Studies on the effects of structural parameters on jetcharacteristics of nozzlesin in lubricating aviation gears
-
摘要: 为了研究喷嘴结构对喷嘴射流扩散角和射流流量的影响,采用基于FLUENT的大涡数值模拟方法对喷嘴三维射流流场进行了二相流仿真和单相流仿真,分别通过高速可视化和喷射滑油称重的方法测量了喷嘴射流扩散角和射流流量,并用测量结果对二相流仿真和单相流仿真进行了合理性验证.当喷嘴长径比大于2且喷孔轴线与喷孔上游管道轴线的夹角在0°~90°之间时沿喷孔轴线距喷孔出口100mm范围内射流扩散角近似为零,且增加喷孔直径、喷孔轴线与喷孔上游管道轴线的夹角或者减小喷孔轴向长度均会引起射流流量的增加.结果表明:当喷嘴长径比大于2且喷孔轴线与喷孔上游管道轴线的夹角在0°~90°的范围内变化时对射流扩散角的影响很小;喷孔直径、喷孔轴向长度和喷孔轴线与上游管道轴线的夹角通过影响局部损失和沿程损失,从而影响喷嘴射流流量.Abstract: In order to study the effects of the supply pressure and temperature of oil on the diffusion angle and volume flux of jet oil sprayed by nozzles of gear cases, both the two phase and single phase flow models of the jet flow field of three dimensional nozzles were simulated by employing the Large Eddy Simulation based on the FLUENT. The rationality of the simulation results of the two phase and single phase flow models of jet flow field of three dimensional nozzles was demonstrated by the diffusion angle and volume flux of jet oil measured by the method of high speed visualization and weighting jet oil, respectively. The diffusion angle of jet was approximately zero within the scope of 100 millimeters along the axis apart from the exit of nozzle when the ratio of length to diameter was greater than 2 and the angle between the axis of nozzle orifice and the axis of upstream flow channel changed in the range of 0 to 90 degree. The volume flux of jet oil increased as the orifice diameter, the angle between orifice axis and upstream axis increased and as the orifice axial length decreased. The result indicate that the diffusion angle of jet is not affected in actual working conditions when the ratio of length to diameter is greater than 2 and the angle between the axis of nozzle orifice and the axis of upstream flow channel changes in the range of 0 to 90 degree. Both the local loss and the linear loss are influenced by the change of the orifice diameter, the orifice axial length and the angle between orifice axis and upstream axis, finally leading to variation of volume flux of jet.
-
Key words:
- nozzle /
- oil jet lubrication /
- large eddy simulation /
- diffusion angle of jet /
- volume flux of jet
-
[1] 《航空发动机设计手册》总编委会.航空发动机设计手册:第12册传动及润滑系统[M].北京:航空工业出版社,2002. [2] 《航空发动机设计手册》总编委会.航空发动机设计手册:第13册减速器[M].北京:航空工业出版社,2002. [3] 贾月梅.流体力学[M].北京:国防工业出版社,2006. [4] 刘沛清.自由紊动射流理论[M].北京:北京航空航天大学出版社,2008. [5] CAI Jinsheng,Tsai H M,LIU Feng.Numerical simulation of vortical flows in the near field of jets from notched circular nozzles[J].Computers & Fluids,2010,39(3):539-552. [6] SUN Zuoyu,LI Guoxiu,CHEN Chuan,et al.Numerical investigation on effects of nozzle's geometric parameters on the flow and the aviation characteristics within injector's nozzle for a high-pressure common-rail DI diesel engine[J].Energy Conversion and Management,2015,89(1):843-861. [7] Xiao F,Dianat M,McGuirk J J.LES of turbulent liquid jet primary breakup in turbulent coaxial air flow[J].International Journal of Multiphase Flow,2014,60(4):103-118. [8] 王延忠,牛文韬,唐文,等.喷油方位参数对航空直齿轮喷油润滑过程的影响分析[J].航空动力学报,2015,30(7):1605-1610. WANG Yanzhong,NIU Wentao,TANG Wen,et al.Analysis on influence of spray orientation parameters on spray lubrication process of aero spur gears[J].Journal of Aerospace Power,2015,30(7):1605-1610.(in Chinese) [9] 王延忠,牛文韬,唐文,等.喷油嘴喷射方向偏离的影响因素[J].航空动力学报,2012,27(7):1665-1670. WANG Yanzhong,NIU Wentao,TANG Wen,et al.Research on deflection of nozzle spray direction[J].Journal of Aerospace Power,2012,27(7):1665-1670.(in Chinese) [10] 康灿,张峰,杨敏官,等.环形水射流流场的实验研究与统计分析[J].实验流体力学,2011,25(1):7-12. KANG Can,ZHANG Feng,YANG Minguan,et al.Experimental and statistical analysis of water jet discharged from an annular nozzle[J].Journal of Experiments in Fluid Mechanics,2011,25(1):7-12.(in Chinese) [11] 柴宏生.亚音速射流试验台的设计与流场模拟[D]. 武汉:华中科技大学,2012. CAI Hongsheng.Design of subsonic velocity jet test platform and flow field simulation[D].Wuhan:Huazhong University of Science and Technology,2012.(in Chinese) [12] 刘奕,郭印诚,张会强,等.平面射流及平面射流火焰中拟序结构的实验研究[J].清华大学学报:自然科学版, 2002,42(2):243-246. LIU Yi,GUO Yincheng,ZHANG Huiqiang,et al.Experimental study of coherent structures in planar jets and planar jet flames[J].Journal of Tsinghua University:Science and Technology,2002,42(2):243-246.(in Chinese) [13] 王延忠,牛文韬,唐文,等.航空直齿轮喷油润滑油气两相流分析[J].航空动力学报,2013,28(2):439-444. WANG Yanzhong,NIU Wentao,TANG Wen,et al.Research on oil-air multiphase flow of spray lubrication of aero spur gears[J].Journal of Aerospace Power,2013,28(2):439-444.(in Chinese) [14] TIAN Xiushan,ZHAO Hui,LIU Haifeng,et al.Three-dimensional large eddy simulation of round liquid jet primary breakup in coaxial gas flow using the VOF method[J].Fuel Processing Technology,2015,131(3):396-402. [15] 周建钊,徐肖攀,朱自成,等.基于ICEM CFD与ANSYS FLUENT的热力射流喷嘴流场分析[J].机床与液压,2014,42(17):157-160,122. ZHOU Jianzhao,XU Xiaopan,ZHU Zicheng,et al.Flow field analysis of thermal jet nozzle based on ICEM CFD and ANSYS FLUENT[J].Machine Tools and Hydraulics,2014,42(17):157-160,122.(in Chinese) [16] 禹言芳,李春晓,孟辉波,等.不同形状喷嘴的射流流动与卷吸特性[J].过程工程学报,2014,14(4):549-555. YU Yanfang,LI Chunxiao,MENG Huibo,et al.The jet flow and entrainment characteristics of different shape of nozzles[J].Chinese Journal of Process Engineering,2014,14(4):549-555.(in Chinese) [17] WANG Fujun,FANG Tiegang.Liquid jet breakup for non-circular orifices under low pressures[J].International Journal of Multiphase Flow,2015,72:248-262. [18] 张兆顺,崔桂香,许春晓.湍流大涡数值模拟的理论和应用[M].北京:清华大学出版社,2008. [19] 唐家鹏.FLUENT 14.0超级学习手册[M].北京:人民邮电出版社,2013.
点击查看大图
计量
- 文章访问数: 1062
- HTML浏览量: 3
- PDF量: 597
- 被引次数: 0