基于混合润滑理论的航空作动器密封性能分析

欧阳小平; 薛志全; 彭超; 郭生荣; 周清和; 杨华勇

doi:10.13700/j.bh.1001-5965.2015.0387

基于混合润滑理论的航空作动器密封性能分析

doi: 10.13700/j.bh.1001-5965.2015.0387

1.
浙江大学流体动力与机电系统国家重点实验室, 杭州 310027
2. 中航工业金城南京机电液压工程研究中心, 南京 211106

基金项目: 国家自然科学基金(51275450,51221004);国家"973"计划(2014CB046403)

详细信息

作者简介:
欧阳小平男,硕士,副教授,硕士生导师。主要研究方向:飞机液压、电液控制以及外骨骼机器人。Tel.:0571-87951274 E-mail:ouyangxp@zju.edu.cn

通讯作者:
欧阳小平,Tel.:0571-87951274 E-mail:ouyangxp@zju.edu.cn

中图分类号: TH137.51
计量
- 文章访问数: 995
- HTML全文浏览量: 59
- PDF下载量: 481
- 被引次数: 0
出版历程
- 收稿日期: 2015-06-12
- 网络出版日期: 2016-02-20

Analysis on aircraft cylinder seal property based on mixed lubrication theory

1.
State Key Laboratory of Fluid Power & Mechatronic Systems, Zhejiang University, Hangzhou 310027, China
2. Nanjing Engineering Institute of Aircraft Systems, Jincheng, AVIC, Nanjing 211106, China

摘要

摘要: 针对航空作动器不同压力、温度以及作动速度的工作环境,以Trelleborg公司Turcon VL密封为代表,利用混合润滑理论对其性能进行分析,揭示机载工况对航空作动器密封性能的影响规律。建立了基于混合润滑理论的宏观与微观多场耦合模型,包括:考虑空化及流动因子的Reynolds方程油膜模型、Greenwood-Williamson(G-W)的微观接触模型以及Fourier的传热模型。通过有限体积法求解,分析不同压力下宏观接触压力、微观接触压力以及油膜压力分布特点。研究结果表明:随流体压力增大,泄漏量与摩擦力都近似线性增大;在25℃时无泄漏,而温度升高至135℃时产生少许泄漏;随作动速度增大,摩擦力减小但泄漏量增大。
- 航空作动器 /
- VL密封 /
- 混合润滑模型 /
- 多场耦合 /
- 有限体积法
Abstract: Aimed to investigate the influences of working conditions such as different pressures, temperatures and velocities on the performance of the seal of the aircraft cylinder, the Turcon VL seal from Trelleborg AB was analyzed based on the mixed lubrication theory. The macro and micro multi-field coupling model based on the mixed lubrication theory was built, which mainly includes fluid model with cavitation and fluid factors in Reynolds equation, micro contact model of Greenwood-Williamson(G-W) and heat transfer model of Fourier. By computing the model with finite volume method, the characteristics of macro contact pressure, micro contact pressure and oil pressure distribution under different fluid pressures were analyzed. The research results show that the seal leakage and friction increases nearly linearly with the fluid pressure increasing, the seal has no leakage at 25℃ but has some at 135℃, and the seal friction decreases but leakage increases with the cylinder velocity increasing.
- aircraft cylinder /
- VL seal /
- mixed lubrication model /
- multi-field coupling /
- finite volume method

HTML全文

参考文献(21)

[1]	王占林. 飞机高压液压能源系统[M].北京:北京航空航天大学出版社,2004:2-3. WANG Z L.The aircraft high pressure hydraulic energy system[M].Beijing:Beihang University Press,2004:2-3(in Chinese).
[2]	NIKAS G K. Eighty years of research on hydraulic reciprocating seals:Review of tribological studies and related topics since the 1930s[J].Journal of Engineering Tribology,2010,224(1):1-23.
[3]	NAU B S. An historical review of studies of polymeric seals in reciprocating hydraulic systems[J].Journal of Engineering Tribology,1999,213(3):215-226.
[4]	YANG B,SALANT R F.Elastohydrodynamic lubrication simulation of O-ring and U-cup hydraulic seals[J].Journal of Engineering Tribology,2011,225(7):603-610.
[5]	SALANT R F,MASER N,YANG B.Numerical model of a reciprocating hydraulic rod seal[J].Journal of Tribology,2007,129(1):577-583.
[6]	YANG B,SALANT R F.Numerical model of a reciprocating rod seal with a secondary lip[J].Tribology Transactions,2008,51(2):119-127.
[7]	YANG B,SALANT R F.Numerical model of a tandem reciprocating hydraulic seal[J].Journal of Tribology,2008,130(3):032201-1-032201-7.
[8]	YANG B,SALANT R F.Soft EHL simulations of U-cup and step hydraulic seals[J].Journal of Tribology,2009,131(2):021501-1-021501-10.
[9]	SCHMIDT T,ANDRE M,POLL G.A transient 2D-finite-element approach for the simulation of mixed lubrication effects of reciprocating hydraulic rod seals[J].Tribology International,2010,43(10):1775-1785.
[10]	ÖNGVN Y,ANDRÉ M,BARTEL D,et al.An axisymmetric hydrodynamic interface element for finite-element computations of mixed lubrication in rubber seals[J].Journal of Engineering Tribology,2008,222(3):471-481.
[11]	MVLLER H K,NAU B S.Fluid sealing technology principles and applications[M].New York:Marcel Dekker Inc.,1998:112-117.
[12]	TRELLEBORG. Airspace sealing systems[EB/OL].[2015-03-12].http://tss-static.com/remotemedia/media/globalformastercontent/downloadsautomaticlycreatedbyscript/catalogs/aerospace_gb_en.pdf.
[13]	ANSYS Inc. ANSYS elements reference[Z].ANSYS Release 15.0.2014.
[14]	TRELOAR L R G. The physics of rubber elasticity[M].New York:Oxford University Press,1975:65-74.
[15]	PAYVAR P,SALANT R F.A computational method for cavitation in a wavy mechanical seal[J].Journal of Tribology,1992,114(1):199-204.
[16]	PATIR N,CHENG H S.An average flow model for determining effects of three-dimensional roughness on partial hydrodynamic lubrication[J].Journal of Tribology,1978,100(1):12-17.
[17]	PATIR N,CHENG H S.Application of average flow model to lubrication between rough sliding surfaces[J].Journal of Tribology,1979,101(2):220-229.
[18]	GREENWOOD J A,WILLIAMSON J B P.Contact of nominally flat rough surfaces[J].Proceedings of the Royal Society A,1966,295(1442):300-319.
[19]	黄平. 润滑数值计算方法[M].北京:高等教育出版社,2012:137-140. HUANG P.The numerical calculation method of lubrication[M].Beijing:Higher Education Press,2012:137-140(in Chinese).
[20]	BHUSHAN B. Principles and applications of tribology[M].New York:Wiley,1999:407-408.
[21]	温诗铸,黄平.摩擦学原理[M].4版.北京:清华大学出版社,2012:10-11. WEN S Z,HUANG P.Principle of tribology[M].4th ed.Beijing:Tsinghua University Press,2012:10-11(in Chinese).