发明名称 GAS TURBINE COMBUSTOR
摘要 An object of the present invention is to provide a combustor having a premixing burner, wherein a conical flame can be formed and the metal temperature at a liner and a burner end face can be reduced. The combustor has at least one premixing burners for premixing fuel with air and jetting the mixed gas into a chamber for combustion. A cylindrical guide attached to an outer circumferential portion of an end face of the burner is provided with air supply holes. An interval D1 defined between the adjacent air supply holes and an interval D2 defined between each air supply hole and the outlet end face of the burner are each made narrower than the quenching distance in the premixed gas jetted from the premixing burner.
申请公布号 US2014083102(A1) 申请公布日期 2014.03.27
申请号 US201314018469 申请日期 2013.09.05
申请人 HITACHI, LTD. 发明人 MIURA KEISUKE;DOD SATOSHI;KOGANEZAWA TOMOMI;HIRATA YOSHITAKA;ABE KAZUKI
分类号 F23R3/28 主分类号 F23R3/28
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