为研究非轴对称静叶应用于风扇/压气机中提高畸变条件下工作性能和稳定性的可行性,设计一种非轴对称静叶结构,并将其应用于某单级风扇.通过对均匀进口条件下原型风扇和非轴对称风扇流场进行求解,得到两型风扇的特性曲线,并对两型风扇在设计点工况下流场进行对比分析.结果表明:非轴对称风扇效率在最高效率点附近要高于轴对称风扇,但其稳定工作范围明显小于轴对称风扇;采用非轴对称静叶会增加动叶内的非定常扰动,使工作稳定性下降;非轴对称静叶区域内的角区分离得到明显抑制,流场得到改善.
In order to study the feasibility of nonaxisymmetric stator in transonic fan with distorted inlet, a nonaxisymmetric stator was designed. Numerical simulations were performed to investigate the performance of axisymmetric fan and nonaxisymmetric fan with clean inlet. The performance characteristic of the fans were obtained, and the unsteady flow fields at design point were compared and analyzed. Results indicate that the efficiency of nonaxisymmetric fan is higher than that of axisymmetric one near the maximum efficiency point, but its stable working range is smaller than that of axisymmetric one obviously. Unsteady destabilization in the rotor flow field increases because of the nonaxisymmetric structure. While, corner separation is restrained in the stator hub and flow field is improved.
[1]VUNNAM K, HOOVER R. Modeling of inlet distortion using a combined turbofan and nacelle inlet model during crosswind and low speed forward operation[C]// ASME Proceedings. Vancouver, British Columbia, Canada: International Gas Turbine Institute, 2011, 1: 371-380.
[2]SUN Peng, GAO Hai-yang, ZHONG Jing-jun, et al. Study on the influence of total pressure distortion on end wall flow field in a supersonic compressor[C]// ASME Proceedings . San Antonio, Texas, USA: International Gas Turbine Institute, 2013, 6C: V06CT42A017.
[3]ROSE M G. Nonaxisymmetric endwall profiling in the HP NGVs of an axial flow gas turbine[R].ASME 1994:94-GT-249.
[4]HOEGER M, CARDAMONE P. FOTTNER L. Influence of endwall contouring on the transonic flow in a compressor vane[R]. ASME Paper, 2002 : GT-2002-30440.
[5]HARVEY N W. Some effects of nonaxisymmetric endwall profiling on axial flow compressor aero dynamics Part I:linear cascade investigation[R].ASME Paper, 2008 :GT200850990.
[6]李国君,马晓永,李军.非轴对称端壁成型及其对叶栅损失影响的数值研究[J]. 西安交通大学学报, 2005,39(11): 9-12.
LI Guo-jun. MA Xiao-yong. LI Jun. Non-axisymmetric turbine end wall profiling and numerical investigation of its effect on the turbine cascade loss[J]. Journal of Xi’an Jiaotong University, 2005,39(11): 9-12 (in Chinese).
[7]孙平, 高翔, 李传鹏. 非轴对称端壁对压气机性能和流动特性的影响[J]. 科技创新导报, 2012 (25): 85-87.
SUN Ping. GAO Xiang. LI Chuan-peng. Influence of nonaxisymmetric endwall contour on compressor performance and fluid dynamics[J]. Science and Technology Innovation Herald, 2012 (25): 85-87. (in Chinese)
[8]赵养正,刘前智,廖明夫. 非均匀栅距对压气机叶片非定常气动力的影响[J]. 推进技术,2007, 28(2):167-169.
ZHAO Yang-zheng. LIU Qian-zhi. LIAO Ming-fu. Effects of uneven blade spacing on unsteady blade forcing in an axial compressor[J]. Journal of Propulsion Technology, 2007, 28(2):167-169. (in Chinese)
[9]白志刚,刘前智. 非均匀栅距对轴流压气机流动影响的数值研究[J]. 航空工程进展,2010, 1(1):90-94.
BAI Zhi-gang. LIU Qian-zhi. Numerical study of the effects of uneven blade spacing on the flow in an axial compressor[J]. Advances in Aeronautical Science and Engineering. 2010, 1(1):90-94. (in Chinese)
[10]孙鹏. 总压畸变对跨声速压气机流场结构影响的全流道数值模拟[D]. 哈尔滨:哈尔滨工业大学, 2007.
SUN Peng. All annulus numerical simulation of total pressure distortion effect in a transonic fan[D].Harbin:Harbin Institute of Technology,2007. (in Chinese)
[11]SUN Peng, ZHONG Jing-jun, YANG Mu-xiao, et al. Effects of bowed stator on a fan characteristic with distorted inlet[C]// ASME Proceedings. Glasgow, UK: International Gas Turbine Institute,2010, 7: 2585-2591.
[12]张靖煊. 畸变条件下轴流压气机叶顶间隙流对流动失稳影响的非定常机制[D]. 北京:中国科学院研究生院, 2007.
ZHANG Jing-xuan. The unsteady mechanism and the role of tip clearance flow in distortion induced instability in an axial compressor[D]. Beijing: Graduate School of the Chinese Academy of Sciences,2007. (in Chinese)