进口畸变下新型处理机匣改善压气机性能的机理研究

推进技术 ›› 2014, Vol. 35 ›› Issue (8): 1040-1047.

进口畸变下新型处理机匣改善压气机性能的机理研究

张皓光¹,王云鹏¹,吴　俊¹,楚武利^1,2,吴艳辉¹,刘传乐¹

西北工业大学动力与能源学院,陕西西安 710072;西北工业大学动力与能源学院,陕西西安 710072;西北工业大学动力与能源学院,陕西西安 710072;西北工业大学动力与能源学院,陕西西安 710072;先进航空发动机协同创新中心,北京 100191;西北工业大学动力与能源学院,陕西西安 710072;西北工业大学动力与能源学院,陕西西安 710072

发布日期:2021-08-15
作者简介:张皓光(1981—),男,博士,副教授,研究领域为叶轮机械气动热力学。
基金资助:
国家自然科学基金(51006084)；国家自然科学基金重点项目(51236006)；陕西省自然科学基金(2011JQ7018)；西北工业大学基础研究基金(JC201116)；中央高校基本科研业务专项资金资助(3102014JCY01004)。

Investigation on Mechanism of Perfomance Improvement for Compressor with New Type of Casing Treatment

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;Collaborative Innovation Center of Advanced Aero-Engine,Beijing 100191,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

Published:2021-08-15

摘要/Abstract

摘要： 为了揭示进口畸变下,处理机匣改善压气机性能的机理,采用全通道非定常计算方法研究了进口畸变时新型处理机匣-自适应流通处理机匣对亚声速轴流压气机性能及流场的影响,数值模拟中进口总压畸变通过在进口径向段布置栏杆实现。数值结果表明,进口畸变后采用自适应流通处理机匣能够提高转子的性能,其中效率的增加效果比总压比的明显,并获得近6.8%的综合失速裕度改进量。通过详细地分析压气机内部流场表明,处理机匣后使部分叶顶通道吸力面附面层分离起始位置向后缘移动,最大后移距离约为11%叶顶弦长,削弱了叶顶通道由气流分离造成的不良影响,并抑制叶顶间隙泄漏流从相邻叶片叶顶前缘的溢出,当喷气装置对准叶片通道时,其抑制前缘溢流的效果才是最佳的。

关键词: 进口畸变；压气机；自适应流通；处理机匣；气流分离；前缘溢流

Abstract: Influences of the performance and flow-field of subsonic axial-flow compressor are investigated with full-annulus unsteady numerical method with self recirculation casing treatment under inlet distortion to uncover the flow mechanism. Inlet distortion is made by setting barriers in the inlet radial passage. The numerical calculative results show that besides gaining 6.8% stall margin improvements,the performance of compressor can be improved with self recirculation casing treatment under inlet distortion and the effect of increasing efficiency is better than the effect of increasing total ratio. The fundamental flow mechanism is obtained by analyzing the flow-filed in rotor passage in details. The detailed analysis of the flow-filed in compressor indicates that the separated locations of blades suction boundary in some tip passage move toward blade trailing with casing treatment and the highest value is about 11% the tip chord length,weakening the bad effect of flow separation and preventing leakage flow spill to adjacent tip passage. When injecting setups face the blade tip passage,the effect of restraining tip clearance leakage flow is the best.

Key words: Inlet distortion; Compressor；Self adapting recirculation；Casing treatment；Flow separation；Leading edge spilling flow

张皓光,王云鹏,吴　俊,楚武利,吴艳辉,刘传乐. 进口畸变下新型处理机匣改善压气机性能的机理研究[J]. 推进技术, 2014, 35(8): 1040-1047.

ZHANG Hao-guang¹,WANG Yun-peng¹,WU Jun¹,CHU Wu-li^1,2,WU Yan-hui¹,LIU Chuan-le¹. Investigation on Mechanism of Perfomance Improvement for Compressor with New Type of Casing Treatment[J]. Journal of Propulsion Technology, 2014, 35(8): 1040-1047.

参考文献

[1] 孙鹏,冯国泰.稳态周向总压畸变对小型风扇影响的全周数值模拟[J].推进技术,2006,27(3): 239-242.(SUN Peng,FENG Guo-tai.Numerical Simulation of Effects of Steady Circumferential Total Pressure Distortion on a Small Fan[J].Journal of Propulsion Technology,2006,27( 3) : 239-242.)
[2] Donald C.Effect of Casing Treatment on Performance of an Inlet Stage for a Transonic Multistage Compressor[R].NASA T MX-3347,1976.
[3] Burger G D,Hodges T R,Keenan M J.Tow Stage Fan iii.Data and Performance with Rotor Tip Casing Treatment Uniform and Distorted Inlet Flows[R].NASA CR-134722,1975.
[4] Hall E J,Heidegger N J.Preformace Prediction of Endwall Treated Fan Rotors with Inlet Distortion[R].AIAA 96-0244.
[5] Donald S Madden,Matt A West.Effects of Inlet Distortion on the Stability of an Advanced Military Swept Fan Stage with Casing Treatment[R].ASME 2005-GT-68693.
[6] 吴虎,黄健,高双林.处理机匣结构对某型跨声速轴流压气机畸变响应特性影响[J].西北工业大学学报,2005,23(5): 567-571.
[7] 吴虎,斯日古楞,高双林.带导流叶排的轴流压气机级叶尖处理机匣容畸变特性[J].航空动力学报,2005,20(4): 619-624.
[8] 黄健,吴虎,张晓东,等.周向槽机匣对轴流压气机转子畸变响应特性的影响[J].推进技术,2008,29(3): 334-338( HUANG jian,WU hu,ZHANG Xiao-dong,et al.Effect of Circumferential Groove Casing on the Response to Distortion of an Axial Flow Compressor Rotor[J].Journal of Propulsion Technology,2008,29(3):334-338.)
[9] Thomas Peters,Thomas Brgener,Leonhard Fottner.Effects of Rotating Inlet Distortion on a 5-Stage Hp-Compressor[R].ASME 2001-GT-0300.
[10] Thomas Peters,Leonhard Fottner.Effects of Co- and Counter-Rotating Inlet Distortions on a 5-Stage Hp-Compressor[R].ASME 2002-GT-30395.
[11] 张皓光.轴流压气机机匣处理的试验与数值研究[D].西安: 西北工业大学,2008.
[12] 张皓光,楚武利,吴艳辉,等.轴向倾斜缝机匣处理影响压气机性能的机理[J].推进技术,2010,31(5): 555-561.(ZHANG Hao-guang,CHU Wu-li,WU Yan-hui,et al.Investigation of the Flow Mechanism of Affecting Compressor Performance with Axial Skewed Slots Casing Treatment[J].Journal of Propulsion Technology,2010,31(5): 555-561.)
[13] 楚武利,张皓光,吴艳辉,等.槽式处理机匣开槽数目对扩稳效果的影响[J].推进技术,2008,29(5): 598-603.(CHU Wu-li,ZHANG Hao-guang,WU Yan-hui,et al.Effects of Grooved Number of Grooved Casing Treatment on Stall Margin[J].Journal of Propulsion Technology,2008,29(5): 598-603.)
[14] Stephanie Weichert,Ivor Day,Chris Freeman.Self-Regulating Casing Treatment for Axial Compressor Stability Enhancement[R].ASME 2011- GT-46024.
[15] Huu Duc Vo,Choon S Tan,Edward M Greitzer.Criteria for Spike Initiated Rotating Stall[R].ASME 2005-GT-68374.(编辑:梅瑛)收稿日期:2013-08-09；修订日期:2013-09-22。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)；陕西省自然科学基金(2011JQ7018)；西北工业大学基础研究基金(JC201116)；中央高校基本科研业务专项资金资助(3102014JCY01004)。作者简介:张皓光(1981—),男,博士,副教授,研究领域为叶轮机械气动热力学。E-mail:zhg@nwpu.edu.cn