级环境下跨声速对转压气机优化设计研究

推进技术 ›› 2017, Vol. 38 ›› Issue (2): 348-355.

级环境下跨声速对转压气机优化设计研究

王海童,王掩刚,先松川

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

发布日期:2021-08-15
作者简介:王海童，男，硕士生，研究领域为叶轮机复杂流动机理及优化。E-mail: 694193932@qq.com 通讯作者:王掩刚，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(51376150)。

Optimization of Transonic Counter-Rotating Compressor in Stage-Environment

School of Power and Energy，Northwestern Polytechnical University，Xi’an710072，China,School of Power and Energy，Northwestern Polytechnical University，Xi’an710072，China and School of Power and Energy，Northwestern Polytechnical University，Xi’an710072，China

Published:2021-08-15

摘要/Abstract

摘要： 为研究不同优化策略对跨声速对转压气机性能以及内部流动机理的影响规律，运用人工神经网络结合遗传算法在级环境下对下游转子轮毂型线和积叠规律分别进行了三维优化设计。结果表明:轮毂型线优化和积叠规律优化分别使下游转子效率提升了1.19%和2.87%，整机效率分别提升了0.48% 和0.63%。轮毂型线优化改善了下游转子叶根区域靠近压力面的分离流动，降低了流动损失；下游转子积叠规律优化有效抑制了下游转子叶根角区分离流动，同时降低了叶顶泄漏流损失；轮毂型线优化对根部角区的调控能力优于积叠规律优化，二者的组合优化有望进一步提升对转压气机性能。

关键词: 跨声速；对转压气机；级环境；优化设计

Abstract: To study the influences of optimization strategies on the internal flow and performance of contra-rotating compressor (TCRC)，this paper employed the artificial neural networks combined with the genetic algorithm to three-dimensional redesign the hub geometric profile and stacking law of the downstream rotor. Results revealed that the efficiency of downstream rotor was promoted by 1.19% and 2.87% and the whole compressor efficiency was promoted by 0.48% and 0.63% through optimizing the hub geometric profile and stacking law，respectively. The optimization of the hub profile could effectively improve the large-scale separation on the pressure side of the blade root of downstream rotor. While the optimization of blade stacking law could suppress the flow separation near the corner area of blade root and additionally it could reduce the loss tip leakage flow. The control of hub profile optimization shows a more effective manipulation on the blade root flow than the stacking law optimization. The combination of these two optimization strategies is expected to achieve further improvement for the performance of the contra-rotating compressor.

Key words: Transonic；Counter-rotating compressor；Stage environment；Optimization design

王海童,王掩刚,先松川. 级环境下跨声速对转压气机优化设计研究[J]. 推进技术, 2017, 38(2): 348-355.

WANG Hai-tong,WANG Yan-gang,XIAN Song-chuan. Optimization of Transonic Counter-Rotating Compressor in Stage-Environment[J]. Journal of Propulsion Technology, 2017, 38(2): 348-355.

参考文献

[1] Sharma P B, Pundir D S. A Study of Flow Structure in a Contra-Rotating Axial Compressor Stage[R]. ISABE 89-7023.
[2] 金东海, 展昭, 桂幸民. 基于混合遗传算法的压气机叶型自动优化设计[J]. 推进技术, 2006, 27(4): 349-353. (JIN Dong-hai, ZHAN Zhao, GUI Xin-min.Automatic Design Optimization of Compressor Blades Based on Hybrid Genetic Algorithm[J]. Journal of Propulsion Technology, 2006, 27(4): 349-353.)
[3] Jha R, Chattopadhyay A, Rajadas J. Optimization of Turbomachinery Airfoil Shape for Improved Performance[C]. AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, 2006:49-68.
[4] Anguita D. An Innovative Technique for the Aerodynamic Design of Turbine Blade Profiles Using Artificial Intelligence[R]. AIAA 2003-3737.
[5] 刘仪, 陈铁. 级环境下叶片弯曲气动特性理论的研究探讨[J]. 汽轮机技术, 1997(4): 244-250.
[6] 汪光文, 周正贵, 胡骏. 基于并行遗传算法压气机叶片自动优化设计[J]. 航空动力学报, 2006, 21(5): 923-929.
[7] 王雷, 刘波, 梁俊, 等. 基于多级环境下的双排对转压气机优化设计[J]. 航空动力学报, 2010, 25(6): 1381-1388.
[8] 周明, 孙树栋. 遗传算法原理及应用[M]. 北京:国防工业出版社, 1999.
[9] Goinis G, Stollenwerk S, Nicke E, et al. Steady State Versus Time-Accurate CFD in an Automated Airfoil Section Optimization of a Counter Rotating Fan Stage[R]. ASME GT2011-46190.
[10] 曹志远, 刘波, 张国臣, 等. 对转压气机三维掠动叶优化设计[J]. 推进技术, 2013, 34(4): 483-492. (CAO Zhi-yuan, LIU bo, ZHANG Guo-chen, et al. Three Dimensional Swept Rotor Blade Optimization Design for a Counter-Rotating Compressor[J]. Journal of Propulsion Technology, 2013, 34(4): 483-492.)
[11] 陈云永. 对转压气机特性、流场分析及三维优化研究[D]. 西安:西北工业大学, 2008.
[12] 王掩刚, 牛楠, 任思源, 等. 双级对转压气机多叶排全三维转子优化分析[J]. 中国机械工程, 2010, 21(11): 1310-1314.
[13] 张鹏. 双级对转压气机全工况优化设计[J]. 航空动力学报, 2014, 29(10): 2434-2442.
[14] 胡应交, 王松涛. 一种对转压气机气动设计方法及其验证[J]. 航空动力学报, 2014, 29(5):1135-1144.
[15] 姜斌, 郑群, 王松涛, 等. 跨声速风扇的弯、掠三维设计研究[J]. 航空动力学报, 2012, 27(8): 1815-1825.
[16] 毛明明. 跨声速轴流压气机动叶弯和掠的数值研究[D]. 哈尔滨:哈尔滨工业大学, 2008.　　　　　　　　　　　　　　收稿日期:2016-10-10；修订日期:2016-10-26。基金项目:国家自然科学基金(51376150)。作者简介:王海童,男,硕士生,研究领域为叶轮机复杂流动机理及优化。E-mail: 694193932@qq.com通讯作者:王掩刚,教授,研究领域为叶轮机械气动热力学。E-mail: wyg704@nwpu.edu.cn(编辑:田佳莹)