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

doi:10.1109/ESARS.2015.7101489

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

Electronic And Electrical Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution book

5 Citations (Scopus)

213 Downloads (Pure)

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.

Original language	English
Title of host publication	2015 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles (ESARS)
Place of Publication	Piscataway, NJ.
Publisher	IEEE
Pages	1-6
Number of pages	6
ISBN (Print)	9781479974009
DOIs	https://doi.org/10.1109/ESARS.2015.7101489
Publication status	Published - 3 Mar 2015
Event	2015 International Conference on Electric Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles - Aachen, Germany Duration: 3 Mar 2015 → 5 Mar 2015

Conference

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

Keywords

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

Access to Document

10.1109/ESARS.2015.7101489

Jones-etal-ESARS2015-sensitivity-analysis-tool-for-consideration-of-full-electric-aircraftAccepted author manuscript, 999 KB

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). IEEE. https://doi.org/10.1109/ESARS.2015.7101489

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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 = "{\textcopyright} 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.; 2015 International Conference on Electric Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles, ESARS ; Conference date: 03-03-2015 Through 05-03-2015",

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doi = "10.1109/ESARS.2015.7101489",

language = "English",

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booktitle = "2015 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles (ESARS)",

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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. et al.
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 proceeding › Conference contribution book

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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.

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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.

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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 doi: 10.1109/ESARS.2015.7101489

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

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Keywords

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

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