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Development and Application of a High Temperature Turbine Test Facility
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 01, 1967 by SAE International in United States
Annotation ability available
A test facility, test rigs, instrumentation techniques, and operating procedures have been developed to provide research and development capability for high temperature air cooled turbine components for gas turbine engines. The installation offers a wide range of flexibility for use as a high pressure air supply and as an experimental compressor test facility.
Instrumentation techniques developed include kryptonated turbine parts and fiber optic infrared probes. These are discussed in detail.
CitationKuintzle, C. and Goldwater, B., "Development and Application of a High Temperature Turbine Test Facility," SAE Technical Paper 670943, 1967, https://doi.org/10.4271/670943.
- WisnieffS. F., and BardachH., “A Radioactive Krypton Diffusion Technique for Temperature Mapping of Turbine Blade Surfaces.” SAE Transactions, Vol. 74 (1966), paper 650704.