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EVALUATION OF KINETIC MECHANISMS FOR DIRECT FIRED SUPERCRITICAL OXY- COMBUSTION OF NATURAL GAS

机译:天然气直接超临界氧燃烧的动力学机理评价

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Existing kinetic mechanisms for natural gas combustion are not validated under supercritical oxy-fuel conditions because of the lack of experimental validation data. Our studies show that different mechanisms have different predictions under supercritical oxy-fuel conditions. Therefore, preliminary designers may experience difficulties when selecting a mechanism for a numerical model. This paper evaluates the performance of existing chemical kinetic mechanisms and produces a reduced mechanism for preliminary designers based on the results of the evaluation. Specifically, the mechanisms considered were GRI-Mech 3.0, USC-Ⅱ, San Diego 204-10-04, NUIG-Ⅰ, and NUIG-Ⅲ. The set of mechanisms was modeled in Cantera and compared against the literature data closest to the application range. The high pressure data set included autoignition delay time in nitrogen and argon diluents up to 85 atm and laminar flame speed in helium diluent up to 60 atm. The high carbon dioxide data set included laminar flame speed with 70% carbon dioxide diluent and the carbon monoxide species profile in an isothermal reactor with up to 95% carbon dioxide diluent. All mechanisms performed adequately against at least one dataset. Among the evaluated mechanisms, USC-Ⅱ has the best overall performance and is preferred over the other mechanisms for use in the preliminary design of supercritical oxy-combustors. This is a significant distinction; USC-Ⅱ predicts slower kinetics than GRI-Mech 3.0 and San Diego 2014 at the combustor conditions expected in a recompression cycle. Finally, the global pathway selection method was used to reduce the USC-Ⅱ model from 111 species, 784 reactions to a 27 species, 150 reactions mechanism. Performance of the reduced mechanism was verified against USC-Ⅱ over the range relevant for high inlet temperature supercritical oxy-combustion.
机译:由于缺乏实验验证数据,在超临界含氧燃料条件下尚未验证现有的天然气燃烧动力学机制。我们的研究表明,在超临界含氧燃料条件下,不同的机理有不同的预测。因此,初步设计者在选择数值模型的机制时可能会遇到困难。本文评估了现有化学动力学机制的性能,并根据评估结果为初步设计人员提供了简化的机制。具体而言,考虑的机制是GRI-Mech 3.0,USC-Ⅱ,圣地亚哥204-10-04,NUIG-Ⅰ和NUIG-Ⅲ。该机制集在Cantera中进行了建模,并与最接近应用范围的文献数据进行了比较。高压数据集包括氮气和氩气稀释剂中高达85 atm的自燃延迟时间以及氦气稀释剂中高达60 atm的层流火焰速度。高二氧化碳数据集包括层流火焰速度(含70%二氧化碳稀释剂)和等温反应器中含高达95%二氧化碳稀释剂的一氧化碳物种分布。所有机制都针对至少一个数据集充分执行。在评估的机制中,USC-Ⅱ具有最佳的整体性能,并且在超临界氧燃烧器的初步设计中优于其他机制。这是一个很大的区别;在再压缩循环中预期的燃烧器条件下,USC-Ⅱ预测的动力学要比GRI-Mech 3.0和San Diego 2014慢。最后,采用全局途径选择方法将USC-Ⅱ模型从111种,784种反应减少到27种,150种反应机理。在USC-Ⅱ的高入口温度超临界氧燃烧相关范围内,对还原机理的性能进行了验证。

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