GAS-TURBINE PLANT EXHAUST SYSTEM Russian patent published in 1999 - IPC

Abstract RU 2141037 C1

FIELD: mechanical engineering; gas-turbine plants. SUBSTANCE: proposed exhaust system has the following devices arranged in tandem: axially radial diffuser formed by outer wall and behind-the-turbine fairing, volute and outlet shaft. Air intake is installed between volume and outlet shaft. Turning flaps are arranged inside air intake. Slot is made in air intake housing from side of front wall of volute. EFFECT: enhanced efficiency of cooling and reduced full pressure losses. 2 dwg

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RU 2 141 037 C1

Authors

Snitko A.A.(Ru)

Serovaev S.G.(Ru)

Ponomarev Nikolaj Nikolaevich

Dates

1999-11-10Published

1997-11-13Filed