Multistage axial-flow turbines : design and performance analysis

Detalhes bibliográficos
Autor(a) principal: Rafael Miguelangel Ascanio Vegas
Data de Publicação: 2012
Tipo de documento: Dissertação
Idioma: eng
Título da fonte: Biblioteca Digital de Teses e Dissertações do ITA
Texto Completo: http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2099
Resumo: Plans for developing turbines in Brazil were present on the conception of CTA six decades ago. In this manner highly specialized work teams is needed to carry out such activity. The Center for Reference on Gas Turbine group has been contributing to research activities at CTA taking account of the study of gas turbines both aeronautical and industrial. In order to complement the group capability and study more complex turbine applications, it is a topic of interest to study steam turbines. Taking advantage from the experience gathered at CRTG, design and performance analysis approaches for axial gas turbines were applied to steam turbines, adjusting the models for working with superheated steam using a loss model for axial turbomachinery to estimate the total pressure loss into the turbine cascade. Such models were implemented in a computer code written in FORTRAN, disposed for reading the design requirements or the conditions for the performance analysis, making the corresponding calculation and reporting the results. It was performed a verification on the results from the design routine, comparing them with data from a commercial program for axial turbine simulation and the used such results to assess its performance at off-design conditions. A case study was conducted regarding a multistage steam turbine working in a combined cycle with a gas turbine. From the energy of the gas turbine exhaust, a three stages steam turbine of 0.5 MW of power was designed. Later, with additional energy generated in the boiler in order to produce more steam, the power capacity of the steam turbine was increased. The results reported from both routines were qualitative consistent to what it was expected a turbine design and off-design performance analysis could be.
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spelling Multistage axial-flow turbines : design and performance analysisTurbinas axiaisTurbinas a vaporAvaliação de desempenhoSimulação computadorizadaEngenharia mecânicaPlans for developing turbines in Brazil were present on the conception of CTA six decades ago. In this manner highly specialized work teams is needed to carry out such activity. The Center for Reference on Gas Turbine group has been contributing to research activities at CTA taking account of the study of gas turbines both aeronautical and industrial. In order to complement the group capability and study more complex turbine applications, it is a topic of interest to study steam turbines. Taking advantage from the experience gathered at CRTG, design and performance analysis approaches for axial gas turbines were applied to steam turbines, adjusting the models for working with superheated steam using a loss model for axial turbomachinery to estimate the total pressure loss into the turbine cascade. Such models were implemented in a computer code written in FORTRAN, disposed for reading the design requirements or the conditions for the performance analysis, making the corresponding calculation and reporting the results. It was performed a verification on the results from the design routine, comparing them with data from a commercial program for axial turbine simulation and the used such results to assess its performance at off-design conditions. A case study was conducted regarding a multistage steam turbine working in a combined cycle with a gas turbine. From the energy of the gas turbine exhaust, a three stages steam turbine of 0.5 MW of power was designed. Later, with additional energy generated in the boiler in order to produce more steam, the power capacity of the steam turbine was increased. The results reported from both routines were qualitative consistent to what it was expected a turbine design and off-design performance analysis could be.Instituto Tecnológico de AeronáuticaJoão Roberto BarbosaRafael Miguelangel Ascanio Vegas2012-06-28info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/masterThesishttp://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2099reponame:Biblioteca Digital de Teses e Dissertações do ITAinstname:Instituto Tecnológico de Aeronáuticainstacron:ITAenginfo:eu-repo/semantics/openAccessapplication/pdf2019-02-02T14:03:48Zoai:agregador.ibict.br.BDTD_ITA:oai:ita.br:2099http://oai.bdtd.ibict.br/requestopendoar:null2020-05-28 19:38:11.476Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáuticatrue
dc.title.none.fl_str_mv Multistage axial-flow turbines : design and performance analysis
title Multistage axial-flow turbines : design and performance analysis
spellingShingle Multistage axial-flow turbines : design and performance analysis
Rafael Miguelangel Ascanio Vegas
Turbinas axiais
Turbinas a vapor
Avaliação de desempenho
Simulação computadorizada
Engenharia mecânica
title_short Multistage axial-flow turbines : design and performance analysis
title_full Multistage axial-flow turbines : design and performance analysis
title_fullStr Multistage axial-flow turbines : design and performance analysis
title_full_unstemmed Multistage axial-flow turbines : design and performance analysis
title_sort Multistage axial-flow turbines : design and performance analysis
author Rafael Miguelangel Ascanio Vegas
author_facet Rafael Miguelangel Ascanio Vegas
author_role author
dc.contributor.none.fl_str_mv João Roberto Barbosa
dc.contributor.author.fl_str_mv Rafael Miguelangel Ascanio Vegas
dc.subject.por.fl_str_mv Turbinas axiais
Turbinas a vapor
Avaliação de desempenho
Simulação computadorizada
Engenharia mecânica
topic Turbinas axiais
Turbinas a vapor
Avaliação de desempenho
Simulação computadorizada
Engenharia mecânica
dc.description.none.fl_txt_mv Plans for developing turbines in Brazil were present on the conception of CTA six decades ago. In this manner highly specialized work teams is needed to carry out such activity. The Center for Reference on Gas Turbine group has been contributing to research activities at CTA taking account of the study of gas turbines both aeronautical and industrial. In order to complement the group capability and study more complex turbine applications, it is a topic of interest to study steam turbines. Taking advantage from the experience gathered at CRTG, design and performance analysis approaches for axial gas turbines were applied to steam turbines, adjusting the models for working with superheated steam using a loss model for axial turbomachinery to estimate the total pressure loss into the turbine cascade. Such models were implemented in a computer code written in FORTRAN, disposed for reading the design requirements or the conditions for the performance analysis, making the corresponding calculation and reporting the results. It was performed a verification on the results from the design routine, comparing them with data from a commercial program for axial turbine simulation and the used such results to assess its performance at off-design conditions. A case study was conducted regarding a multistage steam turbine working in a combined cycle with a gas turbine. From the energy of the gas turbine exhaust, a three stages steam turbine of 0.5 MW of power was designed. Later, with additional energy generated in the boiler in order to produce more steam, the power capacity of the steam turbine was increased. The results reported from both routines were qualitative consistent to what it was expected a turbine design and off-design performance analysis could be.
description Plans for developing turbines in Brazil were present on the conception of CTA six decades ago. In this manner highly specialized work teams is needed to carry out such activity. The Center for Reference on Gas Turbine group has been contributing to research activities at CTA taking account of the study of gas turbines both aeronautical and industrial. In order to complement the group capability and study more complex turbine applications, it is a topic of interest to study steam turbines. Taking advantage from the experience gathered at CRTG, design and performance analysis approaches for axial gas turbines were applied to steam turbines, adjusting the models for working with superheated steam using a loss model for axial turbomachinery to estimate the total pressure loss into the turbine cascade. Such models were implemented in a computer code written in FORTRAN, disposed for reading the design requirements or the conditions for the performance analysis, making the corresponding calculation and reporting the results. It was performed a verification on the results from the design routine, comparing them with data from a commercial program for axial turbine simulation and the used such results to assess its performance at off-design conditions. A case study was conducted regarding a multistage steam turbine working in a combined cycle with a gas turbine. From the energy of the gas turbine exhaust, a three stages steam turbine of 0.5 MW of power was designed. Later, with additional energy generated in the boiler in order to produce more steam, the power capacity of the steam turbine was increased. The results reported from both routines were qualitative consistent to what it was expected a turbine design and off-design performance analysis could be.
publishDate 2012
dc.date.none.fl_str_mv 2012-06-28
dc.type.driver.fl_str_mv info:eu-repo/semantics/publishedVersion
info:eu-repo/semantics/masterThesis
status_str publishedVersion
format masterThesis
dc.identifier.uri.fl_str_mv http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2099
url http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2099
dc.language.iso.fl_str_mv eng
language eng
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv application/pdf
dc.publisher.none.fl_str_mv Instituto Tecnológico de Aeronáutica
publisher.none.fl_str_mv Instituto Tecnológico de Aeronáutica
dc.source.none.fl_str_mv reponame:Biblioteca Digital de Teses e Dissertações do ITA
instname:Instituto Tecnológico de Aeronáutica
instacron:ITA
reponame_str Biblioteca Digital de Teses e Dissertações do ITA
collection Biblioteca Digital de Teses e Dissertações do ITA
instname_str Instituto Tecnológico de Aeronáutica
instacron_str ITA
institution ITA
repository.name.fl_str_mv Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáutica
repository.mail.fl_str_mv
subject_por_txtF_mv Turbinas axiais
Turbinas a vapor
Avaliação de desempenho
Simulação computadorizada
Engenharia mecânica
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