BURNER AND FUEL FEED DEVICE FOR GAS TURBINE Russian patent published in 2011 - IPC F23N1/02 

Abstract RU 2426945 C2

FIELD: power industry.

SUBSTANCE: gas turbine burner includes pressure measurement device for pressure measurement in combustion medium inside gas turbine, which contains the following: measuring point forming the location of pressure measurement, attachment element attaching the pressure measurement device to burner, and extension element; at that, burner supplies combustion medium in non-ignited state to combustion chamber of gas turbine; at that, extension element has elongated shape; at that, measuring point is arranged on distal end of extension element relative to attachment element; at that, pressure measurement device is made so that measuring point is arranged inside burner.

EFFECT: improving operating mode of gas turbine and combustion process in response to measured pressure.

19 cl, 5 dwg

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RU 2 426 945 C2

Authors

Jervard Krister

Andersson Nil'S-Ehrik

Dates

2011-08-20Published

2007-04-20Filed