基于IGV调节策略的氢氨掺混F级燃气轮机变工况特性研究

曹宇翔; 姚宇博; 吕小静; 翁一武

doi:10.19805/j.cnki.jcspe.2026.250533

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基于IGV调节策略的氢氨掺混F级燃气轮机变工况特性研究

更新时间：2026-10-06

- 基于IGV调节策略的氢氨掺混F级燃气轮机变工况特性研究
- Study on Variable Condition Performance of F-Class Gas Turbines with Hydrogen-Ammonia Co-firing Based on IGV Adjustment Strategy
- 动力工程学报 2026年46卷第3期页码：10-18
- 作者机构：
  
  1. 上海交通大学中英国际低碳学院,上海,201306
  2. 上海交通大学机械与动力工程学院,上海,200240
- 作者简介：
  
  曹宇翔(1997—),男,辽宁鞍山人,硕士研究生,研究方向为氢氨掺混燃气轮机通流匹配
  翁一武(通信作者),研究员,博士,E-mail:ywweng@sjtu.edu.cn
- 基金信息：
  
  国家科技重大专项基础研究资助项目(HT-J2019-I-0009-0009)
- DOI：10.19805/j.cnki.jcspe.2026.250533
  中图分类号：
- 网络首发：2026-03-10，
  
  纸质出版：2026-03-10
- 稿件说明：
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曹宇翔,姚宇博,吕小静,翁一武. 基于IGV调节策略的氢氨掺混F级燃气轮机变工况特性研究动力工程学报, 2026, 46(3): 10-18 https://doi.

org/10.19805/j.cnki.jcspe.2026.250533
曹宇翔,姚宇博,吕小静,翁一武. 基于IGV调节策略的氢氨掺混F级燃气轮机变工况特性研究动力工程学报, 2026, 46(3): 10-18 https://doi. DOI： 10.19805/j.cnki.jcspe.2026.250533.

org/10.19805/j.cnki.jcspe.2026.250533 DOI：

摘要

为拓宽重型燃气轮机使用氢氨掺混燃料时的运行区间并提高其热力性能

以半山电厂255.6 MW重型燃气轮机为研究对象

提出基于改变压气机进口导叶(IGV)角度的调节策略

研究不同氢氨掺混比例下燃气轮机性能、透平各级超临界情况以及通流匹配特性。结果表明:基于所建模型

计算得到机组额定工况功率为254.59 MW

效率为36.33%

与设计值的相对误差分别为-0.4%

-1.54%

表明该模型计算结果具有足够精度;重型燃气轮机在使用氢氨掺混燃料时出口级静叶出口处马赫数均超过1

导致机组存在安全隐患且运行性能下降;随氨气体积占比从0增加至100%

IGV角度由81.41°减小到72.77°;通流匹配后出口级静叶马赫数由0.97降低到0.86

燃机效率从37.14%降低到36.64%。

Abstract

To broaden the operating range and improve the thermodynamic performance of heavy-duty gas turbines using hydrogen-ammonia blended fuels

the 255.6 MW heavy-duty gas turbine at Banshan Power Plant was used as the research object. A regulation strategy based on adjusting the inlet guide vane (IGV) angle was proposed to investigate the gas turbine performance

supercritical conditions in turbine stages

and flow matching characteristics under different hydrogen-ammonium blending ratios. Results show that the calculated power and efficiency under the rated operating condition by the established model are 254.59 MW and 36.33% respectively. The relative errors compared to the design values are -0.4% and -1.54% respectively

demonstrating that the model calculations possess sufficient accuracy. When operating with hydrogen-ammonia blended fuels

the Mach number at the exit of the last-stage stator exceeds 1

resulting in potential safety hazards and degraded operational performance. As the ammonia volume fraction increases from 0 to 100%

the IGV angle decreases from 81.41° to 72.77°. After flow matching optimization

the Mach number at the exit of the last-stage stator decreases from 0.97 to 0.86

while the gas turbine efficiency decreases from 37.14% to 36.64%.

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references

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