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Implementation of an Engine Condition Monitoring tool for Airbus Aircraft Aerospace Engineering PDF

102 Pages·2015·14.45 MB·English
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Preview Implementation of an Engine Condition Monitoring tool for Airbus Aircraft Aerospace Engineering

Implementation of an Engine Condition Monitoring tool for Airbus Aircraft Sérgio da Cruz Ribeiro Thesis to obtain the Master of Science Degree in Aerospace Engineering Supervisors: Prof. António José Nobre Martins Aguiar Eng. Hélder António Silva Mendes Examination Committee Chairperson: Prof. Fernando José Parracho Lau Supervisor: Prof. António José Nobre Martins Aguiar Member of the Committee: Prof. Pedro da Graça Tavares Alvares Serrão June 2015 ii “If i have seen further than others, it is by standing upon the shoulders of giants.” Sir Isaac Newton iii Acknowledgments IwouldlikethankProf. Anto´nioJose´ NobreMartinsAguiarfortheopportunityofdevelopingthecurrent dissertation at TAP, which was a truly an enriching experience, and for all the support and hours spent reviewing the work developed. I would also like to give a special thanks and a word of appreciation to Eng. He´lder Anto´nio Silva Mendes for all the guidance, patience, sympathy and without whom I would not have achieved the same results.The friendships made during my internship, could not go without mention, thank you Andre´ Simo˜es, Lu´ıs Vargas, Tiago Duarte and Pedro Soares. I would also like to mentionthecontributionsfromAlexandreGarrinhasandDulceMontez. To all my college friends for all the support and shared experiences. A special thanks to Joa˜o Silva for thetimespentreviewingsomematerialsandkeepingmemotivated. Tomyfamilyfortheunconditionalloveandsupport. Last,butnotleast,toCarolinaOliveiraforallthesupportandsacrificesmade. iv Resumo Com o crescimento da indu´stria aerona´utica o transporte ae´reo tornou-se acess´ıvel a uma populac¸a˜o mais vasta o que tem levantado crescente preocupac¸a˜o com a seguranc¸a deste sector. Para ale´m disso,devidoa`smargensdelucroreduzidasea` intensacompetic¸a˜ocaracter´ısticasdestemercado,as companhias ae´reas tem procurado medidas que melhorem a eficieˆncia dos seus processos operacionais de modo a reduzir custos e trazer benef´ıcios a n´ıvel ambiental. O crescimento e desenvolvimentodaindu´striaimplicatambe´mumaumentonaquantidadededadosdevoodispon´ıveis paraserutilizadosnarealizac¸a˜odeestudoscomavistaamelhorartodaaoperac¸a˜o. Osdadosdevoo sa˜o recolhidos atrave´s de sistemas a bordo da aeronave, sendo posteriormente descodificados e armazenados na estac¸a˜o de dados de voo. Com estes dados podem ser conduzidas ana´lises estat´ısticas como a que e´ realizada pela aplicac¸a˜o desenvolvida durante a presente dissertac¸a˜o. A ferramenta desenvolvida permite analisar a evoluc¸a˜o no tempo da performance dos motores e identificar situac¸o˜es que necessitem de intervenc¸a˜o ou que possam indicar mau funcionamento de algum componente. Foi desenvolvido um algoritmo para optimizar o tratamento de dados assim como uma aplicac¸a˜o interactiva que permite uma ana´lise mais dinaˆmica da evoluc¸a˜o dos paraˆmetros de performance dos motores. Esta aplicac¸a˜o online esta´ acess´ıvel a qualquer altura pondo a` disposic¸a˜o dosva´riosdepartamentosdaempresainformac¸a˜oquedeoutraformaseriamaisdif´ıcildeobter. Palavras-chave: Dados de voo, Engine Condition Monitoring, Evoluc¸a˜o de performance, Correcc¸a˜odeparaˆmetrosdeturbinasaga´s,Pontosdeestabilidade. v Abstract The growth of the aviation industry implies its accessibility to a broader population and this raises particular concerns about air transport safety. Also, due to the low profit margins and intense competitivenessofthismarket,airlinecompaniesarefocusingonmakingtheiroperationmoreefficient in order to reduce costs and become more environmentally friendly. The growth and development of the industry also means an increase in the existing on-flight data available to perform studies with the objective of improving existing processes. Data is collected through systems aboard the aircraft, being posteriorlydecodedandstoredattheFDdepartment. Statisticalanalysis,suchastheonedonebythe applicationdevelopedduringthecurrentdissertation,canbeperformedusingthisdata. Thedeveloped tool allows the analysis of engine performance parameters through time and identifies situations that require intervention or may indicate malfunction of some engine component. An algorithm that optimizes data processing in terms of time and computational resources required was also developed, aswellasaninteractiveapplicationthatallowsadynamicanalysisoftheevolutionofsaidparameters. Thisisanonlineapplicationthatcanbeaccessedanywhereneeded,makingavailableinformationthat wouldotherwisebedifficulttoobtain. Keywords: Flight Data, , Engine Condition Monitoring, Performance Trends, Corrected Gas TurbineParameters,StabilityPoints. vi Contents Acknowledgments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . iv Resumo . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . v Abstract . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . vi ListofTables . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . xi ListofFigures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . xv Nomenclature . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . xvii Glossary xviii Glossary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . xxi 1 Introduction 1 1.1 Motivation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 1.2 Objectives . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 1.3 Structureofthedocument . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 2 EngineConditionMonitoring 4 2.1 Condition-basedMaintenance. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 2.2 TurbofanEngine . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 2.3 DataSourcing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7 2.3.1 RecordinganddisplayofData . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7 vii 2.3.2 SystemsforDataCollection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12 2.4 TrendMonitoring . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13 2.4.1 TrendMonitoringParameters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14 2.4.2 EGTMargin . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15 2.4.3 CruisePerformanceTrending . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18 2.4.4 Baselinemodelandtrendmonitoring. . . . . . . . . . . . . . . . . . . . . . . . . . 18 2.4.5 Performancedeteriorationdetection . . . . . . . . . . . . . . . . . . . . . . . . . . 19 2.5 EngineParameterCorrections . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21 2.6 Conclusion . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 24 3 TAPPortugal 25 3.1 TheFleet . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 26 3.2 FlightDataDepartmentatTAP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 26 3.2.1 AnalysisGroundStation(AGS) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27 3.2.2 FlightPhaseIdentification . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 29 3.2.3 DataExporting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 30 3.3 Conclusion . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 31 4 DevelopinganECMTool 32 4.1 ECMandcruisetrendanalysisconsiderations. . . . . . . . . . . . . . . . . . . . . . . . . 32 4.1.1 StabilityPointsearchcriteria . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 33 4.1.2 ParameterFiltering . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 35 4.1.3 FixedWindowandGlidingWindowstableframesearch . . . . . . . . . . . . . . . 36 4.1.4 QualityNumber . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 37 4.1.5 Applicationofparametercorrections . . . . . . . . . . . . . . . . . . . . . . . . . . 37 viii 4.1.6 EngineBleedanditseffects . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 39 4.1.7 BaselineDefinition . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 41 4.1.8 TrendMonitoring . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 42 4.2 Algorithmforin-flightperformanceanalysis . . . . . . . . . . . . . . . . . . . . . . . . . . 43 4.3 Improvementsdeveloped . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 47 4.3.1 LoadingFlightsfromtheFlightDB . . . . . . . . . . . . . . . . . . . . . . . . . . . 48 4.3.2 Optimizationofdataprocessing . . . . . . . . . . . . . . . . . . . . . . . . . . . . 49 4.3.3 BasicConditionsandstabilitycriteriadefinition . . . . . . . . . . . . . . . . . . . . 51 4.3.4 MinimumandnormalPackFlowBaselines . . . . . . . . . . . . . . . . . . . . . . 52 4.3.5 DevelopmentofaWeb-basedUserInterface . . . . . . . . . . . . . . . . . . . . . 53 4.4 Conclusion . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 55 5 Results 56 5.1 Validatingthealgorithm . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 56 5.2 CaseStudy-HPTCCvalvefailure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61 5.3 Conclusion . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 65 6 Conclusions 66 6.1 Achievements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 66 6.2 FutureWork. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 67 Bibliography 70 A ExportedParameters 71 B PackFlowSelection 73 C BaselinesFirstanalysis 74 ix D BaselinesSecondanalysis 76 E BaselinesCaseStudy 78 F FlightPhaseIdentification 80 x

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4.5 Converged Stability Criteria for Airbus A330 [3] 45 .. EFIS Electronic Flight Instrument System. 11. EGT Exhaust Gas
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