Spray, flowfield, and combustion characteristics of an external mixing atomizer in a novel cavity-swirler-based combustor

被引:6
|
作者
He, Wu [1 ,2 ]
Zhao, Yuling [3 ]
Fan, Weijun [1 ]
机构
[1] Beihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China
[2] China Beijing Power Machinery Res Inst, Beijing 100074, Peoples R China
[3] Jiangsu Univ, Sch Energy & Power, Zhenjiang 212003, Peoples R China
基金
中国国家自然科学基金;
关键词
TRAPPED-VORTEX; PERFORMANCE; KEROSENE; COMPACT;
D O I
10.1063/5.0184223
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
This paper presents an investigation into the performance of two external mixing atomizers designed for a novel cavity-swirler-based combustor, with the aim of achieving high combustion efficiency and uniform outlet temperature distribution. Experimental and numerical analyses were conducted to study the spray characteristics of the atomizers, including the Sauter mean diameter (SMD) and spray angle. The flow field, combustion efficiency, outlet temperature distribution, and pattern factor of the two atomizers were examined under atmospheric pressure and a temperature of 473 K. The results show that the external mixing prefilming atomizer (case-1) exhibits larger SMD and spray angle compared to the external mixing pressure-swirl atomizer (case-2). Furthermore, case-1 demonstrates higher combustion efficiency than case-2 under pilot-only fueling conditions, which is attributed to the larger wake regions achieved by case-1. Interestingly, under pilot-main fueling conditions, case-2 achieves higher combustion efficiency than case-1. This is due to the smaller SMD and longer residence time achieved by case-2. Moreover, case-1 demonstrates more uniform outlet temperature distribution and smaller pattern factor than case-2. This is mainly attributed to the large-scale axial vortex generated by case-2, which significantly improves the mixing intensity between cavity and mainstream.
引用
收藏
页数:19
相关论文
共 33 条
  • [31] Numerical investigation on implications of four strut injectors on combustion characteristics of a Doubly-Dual cavity-based scramjet combustor
    Suneetha, Lakka
    Randive, Pitambar
    Pandey, K. M.
    INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 45 (56) : 32128 - 32144
  • [32] Numerical investigation on the combustion characteristics of boron powder fuel under H2/Air flame in a supersonic cavity-based combustor
    Han, Wenxue
    Hu, Chunbo
    Li, Junjie
    Yang, Jinyuan
    Wei, Ronggang
    Lei, Rong
    Li, Chao
    INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2024, 53 : 343 - 352
  • [33] Comparison of combustion characteristics of four strut injectors with that of three strut injectors by numerically investigating doubly-dual cavity-based scramjet combustor
    Kireeti, S. K.
    Sastry, G. Ravi Kiran
    Gugulothu, S. K.
    Deepanraj, B.
    Sundar, L. Syam
    Arthi, M.
    SUSTAINABLE ENERGY TECHNOLOGIES AND ASSESSMENTS, 2022, 53