发明名称 COMBUSTOR AND GAS TURBINE
摘要 PROBLEM TO BE SOLVED: To provide a stably operable combustor efficiently performing a low NOx operation in a wide operation range. SOLUTION: In this combustor including a pilot nozzle 13 to which pilot fuel is supplied to form diffusion flame, and a main nozzle which is disposed along the pilot nozzle 13 and to which main fuel is supplied to form air-fuel pre-mixture ignited by the diffusion flame, the pilot nozzle 13 includes a pre-mixing injection section 20 for injecting sub-fuel to the direction separating from an outer peripheral face of the pilot nozzle 13, in a gas flow channel for combustion between the pilot nozzle 13 and the main nozzle. COPYRIGHT: (C)2010,JPO&INPIT
申请公布号 JP2010190540(A) 申请公布日期 2010.09.02
申请号 JP20090037832 申请日期 2009.02.20
申请人 MITSUBISHI HEAVY IND LTD 发明人 TAKIGUCHI TOMOSHI;AKAMATSU SHINJI;ONOZUKA FUMI;OMAE KATSUSADA;MUKAI HIDEO;NAKAMURA SOSUKE
分类号 F23R3/34;F23R3/14;F23R3/28;F23R3/32 主分类号 F23R3/34
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