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Thin-film temperature sensors for gas turbine engines Problems and prospectsThe erosion and corrosion of thermocouples used to measure the temperature in turbine engines are studied. Structural and metallurgical interactions and instabilities at thermocouple interfaces are analyzed. Consideration is given to the adhesion, dielectric quality, surface topography, and hardness of the thermal oxides; it is observed that the structural and thermoelectric stability of thin-film thermocouple elements depends on adhesion, surface topography, and dielectric strength. The electrical conductivity and impurity content of the oxide scale are evaluated. Methods for improving the adhesion of thermocouples on the alumina surfaces are described. Compositional inhomogeneities in the sensors and contamination of the thermocouple elements are examined. The fabrication of the thermocouples is discussed. It is noted that Al2O3 and Si3N4 are useful for developing stable thermocouple elements on the surface of the blades and vanes.
Document ID
19870038835
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
External Source(s)
Authors
Budhani, R. C.
(California Univ. Los Angeles, CA, United States)
Prakash, S.
(California Univ. Los Angeles, CA, United States)
Bunshah, R. F.
(California, University Los Angeles, United States)
Date Acquired
August 13, 2013
Publication Date
December 1, 1986
Publication Information
Publication: Journal of Vacuum Science and Technology A
Volume: 4
ISSN: 0734-2101
Subject Category
Instrumentation And Photography
Accession Number
87A26109
Funding Number(s)
CONTRACT_GRANT: NAG3-451
Distribution Limits
Public
Copyright
Other

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