| Citation: | XU Xinting, ZENG Wen, LIU Kai, et al. Experimental testing and numerical calculation of flow field characteristics in a double stage axial swirl combustor[J]. Journal of Aerospace Power, 2025, 40（10）：20230776 doi: 10.13224/j.cnki.jasp.20230776
|
The flow field structure and characteristics in a double stage axial swirl combustion chamber of an aero-engine were experimentally tested and numerically calculated, and the flow field structure, streamline and velocity distribution characteristics on the different longitudinal and cross sections in the combustion chamber under different conditions were obtained. The results showed that there were two symmetric distribution angle recirculation zones and one central recirculation zone on the longitudinal section in the combustion chamber. With the increase of distance along the positive
| [1] |
MEIER W, DUAN X R, WEIGAND P. Investigations of swirl flames in a gas turbine model combustor: Ⅱ turbulence-chemistry interactions[J]. Combustion and Flame, 2006, 144(1/2): 225-236.
|
| [2] |
JOHNSON M R, LITTLEJOHN D, NAZEER W A, et al. A comparison of the flowfields and emissions of high-swirl injectors and low-swirl injectors for lean premixed gas turbines[J]. Proceedings of the Combustion Institute, 2005, 30(2): 2867-2874. doi: 10.1016/j.proci.2004.07.040
|
| [3] |
DHANUKA S K, TEMME J E, DRISCOLL J F, et al. Vortex-shedding and mixing layer effects on periodic flashback in a lean premixed prevaporized gas turbine combustor[J]. Proceedings of the Combustion Institute, 2009, 32(2): 2901-2908. doi: 10.1016/j.proci.2008.06.155
|
| [4] |
胡建, 郑婷婷, 胡好生, 等. 双级旋流器偏心对出口流场影响[J]. 航空动力学报, 2020, 35(7): 1447-1456. HU Jian, ZHENG Tingting, HU Haosheng, et al. Double-swirler misalignment effect on outlet flow field[J]. Journal of Aerospace Power, 2020, 35(7): 1447-1456. (in Chinese
HU Jian, ZHENG Tingting, HU Haosheng, et al. Double-swirler misalignment effect on outlet flow field[J]. Journal of Aerospace Power, 2020, 35(7): 1447-1456. (in Chinese)
|
| [5] |
于锦峰, 郭志辉, 张君锋, 等. 套筒长度对火焰筒流场和雾化特性的影响[J]. 航空动力学报, 2009, 24(11): 2506-2513. YU Jinfeng, GUO Zhihui, ZHANG Junfeng, et al. Experimental study the effect of flare sleeve length on the flowfield and spray characterization of a combustor swirl cup[J]. Journal of Aerospace Power, 2009, 24(11): 2506-2513. (in Chinese
YU Jinfeng, GUO Zhihui, ZHANG Junfeng, et al. Experimental study the effect of flare sleeve length on the flowfield and spray characterization of a combustor swirl cup[J]. Journal of Aerospace Power, 2009, 24(11): 2506-2513. (in Chinese)
|
| [6] |
YAN Y W, LIU Y P, LIU Y C, et al. Experimental and computational investigations of flow dynamics in LPP combustor[J]. The Aeronautical Journal, 2017, 121(1240): 790-802. doi: 10.1017/aer.2017.31
|
| [7] |
邓远灏, 颜应文, 党龙飞, 等. 贫油预混预蒸发低污染燃烧室流场特性试验[J]. 航空动力学报, 2015, 30(10): 2416-2424. DENG Yuanhao, YAN Yingwen, DANG Longfei, et al. Experiment of flow field characteristics in a lean premixed prevaporized low emission combustor[J]. Journal of Aerospace Power, 2015, 30(10): 2416-2424. (in Chinese
DENG Yuanhao, YAN Yingwen, DANG Longfei, et al. Experiment of flow field characteristics in a lean premixed prevaporized low emission combustor[J]. Journal of Aerospace Power, 2015, 30(10): 2416-2424. (in Chinese)
|
| [8] |
WANG Shanwu, YANG V, HSIAO G, et al. Large-eddy simulations of gas-turbine swirl injector flow dynamics[J]. Journal of Fluid Mechanics, 2007, 583: 99-122. doi: 10.1017/S0022112007006155
|
| [9] |
VASHAHI F, LEE S, LEE J. Experimental and computational analysis of the swirling flow generated by an axial counter-rotating swirler in a rectangular model chamber using water test rig[J]. Journal of Engineering for Gas Turbines and Power, 2017, 139(8): 081501. doi: 10.1115/1.4035734
|
| [10] |
VASHAHI F, LEE J. On the emerging flow from a dual-axial counter-rotating swirler; LES simulation and spectral transition[J]. Applied Thermal Engineering, 2018, 129: 646-656. doi: 10.1016/j.applthermaleng.2017.10.058
|
| [11] |
XIAO Wei, HUANG Yong. Lean blowout limits of a gas turbine combustor operated with aviation fuel and methane[J]. Heat and Mass Transfer, 2016, 52(5): 1015-1024. doi: 10.1007/s00231-015-1622-3
|
| [12] |
赵婷杰, 于小兵, 卢铭涛, 等. 旋流杯燃烧室头部冷却设计及其对壁温的影响[J]. 航空动力学报, 2023, 38(8): 1975-1983. ZHAO Tingjie, YU Xiaobing, LU Mingtao, et al. Cooling design for head of swirl-cup combustor and its effect on wall temperature[J]. Journal of Aerospace Power, 2023, 38(8): 1975-1983. (in Chinese
ZHAO Tingjie, YU Xiaobing, LU Mingtao, et al. Cooling design for head of swirl-cup combustor and its effect on wall temperature[J]. Journal of Aerospace Power, 2023, 38(8): 1975-1983. (in Chinese)
|
| [13] |
DHANUKA S K, TEMME J E, DRISCOLL J F. Lean-limit combustion instabilities of a lean premixed prevaporized gas turbine combustor[J]. Proceedings of the Combustion Institute, 2011, 33(2): 2961-2966. doi: 10.1016/j.proci.2010.07.011
|
| [14] |
FU Yongqiang, CAI Jun, ELKADY A, et al. Fuel and equivalence ratio effects on spray combustion of a counter-rotating swirler[C]// Aerospace Sciences Meeting and Exhibit. Reno, US: AIAA, 2005: 0354.1-0354.13.
|
| [15] |
DHANUKA S K. An experimental study of the stable and unstable operation of an LPP gas turbine combustor[D]. Ann Arbor, US: University of Michigan, 2008.
|
| [16] |
FU Yongqiang, CAI Jun, JENG S M, et al. Characteristics of the swirling flow generated by a counter-rotating swirler[C]//43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Cincinnati, US: AIAA, 2007: 5690.1-5690.11.
|
| [17] |
常峰, 林宏军, 程明, 等. 低旋流中心分级燃烧室流场特性研究[J]. 推进技术, 2020, 41(6): 1334-1339. CHANG Feng, LIN Hongjun, CHENG Ming, et al. Study on flow field characteristics of low swirl concentric staged combustor[J]. Journal of Propulsion Technology, 2020, 41(6): 1334-1339. (in Chinese
CHANG Feng, LIN Hongjun, CHENG Ming, et al. Study on flow field characteristics of low swirl concentric staged combustor[J]. Journal of Propulsion Technology, 2020, 41(6): 1334-1339. (in Chinese)
|
| [18] |
闫东博, 张群, 汪玉明, 等. 双级轴向旋流器性能评估方法(一): 综合旋流强度的影响[J]. 航空动力学报, 2017, 32(7): 1592-1598. YAN Dongbo, ZHANG Qun, WANG Yuming, et al. Performance evaluation methods of two-stage axial swirler: Ⅰinfluence of total swirling intensity[J]. Journal of Aerospace Power, 2017, 32(7): 1592-1598. (in Chinese
YAN Dongbo, ZHANG Qun, WANG Yuming, et al. Performance evaluation methods of two-stage axial swirler: Ⅰinfluence of total swirling intensity[J]. Journal of Aerospace Power, 2017, 32(7): 1592-1598. (in Chinese)
|
| [19] |
张群, 闫东博, 邢力, 等. 双级轴向旋流器性能评估方法(二): 旋流器下游几何结构的影响[J]. 航空动力学报, 2017, 32(8): 1809-1814. ZHANG Qun, YAN Dongbo, XING Li, et al. Performance evaluation methods of two-stage axial swirlers: Ⅱ influence of swirler rear geometric structure[J]. Journal of Aerospace Power, 2017, 32(8): 1809-1814. (in Chinese
ZHANG Qun, YAN Dongbo, XING Li, et al. Performance evaluation methods of two-stage axial swirlers: Ⅱ influence of swirler rear geometric structure[J]. Journal of Aerospace Power, 2017, 32(8): 1809-1814. (in Chinese)
|
| [20] |
汪玉明, 肖为, 王志凯, 等. 双级轴向旋流器气量分配对流场特性影响的数值模拟与试验验证[J]. 航空发动机, 2022, 48(1): 26-32. WANG Yuming, XIAO Wei, WANG Zhikai, et al. Numerical simulation and test verification of the influence of airflow splits on the flow field characteristics in dual-axial swirlers[J]. Aeroengine, 2022, 48(1): 26-32. (in Chinese
WANG Yuming, XIAO Wei, WANG Zhikai, et al. Numerical simulation and test verification of the influence of airflow splits on the flow field characteristics in dual-axial swirlers[J]. Aeroengine, 2022, 48(1): 26-32. (in Chinese)
|
| [21] |
韩启祥, 许铁军, 黄健. 双旋流器单头部模型燃烧室冷态流场试验[J]. 航空动力学报, 2008, 23(8): 1370-1374. HAN Qixiang, XU Tiejun, HUANG Jian. Experimental study of flow field of a model combustor with two swirlers[J]. Journal of Aerospace Power, 2008, 23(8): 1370-1374. (in Chinese
HAN Qixiang, XU Tiejun, HUANG Jian. Experimental study of flow field of a model combustor with two swirlers[J]. Journal of Aerospace Power, 2008, 23(8): 1370-1374. (in Chinese)
|
DownLoad:
