Review of distributed hybrid electric propulsion aircraft technology

被引：0
|
作者：
Zhu B. [1 ]
Yang X. [1 ]
Zong J. [1 ]
Deng X. [1 ]
机构：
[1] College of Aerospace Science and Engineering, National University of Defense Technology, Changsha
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2022年 / 43卷 / 07期
基金：
中国国家自然科学基金;
关键词：
distributed hybrid electric propulsion system; driven by historical big data; electric aviation; energy management; principle prototype designing;
D O I：
10.7527/S1000-6893.2021.25556
中图分类号：
学科分类号：
摘要：
Distributed hybrid electric propulsion system has great potential and advantage in development of general electric aviation. By the optimization of secondary power system, hybrid electric technology can not only heighten the utilization efficiency of energy, but also satisfied the distributed arrangement of power system for higher propulsive efficiency. The paper firstly summarized the current major types of electric aircraft, reviewed the history background of distributed electric propulsion aircraft. Then, the research status of distributed hybrid electric propulsion aircraft technology is summarized, this part mainly discussed the distributed layout technology of propulsion system, type-selection design of hybrid electric propulsion system, modeling and energy management of hybrid electric propulsion system, and so on. The key technologies of distributed hybrid electric propulsion at home and abroad are discussed fully. Eventually, combined with the research of the team, the difficult point problems and solutions of distributed hybrid electric propulsion aircraft are discussed in detail, including dynamic management strategy of energy based on complex system optimization control, optimal energy distribution prediction model driven by historical big data, and principle prototype designing of distributed hybrid electric propulsion system. The main content of this paper clarify the design thoughts and analysis method for distributed hybrid electric propulsion system and energy arrangement, which can provide references for the research of electric propulsion aircraft technology. © 2022 AAAS Press of Chinese Society of Aeronautics and Astronautics. All rights reserved.
引用
收藏
相关论文
共 38 条
  • [1] FRIEDRICH C, ROBERTSON P A., Design of hybrid-electric propulsion systems for light aircraft, 14th AIAA Aviation Technology, Integration, and Operations Conference, (2014)
  • [2] OELBERG E., A hybrid optimal control approach to maximum endurance of aircraft, pp. 1-28, (2018)
  • [3] SHI W X, LIU P Z, WANG J H, Et al., Calculate the performance of multi-rotor UAV [C], The 12th National Conference on Signal and Intelligent Information Processing and Application, pp. 56-60, (2018)
  • [4] LI Y P., Conceptual design for solar/hydrogen hybrid powered small-scale UAV, pp. 1-21, (2014)
  • [5] FREDERICKS W J, MCSWAIN R G, BEATON B F, Et al., Greased lightning (GL-10) flight testing campaign: NASA/TM-2017-219643, (2017)
  • [6] RIGHI H., Hybrid electric aircraft, pp. 1-21, (2016)
  • [7] SAEED A S, YOUNES A B, ISLAM S, Et al., A review on the platform design, dynamic modeling and control of hybrid UAVs, 2015 International Conference on Unmanned Aircraft Systems (ICUAS), pp. 806-815, (2015)
  • [8] FINGER D F, BRAUN C, BIL C., A review of configuration design for distributed propulsion transitioning VTOL aircraft, 2017 ASIA-Pacific International Symposium on Aerospace Technology, pp. 1-15, (2017)
  • [9] SILVAS E, HOFMAN T, MURGOVSKI N, Et al., Review of optimization strategies for system-level design in hybrid electric vehicles [J], IEEE Transactions on Vehicular Technology, 66, 1, pp. 57-70, (2017)
  • [10] WANG Y Y., Overview of global electric aircraft develop-ment
1234