Sheykhbaglou Soroush, Ghahremani Amirreza, Tabejamaat Sadegh, Sánchez-Sanz Mario
School of Mechanical, Aerospace, and Maritime Engineering, Amirkabir University of Technology (Tehran Polytechnic), Tehran, Iran.
Departamento de Ingeniería Térmica y de Fluidos, Universidad Carlos III de Madrid, Leganés 28911, Spain.
Heliyon. 2024 Jan 6;10(2):e24250. doi: 10.1016/j.heliyon.2024.e24250. eCollection 2024 Jan 30.
Direct energy conversion systems, such as thermophotovoltaic and thermoelectric generators, have received increasing attention in micro power generation. Micro and meso-scale combustors are one of the most core components in these systems. So, developing combustion stabilization technologies for micro or meso-scale combustors is of great importance. In these systems, a hydrocarbon fuel with high energy density is burned in a micro or meso-scale combustor. Many studies have been conducted to explore various combustion stabilization techniques, but as a novelty, in this work, we study the combustion and thermal performance of a meso-scale micro power generator powered by a swirling fuel jet discharging into a co- or counter-rotating air coflow. To do so, we used 3D-printed axial swirlers with double annulus to form the swirling co- and counter-rotating fuel (methane) jet-air coflow configurations at various air and fuel flow rates. Blow-out limit, flame characteristics, combustor mean outer wall temperature, pollutant emissions, emitter efficiency, and normalized temperature standard deviation are investigated in this study. The results show that swirl addition enhances the blow-out limit significantly and co-rotating swirling flows generally enhances the flame blow-out limit when compared with the counter-rotating swirling flows mode at high fuel flow rates. Moreover, the combustor with co-rotating swirling flows has shorter lift-off height and longer flame length. The sensitivity of the flame lift-off height to an increment of the fuel mass flow rate is smaller in co-rotating than in counter-rotating swirling flows (more than ). Furthermore, it is observed that under the same operating conditions, co-rotating swirling flows exhibit lower values of and in the flue gas and higher values of mean outer wall temperature, combustion efficiency, emitter efficiency, and normalized temperature standard deviation. The enhancement of the emitter efficiency by implementing co-swirl configuration is about , , and for the methane flow rates of , , and , respectively when compared with the counter-swirl mode. The results of this work can provide useful information to choose between co- and counter-rotating flows for combustors of combustion-based micro power generators.
直接能量转换系统,如热光伏和热电发电机,在微型发电领域受到了越来越多的关注。微型和中尺度燃烧器是这些系统中最核心的部件之一。因此,开发微型或中尺度燃烧器的燃烧稳定技术具有重要意义。在这些系统中,具有高能量密度的碳氢化合物燃料在微型或中尺度燃烧器中燃烧。已经进行了许多研究来探索各种燃烧稳定技术,但作为一项创新,在本工作中,我们研究了由旋转燃料射流排放到同向或反向旋转的空气并流中驱动的中尺度微型发电机的燃烧和热性能。为此,我们使用了具有双环的3D打印轴向旋流器,以在各种空气和燃料流速下形成旋转的同向和反向旋转燃料(甲烷)射流 - 空气并流配置。本研究考察了熄火极限、火焰特性、燃烧器平均外壁温度、污染物排放、发射器效率和归一化温度标准差。结果表明,添加旋流显著提高了熄火极限,并且在高燃料流速下,与反向旋转旋流模式相比,同向旋转旋流通常会提高火焰熄火极限。此外,具有同向旋转旋流的燃烧器具有较短的火焰抬升高度和较长的火焰长度。同向旋转时火焰抬升高度对燃料质量流量增加的敏感度比反向旋转时小(超过)。此外,观察到在相同的运行条件下,同向旋转旋流在烟气中的和值较低,而平均外壁温度、燃烧效率、发射器效率和归一化温度标准差的值较高。与反向旋流模式相比,对于甲烷流速分别为、和时,通过实施同向旋流配置,发射器效率的提高分别约为、和。本工作的结果可为基于燃烧的微型发电机燃烧器在同向和反向旋转流之间的选择提供有用信息。