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Grant: Collaborative Research and Development Grants

University of Waterloo

$80,000.00

Quickest change detection, statistical learning and nonlinear filtering of jet engine data

FY 2019-20

Summary
Modern jet engines are some of the most expensive components on an aircraft and are engineered to be extremely reliable at great cost (up to $25 million per engine). Yet they can still experience unexpected catastrophic failure, resulting in tragedy and loss of life. In order to monitor engine health and performance, each engine is equipped with about 100 sensors that measure engine performance parameters, from pressure and temperature of the engine gas path to vibration of the rotating components. The goals of the proposed collaborative research are to develop novel mathematical and statistical methods that exploit new sensing capabilities on engines for (i) constructing new anomaly-detection schemes and quickest-change detection algorithms; and (ii) discovering instability limits, thus preventing damage to engine components and lengthening their life-span. The research proposed here uses both model-based and data-driven theories to develop efficient numerical algorithms for quickest change detection, statistical learning and nonlinear filtering targeted at our specific problem.Theme 1, the proposed quickest-change detection, will be a vital procedure for engine performance monitoring. Once a change in an engine state has occurred, that change must be detected as soon as possible, while minimizing false detections. Theme 2 of the proposal focuses on the data-driven methods appropriate for data generated by jet engines. When no explicit dynamical model is available, system knowledge boils down to real-time measurements, possibly complemented by process history. Advances made in collaboration with the industry partner, TECSIS Corporation, will have a lasting impact on the Prognosis and Health Management (PHM) techniques for detecting abrupt changes or anomalies in gas turbine engines. The proposed data-centric methods will benefit the aerospace industry at large as well as open new research perspectives and domains that rely heavily on measurements for system monitoring and control.
Program
Collaborative Research and Development Grants
Location
Ontario, Canada
Recipient Type
Academia
Type
Grant
Source
NSERC's Awards Data

As published

Application id
543433-2019
Name nom
Namachchivaya, NavaratnamSri
Department département
Applied Mathematics
Organization id
33
Institution établissement
University of Waterloo
Province en
Ontario
Province fr
Ontario
Country en
CANADA
Country fr
CANADA
Fiscal year exercice financier
2019
Competition year année de concours
2019
Award amount
80000
Program id
CRDPJ
Program name en
Collaborative Research and Development Grants
Program name fr
Subventions de recherche et développement coopérative
Group en
RESEARCH PARTNERSHIPS
Group fr
PARTENARIATS DE RECHERCHE
Committee code
96
Committee name en
RPP Internal Decision Cttee
Committee name fr
Cté de décision interne - PPR
Area of application code
703
Area of application group en
Transportation systems and services
Area of application group fr
Services et systèmes de transport
Area of application en
Aerospace
Area of application fr
Aérospatial
Research subject code
2950
Research subject group en
Applied mathematics
Research subject group fr
Mathématiques appliquées
Research subject en
Applied mathematics
Research subject fr
Mathématiques appliquées
Installment
inst:1 - 1
Partie
1
Nb partie
1
Application title
Quickest change detection, statistical learning and nonlinear filtering of jet engine data
Keyword
NSERC
Application summary
Modern jet engines are some of the most expensive components on an aircraft and are engineered to be extremely reliable at great cost (up to $25 million per engine). Yet they can still experience unexpected catastrophic failure, resulting in tragedy and loss of life. In order to monitor engine health and performance, each engine is equipped with about 100 sensors that measure engine performance parameters, from pressure and temperature of the engine gas path to vibration of the rotating components. The goals of the proposed collaborative research are to develop novel mathematical and statistical methods that exploit new sensing capabilities on engines for (i) constructing new anomaly-detection schemes and quickest-change detection algorithms; and (ii) discovering instability limits, thus preventing damage to engine components and lengthening their life-span. The research proposed here uses both model-based and data-driven theories to develop efficient numerical algorithms for quickest change detection, statistical learning and nonlinear filtering targeted at our specific problem.Theme 1, the proposed quickest-change detection, will be a vital procedure for engine performance monitoring. Once a change in an engine state has occurred, that change must be detected as soon as possible, while minimizing false detections. Theme 2 of the proposal focuses on the data-driven methods appropriate for data generated by jet engines. When no explicit dynamical model is available, system knowledge boils down to real-time measurements, possibly complemented by process history. Advances made in collaboration with the industry partner, TECSIS Corporation, will have a lasting impact on the Prognosis and Health Management (PHM) techniques for detecting abrupt changes or anomalies in gas turbine engines. The proposed data-centric methods will benefit the aerospace industry at large as well as open new research perspectives and domains that rely heavily on measurements for system monitoring and control.