发明名称 A STAGED COMBUSTION CHAMBER FOR A GAS TURBINE
摘要 A three-stage lean burn combustion chamber (28) comprises a primary combustion zone (36), a secondary combustion zone (40) and a tertiary combustion zone (44). Each of the combustion zones (36,40,44) is supplied with premixed fuel and air by respective fuel and air mixing ducts (54,70,92). The fuel and air mixing ducts (54, 70, 92) have a plurality of air injections apertures (62,64,76,98) spaced apart in the direction of flow through the fuel and air mixing ducts (54,70,92). The apertures (62,64,76,98) reduce the magnitude of the fluctuations in the fuel to air ratio of the fuel and air mixture supplied into the at least one combustion zone (36,40,44). This reduces the generation of harmful vibrations in the combustion chamber (28).
申请公布号 CA2328283(C) 申请公布日期 2009.08.04
申请号 CA20002328283 申请日期 2000.12.14
申请人 ROLLS-ROYCE PLC;ROLLS-ROYCE CANADA LIMITED 发明人 FREEMAN, CHRISTOPHER;DAY, IVOR JOHN;SCARINCI, THOMAS
分类号 F23R3/06;F23R3/34;F23C6/04;F23D14/62;F23R3/14;F23R3/16;F23R3/28;F23R3/32 主分类号 F23R3/06
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