Key technologies and challenges of high⁃performance servo⁃motor⁃pumps

被引:0
作者
Lyu, Dingchong [1 ]
Zhao, Shoujun [2 ,3 ]
Zeng, Si [2 ,3 ]
Fu, Jian [1 ]
Hu, Xintong [1 ]
Liu, Huixiang [2 ]
Miao, Kefei [2 ,3 ]
Fu, Yongling [1 ]
机构
[1] School of Mechanical Engineering and Automation, Beihang University, Beijing
[2] Beijing Institute of Precision Mechatronics and Controls, Beijing
[3] Innovation Center of Control Actuation, Beijing
来源
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2024年 / 45卷 / 15期
关键词
dynamic characteris⁃ tics; electro-hydrostatic actuator; integrated design; power density; power-by-wire; servo-motor-pump;
D O I
10.7527/S1000-6893.2024.30225
中图分类号
学科分类号
摘要
Servo Motor Pumps(SMP)play a decisive role as central power and control elements for the performance limits in Electro-Hydrostatic Actuators (EHAs). Internationally renowned hydraulic companies such as Moog and Parker have introduced SMPs for aerospace and high value Industrial applications. In recent years,Chinese research in the field of high-performance SMPs has made some progress,but is still far from mature. This article provides a comprehensive overview of SMPs in terms of aerospace applications and also considers other fields such as robotics,marine and industrial applications. Based on the analyzed applications and developments,the five key performance characteristics such as high power-to-weight ratio,high dynamic range,long service life,low noise and intelligence are summarized,and the difficulties in theory and key technologies are discussed to make suggestions for high-performance EHAs and their key components. © 2024 Chinese Society of Astronautics. All rights reserved.
引用
收藏
相关论文
共 127 条
[1]  
ZHAO S J, HE J, ZHANG Y Q., The study on the dynamic capability of an electro-hydrostatic actuator to drive a large inertia load, 2016 IEEE International Conference on Aircraft Utility Systems, pp. 836-841, (2016)
[2]  
ZHAO J A, FU J, LI Y C, Et al., Flow characteristics of integrated motor-pump assembly with phosphate ester medium for aerospace electro-hydrostatic actuators[J], Chinese Journal of Aeronautics, 36, 9, pp. 392-407, (2023)
[3]  
BATISTA T A R., Modeling and analysis of an electrohydrostatic system using asymmetrical cylinder for industrial and mobile machinery, (2018)
[4]  
MARE J C., Aerospace actuators 2:Signal-by-wire and power-by-wire, pp. ix-xxvi, (2017)
[5]  
BRUZZESE C, TESSAROLO A, MAZZUCA T, Et al., A closer look to conventional hydraulic ship actuator systems and the convenience of shifting to (possibly) all-electric drives[C], 2013 IEEE Electric Ship Technologies Symposium, pp. 220-227, (2013)
[6]  
LIAO J, HE L, CHEN Z B, Et al., Overview of submarine steering system noise, Chinese Journal of Ship Research, 17, 5, pp. 74-84, (2022)
[7]  
KARANOVIC V, JOCANOVIC M, JOVANOVIC V., Review of development stages in the conceptual design of an electro hydrostatic actuator for robotics[J], Acta Poly-technica Hungarica, 11, 5, pp. 59-79, (2014)
[8]  
RAGHAVENDRA D R., Electrohydraulic servo systems [M], pp. 43-90, (2023)
[9]  
FU Y L, LI Z F, AN G C, Et al., State of the art and core techniques of edropump, Machine Tool & Hydraulics, 40, 1, pp. 143-149, (2012)
[10]  
CROWDER R, MAXWELL C., Simulation of a prototype electrically powered integrated actuator for civil aircraft, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 211, 6, pp. 381-394, (1997)