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轴流转子梯形周向槽处理机匣的扩稳分析
引用本文:邓敬亮,楚武利,张皓光.轴流转子梯形周向槽处理机匣的扩稳分析[J].航空动力学报,2015,30(7):1721-1730.
作者姓名:邓敬亮  楚武利  张皓光
作者单位:1. 西北工业大学 动力与能源学院, 西安 710072;
基金项目:国家自然科学基金(51006084); 国家自然科学基金重点项目(51236006)
摘    要:为研究不同子午截面形状周向槽的扩稳效果,针对跨声速转子Rotor 67设计了两种梯形周向槽和一种常规等宽周向槽.通过数值模拟,设计转速下带周向槽转子的综合稳定裕度从原始的5.895%均提高到20%以上,其中正梯形槽的扩稳效果最好.周向槽改善了叶片的载荷分布,总体提高了叶片的加功量.对比各种周向槽内部流动状态表明:上游3个槽的贡献率占主要地位,正梯形槽相对扩稳贡献最大. 

关 键 词:扩稳    处理机匣    梯形周向槽    轴流转子    数值模拟
收稿时间:3/3/2014 12:00:00 AM

Stabilizing analysis of trapezoidal circumferential grooves on an axial rotor
DENG Jing-liang,CHU Wu-li and ZHANG Hao-guang.Stabilizing analysis of trapezoidal circumferential grooves on an axial rotor[J].Journal of Aerospace Power,2015,30(7):1721-1730.
Authors:DENG Jing-liang  CHU Wu-li and ZHANG Hao-guang
Institution:1. School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072;2. Collaborative Innovation Center for Advanced Aero-Engine, Beijing 100191, China
Abstract:In order to investigate the stabilizing effect of circumferential grooves in different meridional shapes, two trapezoidal grooves structures and an equal-width grooves structure were designed for the transonic rotor— Rotor 67.The numerical simulations showed that the composite stability margin of circumferential grooves in design speed was increased from 5.9% to more than 20%, and the normal trapezoidal grooves had best effect in the mall flow margin. The blade load distribution was improved, and the average work of the blade was increased too. Comparison of these various grooves shows that the upstream three grooves dominate the biggest contribution, and the normal trapezoidal one's relative contribution to stabilizing effect is the best. 
Keywords:stabilizing  casing treatment  trapezoidal circumferential grooves  axial rotor  numerical simulation
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