Aerodynamic and heat transfer simulation of cooling turbine blade with different tips

Kuahai Yu, Xi Yang, Zhixun Wen, Zhufeng Yue

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

This paper studies the aerodynamic and heat transfer influence of tip structures for cooling turbine blade. Four blades with different tip features are discussed, and coupling aerodynamic and heat transfer method is used to accomplish the simulation. The results show that squealer tip can greatly reduce the heat transfer between tip surface and high temperature gas, and also it reduces tip leakage, to some extent. That's because it exists obviously eddy near the tip surface. Tip injection holes can cool the tip surface effectively, and it will greatly reduce the temperature of tip surface. However, injection holes improve tip leakage slightly.

源语言英语
主期刊名Manufacturing Science and Materials Engineering
763-767
页数5
DOI
出版状态已出版 - 2012
活动2010 International Conference on Manufacturing Science and Materials Engineering, ICMSME 2011 - Shanghai, 中国
期限: 14 10月 201115 10月 2011

出版系列

姓名Advanced Materials Research
443-444
ISSN(印刷版)1022-6680

会议

会议2010 International Conference on Manufacturing Science and Materials Engineering, ICMSME 2011
国家/地区中国
Shanghai
时期14/10/1115/10/11

指纹

探究 'Aerodynamic and heat transfer simulation of cooling turbine blade with different tips' 的科研主题。它们共同构成独一无二的指纹。

引用此