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
  • [21] Numerical investigation on the combustion characteristics of aluminum powder fuel in a supersonic cavity-based combustor
    Feng, Yanbin
    Luo, Shibin
    Song, Jiawen
    Xia, Kunxiong
    Xu, Dequan
    APPLIED THERMAL ENGINEERING, 2023, 221
  • [22] Variation of inlet boundary conditions on the combustion characteristics of a typical cavity-based scramjet combustor
    Huang, Wei
    Wang, Zhen-Guo
    Yan, Li
    Li, Shi-Bin
    Ingham, Derek B.
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2014, 228 (04) : 627 - 638
  • [23] Effect of fuel temperature on mixing characteristics of a kerosene jet injected into a cavity-based supersonic combustor
    Li, Fei
    Wang, Taiyu
    Yang, Kai
    Zhang, Jincheng
    Wang, Hongbo
    Sun, Mingbo
    Wang, Zhenguo
    Li, Peibo
    PHYSICS OF FLUIDS, 2023, 35 (04)
  • [24] A Comparative Evaluation of Combustion Characteristics of Strut and Wall Injection Technique in a Cavity-Based Scramjet Combustor
    Suneetha, Lakka
    Randive, Pitambar R.
    Pandey, Krishna Murari
    ADVANCES IN MECHANICAL ENGINEERING, ICRIDME 2018, 2020, : 823 - 833
  • [25] Powder fuel transport process and mixing characteristics in cavity-based supersonic combustor with different injection schemes
    Luo, Shibin
    Feng, Yanbin
    Song, Jiawen
    Xu, Dequan
    Xia, Kunxiong
    AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 128
  • [26] Numerical Investigation on the Effect of Inflow Mach Numbers on the Combustion Characteristics of a Typical Cavity-Based Supersonic Combustor
    Bordoloi, Namrata
    Pandey, Krishna Murari
    Sharma, Kaushal Kumar
    MATHEMATICAL PROBLEMS IN ENGINEERING, 2021, 2021
  • [27] Research on the mixing characteristics of a cavity based supersonic combustion chamber coupled with secondary recirculation jets
    Dai, Jian
    Chen, Long
    Kong, Fanchao
    INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2024, 92 : 516 - 526
  • [28] Effect of air-injection mode on mainstream-forced entrainment and combustion characteristics of a cavity-based combustor
    Zhao, Yuling
    Gong, Cheng
    Li, Mingyu
    PHYSICS OF FLUIDS, 2024, 36 (08)
  • [29] Experimental study of ignition and combustion characteristics of ethylene in cavity-based supersonic combustor at low stagnation temperature and pressure
    Xiong, Pengfei
    Zheng, Dong
    Tan, Yu
    Tian, Ye
    Le, Jialing
    AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 109
  • [30] Influence of a double-mixer configuration on the mixing and combustion characteristics of a multibypass combustor for a turbine-based combined cycle engine
    Zhao, Wensheng
    Fan, Weijun
    Zhang, Rongchun
    ENERGY, 2024, 304