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Electronic Engine Condition Analysis System
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English
Abstract
A new systems approach has been developed and applied to achieve the inspection, diagnosis, and prognosis of gas turbine engine health by electronic means. The approach combines the power of the special purpose digital computer together with advanced engine fault isolation techniques to achieve a complete operational and maintenance interface. System elements are described and typical examples discussed. Practical applications of the system to several engine models have been made with favorable results.
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Citation
Moses, H., "Electronic Engine Condition Analysis System," SAE Technical Paper 710448, 1971, https://doi.org/10.4271/710448.Also In
References
- Allison J.W. Tracy R.F. “Resume of Current Experience Using Flight Data for Performance Monitoring of Gas Turbine Engines.” Flight Operations Engineering/Pratt and Whitney Aircraft, Report No. 29 October 1969
- Moses H.J. “Computerized Airborne Integrated Data Systems.” Paper No. 70-935 AIAA Second Aircraft Design and Operations Meeting Los Angeles July 1970
- Urban L.A. “Gas Turbine Engine Parameter Interrelationships.” Windsor Locks, Connecticut Hamilton Standard Division of United Aircraft Corporation 1969
- Young F.L. Bays W.J. Reynolds, E.C. Jr. “Measurement and Diagnosis of Jet Engine Vibration.” Paper No. 670870 SAE Aeronautic and Space Engineering and Manufacturing Meeting Los Angeles October 1967