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Control Analysis of Propfan Engine Based on Dual Redundancy Electro-hydrostatic Actuator

  • Beihang University
  • Aero Engine Corporation of China

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

With the advantages of high fault tolerance, high reliability, high dynamic response and high power-to-weight ratio, the propfan engine is one of the most promising aircraft propulsion systems. In this paper, the model and control method of controlling the thrust of the propfan engine by controlling the blade pitch angle through the dual redundant electro-hydrostatic actuator (EHA) are constructed. The variable pitch propfan engine model is constructed by physical mathematical analysis, interpolation fitting and so on. The thrust control of variable pitch engine by dual redundancy EHA is completed by two-phase current control, fuzzy control and other control methods. The reliability of the constructed model and the better response characteristics of the design control method are verified by comparing the simulation experiment with the public data set. This paper provides a reference for thrust control of variable pitch propfan engine.

源语言英语
主期刊名Proceedings of the 18th IEEE Conference on Industrial Electronics and Applications, ICIEA 2023
编辑Wenjian Cai, Guilin Yang, Jun Qiu, Tingting Gao, Lijun Jiang, Tianjiang Zheng, Xinli Wang
出版商Institute of Electrical and Electronics Engineers Inc.
545-550
页数6
ISBN(电子版)9798350312201
DOI
出版状态已出版 - 2023
活动18th IEEE Conference on Industrial Electronics and Applications, ICIEA 2023 - Ningbo, 中国
期限: 18 8月 202322 8月 2023

出版系列

姓名Proceedings of the 18th IEEE Conference on Industrial Electronics and Applications, ICIEA 2023

会议

会议18th IEEE Conference on Industrial Electronics and Applications, ICIEA 2023
国家/地区中国
Ningbo
时期18/08/2322/08/23

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