Influence of pulse frequencies on fluid flow of a twin entry radial turbine rotor inlet
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摘要:
为了更好地了解脉冲频率对双通道涡轮转子进口流动特性的影响,应用ANSYS CFX软件对不同频率(20、40、80 Hz)脉冲进气条件下的双通道径向涡轮进行了非稳态数值计算,探究了进气脉冲频率对双通道涡轮转子进口入射角的影响,并进一步分析了脉冲频率对转子下游流场的影响。结果表明:脉冲频率对转子进口入射角的影响较大,一个脉冲周期内,转子进口入射角出现两个波峰和两个波谷,波峰附近入射角随频率升高而减小,波谷附近入射角随频率升高而增大;入射角沿叶高分布规律可以发现,叶根部分和叶高部分入射角随频率变化趋势相反,另外,叶根分支进口压力更大时,双通道涡轮进口流动特性更稳定。
Abstract:In order to better understand the impact of pulse frequency on the flow characteristics of the twin entry turbine rotor inlet, ANSYS CFX software was applied to numerical calculation of two-channel radial turbines with different frequencies (20, 40, 80 Hz) under the condition of pulse intake, while the distribution law of rotor inlet incidence angle in one pulse period, and the distribution law of blade height and circumferential direction were obtained. The results showed that in one pulse period, there were two peaks and two troughs in the incidence angle of the rotor inlet, the incidence angle near the crest decreased with the increase of frequency, and the incidence angle near the trough increased with the increase of frequency. The incidence angle distribution along the blade height took 0.5 blade height as the dividing point, and the incidence angle of the blade root part and the blade height part presented an opposite trend with the frequency. When the inlet pressure of blade root branch was larger, the inlet flow characteristics of twin entry turbines were more stable.
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Key words:
- pulse flow /
- pulse frequency /
- twin entry radial turbine /
- incidence angle /
- rotor inlet
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表 1 涡轮机模型参数
Table 1. Parameters of turbine model
参数 数值 叶片数 10 进口直径/mm 70 出口直径/mm 46 蜗壳出口直径/mm 64 表 2 不同频率脉冲条件下i平均值与标准差(hub-升工况,0.8叶高位置)
Table 2. Mean value and standard deviation of i under different pulse frequencies (hub-rise condition,0.8 blade height position)
频率/Hz 平均值/(°) 标准差/(°) 20 8.9 18.3 40 10.9 18.6 80 11.2 18.4 表 3 不同频率脉冲条件下i平均值与标准差(hub-降工况,0.2叶高位置)
Table 3. Mean value and standard deviation of i under different pulse frequencies (hub-fall condition,0.2 blade height position)
频率/Hz 平均值/(°) 标准差/(°) 20 5.4 25.9 40 7.5 25.8 80 11.8 25.7 表 4 不同频率脉冲条件下i平均值与标准差(shr-升工况,0.2叶高位置)
Table 4. Mean value and standard deviation of i under different pulse frequencies (shr-rise condition,0.2 blade height position)
频率/Hz 平均值/(°) 标准差/(°) 20 −7.5 16.7 40 −4.9 18.8 80 −1 20 表 5 不同频率脉冲条件下i平均值与标准差(shr-降工况,0.8叶高位置)
Table 5. Mean value and standard deviation of i under different pulse frequencies (shr-fall condition,0.8 blade height position)
频率/Hz 平均值/(°) 标准差/(°) 20 23.8 32.3 40 25.2 31.1 80 26.1 31.5 -
[1] PISCHINGER F,WUNSCHE A. The characteristic behaviors of radial turbines and its influence on the turbocharging process[R]. Tokyo,Japan: International Council on Combustion engines (CIMAC) Conference,1977. [2] SCHORN N A. The radial turbine for small turbocharger applications: evolution and analytical methods for twin-entry turbine turbochargers[J]. SAE International Journal of Engines,2014,7(3): 1422-1442. doi: 10.4271/2014-01-1647 [3] DALE A,WASTON N. Vaneless radial turbocharger turbine performance[R]. London,UK: 3rd International Conference on Turbocharging and Turbochargers,1986. [4] SHAHHOSSEINI M R,HAJILOUY-BENISI A,RAJABIAN M. A numerical and experimental investigation of the effects of flow ratio on the flow and performance characteristics of a twin entry radial turbine[R]. ASME GT2011-46308,2011. [5] SHAHHOSSEINI M R,HAJILOUY-BENISI A,RAD M. Numerical and experimental investigation of the flow and performance characteristics of twin-entry radial turbine under full and partial admission conditions[R]. ASME GT2008-50397,2008. [6] YEO J H,BAINES N C. Laser velocity measurements in a twin-entry vaneless radial turbocharger turbine[J]. JSME International Journal Series B,1994,37(4): 861-870. [7] 丰镇平,张元林. 双进口无叶蜗壳径流涡轮的脉冲流动特性[J]. 车用发动机,1992(3): 37-44. FENG Zhenping,ZHANG Yuanlin. Pulsating flow behaviour in a twin-entry vaneless radial-inflow turbine[J]. Vehicle Engine,1992(3): 37-44. (in ChineseFENG Zhenping, ZHANG Yuanlin. Pulsating flow behaviour in a twin-entry vaneless radial-inflow turbine[J]. Vehicle Engine, 1992(3): 37-44. (in Chinese) [8] 詹志胜,施新,彭文. 异相脉冲进气混流涡轮非定常特性数值模拟[J]. 工程热物理学报,2016,37(1): 51-55. ZHAN Zhisheng,SHI Xin,PENG Wen. Simulation on unsteady performance of a twin-entry mixed-flow turbine under out-of-phase pulse flow conditions[J]. Journal of Engineering Thermophysics,2016,37(1): 51-55. (in ChineseZHAN Zhisheng, SHI Xin, PENG Wen. Simulation on unsteady performance of a twin-entry mixed-flow turbine under out-of-phase pulse flow conditions[J]. Journal of Engineering Thermophysics, 2016, 37(1): 51-55. (in Chinese) [9] PALENSCHAT T,NEWTON P,MARTINEZ-BOTAS R F,et al. 3-D computational loss analysis of an asymmetric volute twin-scroll turbocharger[R]. ASME GT2017-64190,2017. [10] COSTALL A W,MCDAVID R M,MARTINEZ-BOTAS R F,et al. Pulse performance modeling of a twin entry turbocharger turbine under full and unequal admission[J]. Journal of Turbomachinery,2011,133(2): 1. [11] CERDOUN M,GHENAIET A. Unsteady behaviour of a twin entry radial turbine under engine like inlet flow conditions[J]. Applied Thermal Engineering,2018,130: 93-111. doi: 10.1016/j.applthermaleng.2017.11.001 [12] KETATA A,DRISS Z. Characterization of double-entry turbine coupled with gasoline engine under in- and out-phase admission[J]. Energy,2021,236: 121447. doi: 10.1016/j.energy.2021.121447 [13] WANG Zhihui,MA Chaochen,HUANG Zhi,et al. A novel variable geometry turbine achieved by elastically restrained nozzle guide vanes[J]. Proceedings of the Institution of Mechanical Engineers:Part D Journal of Automobile Engineering,2020,234(9): 2312-2329. doi: 10.1177/0954407020909662 [14] HAMEL M,ABIDAT M,ALI LITIM S. Investigation of the mixed flow turbine performance under inlet pulsating flow conditions[J]. Comptes Rendus Mécanique,2012,340(3): 165-176. [15] QI Mingxu,LEI Xinguo,WANG Zhen,et al. Investigation on the flow characteristics of a VNT turbine under pulsating flow conditions[J]. Proceedings of the Institution of Mechanical Engineers,Part D: Journal of Automobile Engineering,2019,233(2): 396-412. doi: 10.1177/0954407017744922 [16] WATSON N,JANOTA M S. Turbocharging the internal combustion engine[M]. New Yark,US: The Macmillan Press Limited,1982. [17] JAPIKSE D,BAINES N C. Introduction to turbomachinery[M]. Oxford,UK: Oxford University Press,1994. -

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