Numerical study on flow distribution characteristics of under-race lubrication oil passage
-
摘要:
为探究环下润滑供油通道滑油流量分配特性,采用volume of fluid(VOF)方法对轴心射流收油环内部两相流动进行了计算,获得了供油通道内油膜形成过程与流场特征,重点讨论了供油温度、主轴转速、供油流量及供油孔径组合对流量分配的影响规律,建立了临界孔径比的无量纲关联式。结果表明:滑油射流冲击收油环中心后形成油膜,其边缘断裂形成油带、油矢甩至侧壁面,最终油膜铺满整个端面;计算工况范围内,滑油分配主要受供油流量及孔径影响,各出口流量随供油流量上升均呈线性增加,滑油分配比随供油流量增加而平均降低15.05%;滑油分配比随下游孔径与孔径比的增加而上升;当无量纲供油流量越大且下游无量纲孔径越小时,临界孔径比越高并趋近于1,当无量纲供油流量降低或下游无量纲孔径增大时,临界孔径比则下降。
Abstract:In order to study the oil distribution characteristics of the under-race lubrication oil passage, the volume of fluid (VOF) method was used to calculate two-phase flow in the axis jet oil receiving scoop, and the formation process of oil film and the flow field characteristics in the passage were obtained. The effects of the oil temperature, shaft speed, oil volume flow rate, and aperture combination on the oil flow distribution were emphatically discussed, and the dimensionless correlation formula of the critical aperture ratio was established. The results showed that, the oil jet impinged on the center of the oil receiving scoop and formed an oil film, and the oil droplets and the oil belts formed by the broken film edge were thrown to the side wall, finally the oil film covered the entire end face. Within the calculation range of operating conditions, the distribution of lubricating oil was mainly affected by the oil volume flow rate and aperture. The flow rate at each outlet increased linearly with the increase of oil volume flow rate, and the oil distribution ratio decreased by an average of 15.05% with the increase of oil volume flow rate. The oil distribution ratio increased with the increase of downstream hole diameter and the aperture ratio. When the dimensionless oil supply flow was larger and the downstream dimensionless hole diameter was smaller, the critical aperture ratio was higher and approached to 1, when the dimensionless oil supply flow decreased or the downstream dimensionless hole diameter increased, the critical aperture ratio declined.
-
表 1 收油环结构参数
Table 1. Structure parameters of oil receiving scoop
mm 参数 数值 收油环内径 40 收油环外径 50 供油孔间距 10 供油孔直径 1.0 供油孔长度 5.0 表 2 滑油物性参数
Table 2. Oil physical parameters
温度/℃ 密度/(kg/m3) 运动黏度/(mm2/s) 60 968.8 12.94 75 957.1 9.05 90 945.6 6.24 105 932.8 4.42 120 920.4 3.30 表 3 旋转流道主要尺寸
Table 3. Main dimensions of rotating tube
mm 位置 直径 长度 入口 6.35 25.4 分支出口 A 6.35 25.4 分支出口B 6.35 25.4 旋流通道 12.7 469.9 表 4 不同参数组合下的临界孔径比
Table 4. Critical aperture ratio at different parameter combinations
Nq $ {R'_{\text{d}}} $ Nd=1.0 Nd=1.2 Nd=1.5 Nd=2.0 1.0 0.836 0.773 0.705 0.621 1.2 0.878 0.809 0.746 0.665 1.3 0.885 0.835 0.761 0.687 1.5 0.901 0.851 0.776 0.706 1.6 0.922 0.862 0.799 0.723 1.8 0.944 0.887 0.809 0.745 2.0 0.951 0.893 0.832 0.757 -
[1] 王酉名. 航空发动机对转轴间集油结构收油效率分析[D]. 沈阳: 沈阳航空航天大学,2019. WANG Youming. Analysis of oil collection efficiency of oil collection structure between rotating shafts of aero-engine[D]. Shenyang: Shenyang Aerospace University,2019. (in ChineseWANG Youming. Analysis of oil collection efficiency of oil collection structure between rotating shafts of aero-engine[D]. Shenyang: Shenyang Aerospace University, 2019. (in Chinese) [2] GAO Wenjun,NELIAS D,BOISSON N,et al. Model formulation of churning losses in cylindrical roller bearings based on numerical simulation[J]. Tribology International,2018,121: 420-434. doi: 10.1016/j.triboint.2018.02.003 [3] 李国权. 航空发动机滑油系统的现状及未来发展[J]. 航空发动机,2011,37(6): 49-52,62. LI Guoquan. Present and future of aeroengin oil system[J]. Aeroengine,2011,37(6): 49-52,62. (in ChineseLI Guoquan. Present and future of aeroengin oil system[J]. Aeroengine, 2011, 37(6): 49-52, 62. (in Chinese) [4] BERNARD D,ROBERT R N,HENRY W W. Bearing assembly: US3269786[P]. 1966-08-30. [5] PABST R H,SILAY W J. Shaft sealing and cooling means: US3325232[P]. 1967-06-13. [6] PRASAD S K,SANGLI P,BUYUKISIK O,et al. Prediction of gas turbine oil scoop capture efficiency[R]. New Delhi,India: ASME 2014 Gas Turbine India Conference,2015. [7] KORSUKOVA E,KRUISBRINK A,MORVAN H,et al. Oil scoop simulation and analysis using CFD and SPH[R]. Seoul,Korea: ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition,2016. [8] PRABHAKAR A,ABAKR Y A,SIMMONS K. Effect of vortex shedding on the performance of scoop based lubrication devices[R]. Charlotte,US: ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition,2017. [9] PRABHAKAR A,ABAKR Y A,SIMMONS K. Numerical investigations to assess the impact of shaft speed on the performance of scoop devices[R]. Oslo,US: ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition,2018. [10] ADENIYI A A,MORVAN H,SIMMONS K. Oil-air flow between the cage and inner race of an aeroengine bearing[R]. Seoul,Korea: Turbo Expo: Power for Land,Sea,and Air,2016. [11] KRUG M B,PEDUTO D,KURZ W,et al. Experimental investigation into the efficiency of an aero-engine oil jet supply system[J]. Journal of Engineering for Gas Turbines and Power,2015,137(1): 011505. doi: 10.1115/1.4028255 [12] KOJIMA M,FUKUMURA K,YASUE H. A study on the lubricating oil flow in the automatic transmission[R]. Warrendale,US: SAE International,1991. [13] CHENG Sunwen,YANG W J. Hysteresis in oil flow through a rotating tube with twin exit branches[J]. International Journal of Rotating Machinery,1997,3(4): 249-258. doi: 10.1155/S1023621X97000237 [14] 姜乐,刘振侠,吕亚国. 环下润滑内部空气场流动特性数值计算研究[R]. 昆明: 中国航天第三专业信息网第四十届技术交流会暨第四届空天动力联合会议,2019. [15] 姜乐,刘振侠,吕亚国. 环下润滑结构对径向收油环收油效率影响的数值计算研究[J]. 推进技术,2020,41(6): 1387-1395. JIANG Le,LIU Zhenxia,LYU Yaguo. Numerical investigation for effects of under-race lubrication structure on oil capture efficiency of radial oil scoop[J]. Journal of Propulsion Technology,2020,41(6): 1387-1395. (in ChineseJIANG Le, LIU Zhenxia, LYU Yaguo. Numerical investigation for effects of under-race lubrication structure on oil capture efficiency of radial oil scoop[J]. Journal of Propulsion Technology, 2020, 41(6): 1387-1395. (in Chinese) [16] 吕亚国,姜乐,高晓果,等. 高速轴承环下润滑收油叶片结构参数与工况参数间的匹配关系[J]. 航空学报,2022,43(10): 426037. LYU Yaguo,JIANG Le,GAO Xiaoguo,et al. Matching relationship between structural parameters and operating parameters of oil scoop blade for high speed bearing with under race lubrication[J]. Acta Aeronautica et Astronautics Sinica,2022,43(10): 426037. (in ChineseLYU Yaguo, JIANG Le, GAO Xiaoguo, et al. Matching relationship between structural parameters and operating parameters of oil scoop blade for high speed bearing with under race lubrication[J]. Acta Aeronautica et Astronautics Sinica, 2022, 43(10): 426037. (in Chinese) [17] 朱冬磊,陈国定,李炎军,等. 中介轴承环下流道滑油流动及润滑效率分析[J]. 航空学报,2019,40(11): 304-318. ZHU Donglei,CHEN Guoding,LI Yanjun,et al. Inner ring oil flow and lubrication efficiency analysis of intershaft bearing[J]. Acta Aeronautica et Astronautica Sinica,2019,40(11): 304-318. (in ChineseZHU Donglei, CHEN Guoding, LI Yanjun, et al. Inner ring oil flow and lubrication efficiency analysis of intershaft bearing[J]. Acta Aeronautica et Astronautica Sinica, 2019, 40(11): 304-318. (in Chinese) [18] 强轲,徐让书,戴海宁,等. 某型航空发动机轴间轴承集油结构内的两相流动数值计算[J]. 润滑与密封,2020,45(11): 118-124. QIANG Ke,XU Rangshu,DAI Haining,et al. Numerical calculation of two-phase flow in the oil-collecting structure of an aero-engine intershaft bearing[J]. Lubrication Engineering,2020,45(11): 118-124. (in Chinese). doi: 10.3969/j.issn.0254-0150.2020.11.018QIANG Ke, XU Rangshu, DAI Haining, et al. Numerical calculation of two-phase flow in the oil-collecting structure of an aero-engine intershaft bearing[J]. Lubrication Engineering, 2020, 45(11): 118-124. (in Chinese). doi: 10.3969/j.issn.0254-0150.2020.11.018 [19] 覃经文,曾广乐,郭晖,等. 某涡轴发动机轴承环下润滑结构试验研究[J]. 润滑与密封,2019,44(7): 138-142. QIN Jingwen,ZENG Guangle,GUO Hui,et al. Experimental research on under-race lubrication of bearing for a turboshaft aeroengine[J]. Lubrication Engineering,2019,44(7): 138-142. (in ChineseQIN Jingwen, ZENG Guangle, GUO Hui, et al. Experimental research on under-race lubrication of bearing for a turboshaft aeroengine[J]. Lubrication Engineering, 2019, 44(7): 138-142. (in Chinese) [20] HIRT C W,NICHOLS B D. of fluid (VOF) method for the dynamics of free boundaries[J]. Journal of Computational Physics,1981,39(1): 201-225. doi: 10.1016/0021-9991(81)90145-5 [21] PALEO CAGEAO P,SIMMONS K,PRABHAKAR A,et al. Assessment of the oil scoop capture efficiency in high speed rotors[J]. Journal of Engineering for Gas Turbines and Power,2019,141(1): 012401. doi: 10.1115/1.4040812 [22] 朱泽韬,吕亚国,朱鹏飞,等. 轴心射流收油环内部油气流动特性的数值模拟研究[J]. 推进技术,2024,45(2): 63-72. ZHU Zetao,LYU Yaguo,ZHU Pengfei,et al. Numerical simulation study of oil-air flow characteristics in axis jet oil receiving scoop[J]. Journal of Propulsion Technology,2024,45(2): 63-72. (in ChineseZHU Zetao, LYU Yaguo, ZHU Pengfei, et al. Numerical simulation study of oil-air flow characteristics in axis jet oil receiving scoop[J]. Journal of Propulsion Technology, 2024, 45(2): 63-72. (in Chinese) -

下载: