Stabilizer for gas turbine combustors and gas turbine combustor

Power plants – Combustion products used as motive fluid – Combustion products generator

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Details

60749, 60743, F02C 102

Patent

active

055751539

ABSTRACT:
A plurality of turbulence promotors (11) are arranged on a surface of a stabilizer (11) comprising a stabilizer portion (14) contacting combustion gas and support portion (15) for rectifying flow except for a heat receiving surface (13) contacting with combustion gas to promote heat transfer from the stabilizer to an air fuel flow. The distance between the turbulence promotor closest to the heat receiving surface (13) and the heat receiving surface is at least 4 times the height of said turbulence promotor to prevent back fire due to provision of the turbulence promotor.

REFERENCES:
patent: 5216885 (1993-06-01), Taniguchi et al.

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