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Integrated control and health monitoring capacitive displacement sensor development task. Orbit transfer rocket engine technology programThe development of a miniature multifunction turbomachinery shaft displacement sensor using state-of-the-art non-contract capacitive sensing technology is described. Axial displacement, radial displacement, and speed are sensed using a single probe within the envelope normally required for a single function. A survey of displacement sensing technology is summarized including inductive, capacitive, optical and ultrasonic techniques. The design and operation of an experimental triple function sensor is described. Test results are included showing calibration tests and simultaneous dynamic testing of multiple functions. Recommendations for design changes are made to improve low temperature performance, reliability, and for design of a flight type signal conditioning unit.
Document ID
19890016837
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Collamore, Frank N.
(Aerojet TechSystems Co. Sacramento, CA, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1989
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-CR-182279
NAS 1.26:182279
Report Number: NASA-CR-182279
Report Number: NAS 1.26:182279
Accession Number
89N26208
Funding Number(s)
CONTRACT_GRANT: NAS3-23772
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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