Line-connected permanent magnet generator with adjustable excitation for variable-frequency AC aircraft power systems

被引:0
作者
Liu, Haoyu [1 ]
Jewell, Geraint W. [1 ]
Chen, Xiao [1 ]
机构
[1] Univ Sheffield, EEE Dept, Sheffield, S Yorkshire, England
来源
2023 IEEE INTERNATIONAL ELECTRIC MACHINES & DRIVES CONFERENCE, IEMDC | 2023年
关键词
line-connected generators; permanent magnet; adjustable excitation; variable-frequency; aircraft power system;
D O I
10.1109/IEMDC55163.2023.10239086
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Although permanent magnet synchronous machines are often a favored option for aerospace applications due to their high-power density and high efficiency, they almost always need to operate in conjunction with power electronics inverters in order to realize the desired power quality over a wide range of speeds and loads. The presence of these inverters leads to concerns of system complexity, reliability and overall system-level power density. This paper proposes a directly line-connected permanent magnet generator with adjustable field excitation for variable-frequency AC aircraft power systems. The voltage regulation at various load and speed conditions is achieved by controlling the space off between a pair of flux shorting endplates and the rotor core. The proposed topology is shown to be capable of meeting the speed regulation, load regulation and power quality requirements set in MIL-STD-704 for a representative power rating, by a combination of aspect ratio adjustment, winding short pitching, asymmetric rotor pole shaping, stator tooth shaping, and geometry parameter global optimization. Compared to the conventional permanent magnet generator in tandem with inverters, the proposed line-connected permanent magnet generator with adjustable excitation has the potential to eliminate the complexity and reliability concerns over power electronics inverters.
引用
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页数:7
相关论文
共 8 条
[1]  
Aircraft US Military, 1991, MIL-STD-704F
[2]  
[Anonymous], 2011, P 2011 INT C EL MACH, DOI DOI 10.1109/ICEMS.2011.6073754
[3]   Design, construction, and testing of an aero-engine starter-generator for the more-electric aircraft [J].
Balachandran, Ajith ;
Boden, Mark ;
Sun, Zhigang ;
Forrest, Stephen J. ;
Ede, Jason D. ;
Jewell, Geraint W. .
JOURNAL OF ENGINEERING-JOE, 2019, (17) :3474-3478
[4]   Aircraft power systems: Technology, state of the art, and future trends [J].
Emadi, A ;
Ehsani, M .
IEEE AEROSPACE AND ELECTRONIC SYSTEMS MAGAZINE, 2000, 15 (01) :28-32
[5]  
Khowja MR, 2018, IEEE TRANSP ELECT C, P570, DOI 10.1109/ITEC.2018.8450246
[6]  
MacMinn S. R., 1989, Proceedings of the IEEE 1989 National Aerospace and Electronics Conference NAECON 1989 (Cat. No.89CH2759-9), P1758, DOI 10.1109/NAECON.1989.40453
[7]  
Raminosoa T, 2011, IEEE ENER CONV, P2798, DOI 10.1109/ECCE.2011.6064145
[8]   More Electric Aircraft: Review, Challenges, and Opportunities for Commercial Transport Aircraft [J].
Sarlioglu, Bulent ;
Morris, Casey T. .
IEEE TRANSACTIONS ON TRANSPORTATION ELECTRIFICATION, 2015, 1 (01) :54-64