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高低齿迷宫气封在汽轮机级中应用的数值研究
引用本文:张宏涛,王祥锋,顾忠华,韩万金. 高低齿迷宫气封在汽轮机级中应用的数值研究[J]. 科学技术与工程, 2013, 13(21): 6094-6100
作者姓名:张宏涛  王祥锋  顾忠华  韩万金
作者单位:哈尔滨工业大学能源科学与工程学院,哈尔滨工业大学能源科学与工程学院,哈尔滨工业大学能源科学与工程学院,哈尔滨工业大学能源科学与工程学院
基金项目:国家自然科学基金委创新研究群体
摘    要:为了研究迷宫汽封应用于实际结构的汽轮机中的流动特性及密封机理,采用商业软件CFX数值模拟了带有平衡孔和迷宫密封结构的某汽轮机高压一级半汽轮机内部流动。以第八级静叶隔板汽封为例,详细分析了所采用的高低齿迷宫气封的流动特性及密封机理。结果表明:在静叶隔板中应用转子带台阶的高低齿迷宫气封,与直通型迷宫气封相比,使泄漏气流发生多次折转,产生数量众多的大涡拟序结构与杂乱无章的小涡旋,强化了泄漏气流的动能耗散,从而明显增加了静叶隔板的密封性能。优化匹配迷宫气封的转子台阶、长短齿与大小间隙,能够进一步提高迷宫气封的气动性能。

关 键 词:汽轮机级  迷宫汽封  泄漏流动  平衡孔  数值模拟
收稿时间:2013-04-09
修稿时间:2013-04-22

Numerical Study on the Application of Stepped Labyrinth Seal in Turbine Stage
ZHANG Hong-tao,WANG Xiang-feng,GU Zhong-hua,HAN Wan-jin. Numerical Study on the Application of Stepped Labyrinth Seal in Turbine Stage[J]. Science Technology and Engineering, 2013, 13(21): 6094-6100
Authors:ZHANG Hong-tao  WANG Xiang-feng  GU Zhong-hua  HAN Wan-jin
Affiliation:1(College of Energy science and engineering,Harbin Institute of Technology 1,Harbin 150001,P.R.China;Harbin Turbine Company Limited 2,Harbin 150046,P.R.China)
Abstract:In order to study the flow characteristics and sealing mechanism of the labyrinth seal used in turbine with actual structure, numerical simulation on the three-dimensional flow field of one and a half turbine stage with balance holes and the labyrinth seal structure was carried out by using the commercial software CFX, and the detailed analysis of the flow characteristics and sealing mechanism of the static diaphragm stepped labyrinth seal was carried out. The results shows that: compared with straight-through labyrinth seal, in the stator diaphragm, rotor with stepped teeth labyrinth seal can make the leakage flow occur turning repeatedly, produce numerous large eddy coherent structure and disorder small vortex, and strengthen kinetic energy dissipation of the leakage flow, which can increase sealing performance of the stator diaphragm obviously. Optimization matching of rotor steps, high and short teeth and the size of gap of labyrinth seals, which can further improve the aerodynamic performance of labyrinth seal.
Keywords:turbine stage   labyrinth seal   leakage flow   balance hole, numerical simulation
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