2019
DOI: 10.1016/j.applthermaleng.2018.11.082
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Multi-objective optimization approach toward conceptual design of gas turbine combustor

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Cited by 31 publications
(17 citation statements)
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“…Observa-se, no interior da pá, que para maiores valores de vazão de resfriamento as solicitações térmicas da pá serão menores. Menores gradientes de temperatura na pá geram menos variações de propriedades no interior do material e evita níveis de dilatação distintos em uma mesma região, evitando assim possíveis trincas, fadiga térmica, deformações localizadas, dentre outros problemas, conforme constatados por Sahith et al (2018) e Ersayin e Ozgener (2015).…”
Section: Resultsunclassified
See 1 more Smart Citation
“…Observa-se, no interior da pá, que para maiores valores de vazão de resfriamento as solicitações térmicas da pá serão menores. Menores gradientes de temperatura na pá geram menos variações de propriedades no interior do material e evita níveis de dilatação distintos em uma mesma região, evitando assim possíveis trincas, fadiga térmica, deformações localizadas, dentre outros problemas, conforme constatados por Sahith et al (2018) e Ersayin e Ozgener (2015).…”
Section: Resultsunclassified
“…Foram utilizados os dados operacionais da turbina NASA Energy Efficient Engine GE-E3 (WENTONG et al, 2018;SABOOHI et al 2019;DAVIS e STEARNS, 1985;HALILA et al, 1982), conforme indicados na Tabela 1. Tal turbina há bastante tempo tem servido de base para cálculos termodinâmicos na área, dada a sua boa eficiência operacional.…”
Section: Metodologiaunclassified
“…Approach III: Reviewing the design studies and parametric studies in terms of the type and phase of the injected or added humidifier (water or vapor); addition of different diluents to the combustion process; comparing addition of humidifier to the fuel side or oxidizer (air) side; the point at where the humidifier is injected or added (combustion chamber, compressor, or gas turbine); type of flame or combustion (premixed, partially premixed, or non-premixed); and the type of fuel used in the combustion process. Approach IV: Providing the significant design goals (performance parameters), even under undesirable conditions should be monitored [3]. Parameters such as maximum efficiency, lowest pressure loss, minimum emission, suitable outlet temperature distribution, combustion and flame stability, and reliability.…”
Section: Introductionmentioning
confidence: 99%
“…Rogero and Rubini [3], for example, employed an aerothermal network model and an evolutionary optimization algorithm to optimize for 22 performance targets while minimizing cooling flow and NOx emissions. Wyse et al [4] employed a similar network model of a combustion system to minimise NOx and CO through a Tabu search while, more recently, Saboohi et al [5] employed a chemical network model within a multi-objective optimization attempting to also reduce NOx and CO.…”
Section: Introductionmentioning
confidence: 99%