The paper describes the development and initial field experience with a new high efficiency 26,000/30,000 hp gas turbine. Exhaust heat from the power turbine was used to boost the installation thermal efficiency and provide icing protection for the inlet. Wherever possible, proven power turbine design concepts were combined with the advances of a “second generation” aircraft derivative gas generator to produce a reliable machine which was introduced with a minimum of development time. To assure field success, a special test facility was constructed and the unit subjected to a full load mechanical and performance test under simulated field condition.
Development and Field Experience of a New 29000 HP Gas Turbine
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Hubbard, JK, & Austin, C. "Development and Field Experience of a New 29000 HP Gas Turbine." Proceedings of the ASME 1980 International Gas Turbine Conference and Products Show. Volume 1B: General. New Orleans, Louisiana, USA. March 10–13, 1980. V01BT02A058. ASME. https://doi.org/10.1115/80-GT-152
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