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上游尾迹与涡轮转子泄漏流相互作用数值模拟
引用本文:邹正平,綦蕾,李维,刘火星.上游尾迹与涡轮转子泄漏流相互作用数值模拟[J].航空动力学报,2010,25(1):58-66.
作者姓名:邹正平  綦蕾  李维  刘火星
作者单位:1.北京航空航天大学 能源与动力工程学院 航空发动机气动热力科技重点实验室航空发动机数值仿真研究中心, 北京 100191
基金项目:国家自然科学基金,重点实验室基金 
摘    要:叶轮机内部流动本质上是周期性非定常的,研究涡轮转子叶尖区域的非定常相互作用机理,对提高小展弦比高负荷涡轮性能具有重要意义.利用数值模拟方法研究了上游静子尾迹与涡轮转子叶尖泄漏流的非定常相互作用,分析了定常结果、时间平均结果以及瞬时时刻结果的流动图画.结果表明:上游静子尾迹与涡轮转子尖区二次流的相互作用能明显影响泄漏涡和机匣通道涡的时空演化规律,从而改变转子尖区的损失分布.上游尾迹在转子通道中传播时,诱导泄漏涡和通道涡区域出现周期性的扰动涡对,扰动涡对沿着泄漏涡和通道涡的轨迹向下游运动,使得转子尖区二次流结构呈现周期性变化. 

关 键 词:涡轮转子    非定常相互作用    上游尾迹    叶尖泄漏涡    机匣通道涡    刮削涡
收稿时间:2008/12/15 0:00:00
修稿时间:4/28/2009 2:27:28 PM

Numerical simulations of upstream wake-tip leakage vortex interactions in turbine rotor
ZOU Zheng-ping,QI Lei,LI Wei and LIU Huo-xing.Numerical simulations of upstream wake-tip leakage vortex interactions in turbine rotor[J].Journal of Aerospace Power,2010,25(1):58-66.
Authors:ZOU Zheng-ping  QI Lei  LI Wei and LIU Huo-xing
Institution:1.Aeroengine Numerical Simulation Research Center, National Key Laboratory of Science and Technology on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100191, China2.China Aviation Powerplant Research Institute, Aviation Industry Corporation of China, Zhuzhou 412002, China
Abstract:The internal flow of turbomachinery is intrinsically unsteady, so investigating the unsteady interactions in the tip region of turbine rotor are meaningful for improving the performance of low aspect/high loading turbine. The upstream wake-tip leakage vortex interactions in a turbine rotor were simulated by a 3-D unsteady viscous solver. The flow diagrams of steady, time-averaged and transient results were analyzed. The results indicate that the unsteady interactions between the upstream wake and the rotor tip regions have changed the spatio-temporal evolution of the tip leakage vortex and the passage vortex, consequently the loss is changed. Due to the wakes the tip leakage vortices and the passage vortices are separated into periodic perturbation counterrotating vortices. These counterrotating vortices move downstream along the tip leakage vortex path.
Keywords:turbine rotor  unsteady interaction  upstream wake  tip leakage vortex  casing passage vortex  scraping vortex
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