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基于Aspen Plus平台对混空轻烃燃气制气系统的研究
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作者 康新星 王景刚 +4 位作者 柳朋浩 张书元 严康 耿金 刘宇腾 《化工技术与开发》 CAS 2023年第11期13-18,共6页
研究混空轻烃燃气制气系统,优化制气参数,对设定混空轻烃燃气实际工程管网的输送压力具有指导意义,可为选择轻烃油种类以及调控轻烃油的体积分数值提供一定的理论依据。本文利用Aspen Plus对混空轻烃燃气的制气系统进行模拟,首先基于一... 研究混空轻烃燃气制气系统,优化制气参数,对设定混空轻烃燃气实际工程管网的输送压力具有指导意义,可为选择轻烃油种类以及调控轻烃油的体积分数值提供一定的理论依据。本文利用Aspen Plus对混空轻烃燃气的制气系统进行模拟,首先基于一定混空比范围下较低的露点温度,确定制气系统的制气压力,再在此基础上分析混空轻烃燃气中轻烃油体积分数的影响因素。研究结果表明,混空比范围为3.5~5、较低的露点温度工况下,最佳制气压力为0.055MPa。轻烃油体积分数的影响因素包括轻烃油流量、空气流量、有无外加输入热量等,轻烃油体积分数值随轻烃油流量、外加输入热量的增加而升高,随空气流量的增加而降低。综合考虑,选取第Ⅲ类轻烃油(组分为C413.45%、正戊烷48.32%、异戊烷38.17%、C60.06%)作为混空轻烃燃气制气的原料。 展开更多
关键词 ASPENPLUS 轻烃燃气 露点温度 轻烃油体积分数 热值
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混空轻烃燃气露点计算方法的探究 被引量:6
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作者 樊玉光 史冬雨 +1 位作者 魏嘉 张硕 《石油工业技术监督》 2018年第5期3-5,共3页
混空轻烃燃气作为我国新能源领域的一种新兴燃气,其相关工艺参数标准尤其是露点的制定仍然很不完善。现有标准CJ/T 341—2010《混空轻烃燃气》中对于混空燃气露点的计算方法存在计算范围相对狭小,对轻烃原料中的重质组分考虑不全等问题... 混空轻烃燃气作为我国新能源领域的一种新兴燃气,其相关工艺参数标准尤其是露点的制定仍然很不完善。现有标准CJ/T 341—2010《混空轻烃燃气》中对于混空燃气露点的计算方法存在计算范围相对狭小,对轻烃原料中的重质组分考虑不全等问题。针对此种情况,提出了一种多组分物系利用相平衡常数计算露点的方法,利用企业提供的一种原料数据进行了相关露点计算。对比天然气,研究了水含量对混空轻烃燃气露点的影响,提出了混空燃气制造、运输工程中需要注意的相关事项。 展开更多
关键词 混空燃气 工艺参数标准 露点 计算方法
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混空轻烃燃气露点测试分析及控制 被引量:5
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作者 史冬雨 黄泽奇 《云南化工》 CAS 2018年第1期130-131,共2页
面对我国能源供求上日渐突出的问题,以及石化行业副产物种类繁多、利用不充分的现状,混空轻烃燃气技术作为一种行之有效的解决方法被提出来。利用Aspen plus软件对混空燃气露点进行计算,并根据轻烃原料中各组分的含量模拟出露点与空气... 面对我国能源供求上日渐突出的问题,以及石化行业副产物种类繁多、利用不充分的现状,混空轻烃燃气技术作为一种行之有效的解决方法被提出来。利用Aspen plus软件对混空燃气露点进行计算,并根据轻烃原料中各组分的含量模拟出露点与空气流量及输出压力之间的关系;当空气中含有水分时,模拟出露点与输入空气中水分含量之间的关系。得到空气占比的增大以及输送压力的降低均会降低燃气露点,总结上述模拟结果,给出混空燃气在制造及运输过程中的相关建议。 展开更多
关键词 混空燃气 露点 制造运输
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民用混空轻烃燃气燃烧研究 被引量:1
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作者 樊玉光 任哲 +2 位作者 刘凯 韩桔 郭佳鑫 《云南化工》 CAS 2019年第12期74-75,共2页
混空轻烃燃气用于民用必须解决在灶具上的燃烧问题。通过计算比较混空轻烃燃气和12T天然气的各种燃烧特性参数以及在天然气灶具上的火孔出口流速和点火,分析混空轻烃燃气在天然气灶具上的燃烧。
关键词 轻烃燃气 天然气 燃气 燃烧
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混空轻烃燃气制备过程中的安全性分析 被引量:2
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作者 樊玉光 刘凯 《化工技术与开发》 CAS 2019年第8期56-59,共4页
混空轻烃燃气是一种新型燃气,由空气和经过加热气化的轻烃在混合器内混合制成。混合器内不均匀的浓度分布,会产生处于爆炸极限的区域,影响了制备的安全性。本文利用Fluent软件,对混空轻烃燃气在混合器内4种不同工况下的混合过程进行三... 混空轻烃燃气是一种新型燃气,由空气和经过加热气化的轻烃在混合器内混合制成。混合器内不均匀的浓度分布,会产生处于爆炸极限的区域,影响了制备的安全性。本文利用Fluent软件,对混空轻烃燃气在混合器内4种不同工况下的混合过程进行三维仿真计算,得到混合器内不同位置混空轻烃燃气的浓度分布情况,对流场中不同浓度分布下的爆炸危险性进行分析,并提出相应的改进措施,为解决混空轻烃燃气制备过程中潜在的安全性问题提供参考依据。 展开更多
关键词 轻烃燃气 安全性分析 数值模拟
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混空轻烃燃气爆炸极限计算方法的研究 被引量:9
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作者 樊玉光 张硕 +1 位作者 史冬雨 魏嘉 《石油工业技术监督》 2018年第7期40-42,共3页
在新型燃气的生产、置换以及运行等过程中发生的泄漏,都可能产生爆炸极限范围内的混合气体。准确掌握燃气的爆炸极限,对消防报警和安全使用燃气有重要意义。由于燃气爆炸极限受多种因素的影响,很难用一个统一的计算公式对不同混合气体... 在新型燃气的生产、置换以及运行等过程中发生的泄漏,都可能产生爆炸极限范围内的混合气体。准确掌握燃气的爆炸极限,对消防报警和安全使用燃气有重要意义。由于燃气爆炸极限受多种因素的影响,很难用一个统一的计算公式对不同混合气体的爆炸极限进行准确计算。给出了多种爆炸极限的计算方法,比较得出计算混空轻烃燃气爆炸极限的推荐公式。 展开更多
关键词 轻烃燃气 爆炸极限 计算方法
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混空轻烃燃气密度计算方法的研究 被引量:6
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作者 樊玉光 魏嘉 +1 位作者 张硕 史冬雨 《石油工业技术监督》 2018年第4期23-24,28,共3页
燃气的密度对混空轻烃燃气的生产和安全有重要意义。在CJ/T 341-2010《混空轻烃燃气》中没有明确地给出密度计算方法。通过分析混空轻烃燃气的特性,类比天然气的计算标准,提出了混空轻烃燃气密度的理论计算方法,并对具体混空轻烃燃气实... 燃气的密度对混空轻烃燃气的生产和安全有重要意义。在CJ/T 341-2010《混空轻烃燃气》中没有明确地给出密度计算方法。通过分析混空轻烃燃气的特性,类比天然气的计算标准,提出了混空轻烃燃气密度的理论计算方法,并对具体混空轻烃燃气实例进行计算验证。 展开更多
关键词 轻烃燃气 密度 理论计算 标准计算
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混空轻烃燃气发生装置制气工艺研究 被引量:2
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作者 闫永超 陈永东 +1 位作者 董丹丹 刘孝根 《化学工程》 CAS CSCD 北大核心 2022年第1期74-78,共5页
混空轻烃燃气发生装置的工作原理是向装有液态轻烃燃料的储罐内鼓入空气,液态轻烃蒸发附着在空气泡表面形成混空燃气。对混空轻烃燃气发生装置的工艺流程进行模拟,确定空气流量、液态轻烃温度以及气化器内液位是混空燃气制气过程中最大... 混空轻烃燃气发生装置的工作原理是向装有液态轻烃燃料的储罐内鼓入空气,液态轻烃蒸发附着在空气泡表面形成混空燃气。对混空轻烃燃气发生装置的工艺流程进行模拟,确定空气流量、液态轻烃温度以及气化器内液位是混空燃气制气过程中最大的影响因素,轻烃体积分数随空气流量的增大而减小,随外界输入热量、液态轻烃流量的增大而增大。根据轻烃鼓泡制气过程传质及传热特性,确定轻烃鼓泡制气工艺过程的理论计算模型。通过理论计算与试验数据对比,误差小于15%,验证了混空燃气轻烃含量理论计算的可行性,在装置设计过程及制气过程中可依据理论公式精准调控轻烃体积分数。 展开更多
关键词 轻烃燃气 理论模型 流程模拟 试验研究
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混空轻烃燃气气体分布器数值模拟及结构优化 被引量:2
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作者 董丹丹 陈永东 +1 位作者 闫永超 吴晓红 《化学工程》 CAS CSCD 北大核心 2021年第2期54-58,63,共6页
混空轻烃燃气发生装置的工作原理是向装有液态轻烃燃料的储罐内鼓入空气,液态轻烃蒸发附着在空气泡表面形成混空燃气,其中气体分布器对轻烃气化过程起着决定性的作用,是气化装置内的核心部件。建立轻烃气化装置分布器的三维数值模型,模... 混空轻烃燃气发生装置的工作原理是向装有液态轻烃燃料的储罐内鼓入空气,液态轻烃蒸发附着在空气泡表面形成混空燃气,其中气体分布器对轻烃气化过程起着决定性的作用,是气化装置内的核心部件。建立轻烃气化装置分布器的三维数值模型,模拟分布器内气液两相流过程,并针对现有气体分布器结构存在的缺陷提出相应的优化方案,分别对分布器支管尺寸、周向开孔、轴向开孔间距及开孔尺寸进行了优化。研究结果表明:周向开孔存在气体分布不均匀及液体回流,轴向开孔间距为50 mm时,汽化器空间利用率最高;开孔尺寸为10 mm时气液接触面积最大,最利于轻烃的气化。本次研究结果为混空轻烃燃气发生装置中气体分布器的优化设计提供了重要参考。 展开更多
关键词 轻烃燃气 气体分布器 气液两相流 数值模拟
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混空轻烃燃气动力黏度计算研究 被引量:1
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作者 梁远桥 李远玲 +3 位作者 朱璟琦 刘家豪 刘涛 宋光辉 《云南化工》 CAS 2020年第12期70-72,共3页
确定了空气与轻烃燃气的混合比,类比混合气体动力黏度计算法则,采用平方根规律法和REFPROP软件计算出不同混合比下混空轻烃燃气的动力黏度,得到混空轻烃燃气动力黏度较准确的计算方法。结果表明,平方根规律法和REFPROP软件计算得到的混... 确定了空气与轻烃燃气的混合比,类比混合气体动力黏度计算法则,采用平方根规律法和REFPROP软件计算出不同混合比下混空轻烃燃气的动力黏度,得到混空轻烃燃气动力黏度较准确的计算方法。结果表明,平方根规律法和REFPROP软件计算得到的混空轻烃燃气动力黏度值相差不大,可以为混空轻烃燃气管网设计和水力计算提供数据参考。 展开更多
关键词 轻烃燃气 城市燃气 动力黏度 管网设计
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混空轻烃燃气液相析出成核热力学分析 被引量:4
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作者 袁淑霞 张哲锋 +1 位作者 樊玉光 张雄 《过程工程学报》 CAS CSCD 北大核心 2021年第1期116-124,共9页
混空轻烃燃气是将液态轻烃原料汽化、与空气按一定比例混合制成的可燃气体,是一种清洁燃料。但以戊烷为主的轻烃原料常温下为液态,汽化混合后的燃气存在露点较高问题。采用成核热力学理论研究局部温度、压力变化引起的相变/成核驱动力,... 混空轻烃燃气是将液态轻烃原料汽化、与空气按一定比例混合制成的可燃气体,是一种清洁燃料。但以戊烷为主的轻烃原料常温下为液态,汽化混合后的燃气存在露点较高问题。采用成核热力学理论研究局部温度、压力变化引起的相变/成核驱动力,进而研究液滴的成核能,得到混空轻烃燃气液相析出的成核机理、成核能及其与过冷度和过饱和度的关联关系。结果表明,相变/成核所需过冷度和过饱和度随温度、压力的增加而降低;尽管发生完全相变所需过冷度及过饱和度较高,较难达到,但液相析出成核所需过冷度及过饱和度则极易达到,因此防止燃料露点形成的重点是控制从成核到完全相变的发生。 展开更多
关键词 轻烃燃气 成核热力学 露点 过冷度 过饱和度
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Experimental Study on Emission Control of Premixed Catalytic Combustion of Natural Gas Using Preheated Air 被引量:2
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作者 许考 刘中良 +2 位作者 何洪 程水源 马重芳 《Chinese Journal of Chemical Engineering》 SCIE EI CAS CSCD 2007年第1期68-74,共7页
In this paper the premixed catalytic combustion emissions such as CO, unburned hydrocarbon (UHC), NOx and the temperature distribution in the catalytic monolith with ultra low concentration of Pd were studied. Three t... In this paper the premixed catalytic combustion emissions such as CO, unburned hydrocarbon (UHC), NOx and the temperature distribution in the catalytic monolith with ultra low concentration of Pd were studied. Three types of monoliths were used for experiments and the temperature of preheated air was respectively 50℃ , 100℃ and 200℃ . The results showed that preheated air made radial temperature in the catalytic monolith uniform which helped to avoid local hot spots so as to decrease NOx emission. The experiment also proved that the shorter monolith showed much better catalytic combustion performance than longer one and the temperature at the exit of the shorter monolith was relatively lower. On the contrary, the temperature was higher in the longer monolith and the lethal NOx emission was slightly increased. 展开更多
关键词 catalytic combustion preheated air natural gas EMISSION
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Thermodynamic Equilibrium for Mixtures of Combustible Gases and Air
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作者 Richard Martin Gibbons 《Journal of Energy and Power Engineering》 2016年第9期561-565,共5页
Standard treatments of thermodynamic equilibrium are incomplete. They do not take account of all factors determining equilibrium, cannot explain why many systems do not reach equilibrium and do not discuss the questio... Standard treatments of thermodynamic equilibrium are incomplete. They do not take account of all factors determining equilibrium, cannot explain why many systems do not reach equilibrium and do not discuss the questions of reaching and maintaining equilibrium. The arguments presented here provide a single physical definition of thermodynamic equilibrium that accounts for all factors determining thermodynamic equilibrium for mixtures of combustible gases and air. Based on the standard delrmition of thermodynamic equilibrium, the MBD (Maxwell Boltzmann distribution) and a simple molecular model lead to three possible types of equilibrium. The regions of temperature pressure and composition for each type of equilibrium are defined by the measured values of ignition temperatures and the explosive and flammability limits. How this definition of thermodynamic equilibrium can be extended to all molecular systems is discussed in the following papers. 展开更多
关键词 THERMODYNAMICS EQUILIBRIUM Gibbs function statistical mechanics thermo-physical properties
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Single-step chemistry model and transport coefficient model for hydrogen combustion 被引量:3
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作者 WEN Jennifer WANG ChangJian +1 位作者 LU ShouXiang GUO Jin 《Science China(Technological Sciences)》 SCIE EI CAS 2012年第8期2163-2168,共6页
To satisfy the needs of large-scale hydrogen combustion and explosion simulation,a method is presented to establish single-step chemistry model and transport model for fuel-air mixture.If the reaction formula for hydr... To satisfy the needs of large-scale hydrogen combustion and explosion simulation,a method is presented to establish single-step chemistry model and transport model for fuel-air mixture.If the reaction formula for hydrogen-air mixture is H2+0.5O2→H2O,the reaction rate model is ?? =1.13×10?5[H2][O2]exp(?46.37T0/T) mol(cm3 s)?1,and the transport coefficient model is ?=K/CP=ρD=7.0×10?5T 0.7 g(cm s)?1.By using current models and the reference model to simulate steady Zeldovich-von Neumann-Doering(ZND) wave and free-propagating laminar flame,it is found that the results are well agreeable.Additionally,deflagration-to-detonation transition in an obstructed channel was also simulated.The numerical results are also well consistent with the experimental results.These provide a reasonable proof for current method and new models. 展开更多
关键词 hydrogen combustion singe-step chemistry model transport coefficient model
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Experimental Investigation on Plasma-assisted Combustion Characteristics of Premixed Propane/Air Mixture 被引量:1
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作者 LIU Xingjian HE Liming +2 位作者 YU Jinlu ZENG Hao JIN Tao 《Journal of Thermal Science》 SCIE EI CAS CSCD 2015年第3期283-289,共7页
A detailed study on the plasma-assisted combustion(PAC) characteristics of premixed propane/air mixture is presented. The PAC is measured electrically, as well as optically with a multichannel spectrometer. The charac... A detailed study on the plasma-assisted combustion(PAC) characteristics of premixed propane/air mixture is presented. The PAC is measured electrically, as well as optically with a multichannel spectrometer. The characteristics are demonstrated by stable combustion temperature and combustion stability limits, and the results are compared with conventional combustion(CC). Stable combustion temperature measurements show that the introduction of PAC into combustion system can increase the stable combustion temperature, and the increment is more notable with an increase of discharge voltage. Besides, the rich and weak limits of combustion stability are both enlarged when plasma is applied into the combustion process and the increase of discharge voltage results in the expansion of combustion stability limits as well. The measurements of temperature head and emission spectrum illustrate that the kinetic enhancement caused by reactive species in plasma is the main enhancement pathway for current combustion system. 展开更多
关键词 Plasma-assisted combustion Stable combustion temperature Combustion stability limits Mechanism
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On the Controlling Factor of Catalyst Temperature in C_3H_8-Air Mixture
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作者 Goro ONUMA ,Mitsuaki TANABE, Kiyoshi AOKI (Department of Aerospace Engineering, College of Science and Technology, Nihon University 7-24-l Narashinodai, Funabashi, Chiba, 274-8501, Japan) 《Journal of Thermal Science》 SCIE EI CAS CSCD 2001年第1期87-91,共5页
Catalytic combustion of propane-air mixture was investigated. Platinum catalysts over a flat stainless steel with γ- alumina washcoat were employed. The employed burner has three catalysts set parallel to the mixture... Catalytic combustion of propane-air mixture was investigated. Platinum catalysts over a flat stainless steel with γ- alumina washcoat were employed. The employed burner has three catalysts set parallel to the mixture flow, spaced at an interval of 5, 10 and 15 mm. Both experiment and numerical simulation were made at inlet temperature of 553 K, inlet velocity of 3 to 7 m/s and equivalence ratio of 0.3 to 0.5. In the numerical simulation, two-dimensional,. steady state model was developed to calculate the temperature and species concentration in gas-phase. In this model, chemical reaction on the catalyst surface and that in the gas phase were assumed to occur in three-steps. The numerical results show good agreement with experimental results. It was found that the properties of the catalyst strongly affect the catalyst surface temperature. Especially, the thermal conductivity of catalysthas a great effect, while the emissivity of catalyst has less effect. 展开更多
关键词 catalytic combustion surface temperature.
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Experimental Investigation on Ignition and Lean Blow-out Performance of a Multi-sector Centrally Staged Combustor 被引量:2
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作者 LIU Fuqiang ZHANG Kaiyu +4 位作者 MU Yong LIU Cunxi YANG Jinhu Xu Gang ZHU Junqiang 《Journal of Thermal Science》 SCIE EI CAS CSCD 2014年第5期480-485,共6页
Improvement on extinction and pollution emission have become one of the most prominent research topics in gas turbine.It is widely recognized that the fuel/air mixture distribution in the recirculation zone is a criti... Improvement on extinction and pollution emission have become one of the most prominent research topics in gas turbine.It is widely recognized that the fuel/air mixture distribution in the recirculation zone is a critical factor in improving lean blow-out(LBO) and ignition.This paper proposed a new low emission scheme with fuel staged centrally and hybrid injector to improve flameout and emission.A relative small amount of fuel enters into central pilot airblast atomizer burner and then atomized by inner swirl air.The remaining majority of fuel is directly injected into vane channels of the primary swirler through a series of holes located on the sidewall of the main stage.Only pilot stage is fueled under ignition and lean flameout condition.The uniformity of fuel/air mixture distribution in the primary zone of the new design decreases NOX emission,meanwhile the fuel air mixture in pilot recirculation zone is locally rich to improve flameout and ignition.Experimental investigation was conducted to compare the new scheme with baseline design of dual-swirler in terms of LBO and ignition characteristics under the same condition in a multi-sector combustor.It is found that the fuel-air ratio of ignition limit and LBO decrease with the reference velocity increasing.The experimental results also show that the new scheme successfully improve lean blow-out and broaden the operation range of the combustor.The experimental results indicated that the centrally staged scheme can widen the operation boundary of the combustor and can provide guidance for design and optimization of combustion chamber. 展开更多
关键词 Ignition Lean blow-out Staged combustor Pilot stage Fuel air ratio
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Flame Propagation Through Concentration Gradient
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作者 JunyaIINO MitsuakiTANABE 《Journal of Thermal Science》 SCIE EI CAS CSCD 2000年第4期371-375,共5页
The experiment was carried out in homogeneous propane-air mixture and in several concentration gradient of mixture. Igniter is put on the upper side of the combustion chamber In concentration gradient experiment, fixt... The experiment was carried out in homogeneous propane-air mixture and in several concentration gradient of mixture. Igniter is put on the upper side of the combustion chamber In concentration gradient experiment, fixture was ignited from lean side. An experimental study was conducted in a combustion chamber. The combustion chamber has glass windows for optical measurements at any side. For the measurement of distribution of fuel concentration, infrared absorption method using 3.39μm He-Ne laser was used, and for the observation of propagating flame, Schlieren method was employed. As a measurement result of flame propagation velocity and flammable limit, for a mixture of an identical local equivalence ratio, flame propagation velocity in concentration gradient is faster than that in homogeneous mixture, and rich flammable limit in concentration gradient shows a tendency to be higher than that in homogeneous mixture. 展开更多
关键词 COMBUSTION name propagation homogeneous mixture concentration gradient local equivalence ratio.
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