| 静叶片时序效应对压气机叶片非定常气动负荷的影响 |
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| 引用本文： | 颜培刚,李绍斌,陈浮,王仲奇.静叶片时序效应对压气机叶片非定常气动负荷的影响[J].航空动力学报,2008,23(1):117-124. |
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| 作者姓名： | 颜培刚 李绍斌 陈浮 王仲奇 |
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| 作者单位： | 1. 哈尔滨工业大学,能源科学与工程学院,哈尔滨,150001
2. 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： | 国家自然科学基金重点项目(50236020) |
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| 摘 要： | 采用数值方法对两级低速压气机中径处的流场进行非定常模拟。研究第二排静叶在两个典型周向位置上的叶片气动负荷,分析各列叶栅气动负荷的非定常波动以及静叶时序效应对叶栅气动负荷的影响。对各列叶栅的非定常气动力和气动力矩进行频谱分析,探讨叶列间的非定常气动干扰。结果表明,时序效应对静叶片气动负荷的影响明显高于动叶片的。时序效应能够提高压气机的性能与叶片寿命.
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| 关 键 词： | 航空、航天推进系统 时序效应 非定常干扰 气动负荷 压气机 |
| 文章编号： | 1000-8255(2008)01-0117-08 |
| 收稿时间： | 2006/12/11 0:00:00 |
| 修稿时间： | 2006年12月11 |
Effects of stator clocking on unsteady aerodynamic loads of a compressor blade |
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| YAN Pei-gang,LI Shao-bin,Chen Fu and WANG Zhong-qi.Effects of stator clocking on unsteady aerodynamic loads of a compressor blade[J].Journal of Aerospace Power,2008,23(1):117-124. |
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| Authors: | YAN Pei-gang LI Shao-bin Chen Fu and WANG Zhong-qi |
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| Institution: | School of Energy Science and Engineering, Harbin Institute of Technology Energy, Harbin 150001, China;National Key Laboratory on Aero-Engines, Beijing University of Aeronautics and Astronautics, Beijing 100083, China;School of Energy Science and Engineering, Harbin Institute of Technology Energy, Harbin 150001, China;School of Energy Science and Engineering, Harbin Institute of Technology Energy, Harbin 150001, China |
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| Abstract: | Numerical simulation was applied to the unsteady flow at the mid span of a twostage low-speed compressor.The aerodynamic load of the second row of stator blade at two typical circumferential positions was investigated.The influence of unsteady aerodynamic load of each blade cascade and the stator clocking effect on blade aerodynamic load was also analyzed.Through spectrum analysis of the unsteady aerodynamic forces and moments of each blade cascade,the unsteady aerodynamic interferences between blades were discussed.The results show that,the influence of stator clocking effects on the stator blade's unsteady aerodynamic loads is larger than that on the rotor blade.Stator clocking effect can help improve the compressor performance and its blade service life. |
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| Keywords: | aerospace propulsion system clocking effect unsteady interaction aerodynamic load compressor |
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