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

作　　者：陆亮[1,2] 徐寅鹏 李梦如 张小洁[3] 凌扬洋 李鸿向 LU Liang;XU Yinpeng;LI Mengru;ZHANG Xiaojie;LING Yangyang;LI Hongxiang(School of Mechanical Engineering,Tongji University,Shanghai 201804,China;State Key Laboratory of Fluid Power and Mechatronic Systems,Hangzhou 310007,China;Jiangsu Jinling Intelligent Manufacturing Research Institute Co.,Ltd.,Nanjing 210006,China)

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

出　　处：《同济大学学报（自然科学版）》2024年第5期805-814,共10页Journal of Tongji University:Natural Science

基　　金：国家重点研发计划(2019YFB2005102);国家自然科学基金(52075387);上海市自然科学基金(22ZR1464400);流体动力与机电系统国家重点实验室开放基金(GZKF-201907)。

摘　　要：针对无人机、战术弹、支线民航等小型飞行器航空发动机燃油计量系统与推力矢量系统微小流量的伺服控制需求,就旋转直驱伺服阀偏心球副传动接口与非全周节流阀口等关键结构进行了尺寸约束设计分析,并就节流阀口宽度、球副偏心距以及驱动电机转动惯量等重要参数进行了优化分析,给出了伺服阀结构设计的优化区间。在此基础上,研究提出了电机转角与电流双闭环控制方法,幅频响应实测结果与理论分析较为一致,200 Hz以上高频响应满足实际需求,且双闭环控制方法大幅降低了伺服阀响应超调并提升了稳定性。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-fullcircle 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 closedloop 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 

分 类 号：V249.1[航空宇航科学与技术—飞行器设计] TH137.5[机械工程—机械制造及自动化]