Numerical Study on Convective Heat Transfer of Liquid Metal Gallium in Turbine Guide Vane

Author:

Zhang Zhe1,Wu Zeyu2,Luo Xiang2,Liu Weitong2

Affiliation:

1. School of Energy and Power Engineering, Beihang University, Beijing 100191, China

2. Research Institute of Aero-Engine, Beihang University, Beijing 100191, China

Abstract

The traditional blade cooling method can no longer meet the requirements of high cooling efficiency in modern engines. In order to solve this cooling problem, this paper proposes cooling turbine guide blades based on liquid metal. The feasibility was preliminarily verified using a one-dimensional heat conduction model. Then, using a numerical method, we found that the cooling effect of liquid metal is much better than that of air cooling. The main reason for its good cooling effect is that the heat transfer coefficient of liquid metal reaches a magnitude of tens of thousands. Moreover, as the inlet temperature of the liquid metal decreases and the inlet Reynolds number increases, the liquid cooling effect becomes better. The definition of the heat transfer quality factor can reflect the reasons for the influence of the inlet temperature of the liquid metal.

Publisher

MDPI AG

Subject

Aerospace Engineering

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