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双燃料燃烧器结构对火焰温度对称性影响研究 被引量:2

The Research of the Effect of Dual Fuel Burner's Structure on the Symmetry of Flame Temperature
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摘要 探索了解决双液体燃料混燃燃烧火焰温度场不对称问题的方法以及研究了燃料比对火焰温度场对称性的影响。通过对三种不同结构的双燃料燃烧器进行不同燃料比下的燃烧实验,获得火焰温度场分布,来研究火焰温度场对称性。研究表明:具有2个互成180o对称布置的甲醇燃料喷嘴燃烧器和具有3个互成120o均匀布置的甲醇燃料喷嘴燃烧器,在一定程度上可以提高火焰温度场对称性;燃料比对三种燃烧器的火焰温度场对称性有较大的影响;具有2个互成180o对称布置的甲醇燃料喷嘴和具有3个互成120o均匀布置的甲醇燃料喷嘴的燃烧器火焰温度场对称性差距很小。 A way to solve the problem of dissymmetry temperature of double liquid mixing combustion flame was studied and the effect of fuel ratio on the symmetry of flame temperature field was researched.The flame temperature field distribution was obtained by the combustion exper?iment under different fuel ratios for three different types of dual-fuel burners to study the symmetry of the flame temperature field.The study shows that a burner with two methanol fuel nozzles symmetrically arranged 180 degrees to each other and a burner that are evenly arranged with 120 degrees methanol fuel nozzles can improve the symmetry of the flame temperature field to some degree.The fuel ratio has a great influence on the symmetry of the three burners flame temperature field.The symmetry of the flame temperature field of the burner with two methanol fuel nozzles symmetrically arranged 180 degrees to each other and the burner that are evenly arranged with 120 degrees methanol fuel nozzles is not significant.
作者 张全 武亚男 ZHANG Quan;WU Yanan(School of Energy Science and Engineering,Central South University,Changsha 410083,China)
出处 《工业加热》 CAS 2018年第4期4-6,共3页 Industrial Heating
关键词 燃料喷嘴 温度对称性 燃料比 fuel nozzle temperature symmetry fuel ratio
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  • 1申国强.脉冲燃烧控制技术在燃油时效退火炉上的应用[J].中国铸造装备与技术,2005,40(5):51-53. 被引量:3
  • 2倪维斗.有关新能源发展的思考[R].北京:2009年中阁新能源及可再生能源科技发展沦坛,2009.
  • 3国家标准GBI6663-1996.醇基液体燃料[M].北京:中国标准出版社,1997.
  • 4张全,刘洋,赵军,等.后石油时代的选择--醇基燃料[R].北京:2009年中国新能源及可再生能源科技发展论坛,2009.
  • 5[2]A Waithe Kenrick.Experimental and computational investigation of multiple injection ports in a convergent-divergent nozzle for fluidic thrust vectoring.AIAA 2003-3802.
  • 6[4]A J Hamer,R J Roby.CFD modeling of a gas turbine combustor using reduced chemical kinetic mechanisms.AIAA97-3242.
  • 7[5]E J Fuller,C E Smith.Integrated CFD modeling of gas turbine combustor.AIAA-93 -2196.
  • 8肖劲松,黄建荣.时序脉冲燃烧控制技术在回火炉上的应用[J].金属材料与冶金工程,2007,35(4):50-53. 被引量:13
  • 9BRANDT D E, WESORIEK R R. GE gas turbine design philosophy [R]. GER-3434d, Schenectady.. GE Power Systems, 1994.
  • 10FANACA D, ALEMELA P R, HIRSCH C, et al. Comparison of the flow field of a swirl stabilized premixed burner in an annular and a single burner combustion chamber [J]. Journal of Engineering for Gas Turbines and Power, 2010, 132 (7): 071502-1- 071502-7.

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