A micro-fabricated current sensor for arc fault detection of aircraft wiring

Brian G Moffat, Marc Phillipe Yves Desmulliez, Keith Edgar Brown, Chintan Desai, David Flynn, Alistair Sutherland

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

Abstract

This paper presents the design and manufacture of a miniaturised current sensor for detecting partial discharges and the are fault current signatures that indicate that aircraft wire and interconnect have reached end of life/point of failure. The bandwidth of the sensor is in the range of 200MHz to detect fast rise time current spikes which are indicative of intermittent degradation of the wire and interconnect that result in partial discharge and arcing. The sensor is a Rogowski coil manufactured using the UV-LIGA manufacturing process.

Original languageEnglish
Title of host publication2nd Electronics System-Integration Technology Conference, 2008
PublisherIEEE
Pages299-304
Number of pages6
ISBN (Electronic)978-1-4244-2814-4
ISBN (Print)978-1-4244-2813-7
DOIs
Publication statusPublished - 2008
Event2nd Electronics System-Integration Technology Conference - University of Greenwich, Greenwich, United Kingdom
Duration: 1 Sep 20084 Sep 2008
Conference number: 14295
https://www.ieee.org/conferences_events/conferences/conferencedetails/index.html?Conf_ID=14295 (Conference website)

Conference

Conference2nd Electronics System-Integration Technology Conference
Abbreviated titleESTC 2008
CountryUnited Kingdom
CityGreenwich
Period1/09/084/09/08
OtherAdvanced Packaging, Emerging Technologies, Electronicsystemintegration for Healthcare, Manufacturing and Test Technologies, New Materials & Processes, Modelling, Simulation and Design, Optoelectronics, Technology and Reliability for Nano and Micro Structures, Power Electronics, Assembly of Alternative Energy Sources
Internet address

Keywords

  • LOCATION
  • WIRES

Cite this

Moffat, B. G., Desmulliez, M. P. Y., Brown, K. E., Desai, C., Flynn, D., & Sutherland, A. (2008). A micro-fabricated current sensor for arc fault detection of aircraft wiring. In 2nd Electronics System-Integration Technology Conference, 2008 (pp. 299-304). IEEE. https://doi.org/10.1109/ESTC.2008.4684365
Moffat, Brian G ; Desmulliez, Marc Phillipe Yves ; Brown, Keith Edgar ; Desai, Chintan ; Flynn, David ; Sutherland, Alistair. / A micro-fabricated current sensor for arc fault detection of aircraft wiring. 2nd Electronics System-Integration Technology Conference, 2008. IEEE, 2008. pp. 299-304
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title = "A micro-fabricated current sensor for arc fault detection of aircraft wiring",
abstract = "This paper presents the design and manufacture of a miniaturised current sensor for detecting partial discharges and the are fault current signatures that indicate that aircraft wire and interconnect have reached end of life/point of failure. The bandwidth of the sensor is in the range of 200MHz to detect fast rise time current spikes which are indicative of intermittent degradation of the wire and interconnect that result in partial discharge and arcing. The sensor is a Rogowski coil manufactured using the UV-LIGA manufacturing process.",
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author = "Moffat, {Brian G} and Desmulliez, {Marc Phillipe Yves} and Brown, {Keith Edgar} and Chintan Desai and David Flynn and Alistair Sutherland",
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Moffat, BG, Desmulliez, MPY, Brown, KE, Desai, C, Flynn, D & Sutherland, A 2008, A micro-fabricated current sensor for arc fault detection of aircraft wiring. in 2nd Electronics System-Integration Technology Conference, 2008. IEEE, pp. 299-304, 2nd Electronics System-Integration Technology Conference, Greenwich, United Kingdom, 1/09/08. https://doi.org/10.1109/ESTC.2008.4684365

A micro-fabricated current sensor for arc fault detection of aircraft wiring. / Moffat, Brian G; Desmulliez, Marc Phillipe Yves; Brown, Keith Edgar; Desai, Chintan; Flynn, David; Sutherland, Alistair.

2nd Electronics System-Integration Technology Conference, 2008. IEEE, 2008. p. 299-304.

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

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N2 - This paper presents the design and manufacture of a miniaturised current sensor for detecting partial discharges and the are fault current signatures that indicate that aircraft wire and interconnect have reached end of life/point of failure. The bandwidth of the sensor is in the range of 200MHz to detect fast rise time current spikes which are indicative of intermittent degradation of the wire and interconnect that result in partial discharge and arcing. The sensor is a Rogowski coil manufactured using the UV-LIGA manufacturing process.

AB - This paper presents the design and manufacture of a miniaturised current sensor for detecting partial discharges and the are fault current signatures that indicate that aircraft wire and interconnect have reached end of life/point of failure. The bandwidth of the sensor is in the range of 200MHz to detect fast rise time current spikes which are indicative of intermittent degradation of the wire and interconnect that result in partial discharge and arcing. The sensor is a Rogowski coil manufactured using the UV-LIGA manufacturing process.

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Moffat BG, Desmulliez MPY, Brown KE, Desai C, Flynn D, Sutherland A. A micro-fabricated current sensor for arc fault detection of aircraft wiring. In 2nd Electronics System-Integration Technology Conference, 2008. IEEE. 2008. p. 299-304 https://doi.org/10.1109/ESTC.2008.4684365