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2 165 032

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IPC

(21) (22)

Application

99110418/06, 1999-05-20

(24)

Start date

1999-05-20

(22)

Actual filing date

1999-05-20

(45)

Published

2001-04-10

(72)

Inventor

Vitoshkin A.A.Voronin V.N.Belogubets F.A.Gura A.N.Ivanov V.A.Rachuk V.S.Sukhov A.I.Trofimov V.I.Turtushov V.A.Jakovlev A.Ja.

(73)

Holder

Federal'Noe Gosudarstvennoe Unitarnoe Predprijatie Konstruktorskoe Bjuro KhimavtomatikiPredprijatie Po Dobyche, Pererabotke I Transportirovke Gaza Aktsionernoe Obshchestvo

GAS-TURBINE UNIT Russian patent published in 2001 - IPC

Abstract RU 2165032 C2

FIELD: thermal engineering. SUBSTANCE: gas- turbine unit gas has turbine and compressor mounted on common shaft and combustion chamber with fuel injectors. Combustion chamber communicates at its outlet directly with turbine inlet and at its inlet, with compressor outlet through jet apparatus. Fuel injectors communicate with fuel tank through shut-off starting valve and feed pump system. Jet apparatus is made in the form of injector communicating with external high-pressure air supply. Pump system is provided with separate variable-speed electric drive or turbine drive. EFFECT: improved performance characteristics due to facilitated starting of unit. 3 cl, 2 dwg

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RU 2 165 032 C2

Authors

Vitoshkin A.A.

Voronin V.N.

Belogubets F.A.

Gura A.N.

Ivanov V.A.

Rachuk V.S.

Sukhov A.I.

Trofimov V.I.

Turtushov V.A.

Jakovlev A.Ja.

Dates

2001-04-10—Published

1999-05-20—Filed