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天然气简化反应机理构建与验证

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采用6种详细反应机理对多工况条件下天然气的着火延迟时间、层流燃烧速度以及氧化过程中主要组分摩尔分数进行了数值计算,并与相应试验数据进行了对比分析.结果表明:相比于其他5种详细反应机理,Aramco2.0机理在天然气的着火延迟、层流燃烧以及氧化特性的预测上精度最高.基于Aramco 2.0机理,通过路径敏感性分析、生成速率分析与反应路径分析,形成了天然气(CH4/C2H6/C3H8)的初始简化机理(包含21种组分、150个反应);同时,基于解耦法,耦合初始简化反应机理中的C1~C3反应机理、H2/CO详细反应机理和NOx简化反应机理,构建了天然气的简化反应机理(包含40种组分、189个反应).通过与相应试验数据的对比发现,该简化反应机理能很好地预测多工况条件下天然气的着火延迟、层流燃烧与氧化特性.
Construction and validation of reduced reaction mechanism of natural gas
The ignition delay time,the laminar combustion speed of natural gas and the main species concentrations in the natural gas oxidation process were simulated by six detailed reaction mechanisms,and also compared with corresponding experimental data.The results showed that,compared with the other five detailed reaction mechanisms,Aramco 2.0 mechanism had the highest accuracy in predicting the ignition delay,laminar combustion and oxidation characteristics of natural gas.Based on Aramco 2.0 mechanism,an initial reduced reaction mechanism(including 21 species and 150 reactions)of natural gas(including CH4,C2H6 and C3H8)was formed using the path sensitivity analysis,production rate analysis and reaction path analysis.At the same time,based on decoupling method,through combining the reaction mechanism of C1—C3 in the initial reduced reaction mechanism with the detailed reaction mechanism of H2/CO and the reduced reaction mechanism of NOx,the reduced reaction mechanism of natural gas was constructed(including 40 species and 189 reactions).Compared with the corresponding experimental data,it was found that the reduced reaction mechanism can well predict the ignition delay,laminar combustion and oxidation characteristics of natural gas under various conditions.

natural gasreduced reaction mechanismdecoupling methodpath sensitivity analysisrate of production analysis

宋晨星、曾文、陈潇潇、胡二江、常亚超、马宏宇

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沈阳航空航天大学航空发动机学院,沈阳 110136

西安交通大学能源与动力工程学院动力工程多相流国家重点实验室,西安 710049

大连理工大学海洋能源利用与节能教育部重点实验室,辽宁大连 116024

中国航发沈阳发动机研究所,沈阳 110015

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天然气 简化反应机理 解耦法 路径敏感性分析 生成速率分析

国家科技重大专项

2017-Ⅲ-0006-0031

2024

航空动力学报
中国航空学会

航空动力学报

CSTPCD北大核心
影响因子:0.59
ISSN:1000-8055
年,卷(期):2024.39(4)
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