ACTA AERONAUTICAET ASTRONAUTICA SINICA >
Theoretical and experimental study of leakage characteristics of honeycomb seal
Received date: 2016-06-07
Revised date: 2016-07-17
Online published: 2016-08-03
Supported by
National Natural Science Foundation of China (11302133, 51675351); Natural Foundation of Liaoning Province (2015020113)
The leakage characteristics of the honeycomb seal directly influence the working efficiency of the aero-engine. The leakage characteristics of honeycomb seal are analyzed using theoretical and experimental methods. The CFD model for the flow characteristic of honeycomb seal is developed to analyze the influence of rotational speed, inlet/outlet pressure ratio, subtense distance, cell depth, and wall thickness on seal leakage and to reveal the densification mechanism of honeycomb seal. The seal leakage test rig is designed and built to analyze the influence of the inlet/outlet pressure ratio and the rotational speed on leakage of honeycomb seal. Numerical analysis and experimental tests are conducted to verify each other. Based on the Egli formula for leakage quantity of the traditional classic labyrinth seal, the calculation formula for the leakage quantity of honeycomb seal is constructed, considering the factors influencing the leakage characteristics of honeycomb seal. The results show that the cell depth, subtense distance and wall thickness can influence the development of the vortex system and the density of honeycomb holes, and thereby influence the leakage. The more fully the vortex system develops and the greater the density of honeycomb hole is, the less honeycomb seal leakage will be. The results show that the rotational speed has little influence on the honeycomb seal leakage. The leakage linearly increase with the increasing inlet/outlet pressure ratio. With the increase of the honeycomb cell depth, the honeycomb seal leakage is firstly reduced and is then stabilized. With the increase of the subtense distance, the honeycomb seal leakage decreases initially, and then increases in small particle size range. With the increase of the wall thickness, the honeycomb seal leakage increases linearly initially, and then slowly increases. The results of this study can assist in improving the design of annular seal.
SUN Dan , WANG Mengfei , AI Yanting , XIAO Zhonghui , MENG Jigang , LI Yun . Theoretical and experimental study of leakage characteristics of honeycomb seal[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017 , 38(4) : 420512 -420512 . DOI: 10.7527/S1000-6893.2016.0214
[1] 晏鑫, 李军, 丰镇平. 预旋对蜂窝密封和迷宫密封内流动传热特性影响[J]. 航空动力学报, 2009, 24(4):772-776. YAN X, LI J, FENG Z P. Influence of inletpreswirl on discharge and heat transfer characteristics of honeycomb and smooth labyrinth seals[J]. Journal of Aerospace Power, 2009, 24(4):772-776 (in Chinese).
[2] CHILDS D W, ELROD D, HALE K. Annular honeycomb seals:Test results for leakage and rotor-dynamic coefficients; comparisons to labyrinth and smooth configurations[J]. Journal of Tribology, 1989, 111(2):502-511.
[3] 张毅, 曹丽华, 索付军. 蜂窝密封泄漏流动特性影响因素的数值研究[J]. 动力工程学报, 2013, 33(10):775-781. ZHANG Y, CAO L H, SUO F J. Numerical investigation on factors influencing leakage flow characteristics of honeycomb seals[J]. Journal of Chinese Society of Power Engineering, 2013, 33(10):775-781 (in Chinese).
[4] MIRKO M, COSIMO B, DANIELE M, et al. Flat plate honeycomb seals friction factor analysis[J]. Journal of Engineering for Gas Turbines and Power, 2015, 138(7):072505.1-072505.10.
[5] ALESSIO D, ANDREA R, ELENA C, et al. Numerical analysis of honeycomb labyrinth seals:Cell geometry and fin tip thickness impact on the discharge coefficients[C]//Proceedings of ASME Turbo Expo 2015:Turbine Technical Conference and Exposition, 2015.
[6] 索付军. 蜂窝密封内部耗散机理的数值研究[D]. 吉林:东北电力大学, 2013:10-15. SUO F J. Numerical investigation on the influence leakage flow characteristics of honeycomb seal[D]. Jilin:Northeast Dianli University, 2013:10-15 (in Chinese).
[7] 晏鑫, 李军, 丰镇平. 蜂窝密封内流动传热及转子动力特性的研究进展[J]. 力学进展, 2011, 41(2):201-216. YAN X, LI J, FENG Z P. Review of the discharge, heat transfer and rotor-dynamic characteristics of honeycomb seals[J]. Advanced in Mechanics, 2011, 41(2):201-216 (in Chinese).
[8] 吕江, 何立东, 王晨阳. 蜂窝密封在小功率汽轮机轴端密封上的应用[J]. 润滑与密封, 2015, 40(6):90-94. LV J, HE L D, WANG C Y. Application of honeycomb seal on shaft-end seal of low power steam turbines[J]. Lubrication Engineering, 2015, 40(6):90-94 (in Chinese).
[9] 李志刚, 宁霄, 晏鑫. 蜂窝面迷宫密封泄漏特性和鼓风加热特性研究[J]. 工程热物理学报, 2015, 36(6):1196-1200. LI Z G, NING X, YAN X. Investigation on leakage characteristics and windage heating of honeycomb labyrinth seal[J]. Journal of Engineering Thermophysics, 2015, 36(6):1196-1200 (in Chinese).
[10] HE L D, YUAN X, JIN Y. Experimental investigation of the sealing performance of honeycomb seals[J]. Chinese Journal of Aeronautics, 2011, 24(1):13-17.
[11] 李金波, 何立东. 蜂窝密封流场旋涡能量耗散的数值研究[J]. 中国电机工程学报, 2007, 27(32):67-71. LI J B, HE L D. Energy dissipation of vortexes in honeycomb seals using numerical simulation[J]. Proceedings of the CSEE, 2007, 27(32):67-71 (in Chinese).
[12] 孙丹, 王双, 艾延廷. 阻旋栅对密封静力与动力特性影响的数值分析与实验研究[J]. 航空学报, 2015, 36(9):3002-3011. SUN D, WANG S, AI Y T. Numerical and experimental research on performance of swirl brakes for the static and dynamic characteristics of seals[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(9):3002-3011 (in Chinese).
[13] STOKER H L. Determining and improving labyrinth seal performance in current and advanced high performance gas turbines:AGARD CP 273[R]. 1978.
[14] STOKER H, COX D, HOLLE G. Aerodynamic performance of conventional and advanced design labyrinth seal leakage with solid-smooth, abradable and honeycomb lands:NASA-CR-135307[R]. Washington, D.C.:NASA, 1997.
[15] SCHRAMM V, WILLENBORG K, KIM S. Influence of a honeycomb facing on the flow through a stepped labyrinth seal[J]. Journal of Engineering for Gas Turbines and Power, 2002, 124(1):140-146.
[16] KOOL G, BINGEN F, PAOLILLO R. High temperature, high speed seal test rig-design, build, and validation:AIAA-2005-3902[R]. Reston:AIAA, 2005.
[17] PAOLILLO R, VASHIST T K, CLOUD D, et al. Rotating seal rig experiments:Test results and analysis modeling[J]. ASME Turbo Expo 2006:Power for Land, Sea and Air, 2006, 32(10):1551-1559.
[18] 李军, 邓清华, 丰镇平. 蜂窝汽封和迷宫式汽封流动性能比较的数值研究[J]. 中国电机工程学报, 2005, 25(16):108-111. LI J, DENG Q H, FENG Z P. Comparison of the flow characteristics for the honeycomb and labyrinth seal using numerical simulation[J]. Proceedings of the CSEE, 2005, 25(16):108-111 (in Chinese).
[19] LI J, KONG S R, YAN X. Numerical investigation on leakage performance of the rotating labyrinth honeycomb seal[J]. Journal of Engineering for Gas Turbine and Power, 2010, 132(6):062501.1-062501.11.
[20] YAN X, LI J, SONG L M, et al. Investigations on the discharge and total temperature increase characteristics of the labyrinth seals with honeycomb and smooth lands[J]. Journal of Turbomachinery, 2009, 131(4):041009.1-041009.8.
[21] 陈秀秀, 晏鑫, 李军. 蜂窝叶顶密封对透平气动性能的影响研究[J]. 西安交通大学学报, 2016, 50(4):1-7. CHEN X X, YAN X, LI J. Effect of honeycomb shroud seals on aerodynamic performance of turbine stages[J]. Journal of Xi'an Jiaotong University, 2016, 50(4):1-7 (in Chinese).
[22] 李志刚, 李军, 丰镇平. 蜂窝密封流动特性的数值研究和泄漏量计算公式的构造[J]. 机械工程学报, 2011, 47(2):142-148. LI Z G, LI J, FENG Z P. Numerical investigation on discharge behavior and prediction formula establishment of leakage flow rate of honeycomb seal[J]. Journal of Mechanical Engineering, 2011, 47(2):142-148 (in Chinese).
[23] GAMAL A J M, VANCE J M. Labyrinth seal leakage tests:Tooth profile, tooth thickness, and eccentricity effects[J]. Journal of Engineering for Gas Turbines and Power, 2008, 130(1):012510.1-012510.11.
/
〈 |
|
〉 |