2011
DOI: 10.1109/jsen.2010.2055559
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Inductive Sensor for Lightning Current Measurement, Fitted in Aircraft Windows—Part II: Measurements on an A320 Aircraft

Abstract: DOI to the publisher's website. • The final author version and the galley proof are versions of the publication after peer review. • The final published version features the final layout of the paper including the volume, issue and page numbers. Link to publication General rights Copyright and moral rights for the publications made accessible in the public portal are retained by the authors and/or other copyright owners and it is a condition of accessing publications that users recognise and abide by the legal… Show more

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Cited by 10 publications
(11 citation statements)
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“…Its main goals are to measure lightning strike parameters, to determine entry and exit points on the aircraft structure, and to assess the possible structural damage. It was comprehensively described in a series of publications (de Boer et al, ; Hervé et al, ; Stelmashuk et al, , ; van Deursen, ; van Deursen & Stelmashuk, ; Zwemmer et al, ). The ILDAS system was extended with two LaBr3 40 × 40 mm 2 cylindrical scintillation detectors.…”
Section: Instrument and Datamentioning
confidence: 99%
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“…Its main goals are to measure lightning strike parameters, to determine entry and exit points on the aircraft structure, and to assess the possible structural damage. It was comprehensively described in a series of publications (de Boer et al, ; Hervé et al, ; Stelmashuk et al, , ; van Deursen, ; van Deursen & Stelmashuk, ; Zwemmer et al, ). The ILDAS system was extended with two LaBr3 40 × 40 mm 2 cylindrical scintillation detectors.…”
Section: Instrument and Datamentioning
confidence: 99%
“…The ILDAS system contains one electric field sensor ( E field) and eight magnetic field window sensors ( H field). Photographs of the system and operational details can be found in Kochkin et al () and van Deursen (). Both sensors are differentiating, and subsequent analog integration provides a flat response over the frequency band from 100 Hz to 10 MHz for H field and 10 Hz to 500 kHz for E field.…”
Section: Instrument and Datamentioning
confidence: 99%
“…A is of the same order as the window surface; the analytical solution for a circular window with radius r w is A = r 2 w . A numerical analysis of the window sensor takes the actual shape of the window and the mounting flanges into account [56,54]. Measured and calculated values agreed better than 5% for an aircraft with a thin metallic hull such as an Airbus A320 [54].…”
Section: Ildas H and E Sensorsmentioning
confidence: 94%
“…A numerical analysis of the window sensor takes the actual shape of the window and the mounting flanges into account [56,54]. Measured and calculated values agreed better than 5% for an aircraft with a thin metallic hull such as an Airbus A320 [54]. The horizontal wire makes the sensor respond to the horizontal component of the current density K 0 ; a vertical wire to the vertical component of K 0 , be it with different sensitivity because of the ellipsoidal window.…”
Section: Ildas H and E Sensorsmentioning
confidence: 99%
“…Furthermore, most of the commercially available components are bulky and cannot easily be implemented in compact setups. Therefore, homemade sensors such as D-I (Differentiating-Integrating) systems, capacitive voltage probes, Rogowski coils [13]- [18] or even electro-optic probes are often employed [19], [20].…”
Section: A Motivationmentioning
confidence: 99%