dates

2001-05-27—Published

1999-06-21—Filed