Full Text:   <1120>

Summary:  <356>

CLC number: TH137.51

On-line Access: 2016-03-07

Received: 2015-10-26

Revision Accepted: 2016-01-18

Crosschecked: 2016-02-22

Cited: 1

Clicked: 1534

Citations:  Bibtex RefMan EndNote GB/T7714

 ORCID:

Xiao-ping Ouyang

http://orcid.org/0000-0002-2090- 7123

Xu Fang

http://orcid.org/0000-0001-7756-4371

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Journal of Zhejiang University SCIENCE A 2016 Vol.17 No.3 P.202-214

10.1631/jzus.A1500286


An investigation into the swash plate vibration and pressure pulsation of piston pumps based on full fluid-structure interactions


Author(s):  Xiao-ping Ouyang, Xu Fang, Hua-yong Yang

Affiliation(s):  The State Key Laboratory of Fluid Power and Mechatronic Systems, Zhejiang University, Hangzhou 310027, China

Corresponding email(s):   ouyangxp@zju.edu.cn

Key Words:  Vibration, Pulsation, Swash plate, Aircraft, Piston pump, Fluid-structure interaction (FSI)


Xiao-ping Ouyang, Xu Fang, Hua-yong Yang. An investigation into the swash plate vibration and pressure pulsation of piston pumps based on full fluid-structure interactions[J]. Journal of Zhejiang University Science A, 2016, 17(3): 202-214.

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Abstract: 
In this paper, dynamic analyses of the swash plate vibration and pressure pulsation of an aircraft piston pump based on fluid-structure interactions (FSIs) are presented. Models of the swash plate piston pumps with three FSIs (named full FSIs and non FSI) are given. The simulation results of the discharge pressures at different rotation speeds in the synthesized pump model and experiments show good agreement. The numerical simulation results of the forces on the swash plate and the flow rate of the outlet chamber are presented and compared. The results of the two models show that the discharge pressure pulsation mostly depends on the kinematic relations of the piston slipper-shoe units (FSI-1), and is almost isolated from the swash plate vibration. The full FSIs simulation shows that the swash plate vibration is strongly influenced by the pressure pulsation through the control actuator mechanism (FSI-2) and the control valve mechanism (FSI-3), but the non FSI model does not show the same result. The full FSIs model is much more accurate in predicting the vibration of the swash plate and the pulsation of the discharge pressure than the non FSI model.

This paper models the full order dynamics of the swashplate type pump, used in aerospace applications. The contribution of the paper appears to be in the fact that a reduced order model (non-FSI) is compared to a full order model (full-FSI) and it is shown that the full order model compares more favorably with the experimental results in which various vibration characteristics have been measured. The message that I take from this paper is that, when seeking to understand the vibration characteristics of the machine it is important to consider the higher-order dynamics.

基于流构全耦合模型的柱塞泵斜盘振动和压力脉动的研究

目的:航空柱塞泵是飞机液压系统的核心元件,具有高压高转速的特点,其压力脉动是飞机液压系统振动的主要激励源,对飞机液压系统的安全性和可靠性具有重要影响。本文首次全面分析了压力脉动和斜盘振动之间的关系,对降低柱塞泵的压力脉动、提高其可靠性具有重要理论意义。
创新点:1. 将柱塞泵压力脉动和斜盘振动相结合,综合分析两者相互作用关系;2. 综合分析柱塞、斜盘控制阀、斜盘控制柱塞三者间的作用关系,建立全耦合模型。通过仿真分析和实验验证,指出普通模型的局限性以及全耦合模型在研究斜盘振动与压力脉动的真实内在关系的可靠性。
方法:1. 通过仿真和试验对比,分析全耦合模型和普通模型在压力脉动仿真结果上的差别及原因;2. 通过对比分析,确定全耦合模型在斜盘振动仿真方面具有的较高精度;3. 通过柱塞泵高压腔流量仿真结果,讨论柱塞泵压力脉动成因以及与斜盘的振动关系;4. 通过斜盘力矩仿真分析讨论斜盘振动成因以及与压力脉动的关系;5. 通过分析压力脉动、斜盘振动和转速三者间的关系,探讨减轻斜盘振动与减小压力脉动的有效途径。
结论: 1. 全耦合模型的精确度比普通模型高,能较好地预测斜盘振动和压力脉动状态。 2. 斜盘振动的基频部分主要取决于压力脉动的动态特性,同时还受控制阀机构(FSI-3)和变量柱塞机构(FSI-2)的动态特性影响。压力脉动主要由柱塞泵的柱塞运动关系(FSI-1)决定,不受斜盘高频振动影响。

关键词:振动;脉动;斜盘;航空;柱塞泵;流构耦合

Darkslateblue:Affiliate; Royal Blue:Author; Turquoise:Article

Reference

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