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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
dc.relation.referencesMattingly, J.D.; Heiser, W.H.; Pratt, D.T. Aircraft Engine Design, 2nd ed.; American Institute of Aeronautics and Astronautics, Inc.: San Francisco, CA, USA, 2002.en_US
dc.relation.referencesLefebvre, A.H.; Ballal, D.R. Gas Turbine Combustion Alternative Fuels and Emissions, 3rd ed.; CRC Press: Boca Raton, FL, USA, 2010.en_US
dc.relation.referencesWorth, N.A.; Dawson, J.R. Modal Dynamics of Self-Excited Azimuthal Instabilities in an Annular Combustion Chamber. Combust. Flame 2013, 160, 2476–2489. [CrossRef]en_US
dc.relation.referencesMark, C.P.; Selwyn, A. Design and Analysis of Annular Combustion Chamber of a Low Bypass Turbofan Engine in a Jet Trainer Aircraft. Propuls. Power Res. 2016, 5, 97–107. [CrossRef]en_US
dc.relation.referencesLivebardon, T.; Moreau, S.; Poinsot, T.; Bouty, E. Numerical Investigation of Combustion Noise Generation in a Full Annular Combustion Chamber. In Proceedings of the 21st AIAA/CEAS Aeroacoustics Conference, Dallas, TX, USA, 22–26 June 2015; AIAA AVIATION Forum. American Institute of Aeronautics and Astronautics: Reston, VA, USA, 2015.en_US
dc.relation.referencesWolf, P.; Balakrishnan, R.; Staffelbach, G.; Gicquel, L.Y.M.; Poinsot, T. Using LES to Study Reacting Flows and Instabilities in Annular Combustion Chambers. Flow Turbul. Combust. 2012, 88, 191–206. [CrossRef]en_US
dc.relation.referencesMeloni, R.; Ceccherini, G.; Michelassi, V.; Riccio, G. Analysis of the Self-Excited Dynamics of a Heavy-Duty Annular Combustion Chamber by Large-Eddy Simulation. J. Eng. Gas Turbines Power 2019, 141, 111016. [CrossRef]en_US
dc.relation.referencesKhandelwal, B. Theory of Aerospace Propulsion—Second Edition P. M. Sforza Elsevier Butterworth-Heinemann, The Boulevard, Langford Lane, Kidlington, Oxford, OX5 1GB, UK. 2017. Xx; 827pp. Illustrated £82.99. ISBN 978-0-12-809326-9. Aeronaut. J. 2019, 123, 1310–1311. [CrossRef]en_US
dc.relation.referencesFu, Z.; Gao, H.; Zeng, Z.; Liu, J. Numerical Analysis on Multi-Field Characteristics and Synergy in a Large-Size Annular Combustion Chamber with Double Swirlers. Comput. Model. Eng. Sci. 2020, 122, 805–830. [CrossRef]en_US
dc.relation.referencesGhahramani, Z.; Zareh, M. Design, Numerical and Experimental Investigation of High Swirling Flow in an Annular Combustion Chamber. Int. J. Adv. Des. Manuf. Technol. 2021, 14, 73–83. [CrossRef]en_US
dc.relation.referencesBalijepalli, R.; Dasore, A.; Rajak, U.; Siva Kumar Reddy, Y.; Varma, T.N. Design and Optimisation of Annulus Combustion Chamber of Gas Turbine Engine: An Analytical and Numerical Approach BT—Advancement in Materials, Manufacturing and Energy Engineering; Verma, P., Samuel, O.D., Verma, T.N., Dwivedi, G., Eds.; Springer Nature: Singapore, 2022; Volume II, pp. 553–567.en_US
dc.relation.referencesJagadish, V.; Anandarao, G.; Maddaiah, K.C.; Hussain, S.; Krishna, V.S. Design and Analysis of Gas Turbine Combustion Chamber. AIP Conf. Proc. 2023, 2492, 20031. [CrossRef]en_US
dc.relation.referencesLiu, C.; Yang, J.; Dong, Q.; Lai, C.; Zhao, J.; Lin, J.; Liu, M. Experimental and Numerical Study on Flow Field Characteristics of a Combustion Chamber with Double-Stage Counter-Rotating Swirlers. Int. Commun. Heat Mass Transf. 2024, 151, 107245. [CrossRef]en_US
dc.relation.referencesBahr, D.W. Aircraft Turbine Engine NOx Emission Limits: Status and Trends. In Proceedings of the ASME 1992 International Gas Turbine and Aeroengine Congress and Exposition, Cologne, Germany, 1–4 June 1992.en_US
dc.relation.referencesLangston, L.S. Gas Turbines. In Encyclopedia of Energy; Cleveland, C.J., Ed.; Elsevier: New York, NY, USA, 2004; pp. 221–230, ISBN 978-0-12-176480-7.en_US
dc.relation.referencesBoyce, M.P. Gas Turbine Engineering Handbook; Elsevier: Oxford, UK, 2006.en_US
dc.relation.referencesKnight, H.;Walker, R. The Component Pressure Losses in Combustion Chambers; Cranfield University: Cranfield, UK, 2012.en_US
dc.relation.referencesClemente Mendoza, A.A. Diseño de Generadores de Vórtice de Una Cámara de Combustión de Turbina de Gas. Master’s Thesis, Instituto Politécnico Nacional, Unidad Zacatenco, Mexico City, Mexico, 2019.en_US
dc.relation.referencesPegemanyfar, N.; Pfitzner, M. State-of-the-Art Combustor Design Utilizing the Preliminary Combustor Design System PRECODES. In Proceedings of the ASME Turbo Expo 2008: Power for Land, Sea, and Air, Berlin, Germany, 9–13 June 2008; Volume 3.en_US
dc.relation.referencesShahril, A.; Samin, R.; Juraidi, J.M.; Daut, J. Structural Analysis of Brake Disc Using Dynamic Simulation. ARPN J. Eng. Appl. Sci. 2015, 10, 7805–7808.en_US
dc.relation.referencesBozorgi, A.; Javidpour, E.; Riasi, A.; Nourbakhsh, A. Numerical and Experimental Study of Using Axial Pump as Turbine in Pico Hydropower Plants. Renew. Energy 2013, 53, 258–264. [CrossRef]en_US
dc.relation.referencesAbou-Taouk, A.; Whiddon, R.; Sigfrid, I.; Eriksson, L.-E. CFD Investigation of Swirl-Stabilized Flexi-Fuel Burner Using Methane- Air Mixture for Gas Turbines. In International Society for Airbreathing Engines, ISABE, Gothenburg; American Institute of Aeronautics and Astronautics Inc.: Reston, VA, USA, 2011; pp. 1–13.en_US
dc.relation.referencesSnow, D.B.; Avery, B.D.; Bodin, L.A.; Htc, L.T.V.; Baldasare, P.; Htc, L.T.V.;Washburn, G.F.; Ktc, L.T. V Nasa Tm. 1974. Available online: https://ntrs.nasa.gov/citations/19740024319 (accessed on 26 May 2024).en_US
dc.relation.referencesGoldmann, A.; Sauter,W.; Oettinger, M.; Kluge, T.; Schröder, U.; Seume, J.R.; Friedrichs, J.; Dinkelacker, F. A Study on Electrofuels in Aviation. Energies 2018, 11, 392. [CrossRef]en_US
dc.relation.referencesSaravanamuttoo, H.I.H.; Rogers, G.F.C.; Cohen, H. Gas Turbine Theory; Prentice Hall: Hoboken, NJ, USA, 2001; ISBN 9780130158475.en_US
dc.relation.referencesClean Energy Technologies 2022. Available online: https://doi.org/10.5772/intechopen.102298 (accessed on 26 May 2024).en_US
dc.relation.referencesZhang, C.; Hui, X.; Lin, Y.; Sung, C.-J. Recent Development in Studies of Alternative Jet Fuel Combustion: Progress, Challenges, and Opportunities. Renew. Sustain. Energy Rev. 2016, 54, 120–138. [CrossRef]en_US
dc.relation.referencesHennecke, C. Failure Detection in an Annular Combustion Chamber with Experimental and Numerical Methods. J. Aeronaut. Aerosp. Eng. 2017. Available online: https://www.semanticscholar.org/paper/Failure-Detection-in-an-Annular-Combustion- Chamber-Hennecke-VonderHaar/c0a1888f0cd2fc625dfbce13a0c5cd7b9a363c16 (accessed on 26 May 2024).en_US
dc.relation.referencesZeng, W.; Liu, J.; Yu, L.; Ma, H.; Zheng, W. Reaction Kinetic Simulation of the Combustion and Emission Characteristics of a Dual-Fuel Aero-Engine. Fuel 2019, 237, 352–360. [CrossRef]en_US
dc.relation.referencesBenim, A.C.; Iqbal, S.; Meier, W.; Joos, F.; Wiedermann, A. Numerical Investigation of Turbulent Swirling Flames with Validation in a Gas Turbine Model Combustor. Appl. Therm. Eng. 2017, 110, 202–212. [CrossRef]en_US
dc.relation.referencesGarcía-León, R.A.; Perez Rojas, E. Analysis of the Amount of Heat Flow between Cooling Channels in Three Vented Brake Discs. Ing. Univ. 2017, 21, 71–96. [CrossRef]en_US
dc.relation.referencesGarcía-León, R.A.; Afanador-García, N.; Gómez-Camperos, J.A. Numerical Study of Heat Transfer and Speed Air Flow on Performance of an Auto-Ventilated Disc Brake. Fluids 2021, 6, 160. [CrossRef]en_US
dc.relation.referencesHabibi, F.I.; Hartono, F.; Prayogo, H. Optimization of an Annular Combustion Chamber for Micro Turbo Jet System. IOP Conf. Ser. Mater. Sci. Eng. 2019, 645, 12009. [CrossRef]en_US
dc.relation.referencesTuma, J.; Kubata, J.; Betak, V.; Hybl, R. Experimental and Numerical Research of a Novel Combustion Chamber for Small Gas Turbine Engines. EPJ Web Conf. 2013, 45, 01091. [CrossRef]en_US
dc.identifier.DOIhttps://doi.org/10.3390/fluids9070161en_US


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