Methods to establish component reliability have been in existence for nearly forty years. However, these methods have not been applied to gas turbine systems, because of a lack of consistent definitions and methodology. This paper describes a systematic procedure for calculating control-system reliability, which also can be extended to calculations for mechanical equipment. This is accomplished by a computerized model. Using the results of this model, practical methods and configurations are described to improve gas turbine reliability, such as: redundancy of essential components; quality of components; environmental factors; sensing devices and actuators; and circuits and logic design. The paper also compares these methods and the resulting reliability improvements in system cost and complexity.
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April 1989
Research Papers
Gas Turbine Reliability: How? How Much? Where?
H. D. Lenz,
H. D. Lenz
Cooper Industries, EN-Tronic Controls, Mount Vernon, OH 43050
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H. W. Hill, Jr.
H. W. Hill, Jr.
Ohio University, Electrical and Computer Engineering, Athens, OH 45701
Search for other works by this author on:
H. D. Lenz
Cooper Industries, EN-Tronic Controls, Mount Vernon, OH 43050
H. W. Hill, Jr.
Ohio University, Electrical and Computer Engineering, Athens, OH 45701
J. Eng. Gas Turbines Power. Apr 1989, 111(2): 232-236 (5 pages)
Published Online: April 1, 1989
Article history
Received:
September 15, 1987
Online:
October 15, 2009
Citation
Lenz, H. D., and Hill, H. W., Jr. (April 1, 1989). "Gas Turbine Reliability: How? How Much? Where?." ASME. J. Eng. Gas Turbines Power. April 1989; 111(2): 232–236. https://doi.org/10.1115/1.3240241
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