Performance optimization of grooved slippers for aero hydraulic pumps

被引:13
作者
Chen, Juan [1 ]
Ma, Jiming [2 ]
Li, Jia [3 ]
Fu, Yongling [1 ]
机构
[1] Beihang Univ, Dept Mech Engn & Automat, Beijing 100191, Peoples R China
[2] Beihang Univ, Sino French Engineer Sch, Beijing 100191, Peoples R China
[3] AVIC Xian Flight Automat Control Res Inst, Xian 710065, Peoples R China
基金
中国国家自然科学基金;
关键词
Arbitrary Lagrangian-Eulerian (ALE); Computational fluid dynamics (CFD); Grooved slipper; Hydraulic pump; Navier-Stokes equation; Performance analysis; AXIAL PISTON PUMPS; FINITE-ELEMENT-METHOD; LUBRICATION; MOTORS; BEARINGS; DESIGN;
D O I
10.1016/j.cja.2015.12.021
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A computational fluid dynamics (CFD) simulation method based on 3-D Navier-Stokes equation and Arbitrary Lagrangian-Eulerian (ALE) method is presented to analyze the grooved slipper performance of piston pump. The moving domain of grooved slipper is transformed into a fixed reference domain by the ALE method, which makes it convenient to take the effects of rotate speed, body force, temperature, and oil viscosity into account. A geometric model to express the complex structure, which covers the orifice of piston and slipper, vented groove and the oil film, is constructed. Corresponding to different oil film thicknesses calculated in light of hydrostatic equilibrium theory and boundary conditions, a set of simulations is conducted in COMSOL to analyze the pump characteristics and effects of geometry (groove width and radius, orifice size) on these characteristics. Furthermore, the mechanics and hydraulics analyses are employed to validate the CFD model, and there is an excellent agreement between simulation and analytical results. The simulation results show that the sealing land radius, orifice size and groove width all dramatically affect the slipper behavior, and an optimum tradeoff among these factors is conducive to optimizing the pump design. (C) 2015 The Authors. Production and hosting by Elsevier Ltd. on behalf of Chinese Society of Aeronautics and Astronautics.
引用
收藏
页码:814 / 823
页数:10
相关论文
共 38 条
[1]   A comparison between computational fluid dynamic and Reynolds approaches for simulating transient EHL line contacts [J].
Almqvist, T ;
Almqvist, A ;
Larsson, R .
TRIBOLOGY INTERNATIONAL, 2004, 37 (01) :61-69
[2]   Leakage and Groove Pressure of an Axial Piston Pump Slipper with Multiple Lands [J].
Bergada, J. M. ;
Haynes, J. M. ;
Watton, J. .
TRIBOLOGY TRANSACTIONS, 2008, 51 (04) :469-482
[3]   A complete analysis of axial piston pump leakage and output flow ripples [J].
Bergada, J. M. ;
Kumar, S. ;
Davies, D. Ll ;
Watton, J. .
APPLIED MATHEMATICAL MODELLING, 2012, 36 (04) :1731-1751
[4]  
Bergada J.M., 2002, P JFPS INT S FLUID P, V2002, P259, DOI [10.5739/isfp.2002.259, DOI 10.5739/ISFP.2002.259]
[5]  
Bergada J.M., 2002, SM INT M ECHANICAL E, P69
[6]  
Bergada JM, 2008, J DYN SYST MEAS CONT, V130, P141
[7]  
Boinghoff O., 1977, VDI-FORSCHUNGSH, P1
[8]   CFD analysis of a low friction pocketed pad bearing [J].
Braidic-Mitidieri, P ;
Gosman, AD ;
Ioannides, E ;
Spikes, HA .
JOURNAL OF TRIBOLOGY-TRANSACTIONS OF THE ASME, 2005, 127 (04) :803-812
[9]   CBS versus GLS stabilization of the incompressible Navier-Stokes equations and the role of the time step as stabilization parameter [J].
Codina, R ;
Zienkiewicz, OC .
COMMUNICATIONS IN NUMERICAL METHODS IN ENGINEERING, 2002, 18 (02) :99-112
[10]  
Deeken M., 2003, O+ P Olhydraulik und Pneumatik, V47, P11