发明名称 Torch igniter
摘要 An improved torch igniter for use in devices such as thrust augmenters, gas turbine engines, ramjets, combined-cycle engines and industrial burners. The torch igniter includes a housing with a combustion chamber. Fuel and oxidizer are delivered into the combustion chamber and ignited by an electronic ignition source, such as a plasma jet igniter or a spark igniter, so that an upstream recirculation zone and a downstream recirculation zone are created. The upstream recirculation zone stabilizes and pilots combustion within the combustion chamber, while the downstream recirculation zone augments the combustion event. Byproducts of the combustion event within the torch igniter provide a high mass flux with high thermal energy and strong ignition source radicals that are discharged through a neck portion of the housing and are thereafter employed to initiate a primary combustion event in a primary combustor.
申请公布号 US6748735(B2) 申请公布日期 2004.06.15
申请号 US20020217972 申请日期 2002.08.13
申请人 THE BOEING COMPANY 发明人 SCHMOTOLOCHA STEPHEN N.;MORRIS DONALD H.;MORRISON, JR. CALVIN Q.;PEDERSON ROBERT J.
分类号 F23Q13/00;(IPC1-7):F02C7/26;F02C7/264 主分类号 F23Q13/00
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