叶顶密封周向流动及流体激振抑制方法研究

张尧,张万福,顾乾磊,陈璐琪,马凯,李春

振动与冲击 ›› 2020, Vol. 39 ›› Issue (10) : 228-233.

PDF(1966 KB)
PDF(1966 KB)
振动与冲击 ›› 2020, Vol. 39 ›› Issue (10) : 228-233.
论文

叶顶密封周向流动及流体激振抑制方法研究

  • 张尧,张万福,顾乾磊,陈璐琪,马凯,李春
作者信息 +

Research on suppression method for circumferential flow and fluid-induced vibration of blade tip seal

  • ZHANG Yao, ZHANG Wanfu, GU Qianlei, CHEN Luqi, MA Kai, LI Chun
Author information +
文章历史 +

摘要

控制叶顶间隙流体进口预旋及周向流动是减小密封流体激振力的主要方法。基于计算流体力学方法,通过在汽轮机某级叶顶间隙入口的动(围带)、静(汽缸)部件上增加新型微型叶栅,研究新型结构对叶顶间隙流体周向流动及流体激振抑制效果。结果表明:在新型微型叶栅的作用下,流体在叶顶密封入口由正预旋变为负预旋,密封有效阻尼系数由负变正,有效抑制了流体激振,提高了转子稳定性;将微型叶栅安装在围带上时对流体激振的抑制效果整体优于安装在汽缸上,且每两动叶片间数量为10个(围带叶栅)与6个(汽缸叶栅)时,转子系统稳定性最好。

Abstract

The main method to reduce fluid-induced vibration is to control the inlet preswirl and circumferential flow of tip clearance.This paper established three-dimensional computational fluid dynamics (CFD) models of a steam turbine control stage, to study the effect of a new structure on circumferential flow and fluid-induced vibration, by adding the micro cascades on the shroud and cylinder inlet of tip clearance.Calculated results show that under the action of micro cascades, the fluid preswirl at sealing inlet changes from positive to negative, and the effective damping coefficient changes from negative to positive.It was proved that the fluid-induced vibration is effectively suppressed and the rotor stability is improved.It has better suppression effect of fluid-induced vibration when the micro cascades mounted on the shroud rather than on the cylinder.The rotor system has the best stability when there are 10 micro cascades on the shroud and 6 micro cascades on the cylinder between two rotor blades.

关键词

叶顶密封 / 流体激振 / 微型叶栅 / 进口预旋

Key words

tip seal / fluid-induced vibration / micro cascades / inlet preswirl

引用本文

导出引用
张尧,张万福,顾乾磊,陈璐琪,马凯,李春. 叶顶密封周向流动及流体激振抑制方法研究[J]. 振动与冲击, 2020, 39(10): 228-233
ZHANG Yao, ZHANG Wanfu, GU Qianlei, CHEN Luqi, MA Kai, LI Chun. Research on suppression method for circumferential flow and fluid-induced vibration of blade tip seal[J]. Journal of Vibration and Shock, 2020, 39(10): 228-233

参考文献

[1]      何立东,夏松波.转子密封系统流体激振及其减振技术研究简评[J].振动工程报,1999,12(1):64-72.
He Lidong, Xia Songbo. Review on aerodynamic excitation and its elimination method in the rotor seal system[J]. Journal of Vibration Engineering, 1999, 12(1): 64-72.
[2]     Hartmut Krain. Review of centrifugal compressor’s application and development[J]. ASME J. Turbomachinery, 2005, 127: 25-34.
[3]     曹树谦,陈宇恕. 现代密封转子动力学研究综述[J]. 工程力学,2009(2):68-79.
Cao Shuqian, Chen Yushu. A review of modern rotor/seal dynamics[J]. Engineering Mechanics, 2009(2): 68-79.
[4]      Rosenberg C. Investigating aerodynamics transverse force in labyrinth seals in cases involving rotor eccentricity. C. E. Tran. 083[J]. Translated from Energnmashinostrojohic, 1974(8): 15-17.
[5]     王世柱,李志刚,李军,等. 旋转动密封非定常气流激振转子动力特性研究[J]. 工程热物理学报,2015,36(8):1672-1676.
Wang Shizhu, Li Zhigang, Li Jun, et al. Numerical investigations on unsteady flow excitation rotor-dynamic characteristics of rotating seal[J]. Journal of Engineering Thermophysics, 2015, 36(8): 1672-1676.
[6]     陈尧兴,李志刚,李军. 进口预旋对高压迷宫密封流体激振转子动力特性的影响[J]. 润滑与密封,2017(11):1-6.
Chen Yaoxing, Li Zhigang, Li Jun. Effects of inlet preswirl on the flow excitation Rotordynamic characteristics of labyrinth seal[J]. Lubrication Engineering, 2017(11): 1-6.
[7]     Childs D W, Mclean J E, Zhang M, et al. Rotordynamic performance of a negative-swirl brake for tooth-on-stator labyrinth seal[J]. ASME Journal of Engineering for Gas Turbines and Power, 2015, 138(6): V07AT31A011.
[8]     Vannini G, Mazzali C, Underbakke H. Rotordynamic computational and experimental characterization of a convergent honeycomb seal tested with negative preswirl, high pressure with static eccentricity and angular misalignment[J]. ASME Journal of Engineering for Gas Turbines and Power, 2017, 139: 052502. 1-10..
[9]     李军,李志刚. 袋型阻尼密封泄漏流动和转子动力特性的研究进展[J]. 力学进展,2011,41(5):379-395.
Li Jun, Li Zhigang. Research progress on leakage flow and dynamic characteristics of Pocket Damper Seals[J]. Advances in Mechanics, 2011, 41(5): 379-395.
[10]     Nielsen K K, Jønck K, Underbakke H. Hole-pattern and honeycomb seal rotordynamic forces: validation of CFD-based prediction techniques[C]// ASME Turbo Expo 2012: Turbine Technical Conference and Exposition. 2012: 1017-1029.
[11]     Khaleghi H, Tousi A M. Role of tip injection in desensitizing the compressor to the tip clearance size[J]. Aerospace Science & Technology, 2016, 52: 10-17.
[12]     Gao J, Zheng Q, Liu Y, et al. Reduction of turbine tip clearance losses at design and off-design incidences by non-uniform tip injection[J]. Proceedings of the Institution of Mechanical Engineers Part A Journal of Power & Energy, 2014, 228(8): 889-902.
[13]     吕成龙,何立东,涂霆. 反旋流抑制密封间隙内流体激振研究[J]. 液压气动与密封,2014,34(10):28-31.
Lv Chenglong, He Lidong, Tu Ting. Study on suppressing fluid-induced vibration in the seal clearance by anti-swirl flow[J]. Hydraulics Pneumatics & Seals, 2014, 34(10): 28-31.
[14]     Wallis A M, Denton J D, Demargne A A J. The Control of Shroud Leakage Flows to Reduce Aerodynamic Losses in a Low Aspect Ratio, Shrouded Axial Flow Turbine[J]. Journal of Turbomachinery, 2001, 123(2): 334–341.
[15]     Schlienger J, Pfau A, Kalfas A I, et al. Effects of Labyrinth Seal Variation on Multistage Axial Turbine Flow[C]. Proceedings of ASME Turbo Expo, June 16-19, 2003, Altanta, Georgia, USA, 2003: 1-13.
[16]     Jia W, Liu H X. Computational Study of the Effects of Shroud Geometric Variation on Turbine Performance in a 1.5-Stage High-Loaded Turbine[J]. Journal of Thermal Science, 2013, 22(5): 439-446.
[17]     Rosic B, Denton J D. Control of Shroud Leakage Loss by Reducing Circumferential Mixing[J]. Journal of Turbomachinery, 2008, 130: (021010-1)-(021010-7).
[18 ]     Gao J, Zheng Q, Yue G, et al. Control of Shroud Leakage Flows to Reduce Mixing Losses in a Shrouded Axial Turbine[C]. Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science, 2012, 226: 1263-1277.
[19]     Barmpalias K G, Abhari R S, Kalfas A I, et al. Design Considerations for Axial Steam Turbine Rotor Inlet Cavity Volume and Length Scale[J]. Journal of Turbomachinery, 2012, 134: (051031-1)–(051031-9).

PDF(1966 KB)

430

Accesses

0

Citation

Detail

段落导航
相关文章

/