燃气和燃氢涡轮叶栅端壁传热和气膜冷却特性OA
Endwall Heat Transfer Characteristics and Film Cooling Performance of Gas-and Hydrogen-Combustion Turbine Cascades
在"碳达峰""碳中和"能源转型目标下,燃气轮机掺氢和全氢燃烧已成为源头降碳的重要举措.零碳工质(氢气)燃烧会导致产物中水蒸气比例升高及热物性改变,这会显著影响下游涡轮叶栅气热性能.研究了不同工质(甲烷和氢气)燃烧后的组分变化,对比分析了不同燃气组分和吹风比1.0、2.5和3.5对叶栅端壁传热特性和气膜冷却性能的影响.研究表明:零碳工质燃烧产物中水分含量增加,近端壁比热容增大,这导致端壁局部传热系数显著增加(增幅约10%)和冷却效率显著下降(降幅约10%).随着吹风比增加(由1.0到3.5),零碳工质导致的端壁气热性能衰退现象逐渐弱化,其平均传热系数增幅从约7.0%降至约4.5%,冷却效率降幅从约6.0%降至约4.0%.研究成果揭示了燃烧工质转变对下游叶栅气热性能的影响机制,可为燃氢涡轮叶栅高效冷却布局设计提供技术参考.
In the energy-transition context of"carbon peak"and"carbon neutrality",hydrogen blending and full hydrogen combustion of gas turbine have become important measures for reducing carbon emission at the source.The combustion of zero-carbon working fluid(hydrogen)leads to an increase of water vapor in combustion products and changes in thermophysical properties,thus,the aerothermal performance of downstream turbine cascades would be significantly affected.The composition changes in combustion products of different working fluids(methane and hydrogen)were studied,and the effects of gas composition and blowing ratios of 1.0,2.5 and 3.5 on the endwall heat transfer characteristics and film cooling performance of cascades were compared and analyzed.Results indicated that in the combustion products of zero-carbon working fluid,the water vapor content increased,the near-endwall specific heat capacity raised accordingly,leading to a significant increase in the local endwall heat transfer coefficient(approximately 10%)and a notable decrease in cooling efficiency(approximately 10%).With the blowing ratio being raised from 1.0 to 3.5,the degradation of endwall aerothermal performance caused by zero-carbon working fluid gradually weakened,thereafter,the increase amplitude of average heat transfer coefficient dropped from about 7.0% to 4.5%,and the decrease amplitude of cooling efficiency reduced from about 6.0% to 4.0%.The research results reveal the impact mechanism of combustion working fluid conversion on the aerothermal performance of downstream cascades,providing technical references for design of high-efficiency cooling layouts of hydrogen-combustion.
黄海;张昊;白波;李志刚;李军
西安交通大学 叶轮机械研究所,西安 710049西安交通大学 叶轮机械研究所,西安 710049西安交通大学 叶轮机械研究所,西安 710049西安交通大学 叶轮机械研究所,西安 710049西安交通大学 叶轮机械研究所,西安 710049
能源科技
燃气轮机燃氢涡轮静叶端壁传热特性气膜冷却特性
gas turbinehydrogen-combustion turbinevane endwallheat transfer characteristicsfilm cooling performance
《热力透平》 2026 (1)
1-9,9
国家自然科学基金(52406054)
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