COMBUSTION CHAMBER OF GAS TURBINE Russian patent published in 2017 - IPC F23R3/28 

Abstract RU 2633249 C2

FIELD: power industry.

SUBSTANCE: combustion chamber of gas turbine, which comprises a front panel, an elongated sleeve with the first end and the second end, and a burner installed in the sleeve. The second end of the sleeve is installed without sealing on the front panel. Sleeve and burner are configured to provide a burner, slidably mounted in the sleeve.

EFFECT: invention provides tuning to overcome pressure fluctuations and also facilitates more efficient extraction of burners.

13 cl, 7 dwg

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RU 2 633 249 C2

Authors

Paskualotto Ennio

Khellat Yan

Shissel Pirmin

Dates

2017-10-11Published

2013-03-25Filed