Effect of swirl cup's primary swirl number on ignition performance
-
摘要: 所有的旋流杯结构均为一级多斜孔和二级径向直叶片,喷嘴均为单油路离心喷嘴.为了研究旋流杯空气雾化喷嘴一级旋流数对小型燃烧室点火性能的影响,采用单头部矩形回流燃烧室,在进口为常温常压、燃烧室压降为0.5%~5%的条件下,对3个一级旋流数不同的旋流杯进行了点火实验.实验结果表明:一级旋流数对点火性能影响明显,相同压降下,一定变化范围内,一级旋流数的增加影响了下游流场的分布,有利于火核沿回流区向上游传播,并在旋流杯出口形成稳焰,因此一级强旋旋流杯点火性能更好.Abstract: All swirl cups have the same primary inclined multi hole and secondary radial straight blade and a simplex pressure atomizer. The effects of primary swirl number of airblast atomizer on small combustion ignition performance were examined. The ignition experiments for swirl cups with three different primary swirl numbers were conducted under atmospheric pressure and temperature in a rectangular reflux combustion chamber, and the pressure drop across the flame tube was between 0.5% and 5% of inlet total pressure. The experimental results show that the primary swirl number significantly influence the ignition performance. Under the same pressure drop, within a certain range, the increase of primary swirl number affects the downstream flow field distribution, which is beneficial for fire nuclear spreading along the upstream of recirculation region and forming a steady flame in the swirl cup exit. So the swirl cup with strong primary vortex has better ignition performance.
-
[1] 方昌德.世界航空发动机手册[M].北京:航空工业出版社, 1996. Fang C D.World aviation engine mannual[M].Beijing:Aviation Industry Press, 1996(in Chinese). [2] 彭云晖, 林宇震, 许全宏, 等.双旋流空气雾化喷嘴喷雾、流动和燃烧性能[J].航空学报, 2008, 29(1):1-14. Peng Y H, Lin Y Z, Xu Q H, et al.Atomization, aerodynamics and combustion performance of swirl cup[J].Acta Aeronautica et Astronautica Sinica, 2008, 29(1):1-14(in Chinese). [3] 林宇震, 许全宏, 刘高恩.燃气轮机燃烧室[M].北京:国防工业出版社, 2008:107. Lin Y Z, Xu Q H, Liu G E.Gas turbine combustor[M].Beijing:National Defence Industry Press, 2008:107(in Chinese). [4] 徐华胜, 黄义勇, 王秀兰.喷嘴供油特性对双旋流器头部气动雾化效果的影响研究[J].燃气涡轮试验与研究, 2004, 17(2):14-17. Xu H S, Huang Y Y, Wang X L.Study on the effect of fuel jet characteristics on airblast atomization performance for device with two-stage swirler[J].Gas Turbine Experiment and Research, 2004, 17(2):14-17(in Chinese). [5] Hsiao G, Mongia H C, Vij A.Swirl cup modeling part Ⅱ:inlet boundary conditions, AIAA-2003-1350[R].Reston:AIAA, 2003. [6] Hsiao G, Mongia H C.Swirl cup modeling part Ⅲ:grid independent solution with different turbulence models, AIAA-2003-1349[R].Reston:AIAA, 2003. [7] Cai J, Fu Y, Elkadi A, et al.Swirl cup modeling part Ⅳ:effect of confinement on flow characteristics, AIAA-2003-0486[R].Reston:AIAA, 2003. [8] Wang S, Yang V, Mongia H C, et al, Modeling of gas turbine swirl cup dynamics, part Ⅴ:Large eddy simulation of cold flow, AIAA-2003-0485[R].Reston:AIAA, 2003. [9] Stevens E J, Held T J, Mongia H C.Swirl cup modeling part Ⅷ:spray combustion in CFM-56 single cup flame tube, AIAA-2003-0319[R].Reston:AIAA, 2003. [10] Wang H Y, McDonell V G, Samuelsen G S.Influence of hardware design on the flow field structures and the patterns of droplet dispersion, Part I:mean quantities[J].Journal of Engineering for Gas Turbines and Power, 1995, 117(2):282-289. [11] Ateshkadi A, McDonell V G, Samuelsen G S.Effect of hardware geometry on gas and drop behavior in a radial mixer spray[J].Proceedings of the 1998 27th International Symposium on Combustion, 1998, 2:1985-1992. [12] 罗国良, 宋双文, 胡好生, 等.旋流杯空气雾化喷嘴套筒出口形状对小型燃烧室点火性能的影响[J].航空动力学报, 2001, 22(8):1708-1712. Luo G L, Song S W, Hu H S, et al.Influences of the swirl cup flares design on the small combustor ignition performance[J].Journal of Aerospace Power, 2011, 22(8):1708-1712(in Chinese). [13] 康尧, 林宇震, 霍伟业, 等.双级旋流杯结构变化对点火特性的影响研究[J].推进技术, 2014, 35(5):675-679. Kang Y, Lin Y Z, Huo W Y, et al.Effect of hardware geometry of dual-stage swirl cup on ignition performance[J].Journal of Propulsion Technology, 2014, 35(5):675-679(in Chinese). [14] 林宇震, 林培华, 许全宏, 等.复合式收扩套筒空气雾化喷嘴燃烧室点火研究[J].航空动力学报, 2007, 28(3):342-346. Lin Y Z, Lin P H, Xu Q H, et al.Research on ignition performance of a hybrid airblast atomizer combustor with convergent-divergent sleeve[J].Journal of Aerospace Power, 2007, 28(3):342-346(in Chinese). [15] 黄勇, 林宇震, 樊未军, 等.燃烧与燃烧室[M].北京:北京航空航天大学出版社, 2006:264. Huang Y, Lin Y Z, Fan W J, et al.Combustion and Combustors[M].Beijing:Beihang University Press, 2006:264(in Chinese).
点击查看大图
计量
- 文章访问数: 1200
- HTML全文浏览量: 151
- PDF下载量: 560
- 被引次数: 0