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微小流量旋转直驱伺服阀传控特性分析与优化

陆亮 徐寅鹏 李梦如 张小洁 凌扬洋 李鸿向

同济大学学报(自然科学版)2024,Vol.52Issue(5):805-814,10.
同济大学学报(自然科学版)2024,Vol.52Issue(5):805-814,10.DOI:10.11908/j.issn.0253-374x.22334

微小流量旋转直驱伺服阀传控特性分析与优化

Analysis and Optimization of Transmission and Control Characteristics of Micro-Flow Rotary Direct-Drive Servo Valve

陆亮 1徐寅鹏 2李梦如 2张小洁 3凌扬洋 3李鸿向3

作者信息

  • 1. 同济大学机械与能源工程学院,上海 201804||流体动力与机电系统国家重点实验室,浙江杭州 310007
  • 2. 同济大学机械与能源工程学院,上海 201804
  • 3. 江苏金陵智造研究院有限公司,江苏南京 210006
  • 折叠

摘要

Abstract

Aimed at the micro-flow servo control requirements of fuel metering system and thrust vector system of small aircraft such as un-manned aerial vehicle,tactical missile and regional civil aviation,the size constraint and design analysis of key structures such as eccentric ball pair transmission interface and non-full-circle throttle valve port of rotary direct-drive servo valve is conducted.The optimization analysis of important parameters such as throttle valve port width,ball pair eccentricity,and driving motor moment of inertia is performed,and the optimization interval of servo valve structure design is given.In addition,a double closed-loop control method for motor angle and current is proposed.The measured results of amplitude-frequency response are consistent with the theoretical analysis,and the high frequency response above 200 Hz meets the actual requirements.The double closed-loop control method greatly reduces the response overshoot of servo valve and improves the stability.

关键词

旋转直驱伺服阀/微小流量/传动与控制/建模分析/设计优化

Key words

rotary direct-drive servo valve/micro-flow/transmission and control/modeling analysis/design optimization

分类

航空航天

引用本文复制引用

陆亮,徐寅鹏,李梦如,张小洁,凌扬洋,李鸿向..微小流量旋转直驱伺服阀传控特性分析与优化[J].同济大学学报(自然科学版),2024,52(5):805-814,10.

基金项目

国家重点研发计划(2019YFB2005102) (2019YFB2005102)

国家自然科学基金(52075387) (52075387)

上海市自然科学基金(22ZR1464400) (22ZR1464400)

流体动力与机电系统国家重点实验室开放基金(GZKF-201907) (GZKF-201907)

同济大学学报(自然科学版)

OA北大核心CSTPCD

0253-374X

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