Investigation on Oil Supply Pressure Characteristics of Pressure Differential Valve

被引:0
作者
Wang, Yong [1 ,2 ]
Pi, Qin [2 ]
Chen, Jie [2 ]
Liu, Houlin [2 ]
Yang, Sijia [2 ]
机构
[1] Department of Precision Manufacturing Engineering, Suzhou Vocational Institute Of Industrial Technology, Suzhou
[2] Research Center of Fluid Machinery Engineering and Technology, Jiangsu University, Zhenjiang
关键词
aero-engine lubrication system; numerical simulation; pressure characteristics; pressure differential valve; structure parameters; test;
D O I
10.5293/IJFMS.2024.17.3.151
中图分类号
学科分类号
摘要
The unreasonable design of pressure differential valve may lead to unstable oil supply of aero-engine lubrication system. In order to find the optimization method of pressure differential valve structure, taking the oil supply subsystem of lubrication system as the research object, to study the effect of different pressure differential valve structure parameters on the oil supply pressure characteristics of aero-engine lubrication system by using a combination of numerical simulation and experimental verification. The results show that: (1) The reduction of spool damping hole diameter can improve the stability of oil supply pressure, but the dynamic performance becomes worse, and there is a large pressure peak; (2) Increase the diameter of the overflow hole can optimize the dynamic characteristics and stability of the oil supply pressure at the same time, to achieve stable oil supply; (3) Reduce the spring stiffness can weaken the oil supply pressure fluctuations and improve the stability of oil supply, but the pressure overshoot and rise time increase, resulting in poor dynamic performance. © 2024, Turbomachinery Society of Japan. All rights reserved.
引用
收藏
页码:151 / 163
页数:12
相关论文
共 41 条
  • [1] Li A., Zhang S., Shi H., Simulation study for lubrication oil supply system for an aero-engine, Journal of Shenyang University of Aeronautics and Astronautics, 29, 3, pp. 21-24, (2012)
  • [2] Tang S.N., Zhu Y., Yuan S.Q, Intelligent Fault Identification of Hydraulic Pump Using Deep Adaptive Normalized CNN and Synchrosqueezed Wavelet Transform, Reliability Engineering and System Safety, 224, 224, (2022)
  • [3] Li H.X., Li G.Q, Technology development thought on aero-engine power transmission system, Aeroengine, 39, 2, pp. 1-5, (2013)
  • [4] Tang S.N., Zhu Y., Yuan S.Q, Intelligent Fault Diagnosis of Hydraulic Piston Pump Based on Deep Learning and Bayesian Optimization, ISA Transactions, 129, (2022)
  • [5] Li Y., The Fault Diagnosis Analysis on a Model of the Air Engine Lubrication System, (2010)
  • [6] Zhu Y., Li G.P., Tang S.N., Acoustic Signal-based Fault Detection of Hydraulic Piston Pump using a Particle Swarm Optimization Enhancement CNN, Applied Acoustics, 192, (2022)
  • [7] Shen W., Discussion on aero engine mechanical system technology, Int. Comb. Eng & Par, 1, pp. 68-70, (2022)
  • [8] Su Y.Y., Mao F.R., Lu B., Analysis of flow simulation on an aero-engine lubrication system, Aeroengine, 42, pp. 70-74, (2016)
  • [9] Zhao H.D., Mao F.R., G J., Research and application on pressure differential valve of lubrication system, J. Propul. Technol, 43, pp. 44-48, (2017)
  • [10] Li L.L., Xie G.H., Oil system design of a certain turbo-jet engine, Aeroengine, 22, pp. 493-495, (2001)