首页|掺氢比对低排放燃烧室性能影响研究

掺氢比对低排放燃烧室性能影响研究

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为了探究传统天然气燃气轮机对氢气燃料的适应性,基于现役某型工业低排放燃气轮机结构和性能,用数值模拟方法分析了燃料中氢气比例对低排放燃烧室性能的影响,确定了燃烧室燃用甲烷和氢气燃料的换用性能.研究表明:在1.0额定工况,掺氢比小于等于30%时,燃烧室不发生回火,喷嘴内部和火焰筒肩部回流区的温度以及燃烧室的总压损失随掺氢比的升高而升高,NOx排放体积分数小幅升高,CO排放体积分数减少;当掺氢比大于30%时,燃烧室发生回火,喷嘴和火焰筒肩部回流区温度、总压损失、NOx排放体积分数大幅升高,CO排放基本为零.在其他工况下,负荷变化对燃烧室边界条件影响较为复杂,对喷嘴回火边界影响无单调性变化规律.
Study on the Influence of Hydrogen Blending Ratio on Low Emission Combustor Performance
To explore the adaptability of traditional natural gas turbines to hydrogen fuel,based on the structure and performance of a certain type of industrial low-emission gas turbine,the influence of the proportion of hydrogen in the fuel on the performance of the low-emission combustion chamber was ana-lyzed by numerical simulation method,and the conversion performance of methane and hydrogen fuel in the combustion chamber was determined.The results show that under the full load condition,when the hydrogen mixing ratio is less than 30%,the combustion chamber does not backfire,the temperature in the nozzle and the circulating zone of the flame tube shoulder and total pressure loss in the combustion chamber increase with the increase of the hydrogen mixing ratio,the NOx emission volume fraction in-creases slightly,and the CO emission volume fraction decreases;when the hydrogen mixing ratio is more than 30%,the combustion chamber is tempered,and the temperature in the nozzle and the circulating zone of the flame tube shoulder,the total pressure loss and NOx emission volume fraction increase signifi-cantly,and the CO emission is almost 0.Under other working conditions,the influence of the load varia-tion on the combustion chamber boundary condition is complex,and the influence of the gas turbine working condition on the nozzle tempering boundary has no monotonicity variation.

industrial gas turbinecombustorhydrogen blending combustionpremixed combustion

秦琨、王威、李妍萍、李名家

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中国船舶集团有限公司第七○三研究所,黑龙江哈尔滨 150078

船舶与海洋工程特种装备和动力系统国家工程研究中心,黑龙江哈尔滨 150078

工业燃气轮机 燃烧室 掺氢燃烧 预混燃烧

国家科技重大专项国家科技重大专项黑龙江省"百千万"工程科技重大专项中船集团自立科技项目黑龙江省自然科学基金

2017-Ⅲ-006-0031J2019-Ⅲ-0012-0552019ZX03A03202109ZTD2021E001

2024

热能动力工程
中国 哈尔滨 第七0三研究所

热能动力工程

CSTPCD北大核心
影响因子:0.345
ISSN:1001-2060
年,卷(期):2024.39(3)
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