燃料分级对舰船燃气轮机燃烧室热声振荡的影响

周宇凡; 陆羽笛; 吴慧羽; 刘先达; 葛冰

doi:10.19805/j.cnki.jcspe.2026.250030

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燃料分级对舰船燃气轮机燃烧室热声振荡的影响

动力设备与系统 | 更新时间：2026-10-10

- 燃料分级对舰船燃气轮机燃烧室热声振荡的影响
- Effect of Fuel Staging on Thermoacoustic Oscillation of a Marine Gas Turbine Combustor
- 动力工程学报 2026年46卷第5期页码：82-89,96
- 作者机构：
- 作者简介：
  
  周宇凡(2000—),男,上海人,硕士研究生,研究方向为燃气轮机整机循环性能及燃烧室燃烧不稳定性。葛冰(通信作者),男,副研究员,博士,E-mail:Gebing@sjtu.edu.cn。
- 基金信息：
  
  国家科技重大专项资助项目(J2019-Ⅱ-0018-0039)
- DOI：10.19805/j.cnki.jcspe.2026.250030
  中图分类号： TK478.9
- 纸质出版：2026
- 稿件说明：
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周宇凡, 陆羽笛, 吴慧羽, 刘先达, 葛冰. 燃料分级对舰船燃气轮机燃烧室热声振荡的影响[J]. 动力工程学报, 2026, 46(5): 82-89,96.
周宇凡, 陆羽笛, 吴慧羽, 刘先达, 葛冰. 燃料分级对舰船燃气轮机燃烧室热声振荡的影响[J]. 动力工程学报, 2026, 46(5): 82-89,96. DOI： 10.19805/j.cnki.jcspe.2026.250030.

DOI： 10.19805/j.cnki.jcspe.2026.250030

摘要

针对为舰船燃气轮机设计的十喷嘴柴油燃烧室开展试验

采用脉动压力和图像同步采集的方法采集数据

并采用本征正交分解(POD)的方法研究燃料分级方案对热声稳定性的影响。结果表明:对于柴油多喷嘴贫预混燃烧室

开启值班级喷嘴后振荡频率相较于开启前降低了11%;调节燃料分级比可以抑制燃烧室的压力脉动

脉动幅值降低比例可达到60%;不开启值班级时振荡模式为双周期极限环振荡

而开启值班级后的振荡为单周期极限环振荡;火焰热释放率振荡与压力振荡的频率基本吻合

各喷嘴达到热声耦合状态;振荡的主要能量集中于全局的轴向同步振荡

但同时存在能量较低的周向振荡模式。

Abstract

For a ten-nozzle diesel combustor designed for marine gas turbine

experiments were conducted to analyze the effect of fuel staging on its thermoacoustic instability properties by using simultaneous pulsation pressure and image acquisition method and proper orthogonal decomposition (POD) method. Results show that in a diesel multi-nozzle lean premix combustion chamber

the oscillation frequency after opening the pilot nozzle decreases by 11% compared to before opening. Adjusting the fuel staging can suppress the pressure pulsation within the combustion chamber by up to 60%. The oscillation mode is a double limit cycle oscillation with pilot nozzle off

while the oscillation becomes a single limit cycle oscillation with pilot nozzle on. The frequency of the flame heat-release rate oscillation is largely in line with the frequency of pressure oscillation

with the nozzles in the state of thermo-acoustic coupling. The main energy of the oscillations is concentrated in the global axial synchronous oscillation

and there are also circumferential oscillation modes with reduced energy.

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references

闫大海, 张晗. 船用燃气轮机发展趋势分析[J]. 舰船科学技术, 2021, 43(19): 84-88.YAN Dahai, ZHANG Han. Development trend analysis of marine gas turbine[J]. Ship Science and Technology, 2021, 43(19): 84-88.

BARSI D, BONO A, SATTA F, et al. Gas turbine prime movers fuelled by LNG as a future alternative for sustainable power in marine propulsion: current emission policy assessment and exhaust quality evaluation[J]. E3S Web of Conferences, 2019, 113: 02018.

梁恩广, 张辰杰, 余志健, 等. 燃气轮机轴向贫燃分级燃烧技术进展[J]. 动力工程学报, 2024, 44(9): 1328-1339.LIANG Enguang, ZHANG Chenjie, YU Zhijian, et al. Progress in axial staged lean premixed combustion technology of gas turbines[J]. Journal of Chinese Society of Power Engineering, 2024, 44(9): 1328-1339.

YORK W D, SIMONS D W, FU Yongqiang. Operational flexibility of GE's F-class gas turbines with the DLN2.6+ combustion system[C] //Proceedings of the ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition. Oslo, Norway: ASME, 2018.

ANGELLO L, NOBLE B, STEELE R, et al. Dry low NOx (DLN) combustion system operability considerations[C] //Proceedings of the ASME Turbo Expo 2022: Turbomachinery Technical Conference and Exposition. Rotterdam, Netherlands: ASME, 2022.

KASKAN W E, NOREEN A E. High-frequency oscillations of a flame held by a bluff body[J]. Journal of Fluids Engineering, 1955, 77(6): 885-891.

BOURGOUIN J F, DUROX D, MOECK J P, et al. Self-sustained instabilities in an annular combustor coupled by azimuthal and longitudinal acoustic modes[C] //Proceedings of the ASME Turbo Expo 2013: Turbine Technical Conference and Exposition. San Antonio: ASME, 2013.

KIM J, GILLMAN W, JOHN T, et al. Experimental investigation of fuel staging effect on modal dynamics of thermoacoustic azimuthal instabilities in a multi-nozzle can combustor[C] //Proceedings of the ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition. [S.l.] : ASME, 2021.

KIM J, GILLMAN W, WU D, et al. Identification of high-frequency transverse acoustic modes in multi-nozzle can combustors[C] //Proceedings of the ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition. [S.l.] : ASME, 2020.

SUN Peifeng, YUAN Yiren, GE Bing, et al. Combustion oscillation characteristics and flame structures in a lean premixed prevaporized combustor[J]. Energy & Fuels, 2017, 31(9): 10060-10067.

TEMME J E, ALLISON P M, DRISCOLL J F. Combustion instability of a lean premixed prevaporized gas turbine combustor studied using phase-averaged PIV[J]. Combustion and Flame, 2014, 161(4): 958-970.

任乐乐, 熊燕, 刘志刚, 等. 甲烷预混多喷嘴阵列燃烧器热声振荡模态实验研究[J]. 热能动力工程, 2023, 38(5): 30-41.REN Lele, XIONG Yan, LIU Zhigang, et al. Experimental study on thermo-acoustic oscillation modes of a methane premixed multi-nozzle array combustor[J]. Journal of Engineering for Thermal Energy and Power, 2023, 38(5): 30-41.

KAO Yihuan, TAMBE S B, JENG S M. Aerodynamics study of a linearly-arranged 5-swirler array[C] //ASME Turbo Expo 2014: Turbine Technical Conference and Exposition. Dsseldorf: ASME, 2014.

SAMARASINGHE J, PELUSO S J, QUAY B D, et al. The three-dimensional structure of swirl-stabilized flames in a lean premixed multinozzle can combustor[J]. Journal of Engineering for Gas Turbines and Power, 2016, 138(3): 031502.

WORTH N A, DAWSON J R. Tomographic reconstruction of OH* chemiluminescence in two interacting turbulent flames[J]. Measurement Science and Technology, 2013, 24(2): 024013.

陆羽笛, 史挺, 姜海燕, 等. 贫预混多喷嘴燃烧流场及火焰结构几何模化方法研究[J]. 热能动力工程, 2024, 39(6): 49-58.LU Yudi, SHI Ting, JIANG Haiyan, et al. Study on geometric modeling of flow field and flame structure of a lean premixed multi-nozzle combustor[J]. Journal of Engineering for Thermal Energy and Power, 2024, 39(6): 49-58.

陆羽笛, 金明, 李昱泽, 等. 燃料分级对贫预混多喷嘴燃烧器火焰动态响应特性影响的实验研究[J]. 推进技术, 2024, 45(4): 2210097.LU Yudi, JIN Ming, LI Yuze, et al. Experimental study on effects of fuel staging on flame dynamic response of a lean premixed multi-nozzle burner[J]. Journal of Propulsion Technology, 2024, 45(4): 2210097.

张自来, 杜世强, 葛冰, 等. 声音信号在贫油预混预蒸发振荡燃烧分析中的应用[J]. 动力工程学报, 2018, 38(2): 114-119.ZHANG Zilai, DU Shiqiang, GE Bing, et al. Application of acoustic signals in analysis of lean premixed prevaporized oscillation combustion[J]. Journal of Chinese Society of Power Engineering, 2018, 38(2): 114-119.

LUMLEY J L. The structure of inhomogeneous turbulent flows[M] //YAGLOM A M, TATARSKI V I. Atmospheric Turbulence and Radio Wave Propagation. Moskow: Nauka, 1967: 166-178.

SIROVICH L. Turbulence and the dynamics of coherent structures. I. Coherent structures[J]. Quarterly of Applied Mathematics, 1987, 45(3): 561-571.

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