机械工程

偏转板伺服阀射流盘组件的压力特性预测与分析

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  • 1. 同济大学 机械与能源工程学院,上海 201804;2. 南京机电液压工程研究中心 航空机电系统综合航空科技重点实验室,江苏 南京 210061;3. 上海航天控制技术研究所 上海 201109

李双路 (1995-),男,博士生,主要从事偏转板伺服阀基础理论研究。E-mail: 1710765@ tongji. edu. cn

收稿日期: 2019-11-28

  修回日期: 2020-05-11

  网络出版日期: 2020-09-01

基金资助

国家自然科学基金资助项目 (51775383); 国家重点研发计划项目 (2018YFB2001100); 上海航天科技创新基金资助项目 (SAST2017093)

Pressure Characteristic Prediction and Analysis of Deflector Jet Servo Valve Jet-Pan Components

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  • 1. School of Mechanical Engineering,Tongji University,Shanghai 201804,China; 2. Aviation Key Laboratory of Science
    and Technology on Aero Electromechanical System Integration,Nanjing Mechatronic and Hydraulic Engineering Research Centre,Nanjing 210061,Jiangsu,China; 3. Shanghai Aerospace Control Technology Institute,Shanghai 201109,China
李双路 (1995-),男,博士生,主要从事偏转板伺服阀基础理论研究。E-mail: 1710765@ tongji. edu. cn

Received date: 2019-11-28

  Revised date: 2020-05-11

  Online published: 2020-09-01

Supported by

Supported by the National Natural Science Foundation of China (51775383),the National Key Research and Development Program of China (2018YFB2001100) and the Shanghai Aerospace Science Technology Innovation Foundation Project (SAST2017093)

摘要

针对偏转板伺服阀射流盘组件两腔恢复压力不对称和一致性差的问题,建立了考虑射流盘尺寸和形位误差时的流场仿真模型,采用多元线性回归分析方法研究了射流盘的形状因素与压力特性之间的关系; 通过神经网络算法实现了不同尺寸和形位误差组合下的射流盘组件两腔恢复压力的预测,并研究了导致两腔压差超差的形状因素分布情况。结果表明: 恢复压力的主要影响因素包括劈尖宽度、射流口宽度、射流盘厚度、接收腔圆角以及劈尖对称度; 两腔压差的主要影响因素为劈尖对称度、射流口垂直度、接收腔圆角以及内角对称度; 射流盘的两腔压差大小呈正态分布规律,压差超差主要是多个因素组合引起,但即使所有形状因素符合设计要求,也可能出现压差超差。实验结果与理论结果相符。

本文引用格式

李双路, 訚耀保, 刘敏鑫, 等 . 偏转板伺服阀射流盘组件的压力特性预测与分析[J]. 华南理工大学学报(自然科学版), 2020 , 48(9) : 71 -78 . DOI: 10.12141/j.issn.1000-565X.190867

Abstract

For the asymmetry and poor consistency of recovery pressures in the two receiving cavities of deflector jet servo valve,flow field simulation model considering the size and shape error of the jet-pan was established and the relationship between the shape factors of the jet-pan and the pressure characteristics was studied by using multi-ple linear regression analysis. The neural network algorithm was used to predict the recovery pressure of jet-pan components under different size and shape error combinations,and the shape factors distribution which cause the pressure difference excess was studied as well. Research shows that the main factors affecting the recovery pressure include the width of wedge,the width of jet orifice,the thickness of jet-pan,the round corners of receiving cavities and the symmetry of wedge. And the main factors of the pressure difference between the two cavities are the symme-try of the wedge,the verticality of the jet orifice,the symmetry of round corners and the inner angle of the receiving cavities. The pressure difference between the two cavities is in normal distribution. The pressure difference excess is caused by the combination of several factors,but even if all the shape factors meet the design requirements,the pressure difference excess may occur. Experimental results agree with the theoretical results.

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