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Technique for temperature compensation of eddy-current proximity probesEddy-current proximity probes are used in turbomachinery evaluation testing and operation to measure distances, primarily vibration, deflection, or displacment of shafts, bearings and seals. Measurements of steady-state conditions made with standard eddy-current proximity probes are susceptible to error caused by temperature variations during normal operation of the component under investigation. Errors resulting from temperature effects for the specific probes used in this study were approximately 1.016 x 10 to the -3 mm/deg C over the temperature range of -252 to 100 C. This report examines temperature caused changes on the eddy-current proximity probe measurement system, establishes their origin, and discusses what may be done to minimize their effect on the output signal. In addition, recommendations are made for the installation and operation of the electronic components associated with an eddy-current proximity probe. Several techniques are described that provide active on-line error compensation for over 95 percent of the temperature effects.
Document ID
19890006009
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Masters, Robert M.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1989
Subject Category
Instrumentation And Photography
Report/Patent Number
E-4316
NASA-TP-2880
NAS 1.60:2880
Report Number: E-4316
Report Number: NASA-TP-2880
Report Number: NAS 1.60:2880
Accession Number
89N15380
Funding Number(s)
PROJECT: RTOP 506-42-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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