Review of design and challenges of DC SSPC in more electric aircraft
Solid State Power Controller (SSPC) is gaining popularity, replacing mechanical switches and circuit breakers, in niche markets like electrical power distribution systems of the more electric aircraft. Significant amount of research is being conducted to develop high power SSPCs to cater the dynamic...
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sg-ntu-dr.10356-1465062021-02-22T07:50:15Z Review of design and challenges of DC SSPC in more electric aircraft Molligoda, Devinda A. Chatterjee, Pradip Gajanayake, Chandana J. Gupta, Amit Kumar Tseng, King Jet School of Electrical and Electronic Engineering 2016 IEEE 2nd Annual Southern Power Electronics Conference (SPEC) Rolls Royce Singapore Rolls-Royce@NTU Corporate Lab Engineering::Electrical and electronic engineering::Power electronics SSPC More Electrical Aircraft Solid State Power Controller (SSPC) is gaining popularity, replacing mechanical switches and circuit breakers, in niche markets like electrical power distribution systems of the more electric aircraft. Significant amount of research is being conducted to develop high power SSPCs to cater the dynamic, distributed load management. The 28V SSPCs are widely used for protection and control of the secondary distribution system. Although there are high current SSPCs for low bus voltages, the 270V SSPCs are not mature and high current 270V SSPCs are not available in the market or having limited capability, which would be used in the primary power distribution system of the aircraft. This paper presents the market availability, design challenges the design engineer should be aware of and various approaches adopted to design and develop a high current 270V DC SSPC for more electric aircraft system, its key features which may not have been available in the traditional switches and future trends. National Research Foundation (NRF) Accepted version This work is jointly funded by National Research Foundation (NRF) Singapore, Rolls-Royce Singapore Pte. Ltd, and Nanyang Technological University, Singapore. 2021-02-22T07:50:15Z 2021-02-22T07:50:15Z 2017 Conference Paper Molligoda, D. A., Chatterjee, P., Gajanayake, C. J., Gupta, A. K., & Tseng, K. J. (2017). Review of design and challenges of DC SSPC in more electric aircraft. Proceedings of the IEEE Southern Power Electronics Conference (SPEC), 1-5. doi:10.1109/SPEC.2016.7846117 https://hdl.handle.net/10356/146506 10.1109/SPEC.2016.7846117 1 5 en © 2016 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting/republishing this material for advertising or promotional purposes, creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works. The published version is available at: https://doi.org/10.1109/SPEC.2016.7846117 application/pdf |
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Engineering::Electrical and electronic engineering::Power electronics SSPC More Electrical Aircraft Molligoda, Devinda A. Chatterjee, Pradip Gajanayake, Chandana J. Gupta, Amit Kumar Tseng, King Jet Review of design and challenges of DC SSPC in more electric aircraft |
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Solid State Power Controller (SSPC) is gaining popularity, replacing mechanical switches and circuit breakers, in niche markets like electrical power distribution systems of the more electric aircraft. Significant amount of research is being conducted to develop high power SSPCs to cater the dynamic, distributed load management. The 28V SSPCs are widely used for protection and control of the secondary distribution system. Although there are high current SSPCs for low bus voltages, the 270V SSPCs are not mature and high current 270V SSPCs are not available in the market or having limited capability, which would be used in the primary power distribution system of the aircraft. This paper presents the market availability, design challenges the design engineer should be aware of and various approaches adopted to design and develop a high current 270V DC SSPC for more electric aircraft system, its key features which may not have been available in the traditional switches and future trends. |
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School of Electrical and Electronic Engineering |
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School of Electrical and Electronic Engineering Molligoda, Devinda A. Chatterjee, Pradip Gajanayake, Chandana J. Gupta, Amit Kumar Tseng, King Jet |
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Conference or Workshop Item |
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Molligoda, Devinda A. Chatterjee, Pradip Gajanayake, Chandana J. Gupta, Amit Kumar Tseng, King Jet |
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Molligoda, Devinda A. |
title |
Review of design and challenges of DC SSPC in more electric aircraft |
title_short |
Review of design and challenges of DC SSPC in more electric aircraft |
title_full |
Review of design and challenges of DC SSPC in more electric aircraft |
title_fullStr |
Review of design and challenges of DC SSPC in more electric aircraft |
title_full_unstemmed |
Review of design and challenges of DC SSPC in more electric aircraft |
title_sort |
review of design and challenges of dc sspc in more electric aircraft |
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2021 |
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https://hdl.handle.net/10356/146506 |
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1695706213934694400 |