A pre-design sensitivity analysis tool for consideration of full electrical aircraft propulsion electrical power system architectures

C.E. Jones, P.J. Norman, S.J. Galloway, G.M. Burt, M. Armstrong, A. Bollman

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

4 Citations (Scopus)

Abstract

Turbo-electric distributed power (TeDP) systems proposed for hybrid wing body (HWB) N3-X aircraft are complex, superconducting electrical networks, which must be developed to meet challenging weight, efficiency and propulsor power requirements. An integrated system sensitivity analysis tool is presented, which can be used to support rapid appraisal studies of architectures, protection systems and redundancy requirements for TeDP systems. The use of this tool can help direct future research on TeDP systems towards the key challenges relevant to meeting the stringent weight and efficiency targets set out for N+3 aircraft concepts.
LanguageEnglish
Title of host publication2015 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles (ESARS)
Place of PublicationPiscataway, NJ.
PublisherIEEE
Pages1-6
Number of pages6
ISBN (Print)9781479974009
DOIs
Publication statusPublished - 3 Mar 2015
Event2015 International Conference on Electric Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles - Aachen, Germany
Duration: 3 Mar 20155 Mar 2015

Conference

Conference2015 International Conference on Electric Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles
Abbreviated titleESARS
CountryGermany
CityAachen
Period3/03/155/03/15

Fingerprint

Aircraft propulsion
Sensitivity analysis
Aircraft
Redundancy

Keywords

  • turbo-electric distributed propulsion (TeDP)
  • sensitivity analysis
  • superconducting systems
  • aircraft
  • aerospace propulsion
  • aircraft power systems

Cite this

Jones, C. E., Norman, P. J., Galloway, S. J., Burt, G. M., Armstrong, M., & Bollman, A. (2015). A pre-design sensitivity analysis tool for consideration of full electrical aircraft propulsion electrical power system architectures. In 2015 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles (ESARS) (pp. 1-6). Piscataway, NJ.: IEEE. https://doi.org/10.1109/ESARS.2015.7101489
Jones, C.E. ; Norman, P.J. ; Galloway, S.J. ; Burt, G.M. ; Armstrong, M. ; Bollman, A. / A pre-design sensitivity analysis tool for consideration of full electrical aircraft propulsion electrical power system architectures. 2015 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles (ESARS). Piscataway, NJ. : IEEE, 2015. pp. 1-6
@inproceedings{6ecaeff3bcd9412baac3fb9823420bc6,
title = "A pre-design sensitivity analysis tool for consideration of full electrical aircraft propulsion electrical power system architectures",
abstract = "Turbo-electric distributed power (TeDP) systems proposed for hybrid wing body (HWB) N3-X aircraft are complex, superconducting electrical networks, which must be developed to meet challenging weight, efficiency and propulsor power requirements. An integrated system sensitivity analysis tool is presented, which can be used to support rapid appraisal studies of architectures, protection systems and redundancy requirements for TeDP systems. The use of this tool can help direct future research on TeDP systems towards the key challenges relevant to meeting the stringent weight and efficiency targets set out for N+3 aircraft concepts.",
keywords = "turbo-electric distributed propulsion (TeDP), sensitivity analysis, superconducting systems, aircraft, aerospace propulsion, aircraft power systems",
author = "C.E. Jones and P.J. Norman and S.J. Galloway and G.M. Burt and M. Armstrong and A. Bollman",
note = "{\circledC} 2015 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.",
year = "2015",
month = "3",
day = "3",
doi = "10.1109/ESARS.2015.7101489",
language = "English",
isbn = "9781479974009",
pages = "1--6",
booktitle = "2015 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles (ESARS)",
publisher = "IEEE",

}

Jones, CE, Norman, PJ, Galloway, SJ, Burt, GM, Armstrong, M & Bollman, A 2015, A pre-design sensitivity analysis tool for consideration of full electrical aircraft propulsion electrical power system architectures. in 2015 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles (ESARS). IEEE, Piscataway, NJ., pp. 1-6, 2015 International Conference on Electric Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles, Aachen, Germany, 3/03/15. https://doi.org/10.1109/ESARS.2015.7101489

A pre-design sensitivity analysis tool for consideration of full electrical aircraft propulsion electrical power system architectures. / Jones, C.E.; Norman, P.J.; Galloway, S.J.; Burt, G.M.; Armstrong, M.; Bollman, A.

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

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

TY - GEN

T1 - A pre-design sensitivity analysis tool for consideration of full electrical aircraft propulsion electrical power system architectures

AU - Jones, C.E.

AU - Norman, P.J.

AU - Galloway, S.J.

AU - Burt, G.M.

AU - Armstrong, M.

AU - Bollman, A.

N1 - © 2015 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.

PY - 2015/3/3

Y1 - 2015/3/3

N2 - Turbo-electric distributed power (TeDP) systems proposed for hybrid wing body (HWB) N3-X aircraft are complex, superconducting electrical networks, which must be developed to meet challenging weight, efficiency and propulsor power requirements. An integrated system sensitivity analysis tool is presented, which can be used to support rapid appraisal studies of architectures, protection systems and redundancy requirements for TeDP systems. The use of this tool can help direct future research on TeDP systems towards the key challenges relevant to meeting the stringent weight and efficiency targets set out for N+3 aircraft concepts.

AB - Turbo-electric distributed power (TeDP) systems proposed for hybrid wing body (HWB) N3-X aircraft are complex, superconducting electrical networks, which must be developed to meet challenging weight, efficiency and propulsor power requirements. An integrated system sensitivity analysis tool is presented, which can be used to support rapid appraisal studies of architectures, protection systems and redundancy requirements for TeDP systems. The use of this tool can help direct future research on TeDP systems towards the key challenges relevant to meeting the stringent weight and efficiency targets set out for N+3 aircraft concepts.

KW - turbo-electric distributed propulsion (TeDP)

KW - sensitivity analysis

KW - superconducting systems

KW - aircraft

KW - aerospace propulsion

KW - aircraft power systems

UR - http://ieeexplore.ieee.org/xpl/mostRecentIssue.jsp?punumber=7091733

U2 - 10.1109/ESARS.2015.7101489

DO - 10.1109/ESARS.2015.7101489

M3 - Conference contribution book

SN - 9781479974009

SP - 1

EP - 6

BT - 2015 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles (ESARS)

PB - IEEE

CY - Piscataway, NJ.

ER -

Jones CE, Norman PJ, Galloway SJ, Burt GM, Armstrong M, Bollman A. A pre-design sensitivity analysis tool for consideration of full electrical aircraft propulsion electrical power system architectures. In 2015 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles (ESARS). Piscataway, NJ.: IEEE. 2015. p. 1-6 https://doi.org/10.1109/ESARS.2015.7101489