二氧化碳环境下氧-甲烷燃烧全球机制的发展

Owen M. Pryor, Subith S. Vasu, Xijia Lu, D. Freed, B. Forrest
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引用次数: 4

摘要

最近有一些关于甲烷全氧燃烧火焰动力学模型的研究。主要的挑战是,没有一种机制是用来理解点火的时间尺度的。在此基础上,建立了甲烷在全氧燃料环境下的三步燃烧机理。该机制是用一个封闭的间歇式均质间歇式反应器在恒压下模拟的,并与使用详细机制进行的基线模拟进行了比较。所有的甲烷模拟均采用XCH4 = 0.05, XO2 = 0.10和XCO2 = 0.85的混合物。采用全局机构平衡方法改变机构,以确保稳态值与参考值匹配,并使用优化方案进一步改变机构,以匹配激波管中采集的实验数据。将全球机制的甲烷、CO时程和温度分布的模拟结果与详细机制的模拟结果进行了比较。用点火延迟时间表示燃烧的时间尺度。在当前的模拟中,这被定义为燃烧过程中甲烷浓度达到其初始值5%所需的时间。使用这种方法,三步甲烷燃烧机制在压力(1至10 bar)和初始温度(1500至2000 K)范围内对贫燃料和化学计量混合物的点火时间都有很好的改善,但无法预测30 bar或富燃料混合物的点火延迟时间。目前的工作重点是将这种新的全球机制扩展到更高的压力和合成气混合物。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Development of a Global Mechanism for Oxy-Methane Combustion in a CO2 Environment
There has been some recent work on the global kinetic modeling of flames in oxy-fuel combustion for methane. The main challenge is that none of the mechanisms were developed to understand the time-scales of ignition. Here, a 3-step mechanism was developed for methane combustion in oxy-fuel environment. The mechanisms were simulated using a closed batch homogeneous batch reactor with constant pressure and compared to baseline simulations performed using a detailed mechanism. All simulations were performed for methane used a mixture of XCH4 = 0.05, XO2 = 0.10 and XCO2 = 0.85. Mechanisms were altered using the global mechanism equilibrium approach to ensure that the steady-state values matched the reference values and were further altered using an optimization scheme to match experimental data that was taken in a shock tube. Simulation results of methane, CO time-histories, and temperature profiles from the global mechanism were compared to those from the detailed mechanism. Ignition delay times were used to represent the time-scales of combustion. This was defined for current simulations as the time required for methane concentration to reach 5% of its initial value during combustion. Using this approach, the 3-step methane combustion mechanism showed excellent improvement in the ignition timing over a range of pressures (1 to 10 bar) and initial temperatures (1500 to 2000 K) for both lean and stoichiometric mixtures but fails to predict ignition delay times at 30 bar or the ignition delay times of fuel rich mixtures. Ongoing effort focuses on extending this new global mechanism to higher pressures and to syngas mixtures.
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