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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Main Authors: Molligoda, Devinda A., Chatterjee, Pradip, Gajanayake, Chandana J., Gupta, Amit Kumar, Tseng, King Jet
Other Authors: School of Electrical and Electronic Engineering
Format: Conference or Workshop Item
Language:English
Published: 2021
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Online Access:https://hdl.handle.net/10356/146506
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Institution: Nanyang Technological University
Language: English
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spelling 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
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic Engineering::Electrical and electronic engineering::Power electronics
SSPC
More Electrical Aircraft
spellingShingle 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
description 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.
author2 School of Electrical and Electronic Engineering
author_facet School of Electrical and Electronic Engineering
Molligoda, Devinda A.
Chatterjee, Pradip
Gajanayake, Chandana J.
Gupta, Amit Kumar
Tseng, King Jet
format Conference or Workshop Item
author Molligoda, Devinda A.
Chatterjee, Pradip
Gajanayake, Chandana J.
Gupta, Amit Kumar
Tseng, King Jet
author_sort 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
publishDate 2021
url https://hdl.handle.net/10356/146506
_version_ 1695706213934694400