涡轮叶片双排气膜冷却效率叠加计算准确性研究

孟通; 朱惠人; 刘存良; 徐博涵

doi:10.7652/xjtuxb201804008

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涡轮叶片双排气膜冷却效率叠加计算准确性研究

更新时间：2025-07-09

- 涡轮叶片双排气膜冷却效率叠加计算准确性研究
- Superposition Prediction Accuracy of Film Cooling Efficiency on Turbine Blade
- 西安交通大学学报 2018年52卷第4期页码：55-62
- 作者机构：
  
  西北工业大学动力与能源学院,西安,710072
- 作者简介：
- 基金信息：
  
  : 2017-11-08。作者简介: 孟通(1989—),男,博士生;朱惠人(通信作者),男,教授,博士生导师。基金项目: 国家重点基础研究发展计划资助项目(2013CB035702)
- DOI：10.7652/xjtuxb201804008
  中图分类号： V231.1
- 网络首发：2018-04-10，
  
  纸质出版：2018
- 稿件说明：
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孟通, 朱惠人, 刘存良, 等. 涡轮叶片双排气膜冷却效率叠加计算准确性研究[J]. 西安交通大学学报, 2018,52(4):55-62.

Superposition Prediction Accuracy of Film Cooling Efficiency on Turbine Blade[J]. 2018, 52(4): 55-62.
孟通, 朱惠人, 刘存良, 等. 涡轮叶片双排气膜冷却效率叠加计算准确性研究[J]. 西安交通大学学报, 2018,52(4):55-62. DOI： 10.7652/xjtuxb201804008.

Superposition Prediction Accuracy of Film Cooling Efficiency on Turbine Blade[J]. 2018, 52(4): 55-62. DOI： 10.7652/xjtuxb201804008.

摘要

为进一步了解涡轮叶片上多排气膜间的流动及换热规律

选取对气膜冷却效率有影响的3种典型因素(叶片型面、吹风比、孔排方式)进行了实验及数值计算研究

验证了涡轮叶片气膜冷却效率叠加计算的适用性。结果表明:由于叶片型面曲率的存在

叶片吸力面为凸面气膜更容易吹脱

气膜孔后冷却效率叠加计算误差约为5%; 叶片压力面为凹面气膜被压向壁面

前后排气膜间影响较大

叠加计算值比实验值约高13%。孔排排布方式对叠加计算结果同样有影响

叉排结构中气膜间呈现“块状叠加”现象

叠加计算值与实验值相比误差在5%以内。顺排结构中气膜呈现“层状叠加”现象

计算结果偏高

误差在10%左右。吹风比对冷却效率叠加计算准确性有较大影响

低吹风比时叠加计算较准确

随着吹风比增加叠加误差逐渐增大。针对叠加计算误差较大的工况

本文提出了相应的计算修正公式。

Abstract

Experimental and numerical simulations were conducted on turbine blade to figure out influences of three typical factors(vane curvature

blowing ratio and hole arrangement)on superposition prediction of film cooling efficiency. Results show that because of the convex blade surface on the suction side

jet is easy to be blown off and the computational error of superposition of film cooling efficiency is about 5%. On the pressure side

jet is easy to be pressed onto the wall and the prediction becomes inaccurate

hence the superposition calculation result is about 13% higher than experimental value. Another significant influence results from hole arrangement

the superposition prediction on staggered hole arrangement is nearly the same as the measured value

while it is much higher for in-line arrangement. Blowing ratio also has an obvious influence on the accuracy of superposition prediction for film cooling holes on both pressure side and suction side. At low blowing ratio

results obtained by Sellers method agree well with the experimental ones

while as blowing ratio increases

the accuracy of superposition prediction is decreased. At last

modification of Sellers method is suggested to improve the prediction accuracy.

关键词

Keywords

references

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