Chemi-luminescence Measurement and Exact Dynamic Mode Decomposition for Combustion-Instability Analysis in a Gas Turbine Combustor

被引：0

作者：

Seong, Ji Hwan ^{[1
]}

Wang, Yuangang ^{[1
]}

Park, Soon Been ^{[1
]}

Hwang, Jeongjae ^{[2
]}

Lee, Won June ^{[2
]}

Sohn, Chae Hoon ^{[1
]}

机构：

[1] Sejong Univ, Dept Mech Engn, Seoul, Seoul, South Korea

[2] Korea Inst Machinery & Mat, Dept Carbon free Power Generat, GT Res Team, Daejeon, South Korea

来源：

JOURNAL OF THE KOREAN SOCIETY OF COMBUSTION | 2024年 / 29卷 / 03期

关键词：

Exact dynamic mode decomposition; Fast Fourier transform; Growth rate; Mode shape; Combustion instability;

D O I：

10.15231/jksc.2024.29.3.053

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 ;

摘要：

To analyze combustion instability in the combustor of a gas turbine, the results of chemi-luminescence measurement are applied for the exact dynamic mode decomposition (EDMD) as hydrogen blending ratio, pilot split ratio, and operating pressure. The resonant frequencies obtained using fast Fourier transform (FFT) and EDMD are compared to confirm the growth rate and mode shape. The effect of hydrogen blending ratio, pilot split ratio, and pressure on the combustion instability was confirmed by comparing these results and used for analysis of combustion instability.

引用

页码：53 / 61

页数：9

共 8 条

[1] Koopman-mode decomposition of the cylinder wake [J].

Bagheri, Shervin .

JOURNAL OF FLUID MECHANICS, 2013, 726 :596-623

[2] Thermoacoustic instability and flame transfer function in a lean direct injection model gas turbine combustor [J].

Joo, Seongpil ;

Kwak, Sanghyeok ;

Lee, Jongguen ;

Yoon, Youngbin .

AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 116

[3] Analysing the performance, fuel cost and emission parameters of the 50 MW simple and recuperative gas turbine cycles using natural gas and hydrogen as fuel [J].

Koc, Yildiz ;

Yagli, Huseyin ;

Goerguelue, Adnan ;

Koc, Ali .

INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 45 (41) :22138-22147

[4] Comprehensive Combustion Stability Analysis Using Dynamic Mode Decomposition [J].

Rajasegar, Rajavasanth ;

Choi, Jeongan ;

McGann, Brendan ;

Oldani, Anna ;

Lee, Tonghun ;

Hammack, Stephen D. ;

Carter, Campbell D. ;

Yoo, Jihyung .

ENERGY & FUELS, 2018, 32 (09) :9990-9996

[5] NOx reduction in an axially staged gas turbine model combustor through increase in the combustor exit Mach number [J].

Rodrigues, Neil S. ;

Busari, Oluwatobi ;

Senior, William C. B. ;

McDonald, Colin T. ;

Chen, YunTao ;

North, Andrew J. ;

Laster, Walter R. ;

Meyer, Scott E. ;

Lucht, Robert P. .

COMBUSTION AND FLAME, 2020, 212 :282-294

[6] Experimental study on impacts of fuel type on thermo-acoustic instability in a gas turbine model combustor [J].

Ruan, Can ;

Chen, FeiEr ;

Yu, Tao ;

Cai, WeiWei ;

He, ZhuoYao ;

Mao, YeBing ;

Li, XinLing ;

Lu, XingCai .

SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2021, 64 (06) :1345-1358

[7] Dynamic mode decomposition of numerical and experimental data [J].

Schmid, Peter J. .

JOURNAL OF FLUID MECHANICS, 2010, 656 :5-28

[8] Combustion Instability Analysis of a Model Gas Turbine by Application of Dynamic Mode Decomposition [J].

Wang, Yuangang ;

Son, Jinwoo ;

Sohn, Chae Hoon ;

Yoon, Jisu ;

Bae, Jinhyun ;

Yoon, Youngbin .

JOURNAL OF THE KOREAN SOCIETY OF COMBUSTION, 2019, 24 (01) :51-56

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