Protection system considerations for DC distributed electrical propulsion systems

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

Research output: Contribution to conferencePaper

2 Citations (Scopus)

Abstract

Distributed electrical propulsion for aircraft, also known as turbo-electric distributed propulsion (TeDP), will require a complex electrical power system which can deliver power to multiple propulsor motors from gas turbine driven generators. To ensure that high enough power densities are reached, it has been proposed that such power systems are superconducting. Key to the development of these systems is the understanding of how faults propagate in the network, which enables possible protection strategies to be considered and following that, the development of an appropriate protection strategy to enable a robust electrical power system with fault ride-through capability. This paper investigates possible DC protection strategies for a radial DC architecture for a TeDP power system, in terms of their ability to respond appropriately to a DC fault and their impact on overall system weight and efficiency. This latter aspect has already been shown to be critical to shaping the overall TeDP concept competitiveness.
LanguageEnglish
Number of pages9
DOIs
Publication statusPublished - 15 Sep 2015
EventSAE Aerotech Congress and Exhibition - Seattle, WA., United States
Duration: 21 Sep 201524 Sep 2015

Conference

ConferenceSAE Aerotech Congress and Exhibition
CountryUnited States
CitySeattle, WA.
Period21/09/1524/09/15

Fingerprint

Propulsion
Turbogenerators
Gas turbines
Aircraft

Keywords

  • turbo-electric distributed propulsion
  • aero-electrical power systems
  • electrical protection
  • supercondutcting

Cite this

Jones, C. E., Davies, K., Norman, P., Galloway, S., Burt, G., Armstrong, M., & Bollman, A. (2015). Protection system considerations for DC distributed electrical propulsion systems. Paper presented at SAE Aerotech Congress and Exhibition, Seattle, WA., United States. https://doi.org/10.4271/2015-01-2404
Jones, C. E. ; Davies, K. ; Norman, P. ; Galloway, S. ; Burt, G. ; Armstrong, M. ; Bollman, A. / Protection system considerations for DC distributed electrical propulsion systems. Paper presented at SAE Aerotech Congress and Exhibition, Seattle, WA., United States.9 p.
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Jones, CE, Davies, K, Norman, P, Galloway, S, Burt, G, Armstrong, M & Bollman, A 2015, 'Protection system considerations for DC distributed electrical propulsion systems' Paper presented at SAE Aerotech Congress and Exhibition, Seattle, WA., United States, 21/09/15 - 24/09/15, . https://doi.org/10.4271/2015-01-2404

Protection system considerations for DC distributed electrical propulsion systems. / Jones, C. E.; Davies, K.; Norman, P.; Galloway, S.; Burt, G.; Armstrong, M.; Bollman, A.

2015. Paper presented at SAE Aerotech Congress and Exhibition, Seattle, WA., United States.

Research output: Contribution to conferencePaper

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AU - Jones, C. E.

AU - Davies, K.

AU - Norman, P.

AU - Galloway, S.

AU - Burt, G.

AU - Armstrong, M.

AU - Bollman, A.

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AB - Distributed electrical propulsion for aircraft, also known as turbo-electric distributed propulsion (TeDP), will require a complex electrical power system which can deliver power to multiple propulsor motors from gas turbine driven generators. To ensure that high enough power densities are reached, it has been proposed that such power systems are superconducting. Key to the development of these systems is the understanding of how faults propagate in the network, which enables possible protection strategies to be considered and following that, the development of an appropriate protection strategy to enable a robust electrical power system with fault ride-through capability. This paper investigates possible DC protection strategies for a radial DC architecture for a TeDP power system, in terms of their ability to respond appropriately to a DC fault and their impact on overall system weight and efficiency. This latter aspect has already been shown to be critical to shaping the overall TeDP concept competitiveness.

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Jones CE, Davies K, Norman P, Galloway S, Burt G, Armstrong M et al. Protection system considerations for DC distributed electrical propulsion systems. 2015. Paper presented at SAE Aerotech Congress and Exhibition, Seattle, WA., United States. https://doi.org/10.4271/2015-01-2404