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柱塞式能量回收马达配流副锥度角的分析与试验
引用本文:李少年, 梁涛, 包尚令, 王煜, 周致元, 李曦. 柱塞式能量回收马达配流副锥度角的分析与试验[J]. 农业工程学报, 2022, 38(20): 20-29. DOI: 10.11975/j.issn.1002-6819.2022.20.003
作者姓名:李少年  梁涛  包尚令  王煜  周致元  李曦
作者单位:1.兰州理工大学能源与动力工程学院,兰州 730050;2.燕山大学机械工程学院,秦皇岛 066099
基金项目:国家自然科学基金资助项目(52165006)
摘    要:柱塞式能量回收马达是将液压马达与发电机一体化的新一代液压能量回收装置,缸体-配流轴组成的配流副是其关键摩擦副之一,配流副配合面锥度角的选择对马达的配流、承载和摩擦磨损特性有重要影响。该研究采用理论分析、数值模拟和试验测试的方法,探讨柱塞式能量回收马达配流副锥度角的最优值选择。首先根据配流副结构与尺寸,明确锥度角范围,然后以36°、39°、42°和45°共4个配流副锥度角为对象。分别从流场仿真、弱流固耦合和摩擦磨损试验3个方面,评价各锥度角配流副的柱塞腔油液压力与压力脉动、配流副部件应力与变形、配流副摩擦磨损等性能。结果发现配流副锥度角为42°和45°时,位于配流副上死点的柱塞腔内油液压力和压力波动较小,压力分别为4.66、4.62 MPa、压力波动幅度分别为3.307和3.246 MPa;在柱塞腔与高压油孔接通阶段,柱塞腔油液压力波动幅度分别为0.324、0.322 MPa;两种锥度角下的配流轴最大等效应力皆远小于其屈服强度;锥度角为42°缸体的最大等效应力占屈服强度比例较45°锥度角大0.74个百分点,最大变形量大0.251 μm;两种锥度角的配流副没有强度失效的风险,虽然有微量弹性变形,但对配流副的正常工作影响极小。相较于45°锥度角,42°锥度角摩擦副的平均摩擦系数小0.012,且波动小、稳定性好;上、下试件的磨损率分别小1.966×10-6和7.601×10-6 mm3/(N·mm)。所以42°锥度角有利于能量回收马达配流副的稳定工作及高效运转。研究结果可为柱塞式能量回收马达的设计提供参考。

关 键 词:马达  流场  仿真  应力  变形  配流副  锥度角  摩擦磨损
收稿时间:2022-07-27
修稿时间:2022-09-27

Analysis and tests of the taper angle of flow distribution pair in a piston type energy recovery motor
Li Shaonian, Liang Tao, Bao Shangling, Wang Yu, Zhou Zhiyuan, Li Xi. Analysis and tests of the taper angle of flow distribution pair in a piston type energy recovery motor[J]. Transactions of the Chinese Society of Agricultural Engineering (Transactions of the CSAE), 2022, 38(20): 20-29. DOI: 10.11975/j.issn.1002-6819.2022.20.003
Authors:Li Shaonian  Liang Tao  Bao Shangling  Wang Yu  Zhou Zhiyuan  Li Xi
Affiliation:1.College of Energy and Power Engineering, Lanzhou University of Technology, Lanzhou 730050, China;2.School of Mechanical Engineering, Yanshan University, Qinhuangdao 066099, China
Abstract:Abstract: A piston-type energy recovery motor is integrated the hydraulic motor and generator into a new generation of hydraulic energy recovery device. Among them, the flow distribution (friction) pair is composed of the cylinder block and flow distribution shaft. The taper angle of the friction surface on the flow distribution pair can pose an important impact on the oil flow distribution, load-bearing, friction and wear characteristics of the motor. In this study, an optimal combination of the taper angle was explored using the theoretical analysis, numerical simulation, and experimental test. Firstly, the available range of a taper angle was determined, according to the structure and size of the flow distribution pair in the motor. Four taper angles of 36°, 39°, 42°, and 45°were then selected as the research objects. Secondly, the fluid domain models were established to grid the four taper distribution pairs. The pressure contours and velocity vector diagrams were obtained for the four taper angles, in order to analyze the oil pressure fluctuation in the piston chamber and the leakage in the oil film. The solid domain grid models of distribution pairs were achieved at the taper angles of 42°and 45°and then to evaluate the stress and deformation of the cylinder block and the flow distribution shaft. Finally, the friction test pieces were made according to the motion and friction surface between the cylinder and the flow distribution shaft for the friction test. Specifically, the materials of the upper and lower test pieces were matched with those of the cylinder block and flow distribution shaft. The friction coefficient and wear amount of pairs were obtained at the taper angles of 42°and 45°during friction and wear experiments. The result showed that the oil pressures were 4.66 and 4.62 MPa in the piston chamber located in the high-pressure dead point at the taper angles of 42°and 45°, respectively, whereas, the amplitudes of pressure fluctuation were 3.307 and 3.246 MPa, respectively. Furthermore, the amplitudes of oil pressure fluctuation in the piston chamber were 0.324 and 0.322 MPa, respectively, in the process of connection between the piston chamber and the high pressure oil hole. There were the smaller amplitudes in the three-group data among the four taper angles. As such, the higher volume efficiency of the motor was achieved in the smaller leakage of the flow distribution pair, where the oil was transited smoothly at the taper angles of 42°and 45°in the piston chamber. The maximum equivalent stress of the flow distribution shaft was much less than the yield strength at the taper angle of 42°and 45°. There was 0.74 percentage points larger proportion of the maximum equivalent stress to the yield strength of cylinder block at the taper angle of 42°, compared with the taper angle of 45°. The maximum deformation of cylinder block was 0.251 μm. There was no failure risk of strength invalidation for the components of flow distribution pair at the two taper angles. Only a slightly impact was observed on the normal operation of the flow distribution pair, although the slight elastic deformation existed in this case. The average friction coefficient was less than 0.012 at the taper angle of 42°, indicating the small fluctuation and excellent stability. More importantly, the wear rates of the upper and lower pieces were 1.966×10-6 and 7.601×10-6 mm3/(N·mm) less at the taper angle of 42°than those of 45°, respectively. Therefore, the taper angle of 42° was conducive to the stable and efficient operation of the energy recovery motor. The finding can provide a strong reference to design the flow distribution pair of piston-type energy recovery motor.
Keywords:motors   flow field   simulation   stresses   deformation   flow distribution pair   taper angle   friction and wear
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