组合压气机中导流叶片的尾迹抖动特性
Stator wake variability in a combined compressor
-
摘要: 为明确多排叶栅压气机中影响静叶尾迹抖动特性的因素及机理,探索调制静叶尾迹抖动周期和幅值的方法,采用数值方法对设计流量为1.12kg/s,转速为60000r/min的一级轴流和离心叶轮组成的组合压气机的非定常流场进行模拟.结果表明:静叶尾迹抖动除受几何因素影响外,还受上下游转子干涉影响,且上下游转子叶片通过频率的异同将影响静叶尾迹抖动的周期性.当上下游转子叶片同频通过时,改变动叶的时序位置可以调制静叶尾迹抖动幅值的大小.另外,静叶尾迹抖动幅值沿叶高方向并不相同,低叶高处静叶尾迹抖动幅值明显大于中、高叶高处静叶尾迹抖动幅值.Abstract: The unsteady flow in a combined compressor,which consists of axial flow and centrifugal compressor impellers,was simulated numerically at mass flow of 1.15kg/s and speed of 60kr/min (design point).The objective was an in-depth analysis of the factors caused stator wake variability.In addition,a method about changing cycle and amplitude of stator wake variability was presented.The results indicate that:stator wake variability is influenced by geometric factor,up- and downstream moving rows.The blade passaging frequencies of up- and downstream rotor are related with the cycle of stator wake variability.Note that the equal blade passaging frequencies in all stages,the clocking positions have much effect on the amplitudes of stator wake variability.Moreover,along the blade’s highness,the amplitudes of stator wake variability are different,which located at low span was greater than that at mid-span and high-span.
-
Key words:
- combined compressor /
- unsteady /
- mixing /
- wake variability /
- modulation
-
[1] Prato J,Lakshminarayana B.Investigation of compressor rotor wake structure at peak pressure rise coefficient and effects of loading[J].ASME Journal of Turbomachinery,1993,115(2):487-500. [2] Pullan G,Denton J D,Dunkley M J.An experimental and computational study of the formation of a streamwise shed vortex in a turbine stage[J].ASME Journal of Turbomachinery,2003,125(2):291-297. [3] Mayle R E.The role of laminar-turbulent transition in gas turbine engines[J].ASME Journal of Turbomachinery,1991,113(3):509-537. [4] Halstead D E,Wisler D C,Okiishi T H,et al.Boundary layer development in axial compressors and turbines part 1 of 4:composite picture[J].ASME Journal of Turbomachinery,1997,119(1):114-127. [5] Ernst M,Michel A,Jeschke P.Analysis of rotor-stator-interaction and blade-to-blade measurements in a two stage axial flow compressor[J].ASME Journal of Turbomachinery,2011,133(1):011027(12 pages). [6] Nolan S P R,Botros B B,Tan C S,et al.Effects of upstream wake phasing on transonic axial compressor performance[J].ASME Journal of Turbomachinery,2011,133(2):021010(12 pages). [7] Key N L,Lawless P B,Fleeter S.Rotor wake variability in a multistage compressor[J].Journal of Propulsion and Power,2010,26(2):344-352. [8] Estevadeordal J,Gogineni S,Goss L.DPIV study of wake rotor synchronization in a transonic compressor.AIAA Paper, 2001-3095,2001. [9] Sanders A J,Fleeter S.Rotor blade-to-blade wake variability and effect on downstream vane response[J].Journal of Propulsion and Power,2002,18(2):456-464. [10] 刘波,曹志鹏,蔡元虎,等.叶栅流场尾迹中非定常涡系的数值模拟[J].西北工业大学学报,2005,23(5):562-566. LIU Bo,CAO Zhipeng,CAI Yuanhu,et al.Numerical simulation of unsteady vortex in the wake of cascade flow[J].Journal of Northwestern Polytechnical University,2005,23(5):562-566.(in Chinese) [11] 项效镕,刘波,王庆伟,等.小型轴流压气机静叶排出口尾迹流动特性[J].航空学报.2009,(11):2045-2051. XIANG Xiaorong,LIU Bo,WANG Qingwei,et al.Flow characterics of stator wale in small axial compressor[J].Acta Aeronautica et Astronautica Sinica,2009,30(11):2045-2051.(in Chinese) [12] Oro J M F,Díaz K M A,Morros C S,et al.Analysis of the deterministic unsteady flow in a low-speed axial fan with inlet guide vanes[J].Journal of Fluids Engineering,2008,130(3):031101(12 pages).
点击查看大图
计量
- 文章访问数: 1640
- HTML浏览量: 6
- PDF量: 449
- 被引次数: 0