发明名称 FUEL INJECTOR BAR FOR GAS TURBINE ENGINE COMBUSTOR HAVING TRAPPED VORTEX CAVITY
摘要 PROBLEM TO BE SOLVED: To supply fuel to cavity sections which can have relatively small spaces and a flow passage through which an air flow is fed to a cavity section by making the fuel to be fed to the flow passages formed in a dome inlet module or the cavities through a fuel injector bar. SOLUTION: Fuel is only fed from the injection nozzle of a fuel injector bar 50 and air is also blown into cavities 40 and 42 through passages 92 and 94 respectively provided at the intersections of a rear wall and external and internal walls and a passage 96 provided at the intersections of a front wall and the external and internal walls. Consequently, the trapped vortexes of the fuel and air are formed in the cavities 40 and 42. Thereafter, the air-fuel mixed gases in the cavities 40 and 42 are ignited by means of, for example, an igniter 100 and combustion gases are produced in the cavities 40 and 42. Thereafter, the combustion gases are discharged from the cavities 40 and 42 across the downstream end of a dome inlet module 20 and interacts with the main-flow air flowing through a flow passage 38.
申请公布号 JP2000193243(A) 申请公布日期 2000.07.14
申请号 JP19990293071 申请日期 1999.10.15
申请人 GENERAL ELECTRIC CO <GE> 发明人 DAVID LEWIS BARRAS;ARTHUR WESLEY JOHNSON
分类号 F23R3/52;F23R3/12;F23R3/28;F23R3/54;(IPC1-7):F23R3/52 主分类号 F23R3/52
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