Study of Heat Transfer Characteristics of Different Cooling Configurations inside a Typical Low Pressure Turbine Blade
|更新时间:2026-07-07
|
Study of Heat Transfer Characteristics of Different Cooling Configurations inside a Typical Low Pressure Turbine Blade
Vol. 20, Issue 4, (2005)
作者机构:
北京航空航天大学航空发动机气动热力重点实验室,北京,100083
作者简介:
基金信息:
DOI:
CLC:
Published:2005
稿件说明:
移动端阅览
ZHANG Li-min, WEN Jie, DING Shui-ting, et al. Study of Heat Transfer Characteristics of Different Cooling Configurations inside a Typical Low Pressure Turbine Blade[J]. 2005, 20(4).
DOI:
ZHANG Li-min, WEN Jie, DING Shui-ting, et al. Study of Heat Transfer Characteristics of Different Cooling Configurations inside a Typical Low Pressure Turbine Blade[J]. 2005, 20(4).DOI:
Study of Heat Transfer Characteristics of Different Cooling Configurations inside a Typical Low Pressure Turbine Blade
Numerical simulation and experiment were carried out to study the characteristic of different cooling configurations in a typical low pressure turbine blade.Numerical simulations were performed to investigate the heat transfer of original blade and the improved blades.The numerical results show a good agreement with the experimental ones.Compared to the original blade
the improved blade enhanced the heat transfer effectiveness about 7.8%.The research results indicate that the configuration improving of the inner passage not only reinforces the performance of heat transfer
but also improves temperature distribution and avoids superheated regions.