| 吹气型周向槽机匣处理扩稳机理的研究 |
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| 引用本文： | 张皓光,楚武利,吴艳辉,邓文剑,张夏.吹气型周向槽机匣处理扩稳机理的研究[J].航空动力学报,2007,22(6):961-966. |
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| 作者姓名： | 张皓光 楚武利 吴艳辉 邓文剑 张夏 |
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| 作者单位： | 西北工业大学,动力与能源学院,西安710072 |
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| 摘 要： | 实验证明在周向环槽中加入切向吹气可以比原型处理机匣获得更大的稳定裕度.分别对带吹气型周向槽机匣处理与原型机匣处理的孤立转子进行全三维数值计算,计算得到的总性能特性线同实验符合良好.通过详细地对比分析两种机匣处理的叶顶区域流场,揭示了吹气型周向槽机匣处理比未吹气的原型机匣处理获得更大的稳定裕度和提高效率的机理.
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| 关 键 词： | 航空、航天推进系统 轴流压气机 吹气型机匣处理 数值模拟 流场 机匣处理 扩稳机理 研究 casing treatment blowing associated improvement margin 效率 流场 区域 分析 实验 特性线 性能 三维数值计算 孤立转子 稳定裕度 处理机匣 原型 |
| 文章编号： | 1000-8055(2007)06-0961-06 |
| 收稿时间： | 2006/5/17 0:00:00 |
| 修稿时间： | 2006年5月17日 |
Mechanism of stall margin improvement associated with the blowing circumferential grooved casing treatment |
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| ZHANG Hao-guang,CHU Wu-li,WU Yan-hui,DENG Wen-jian and ZHANG Xia.Mechanism of stall margin improvement associated with the blowing circumferential grooved casing treatment[J].Journal of Aerospace Power,2007,22(6):961-966. |
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| Authors: | ZHANG Hao-guang CHU Wu-li WU Yan-hui DENG Wen-jian and ZHANG Xia |
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| Institution: | School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072, China;School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072, China;School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072, China;School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072, China;School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072, China |
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| Abstract: | Tangent blowing in the circumferential grooves has the effect of achieving broader stall margin in the previous experiments.Three-dimentional numerical simulation has been performed for a subsonic axial-flow compressor rotor both with the blowing circumferential grooved casing treatment and archetypal casing treatment.The calculated overall performance lines showed good agreement with the experiments.The mechanism was that the blowing circumferential grooved casing treatment can achieve broader safety margin and improve the efficiency compared with archetypal casing treatment.This conclusion was obtained by detailed analyzing the flow-field at the blade tip of two kinds of casing treatment. |
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| Keywords: | aerospace propulsion system axial-flow compressor casing treatment with blowing flow-field |
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