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Parametric modelling system of gas turbine combustor

Xi Chen   ORCID icon orcid.org/0000-0003-0101-8336 ; College of Power and Energy Engineering, Harbin Engineering University, Harbin Heilongjiang 150001, China
Hongtao Zheng ; College of Power and Energy Engineering, Harbin Engineering University, Harbin Heilongjiang 150001, China
Gang Pan ; College of Power and Energy Engineering, Harbin Engineering University, Harbin Heilongjiang 150001, China
Xiangyu Jia ; College of Power and Energy Engineering, Harbin Engineering University, Harbin Heilongjiang 150001, China

Puni tekst: engleski, pdf (2 MB) str. 1213-1219 preuzimanja: 792* citiraj
APA 6th Edition
Chen, X., Zheng, H., Pan, G. i Jia, X. (2014). Parametric modelling system of gas turbine combustor. Tehnički vjesnik, 21 (6), 1213-1219. Preuzeto s https://hrcak.srce.hr/131197
MLA 8th Edition
Chen, Xi, et al. "Parametric modelling system of gas turbine combustor." Tehnički vjesnik, vol. 21, br. 6, 2014, str. 1213-1219. https://hrcak.srce.hr/131197. Citirano 26.02.2021.
Chicago 17th Edition
Chen, Xi, Hongtao Zheng, Gang Pan i Xiangyu Jia. "Parametric modelling system of gas turbine combustor." Tehnički vjesnik 21, br. 6 (2014): 1213-1219. https://hrcak.srce.hr/131197
Harvard
Chen, X., et al. (2014). 'Parametric modelling system of gas turbine combustor', Tehnički vjesnik, 21(6), str. 1213-1219. Preuzeto s: https://hrcak.srce.hr/131197 (Datum pristupa: 26.02.2021.)
Vancouver
Chen X, Zheng H, Pan G, Jia X. Parametric modelling system of gas turbine combustor. Tehnički vjesnik [Internet]. 2014 [pristupljeno 26.02.2021.];21(6):1213-1219. Dostupno na: https://hrcak.srce.hr/131197
IEEE
X. Chen, H. Zheng, G. Pan i X. Jia, "Parametric modelling system of gas turbine combustor", Tehnički vjesnik, vol.21, br. 6, str. 1213-1219, 2014. [Online]. Dostupno na: https://hrcak.srce.hr/131197. [Citirano: 26.02.2021.]
Puni tekst: hrvatski, pdf (2 MB) str. 1213-1219 preuzimanja: 291* citiraj
APA 6th Edition
Chen, X., Zheng, H., Pan, G. i Jia, X. (2014). Parametarski sustav modeliranja komore izgaranja plinske turbine. Tehnički vjesnik, 21 (6), 1213-1219. Preuzeto s https://hrcak.srce.hr/131197
MLA 8th Edition
Chen, Xi, et al. "Parametarski sustav modeliranja komore izgaranja plinske turbine." Tehnički vjesnik, vol. 21, br. 6, 2014, str. 1213-1219. https://hrcak.srce.hr/131197. Citirano 26.02.2021.
Chicago 17th Edition
Chen, Xi, Hongtao Zheng, Gang Pan i Xiangyu Jia. "Parametarski sustav modeliranja komore izgaranja plinske turbine." Tehnički vjesnik 21, br. 6 (2014): 1213-1219. https://hrcak.srce.hr/131197
Harvard
Chen, X., et al. (2014). 'Parametarski sustav modeliranja komore izgaranja plinske turbine', Tehnički vjesnik, 21(6), str. 1213-1219. Preuzeto s: https://hrcak.srce.hr/131197 (Datum pristupa: 26.02.2021.)
Vancouver
Chen X, Zheng H, Pan G, Jia X. Parametarski sustav modeliranja komore izgaranja plinske turbine. Tehnički vjesnik [Internet]. 2014 [pristupljeno 26.02.2021.];21(6):1213-1219. Dostupno na: https://hrcak.srce.hr/131197
IEEE
X. Chen, H. Zheng, G. Pan i X. Jia, "Parametarski sustav modeliranja komore izgaranja plinske turbine", Tehnički vjesnik, vol.21, br. 6, str. 1213-1219, 2014. [Online]. Dostupno na: https://hrcak.srce.hr/131197. [Citirano: 26.02.2021.]

Sažetak
In the numerical simulation research of gas turbine combustor, there are plenty repetitive operations such as modelling and meshing. Parametric design idea is about simplifying it. This paper establishes a parametric modelling system of gas turbine combustor, mainly for the flame tube components, which includes parametric modelling and simple mesh generation. Taking a swirler as example, this paper introduces the parametric modelling system in detail. It also shows that the database contains different swirler and flame tube structure types. The system is designed under the UG secondary development platform, based on graphics template of parametric design method. The parametric modelling system has good practicability and universality, only takes a few minutes to update a model, and can update the database anytime to add new structure types. It is a utility for aid of both combustion chamber design and performance optimization research work.

Ključne riječi
combustor; gas turbine; parametric modelling; secondary development

Hrčak ID: 131197

URI
https://hrcak.srce.hr/131197

[hrvatski]

Posjeta: 1.433 *