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Thin film temperature sensorThin film surface temperature sensors were developed. The sensors were made of platinum-platinum/10 percent rhodium thermocouples with associated thin film-to-lead wire connections and sputtered on aluminum oxide coated simulated turbine blades for testing. Tests included exposure to vibration, low velocity hydrocarbon hot gas flow to 1250 K, and furnace calibrations. Thermal electromotive force was typically two percent below standard type S thermocouples. Mean time to failure was 42 hours at a hot gas flow temperature of 1250 K and an average of 15 cycles to room temperature. Failures were mainly due to separation of the platinum thin film from the aluminum oxide surface. Several techniques to improve the adhesion of the platinum are discussed.
Document ID
19800009165
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Grant, H. P.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Przybyszewski, J. S.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Date Acquired
September 4, 2013
Publication Date
February 15, 1980
Subject Category
Instrumentation And Photography
Report/Patent Number
PWA-5526-31
NASA-CR-159782
Report Number: PWA-5526-31
Report Number: NASA-CR-159782
Accession Number
80N17425
Funding Number(s)
CONTRACT_GRANT: NAS3-20768
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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