An Overview of the NASA Aviation Safety Program Propulsion Health Monitoring Element

Abstract : The NASA Aviation Safety Program (AvSP) has been initiated with aggressive goals to reduce the civil aviation accident rate. To meet these goals, several technology investment areas have been identified including a sub-element in propulsion health monitoring (PHM). Specific AvSP PHM objectives are to develop and validate propulsion system health monitoring technologies designed to prevent engine malfunctions from occurring in flight, and to mitigate detrimental effects in the event an in-flight malfunction does occur. A review of available propulsion system safety information was conducted to help prioritize PHM areas to focus on under the AvSP. It is noted that when a propulsion malfunction is involved in an aviation accident or incident, it is often a contributing factor rather than the sole cause for the event. Challenging aspects of the development and implementation of PHM technology such as cost, weight, robustness, and reliability are discussed. Specific technology plans are overviewed including vibration diagnostics, model-based controls and diagnostics, advanced instrumentation, and general aviation propulsion system health monitoring technology. Propulsion system health monitoring, in addition to engine design, inspection, maintenance, and pilot training and awareness, is intrinsic to enhancing aviation propulsion system safety.

[1]  Detection and measurement of fatigue crack in HSLA steel with a dedicated ultrasonic pulse transmission method , 1997 .

[2]  David L. Doel,et al.  TEMPER - A gas-path analysis tool for commercial jet engines , 1992 .

[3]  Lisa C. Martin,et al.  Thin Film Sensors for Minimally-Intrusive Measurements in Harsh High Temperature Environment , 1998 .

[4]  Alan H. Epstein,et al.  Active Stabilization of Rotating Stall and Surge in a Transonic Single Stage Axial Compressor , 1997 .

[5]  Shrider Adibhatla,et al.  Evaluation of a nonlinear PSC algorithm on a variable cycle engine , 1993 .

[6]  Alan H. Epstein,et al.  Influence of compressor deterioration on engine dynamic behavior and transient stall-margin , 2000 .

[7]  Edward M. Greitzer,et al.  1997 Best Paper Award—Controls and Diagnostics Committee: Active Stabilization of Rotating Stall and Surge in a Transonic Single-Stage Axial Compressor , 1998 .

[8]  Louis A. Urban,et al.  Gas Path Analysis Applied to Turbine Engine Condition Monitoring , 1973 .

[9]  Andrew Green The development of engine health monitoring for gas turbine engine health and life management , 1998 .

[10]  James D. Paduano,et al.  Controls and Diagnostics Committee Best 1994 Paper Award: Modeling for Control of Rotating Stall in High-Speed Multistage Axial Compressors , 1996 .

[11]  David L. Doel,et al.  An Assessment of Weighted-Least-Squares-Based Gas Path Analysis , 1993 .

[12]  C Dupuy [Too much is too much]. , 1995, Soins. Psychiatrie.

[13]  G P Sallee,et al.  PROPULSION SYSTEM MALFUNCTION PLUS INAPPROPRIATE CREW RESPONSE (PSM+ICR). , 1999 .

[14]  Donald L. Simon,et al.  NASA aviation safety program: Aircraft Engine Health Management Data Mining Tools roadmap , 2000, SPIE Defense + Commercial Sensing.

[15]  James D. Paduano,et al.  Modeling for Control of Rotating Stall in High Speed Multi-Stage Axial Compressors , 1994 .

[16]  Jaiwon Shin The NASA Aviation Safety Program: Overview , 2000 .

[17]  Alan H. Epstein,et al.  Prestall Behavior of Several High-Speed Compressors , 1995 .

[18]  Scott Dahl,et al.  Smart coatings for in-situ monitoring of engine components , 1999, Smart Structures.

[19]  R. Luppold,et al.  Estimating in-flight engine performance variations using Kalman filter concepts , 1989 .

[20]  George W. Gallops,et al.  Real-Time Estimation of Gas Turbine Engine Damage Using a Control Based Kalman Filter Algorithm , 1991 .

[21]  Charles Huettner Partnership for Safety Research , 1998 .

[22]  Shrider Adibhatla,et al.  MODEL-BASED INTELLIGENT DIGITAL ENGINE CONTROL (MoBIDEC) , 1997 .

[23]  Allan J. Volponi,et al.  Mathematical Methods of Relative Engine Performance Diagnostics , 1992 .

[24]  John S. Orme,et al.  Subsonic flight test evaluation of a performance seeking control algorithm on an F-15 airplane , 1992 .

[25]  H.E.G. Powrie,et al.  Engine health monitoring: Towards total prognostics , 1999, 1999 IEEE Aerospace Conference. Proceedings (Cat. No.99TH8403).

[26]  F. Moore,et al.  A Theory of Post-Stall Transients in Axial Compression Systems: Part I—Development of Equations , 1986 .

[27]  Shrider Adibhatla,et al.  Intelligent Engine Control (IEC) , 1992 .