脊状结构组合式轮片状阴极工作齿齿形优化设计

doi:10.3969/j.issn.1000-1093.2015.08.019

兵工学报 ›› 2015, Vol. 36 ›› Issue (8): 1508-1517.doi: 10.3969/j.issn.1000-1093.2015.08.019

脊状结构组合式轮片状阴极工作齿齿形优化设计

贾建利^1，2，刘金合¹，沈建强²

(1.西北工业大学材料学院，陕西西安 710072; 2.西安工业大学机电工程学院，陕西西安 710021)

收稿日期:2014-09-09 修回日期:2014-09-09 上线日期:2015-10-16
作者简介:贾建利（1979—），男，博士研究生
基金资助:
武器装备预先研究项目（62202014502）；陕西省特种加工重点实验室开放基金项目（ST12012）；兵器预先研究基金项目(62201070712)

The Optimization of Assembled Turntable Working Teeth Cathode Profile with Riblet Surface

JIA Jian-li^1,2, LIU Jin-he¹, SHEN Jian-qiang²

(1.School of Materials Science and Engineering, Northwestem Polytechnical University, Xi’an 710072, Shaanxi, China;2.School of Mechatronic Engineering, Xian Technological University, Xian 710021, Shaanxi, China)

Received:2014-09-09 Revised:2014-09-09 Online:2015-10-16

摘要/Abstract

摘要： 针对组合式轮片状阴极工作齿（TWTC）齿形优化设计，研究脊状结构的形状参数与减阻量之间的关系。根据湍流边界层粘性底层流速服从线性分布的规律，利用粘性底层流速分布公式来计算流场特性参数，提出将脊状结构、圆角过渡用于组合式TWTC齿形修形。对未修形、脊状结构、圆角过渡组合式TWTC修形的电解加工间隙流场进行仿真和试验验证。结果表明：采用脊状结构修形工作齿可以有效减小电解液流道的阻力，提高加工间隙电解液的流速，使加工间隙最高流速从42.5 m/s提高到58.6 m/s，加速了阳极溶解速度，提高了材料去除率；采用圆角过渡修形工作齿能够减少、甚至避免空穴、涡流、分离、气泡现象产生，实现均匀小间隙稳定深孔内螺旋线加工，提高加工精度和表面质量。

关键词: 兵器科学与技术, 脊状结构, 电解加工, 阴极, 流场

Abstract: The relation between shape parameter and drag reduction of the riblet surface is discussed to optimize the teeth profile of assembled turntable working teeth cathode (TWTC). According to the linear distributing law to which the flow velocity in viscous sublayer of turbulence boundary layer submits, the characteristic parameters of flow field are calculated by the formula of flow velocity in viscous sublayer, and then a scheme of using the riblet surface and transition fillets for working-teeth is investigated. The flow field in the machining gap of the un-optimized TWTC with riblet surface and transition fillets is verified by simulation and experiments. The results show that the assembled TWTC with riblet surface greatly reduces the resistance of electrolyte flow channel and increases the maximum flow velocity of electrolyte in the machining gap from 42.5 m/s to 58.6 m/s. Meanwhile, it boosts anodic dissolution rate as well as material removal rate of electrochemical machining. The cavitations, eddy flow, separation and bubble can be decreased and even avoided using the transition fillets between working teeth, which realize the stable machining of internal spiral line in the uniformed gap and improve the machining accuracy and surface quality of electrochemical machining.

Key words: ordnance science and technology, riblet surface, electrochemical machining, cathode, flow field

中图分类号:

TG662

贾建利，刘金合，沈建强. 脊状结构组合式轮片状阴极工作齿齿形优化设计[J]. 兵工学报, 2015, 36(8): 1508-1517.

JIA Jian-li, LIU Jin-he, SHEN Jian-qiang. The Optimization of Assembled Turntable Working Teeth Cathode Profile with Riblet Surface[J]. Acta Armamentarii, 2015, 36(8): 1508-1517.

参考文献

［1］ Rajurkar K P, McGeough J A. Newdevelopment of electrochemical machining [J]. Annals of the CIRP, 1999,48(2): 567-579.
[2] Walsh M J. Turbulent boundary layer drag reduction using riblets [C]∥AIAA 20th Aerospace Sciences Meeting. Orlando, Florida, New York: AIAA, 1982.
[3] Walsh M J. Riblets as a viscous drag reduction technique [J]. AIAA Journal, 1983, 21(4): 485-486.
[4] Walsh M J.Riblets in viscous drag reduction in boundary layers[J]. Progress in Astronautics and Aeronautics, 1990, 123: 203-261.
[5] 胡海豹,宋保维,刘占一,等.基于湍流边界层时均速度分布的脊状表面减阻规律研究[J].航空动力学报,2009,24(5): 1041-1047.
HU Hai-bao, SONG Bao-wei, LIU Zhan-yi, et al. Research about the characteristic of drag reduction over riblets surface based on average velocity profile in the turbulent boundary layer [J]. Journal of Aerospace Power, 2009, 24 (5): 1041-1047. (in Chinese)
[6] Hu H B, Song B W, Liu G S, et al. A simulation study of the turbulent drag reduction mechanisms derived from shark skin [J]. Journal of China Ordnance, 2009,5( 3):168-174.
[7] 刘占一,宋保维,胡海豹,等.脊状表面减阻特性的风洞试验研究 [J].实验力学,2008, 23(5): 469-474.
LIU Zhan-yi, SONG Bao-wei, HU Hai-bao, et al. Experiment investigation on the drag-reduction characteristics above riblet surface in wind tunnel [J]. Journal of Experimental Mechanics, 2008, 23(5):469-474. (in Chinese)
[8] Anderson E J, MacGillivrary P S, DeMont M E. Scallop shells exhibit optimization of riblet dimensions for drag reduction [J]. Biological Bulletin, 1997,192(3): 341-344.
[9] 胡海豹,黄桥高,刘占一, 等. 脊状表面减阻机理的研究[J]. 摩擦学学报, 2010, 30(1):32-37.
HU Hai-bao, HUANG Qiao-gao, LIU Zhan-yi, et al. Dragreduction mechanism of riblet surface [J]. Journal of Tribology, 2010, 30(1):32-37. (in Chinese)
[10] Reif W E. Morphogenesis and function of the squamation in sharks [J]. Neues Jahrbuch fur Geologie and Palaentologie, 1982, 164:172-183.
[11] 范植坚, 王天诚. 电解加工技术及其研究方法[M]. 北京: 国防工业出版社, 2004: 95~112.
FAN Zhi-jian, WANG Tian-cheng. Technology andapplication of electrochemical machining [M]. Beijing: National Defense Industry Press, 2004: 95-112.(in Chinese)
[12] Bechert D W, Bruse M, Hage W, et al. Biological surface and their technological application—laboratory and flight experiments on drag reduction and separation control [M]. New York, US: AIAA, 1997:1-34.
[13] Feng B B, Chen D R, Wang J D, et al. Drag reducing and increasing mechanism on triangular riblet surface [J]. Transactions of Nanjing University of Aeronautics and Astronautics, 2014, 31(1):78-84.
[14] Raschi W, Elsom J. Comments on the structure and development of the drag reduction-type placoid scale [M]. Japan: The Ichthyological Society of Japan, 1986:408–424.
[15] Bechert D W, Bartenwerfer M, Hoppe G, et al. Drag reduction mechanisms derived from shark skin [C]∥The 15th ICAS Congress. London, England:AIAA, 1986.
[16] 王晋军, 李亚臣. 沟槽面三角翼减阻特性实验研究[J]. 空气动力学学报, 2001, 19(3): 283-287.
WANG Jin-jun, LI Ya-chen.Experimental studies on the drag reduction characteristics for flow over delta wings with riblets surfaces [J]. Acta Aerodynamica Sinica, 2001, 19(3): 283-287.(in Chinese)
[17] Bechert D W, Bruse M, Hage W. Experiment with three-dimensional riblets as an idealized model of shark skin [J]. Experiments in Fluids, 2000, 28(3):403-412.

[1]	田丰，苗龙，梁福文，宋家辉，何梓豪，武志文，王宁飞. 空心阴极羽流等离子体放电不稳定性二维仿真模型[J]. 兵工学报, 2024, 45(4): 1208-1218.
[2]	雷特, 武郁文, 徐高, 邱彦铭, 康朝辉, 翁春生. 基于大涡模拟方法的三维旋转爆轰流场结构研究[J]. 兵工学报, 2024, 45(1): 85-96.
[3]	王明环, 吕明, 何凯磊, 郑劲松, 许雪峰. 超声辅助微细电解加工间隙空化微射流对材料蚀除的影响[J]. 兵工学报, 2023, 44(8): 2368-2380.
[4]	刘喜燕, 袁绪龙, 罗凯, 鲁娜. 跨介质航行器出入水连续弹道试验与仿真[J]. 兵工学报, 2023, 44(5): 1225-1236.
[5]	张春，王宝寿. 水下航行体超声速射流与尾空泡耦合作用初期的流场特性[J]. 兵工学报, 2022, 43(7): 1685-1694.
[6]	周伯俊, 于传强，刘志浩，柯冰. 基于高压储能的特种车辆快速起竖技术与验证[J]. 兵工学报, 2022, 43(7): 1488-1497.
[7]	高月光，冯顺山，刘云辉，黄岐. 不同端盖厚度的圆柱形装药壳体破片初速分布[J]. 兵工学报, 2022, 43(7): 1527-1536.
[8]	孟豪龙，翁春生，武郁文，郑权，肖强，王放，白桥栋. 环形燃烧室中凹腔对C₂H₄/Air旋转爆轰流场影响的数值模拟[J]. 兵工学报, 2022, 43(5): 1063-1074.
[9]	李旭, 刘彦, 安丰江, 王虹富, 许迎亮. 行星式球磨颗粒流场分布与形貌变化规律[J]. 兵工学报, 2022, 43(4): 876-891.
[10]	聂春生，杨光，聂亮，周禹，赵良. 飞行器热解炭化材料烧蚀产物对等离子体流场的影响规律[J]. 兵工学报, 2022, 43(3): 513-523.
[11]	周柏航，陶如意，王浩，阮文俊. 带侵蚀燃烧效应的阶梯多根装药火箭发动机三维内流场特性[J]. 兵工学报, 2021, 42(8): 1604-1612.
[12]	王丹宇，南风强，廖昕，肖忠良，堵平，王彬彬. 考虑化学反应的大口径火炮炮口流场特性[J]. 兵工学报, 2021, 42(8): 1624-1630.
[13]	聂春生，袁野，周禹，黄建栋，陈轩，张青青. 纯碳/碳材料烧蚀对飞行器等离子体流场的影响[J]. 兵工学报, 2021, 42(2): 320-326.
[14]	游鹏，周克栋，赫雷，缪桓举. 含运动弹头的手枪膛口射流噪声场特性[J]. 兵工学报, 2021, 42(12): 2597-2605.
[15]	席运志，王宁飞，李军伟，张智慧. 基于旋转阀的固体火箭发动机燃烧室压强振荡特性[J]. 兵工学报, 2021, 42(1): 33-44.

脊状结构组合式轮片状阴极工作齿齿形优化设计

The Optimization of Assembled Turntable Working Teeth Cathode Profile with Riblet Surface

PDF

可视化

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 15

编辑推荐

Metrics

本文评价