The first LM2500 “second generation” gas generator was placed in gas transmission service in December 1970. Derived from the TF39 and CF6 engines, advanced aircraft power plants in service since 1965 for the Air Force C5A transport and the new wide-bodied commercial airlines, the LM2500 has accumulated over 315,000 operational hours in gas transmission service. During this period, the LM2500 has demonstrated the capability to exceed 45,000 hr without major overhaul. Demonstrated reliability and availability have exceeded 99 percent. This paper describes the evolution of the LM2500 from its aircraft progenitors in order to illustrate the effect of the initial design concepts embodied upon reliability, availability, maintainability and life cycle-costs. Included is a discussion of the overall influence of initial acquisition, fuel, maintenance, and repair costs and their effects on system availability and overall life-cycle cost.
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ASME 1979 International Gas Turbine Conference and Exhibit and Solar Energy Conference
March 12–15, 1979
San Diego, California, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7967-2
PROCEEDINGS PAPER
The “Second Generation” LM2500: An Example of High Level of Reliability/Availability With Low Life-Cycle Costs
R. B. Spector
R. B. Spector
General Electric Co., Evendale, OH
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R. B. Spector
General Electric Co., Evendale, OH
Paper No:
79-GT-79, V01AT01A079; 9 pages
Published Online:
April 24, 2015
Citation
Spector, RB. "The “Second Generation” LM2500: An Example of High Level of Reliability/Availability With Low Life-Cycle Costs." Proceedings of the ASME 1979 International Gas Turbine Conference and Exhibit and Solar Energy Conference. Volume 1A: Gas Turbines. San Diego, California, USA. March 12–15, 1979. V01AT01A079. ASME. https://doi.org/10.1115/79-GT-79
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