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Development of high intensity low emission combustor for achieving flameless combustion of liquid fuels

机译:开发用于实现液体燃料无焰燃烧的高强度低排放燃烧器

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This paper presents the experimental and numerical results for a two stage combustor capable of achieving flameless combustion with liquid fuels for different thermal heat inputs of 20, 30, 40 and 60kW and heat release density of 5–15MW/m3. Combustion characteristics and pollutant emissions are studied for three different fuels, kerosene, diesel and gasoline. The influence of droplet diameter on pollutant emissions at all conditions is studied. The fuel and oxidizer are supplied at ambient conditions. The concept of high swirl flows has been adopted to achieve high internal recirculation rates, residence time and increased dilution of the fresh reactants in the primary combustion zone, resulting in flameless combustion mode. Air is injected through four tangential injection ports located near the bottom of the combustor and liquid fuel is injected through a centrally mounted pressure swirl injector. Computational analysis of the flow features shows that decrease in the exit port diameter of the primary chamber increases the recirculation rate of combustion products and helps in achieving the flameless combustion mode. Based on preliminary computational studies, a 30mm primary chamber exit port diameter is chosen for experimental studies. Detailed experimental investigations show that flameless combustion mode was achieved with evenly distributed combustion reaction zone and uniform temperature distribution in the combustor. Pollutant emissions of CO, NOx, CxHyare measured and compared for all operating conditions of different fuels and different thermal inputs. The acoustic emission levels are reduced by 6–8dB as combustion mode shifts from conventional mode to flameless combustion mode.
机译:本文介绍了两级燃烧器的实验和数值结果,该燃烧器能够以20、30、40和60kW的不同热输入和5–15MW / m3的放热密度实现液体燃料的无焰燃烧。研究了三种不同燃料煤油,柴油和汽油的燃烧特性和污染物排放。研究了在所有条件下液滴直径对污染物排放的影响。燃料和氧化剂在环境条件下供应。高涡流的概念已被采用,以实现较高的内部再循环率,停留时间以及在主燃烧区中新鲜反应物的稀释增加,从而实现了无焰燃烧模式。空气通过位于燃烧室底部附近的四个切向喷射口喷射,而液体燃料通过中央安装的压力旋流喷射器喷射。流动特性的计算分析表明,主室出口直径的减小会增加燃烧产物的再循环率,并有助于实现无焰燃烧模式。根据初步的计算研究,选择30mm主腔室出口直径进行实验研究。详细的实验研究表明,在燃烧室内均匀分布的燃烧反应区和均匀的温度分布下实现了无焰燃烧模式。针对不同燃料和不同热输入的所有运行条件,测量并比较了CO,NOx,CxHy的污染物排放。当燃烧模式从传统模式转换为无焰燃烧模式时,声发射级降低6–8dB。

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