基于微燃气轮机模型燃烧室的氨燃烧实验

李坤; 吴殿武; 陈龙威; 陈治强; 范学军; 陈亮

doi:10.19666/j.rlfd.202502070

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基于微燃气轮机模型燃烧室的氨燃烧实验

新能源发电技术 | 更新时间：2025-11-21

- 基于微燃气轮机模型燃烧室的氨燃烧实验
- Experimental study on ammonia combustion based on micro gas turbine model combustion chamber
- 热力发电 2025年第11期页码：68-75
- 作者机构：
- 作者简介：
- 基金信息：
  
  国家自然科学基金项目（T2341001）;合肥综合性国家科学中心能源研究院独立项目（22KZS304,22KZS301）~~
- DOI：10.19666/j.rlfd.202502070
  中图分类号：
- 纸质出版：2025
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李坤, 吴殿武, 陈龙威, 等. 基于微燃气轮机模型燃烧室的氨燃烧实验[J]. 热力发电, 2025,(11):68-75.

李坤, 吴殿武, 陈龙威, et al. Experimental study on ammonia combustion based on micro gas turbine model combustion chamber[J]. Thermal Power Generation, 2025, (11): 68-75.
李坤, 吴殿武, 陈龙威, 等. 基于微燃气轮机模型燃烧室的氨燃烧实验[J]. 热力发电, 2025,(11):68-75. DOI： 10.19666/j.rlfd.202502070.

李坤, 吴殿武, 陈龙威, et al. Experimental study on ammonia combustion based on micro gas turbine model combustion chamber[J]. Thermal Power Generation, 2025, (11): 68-75. DOI： 10.19666/j.rlfd.202502070.

摘要

为探索氨燃料在燃气轮机燃烧室模拟件内的点火和稳定燃烧性能，分别对不同预热温度及裂解度的氨气进行点火燃烧实验研究，获得一定实验条件下氨燃料的点火及燃烧规律。实验结果表明：氨气稳定燃烧需满足裂解度不小于30%且空气预热器温度不小于643 K；在空气预热器温度743～943 K，燃烧时长5～40 s内，燃烧室内部温度、尾部温度及压力基本随空气预热器温度与燃烧时长的增加而升高；空气预热器温度显著影响NO排放，在673 K时NO排放体积分数最低，为376μL/L，此时燃烧效率为96%。零维模拟计算结果表明，增大压力、氨气裂解度和温度有助于缩短点火延迟时间，且较高的氢气含量和略微富燃的状态可促进层流火焰速度的增加，优化氨的燃烧。

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