| Citation: | CHU Wuli, HE Xudong, YANG Jibo, et al. Effects of blade single and coupling errors on axial flow compressor performance[J]. Journal of Aerospace Power, 2024, 39（11）：20220941 doi: 10.13224/j.cnki.jasp.20220941
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Due to the limitation of processing technology and other factors, there is always a small error between the theoretical blade profile and the actual blade profile in the actual processing. For transonic compressor Rotor 37, the influences of axial position and stagger angle errors on the uncertainty of compressor aerodynamic performance were studied by numerical simulation and NIPC (non-intrusive polynomial chaos method). The conclusion indicated that, for machining errors with zero mean standard normal distribution of axial position and stagger angle, the sensitivity of rotor aerodynamic performance was approximately the same when they changed singly or in coupling, only individual parameters were different. The correlation between the aerodynamic performance of axial flow compressor and each error was strong or weak, and attention shall be paid to the performance parameters with strong correlation during processing. The influence of blade coupling error on compressor lied in the superposition of the influences of blade axial position error and stagger angle error.
| [1] |
陈懋章,刘宝杰. 风扇/压气机气动设计技术发展趋势: 用于大型客机的大涵道比涡扇发动机[J]. 航空动力学报,2008,23(6): 961-975. CHEN Maozhang,LIU Baojie. Fan/compressor aero design trend and challenge on the development of high bypass ratio turbofan[J]. Journal of Aerospace Power,2008,23(6): 961-975. (in Chinese
CHEN Maozhang, LIU Baojie. Fan/compressor aero design trend and challenge on the development of high bypass ratio turbofan[J]. Journal of Aerospace Power, 2008, 23(6): 961-975. (in Chinese)
|
| [2] |
郭正涛,楚武利,晏松,等. 加工误差对压气机叶栅气动性能及稳定性影响的数据挖掘[J]. 推进技术,2022,43(3): 141-153. GUO Zhengtao,CHU Wuli,YAN Song,et al. Data mining on effects of manufacturing error on aerodynamic performance and stability of compressor cascade[J]. Journal of Propulsion Technology,2022,43(3): 141-153. (in Chinese
GUO Zhengtao, CHU Wuli, YAN Song, et al. Data mining on effects of manufacturing error on aerodynamic performance and stability of compressor cascade[J]. Journal of Propulsion Technology, 2022, 43(3): 141-153. (in Chinese)
|
| [3] |
KLAPPROTH J. Approximate relative-total-pressure losses of an infinite cascade of supersonic blades with finite leading-edge thickness[R]. NACA RM E9L21,1950.
|
| [4] |
ROELKE R J,HAAS J E. The effect of rotor blade thickness and surface finish on the performance of a small axial flow turbine[J]. Journal of Engineering for Power,1983,105(2): 377-382. doi: 10.1115/1.3227426
|
| [5] |
ROBERTS W B,ARMIN A,KASSASEYA G,et al. The effect of variable chord length on transonic axial rotor performance[J]. Journal of Turbomachinery,2002,124(3): 351-357. doi: 10.1115/1.1459734
|
| [6] |
GARZON V. Probabilistic aerothermal design of compressor airfoils[D]. Cambridge,US: Massachusetts Institute of Technology,2003.
|
| [7] |
WUNSCH D,HIRSCH C,NIGRO R,et al. Quantification of combined operational and geometrical uncertainties in turbo-machinery design[R]. ASME Paper GT 2015-43399,2015.
|
| [8] |
李宇,邹正平,刘火星,等. 叶片安装角偏差对涡轮通道内热斑迁移的影响[J]. 工程热物理学报,2009,30(6): 944-948. LI Yu,ZOU Zhengping,LIU Huoxing,et al. Influence of blade-stagger departure on the migration of hot streak in turbine passage[J]. Journal of Engineering Thermophysics,2009,30(6): 944-948. (in Chinese doi: 10.3321/j.issn:0253-231X.2009.06.011
LI Yu, ZOU Zhengping, LIU Huoxing, et al. Influence of blade-stagger departure on the migration of hot streak in turbine passage[J]. Journal of Engineering Thermophysics, 2009, 30(6): 944-948. (in Chinese) doi: 10.3321/j.issn:0253-231X.2009.06.011
|
| [9] |
郑似玉,滕金芳,羌晓青. 轮廓度加工超差对压气机气动性能影响的数值研究[J]. 科学技术与工程,2016,16(29): 317-320. ZHENG Siyu,TENG Jinfang,QIANG Xiaoqing. Numerical investigation of profile variability on axial compressor flow field performance[J]. Science Technology and Engineering,2016,16(29): 317-320. (in Chinese doi: 10.3969/j.issn.1671-1815.2016.29.055
ZHENG Siyu, TENG Jinfang, QIANG Xiaoqing. Numerical investigation of profile variability on axial compressor flow field performance[J]. Science Technology and Engineering, 2016, 16(29): 317-320. (in Chinese) doi: 10.3969/j.issn.1671-1815.2016.29.055
|
| [10] |
郑似玉,滕金芳,羌晓青. 位置度超差对轴流压气机流场性能影响的数值研究[J]. 流体机械,2016,44(11): 20-24. ZHENG Siyu,TENG Jinfang,QIANG Xiaoqing. Numerical investigation of positional variability on axial compressor flow field performance[J]. Fluid Machinery,2016,44(11): 20-24. (in Chinese doi: 10.3969/j.issn.1005-0329.2016.11.005
ZHENG Siyu, TENG Jinfang, QIANG Xiaoqing. Numerical investigation of positional variability on axial compressor flow field performance[J]. Fluid Machinery, 2016, 44(11): 20-24. (in Chinese) doi: 10.3969/j.issn.1005-0329.2016.11.005
|
| [11] |
郑似玉,滕金芳,羌晓青. 压气机叶片扭转度加工超差分析与研究[J]. 节能技术,2017,35(2): 99-102,112. ZHENG Siyu,TENG Jinfang,QIANG Xiaoqing. Numerical research of twisted variability on axial compressor performance[J]. Energy Conservation Technology,2017,35(2): 99-102,112. (in Chinese doi: 10.3969/j.issn.1002-6339.2017.02.001
ZHENG Siyu, TENG Jinfang, QIANG Xiaoqing. Numerical research of twisted variability on axial compressor performance[J]. Energy Conservation Technology, 2017, 35(2): 99-102, 112. (in Chinese) doi: 10.3969/j.issn.1002-6339.2017.02.001
|
| [12] |
于贤君,庞健,刘宝杰. 低速模拟在叶型加工偏差影响研究的应用[J]. 工程热物理学报,2018,39(7): 1436-1446. YU Xianjun,PANG Jian,LIU Baojie. The application of low-speed simulation in researching the impact of blades manufacturing deviation on aerodynamic performance[J]. Journal of Engineering Thermophysics,2018,39(7): 1436-1446. (in Chinese
YU Xianjun, PANG Jian, LIU Baojie. The application of low-speed simulation in researching the impact of blades manufacturing deviation on aerodynamic performance[J]. Journal of Engineering Thermophysics, 2018, 39(7): 1436-1446. (in Chinese)
|
| [13] |
程超,吴宝海,郑海,等. 叶片加工误差对压气机性能的影响[J]. 航空学报,2020,41(2): 623237. CHENG Chao,WU Baohai,ZHENG Hai,et al. Effect of blade machining errors on compressor performance[J]. Acta Aeronautica et Astronautica Sinica,2020,41(2): 623237. (in Chinese
CHENG Chao, WU Baohai, ZHENG Hai, et al. Effect of blade machining errors on compressor performance[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(2): 623237. (in Chinese)
|
| [14] |
SUDER K L,CELESTINA M L. Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor[J]. Journal of Turbomachinery,1996,118(2): 218-229. doi: 10.1115/1.2836629
|
| [15] |
张燕峰. 高载荷压气机端壁流动及其控制策略研究[D]. 西安: 西北工业大学,2010. ZHANG Yanfeng. Investigation of end wall flow behavior and its control strategies in highly loaded compressor[D]. Xi’an: Northwestern Polytechnical University,2010. (in Chinese
ZHANG Yanfeng. Investigation of end wall flow behavior and its control strategies in highly loaded compressor[D]. Xi’an: Northwestern Polytechnical University, 2010. (in Chinese)
|
| [16] |
中国航空工业总公司. 叶片叶型的标注、公差与叶身表面粗糙度:HB5647 [S]. 北京: 中国航空工业总公司,1999: 15-25.
|
| [17] |
庄皓琬,滕金芳,朱铭敏,等. 考虑加工公差的叶片对压气机气动性能的影响[J]. 上海交通大学学报,2020,54(9): 935-942. ZHUANG Haowan,TENG Jinfang,ZHU Mingmin,et al. Impacts of blades considering manufacturing tolerances on aerodynamic performance of compressor[J]. Journal of Shanghai Jiao Tong University,2020,54(9): 935-942. (in Chinese
ZHUANG Haowan, TENG Jinfang, ZHU Mingmin, et al. Impacts of blades considering manufacturing tolerances on aerodynamic performance of compressor[J]. Journal of Shanghai Jiao Tong University, 2020, 54(9): 935-942. (in Chinese)
|
| [18] |
WIENER N. The homogeneous chaos[M]. Baltimore,US: The Johns Hopkins University Press,2013.
|
| [19] |
DEVROYE L. Non-uniform random variate generation[M]. New York: Springer,1986.
|
| [20] |
姬田园,楚武利,戴雨晨,等. 叶顶间隙偏差对叶片气动性能影响的不确定性研究[J]. 推进技术,2022,43(10): 134-146. JI Tianyuan,CHU Wuli,DAI Yuchen,et al. Uncertainty research of effects of blade tip clearance deviation on blade aerodynamic performance[J]. Journal of Propulsion Technology,2022,43(10): 134-146. (in Chinese
JI Tianyuan, CHU Wuli, DAI Yuchen, et al. Uncertainty research of effects of blade tip clearance deviation on blade aerodynamic performance[J]. Journal of Propulsion Technology, 2022, 43(10): 134-146. (in Chinese)
|
| [21] |
DEBUSSCHERE B J,NAJM H N,PÉBAY P P,et al. Numerical challenges in the use of polynomial chaos representations for stochastic processes[J]. SIAM Journal on Scientific Computing,2004,26(2): 698-719. doi: 10.1137/S1064827503427741
|
| [22] |
LOEVEN G J A,WITTEVEEN J A S,BIJL H. Probabilistic collocation: an efficient non-intrusive approach for arbitrarily distributed parametric uncertainties[R]. AIAA 2007-317,2007.
|
| [23] |
PARUSSINI L,PEDIRODA A V. Investigation of multi geometric uncertainties by different polynomial chaos methodologies using a fictitious domain solver[J]. CMES: Computer Modeling in Engineering & Sciences,2008,23(1): 29-52.
|
| [24] |
ABADI M,BARHAM P,CHEN Jianmin,et al. TensorFlow: a system for large-scale machine learning[C]//Proceedings of the 12th USENIX conference on Operating Systems Design and Implementation. New York: ACM,2016: 265-283.
|
| [25] |
蔡宇桐,高丽敏,马驰,等. 基于NIPC的压气机叶片加工误差不确定性分析[J]. 工程热物理学报,2017,38(3): 490-497. CAI Yutong,GAO Limin,MA Chi,et al. Uncertainty quantification on compressor blade considering manufacturing error based on NIPC method[J]. Journal of Engineering Thermophysics,2017,38(3): 490-497. (in Chinese
CAI Yutong, GAO Limin, MA Chi, et al. Uncertainty quantification on compressor blade considering manufacturing error based on NIPC method[J]. Journal of Engineering Thermophysics, 2017, 38(3): 490-497. (in Chinese)
|
| [26] |
MARIA MAZZONI C,AHLFELD R,ROSIC B,et al. Uncertainty quantification of leakages in a multistage simulation and comparison with experiments[J]. Journal of Fluids Engineering,2018,140(2): 021110. doi: 10.1115/1.4037983
|
| [27] |
马驰,高丽敏,李瑞宇,等. 真实运行状态下叶顶间隙尺寸波动对跨声速转子气动性能的影响研究[J]. 推进技术,2020,41(9): 1958-1966. MA Chi,GAO Limin,LI Ruiyu,et al. Effects of tip clearance size fluctuation in actual operations on aerodynamic performance of a transonic rotor[J]. Journal of Propulsion Technology,2020,41(9): 1958-1966. (in Chinese
MA Chi, GAO Limin, LI Ruiyu, et al. Effects of tip clearance size fluctuation in actual operations on aerodynamic performance of a transonic rotor[J]. Journal of Propulsion Technology, 2020, 41(9): 1958-1966. (in Chinese)
|
| [28] |
郭正涛,楚武利,姬田园,等. 端壁倒圆半径误差对高负荷静叶栅性能影响的不确定性分析[J]. 航空动力学报,2021,36(10): 2173-2185. GUO Zhengtao,CHU Wuli,JI Tianyuan,et al. Uncertainty analysis of effects of end wall fillet radius error on high-load stator cascade performance[J]. Journal of Aerospace Power,2021,36(10): 2173-2185. (in Chinese
GUO Zhengtao, CHU Wuli, JI Tianyuan, et al. Uncertainty analysis of effects of end wall fillet radius error on high-load stator cascade performance[J]. Journal of Aerospace Power, 2021, 36(10): 2173-2185. (in Chinese)
|
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