Radiation heat transfer model for complex superalloy turbine blade in directional solidification process based on finite element method

China Foundry - Tập 13 - Trang 123-132 - 2016
Dun-ming Liao1, Liu Cao1, Tao Chen1, Fei Sun1, Yong-zhen Jia1, Zi-hao Teng1, Yu-long Tang1
1State Key Laboratory ofMaterials Processing and Die & Mould Technology, Huazhong University of Science and Technology, Wuhan, China

Tóm tắt

For the sake of a more accurate shell boundary and calculation of radiation heat transfer in the Directional Solidification (DS) process, a radiation heat transfer model based on the Finite Element Method (FEM) is developed in this study. Key technologies, such as distinguishing boundaries automatically, local matrix and lumped heat capacity matrix, are also stated. In order to analyze the effect of withdrawing rate on DS process, the solidification processes of a complex superalloy turbine blade in the High Rate Solidification (HRS) process with different withdrawing rates are simulated; and by comparing the simulation results, it is found that the most suitable withdrawing rate is determined to be 5.0 mm∙min-1. Finally, the accuracy and reliability of the radiation heat transfer model are verified, because of the accordance of simulation results with practical process.

Tài liệu tham khảo

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