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    Allam循环中CH4/O2/CO2燃烧机理简化与高压燃烧特性

    Simplification of CH4/O2/CO2 Combustion Mechanism and High-Pressure Combustion Characteristics in the Allam Cycle

    • 摘要: 在目前,Allam循环在富CO2高压环境下的基础燃烧特性尚不明确,且现有详细反应机理较为复杂、计算效率低,这制约了相关燃烧器的设计与优化。本文面向CH4/O2/CO2体系开展燃烧特性与机理简化,采用敏感性分析与直接关系图法,分别简化了适用于常压的GRI3.0机理和适用于高压的Aramco3.0机理,在0.1-10MPa压力范围内以层流火焰速度与点火延迟时间为指标进行验证,确保误差小于5%。简化后,GRI3.0机理的组分与反应数均减少约40%,Aramco3.0机理的组分与反应数均减少约55%。基于简化机理的模拟表明,Aramco3.0机理因包含CH3O2、CH3O2H等关键中间体,在反应路径及转化率上与GRI3.0机理存在显著差异。燃烧特性分析显示:层流火焰速度与初始温度正相关,对压力的敏感性随温度升高而增强;其随当量比的变化在低压下先增后减,在高压下单调上升。点火延迟时间与初始温度负相关,且随压力升高下降趋缓。本研究为Allam循环的燃烧模拟与优化提供了高效可靠的机理工具,也为超临界CO2动力循环研究奠定了理论基础。

       

      Abstract: Currently, the fundamental combustion characteristics of the Allam cycle under high-pressure CO2-rich environments remain unclear, and existing detailed reaction mechanisms are relatively complex with low computational efficiency, which constrains the design and optimization of related combustors. This work focuses on the CH4/O2/CO2 system to study combustion characteristics and mechanism reduction. Using sensitivity analysis and the direct relation graph method, the GRI3.0 mechanism suitable for atmospheric pressure and the Aramco3.0 mechanism suitable for high pressure were respectively reduced. Validation was performed over a pressure range of 0.1–10 MPa using laminar flame speed and ignition delay time as metrics, ensuring errors within 5%. After reduction, the species and reaction counts in the GRI3.0 mechanism were decreased by about 40%, while those in the Aramco3.0 mechanism were reduced by about 55%. Simulations based on the reduced mechanisms show that, due to the inclusion of key intermediates such as CH3O2 and CH3O2H, the Aramco3.0 mechanism differs significantly from the GRI3.0 mechanism in reaction pathways and conversion rates. Analysis of combustion characteristics reveals: laminar flame speed is positively correlated with initial temperature, and its sensitivity to pressure increases with rising temperature; its variation with equivalence ratio first increases and then decreases at low pressure, while it increases monotonically at high pressure. Ignition delay time is negatively correlated with initial temperature and decreases more slowly as pressure rises. This study provides an efficient and reliable mechanistic tool for combustion simulation and optimization of the Allam cycle, and also lays a theoretical foundation for research on supercritical CO2 power cycles.

       

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