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USAF Application of Airborne Recorders for Propulsion Diagnostics
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 01, 1967 by SAE International in United States
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The United States Air Force is evaluating the application of an airborne analyzer and digital recording system to assess, diagnose, and predict turbojet engine health on an immediate and long-term basis.
This paper presents a brief discussion of the C-141 “Lead-the-Force” System, the C-5A Malfunction Detection, Analysis, and Recording Subsystem, and discusses in detail the Engine Analyzer System (EASY). The EASY discussion includes the design philosophy, hardware, test programs, computer programs, and test results.
CitationCarlson, R., "USAF Application of Airborne Recorders for Propulsion Diagnostics," SAE Technical Paper 670359, 1967, https://doi.org/10.4271/670359.
- Rumer W. I. “Turbojet Engine Analyzer System Study.” June 1963
- Douglass M. E. “Turbojet Engine Analyzer Design Study.” April 1963
- Douglass M. E. “Processing of Engine Data for Development of Turbojet Engine Analyzer.” August 1964
- Douglass M. E. “Processing of Engine Data for Development of Turbojet Engine Analyzer.” January 5 1965