分体滑动导叶可调涡轮激波与载荷波动机制

doi:10.3969/j.issn.1004-132X.2020.15.003

中国机械工程 ›› 2020, Vol. 31 ›› Issue (15): 1778-1786.DOI: 10.3969/j.issn.1004-132X.2020.15.003

分体滑动导叶可调涡轮激波与载荷波动机制

杨登峰¹, 潘俞舟¹, 王贵召², 老大中³, HU Leon⁴

1. 东北大学秦皇岛分校控制工程学院, 秦皇岛, 066004;
2. 国家电投集团周口燃气热电有限公司, 周口, 466200;
3. 北京理工大学宇航学院, 北京, 100081;
4. Ford Motor Company, MI 48124, Dearborn, USA

收稿日期:2019-07-02 出版日期:2020-08-10 发布日期:2020-08-26
通讯作者: 老大中(通信作者),男,1957年生,副教授。E-mail:laodazhong@tsinghua.org.cn。
作者简介:杨登峰,男,1985年生,博士、讲师。主要研究方向为热机气动热力学。
基金资助:
国家自然科学基金资助项目(51576015);中央高校基本科研业务费专项资金资助项目(N182303033)；东北大学秦皇岛分校科研启动基金资助项目(9060310952001)

Mechanism of Shock and Load Fluctuation of Variable Nozzle Turbines with Split Sliding Guide Vanes

YANG Dengfeng¹, PAN Yuzhou¹, WANG Guizhao², LAO Dazhong³, HU Leon⁴

1. School of Control Engineering, Northeastern University at Qinhuangdao, Qinhuangdao, Hebei, 066004;
2. State Power Investment Group Zhoukou Gas Thermal Power Co., Ltd., Zhoukou, Henan, 466200;
3. School of Aerospace Engineering, Beijing Institute of Technology, Beijing, 100081;
4. Ford Motor Company, MI 48124, Dearborn, USA

Received:2019-07-02 Online:2020-08-10 Published:2020-08-26

摘要/Abstract

摘要： 针对某柴油机用可调涡轮在低速工况下的低效强激波特征，提出并设计了一种分体滑动导叶，并在10%、40%和100% 3个典型开度下进行了定常/非定常数值计算。结果表明：分体滑动导叶在小开度下可实现对间隙泄漏流动的有效抑制，大幅度提高涡轮效率；在10%开度下，分体滑动导叶提高了涡轮10%的峰值效率，同时涡轮效率在40%和全开工况下也有不同程度的提高。此外，通过合理设计转静间距，分体滑动导叶尾缘激波被大幅度削弱。导叶间隙泄漏流和尾缘激波的抑制可有效弱化转子定子干涉强度，降低下游转子叶片表面载荷波动幅值，提高转子叶片的可靠性。

关键词: 可调涡轮, 分体滑动导叶, 激波, 间隙泄漏流, 载荷波动

Abstract: In view of the low efficiency and strong shock characteristics of the variable nozzle turbines in a diesel engine at low speed, a split sliding guide vane was proposed and designed, and the steady/unsteady numerical calculations were carried out under three typical nozzle openings of 10%, 40% and 100%. Results show that the split sliding guide vanes may effectively restrain the clearance leakage flows and greatly improve turbine efficiency under the small nozzle openings. Under the conditions of 10% opening, the turbine peak efficiency is improved by 10%, besides, turbine efficiency is also improved to different degrees under other openings. At the same time, the trailing edge shocks of the split sliding guide vanes are greatly weakened by the reasonable design of rotor-stator spacing. The weakening of guide blade clearance leakage flows and trailing edge shocks reduces the rotor-stator interference, thus weakens the intensity of load fluctuation on downstream rotor blades and increases the reliability of rotor blades.

Key words: variable nozzle turbine, split sliding guide vane, shock, clearance leakage flow, load fluctuation

中图分类号:

TK413.5

杨登峰, 潘俞舟, 王贵召, 老大中, HU Leon. 分体滑动导叶可调涡轮激波与载荷波动机制[J]. 中国机械工程, 2020, 31(15): 1778-1786.

YANG Dengfeng, PAN Yuzhou, WANG Guizhao, LAO Dazhong, HU Leon. Mechanism of Shock and Load Fluctuation of Variable Nozzle Turbines with Split Sliding Guide Vanes[J]. China Mechanical Engineering, 2020, 31(15): 1778-1786.

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参考文献

[1] MATSUNMOTO K, JINNAI Y. Development of Variable Geometry Turbocharger for Diesel Passenger Car[C]//The 6th International Conference on Turbocharging and Air Management System. London, 1988:329-346.
[2] OKAZAKI Y, MATSUDAIRA N. A Case of Variable Geometry Turbocharger Development[C]//The Third International Conference on Turbocharging and Turbochargers. London, 1986:191-195.
[3] 马朝臣, 朱庆, 杨长茂, 等. 涡轮调节方式对增压柴油机匹配性能的影响[J]. 内燃机学报, 2000, 18(2):165-167. MA Chaochen, ZHU Qiang, YANG Changmao, et al. Effect of Turbine Adjustment Methods on Matching Performance of Turbocharged Diesel Engine[J]. Transactions of Csice, 2000, 18(2):165-167.
[4] BAINES N C. Fundamentals of Turbocharging[M]. White River Junction, Vermont:Concepts NREC, 2005.
[5] MORI I, KIYOHIRO S, KOICHI M, et al. A Study on Improving Fuel Consumption of Heavy-Duty Diesel Engine Specifically Designed for Long-Haul Trucks on Highway[J]. SAE Technical Paper, 2015-01-1256.
[6] WATSON N. Turbocharging the Internal Combustion Engine[M]. London:The Macmillan Press Ltd., 1982.
[7] LIU Y, YANG C, YANG D, et al. Investigations on the Aerodynamic Characteristics and Blade Excitations of the Radial Turbine with Pulsating Inlet Flow[J]. International Journal of Turbo & Jet-Engines, 2016, 33(1):69-80.
[8] LIU Yinhong, YANG Ce, QI Mingxu, et al. Shock, Leakage Flow and Wake Interactions in a Radial Turbine with Variable Guide Vanes[J]. ASME Paper, 2014, No. GT2014-25888.
[9] SPENCE S W T, DORAN W J, ARTT D W. Experimental Performance Evaluation of a 99.0 mm Radial Inflow Nozzled Turbine at Larger Stator-rotor Throat Area Ratios[J]. Proc. IMechE, Part A, 1999,213:205-218.
[10] DORAN W J, SPENCE S W T, ARTT D W. Experimental Performance Evaluation of a 99.0 mm Radial Inflow Nozzled Turbine with Varying Shroud Profiles[J]. Proc. IMechE, Part A, 2001,215:267-280.
[11] ALISTER S, SPENCE S W T, ARTT D W, et al. Experimental and Numerical Investigation of Varying Stator Design Paprameters for a Radial Turbine[J]. ASME Paper, 2006, No. GT2006-90152.
[12] TAMAKI H, GOTO S, UNNO M, IWAKAMI A, et al. The Effect of Clearance Flow of Variable Area Nozzle on Radial Turbine Performance[J]. ASME Paper, 2008, No. 2008-GT-50461.
[13] YANG Dengfeng, YANG Ce, LAO Dazhong, et al. A Detailed Investigation of a Variable Nozzle Turbine with Novel Forepart Rotation Guide Vane[J]. Proc. IMechE, Part D:Journal of Automobile Engineering, 2019, 233(4):994-1007.
[14] HU L J, YANG C, SUN H, et al. Numerical Analysis of Nozzle Clearance Effect on Turbine Performance[J]. Chin. J. Mech. Eng., 2011, 24(4):618-625.
[15] WALKINGSHAW J, SPENCE S, EHRHARD J, et al. A Numerical Study of the Flow Fields in a Highly Off-design Variable Geometry Turbine[J]. ASME Paper, 2010, No. GT2010-22669.
[16] CHEN H. Turbine Wheel Design for Garrett Advanced Variable Geometry Turbines for Commercial Vehicle Applications[C]//Proc. 8th International Conference of Turbochargers and Turbocharging. London, 2006:317-327.
[17] LEI Xinguo, QI Mingxu, SUN Harold, et al. Investigation on the Shock Control Using Grooved Surface in a Linear Turbine Nozzle[J]. Journal of Turbomachinery, 2017, 139(12):121008-121008-12.

分体滑动导叶可调涡轮激波与载荷波动机制

Mechanism of Shock and Load Fluctuation of Variable Nozzle Turbines with Split Sliding Guide Vanes

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