Volume 40 Issue 10
Oct.  2025
Turn off MathJax
Article Contents
XIE Xianci, SUN Dan, REN Guozhe, et al. Research and formula construction on wind resistance temperature rise characteristics of the bolt structure on rotor-stator cavity[J]. Journal of Aerospace Power, 2025, 40(10):20240482 doi: 10.13224/j.cnki.jasp.20240482
Citation: XIE Xianci, SUN Dan, REN Guozhe, et al. Research and formula construction on wind resistance temperature rise characteristics of the bolt structure on rotor-stator cavity[J]. Journal of Aerospace Power, 2025, 40(10):20240482 doi: 10.13224/j.cnki.jasp.20240482

Research and formula construction on wind resistance temperature rise characteristics of the bolt structure on rotor-stator cavity

doi: 10.13224/j.cnki.jasp.20240482
  • Received Date: 2024-07-17
    Available Online: 2024-12-18
  • The theoretical model of the windage resistance heating characteristics of the bolt structure in the rotor-stator cavity was analyzed. A numerical solution model for windage resistance heating characteristics of the bolt structure in the rotor-stator cavity was established to analyze the internal flow field characteristics of the rotor-stator cavity and study the influences of structural and operating parameters on windage resistance heating of the bolt structure in the rotor-stator cavity on the basis of verifying the accuracy of the solution model. The theoretical formula for windage resistance heating of the bolt structure in the rotor-stator cavity was constructed using the correction coefficient method. The research results indicated that when the bolt rotated with the rotating disc, the surface of the bolt interacted with the viscous airflow through friction, and the temperature of the gas increased, resulting in windage resistance heating effect. Under the working conditions studied in this article, when the speed increased from 6000 r/min to 15000 r/min, the wind resistance temperature rise coefficient of the bolt structure increased by 24.2%; the inlet flow rate increased from 2.2 g/s to 8.0 g/s, and the wind resistance temperature rise coefficient of the bolt structure decreased by 51.5%; when the number of bolts increased from 6 to 36, the wind resistance temperature rise coefficient of the bolt structure increased by 65.1%; the theoretical formula for windage resistance heating was caused by the bolt structure of the rotor-stator cavity, which can accurately calculate windage resistance heating caused by the bolt structure of the rotor-stator cavity. This article has provided a theoretical basis for the analysis of windage resistance heating characteristics of the bolt structure of the rotor-stator cavity.

     

  • loading
  • [1]
    张美华, 刘振侠, 胡剑平, 等. 旋转盘腔瞬态响应特性的研究[J]. 推进技术, 2014, 35(8): 1056-1062. ZHANG Meihua, LIU Zhenxia, HU Jianping, et al. Study of transient response characteristics of rotating disc cavity[J]. Journal of Propulsion Technology, 2014, 35(8): 1056-1062. (in Chinese

    ZHANG Meihua, LIU Zhenxia, HU Jianping, et al. Study of transient response characteristics of rotating disc cavity[J]. Journal of Propulsion Technology, 2014, 35(8): 1056-1062. (in Chinese)
    [2]
    王嗣鹏, 王源鹤, 邬泽宇, 等. 基于模态分解的轴向通流共转腔流场特性分析[J]. 推进技术, 2024, 45(6): 2304043. WANG Sipeng, WANG Yuanhe, WU Zeyu, et al. Analysis of flow characteristics in rotating cavity with axial throughflow based on modal decomposition[J]. Journal of Propulsion Technology, 2024, 45(6): 2304043. (in Chinese

    WANG Sipeng, WANG Yuanhe, WU Zeyu, et al. Analysis of flow characteristics in rotating cavity with axial throughflow based on modal decomposition[J]. Journal of Propulsion Technology, 2024, 45(6): 2304043. (in Chinese)
    [3]
    曹楠, 窦志伟, 罗翔, 等. 轴向通流旋转盘腔换热特性[J]. 航空动力学报, 2018, 33(5): 1178-1185. CAO Nan, DOU Zhiwei, LUO Xiang, et al. Heat transfer characteristics of a rotating cavity with axial throughflow of cooling air[J]. Journal of Aerospace Power, 2018, 33(5): 1178-1185. (in Chinese

    CAO Nan, DOU Zhiwei, LUO Xiang, et al. Heat transfer characteristics of a rotating cavity with axial throughflow of cooling air[J]. Journal of Aerospace Power, 2018, 33(5): 1178-1185. (in Chinese)
    [4]
    李夫庆, 罗翔, 徐国强. 中心进气转静盘腔的冷气流阻特性实验[J]. 航空动力学报, 2011, 26(6): 1334-1340. LI Fuqing, LUO Xiang, XU Guoqiang. Experimental study of flow friction characteristics for a rotor-stator system with centre inflow of cooling air[J]. Journal of Aerospace Power, 2011, 26(6): 72-83. (in Chinese

    LI Fuqing, LUO Xiang, XU Guoqiang. Experimental study of flow friction characteristics for a rotor-stator system with centre inflow of cooling air[J]. Journal of Aerospace Power, 2011, 26(6): 72-83. (in Chinese)
    [5]
    张达, 罗翔, 徐国强, 等. 转静系盘腔转盘风阻温升实验[J]. 航空动力学报, 2015, 30(5): 1047-1056. ZHANG Da, LUO Xiang, XU Guoqiang, et al. Windage heating experiment on rotating disc in cavity of rotor-stator system[J]. Journal of Aerospace Power, 2015, 30(5): 1047-1056. (in Chinese

    ZHANG Da, LUO Xiang, XU Guoqiang, et al. Windage heating experiment on rotating disc in cavity of rotor-stator system[J]. Journal of Aerospace Power, 2015, 30(5): 1047-1056. (in Chinese)
    [6]
    ZIMMERMANN H, FIRSCHING A, DIBELIUS G H, et al. Friction losses and flow distribution for rotating disks with shielded and protruding bolts[J]. Journal of Engineering for Gas Turbines and Power, 1986, 108(3): 547-552. doi: 10.1115/1.3239945
    [7]
    HAASER F, JACK J, MCGREEHAN W. Windage rise and flowpath gas ingestion in turbine rim cavities[J]. Journal of Engineering for Gas Turbines and Power, 1988, 110(1): 78-85. doi: 10.1115/1.3240090
    [8]
    MILLWARD J A, ROBINSON P H. Experimental investigation into the effects of rotating and static bolts on both windage heating and local heat transfer coefficients in a rotor/stator cavity: ASME Paper 89-GT-196 [R]. Toronto, Canada: ASME, 1989.
    [9]
    DANIELS W A, JOHNSON B V, GRABER D J. Aerodynamic and torque characteristics of enclosed counter-rotating discs[J]. Journal of Turbomachinery, 1991, 113(1): 67-74. doi: 10.1115/1.2927739
    [10]
    OKITA Y, NISHIURA M, YAMAWAKI S, et al. A novel cooling method for turbine rotor-stator rim cavities affected by mainstream ingress[J]. Journal of Engineering for Gas Turbines and Power, 2005, 127(4): 798-806. doi: 10.1115/1.1925647
    [11]
    OKITA Y, YAMAWAKI S. Conjugate heat transfer analysis of turbine rotor-stator system[C]//Proceedings of ASME Turbo Expo: Power for Land, Sea, and Air. Amsterdam, The Netherlands: ASME, 2002: 1103-1113.
    [12]
    LONG C A, MILES A L, COREN D D. Windage measurements in a rotor stator cavity with rotor mounted protrusions and bolts[C]//Proceedings of ASME Turbo Expo: Turbine Technical Conference and Exposition. Copenhagen, Denmark: 2012: 2241-2250.
    [13]
    LOUISE M A. An experimental study of windage due to rotating and static bolts in an enclosed rotor-stator system[D]. Brighton, UK: University of Sussex, 2012.
    [14]
    张达, 罗翔, 徐国强, 等. 表面粗糙或带凸起转盘风阻扭矩实验[J]. 北京航空航天大学学报, 2014, 40(8): 1055-1059. ZHANG Da, LUO Xiang, XU Guoqiang, et al. Windage measurements for rotating disc with protrusions[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(8): 1055-1059. (in Chinese

    ZHANG Da, LUO Xiang, XU Guoqiang, et al. Windage measurements for rotating disc with protrusions[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(8): 1055-1059. (in Chinese)
    [15]
    MOGHADDAM E R, COREN D, LONG C, et al. A numerical investigation of moment coefficient and flow structure in a rotor-stator cavity with rotor mounted bolts[C]//Proceedings of ASME Turbo Expo: Turbine Technical Conference and Exposition. Vancouver, Canada, 2011: 667-679.
    [16]
    COREN D, CHILDS P N, LONG C A. Windage sources in smooth-walled rotating disc systems[J]. Proceedings of the Institution of Mechanical Engineers: Part C Journal of Mechanical Engineering Science, 2009, 223(4): 873-888. doi: 10.1243/09544062JMES1260
    [17]
    MOHAMED S N, CHEW J W, HILLS N J. Effect of bolts on flow and heat transfer in a rotor-stator disk cavity[J]. Journal of Engineering for Gas Turbines and Power, 2017, 139(5): 051901. doi: 10.1115/1.4035144
    [18]
    MOHAMED S N, CHEW J, HILLS N. Flow and windage due to bolts on a rotating disc[J]. Proceedings of the Institution of Mechanical Engineers: Part C Journal of Mechanical Engineering Science, 2017, 231(15): 2925-2941. doi: 10.1177/0954406216642260
    [19]
    MOHAMED S N, CHEW J W, HILLS N J. Simplified protrusion drag and heat transfer modelling of bolts on a rotating disc: ASME Paper GT2015-43501 [R]. Montreal, Canada, 2015.
    [20]
    CAO Nan, LUO Xiang, WU Zeyu, et al. Effect of rotor-mounted protrusion on sealing performance and flow structure in rotor-stator cavity[J]. Chinese Journal of Aeronautics, 2018, 31(11): 2057-2072. doi: 10.1016/j.cja.2018.08.016
    [21]
    TAO Zhi, ZHANG Da, LUO Xiang, et al. Windage heating in a shrouded rotor-stator system[J]. Journal of Engineering for Gas Turbines and Power, 2014, 136(6): 0626021-6260210.
    [22]
    LUO Xiang, ZHANG Da, TAO Zhi, et al. Windage measurements in a rotor-stator system with superimposed cooling and rotor-mounted protrusions[J]. Journal of Engineering for Gas Turbines and Power, 2014, 136(4): 042505. doi: 10.1115/1.4026086
    [23]
    WU Zeyu, LUO Xiang, ZHU Jianqin, et al. Effect of the protrusion shape on gas ingestion of two sealing structures[J]. Chinese Journal of Aeronautics, 2021, 34(4): 320-331. doi: 10.1016/j.cja.2020.09.052
    [24]
    伏宇, 赵丹, 邹咪, 等. 航空发动机旋转盘腔温升特性及抑制方法研究[J]. 燃气涡轮试验与研究, 2021, 34(1): 1-4. FU Yu, ZHAO Dan, ZOU Mi, et al. Study on temperature rise characteristics and suppression method of rotating disk cavity of aero-engine[J]. Gas Turbine Experiment and Research, 2021, 34(1): 1-4. (in Chinese doi: 10.3969/j.issn.1672-2620.2021.01.001

    FU Yu, ZHAO Dan, ZOU Mi, et al. Study on temperature rise characteristics and suppression method of rotating disk cavity of aero-engine[J]. Gas Turbine Experiment and Research, 2021, 34(1): 1-4. (in Chinese) doi: 10.3969/j.issn.1672-2620.2021.01.001
    [25]
    《航空发动机设计手册》总编委会编. 航空发动机设计手册: 第16册 空气系统及传热分析[M]. 北京: 航空工业出版社, 2002. Editorial committee of aero engine design manual. Aero engine design manual: Book 16 transmission and lubrication system[M]. Beijing: Aviation Industry Press, 2002. (in Chinese

    Editorial committee of aero engine design manual. Aero engine design manual: Book 16 transmission and lubrication system[M]. Beijing: Aviation Industry Press, 2002. (in Chinese)
    [26]
    DENECKE J, DULLENKOPF K, WITTIG S, et al. Experimental investigation of the total temperature increase and swirl development in rotating labyrinth seals[C]//Proceedings of ASME Turbo Expo: Power for Land, Sea, and Air. Reno, US: ASME, 2005: 1161-1171.
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (582) PDF downloads(50) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return