Spray, flowfield, and combustion characteristics of an external mixing atomizer in a novel cavity-swirler-based combustor
被引:6
|
作者:
He, Wu
论文数: 0引用数: 0
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机构:
Beihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China
China Beijing Power Machinery Res Inst, Beijing 100074, Peoples R ChinaBeihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China
He, Wu
[1
,2
]
Zhao, Yuling
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机构:
Jiangsu Univ, Sch Energy & Power, Zhenjiang 212003, Peoples R ChinaBeihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China
Zhao, Yuling
[3
]
Fan, Weijun
论文数: 0引用数: 0
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机构:
Beihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R ChinaBeihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China
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
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.
机构:
Jiangsu Univ, Sch Energy & Power, Zhenjiang 212003, Peoples R ChinaJiangsu Univ, Sch Energy & Power, Zhenjiang 212003, Peoples R China
Zhao, Yuling
Li, Mingyu
论文数: 0引用数: 0
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机构:
Jiangsu Univ Sci & Technol, Sch Energy & Power, Zhenjiang 212003, Peoples R ChinaJiangsu Univ, Sch Energy & Power, Zhenjiang 212003, Peoples R China
Li, Mingyu
Zhou, Tiancheng
论文数: 0引用数: 0
h-index: 0
机构:
Jiangsu Univ Sci & Technol, Sch Energy & Power, Zhenjiang 212003, Peoples R ChinaJiangsu Univ, Sch Energy & Power, Zhenjiang 212003, Peoples R China
Zhou, Tiancheng
Shang, Wei
论文数: 0引用数: 0
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机构:
Zhejiang Institude Turbomachinery & Prop Syst, Huzhou 313200, Peoples R ChinaJiangsu Univ, Sch Energy & Power, Zhenjiang 212003, Peoples R China
Shang, Wei
Ge, Zhenghao
论文数: 0引用数: 0
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机构:
Jiangsu Zhongke Res Ctr Clean Energy & Power, Lianyungang 222000, Peoples R ChinaJiangsu Univ, Sch Energy & Power, Zhenjiang 212003, Peoples R China
机构:
Nanjing Univ Aeronaut & Astronaut, Coll Energy & Power Engn, Jiangsu Prov Key Lab Aerosp Power Syst, Nanjing 210016, Peoples R ChinaNanjing Univ Aeronaut & Astronaut, Coll Energy & Power Engn, Jiangsu Prov Key Lab Aerosp Power Syst, Nanjing 210016, Peoples R China
Zhao, Yuling
He, Xiaomin
论文数: 0引用数: 0
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机构:
Nanjing Univ Aeronaut & Astronaut, Coll Energy & Power Engn, Jiangsu Prov Key Lab Aerosp Power Syst, Nanjing 210016, Peoples R ChinaNanjing Univ Aeronaut & Astronaut, Coll Energy & Power Engn, Jiangsu Prov Key Lab Aerosp Power Syst, Nanjing 210016, Peoples R China
He, Xiaomin
Li, Mingyu
论文数: 0引用数: 0
h-index: 0
机构:
Jiangsu Univ Sci & Technol, Zhenjiang Key Lab Marine Power Equipment Performa, Sch Energy & Power, Zhenjiang 212003, Jiangsu, Peoples R ChinaNanjing Univ Aeronaut & Astronaut, Coll Energy & Power Engn, Jiangsu Prov Key Lab Aerosp Power Syst, Nanjing 210016, Peoples R China
Li, Mingyu
Yao, Kanghong
论文数: 0引用数: 0
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机构:
Nanjing Univ Aeronaut & Astronaut, Coll Energy & Power Engn, Jiangsu Prov Key Lab Aerosp Power Syst, Nanjing 210016, Peoples R ChinaNanjing Univ Aeronaut & Astronaut, Coll Energy & Power Engn, Jiangsu Prov Key Lab Aerosp Power Syst, Nanjing 210016, Peoples R China
机构:
Hypersonic Technology Laboratory, College of Aerospace Engineering, National University of Defense Technology, Changsha,410073, ChinaHypersonic Technology Laboratory, College of Aerospace Engineering, National University of Defense Technology, Changsha,410073, China
Zhao, Zijian
Liu, Chaoyang
论文数: 0引用数: 0
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机构:
Hypersonic Technology Laboratory, College of Aerospace Engineering, National University of Defense Technology, Changsha,410073, ChinaHypersonic Technology Laboratory, College of Aerospace Engineering, National University of Defense Technology, Changsha,410073, China
Liu, Chaoyang
Huang, Wei
论文数: 0引用数: 0
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机构:
Hypersonic Technology Laboratory, College of Aerospace Engineering, National University of Defense Technology, Changsha,410073, ChinaHypersonic Technology Laboratory, College of Aerospace Engineering, National University of Defense Technology, Changsha,410073, China
Huang, Wei
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,
2024,
45
(16):
机构:
Beihang Univ, Res Inst Aeroengine, Xueyuan Rd, Beijing 100191, Peoples R ChinaBeihang Univ, Res Inst Aeroengine, Xueyuan Rd, Beijing 100191, Peoples R China
Ren, Dongliang
Fan, Weijun
论文数: 0引用数: 0
h-index: 0
机构:
Beihang Univ, Sch Energy & Power Engn, Natl Key Lab Sci & Technol Aeroengines Aerothermod, Xueyuan Rd, Beijing 100191, Peoples R ChinaBeihang Univ, Res Inst Aeroengine, Xueyuan Rd, Beijing 100191, Peoples R China
Fan, Weijun
Zhang, Rongchun
论文数: 0引用数: 0
h-index: 0
机构:
Beihang Univ, Res Inst Aeroengine, Xueyuan Rd, Beijing 100191, Peoples R ChinaBeihang Univ, Res Inst Aeroengine, Xueyuan Rd, Beijing 100191, Peoples R China