Deep learning-based forecasting modeling of micro gas turbine performance projection: An experimental approach

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Performance forecasting of aeroengines is crucial for achieving better operational efficiency, ensuring safety, reducing costs, and minimizing environmental impact in the aviation industry. It enables engineers and researchers to make informed decisions, leading to advancements in technology and the overall evolution of aviation. This study is focused on the effects of flight conditions on the performance of a turbojet, which in consequence affects the environmental aspect of operation. By investigating the relationships between aeroengine efficiency and performance indicators such as thrust, shaft speed, and exhaust gas temperature (EGT), and flight characteristics expressed in terms of environmental and operational conditions, the study seeks to elucidate these connections. The article's significance lies in its successful application of Long Short-Term Memory (LSTM) networks to predict thrust, shaft speed, and EGT variations in turbojet engines under varying flight conditions. Experimental data from a turbojet test bench is processed with deep learning, specifically LSTM recurrent neural networks that are developed based on Matrix Laboratory (MATLAB). The model inputs are free stream air speed, compressor inlet pressure, combustor inlet temperature, combustor inlet pressure, turbine inlet temperature, turbine inlet pressure, nozzle inlet pressure and fuel flow, and the outputs are thrust, shaft speed and EGT. Predicted thrust closely aligns with actual thrust values, though with minor discrepancies. Shaft speed predictions exhibit a similar trend, while EGT predictions showcase a comparable pattern with slight variations. Despite the prediction errors, a thorough evaluation of median values, box plots, and probability density functions confirms that the models effectively capture available information, though discrepancies may arise from measurement inaccuracies and initial engine conditions. These results show that it is possible to accurately predict turbojet performance using LSTM recurrent neural network. This research paves the way for enhanced aeroengine performance prediction, particularly in scenarios requiring off-board or high-performance applications. © 2023 Elsevier Ltd

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AlanDeğerDil
dc.contributor.authorKilic, Ugur
dc.contributor.authorVillareal-Valderrama, Francisco
dc.contributor.authorAyar, Murat
dc.contributor.authorEkici, Selcuk
dc.contributor.authorAmezquita-Brooks, Luis
dc.contributor.authorKarakoc, T. Hikmet
dc.date.accessioned2026-10-18T20:26:36.598508570Z
dc.date.available2026-10-18T20:26:36.598508570Z
dc.date.issued2024
dc.description.abstractPerformance forecasting of aeroengines is crucial for achieving better operational efficiency, ensuring safety, reducing costs, and minimizing environmental impact in the aviation industry. It enables engineers and researchers to make informed decisions, leading to advancements in technology and the overall evolution of aviation. This study is focused on the effects of flight conditions on the performance of a turbojet, which in consequence affects the environmental aspect of operation. By investigating the relationships between aeroengine efficiency and performance indicators such as thrust, shaft speed, and exhaust gas temperature (EGT), and flight characteristics expressed in terms of environmental and operational conditions, the study seeks to elucidate these connections. The article's significance lies in its successful application of Long Short-Term Memory (LSTM) networks to predict thrust, shaft speed, and EGT variations in turbojet engines under varying flight conditions. Experimental data from a turbojet test bench is processed with deep learning, specifically LSTM recurrent neural networks that are developed based on Matrix Laboratory (MATLAB). The model inputs are free stream air speed, compressor inlet pressure, combustor inlet temperature, combustor inlet pressure, turbine inlet temperature, turbine inlet pressure, nozzle inlet pressure and fuel flow, and the outputs are thrust, shaft speed and EGT. Predicted thrust closely aligns with actual thrust values, though with minor discrepancies. Shaft speed predictions exhibit a similar trend, while EGT predictions showcase a comparable pattern with slight variations. Despite the prediction errors, a thorough evaluation of median values, box plots, and probability density functions confirms that the models effectively capture available information, though discrepancies may arise from measurement inaccuracies and initial engine conditions. These results show that it is possible to accurately predict turbojet performance using LSTM recurrent neural network. This research paves the way for enhanced aeroengine performance prediction, particularly in scenarios requiring off-board or high-performance applications. © 2023 Elsevier Ltd
dc.identifier.doi10.1016/j.engappai.2023.107769
dc.identifier.eissn1873-6769
dc.identifier.issn0952-1976
dc.identifier.scopus2-s2.0-85181071078
dc.identifier.startpage107769
dc.identifier.urihttps://rdlopen.rawdatalibrary.net/r/ebyu/11576
dc.identifier.volume130
dc.identifier.wosWOS:001149719500001
dc.language.isoen
dc.publisherElsevier Ltd
dc.relation.ispartofEngineering Applications of Artificial Intelligence
dc.rightsinfo:eu-repo/semantics/openAccess
dc.subjectGas turbine engine
dc.subjectLearning algorithm
dc.subjectLong short-term memory (LSTM)
dc.subjectPerformance parameters
dc.subjectPrediction
dc.subjectTurbojet engine
dc.subjectAircraft engines
dc.subjectBrain
dc.subjectCombustors
dc.subjectEfficiency
dc.subjectEnvironmental impact
dc.subjectGas turbines
dc.subjectLearning algorithms
dc.subjectLearning systems
dc.subjectLong short-term memory
dc.subjectProbability density function
dc.subjectAero-engine
dc.subjectExhaust gas temperatures
dc.subjectFlight conditions
dc.subjectForecasting models
dc.subjectInlet pressures
dc.subjectPerformance
dc.subjectShaft speed
dc.subjectForecasting
dc.titleDeep learning-based forecasting modeling of micro gas turbine performance projection: An experimental approach
dc.typeArticle
dspace.entity.typePublication
rdl.citation.scopus55
rdl.citation.wos48
rdl.source.indexSCOPUS
rdl.source.indexWOS
rdl.wos.indexScience Citation Index Expanded (SCI-EXPANDED)