Electrical Characterization and Modeling of High Frequency Arcs for Higher Voltage Aerospace Systems

被引:6
作者
Alabani, Abir [1 ]
Ranjan, Prem [1 ]
Jiang, Jun [2 ]
Chen, Lujia [1 ]
Cotton, Ian [1 ]
Peesapati, Vidyadhar [1 ]
机构
[1] Univ Manchester, Dept Elect & Elect Engn, Manchester M13 9PL, England
[2] Nanjing Univ Aeronaut & Astronaut, Dept Elect & Elect Engn, Nanjing 211106, Jiangsu, Peoples R China
关键词
Aircraft and decarbonization; arc discharges; arc flash; arc model; high frequency; high-voltage techniques; AIRCRAFT; FAULT; CHALLENGES;
D O I
10.1109/TTE.2023.3244776
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
Arcing in future high-voltage aerospace systems could occur more frequently and cause irreversible damage to electrical components and system structure, and increase the risk of fire. While arcs seen in low-voltage aerospace systems tend to be long-duration and low-energy events, higher-power but short-duration arcs may occur in high-voltage aerospace systems if they are readily detectable by system protection. This article investigates the characteristics of high current arc faults generated at the ac frequencies expected in future rotating machines used for higher voltage aerospace systems. As such, arcs with a peak current up to 4.6 kA are generated at frequencies in the range of 0.5-2 kHz using an underdamped RLC circuit, under pressures of 0.2-1 bar absolute. High-frequency arcs exhibit a similar characteristic to lower-frequency arcs. A reduction in pressure results in lower arc voltage and arc power. Arcing tests at atmospheric pressure may therefore represent a worst-case scenario and the development of a low-pressure test environment may not be necessary. A black box model is developed to provide good agreement with experimental arc voltage waveforms for different parameters investigated in this study. This is a generalized modeling approach to estimate high-frequency high-voltage arcing characteristics without recourse to experiment.
引用
收藏
页码:4716 / 4725
页数:10
相关论文
共 27 条
[1]   Arc tracking energy balance for copper and aluminum aeronautic cables [J].
Andre, T. ;
Valensi, F. ;
Teulet, P. ;
Cressault, Y. ;
Zink, T. ;
Causse, R. .
14TH HIGH-TECH PLASMA PROCESSES CONFERENCE (HTPP 14), 2017, 825
[2]  
[Anonymous], 2019, European Aviation Environmental Report
[3]  
[Anonymous], 2021, Aircraft Electrical Voltage Level Definitions AIR7502,
[4]  
[Anonymous], 2018, INSIGHT_07-Electrical Power Systems
[5]  
Belijar G., 2017, P SAINT EX TOUL FRAN, P1
[6]   Insulation Materials and Systems for More- and All-Electric Aircraft: A Review Identifying Challenges and Future Research Needs [J].
Borghei, Moein ;
Ghassemi, Mona .
IEEE TRANSACTIONS ON TRANSPORTATION ELECTRIFICATION, 2021, 7 (03) :1930-1953
[7]  
Boukhlifa M., 2019, P IEEE HOLM C EL CON, P1
[8]   History of Aircraft Wiring Arc-Fault Protection [J].
Brusso, Barry C. .
IEEE INDUSTRY APPLICATIONS MAGAZINE, 2017, 23 (03) :6-11
[9]  
Domone J, 2018, Tech. Rep.
[10]   Energy Losses from an Arc Tracking in Aeronautic Cables in DC Circuits [J].
El Bayda, H. ;
Valensi, F. ;
Masquere, M. ;
Gleizes, A. .
IEEE TRANSACTIONS ON DIELECTRICS AND ELECTRICAL INSULATION, 2013, 20 (01) :19-27