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Optical Temperature Sensor For Gas TurbinesNew design promises accuracy even in presence of contamination. Improved sensor developed to measure gas temperatures up to 1,700 degree C in gas-turbine engines. Sensor has conical shape for mechanical strengths and optical configuration insensitive to deposits of foreign matter on sides of cone.
Document ID
19870000566
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Mossey, P. W.
(General Electric Co.)
Date Acquired
August 13, 2013
Publication Date
November 1, 1987
Publication Information
Publication: NASA Tech Briefs
Volume: 11
Issue: 10
ISSN: 0145-319X
Subject Category
Mathematics And Information Sciences
Report/Patent Number
LEW-14276
Accession Number
87B10566
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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