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首页> 外文期刊>International journal of aerospace engineering >Flow Characteristics of a Rich-Quench-Lean Combustor-Combined Low-Emission and High-Temperature Rise Combustion
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Flow Characteristics of a Rich-Quench-Lean Combustor-Combined Low-Emission and High-Temperature Rise Combustion

机译:富淬火-稀薄燃烧器结合的低排放和高温上升燃烧的流动特性

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摘要

To determine the flow field structure and flow characteristics of a rich-quench-lean (RQL) combustor-combined low-emission and high-temperature rise combustion, a two-dimensional PIV technology was used to evaluate the effect of aerodynamic and structural parameters on the flow field and flow characteristics of the combustor. The variation in the total pressure loss of the combustor has little effect on the flow field structure of the combustor. However, the variation in the parameters of primary holes significantly affects the structure of the central recirculation zone, the distribution of local recirculation zones in the rich-burn zone and quenching zone, and the average residence time in the quenching zone. On the plane that passes through the center of the primary hole, the variations in the array mode and diameter of primary holes would form entrainment vortexes with different characteristics, thus affecting the position and flow state of local recirculation in the rich-burn zone and the local structure of the central recirculation zone. As the rotational direction of local recirculation coincides with that of the main air flow in the primary zone, the local center recirculation is intensified. In contrast, it is weakened. As the primary holes are located at half height (H/2) of the combustor, the residence time of air flow at the quenching zone can be shortened by 65% through using the staggered structure of primary holes and increasing the momentum of the partial single-hole jet. The quick-mixing process in the quenching zone is not beneficial to increase the number of primary holes and decrease the momentum of the single-hole jet.
机译:为了确定贫油-贫油(RQL)燃烧器组合的低排放和高温上升燃烧的流场结构和流动特性,使用二维PIV技术评估空气动力和结构参数对燃烧室的流场和流动特性。燃烧器的总压力损失的变化对燃烧器的流场结构影响很小。但是,一次孔参数的变化会显着影响中央再循环区的结构,富燃区和淬火区中局部再循环区的分布以及淬火区中的平均停留时间。在穿过初级孔中心的平面上,初级孔的排列模式和直径的变化会形成具有不同特征的夹带涡流,从而影响富燃区和局部燃烧区局部再循环的位置和流动状态。中央回流区的局部结构。由于局部再循环的旋转方向与主要区域中的主要气流的旋转方向一致,因此局部中心再循环得到加强。相反,它被削弱了。由于初级孔位于燃烧室的一半高度(H / 2),通过使用初级孔的交错结构并增加部分单个的动量,可将气流在淬火区的停留时间缩短65%。孔射流。淬火区的快速混合过程不利于增加一次孔的数量并降低单孔射流的动量。

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  • 来源
    《International journal of aerospace engineering 》 |2019年第1期| 4014120.1-4014120.22| 共22页
  • 作者单位

    Nanjing Univ Aeronaut & Astronaut, Key Lab Aeroengine Thermal Environm & Struct, Minist Ind & Informat Technol, 29 Yudao St, Nanjing 210016, Jiangsu, Peoples R China;

    Nanjing Univ Aeronaut & Astronaut, Key Lab Aeroengine Thermal Environm & Struct, Minist Ind & Informat Technol, 29 Yudao St, Nanjing 210016, Jiangsu, Peoples R China;

    Army Engn Univ PLA, Sch Natl Def Engn, 88 Biaoying Rd, Nanjing 210007, Jiangsu, Peoples R China;

    Nanjing Univ Aeronaut & Astronaut, Key Lab Aeroengine Thermal Environm & Struct, Minist Ind & Informat Technol, 29 Yudao St, Nanjing 210016, Jiangsu, Peoples R China;

    Nanjing Univ Aeronaut & Astronaut, Key Lab Aeroengine Thermal Environm & Struct, Minist Ind & Informat Technol, 29 Yudao St, Nanjing 210016, Jiangsu, Peoples R China;

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