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Application of Ceramics to a Radial Inflow Gas Turbine
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English
Abstract
A development program to increase erosion resistance, extend life, reduce component cost and increase power to weight ratio through the use of a ceramic turbine nozzle section in gas turbine engines is described. Results of engine simulator tests of an all-ceramic nozzle constructed with special relaxing high temperature adhesives are presented.
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Citation
Jordan, F., Napier, J., Metcalfe, A., and Duffy, T., "Application of Ceramics to a Radial Inflow Gas Turbine," SAE Technical Paper 770342, 1977, https://doi.org/10.4271/770342.Also In
References
- Shoemaker H. E. “Techniques for Reducing Sand and Dust Erosion in Small Gas Turbine Engines,” Army Aviation Systems Command August 1970
- “Army Product Improvement Program,” Solar Engineering Report T-4287 June 1970
- Shoemaker H. E. Shumate C. P. “Techniques for Reducing Sand and Dust Erosion” SAE 700706 Sept. 1970
- Beck R. J. “Evaluation of Ceramics for Small Gas Turbine Engines,” SAE 740239 March 1974
- Mumfor S. E. Booker C. R. “Testing of Ceramic Stator Vanes to 2500°F (1371°C),”
- Sanders S. A. Probst H. B. “Behavior of Ceramics at 1200°C in a Simulated Gas Turbine Environment,” SAE 740240
- Lumby R. J. et al. “The Development of Silicon Nitride to Achieve Higher Inlet Temperatures in Land Based Gas Turbines,” SAE 720170