Design of High-temperature High-pressure Full-scale Modelling Cooling Efficiency Experiment Scheme for the First-stage Rotating Blades in an F-class Heavy-duty Gas Turbine

XIONG Yan; BIAN Yunhang; WANG Hui; MA Ye; LIU Zhigang; XU Yingying; HAN Xing; JIANG Dongpo

doi:10.19805/j.cnki.jcspe.2026.250640

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Design of High-temperature High-pressure Full-scale Modelling Cooling Efficiency Experiment Scheme for the First-stage Rotating Blades in an F-class Heavy-duty Gas Turbine

更新时间：2026-10-06

- Design of High-temperature High-pressure Full-scale Modelling Cooling Efficiency Experiment Scheme for the First-stage Rotating Blades in an F-class Heavy-duty Gas Turbine
- Chinese Journal of Power Engineering Vol. 46, Issue 3, Pages: 139-148(2026)
- 作者机构：
  
  1. 中国科学院工程热物理研究所,北京,100190
  2. 中国科学院大学工程科学学院,北京,100049
  3. 江苏中科能源动力研究中心,江苏,连云港,222069
  4. 哈电发电设备国家工程研究中心有限公司,黑龙江,哈尔滨,150028
- 作者简介：
- 基金信息：
- DOI：10.19805/j.cnki.jcspe.2026.250640
  CLC：
- Online First：10 March 2026，
  
  Published：10 March 2026
- 稿件说明：
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熊燕,卞云航,王晖,马也,刘志刚,许莹莹,韩星,姜东坡. F级重型燃气轮机透平第一级动叶高温高压全尺寸模化冷却效率试验方案设计动力工程学报, 2026, 46(3): 139-148 https://doi.

org/10.19805/j.cnki.jcspe.2026.250640
熊燕,卞云航,王晖,马也,刘志刚,许莹莹,韩星,姜东坡. F级重型燃气轮机透平第一级动叶高温高压全尺寸模化冷却效率试验方案设计动力工程学报, 2026, 46(3): 139-148 https://doi. DOI： 10.19805/j.cnki.jcspe.2026.250640.

org/10.19805/j.cnki.jcspe.2026.250640 DOI：

摘要

为获取适用于某重型F级燃气轮机透平第一级动叶的高温高压全尺寸的静态模化综合冷却效率试验方案

同时基于高效低碳燃气轮机试验装置高温喷嘴叶栅试验台得到接近真实条件下的动叶综合冷却效率试验数据

开展了动叶进口条件的模化方法研究、过渡段-第一级静叶一体化转接段和试验段的关键结构设计研究等

然后采用数值模拟和试验验证相结合的方法验证了方案的有效性。试验结果表明:试验方案和模拟方法合理可行

试验结果具有良好的可重复性

可靠性高。该试验方案可以为重型燃气轮机领域后续类似的动叶综合冷却效率试验提供参考。

Abstract

To obtain an experiment scheme for full-scale static modelling comprehensive cooling efficiency under high-temperature and high-pressure in the first-stage rotating blades of an F-class heavy-duty gas turbine

and simultaneously acquire comprehensive cooling efficiency test data of the rotating blades under conditions close to real-world scenarios based on the high-temperature nozzle cascade test rig of the efficient and low-carbon gas turbine test facility

researches were conducted on the modelling method for the inlet conditions of rotating blades

and the key structural design of the transition section-first-stage stationary blade integrated adapter section and the test section. Subsequently

the validity of the scheme was verified by a combined approach of numerical simulation and experimental validation. Experiment results indicate that the experiment scheme and simulation method are reasonable and feasible

with good repeatability and high reliability of experiment results. This test scheme can provide a reference for subsequent similar comprehensive cooling efficiency experiments of rotating blades in the field of heavy-duty gas turbines.

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references

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