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filingDate 2009-09-30-04:00^^<http://www.w3.org/2001/XMLSchema#date>
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publicationDate 2013-03-13-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber JP-5159741-B2
titleOfInvention Control device for gas turbine combustor and control method for gas turbine combustor
abstract <P>PROBLEM TO BE SOLVED: To provide a control device for a gas turbine combustor, which avoids a problem in the reliability of the gas turbine combustor caused by a variation in the concentration of hydrogen in fuel and also maintains low NOx combustion performance. <P>SOLUTION: A burner provided to the gas turbine combustor includes a pilot burner performing diffusion combustion bearing flame stabilizing of the whole combustor and a plurality of the main burner provided on the peripheral side of the pilot burner and performing premixed combustion for performing low NOx combustion. A pilot fuel supply system supplying fuel to the pilot burner and the main fuel supply system supplying fuel to the main burners are provided. At least the main fuel system supplying fuel to the main burners is provided with a hydrogen concentration detector detecting the concentration of hydrogen contained in fuel. A controller is installed for controlling the distribution of the flow rate of fuel supplied to the pilot burner through the pilot fuel supply system and the flow rate of fuel supplied to the main burners through the main fuel supply system, based on the detected concentration of hydrogen. <P>COPYRIGHT: (C)2011,JPO&amp;INPIT
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