Real-Time Gas Turbine Model for Performance Simulations

Detalhes bibliográficos
Autor(a) principal: Gazzetta Junior,Henrique
Data de Publicação: 2017
Outros Autores: Bringhenti,Cleverson, Barbosa,João Roberto, Tomita,Jesuíno Takachi
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Journal of Aerospace Technology and Management (Online)
Texto Completo: http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462017000300346
Resumo: ABSTRACT Industry and universities around the world invest time and money to develop digital computer programs to predict gas turbine performance. This study aims to demonstrate a brand new digital model developed with the ability to simulate gas turbine real time high fidelity performance. The model herein described run faster than 30ms per point, which is compatible with a high-definition video refresh rate: 30 frames per second. This user-friendly model, built in Visual Basic in modular structure, can be easily configured to simulate almost all the existing gas turbine architectures (single, 2 or 3 shaft engines mixed or unmixed flows). In addition, its real time capability enables simulations with the pilot in the loop at earlier design phases when their feedback may lead to design changes for improvements or corrections. In this paper, besides the model description, it is presented the model run time capability as well as a comparison of the simulated performance with a commercial gas turbine tool for single, 2 and 3 shaft engine architecture.
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spelling Real-Time Gas Turbine Model for Performance SimulationsPropulsionGas turbinesAircraft enginesPerformanceComputer simulationABSTRACT Industry and universities around the world invest time and money to develop digital computer programs to predict gas turbine performance. This study aims to demonstrate a brand new digital model developed with the ability to simulate gas turbine real time high fidelity performance. The model herein described run faster than 30ms per point, which is compatible with a high-definition video refresh rate: 30 frames per second. This user-friendly model, built in Visual Basic in modular structure, can be easily configured to simulate almost all the existing gas turbine architectures (single, 2 or 3 shaft engines mixed or unmixed flows). In addition, its real time capability enables simulations with the pilot in the loop at earlier design phases when their feedback may lead to design changes for improvements or corrections. In this paper, besides the model description, it is presented the model run time capability as well as a comparison of the simulated performance with a commercial gas turbine tool for single, 2 and 3 shaft engine architecture.Departamento de Ciência e Tecnologia Aeroespacial2017-09-01info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersiontext/htmlhttp://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462017000300346Journal of Aerospace Technology and Management v.9 n.3 2017reponame:Journal of Aerospace Technology and Management (Online)instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)instacron:DCTA10.5028/jatm.v9i3.693info:eu-repo/semantics/openAccessGazzetta Junior,HenriqueBringhenti,CleversonBarbosa,João RobertoTomita,Jesuíno Takachieng2017-08-18T00:00:00Zoai:scielo:S2175-91462017000300346Revistahttp://www.jatm.com.br/ONGhttps://old.scielo.br/oai/scielo-oai.php||secretary@jatm.com.br2175-91461984-9648opendoar:2017-08-18T00:00Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)false
dc.title.none.fl_str_mv Real-Time Gas Turbine Model for Performance Simulations
title Real-Time Gas Turbine Model for Performance Simulations
spellingShingle Real-Time Gas Turbine Model for Performance Simulations
Gazzetta Junior,Henrique
Propulsion
Gas turbines
Aircraft engines
Performance
Computer simulation
title_short Real-Time Gas Turbine Model for Performance Simulations
title_full Real-Time Gas Turbine Model for Performance Simulations
title_fullStr Real-Time Gas Turbine Model for Performance Simulations
title_full_unstemmed Real-Time Gas Turbine Model for Performance Simulations
title_sort Real-Time Gas Turbine Model for Performance Simulations
author Gazzetta Junior,Henrique
author_facet Gazzetta Junior,Henrique
Bringhenti,Cleverson
Barbosa,João Roberto
Tomita,Jesuíno Takachi
author_role author
author2 Bringhenti,Cleverson
Barbosa,João Roberto
Tomita,Jesuíno Takachi
author2_role author
author
author
dc.contributor.author.fl_str_mv Gazzetta Junior,Henrique
Bringhenti,Cleverson
Barbosa,João Roberto
Tomita,Jesuíno Takachi
dc.subject.por.fl_str_mv Propulsion
Gas turbines
Aircraft engines
Performance
Computer simulation
topic Propulsion
Gas turbines
Aircraft engines
Performance
Computer simulation
description ABSTRACT Industry and universities around the world invest time and money to develop digital computer programs to predict gas turbine performance. This study aims to demonstrate a brand new digital model developed with the ability to simulate gas turbine real time high fidelity performance. The model herein described run faster than 30ms per point, which is compatible with a high-definition video refresh rate: 30 frames per second. This user-friendly model, built in Visual Basic in modular structure, can be easily configured to simulate almost all the existing gas turbine architectures (single, 2 or 3 shaft engines mixed or unmixed flows). In addition, its real time capability enables simulations with the pilot in the loop at earlier design phases when their feedback may lead to design changes for improvements or corrections. In this paper, besides the model description, it is presented the model run time capability as well as a comparison of the simulated performance with a commercial gas turbine tool for single, 2 and 3 shaft engine architecture.
publishDate 2017
dc.date.none.fl_str_mv 2017-09-01
dc.type.driver.fl_str_mv info:eu-repo/semantics/article
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
format article
status_str publishedVersion
dc.identifier.uri.fl_str_mv http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462017000300346
url http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462017000300346
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv 10.5028/jatm.v9i3.693
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv text/html
dc.publisher.none.fl_str_mv Departamento de Ciência e Tecnologia Aeroespacial
publisher.none.fl_str_mv Departamento de Ciência e Tecnologia Aeroespacial
dc.source.none.fl_str_mv Journal of Aerospace Technology and Management v.9 n.3 2017
reponame:Journal of Aerospace Technology and Management (Online)
instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
instname_str Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron_str DCTA
institution DCTA
reponame_str Journal of Aerospace Technology and Management (Online)
collection Journal of Aerospace Technology and Management (Online)
repository.name.fl_str_mv Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
repository.mail.fl_str_mv ||secretary@jatm.com.br
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