Volume 37 Issue 5
May  2022
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ZHAO Huan, LI Yelong, SUN Dan, MU Wei, MA Ting, HU Guangyang. Numerical and experimental investigation on interstage pressure drop equalization of differential multi-stage brush seals[J]. Journal of Aerospace Power, 2022, 37(5): 934-945. doi: 10.13224/j.cnki.jasp.20210248
Citation: ZHAO Huan, LI Yelong, SUN Dan, MU Wei, MA Ting, HU Guangyang. Numerical and experimental investigation on interstage pressure drop equalization of differential multi-stage brush seals[J]. Journal of Aerospace Power, 2022, 37(5): 934-945. doi: 10.13224/j.cnki.jasp.20210248

Numerical and experimental investigation on interstage pressure drop equalization of differential multi-stage brush seals

doi: 10.13224/j.cnki.jasp.20210248
  • Received Date: 2021-05-18
  • Publish Date: 2022-05-28
  • Through analysis of multi-stage brush seal interstage pressure drop distribution characteristic theory,a new brush seal structure of differential stage was presented,and based on the fluid-structure interaction method,a new multi-stage brush seal three-dimensional entity model at all stages was established to build a new multi-stage brush type seal leakage flow characteristics experiment device;through numerical and experimental research under the different working conditions,the effects of structural parameters on pressure drop equilibrium and leakage characteristics of a new type of multi-stage brush seal were analyzed.The results showed that the standard deviation of the equilibrium ratio of pressure drop between different stages of the traditional multi-stage brush seal structure was 8.41,and that of the equilibrium ratio of pressure drop between different stages of the new structure was 4.69 and 2.07.Compared with the traditional structure at each stage,the new differential multi-stage brush seal with the increasing area of the downstream stage can effectively improve the imbalance of pressure drop between stages.Increasing the backing plate protection height could bring about the minimum standard deviation of the equilibrium of pressure drop ratio between different stages of the new structure,and the pressure drop ratio between different stages was close to each other,which can significantly improve the equilibrium of pressure drop between different stages of the new structure.Reducing the thickness of the brush bundle and increasing the clearance between the brush bundle and the rotor surface could make the leakage of the new multi-stage brush seal increase obviously.

     

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  • [1]
    李军,李志刚,张元桥,等.刷式密封技术的研究进展[J].航空发动机,2019,45(2):74-84.
    [2]
    BAYLEY F J,LONG C A.A combined experimental and theoretical study of flow and pressure distributions in a brush seal[J].Journal of Engineering for Gas Turbine and Power,1993,115(2):404-410.
    [3]
    DINC S,DEMIROGLU M,TURNQUIST N,et al.Fundamental design issues of brush seals for industrial applications[J].Journal of Turbomachinery,2002,124(2):293-300.
    [4]
    何立东,袁新,尹新.刷式密封研究的进展[J].中国电机工程学报,2001,21(12):29-33,54.
    [5]
    FLOWE R R.Brush seal development system[R].AIAA 90-2143,1990.
    [6]
    王凯杰,杨义勇,索双富,等.两级刷式密封的流动计算与系统参数的配置研究[J].润滑与密封,2017,42(10):43-47.
    [7]
    刘璐园,张元桥,李军.基于流固耦合方法的刷式密封刷丝变形及接触力特性的数值研究[J].燃气轮机技术,2019,32(1):1-7.
    [8]
    邱波,李军.基于多孔介质局部非热平衡方法的刷式密封耦合传热特性[J].航空动力学报,2015,30(5):1067-1075.
    [9]
    邱波,李军,丰镇平.考虑刷丝变形的刷式密封摩擦热效应研究[J].工程热物理学报,2013,34(11):2030-2034.
    [10]
    吴施志,江平,力宁,等.刷式密封摩擦生热温度场数值计算及试验[J].航空动力学报,2019,34(4):737-743.
    [11]
    邱波,李军.刷式密封传热特性研究[J].西安交通大学学报,2011,45(9):94-100.
    [12]
    邱波,李军,冯增国,等.两级刷式密封泄漏特性的实验与数值研究[J].西安交通大学学报,2013,47(7):7-12.
    [13]
    孙丹,杜宸宇,刘永泉,等.基于ALE流固耦合方法的刷式密封刷丝接触变形特性理论与试验研究[J].机械工程学报,2020,56(9):170-180.
    [14]
    RABEN M,FRIEDRICHS J,FLEGLER J,et al.Brush seals used in steam environments-chronological wear development and the impact of different seal designs[J].Journal of Engineering for Gas Turbines and Power,2016,138(5):051901.1-051901.10.
    [15]
    RABEN M,FRIEDRICHS J,FLEGLER J.Brush seal frictional heat generation-test rig design and validation under steam environment[R].ASME Paper GT-2016-56951,2016.
    [16]
    PUGACHEV A O,DECKNER M.Experimental and theoretical rotordynamic stiffness coefficients for a three-stage brush seal[J].Mechanical Systems and Signal Processing,2012,31:143-154.
    [17]
    HENDRICKS,R C,GRIFFIN T A,KLINE T R,et al.Relative performance comparison between baseline labyrinth and dual brush compressor discharge seals in a T-700 engine test[R].ASME Paper 94-GT-266,1994.
    [18]
    文龙,王之栎,丁蕾,等.双级低滞后刷式密封级间不均衡性分析[J].北京航空航天大学学报,2014,40(8):1154-1159.
    [19]
    李国勤,孙丹,焦忠泽,等.多级低滞后型刷式密封流动传热特性数值研究[J].风机技术,2019,61(5):56-63.
    [20]
    张国强,孙丹,焦忠泽,等.两级刷式密封流动传热特性数值与实验研究[J].风机技术,2020,62(2):44-52.
    [21]
    赵欢,焦忠泽,孙丹,等.多级刷式密封级间压降分配影响因素数值与实验研究[J].航空学报,2020,41(10):79-91.
    [22]
    孙丹,刘宁宁,胡广阳,等.考虑刷丝变形的刷式密封流场特性力学特性流固耦合研究[J].航空动力学报,2016,31(10):2544-2553.
    [23]
    孙丹,卢江,刘永泉,等.篦齿封严风阻温升特性研究[J].航空学报,2018,39(11):70-79.
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