2000 IEEE Aerospace Conference. Proceedings (Cat. No.00TH8484)
DOI: 10.1109/aero.2000.877882
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In-line oil debris monitor for aircraft engine condition assessment

Abstract: K1J 953, tel# (613) 744-3530 Failure Mechanism Dimensional Discrepancies Overrolling of Debris Corrosion Other FatigueAbsrrucr-The development of an in-line, full flow oil debris sensor for aircraft engine condition assessment is described. First used on the F22 fighter, this sensor is the only " all-metals" debris detector in production. The sensor is based on an inductive measurement technique which enables the system to detect, count and classify wear metal particles by size and type (ferromagnetic and nonf… Show more

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Cited by 129 publications
(121 citation statements)
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“…It is observed that the equivalent resistance 2 is a formula of excitation frequency according to (8) and (9). The inductances 1 and 2 are unaffected by the excitation frequency.…”
Section: Advances In Mechanical Engineeringmentioning
confidence: 98%
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“…It is observed that the equivalent resistance 2 is a formula of excitation frequency according to (8) and (9). The inductances 1 and 2 are unaffected by the excitation frequency.…”
Section: Advances In Mechanical Engineeringmentioning
confidence: 98%
“…The short-circuit loop resistance 4 of the ferromagnetic debris can be calculated with formula (8) and formula (9). So the changing rate of the microsensor coil inductance can be described as formula (15) while it detects ferromagnetic debris.…”
Section: Advances In Mechanical Engineeringmentioning
confidence: 99%
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“…They found that cumulative particle counting can be used to indicate the onset and progression of pitting damage in gears. A similar approach has been shown effective for damage detection in bearings [17]. These earlier studies all used inductive in-line sensors for particle detection.…”
Section: Introductionmentioning
confidence: 99%