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Radiation pyrometer for gas turbine bladesA turbine blade temperature measuring system for liquid oxygen turbopumps is reported. The system includes a three mode, two-input optical signal processor, interconnecting cable, and four sensor heads. Two of the heads are aperture type, while the other two are lens type. This system is applicable to a temperature range of 1400 to 2200 F.
Document ID
19740020818
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rohy, D. A. (International Harvester Co. San Diego, CA, United States)
Compton, W. A. (International Harvester Co. San Diego, CA, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1973
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-CR-120250
Report Number: NASA-CR-120250
Accession Number
74N28931
Funding Number(s)
CONTRACT_GRANT: NAS8-28953
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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