Experimental study on ignition characteristics of an integrated inclined combustor

被引:0
作者
Wang, Ge [1 ,2 ]
Yang, Xu [1 ]
Li, Wei [1 ]
Gao, Yi [3 ]
Liu, Yunpeng [1 ]
Yan, Yingwen [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Energy & Power Engn, Nanjing, Peoples R China
[2] Aero Engine Corp China, Hunan Aviat Powerplant Res Inst, Zhuzhou, Peoples R China
[3] Shanghai Jiao Tong Univ, Sch Aeronaut & Astronaut, Shanghai, Peoples R China
关键词
Inclined combustor; Experimental investigation; Ignition property; Flame propagation; Ignition time; ANNULAR COMBUSTOR; SPARK-IGNITION; DYNAMICS; SPRAY;
D O I
10.1016/j.fuproc.2024.108142
中图分类号
O69 [应用化学];
学科分类号
081704 ;
摘要
To obtain the ignition performance of an integrated inclined combustor, we perform an experimental study on the ignition performance of an inclined combustor under various ignition positions, inlet flow rates, and fuel air ratios (FARs). The experimental results reveal the following. 1) During ignition at I1, the inclined combustor presents the best ignition performance. 2) The forward propagation process of flame along the swirler's inclined direction easily realizes flame propagation, whereas the backward flame propagation process in the swirler's inclined direction is difficult to achieve; forward and backward flame propagations exhibit evident differences. 3) The diffusion propagation of swirl flames at the ignition head is the main means swirl flames are generated at the nonignition head. 4) During the ignition process, the combustion intensity increases with the increase in FAR and decreases with the increase in inlet flow rate. 5) The successful ignition time decreases with the increase in inlet flow rate and FAR.
引用
收藏
页数:13
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