| 进气畸变对低速轴流压气机失速特性的影响 |
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| 引用本文： | 蒋华兵,陆亚钧,袁巍,李秋实,侯安平.进气畸变对低速轴流压气机失速特性的影响[J].航空动力学报,2008,23(2):355-360. |
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| 作者姓名： | 蒋华兵 陆亚钧 袁巍 李秋实 侯安平 |
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| 作者单位： | 北京航空航天大学,航空发动机气动热力重点实验室,北京,100083 |
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| 基金项目： | “凡舟”青年科研基金(20060406) |
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| 摘 要： | 利用插板扰流器模拟压气机进口畸变流场,并深入分析了此畸变流场对某单级低速轴流压气机的旋转失速特性的影响.通过对压气机性能瞬时响应、失速扰动信号的发展和失速扰动信号的频谱特性的分析,探讨了进气总压畸变对压气机失速形式、失速强度、失速频率的影响.在畸变区形成的失速扰动将经历形成、发展、衰减甚至消失这一发展过程,只有当阻尼不足以阻止失速扰动的发展和周向传播时,压气机才会进入旋转失速状态,从而影响了压气机失速特性.
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| 关 键 词： | 航空、航天推进系统 进气畸变 旋转失速 压气机 |
| 文章编号： | 1000-8055(2008)02-0355-06 |
| 收稿时间： | 2007/1/23 0:00:00 |
| 修稿时间： | 2007年1月23日 |
Influence of inlet distortion on the stall character of a low speed axial compressor |
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| JIANG Hua-bing,LU Ya-jun,YUAN Wei,LI Qiu-shi and HOU An-ping.Influence of inlet distortion on the stall character of a low speed axial compressor[J].Journal of Aerospace Power,2008,23(2):355-360. |
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| Authors: | JIANG Hua-bing LU Ya-jun YUAN Wei LI Qiu-shi and HOU An-ping |
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| Institution: | National Key Laboratory on Aero-engines, Beijing University of Aeronautics and Astronautics, Beijing 100083, China;National Key Laboratory on Aero-engines, Beijing University of Aeronautics and Astronautics, Beijing 100083, China;National Key Laboratory on Aero-engines, Beijing University of Aeronautics and Astronautics, Beijing 100083, China;National Key Laboratory on Aero-engines, Beijing University of Aeronautics and Astronautics, Beijing 100083, China;National Key Laboratory on Aero-engines, Beijing University of Aeronautics and Astronautics, Beijing 100083, China |
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| Abstract: | Flat baffle was utilized to simulate the inlet distorted flow field,and its influence on the stall character of a low speed single stage axial compressor was investigated.The instantaneous characteristic of the compressor,the development process of stall disturbance and the frequency spectrum of the stall disturbance signal were investigated to explore the influence of inlet distortion on the form,intensity and frequency of rotating stall of the compressor.A stall disturbance formed in the distorted flow sector will experience development and damping when it propagates circumferentially,which will effectively influence the stall character of the compressor.Stall inception occurs only when the damping of the disturbance is insufficient to prevent its growth and surrounding propagation. |
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| Keywords: | aerospace propulsion system inlet distortion rotating stall compressor |
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