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Temperature and pressure measurement techniques for an advanced turbine test facilityA high pressure, high-temperature turbine test facility constructed for use in turbine cooling research is described. Several recently developed temperature and pressure measuring techniques are used in this facility. The measurement techniques, their status, previous applications and some results are discussed. Noncontact surface temperature measurements are made by optical methods. Radiation pyrometry principles combined with photoelectric scanning are used for rotating components and infrared photography for stationary components. Contact (direct) temperature and pressure measurements on rotating components are expected to be handled with an 80 channel rotary data package which mounts on and rotates with the turbine shaft at speeds up to 17,500 rpm. The data channels are time-division multiplexed and converted to digital words in the data package. A rotary transformer couples power and digital data to and from the shaft.
Document ID
19800006117
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Pollack, F. G.
(NASA Lewis Research Center Cleveland, OH, United States)
Cochran, R. P.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1980
Subject Category
Instrumentation And Photography
Report/Patent Number
E-212
NASA-TM-79278
Report Number: E-212
Report Number: NASA-TM-79278
Meeting Information
Meeting: Intern. Gas Turbine Conf. and Ann. Fluids Engr. Conf,
Location: New Orleans
Start Date: March 9, 1980
End Date: March 13, 1980
Sponsors: Am. Soc. Mech. Engr.
Accession Number
80N14374
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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