发明名称 EXTERNALLY FUELED TRAPPED VORTEX CAVITY AUGMENTOR
摘要 A gas turbine engine augmentor (34) includes an externally fueled annular trapped vortex cavity (50) having a cavity opening (142) open to an exhaust flowpath (128) and a sole source of fuel (75) located upstream of the trapped vortex cavity (50) and being operable for injecting fuel (75) into the exhaust flowpath (128) such that at least a portion of the fuel (75) flows into the cavity (50) through a cavity openi ng (142). An exemplary sole source of fuel (75) includes fuel holes (153) in fuel tube s (51) within spray bars (53 and/or 59) operable for injecting the fuel (75) throug h heat shield openings (166) in heat shields (54 and/or 204) surrounding the tubes (51) wherein the fuel holes (153) are located in a radially outermost portion (15 8) of the exhaust flowpath (128). The sole source of fuel (75) may include circumferentially spaced apart radial spray bars (53) and/or integral spray bars (59) integral with radial flameholders (52) and extending radially inwardly into the exhaust flowpath (128) wherein the radial flameholders (52) and radial spray bars (53) are interdigitated.
申请公布号 CA2567533(A1) 申请公布日期 2007.07.12
申请号 CA20062567533 申请日期 2006.11.09
申请人 GENERAL ELECTRIC COMPANY 发明人 VERMEERSCH, MICHAEL LOUIS
分类号 F23R3/20;F02K3/10;F23R3/06;F23R3/12;F23R3/28 主分类号 F23R3/20
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