Control of Three-Source High Voltage Power Network for More Electric Aircraft

被引:0
|
作者
Alnajjar, Mohammed [1 ]
Gerling, Dieter [1 ]
机构
[1] Univ Bundeswehr Munchen, Munich, Germany
关键词
Three-source power network; Two-Generator Engine; High voltage (HV) battery; Voltage stability;
D O I
暂无
中图分类号
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号
0807 ; 0820 ;
摘要
This paper proposes a simulation model of the control strategy for the high voltage power network with three power sources in the future aircraft. These power sources include two generators coupled to the aircraft turbine engine and a high voltage (HV) battery. The two generators together with the battery are delivering the power in parallel to a 270VDC dynamic load. The generators are two six-phase externally excited synchronous machines (EESM) operating in the generation mode. One of these machines is also used as a starter generator (SG). A voltage source inverter (VSI) is utilized to start the engine and to obtain the DC power when the machine is operated as a generator. The second machine is operated only as a generator (G) and the output AC voltage of this machine is passively rectified. The generators and the battery are delivering a maximum power of 160kW to the load. A battery model with a DC/DC converter is used as a third power source and as a load. The operation of the parallel connected sources is analyzed in selected fault conditions.
引用
收藏
页码:232 / 237
页数:6
相关论文
共 50 条
  • [1] Current Sharing in the High Voltage DC Parallel Electric Power System for the More Electric Aircraft
    Xu, Yanwu
    Zhang, Zhuoran
    Li, Jincai
    Yan, Yangguang
    2016 INTERNATIONAL CONFERENCE ON ELECTRICAL SYSTEMS FOR AIRCRAFT, RAILWAY, SHIP PROPULSION AND ROAD VEHICLES & INTERNATIONAL TRANSPORTATION ELECTRIFICATION CONFERENCE (ESARS-ITEC), 2016,
  • [2] Architecture Analysis and Optimization of High Voltage DC Parallel Electric Power System for More Electric Aircraft
    Xu, Yanwu
    Zhang, Zhuoran
    Li, Jincai
    Yan, Yangguang
    2016 IEEE/CSAA INTERNATIONAL CONFERENCE ON AIRCRAFT UTILITY SYSTEMS (AUS), 2016, : 244 - 249
  • [3] Electrical Power Source Model on Board of a More Electric Aircraft
    Eduard-Ionut, Ureche
    2014 INTERNATIONAL CONFERENCE ON APPLIED AND THEORETICAL ELECTRICITY (ICATE), 2014,
  • [4] Variable DC Bus Voltage Control Scheme for the More Electric Aircraft Power Generation System
    Yeoh, Seang Shen
    Rashed, Mohamed
    Bozhko, Serhiy
    Sanders, Mike
    2018 IEEE INTERNATIONAL CONFERENCE ON ELECTRICAL SYSTEMS FOR AIRCRAFT, RAILWAY, SHIP PROPULSION AND ROAD VEHICLES & INTERNATIONAL TRANSPORTATION ELECTRIFICATION CONFERENCE (ESARS-ITEC), 2018,
  • [5] High temperature power electronics for the more electric aircraft
    Palethorpe, B.
    Trainer, D.
    Industrial Diamond Review, 2007, 67 (02): : 19 - 22
  • [6] Regenerative Electric Power for More Electric Aircraft
    Deng, Yuhang
    Foo, Simon Y.
    Bhattacharya, Indranil
    IEEE SOUTHEASTCON 2014, 2014,
  • [7] Control Design and Voltage Stability Analysis of a Droop-Controlled Electrical Power System for More Electric Aircraft
    Gao, Fei
    Bozhko, Serhiy
    Costabeber, Alessandro
    Asher, Greg
    Wheeler, Pat
    IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 2017, 64 (12) : 9271 - 9281
  • [8] Impact of Converters Interactions on Control Design in a Power Electronics Dense Network: Application to More Electric Aircraft
    Czerniewski, Blazej
    Formentini, Andrea
    Dewar, David
    Zanchetta, Pericle
    Schanen, Jean-Luc
    2019 21ST EUROPEAN CONFERENCE ON POWER ELECTRONICS AND APPLICATIONS (EPE '19 ECCE EUROPE), 2019,
  • [9] A 50-kW High-Frequency and High-Efficiency SiC Voltage Source Inverter for More Electric Aircraft
    Yin, Shan
    Tseng, King Jet
    Simanjorang, Rejeki
    Liu, Yong
    Pou, Josep
    IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 2017, 64 (11) : 9124 - 9134
  • [10] A High Power Density Three Phase AC-DC Converter for More Electric Aircraft (MEA)
    Singh, Amit K.
    Das, Pritam
    Panda, S. K.
    2015 9TH INTERNATIONAL CONFERENCE ON POWER ELECTRONICS AND ECCE ASIA (ICPE-ECCE ASIA), 2015, : 1362 - 1367