发明名称 GAS TURBINE COMBUSTOR AND METHOD OF SUPPLYING FUEL TO THE SAME
摘要 PROBLEM TO BE SOLVED: To provide a combustion system less in NOx and superior in combustion stability by solving problems with high level NOx in the case of a diffusion combustion system and with combustion stability due to backfire in the case of a premixture combustion system, at the same time. SOLUTION: A combustion air flow path is arranged coaxially with a fuel flow on the wall face of a combustion chamber to form a coaxial jet with the fuel flow embraced by an air flow, as a porous coaxial jet with these diffused in number. Herein, a circular collar member is provided at the end of a fuel nozzle to form the air flow path perpendicular to the axis of the fuel flow. COPYRIGHT: (C)2004,JPO
申请公布号 JP2004170010(A) 申请公布日期 2004.06.17
申请号 JP20020337356 申请日期 2002.11.21
申请人 HITACHI LTD 发明人 INOUE HIROSHI;KOGANEZAWA TOMOKI;KOBAYASHI SHIGEYOSHI
分类号 F23R3/28;F23R3/04;(IPC1-7):F23R3/28 主分类号 F23R3/28
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