A review of Turboelectric Distributed Propulsion technologies for N+3 aircraft electrical systems

Karen Michelle Davies, Patrick Norman, Catherine Jones, Stuart Galloway, Mark Husband

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

4 Citations (Scopus)

Abstract

In order to minimise the environmental impact of increased air traffic substantial developments in civil aircraft electrical power systems must occur. NASA have set a target to reduce noise by 71dB, NOx emissions by 80% and fuel consumption by 60% for the N+3 generation of aircraft entering into service sometime between 2030 and 2035. Turboelectric Distributed Propulsion (TeDP) is expected to enable these goals to be met. NASA's N3-X concept aircraft comprises gas turbine engines which drive electrical generators and a DC network distributes power to an array of fans, which provide thrust. Interconnection and protection technologies will also be included to achieve desired levels of reliability of supply to the propulsion motors. This paper outlines the architecture of a generic TeDP system, explores its benefits, describes technical challenges that will need to be overcome and discusses the technical implications of implementing TeDP with regards to electrical system power density and safety.
LanguageEnglish
Title of host publication2013 48th International Universities' Power Engineering Conference (UPEC)
Place of PublicationPiscataway, NJ.
PublisherIEEE
Pages1-5
Number of pages5
ISBN (Electronic)9781479932542
DOIs
Publication statusPublished - 2013
Event2013 48th International Universities' Power Engineering Conference (UPEC) - Dublin, Ireland
Duration: 2 Sep 20135 Sep 2013

Conference

Conference2013 48th International Universities' Power Engineering Conference (UPEC)
CountryIreland
CityDublin
Period2/09/135/09/13

Fingerprint

Propulsion
Aircraft
NASA
Fuel consumption
Fans
Gas turbines
Environmental impact
Turbines
Aircraft power systems
Air

Keywords

  • N+3
  • Turboelectric Distributed Propulsion
  • aerospace engines
  • aerospace propulsion
  • air traffic
  • aircraft power systems
  • electric generators
  • electric propulsion
  • gas turbines
  • reliability

Cite this

Davies, K. M., Norman, P., Jones, C., Galloway, S., & Husband, M. (2013). A review of Turboelectric Distributed Propulsion technologies for N+3 aircraft electrical systems. In 2013 48th International Universities' Power Engineering Conference (UPEC) (pp. 1-5). [6714885] Piscataway, NJ.: IEEE. https://doi.org/10.1109/UPEC.2013.6714885
Davies, Karen Michelle ; Norman, Patrick ; Jones, Catherine ; Galloway, Stuart ; Husband, Mark. / A review of Turboelectric Distributed Propulsion technologies for N+3 aircraft electrical systems. 2013 48th International Universities' Power Engineering Conference (UPEC). Piscataway, NJ. : IEEE, 2013. pp. 1-5
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Davies, KM, Norman, P, Jones, C, Galloway, S & Husband, M 2013, A review of Turboelectric Distributed Propulsion technologies for N+3 aircraft electrical systems. in 2013 48th International Universities' Power Engineering Conference (UPEC)., 6714885, IEEE, Piscataway, NJ., pp. 1-5, 2013 48th International Universities' Power Engineering Conference (UPEC), Dublin, Ireland, 2/09/13. https://doi.org/10.1109/UPEC.2013.6714885

A review of Turboelectric Distributed Propulsion technologies for N+3 aircraft electrical systems. / Davies, Karen Michelle; Norman, Patrick; Jones, Catherine; Galloway, Stuart; Husband, Mark.

2013 48th International Universities' Power Engineering Conference (UPEC). Piscataway, NJ. : IEEE, 2013. p. 1-5 6714885.

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

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Davies KM, Norman P, Jones C, Galloway S, Husband M. A review of Turboelectric Distributed Propulsion technologies for N+3 aircraft electrical systems. In 2013 48th International Universities' Power Engineering Conference (UPEC). Piscataway, NJ.: IEEE. 2013. p. 1-5. 6714885 https://doi.org/10.1109/UPEC.2013.6714885