发明名称 GAS TURBINE INLET COOLING COMBUSTOR USING THE BIOFUEL
摘要 <p>The present invention relates to a gas turbine combustor capable of cooling an inlet of a compressor by using water and, specifically, to a gas turbine inlet cooling combustor using a biofuel capable of using a biofuel as coolant, and cooling an inlet of a compressor by injecting the coolant as a biofuel is substituted for a fuel or mixed with the existing fuel. Moreover, the gas turbine combustor using a biofuel is capable of increasing cooling efficiency and output by using it in a field to which most sprays can be applied such as a gas turbine inlet forging system or gas turbine wet compression, a gas turbine combustor wherein fuel diversification is possible, a fuel injector contained in an engine for aviation, for power generation, and for transportation, cool spraying or painting, etc.</p>
申请公布号 KR101526469(B1) 申请公布日期 2015.06.09
申请号 KR20130162443 申请日期 2013.12.24
申请人 KOREA AEROSPACE RESEARCH INSTITUTE 发明人 KIM, HYUNG MO;KANG, JEONG SEEK;PARK, POO MIN
分类号 F02C7/16;F02C7/143;F02C7/22 主分类号 F02C7/16
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