| Citation: | LI Xiaoye, LI Jiayi, CHANG Yunxin, et al. Impact of array micro-tube diffusion burner for hydrogen fuel on combustion instability characteristics[J]. Journal of Aerospace Power, 2025, 40（4）：20240566 doi: 10.13224/j.cnki.jasp.20240566
|
A study on a micro-diffusion hydrogen fuel nozzle was conducted through numerical simulations to analyze the flow and combustion characteristics under cold and hot conditions by altering the circumferential spacing of the air injection holes, the diameter of the hydrogen fuel injection holes, and the position of the hydrogen fuel injection holes. Combustion performance experiments were carried out under ambient temperature and pressure (300 K, 101 kPa) and elevated temperature and pressure (300—533 K, 101 kPa) conditions. The effects of three parameters and the design of cooling holes on thermoacoustic oscillation characteristics were investigated, contributing to the identification of the optimal scheme. The research results indicated that the micro-diffusion nozzle generated a corner vortex recirculation zone during thermoacoustic oscillation. Increasing the airflow and temperature can enhance the mixing of air and fuel, thereby suppressing combustion oscillations. Under the intake conditions of 533 K and 101 kPa, the optimal nozzle scheme achieved stable combustion across a wide equivalence ratio, with an amplitude of less than 12.5 Pa and noise levels below 101 dB, providing a reference for the design of hydrogen fuel combustion chambers and other engineering applications.
| [1] |
项目综合报告编写组. 《中国长期低碳发展战略与转型路径研究》综合报告[J]. 中国人口·资源与环境,2020,30(11): 1-25. Project Comprehensive Report Writing Group. Comprehensive report on “China’s long-term low-carbon development strategy and transition pathways”[J]. China Population,Resources and Environment,2020,30(11): 1-25. (in Chinese
Project Comprehensive Report Writing Group. Comprehensive report on “China’s long-term low-carbon development strategy and transition pathways”[J]. China Population, Resources and Environment, 2020, 30(11): 1-25. (in Chinese)
|
| [2] |
AMPAH J D,JIN Chao,RIZWANUL FATTAH I M,et al. Investigating the evolutionary trends and key enablers of hydrogen production technologies: a patent-life cycle and econometric analysis[J]. International Journal of Hydrogen Energy,2023,48(96): 37674-37707. doi: 10.1016/j.ijhydene.2022.07.258
|
| [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. LIN Yuzhen,XU Quanhong,LIU Gaoen. Cas turbine combustor[M]. Beijing: National Defense Industry Press,2008. (in Chinese
LIN Yuzhen, XU Quanhong, LIU Gaoen. Cas turbine combustor[M]. Beijing: National Defense Industry Press, 2008. (in Chinese)
|
| [4] |
张弛,林宇震,徐华胜,等. 民用航空发动机低排放燃烧室技术发展现状及水平[J]. 航空学报,2014,35(2): 332-350. ZHANG Chi,LIN Yuzhen,XU Huasheng,et al. Development status and level of low emissions combustor technologies for civil aero-engine[J]. Acta Aeronautica et Astronautica Sinica,2014,35(2): 332-350. (in Chinese
ZHANG Chi, LIN Yuzhen, XU Huasheng, et al. Development status and level of low emissions combustor technologies for civil aero-engine[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(2): 332-350. (in Chinese)
|
| [5] |
莫妲,林宇震,韩啸,等. 氢气微混燃烧技术研究现状和未来展望[J]. 航空学报,2024,45(7): 36-62. MO Da,LIN Yuzhen,HAN Xiao,et al. Current status and future prospects of hydrogen micro-mixed combustion technology research[J]. Acta Aeronautica et Astronautica Sinica,2024,45(7): 36-62. (in Chinese
MO Da, LIN Yuzhen, HAN Xiao, et al. Current status and future prospects of hydrogen micro-mixed combustion technology research[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(7): 36-62. (in Chinese)
|
| [6] |
赵钦新,王宗一,邓世丰,等. 氢气燃烧技术及其进展[J]. 科学技术与工程,2022,22(36): 15870-15880. ZHAO Qinxin,WANG Zongyi,DENG Shifeng,et al. Hydrogen combustion technology and progress[J]. Science Technology and Engineering,2022,22(36): 15870-15880. (in Chinese doi: 10.3969/j.issn.1671-1815.2022.36.003
ZHAO Qinxin, WANG Zongyi, DENG Shifeng, et al. Hydrogen combustion technology and progress[J]. Science Technology and Engineering, 2022, 22(36): 15870-15880. (in Chinese) doi: 10.3969/j.issn.1671-1815.2022.36.003
|
| [7] |
MAREK C,SMITH T,KUNDU K. Low emission hydrogen combustors for gas turbines using lean direct injection[C]//Proceedings of the 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Reston,Virigina: AIAA,2005: 3776 .
|
| [8] |
YORK W D,ZIMINSKY W S,YILMAZ E. Development and testing of a low NOX hydrogen combustion system for heavy duty gas turbines[C]//Proceedings of ASME Turbo Expo 2012: Turbine Technical Conference and Exposition,2013: 1395-1405.
|
| [9] |
KIM D,JOO S,YOON Y. Effects of fuel line acoustics on the self-excited combustion instability mode transition with hydrogen-enriched laboratory-scale partially premixed combustor[J]. International Journal of Hydrogen Energy,2020,45(38): 19956-19964. doi: 10.1016/j.ijhydene.2020.05.074
|
| [10] |
ASAI T,DODO S,KARISHUKU M,et al. Multiple-injection dry low-NOx combustor for hydrogen-rich syngas fuel: testing and evaluation of performance in an IGCC pilot plant[J]. Mechanical Engineering Journal,2014,1(5): 14-24.
|
| [11] |
DODO S,ASAI T,KOIZUMI H,et al. Combustion characteristics of a multiple-injection combustor for dry low-NOx combustion of hydrogen-rich fuels under medium pressure[C]//Proceedings of ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition,New York,US: American Society of Mechanical Engineers,2012: 467-476.
|
| [12] |
RAJASEGAR R,MITSINGAS C M,MAYHEW E K,et al. Development and experimental characterization of metal 3D-printed scalable swirl stabilized mesoscale burner array[C]//Proceedings of ASME 2017 International Mechanical Engineering Congress and Exposition,New York,US: American Society of Mechanical Engineers,2018: 58417.
|
| [13] |
CHOI J,RAJASEGAR R,LEE W,et al. Hydrogen enhancement on a mesoscale swirl stabilized burner array[J]. International Journal of Hydrogen Energy,2021,46(46): 23906-23915. doi: 10.1016/j.ijhydene.2021.04.157
|
| [14] |
FUNKE H H W,BECKMANN N,KEINZ J,et al. 30 years of dry-low-NOx micromix combustor research for hydrogen-rich fuels—an overview of past and present activities[J]. Journal of Engineering for Gas Turbines and Power,2021,143(7): 071002. doi: 10.1115/1.4049764
|
| [15] |
FUNKE H H,BORNER S,ROBINSON A,et al. Low NOx H2 combustion for industrial gas turbines of various power ranges[R]Brussels: European Turbine Network,2010.
|
| [16] |
FUNKE H H W,BECKMANN N,ABANTERIBA S. An overview on dry low NOx micromix combustor development for hydrogen-rich gas turbine applications[J]. International Journal of Hydrogen Energy,2019,44(13): 6978-6990. doi: 10.1016/j.ijhydene.2019.01.161
|
| [17] |
FUNKE H H W,BOERNER S,KREBS W,et al. Experimental characterization of low NOx micromix prototype combustors for industrial gas turbine applications[C]//Proceedings of ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition,New York,US: American Society of Mechanical Engineers,2012: 343-353.
|
| [18] |
SUN Xiaoxiao,AGARWAL P,CARBONARA F,et al. Numerical investigation into the impact of injector geometrical design parameters on hydrogen micro-mix combustion characteristic[C]// Turbo Expo: Power for Land,Sea,and Air. New York,US: American Society of Mechanical Engineers,2020,84119.
|
| [19] |
MCCLURE J,ABBOTT D,AGARWAL P,et al. Comparison of hydrogen micromix flame transfer functions determined using RANS and LES[R]. New York,US: Turbo Expo: Power for Land,Sea,and Air,2019.
|
| [20] |
ZGHAL M,SUN Xiaoxiao,GAUTHIER P,et al. Comparison of tabulated and complex chemistry turbulent-chemistry interaction models with high fidelity large eddy simulations on hydrogen flames[R]. New York,US: Turbo Expo: Power for Land,Sea,and Air,2020.
|
| [21] |
林宇震,李林,张弛,等. 液体射流喷入横向气流混合特性研究进展[J]. 航空学报,2014,35(1): 46-57. LIN Yuzhen,LI Lin,ZHANG Chi,et al. Progress on the mixing of liquid jet injected into a crossflow[J]. Acta Aeronautica et Astronautica Sinica,2014,35(1): 46-57. (in Chinese
LIN Yuzhen, LI Lin, ZHANG Chi, et al. Progress on the mixing of liquid jet injected into a crossflow[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(1): 46-57. (in Chinese)
|
| [22] |
彭瀚,黄玥,刘晨,等. 横向射流影响缓燃向爆震转捩过程的实验研究[J]. 航空学报,2017,39(2): 121412. PENG Han,HUANG Yue,LIU Chen,et al. Experimental study on the influence of transverse jet on the deflagration-to-detonation transition process[J]. Acta Aeronautica et Astronautica Sinica,2017,39(2): 121412. (in Chinese
PENG Han, HUANG Yue, LIU Chen, et al. Experimental study on the influence of transverse jet on the deflagration-to-detonation transition process[J]. Acta Aeronautica et Astronautica Sinica, 2017, 39(2): 121412. (in Chinese)
|
| [23] |
KEINZ J,KUSTERER K,HAJ A A,et al. Development and testing of a low NOx micromix combustion chamber for industrial gas turbines[J]. International Journal of Gas Turbine,Propulsion and Power Systems,2017,9(1): 27-36. doi: 10.38036/jgpp.9.1_27
|
| [24] |
FUNKE HARALD H W,NILS B,JAN K,et al. Numerical and experimental evaluation of a dual-fuel dry-low-NOx micromix combustor for industrial gas turbine applications[J]. Journal of Thermal Science and Engineering Applications,2019,11(1): 011015. doi: 10.1115/1.4041495
|
| [25] |
ZIEMANN J,SHUM F,MOORE M,et al. Low-NOx combustors for hydrogen fueled aero engine[J]. International Journal of Hydrogen Energy,1998,23(4): 281-288. doi: 10.1016/S0360-3199(97)00054-2
|
| [26] |
FADOK J. Advanced hydrogen turbine development phase 1 final technical report[R]. Orlando,US: Siemens Power Generation,Incorporated,2008.
|
| [27] |
LIU X W,SHAO W W,TIAN Y,et al. Investigation of H2/CH4-air flame characteristics of a micromix model burner at atmosphere pressure condition[R]. New York,US: Proceedings of ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition,2018.
|
| [28] |
刘勋伟. 含氢燃料多微混射流火焰的燃烧特性与稳焰机制研究[D]. 北京: 中国科学院大学(中国科学院工程热物理研究所),2021. LIU Xunwei. Study on the combustion characteristics and stable flame mechanism of multi-micro-mixed jet flames with hydrogen-containing fuels[D]. Beijing: University of Chinese Academy of Sciences (Institute of Engineering Thermophysics,Chinese Academy of Sciences),2021. (in Chinese
LIU Xunwei. Study on the combustion characteristics and stable flame mechanism of multi-micro-mixed jet flames with hydrogen-containing fuels[D]. Beijing: University of Chinese Academy of Sciences (Institute of Engineering Thermophysics, Chinese Academy of Sciences), 2021. (in Chinese)
|
| [29] |
LIU Xunwei,SHAO Weiwei,LIU Ce,et al. Numerical study of a high-hydrogen micromix model burner using flamelet-generated manifold[J]. International Journal of Hydrogen Energy,2021,46(39): 20750-20764. doi: 10.1016/j.ijhydene.2021.03.157
|
| [30] |
刘贵闯. 稀释剂对合成气微混合燃烧特性影响的数值模拟研究[D]. 哈尔滨: 哈尔滨工业大学,2020. LIU Guichuang. Numerical simulation study on the influence of diluent on the combustion characteristics of syngas micro-mixing[D]. Harbin: Harbin Institute of Technology,2020. (in Chinese
LIU Guichuang. Numerical simulation study on the influence of diluent on the combustion characteristics of syngas micro-mixing[D]. Harbin: Harbin Institute of Technology, 2020. (in Chinese)
|
| [31] |
张永生,张海龙,田龙,等. 稀释合成气微混合燃料喷射燃烧火焰特性研究[J]. 动力工程学报,2015,35(1): 45-49,69. ZHANG Yongsheng,ZHANG Hailong,TIAN Long,et al. Characteristic study on syngas flames with combined CO2 dilution and micro-mixing injection combustion[J]. Journal of Chinese Society of Power Engineering,2015,35(1): 45-49,69. (in Chinese
ZHANG Yongsheng, ZHANG Hailong, TIAN Long, et al. Characteristic study on syngas flames with combined CO2 dilution and micro-mixing injection combustion[J]. Journal of Chinese Society of Power Engineering, 2015, 35(1): 45-49, 69. (in Chinese)
|
| [32] |
田龙. 合成气微混合火焰燃烧及流场特性研究[D]. 北京: 华北电力大学,2014. TIAN Long. Study on combustion and flow field characteristics of syngas micro-mixed flame[D]. Beijing: North China Electric Power University,2014. (in Chinese
TIAN Long. Study on combustion and flow field characteristics of syngas micro-mixed flame[D]. Beijing: North China Electric Power University, 2014. (in Chinese)
|
| [33] |
莫妲,林宇震,马宏宇,等. 基于钝体扰流的氢气微混扩散燃烧组织研究[J]. 航空学报,2024,45(8): 128928. MO Da,LIN Yuzhen,MA Hongyu,et al. Investigation on hydrogen micromix diffusive combustion organization based on bluff body disturbance[J]. Acta Aeronautica et Astronautica Sinica,2024,45(8): 128928. (in Chinese
MO Da, LIN Yuzhen, MA Hongyu, et al. Investigation on hydrogen micromix diffusive combustion organization based on bluff body disturbance[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(8): 128928. (in Chinese)
|
| [34] |
STEINBERG A M,SADANANDAN R,DEM C,et al. Structure and stabilization of hydrogen jet flames in cross-flows[J]. Proceedings of the Combustion Institute,2013,34(1): 1499-1507. doi: 10.1016/j.proci.2012.06.026
|
| [35] |
莫妲,尚守堂,林宇震,等. 一种氢燃料微尺度非预混燃烧室数值模拟[J]. 航空动力学报,2023,38(11): 2701-2710. MO Da,SHANG Shoutang,LIN Yuzhen,et al. Numerical simulation investigation on a hydrogen micromix combustor[J]. Journal of Aerospace Power,2023,38(11): 2701-2710. (in Chinese
MO Da, SHANG Shoutang, LIN Yuzhen, et al. Numerical simulation investigation on a hydrogen micromix combustor[J]. Journal of Aerospace Power, 2023, 38(11): 2701-2710. (in Chinese)
|
| [36] |
昌运鑫,宋恒,韩猛,等. 掺氢功率比对富氢甲烷燃烧振荡特性的影响[J]. 推进技术,2023,44(1): 210673. CHANG Yunxin,SONG Heng,HAN Meng,et al. Effects of hydrogen power ratio on combustion oscillation characteristics of hydrogen-enriched methane[J]. Journal of Propulsion Technology,2023,44(1): 210673. (in Chinese
CHANG Yunxin, SONG Heng, HAN Meng, et al. Effects of hydrogen power ratio on combustion oscillation characteristics of hydrogen-enriched methane[J]. Journal of Propulsion Technology, 2023, 44(1): 210673. (in Chinese)
|
DownLoad:
