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为明晰天然气掺氢发动机非平衡燃烧过程主要(火用)损源,本文利用自点火压力时程对文献中5个代表性CH
4
/H
2
燃烧动力学模型性能进行再评估,基于非平衡态热力学理论初步建立了基元反应(火用)损评估方法,结合详细动力学模型分析了不同约束条件下(温度、当量比、掺氢比)CH
4
/H
2
混合气自点火过程中基元反应(火用)损贡献及其变化规律。结果表明,反应初始温度升高,化学反应(火用)损减少,不完全燃烧损失增加。H
2
掺混虽未显著降低CH
4
燃烧最低(火用)损值,但有效扩展了CH
4
低(火用)损燃烧区。对比了不同温度、不同掺氢比下(火用)损速率和总(火用)损的时程演化,分析了HO
2
和OH自由基产率及其主导基元反应(火用)损贡献,揭示了初始温度和掺氢对燃烧(火用)损影响的动力学机制。进一步对比不同反应路径关键物种吉布斯自由能,从热力学角度解释了CH
4
高/低温氧化路径(火用)损差异。研究结果在基元反应水平上揭示了H
2
介入对CH
4
燃烧(火用)损的影响机制,可为探索减少天然气掺氢发动机(火用)损的控制方法提供理论依据。
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