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Development and Application of a High Temperature Turbine Test Facility
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English
Abstract
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.
Citation
Kuintzle, 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.Also In
References
- Wisnieff S. F. Bardach H. “A Radioactive Krypton Diffusion Technique for Temperature Mapping of Turbine Blade Surfaces.” SAE Transactions 74 1966 650704