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Supervised by Ministry of Industry and Information Technology of The People's Republic of China Sponsored by Harbin Institute of Technology Editor-in-chief Yu Zhou ISSNISSN 1005-9113 CNCN 23-1378/T

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Related citation:ZHOU Hong-ru,GU Zhong-hua,HAN Wan-jin,LIU Zhan-sheng.Numerical simulation of HP rotor cooling configuration using parameterized method[J].Journal of Harbin Institute Of Technology(New Series),2011,18(2):134-138.DOI:10.11916/j.issn.1005-9113.2011.02.026.
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Numerical simulation of HP rotor cooling configuration using parameterized method
Author NameAffiliation
ZHOU Hong-ru Harbin Power Equipment CO.,LTD,Harbin 150040,China 
GU Zhong-hua College of Power and Engineering,Harbin Institute of Technology,Harbin 150001,China 
HAN Wan-jin College of Power and Engineering,Harbin Institute of Technology,Harbin 150001,China 
LIU Zhan-sheng College of Power and Engineering,Harbin Institute of Technology,Harbin 150001,China 
Abstract:
This paper implemented cooling configuration design on certain gas turbine HP rotor using parameterized method.It is convenient for complicated gas turbine blade modeling using parameters and also benefit for the geometry modify in later period.Parameterized modeling is the foundation of air cooling turbine blade design method engineering application.Mesh quality can be awarded when generated complicated cooling configuration blade grids,and also the increase of calculation error can arise by many mesh blocks.Film cooling and serpentine passage can effectively enhance the cooling effectiveness and protect blade.
Key words:  conjugate heat transfer  air cooling turbine  parameterized method  rotor
DOI：10.11916/j.issn.1005-9113.2011.02.026
Clc Number:V235.1
Fund:

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