Fault behaviour of a superconducting turboelectric distributed propulsion aircraft network: a comprehensive sensitivity study

K. M. Davies; P. J. Norman; C. E. Jones; S. J. Galloway; G. M. Burt

doi:10.1109/ESARS.2015.7101487

Fault behaviour of a superconducting turboelectric distributed propulsion aircraft network: a comprehensive sensitivity study

K. M. Davies, P. J. Norman, C. E. Jones, S. J. Galloway, G. M. Burt

Electronic And Electrical Engineering

Research output: Contribution to conference › Paper

7 Citations (Scopus)

104 Downloads (Pure)

Abstract

Variations in the network architecture and component choices of superconducting DC networks proposed for future aircraft propulsion systems could have a significant impact on their fault response. Understanding these potential variations is key to developing effective protection solutions for these aircraft applications. To this end, this paper presents the results of sensitivity studies conducted using a representative model of a faulted superconducting DC network in which key system parameters are varied. Of the parameters considered, network voltage and the cable dimensions are shown to have the greatest impact on fault current profile whilst the rate of change of fault current is shown to be sensitive to network voltage and cable length. The paper concludes by exploring the implications of these findings on the prospective protection strategy for future aircraft propulsion systems.

Original language	English
Number of pages	7
DOIs	https://doi.org/10.1109/ESARS.2015.7101487
Publication status	Published - Mar 2015
Event	International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles, ESARS 2015 - Aachen, Germany Duration: 3 Mar 2015 → 5 Mar 2015

Conference

Conference	International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles, ESARS 2015
Abbreviated title	ESARS2015
Country	Germany
City	Aachen
Period	3/03/15 → 5/03/15

Keywords

fault behaviour
propulsion systems
aircraft propulsion
superconducting DC networks
fault response
turboelectric distributed propulsion (TeDP)

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10.1109/ESARS.2015.7101487

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7 Citations
1 Other report

Architecture, Voltage and Components for a Turboelectric Distributed Propulsion Electric Grid
Armstrong, M. J., Blackwelder, M., Bollman, A., Ross, C., Campbell, A., Jones, C. & Norman, P., 1 Jul 2015, US. 270 p.
Research output: Book/Report › Other report

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Davies, K. M., Norman, P. J., Jones, C. E., Galloway, S. J., & Burt, G. M. (2015). Fault behaviour of a superconducting turboelectric distributed propulsion aircraft network: a comprehensive sensitivity study. Paper presented at International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles, ESARS 2015, Aachen, Germany. https://doi.org/10.1109/ESARS.2015.7101487

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title = "Fault behaviour of a superconducting turboelectric distributed propulsion aircraft network: a comprehensive sensitivity study",

abstract = "Variations in the network architecture and component choices of superconducting DC networks proposed for future aircraft propulsion systems could have a significant impact on their fault response. Understanding these potential variations is key to developing effective protection solutions for these aircraft applications. To this end, this paper presents the results of sensitivity studies conducted using a representative model of a faulted superconducting DC network in which key system parameters are varied. Of the parameters considered, network voltage and the cable dimensions are shown to have the greatest impact on fault current profile whilst the rate of change of fault current is shown to be sensitive to network voltage and cable length. The paper concludes by exploring the implications of these findings on the prospective protection strategy for future aircraft propulsion systems. ",

keywords = "fault behaviour, propulsion systems, aircraft propulsion, superconducting DC networks, fault response, turboelectric distributed propulsion (TeDP)",

author = "Davies, {K. M.} and Norman, {P. J.} and Jones, {C. E.} and Galloway, {S. J.} and Burt, {G. M.}",

year = "2015",

month = mar,

doi = "10.1109/ESARS.2015.7101487",

language = "English",

note = "International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles, ESARS 2015, ESARS2015 ; Conference date: 03-03-2015 Through 05-03-2015",

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Davies, KM, Norman, PJ , Jones, CE , Galloway, SJ & Burt, GM 2015, 'Fault behaviour of a superconducting turboelectric distributed propulsion aircraft network: a comprehensive sensitivity study', Paper presented at International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles, ESARS 2015, Aachen, Germany, 3/03/15 - 5/03/15. https://doi.org/10.1109/ESARS.2015.7101487

Fault behaviour of a superconducting turboelectric distributed propulsion aircraft network : a comprehensive sensitivity study. / Davies, K. M.; Norman, P. J.; Jones, C. E.; Galloway, S. J.; Burt, G. M.

2015. Paper presented at International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles, ESARS 2015, Aachen, Germany.

Research output: Contribution to conference › Paper

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AU - Norman, P. J.

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AU - Burt, G. M.

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N2 - Variations in the network architecture and component choices of superconducting DC networks proposed for future aircraft propulsion systems could have a significant impact on their fault response. Understanding these potential variations is key to developing effective protection solutions for these aircraft applications. To this end, this paper presents the results of sensitivity studies conducted using a representative model of a faulted superconducting DC network in which key system parameters are varied. Of the parameters considered, network voltage and the cable dimensions are shown to have the greatest impact on fault current profile whilst the rate of change of fault current is shown to be sensitive to network voltage and cable length. The paper concludes by exploring the implications of these findings on the prospective protection strategy for future aircraft propulsion systems.

AB - Variations in the network architecture and component choices of superconducting DC networks proposed for future aircraft propulsion systems could have a significant impact on their fault response. Understanding these potential variations is key to developing effective protection solutions for these aircraft applications. To this end, this paper presents the results of sensitivity studies conducted using a representative model of a faulted superconducting DC network in which key system parameters are varied. Of the parameters considered, network voltage and the cable dimensions are shown to have the greatest impact on fault current profile whilst the rate of change of fault current is shown to be sensitive to network voltage and cable length. The paper concludes by exploring the implications of these findings on the prospective protection strategy for future aircraft propulsion systems.

KW - fault behaviour

KW - propulsion systems

KW - aircraft propulsion

KW - superconducting DC networks

KW - fault response

KW - turboelectric distributed propulsion (TeDP)

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Davies KM, Norman PJ , Jones CE , Galloway SJ , Burt GM. Fault behaviour of a superconducting turboelectric distributed propulsion aircraft network: a comprehensive sensitivity study. 2015. Paper presented at International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles, ESARS 2015, Aachen, Germany. https://doi.org/10.1109/ESARS.2015.7101487

Fault behaviour of a superconducting turboelectric distributed propulsion aircraft network: a comprehensive sensitivity study

Abstract

Conference

Keywords

Access to Document

Architecture, Voltage and Components for a Turboelectric Distributed Propulsion Electric Grid

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