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Diseño y análisis numérico de una cámara de combustión anular

dc.contributor.authorMoreno Pacheco, Luis Alfonso
dc.contributor.authorSánchez López, Fernando
dc.contributor.authorBarbosa Saldaña, Juan Gabriel
dc.contributor.authorMartínez Trinidad, José
dc.contributor.authorCarpinteyro Pérez, Mario Alberto
dc.contributor.authorWong Ángel, Wilbert
dc.contributor.authorGarcía León, Ricardo Andrés
dc.coverage.spatialColombiaen_US
dc.date.accessioned2025-10-14T16:09:15Z
dc.date.available2025-10-14T16:09:15Z
dc.date.issued2024-07-16
dc.identifier.issn2311-5521en_US
dc.identifier.urihttps://repositorioinstitucional.ufpso.edu.co/xmlui/handle/20.500.14167/5733
dc.description.abstractEl diseño de una cámara de combustión para turbinas de gas se considera tanto una ciencia como un arte. Este estudio presenta una metodología integral para el diseño de una cámara de combustión anular adaptada a las condiciones de operación de un motor CFM-56, un motor turbofán de alta relación de derivación ampliamente utilizado. El proceso de diseño implicó el cálculo de los criterios básicos y las dimensiones de la carcasa, la camisa, el difusor y el remolino, seguido de un análisis de las secciones de enfriamiento de la camisa. Se realizaron simulaciones numéricas con el software NUMECA y la herramienta de mallado HEXPRESS para predecir el comportamiento y el rendimiento de la cámara de combustión, empleando el modelo de turbulencia κ-ε y el modelo de combustión Flamelet. Se utilizó metano como combustible y se realizaron simulaciones para tres ángulos de inyección de combustible: axial, 45° y 60°. Los resultados demuestran que la cámara de combustión está correctamente dimensionada y logra una combustión completa en todas las configuraciones. La relación de presión es de 0,96, superando los criterios mínimos de diseño. Además, las emisiones de hidrocarburos no quemados son nulas, mientras que los niveles de óxidos de nitrógeno y monóxido de carbono se encuentran por debajo de los límites regulatorios. Estos hallazgos validan la metodología de diseño propuesta, garantizando un rendimiento eficiente y respetuoso con el medio ambiente de la cámara de combustión.en_US
dc.language.isoengen_US
dc.relationhttps://www.mdpi.com/2311-5521/9/7/161en_US
dc.titleDiseño y análisis numérico de una cámara de combustión anularen_US
dc.title.translatedDesign and numerical analysis of an annular combustion chamberen_US
dc.contributor.cvlacRicardo Andrés García León [0001454975]en_US
dc.contributor.googlescholarLuis Alfonso Moreno Pacheco [YlG3DnQAAAAJ]en_US
dc.contributor.googlescholarFernando Sánchez López [1aLg7msAAAAJ]en_US
dc.contributor.googlescholarJuan Gabriel Barbosa Saldaña [LLYVUyQAAAAJ]en_US
dc.contributor.googlescholarRicardo Andrés García León [emeJT3sAAAAJ]en_US
dc.contributor.orcidLuis Alfonso Moreno Pacheco [0000-0001-8723-8836]en_US
dc.contributor.orcidJuan Gabriel Barbosa Saldaña [0000-0001-8590-8082]en_US
dc.contributor.orcidJosé Martínez Trinidad [0000-0002-5445-2681]en_US
dc.contributor.orcidWilbert Wong Ángel [0000-0003-3326-1744]en_US
dc.contributor.orcidRicardo Andrés García León [0000-0002-2734-1425]en_US
dc.contributor.researchgateRicardo Andrés García León [Ricardo-Garcia-Leon]
dc.contributor.scopusLuis Alfonso Moreno Pacheco [23976809300]en_US
dc.contributor.scopusFernando Sánchez López [57201820969]en_US
dc.contributor.scopusJuan Gabriel Barbosa Saldaña [22950055000]en_US
dc.contributor.scopusJosé Martínez Trinidad [8432492800]en_US
dc.contributor.scopusWilbert Wong Ángel [55081966900]en_US
dc.contributor.scopusRicardo Andrés García León [57192545232]en_US
dc.description.abstractenglishDesigning a combustion chamber for gas turbines is considered both a science and an art. This study presents a comprehensive methodology for designing an annular combustion chamber tailored to the operating conditions of a CFM-56 engine, a widely used high bypass ratio turbofan engine. The design process involved calculating the basic criteria and dimensions for the casing, liner, diffuser, and swirl, followed by an analysis of the cooling sections of the liner. Numerical simulations using NUMECA software and the HEXPRESS meshing tool were conducted to predict the combustion chamber’s behavior and performance, employing the κ-ε turbulence model and the Flamelet combustion model. Methane was used as the fuel, and simulations were performed for three fuel injection angles: axial, 45◦, and 60◦. Results demonstrate that the combustion chamber is properly dimensioned and achieves complete combustion for all configurations. The pressure ratio is 0.96, exceeding the minimum design criteria. Additionally, the emissions of unburned hydrocarbons are zero, while nitrogen oxides and carbon monoxide levels are below regulatory limits. These findings validate the proposed design methodology, ensuring efficient and environmentally compliant combustion chamber performance.en_US
dc.subject.proposalTurbinas de gasen_US
dc.subject.proposalCámara de combustión anularen_US
dc.subject.proposalDiseño del combustoren_US
dc.subject.proposalCFDen_US
dc.subject.proposalCFM56en_US
dc.subject.keywordsGas turbinesen_US
dc.subject.keywordsAnnular combustion chamberen_US
dc.subject.keywordsCombustor designen_US
dc.subject.keywordsCFDen_US
dc.subject.keywordsCFM56en_US
dc.publisher.facultyFacultad ingenieríasen_US
dc.type.redcolhttp://purl.org/redcol/resource_type/ARTen_US
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dc.identifier.DOIhttps://doi.org/10.3390/fluids9070161en_US


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