2012Gas Turbine Experiment and ResearchRequires access

Optimization of Turbine Blade Cooling Design with iSIGHT

Song Liu

Open publisher page 1 citations

Abstract

Based on the established turbine blade parametric model,this article chose iSIGHT to optimize the temperature field of turbine blade using inner boundary conditions and to optimize heat transfer coefficient of the structure component using geometry parameters.It successfully reduced the maximum temperature difference of blade section by this method.This research shows some relationships among different parameters,and would be referential for turbine blade cooling design.

About this research paper

What this paper is about

Based on the established turbine blade parametric model,this article chose iSIGHT to optimize the temperature field of turbine blade using inner boundary conditions and to optimize heat transfer coefficient of the structure component using geometry parameters.It successfully reduced the maximum temperature difference of blade section by this method.This research shows some relationships among different parameters,and would be referential for turbine blade cooling design.

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Method / approach

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Available abstract

Based on the established turbine blade parametric model,this article chose iSIGHT to optimize the temperature field of turbine blade using inner boundary conditions and to optimize heat transfer coefficient of the structure component using geometry parameters.It successfully reduced the maximum temperature difference of blade section by this method.This research shows some relationships among different parameters,and would be referential for turbine blade cooling design.

Key concepts: Blade (archaeology), Turbine blade, Mechanical engineering, Parametric statistics, Turbine, Engineering, Heat transfer coefficient, Heat transfer

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