NASA NTRS · 19870000566
Optical Temperature Sensor For Gas Turbines
Abstract
New 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.
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Mossey, P. W.. 1987-11-01. Optical Temperature Sensor For Gas Turbines. https://ntrs.nasa.gov/citations/19870000566
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