Engine Health Management in Safran Aircraft Engines

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Published Oct 3, 2016
Guillaume Bastard Jérome Lacaille Josselin Coupard Yacine Stouky

Abstract

Engine Health Management (EHM) is the up to date solution that is used by Aircraft Engine Manufacturers in order to maintain an engine operative through a reduction of operational events that impact its availability for end customers. The aim of EHM systems is to monitor and forecast the health status of an engine based on operational data in order to reduce the interruption of the clients operations and contribute to provide the best affordable maintenance of an engine. This paper describes the architecture of an EHM system designed to monitor Safran Aircraft Engines products.

How to Cite

Bastard, G., Lacaille, J., Coupard, J., & Stouky, Y. (2016). Engine Health Management in Safran Aircraft Engines. Annual Conference of the PHM Society, 8(1). https://doi.org/10.36001/phmconf.2016.v8i1.2523
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Keywords

PHM, EHM, Engine Health Management, Prognostic Health monitoring, IEHM

References
Bellas, A. et al., (2014). Anomaly detection based on confidence intervals using SOM with an application to Health Monitoring. In WSOM. Saxony (Germany).
Bense, W., (2013). Prognosis and Health Monitoring Systems for Aircraft Engines. In SAE. Montréal (Canada), pp. 1–9.
Flandrois, X. et al., (2009). Expertise Transfer and Automatic Failure Classification for the Engine Start Capability System. In AIAA InfoTech. Seattle (USA, Washington).
Griffaton, J., Picheral, J. & Tenenhaus, A., (2014). Enhanced Visual Analysis of Aircraft Engines Based on Spectrograms. In ISMA. Leuven (Belgium).
Klein, R., Rudyk, E. & Masad, E., (2011a). Decision and Fusion for Diagnostics of Mechanical Components. In PHM. Montreal (Canada): PHMSociety, pp. 1–9.
Klein, R., Rudyk, E. & Masad, E., (2011b). Methods for Diagnostics of Bearings in Non-Stationary Environment. In CM & MFPT. Cardiff (UK, Wales): BINDT, pp. 2–7.
Lacaille, J., (2009a). An Automatic Sensor Fault Detection and Correction Algorithm. In American Institute of Aeronautics and Astronautics (AIAA), ed. Aviation Technology, Integration, and Operations Conference (ATIO). Hilton Head (USA, South Carolina).
Lacaille, J., (2010a). Identification of Defects in an Aircraft Engine.
Lacaille, J., (2012). Monitoring of an Aircraft Engine for Anticipating Maintenance Operations. , p.45.
Lacaille, J., (2010b). Standardization of Data used for Monitoring an Aircraft Engine.
Lacaille, J., (2009b). Standardized Failure Signature for a Turbofan Engine. In IEEE Aerospace conference. Big Sky (USA, Montana): IEEE Aerospace society.
Lacaille, J. et al., (2014). Turbofan Engine Monitoring with Health State Identification and Remaining Useful Life Anticipation. Internationanl Journal on Condition Monitoring (IJCM), (1), pp.1–21.
Lacaille, J. & Côme, E., (2011). Visual Mining and Statistics for a Turbofan Engine Fleet. In IEEE Aerospace Conference. Big Sky (MT): IEEE.
Lacaille, J. & Djiki, R.N., (2009). Model Based Actuator Control Loop Fault Detection. In 8th European Conference on Turbomachinery: Fluid Dynamics and Thermodynamics, ETC 2009 - Conference Proceedings. Gratz (Austria), pp. 889–899.
Lacaille, J., Gouby, A. & Piol, O., (2013). Wear Prognostic on Turbofan Engines. In PHM. pp. 1–8.
Lacaille, J. & Nya Djiki, R., (2010). Detection of Anomalies in an Aircraft Engine.
Massé, J. et al., (2013). System PHM Algorithm Maturation. Chemical Enginering Transactions, 33, pp.283–288.
Rabenoro, T. et al., (2014a). A Methodology for the Diagnostic of Aircraft Engine Based on Indicators Aggregation. In ICDM. Saint Petersburg (Russia).
Rabenoro, T. et al., (2014b). Interpretable Aircraft Engine Diagnostic via Expert Indicator Aggregation. Transactions on Machine Learning, pp.1–21.
Section
Technical Research Papers

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