METHOD AND DEVICE TO START GAS TURBINE PLANT Russian patent published in 2009 - IPC F02C7/26 F01D19/00 

Abstract RU 2374472 C1

FIELD: engines and pumps.

SUBSTANCE: proposed device comprises turbine motor, compressor, combustion chamber, air intake and system to feed compressed air into combustion chamber. Air intake incorporates check valve for it to let air inside the compressor from outside and prohibits back flow, when starting gas is forced into combustion chamber. Note that proposed device comprises also the system that feeds compressed air into gap between aforesaid check valve and compressor. Starting gas is fed directly into combustion chamber and/or on turbomachine rotor blades. In accelerating turbine, gas is forced under pressure into chamber between check valve and turbine plant compressor.

EFFECT: accelerated starting.

5 cl, 4 dwg

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RU 2 374 472 C1

Authors

Bakhturin Dmitrij Aleksandrovich

Dates

2009-11-27Published

2008-03-04Filed