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Beryllium for Gas Turbines
ISSN: 0148-7191, e-ISSN: 2688-3627
Published January 01, 1964 by SAE International in United States
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Beryllium component manufacturing technology and some test results from a recent Brush-General Electric cooperative design evaluation program are presented, along with the design justification for continued effort to develop beryllium into a reliable material for gas turbine components. The data from this program is generally encouraging, but two major problem areas of impact and corrosion were identified. Recommendations are made on specific areas requiring additional effort before the material can go into production in gas turbines.
CitationKing, D., Conliffe, C., and Marble, J., "Beryllium for Gas Turbines," SAE Technical Paper 640388, 1964, https://doi.org/10.4271/640388.
- Lockheed Missiles and Space Division, Strength, Efficiency, and Design Data for Beryllium Structures, by Crawford E. F. and Burns, A. B. ASD TR 61–692, February, 1962.
- The Brush Beryllium Company, The Mechanical Properties of Beryllium, by King, D. B. presented at UCLA during the course “Beryllium, Its Properties and Applications”, March 4–8, 1963.