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Pyrometer for measurement of surface temperature distribution on a rotating turbine bladeA conceptual optical method and some test results are presented for measuring the surface temperature distribution on one of the rotating turbine blades with a surface resolution of 0.05 cm spot diameter at a tip speed of 400 m/sec. The blade is scanned line-by-line by a fixed optical system. During each line-scan, the detector analog output signal is converted to two hundred consecutive digital values that are temporarily stored in a high speed buffer memory, and then transferred at a slower rate to a computer for processing. The signal-to-noise ratio of the silicon avalanche detector is large enough to obtain an accuracy of one percent at 1050 K blade temperature. By averaging 25 scans of the same line the same accuracy can be obtained at 900 K.
Document ID
19720024809
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Buchele, D. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Lesco, D. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1972
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-TM-X-68113
Report Number: NASA-TM-X-68113
Meeting Information
Meeting: Symp. on Instrumentation for Airbreathing Propulsion
Location: Monterey, CA
Country: United States
Start Date: September 19, 1972
End Date: September 21, 1972
Accession Number
72N32459
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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