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首页> 外文期刊>Applied thermal engineering: Design, processes, equipment, economics >Influence of fuel volatility and spray parameters on combustion characteristics and NO_x emission in a gas turbine combustor
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Influence of fuel volatility and spray parameters on combustion characteristics and NO_x emission in a gas turbine combustor

机译:燃料挥发性和喷雾参数对燃气轮机燃烧室燃烧特性和NO_x排放的影响

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The main thrust in research in the field of gas turbine combustion centers around a clean emission, a low liner wall temperature, a desirable exit temperature distribution for turbo-machinery applications along with a fuel economy of the combustion process. An attempt to meet the challenge has been made in the present paper in developing a computational model based on stochastic separated flow analysis of a typical diffusion controlled spray combustion of liquid fuel in a gas turbine combustor to study the influences of fuel volatility and different spray parameters on combustion and emission characteristics. A k–ε model with wall function treatment for near wall region has been adopted for the solution of conservation equations in gas phase. The initial spray parameters are specified by a suitable probability distribution function size distribution and a given spray cone angle. A radiation model for the gas phase, based on first order moment method, has been adopted in consideration of the gas phase as a gray absorbing–emitting medium. Formation of thermal NO_x as a post-combustion reaction process, is determined from Zeldovich mechanism. It is recognized that the combustion efficiency is reduced drastically with a decrease in fuel volatilities at lower spray cone angle. For a given fuel, there is a significant reduction in combustion efficiency at a lower spray cone angle and lower initial SMD. The pattern factor of exit temperature distribution is reduced with a decrease in initial SMD, for all fuels. The influence of spray cone angle on pattern factor is contrasting in nature for fuels with higher and lower volatilities. The pattern factor decreases with an increase in spray cone angle for a higher volatile fuel, whereas, the reverse happens in case of lower volatile fuels. It is found that the bulk exit NOx increases with a decrease in fuel volatility for any given set of values of spray parameters. An increase in spray cone angle increases bulk exit NOx especially for lower volatile fuels, and an increase in initial SMD increases the bulk exit NOx for lower volatile fuels only.
机译:燃气涡轮机燃烧领域的研究重点在于清洁排放,低衬里壁温度,涡轮机械应用所需的出口温度分布以及燃烧过程的燃料经济性。为了开发一种基于随机分离流分析的计算模型,该模型是对燃气轮机燃烧室中液体燃料的典型扩散控制喷雾燃烧的研究,以应对该挑战,以研究燃料挥发性和不同喷雾参数的影响。燃烧和排放特性。气相守恒方程的求解采用了在近壁区域进行壁函数处理的k–ε模型。初始喷雾参数由合适的概率分布函数大小分布和给定的喷雾锥角指定。考虑到气相作为灰色吸收发射介质,已采用基于一阶矩法的气相辐射模型。根据Zeldovich机理确定了作为燃烧后反应过程的热NO_x的形成。已经认识到,在较低的喷雾锥角下,燃烧效率随着燃料挥发性的降低而大大降低。对于给定的燃料,在较低的喷雾锥角和较低的初始SMD下,燃烧效率会大大降低。对于所有燃料,出口温度分布的模式因数随初始SMD的减小而减小。喷雾锥角对模式因子的影响本质上是具有较高和较低挥发性的燃料的对比。对于较高的挥发性燃料,模式因子随喷雾锥角的增加而减小,而在较低的挥发性燃料的情况下则相反。已经发现,对于任何给定的喷雾参数值组,总体出口NOx随着燃料挥发性的降低而增加。喷雾锥角的增加会增加大量出口的NOx,特别是对于挥发性较低的燃料,而初始SMD的增加只会增加挥发性较低的燃料的出口NOx。

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