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叶身融合技术在涡轮中的应用
引用本文:田勇,季路成,邵卫卫,肖云汉.叶身融合技术在涡轮中的应用[J].航空动力学报,2015,30(12):2949-2959.
作者姓名:田勇  季路成  邵卫卫  肖云汉
作者单位:1. 中国科学院工程热物理研究所先进能源动力重点实验室, 北京 100190;
基金项目:国家自然科学基金(51176012,51376023)
摘    要:将叶身融合技术进一步应用于涡轮,探索其技术应用效果.为此,以TTM-stage为原型,施加7种不同的叶身融合模型,并采用数值模拟方法进行了对比研究.结果表明:前缘融合面可削弱马蹄涡;侧融合面可削弱角区分离;对静叶实施融合使动叶进口总温附面层厚度降低,在通道涡作用下高总温流体被部分推离,明显降低了轮毂壁温. 

关 键 词:叶身融合    涡轮    角区分离    绝热壁温    马蹄涡
收稿时间:5/7/2014 12:00:00 AM

Application of blended blade/endwall in turbines
TIAN Yong,JI Lu-cheng,SHAO Wei-wei and XIAO Yun-han.Application of blended blade/endwall in turbines[J].Journal of Aerospace Power,2015,30(12):2949-2959.
Authors:TIAN Yong  JI Lu-cheng  SHAO Wei-wei and XIAO Yun-han
Institution:1. Key Laboratory of Advanced Energy and Power, Institute of Engineering Thermophysics, Chinese Academy of Science, Beijing 100190, China;2. Research Center for Clean Energy and Power, Chinese Academy of Sciences, Lianyungang Jiangsu 222069, China;3. School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China;4. School of Physical Sciences, University of Chinese Academy of Sciences, Beijing 100049, China
Abstract:Blended blade/endwall was applied into turbine for finding out its effectiveness of application. Taking the TTM-stage as example, seven kinds of blended blade/endwall models were designed and numerically simulated and compared. The results show that:the leading edge's blending surface can weaken the horseshoe vortex; the side blending surface can weaken the corner separation; the blending surface of the vane reduces the height of the boundary layer of total temperature at the inlet of the blade, and then the passage vortex moves the fluid of high total temperature away from the hub wall, reducing the adiabatic wall temperature of the hub evidently.
Keywords:blended blade/endwall  turbine  corner separation  adiabatic temperature  horseshoe vortex
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