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Parametric modelling system of gas turbine combustor

Xi Chen orcid id 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: hrvatski pdf 2.328 Kb

str. 1213-1219

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Puni tekst: engleski pdf 2.328 Kb

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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

Podaci na drugim jezicima: hrvatski

Posjeta: 1.911 *