Stabilizer for gas turbine combustors and gas turbine combustor equipped with the stabilizer
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United States of America Patent
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Nov 19, 1996
Grant Date -
N/A
app pub date -
Mar 30, 1994
filing date -
Apr 7, 1993
priority date (Note) -
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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.
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