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Dynamic thermal coupling modeling and analysis of wet electro-hydrostatic actuator
作者姓名:Zongxia JIAO  Yanpeng LI  Tian YU  Chaofan JIANG  Ligang HUANG  Yaoxing SHANG
作者单位:1. School of Automation Science and Electrical Engineering, Beihang University;2. Science and Technology on Aircraft Control Laboratory, Beihang University;3. Research Institute for Frontier Science, Beihang University;4. Ningbo Institute of Technology, Beihang University
基金项目:co-supported by the National Natural Science Foundation of China (No. 51890882);;National Key Research and Development Program of China (No. 2018YFB2000702);
摘    要:The electro-hydrostatic actuator(EHA) used in more electric aircraft(MEA) has been extensively studied due to its advantages of high reliability and high integration. However, this high integration results in a small heat dissipation area, leading to high-temperature problems. Generally,to reduce the temperature, a wet cooling method of using the pump leakage oil to cool the motor is adopted, which can also increase the difficulty of accurately predicting the system temperature in the early desi...

收稿时间:6 January 2021

Dynamic thermal coupling modeling and analysis of wet electro-hydrostatic actuator
Zongxia JIAO,Yanpeng LI,Tian YU,Chaofan JIANG,Ligang HUANG,Yaoxing SHANG.Dynamic thermal coupling modeling and analysis of wet electro-hydrostatic actuator[J].Chinese Journal of Aeronautics,2022,35(6):298-311.
Institution:1. School of Automation Science and Electrical Engineering, Beihang University, Beijing 100083, China;2. Science and Technology on Aircraft Control Laboratory, Beihang University, Beijing 100083, China;3. Research Institute for Frontier Science, Beihang University, 100083 Beijing, China;4. Ningbo Institute of Technology, Beihang University, Ningbo 315800, China
Abstract:The electro-hydrostatic actuator (EHA) used in more electric aircraft (MEA) has been extensively studied due to its advantages of high reliability and high integration. However, this high integration results in a small heat dissipation area, leading to high-temperature problems. Generally, to reduce the temperature, a wet cooling method of using the pump leakage oil to cool the motor is adopted, which can also increase the difficulty of accurately predicting the system temperature in the early design stage. To solve this problem, a dynamic coupling thermal model of a wet EHA is proposed in this paper. In particular, the leakage oil of the pump is used as a coupling item between the electrical system and the hydraulic system. Then, an improved T-equivalent block model is proposed to address the uneven distribution of axial oil temperature inside the motor, and the control node method is applied to hydraulic system thermal modeling. Meanwhile, a dynamic coupling thermal model is developed that enables a dynamic evaluation of the wet EHA temperature. Then, experimental prototypes of wet motor and wet EHA are developed, while the temperature response of the wet motor at different rotation speeds and different loads and the temperature response of the wet EHA at no-load condition were verified experimentally at room temperature, respectively. The maximum temperature difference between the experimental and theoretical results of the wet motor as well as the experimental and theoretical results of the wet EHA is less than 8 °C. These test results indicate that the dynamic coupling thermal model is valid and demonstrate that the thermal coupling modeling method proposed in this paper can provide a basis for the detailed thermal design of EHA.
Keywords:Electro-hydrostatic actuator  Hydraulic  More electric aircraft  Thermal mode  Wet motor
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