PIV MEASUREMENT FOR SWIRLER FLOW FIELD IN GAS TURBINE COMBUSTOR  

航空发动机燃烧室旋流流场特性PIV分析(英文)

作　　者：颜应文[1,2] 李井华[1] 徐榕[1] 邓远灏[1,2] 徐华胜[2] 钟世林[2] 

机构地区：[1]南京航空航天大学能源与动力学院 [2]中国燃气涡轮研究院

出　　处：《Transactions of Nanjing University of Aeronautics and Astronautics》2012年第4期307-317,共11页南京航空航天大学学报（英文版）

基　　金：Supported by the National Natural Science Foundation of China(50906040);the Nanjing University of Aeronautics and Astronautics Research Funding(NZ2012107,NS2010052)~~

摘　　要：The characteristics of swirler flow field, including cold flow field and combustion flow field, in gas tur- bine combustor with two-stage swirler are studied by using particle image velocimetry （PIV）. Velocity compo- nents, fluctuation velocity, Reynolds stress and recirculation zone length are obtained, respectively. Influences of geometric parameter of primary hole, arrangement of primary hole, inlet air temperature, first-stage swirler an- gle and fuel/air ratio on flow field are investigated, respectively. The experimental results reveal that the primary recirculation zone lengths of combustion flow field are shorter than those of cold flow field, and the primary reeir- culation zone lengths decrease with the increase of inlet air temperature and fuel/air ratio. The change of the geo- metric parameter of primary hole casts an important influence on the swirler flow field in two-stage swirler com- bustor.应用粒子图像测速仪(Particle image velocimetry,PIV)研究了具有两级轴向旋流器的航空发动机燃烧室旋流流场特性(包括冷态流场和燃烧流场)。分别研究了不同主燃孔几何大小与空间排布、进口空气温度、一级轴向旋流器旋流角度以及油气比对冷热态流场的影响,分别获得了流场速度大小、脉动速度、雷诺应力以及回流区长度等参数。试验结果表明:燃烧流场的中心回流区长度要比冷态流场中心回流区短;随着进口空气温度和油气比的增加,中心回流区长度减少;同时主燃孔几何参数的变化(主燃孔大小和空间排布)对两级轴向旋流器旋流流场有很大影响。

关 键 词：swirler flow field gas turbine combustor particle image velocimetry primary recirculation zone length 

分 类 号：V231.2[航空宇航科学与技术—航空宇航推进理论与工程]