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燃气轮机环形燃烧室内燃烧流动的数值模拟 总被引:5,自引:0,他引:5
对一个复杂的GE—F101型工业燃气轮机环形燃烧室,采用Reynolds应力湍流模型(RSM)、EBU—Arrhenius湍流燃烧模型和六通量热辐射模型描述其燃烧流动,应用FLUENT软件进行了三维化学反应流场的数值模拟研究。研究结果表明:旋流和燃料进口射流对燃烧室流内温度和流场分布有着重要的影响;利用数值手段得到燃烧室出口的温度分布以判断其能否满足透平叶片进口温度的要求是可行的;燃烧室工作压强对出口的NO分布有着重要影响。在燃用气体燃料时,燃气轮机的NO排放主要来自于热NO,瞬时NO只占很小一部分。图11参6 相似文献
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利用流体分析软件STAR—CD对某回流式燃气轮机燃烧室的内部流场进行了三维冷态数值模拟及两相流反应数值模拟。建立了燃烧室的三维计算几何模型及计算网格,计算了燃烧室的单相流场及喷雾两相流场。在计算中气相采用N-S方程求解,采用高雷诺数κ-ε湍流模型及SIMPISO算法;液相采用Lagrange法处理,采用颗粒群轨道模型。根据计算结果进行流动分析,为进一步进行燃烧室内部燃烧过程的数值计算分析及改善燃烧室的结构设计、降低排放奠定了基础。 相似文献
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环境温度通过改变燃烧室入口空气温度进而影响燃气轮机燃烧稳定性和NO_x排放。为了掌握预混燃烧模式下环境温度对燃气轮机燃烧稳定性和NO_x排放的影响规律,本文以某重型燃气轮机燃烧室为研究对象,采用SAS湍流模型和涡耗散概念燃烧模型,通过改变环境温度,对多旋流喷嘴燃烧室预混燃烧模式下燃烧稳定性和NO_x排放进行了数值计算。研究结果表明:在燃气轮机预混燃烧模式下,提升燃气轮机环境温度,有利于提高燃烧室燃烧稳定性;环境温度从0℃上升到30℃,在不调整燃料和空气流量的情况下,燃烧室出口NO_x排放质量分数增加97.8%。 相似文献
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微型燃气轮机燃烧室性能的数值研究 总被引:5,自引:0,他引:5
针对Capstone公司的C30微型燃气轮机的燃烧室,采用κ—ε湍流模型、EBU—Ambenius湍流燃烧模型描述其燃烧流动,采用扩展Zeldivch机制描述HOx生成;应用分区结构化网格和SIMPLE算法求解控制方程,进行了三维燃烧流动的数值模拟研究,同时对燃烧室的整体性能进行了分析。通过数值计算及结果分析,着重研究了环型贫燃预混燃烧室的燃烧组织形式对燃烧室性能的影响,并探讨了流动控制板对燃烧室内燃烧流动和燃烧室出口HOx分布的影响。数值研究的主要目的是配合新型微型燃气轮机的研制,获得微型燃气轮机燃烧室的设计经验,为研制既有高燃烧效率和燃烧稳定性,又有低HOx排放特性的燃烧室奠定基础。 相似文献
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以甲烷/空气的湍流射流非预混燃烧为对象,建立二维稳态湍流非预混火焰的小火焰模型.利用湍流流动模型和小火焰模型耦合求解,计算出速度、混合分数、温度以及反应标量的摩尔分数在燃烧室内的分布,模拟结果表明小火焰模型能够用来描述燃烧室内燃烧机理. 相似文献
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惰性气体是一种高效、环保、经济的防、抑爆及消防灭火介质,惰气的来源制约了惰气安全防护技术的研究开发.以一种新型燃惰气燃烧室为研究对象,采用了RNGk-ε双方程模型描述湍流流动,随机颗粒轨道模型追踪燃油颗粒运动,考虑了化学反应动力学机制对燃烧的影响,采用了修正的EBU湍流燃烧模型计算燃烧速率,同时采用了离散坐标法表征辐射传热过程,建立了燃烧室三维气雾两相湍流燃烧模型,对燃烧室流动燃烧特性进行了深入数值模拟研究,模拟结果与实验结果的比较表明了数值模型及数值方法的合理性.在数值模拟的基础上对燃惰气燃烧室进行了优化设计,采用了多种强化燃烧技术.对优化设计燃烧室的数值模拟结果表明设计合理,满足设计要求.研究结果为惰气安全技术的开发设计奠定了基础. 相似文献
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Turbulent reacting flows in a generic swirl gas turbine combustor model are investigated both numerically and experimentally. In the investigation, an emphasis is placed upon the external flue gas recirculation, which is a promising technology for increasing the efficiency of the carbon capture and storage process, which, however, can change the combustion behaviour significantly. A further emphasis is placed upon the investigation of alternative fuels such as biogas and syngas in comparison to the conventional natural gas. Flames are also investigated numerically using the open source CFD software OpenFOAM. In the numerical simulations, a laminar flamelet model based on mixture fraction and reaction progress variable is adopted. As turbulence model, the SST model is used within a URANS concept. Computational results are compared with the experimental data, where a fair agreement is observed. 相似文献
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针对燃气轮机燃油燃烧室改成双燃料燃烧室对燃料喷嘴进行一体化概念设计,并采用CFD技术对其双燃料燃烧流场进行数值模拟。针对燃烧室燃用C7H16和裂解气燃料的不同情况,采用标准κ-ε湍流模型、化学平衡条件下的快速化学反应系统和简单概率密度函数(PDF)燃烧模型、液体燃料的喷雾模型以及SIMPLE算法。模拟并对比分析了两种燃料燃烧时的燃烧效率、出口温度均匀性、壁面最高温度以及速度分布等参数随工况变化的趋势,并得出结论:1)不同燃料燃烧时的流场特征基本保持一致;2)裂解气燃料燃烧时,其燃烧效率较高,但出口温度均匀性较差;3)在加入相同焓值的燃料进入燃烧室时,裂解气燃料燃烧得到的出口温度低于燃油的燃烧状态。 相似文献
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对燃气轮机逆流式环形燃烧室,热态三维流场的数值模拟问题进行了研究,建立了三维计算模型,生成了数值计算网格。数值模拟研究表明,改变燃烧室的几个结构参数,可以得到更加合理的流场。通过对关键截面的流动分析,可以判断燃烧室设计的合理性,为进一步优化燃烧室结构设计、改善流场奠定了基础。 相似文献
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Paolo Gobbato Massimo MasiAndrea Toffolo Andrea Lazzaretto 《International Journal of Hydrogen Energy》2011,36(13):7993-8002
The interest for hydrogen-fuelled combustors is recently growing thanks to the development of gas turbines fed by high content hydrogen syngas. The diffusion flame combustion is a well-known and consolidated technology in the field of industrial gas turbine applications. However, few CFD analyses on commercial medium size heavy duty gas turbine fuelled with pure hydrogen are available in the literature. This paper presents a CFD simulation of the air-hydrogen reacting flow inside a diffusion flame combustor of a single shaft gas turbine. The 3D geometrical model extends from the compressor discharge to the gas turbine inlet (both liner and air plenum are included). A coarse grid and a very simplified reaction scheme are adopted to evaluate the capability of a rather basic model to predict the temperature field inside the combustor. The interest is focused on the liner wall temperatures and the turbine inlet temperature profile since they could affect the reliability of components designed for natural gas operation. Data of a full-scale experimental test are employed to validate the numerical results. The calculated thermal field is useful to explain the non-uniform distribution of the temperature measured at the turbine inlet. 相似文献
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Modelling of combustion performances and emission characteristics of coal gases in a model gas turbine combustor 下载免费PDF全文
In recent years, gas mixtures are being used as alternative fuels in combustors. These gas mixtures are obtained by different methods. For instance, coal gasification and carbonization as coal have the largest reserves among fossil fuels. Gas mixtures obtained via coal gasification and carbonization are called water gas, generator gas, town gas and coke oven gas. These fuels contain various gases. As a result of this, heating values of fuels are also different. Therefore, combustion performances and emission characteristics of these fuels need to be investigated. In this study, combustion performances and emissions including CO, CO2 and NOX of water gas, generator gas, town gases, coke oven gas and methane were numerically investigated in a model gas turbine combustor. The numerical modelling of turbulent nonpremixed diffusion flames has been performed in this combustor. Mathematical models used in this study involved the k–ε model of turbulent flow, the PDF/mixture fraction model of nonpremixed combustion and P‐1 radiation model. A CFD code ANSYS Fluent was used for all numerical investigations. Temperature distributions of axial and radial directions were determined. A NOX post‐processor was used for the prediction of NOX emissions from the gas turbine combustor. Modelling was performed for 60 kW thermal power and different equivalance ratios (i.e. Ф = 0.91, Ф = 0.77 and Ф = 0.67). The studied type 1 model gas turbine combustor was modelled for Ф = 0.91 equivalance ratio. Then, Other equivalance ratios were analysed for type 2 model gas turbine combustor. The effect of dilution air on combustion performances and emission characteristics was also investigated. It is concluded that the coke oven gas, the town gas I, town gas II and the water gas are appropriate for usage as alternative fuel, whereas the generator gas is not suitable for gas turbine combustors. Copyright © 2013 John Wiley & Sons, Ltd. 相似文献
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