Multi-Objective Optimization of a Novel Ribbed Honeycomb Heat Sink for an Electro-Hydrostatic Actuator

Author:

Li Yanpeng1234,Han Huijun23,Li Mingzhong23,Zhang Jinhu23,Xing Youwang23,Lei Sheng23,Yu Xiang23

Affiliation:

1. China Coal Research Institute, Beijing 100013, China

2. CCTEG Coal Mining Research Institute, Beiing 100013, China

3. Tiandi Technology Co., Ltd., Beijing 100013, China

4. School of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, China

Abstract

The electro-hydrostatic actuator (EHA) is a new type of power-by-wire (PBW) actuation system, which is utilized to realize a more electric aircraft. However, EHA suffers from serious thermal problems, due to its high integration and high power density. Therefore, a reasonable heat dissipation structure is an essential method for solving this problem. In this paper, a novel ribbed honeycomb heat sink (RHCS) developed by combining a ribbed heat sink (RHS) with a honeycomb heat sink (HCS) is proposed. Moreover, the optimization of heat sink parameters was achieved by using a multi-objective particle swarm optimization algorithm (MOPSO). Initially, the thermal resistance and mass models of the HCS were constructed, based on which the optimal structural parameters of the honeycomb cell were obtained. In addition, the thermal resistance model of RHCS was constructed using the response surface method, and parameters such as rib spacing, height and width were obtained based on MOPSO. Finally, the heat dissipation capability of RHCS was verified using both a simulation and experimental methods, and the results show that the heat dissipation capability of RHCS is about 15%∼20% higher than that of RHS and 7.4%∼10.3% higher than that of HCS. The configuration and design method of RHCS proposed in this paper provide a solution for the thermal design of EHA.

Funder

Science and Technology Innovation Fund of CCTEG Coal Mining Research Institute

Science and Technology Innovation Fund of Tiandi Technology Co., Ltd.

National Natural Science Foundation of China

Publisher

MDPI AG

Subject

Process Chemistry and Technology,Chemical Engineering (miscellaneous),Bioengineering

Reference31 articles.

1. Flight Control Actuation Technology for Next-Generation All-Electric Aircraft;Botten;Technol. Rev.-J.-Millenn.,2000

2. Vladimirov, S.V., and Forde, S. (2006, January 9–16). Demonstration program to design, manufacture and test an autonomous electro-hydrostatic actuator to gimbal large booster-class engines. Proceedings of the 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Sacramento, CA, USA.

3. A Novel Electro Hydrostatic Actuator System with Energy Recovery Module for More Electric Aircraft;Shang;IEEE Trans. Ind. Electron.,2020

4. Review on electro 731 hydrostatic actuator for flight control;Alle;Int. J. Fluid Power,2016

5. Bossche, D.V. (2006, January 3–8). The A380 Flight Control Electrohydrostatic Actuators, Achievements and Lessons Learnt. Proceedings of the 25th International Congress of the International Council of Aeronautical Sciences, Hamburg, Germany.

Cited by 1 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3