首页 | 本学科首页   官方微博 | 高级检索  
     

动叶顶部间隙对1+1/2对转涡轮性能的影响
引用本文:王会社,杨科,赵庆军,张仲柱,赵晓路,徐建中. 动叶顶部间隙对1+1/2对转涡轮性能的影响[J]. 工程热物理学报, 2006, 27(3): 399-401
作者姓名:王会社  杨科  赵庆军  张仲柱  赵晓路  徐建中
作者单位:中国科学院工程热物理研究所,北京,100080;中国科学院工程热物理研究所,北京,100080;中国科学院工程热物理研究所,北京,100080;中国科学院工程热物理研究所,北京,100080;中国科学院工程热物理研究所,北京,100080;中国科学院工程热物理研究所,北京,100080
摘    要:本文对1+1/2对转涡轮中动叶顶部间隙大小对涡轮性能的影响进行了详细的数值模拟。对涡轮总体性能参数、节距平均出口气流角、出口节距平均相对马赫数以及不同叶高的负荷进行了对照,发现间隙对1+1/2对转涡轮性能影响明显,尤其是当间隙较大时。当低压动叶间隙宽度达到高压动叶前缘叶高的4.5%时,低压动叶间隙中流动普遍超音,在设计1+1/2对转涡轮时需要加以重点考虑。

关 键 词:对转涡轮  间隙  泄漏流  数值模拟  性能
文章编号:0253-231X(2006)03-0399-03
修稿时间:2005-11-30

INFLUENCE OF ROTOR TIP CLEARANCE ON PERFORMANCE OF VANELESS COUNTER-ROTATING TURBINE
WANG Hui-She,YANG Ke,ZHAO Qing-Jun,ZHANG Zhong-Zhu,ZHAO Xiao-Lu,XU Jian-Zhong. INFLUENCE OF ROTOR TIP CLEARANCE ON PERFORMANCE OF VANELESS COUNTER-ROTATING TURBINE[J]. Journal of Engineering Thermophysics, 2006, 27(3): 399-401
Authors:WANG Hui-She  YANG Ke  ZHAO Qing-Jun  ZHANG Zhong-Zhu  ZHAO Xiao-Lu  XU Jian-Zhong
Abstract:A detailed unsteady numerical simulation has been carried out to investigate the influence of the rotor tip clearance on the performance of a 1+1/2 counter-rotating turbine (vaneless counter-rotating turbine (VCRT)). Through analyzing the total parameters of performance, the distribution of pitch-averaged outlet air angle, and pitch-averaged outlet relative Mach number and the loadings at different span etc. in VCRT, it can be found that, the tip clearance of the rotors can impose a clear influence on the VCRT's total performance, and the bigger of the clearance, the more of the influence. When the width of the tip clearance is equal to 4.5% of the rotor span, the flow in tip clearance is supersonic in the most area, which is needed to pay more attention in designing VCRT.
Keywords:vaneless counter-rotating turbine  tip clearance  clearance flow  numerical simulation  performance
本文献已被 CNKI 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号