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O_(2)/CO_(2)氛围下正庚烷的燃烧机理研究

Quantum chemical analysis of n-heptane combustion mechanism under O_(2)/CO_(2)atmosphere
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摘要 为研究正庚烷(n-C_(7)H_(16))在O_(2)/CO_(2)氛围下的燃烧特性,提出了基于CO_(2)与H·详细反应路径的C-H燃烧机理。通过密度泛函理论对CO_(2)与H·可能存在的反应路径进行了分析,根据定容燃烧弹实际尺寸建立了计算网格,利用C-H机理计算了正庚烷在不同氛围(空气、53%O_(2)/47%CO_(2)、61%O_(2)/39%CO_(2))下的燃烧过程;搭建了定容燃烧弹可视化实验平台,对正庚烷在不同氛围下的燃烧过程进行了测量;对CO_(2)的反应位点、CO_(2)+H·——→CO+·OH的反应能垒、火焰长度进行了分析。结果表明:C-H机理可以很好地预测正庚烷在O_(2)/CO_(2)氛围下的燃烧火焰长度,在50%O_(2)/50%CO_(2)氛围下的最大误差和平均误差分别为9.60%、2.42%;反应位点分析发现,CO_(2)氧原子的反应活性大于碳原子,氧端的平均局部离子化能和分子表面静电势分别为297.72 kcal/mol、-13.08 kcal/mol;H·与CO_(2)的碳原子和氧原子均可发生结合,反应能垒分别为26.71、11.07 kcal/mol。 In order to study the combustion characteristics of n-heptane under O_(2)/CO_(2)atmosphere,a C-H combustion mechanism based on the detailed reaction paths of CO_(2)and H·was proposed.The possible reaction paths of CO_(2)and H·were analyzed by using density functional theory,and the calculation grids were established according to the actual size of constant volume combustion chamber.The combustion processes of n-heptane under different atmospheres(air,53%O_(2)/47%CO_(2),61%O_(2)/39%CO_(2))were calculated through C-H mechanism.A constant volume incendiary bomb visualization experiment platform was built to measure the combustion process of n-heptane in different atmospheres.The reaction site of CO_(2),the reaction energy barrier of CO_(2)+H·→CO+·OH,and the flame length were analyzed.The results show that the C-H mechanism can well predict the combustion flame length of n-heptane under O_(2)/CO_(2)atmosphere,and the maximum error and the average error are 9.60%and 2.42%respectively under 50%O_(2)/50%CO_(2).The reactivity of oxygen atom of CO_(2)is higher than that of carbon atom,and the average local ionization energy and molecular surface electrostatic potential at the oxygen ends are 297.72 and-13.08 kcal/mol,respectively.H·can combine with carbon atom and oxygen atom of CO_(2),the reaction energy barrier are 26.71 and 11.07 kcal/mol,respectively.
作者 李晨曦 刘永峰 张璐 刘海峰 宋金瓯 何旭 LI Chenxi;LIU Yongfeng;ZHANG Lu;LIU Haifeng;SONG Jin’ou;HE Xu(Beijing Engineering Research Center of Monitoring for Construction Safety,Beijing University of Civil Engineering and Architecture,Beijing 102627,China;State Key Laboratory of Engines,Tianjin University,Tianjin 300072,China;School of Mechanical Engineering,Beijing Institute of Technology,Beijing 100081,China)
出处 《化工学报》 EI CSCD 北大核心 2023年第5期2157-2169,共13页 CIESC Journal
基金 国家自然科学基金项目(51976007) 内燃机燃烧学国家重点实验室开放研究项目(K2023-04) 北京建筑大学研究生创新项目(PG2022129)。
关键词 二氧化碳 计算化学 计算流体力学 定容燃烧弹 反应位点 火焰长度 carbon dioxide computational chemistry computational fluid dynamics constant volume combustion chamber reaction site flame length
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  • 1贾宝山,温海燕,梁运涛,王小云.煤矿巷道内N_2及CO_2抑制瓦斯爆炸的机理特性[J].煤炭学报,2013,38(3):361-366. 被引量:36
  • 2邓军,李会荣,杨迎,侯爽,文振翼.瓦斯爆炸微观动力学及热力学分析[J].煤炭学报,2006,31(4):488-491. 被引量:30
  • 3杨昆,刘伟.管内层流充分发展段等效热边界层的构造及其场协同分析[J].工程热物理学报,2007,28(2):283-285. 被引量:19
  • 4Brazier-Smith P, Jennings S, Latham J. The Interaction of Falling Rain Drops: Coalescence [J].Proccedings of the Royal Society of London A,1972(326) :393-408.
  • 5O' Rourke P J. Collective Droplets on Vaporizing Liquid Sprays [D]. Princeton: University of Princeton, 1981.
  • 6Amsden A A, O'Rourke P J, Butler T D. KIVAⅡ: A Computer Program for Chemically Reactive Flows with Sprays [R]. Los Alamos National Laboratory Report, LA-11560-MS,1989.
  • 7Tennison P J, Georjon T L, Farrell P V, et al. Experimental and Numerical Study of Sprays from a Common Rail Injection System for Use in an HSDI Diesel Engine[C]. SAE Paper 980809, 1998.
  • 8Post S L, Abraham J. Modeling the Outcome of Drop-Drop Collisions in Diesel Sprays [J]. International Journal of Multiphase Flow, 2002,28 (6):997-1 019.
  • 9Schmidt D P, Rutland C J. A New Droplet Collision Algorithm [J]. Journal of Computational Physics, 2000, 64(1):62-80.
  • 10Nordin N P. A Complex Chemistry Modeling of Diesel Spray Combustion[D]. Chalmers: Chalmers University of Technology, 2000.

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