Development of voltage standards for turbo-electric distributed propulsion aircraft power systems

Andrew M. Bollman, Michael J. Armstrong, Catherine E. Jones, Patrick J. Norman, Stuart J. Galloway

Research output: Chapter in Book/Report/Conference proceedingConference contribution book

2 Citations (Scopus)

Abstract

Distributed propulsion is being considered as a possible solution to increase aircraft efficiency, reduce fuel costs and reduce emissions. The size, weight and efficiency of components within a Turbo-electric Distributed Propulsion (TeDP) system are dependent on the voltage level of the electrical power network. Current aircraft voltage standards do not address the architecture of distributed propulsion and so a review of voltage standards from different industries is conducted with areas of commonality addressed. An example of TeDP architecture is presented and analyzed to highlight how current aircraft standards may not apply to TeDP. A summary of challenges in developing standards for a TeDP is compiled with a stakeholder analysis to demonstrate the wide range of industries and personnel with vested interests in the development of voltage standards and recommended practices for TeDP.
LanguageEnglish
Title of host publication2015 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles (ESARS)
PublisherIEEE
Pages1-6
Number of pages6
ISBN (Print)9781479974009
DOIs
Publication statusPublished - Mar 2015
EventInternational Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles, ESARS 2015 - Aachen, Germany
Duration: 3 Mar 20155 Mar 2015

Conference

ConferenceInternational Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles, ESARS 2015
Abbreviated titleESARS2015
CountryGermany
CityAachen
Period3/03/155/03/15

Fingerprint

Propulsion
Electric potential
Aircraft
Aircraft power systems
Industry
Personnel
Costs

Keywords

  • aerospace propulsion
  • distribution networks
  • aircraft power systems
  • voltage measurement
  • current aircraft voltage standards

Cite this

Bollman, A. M., Armstrong, M. J., Jones, C. E., Norman, P. J., & Galloway, S. J. (2015). Development of voltage standards for turbo-electric distributed propulsion aircraft power systems. In 2015 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles (ESARS) (pp. 1-6). IEEE. https://doi.org/10.1109/ESARS.2015.7101488
Bollman, Andrew M. ; Armstrong, Michael J. ; Jones, Catherine E. ; Norman, Patrick J. ; Galloway, Stuart J. / Development of voltage standards for turbo-electric distributed propulsion aircraft power systems. 2015 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles (ESARS). IEEE, 2015. pp. 1-6
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abstract = "Distributed propulsion is being considered as a possible solution to increase aircraft efficiency, reduce fuel costs and reduce emissions. The size, weight and efficiency of components within a Turbo-electric Distributed Propulsion (TeDP) system are dependent on the voltage level of the electrical power network. Current aircraft voltage standards do not address the architecture of distributed propulsion and so a review of voltage standards from different industries is conducted with areas of commonality addressed. An example of TeDP architecture is presented and analyzed to highlight how current aircraft standards may not apply to TeDP. A summary of challenges in developing standards for a TeDP is compiled with a stakeholder analysis to demonstrate the wide range of industries and personnel with vested interests in the development of voltage standards and recommended practices for TeDP.",
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note = "(c) 2015 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other users, 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 components of this work in other works.",
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Bollman, AM, Armstrong, MJ, Jones, CE, Norman, PJ & Galloway, SJ 2015, Development of voltage standards for turbo-electric distributed propulsion aircraft power systems. in 2015 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles (ESARS). IEEE, pp. 1-6, International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles, ESARS 2015, Aachen, Germany, 3/03/15. https://doi.org/10.1109/ESARS.2015.7101488

Development of voltage standards for turbo-electric distributed propulsion aircraft power systems. / Bollman, Andrew M.; Armstrong, Michael J.; Jones, Catherine E.; Norman, Patrick J.; Galloway, Stuart J.

2015 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles (ESARS). IEEE, 2015. p. 1-6.

Research output: Chapter in Book/Report/Conference proceedingConference contribution book

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N1 - (c) 2015 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other users, 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 components of this work in other works.

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N2 - Distributed propulsion is being considered as a possible solution to increase aircraft efficiency, reduce fuel costs and reduce emissions. The size, weight and efficiency of components within a Turbo-electric Distributed Propulsion (TeDP) system are dependent on the voltage level of the electrical power network. Current aircraft voltage standards do not address the architecture of distributed propulsion and so a review of voltage standards from different industries is conducted with areas of commonality addressed. An example of TeDP architecture is presented and analyzed to highlight how current aircraft standards may not apply to TeDP. A summary of challenges in developing standards for a TeDP is compiled with a stakeholder analysis to demonstrate the wide range of industries and personnel with vested interests in the development of voltage standards and recommended practices for TeDP.

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Bollman AM, Armstrong MJ, Jones CE, Norman PJ, Galloway SJ. Development of voltage standards for turbo-electric distributed propulsion aircraft power systems. In 2015 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles (ESARS). IEEE. 2015. p. 1-6 https://doi.org/10.1109/ESARS.2015.7101488