发明名称 Afterburner for combustion of starved-air combustor fuel gas containing suspended solid fuel and fly ash
摘要 An afterburner for use as a secondary combustion chamber in a starved-air combustor system to further combust any combustible material in the combustion gas and entrained solid particle material discharge from the combustion chamber of the starved-air combustor system. The afterburner is lined with refractory and includes a diverter plate positioned transversely to the incoming flow of combustion gases. The afterburner is divided into a plurality of reaction zones, each of which has an associated reaction air supply. The diverter plate imparts a cyclonic flow to the combustion gas which is enhanced by air injected in the combustion zones. The temperature of the gas discharged from the afterburner is monitored and the flow of reaction air controlled responsive to changes in discharge gas temperature from a predetermined temperature.
申请公布号 US4332206(A) 申请公布日期 1982.06.01
申请号 US19800148361 申请日期 1980.05.09
申请人 THE BOEING COMPANY 发明人 TUCKER, GORDON H.;FITCH, ROBERT E.
分类号 F23G5/16;F23G5/50;F23N3/00;(IPC1-7):F23J15/00 主分类号 F23G5/16
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