Load-Sensing Pump Design to Reduce Heat Generation of Electro-Hydrostatic Actuator Systems

被引:12
|
作者
Chao, Qun [1 ]
Zhang, Junhui [1 ]
Xu, Bing [1 ]
Shang, Yaoxing [2 ,3 ]
Jiao, Zongxia [2 ,3 ]
Li, Zhihui [2 ,3 ]
机构
[1] Zhejiang Univ, State Key Lab Fluid Power & Mechatron Syst, Hangzhou 310027, Zhejiang, Peoples R China
[2] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China
[3] Beihang Univ, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R China
基金
中国国家自然科学基金;
关键词
aircraft; electro-hydrostatic actuator (EHA); heat reduction; load-sensing pump; AXIAL PISTON PUMP; SWASH-PLATE; VARIABLE-DISPLACEMENT; PRESSURE CONTROL; PERFORMANCE; SIMULATION; SHAFT;
D O I
10.3390/en11092266
中图分类号
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号
0807 ; 0820 ;
摘要
The electro-hydrostatic actuator (EHA) with variable pump displacement is considered to be a promising alternative to the currently popular EHA with fixed pump displacement in terms of heat reduction. This paper presents a load-sensing pump for the EHA which requires no additional power source and can adjust its volumetric displacement automatically with load pressure. A load-sensing pump prototype was developed and experiments were carried out on a test rig for it under different operating conditions. In addition, an experimental campaign was performed on an EHA test bench with a load-sensing pump and a fixed displacement pump. The results show that the load-sensing pump can decrease its volumetric displacement automatically at high pressure and thus reduce the heat generation of EHA system effectively.
引用
收藏
页数:13
相关论文
共 50 条
  • [1] Design and Analysis of a Direct Load Sensing Electro-Hydrostatic Actuator
    Song Zengning
    Jiao Zongxia
    Shang Yaoxing
    Wu Shuai
    Hu Wunong
    PROCEEDINGS OF 2015 INTERNATIONAL CONFERENCE ON FLUID POWER AND MECHATRONICS - FPM 2015, 2015, : 624 - 627
  • [2] Variable load failure mechanism for high-speed load sensing electro-hydrostatic actuator pump of aircraft
    Cun SHI
    Shaoping WANG
    Xingjian WANG
    Yixin ZHANG
    Chinese Journal of Aeronautics , 2018, (05) : 949 - 964
  • [3] Variable load failure mechanism for high-speed load sensing electro-hydrostatic actuator pump of aircraft
    Shi, Cun
    Wang, Shaoping
    Wang, Xingjian
    Zhang, Yixin
    CHINESE JOURNAL OF AERONAUTICS, 2018, 31 (05) : 949 - 964
  • [4] Variable load failure mechanism for high-speed load sensing electro-hydrostatic actuator pump of aircraft
    Cun SHI
    Shaoping WANG
    Xingjian WANG
    Yixin ZHANG
    Chinese Journal of Aeronautics, 2018, 31 (05) : 949 - 964
  • [5] Research on Control of Active Optimal Load Sensing Electro-Hydrostatic Actuator
    Li Zhihui
    Shang Yaoxing
    Jiao Zongxia
    Wu Shuai
    Pan Qingxin
    2018 IEEE CSAA GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC), 2018,
  • [6] Viscous Pump for Highly Backdrivable Electro-Hydrostatic Actuator
    Kaminaga, Hiroshi
    Tanaka, Hirokazu
    Yasuda, Kazuki
    Nakamura, Yoshihiko
    2012 IEEE INTERNATIONAL CONFERENCE ON ROBOTICS AND AUTOMATION (ICRA), 2012, : 3751 - 3756
  • [7] Partial abrasion modeling and variable load characteristics analysis for high-speed load sensing electro-hydrostatic actuator pump of aircraft
    Shi, Cun
    Wang, Weiyu
    Wang, Shaoping
    Liu, Di
    Zhang, Siyuan
    ADVANCES IN MECHANICAL ENGINEERING, 2024, 16 (10)
  • [8] Active Fault-Tolerant Controller Design for Load Sensing Electro-Hydrostatic Actuator with Optimal Reference Model
    Shi Cun
    Wang Shaoping
    Wang Xingjian
    Wang Jun
    Tomovic, Milcta
    PROCEEDINGS OF THE 35TH CHINESE CONTROL CONFERENCE 2016, 2016, : 6437 - 6442
  • [9] Preliminary design and simulation of Electro-hydrostatic Actuator with Modelica
    Wu, Shuai
    Li, Chunfang
    Zhao, Xiangyu
    Jiao, Zongxia
    Yang, Tao
    2016 IEEE/CSAA INTERNATIONAL CONFERENCE ON AIRCRAFT UTILITY SYSTEMS (AUS), 2016, : 1138 - 1143
  • [10] Modeling and control of a novel electro-hydrostatic actuator with adaptive pump displacement
    Yan WANG
    Shengrong GUO
    Hongkang DONG
    Chinese Journal of Aeronautics, 2020, 33 (01) : 365 - 371