The use of optical pyrometers in axial flow turbines
An optical pyrometer system that can be used to measure metal temperatures over an extended range of temperature has been developed. Real-time flame discrimination permits accurate operation in the gas turbine environment with high flame content. This versatile capability has been used in a number of ways. In experimental engines, a fixed angle pyrometer has been used for turbine health monitoring for the automatic test stand abort system. Turbine blade creep capability has been improved by tailoring the burner profile based on measured blade temperatures. Fixed and traversing pyrometers were used extensively during engine development to map blade surface temperatures in order to assess cooling effectiveness and identify optimum configurations. Portable units have been used in turbine field inspections. A new low temperature pyrometer is being used as a diagnostic tool in the alternate turbopump design for the Space Shuttle main engine. Advanced engine designs will incorporate pyrometers in the engine control system to limit operation to safe temperatures.
- OSTI ID:
- 5652263
- Report Number(s):
- AIAA-Paper-89-2692; CONF-8907118-
- Resource Relation:
- Conference: 25. American Society of Mechanical Engineers joint propulsion conference, Monterey, CA (USA), 10-13 Jul 1989
- Country of Publication:
- United States
- Language:
- English
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Related Subjects
42 ENGINEERING
GAS TURBINE ENGINES
TEMPERATURE MEASUREMENT
ROCKET ENGINES
TURBOMACHINERY
AIRFOILS
CONTROL
COOLING
CREEP
OPTICAL PYROMETERS
TEMPERATURE DISTRIBUTION
TESTING
TURBINE BLADES
ENGINES
HEAT ENGINES
INTERNAL COMBUSTION ENGINES
MACHINERY
MEASURING INSTRUMENTS
MECHANICAL PROPERTIES
PYROMETERS
330103* - Internal Combustion Engines- Turbine
420200 - Engineering- Facilities
Equipment
& Techniques