三旋流器燃烧室出口温度分布的初步试验研究
A preliminary experimental study of pattern factor for a triple swirler combustor
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摘要: 针对高温升燃烧室对出口温度分布系数降低的需求, 采用三头部矩形燃烧室, 对三种不同的三旋流器头部组合方案进行了出口温度分布的试验, 重点研究了三旋流器旋向和头部当量比对燃烧室出口温度分布的影响.出口温度的测试方法采用了燃气分析法.试验结果表明外旋流器与中间旋流器旋向相反时, 出口温度分布均匀;头部当量比小, 出口温度分布均匀.头部当量比应与旋流器旋向共同考虑, 才能优化燃烧室出口温度分布系数.Abstract: To reduce the requirement of high-temperature combustor on pattern factor,a triple swirler was used to test the pattern factors of three different triple swirler packages.The focus of the research was placed on the effects of vane angle of triple swirler and equivalence ratio of the combustor dome on the combustor’s pattern factor.Gas analysis method was used for the measurement of combustor exit temperature.The result show that,when the swirl air from the third swirler and the second swirler was counter-rotating,the combustor exit temperature distribution became more uniform;and the lower the equivalence ratio of the combustor dome,the more uniform the combustor exit temperature distribution was.The vane angle and the equivalence ratio of the combustor dome should be taken into account in order to optimize the combustor’s pattern factor.
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Key words:
- aerospace propulsion system /
- aeroengines /
- combustor /
- pattern factor /
- triple swirler /
- gas analysis
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[1] 胡正义主编.航空发动机设计手册第九册[M].北京:航空工业出版社,2000. [2] Lefebvre A H.Gas turbine combustion-second edition[M].USA:Taylor Francis,1999. [3] 彭云晖.高热容液雾燃烧的基础研究[D].北京:北京航空航天大学,2006. [4] McManus K,Edmond L.Adaptive closed-loop system for control of combustor pattern factor[R].AIAA Paper 96-0843,1996. [5] Miller,McManus M F,Keith R A,et al.An aerodynamic control system for modifying fuel spray distributions[R].AIAA Paper 2000-0192,2000. [6] Ziraksaz,Mohammad H.Approaching the prototype cancombustors by combustion test[R].AIAA Paper 2002-3869,2002. [7] Chen Y,Scarborough D,Liang S,et al.Manipulating pattern factor using synthetic jet actuators[R].AIAA Paper 2000-1023,2000. [8] 李尚维.燃烧室头部部件几何特征对温度场的影响[J].燃气涡轮试验与研究,1996,2:21-28. [9] 李卫东.一种根据燃气成分计算燃气温度的方法[J].中国民航学院学报,2006,24(4):23-26.LI Weidong.Method of calculating gas temperature based on gas composition[J].Journal of Civil Aviation University of China,2006,24(4):23-26. [10] 彭拾义.测定燃烧室出口温度的气体分析法[J].计量技术,1990,1:5-7. [11] 金如山.航空燃气轮机燃烧室[M].北京:宇航出版社,1985.
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