燃烧室
喷嘴
管(容器)
燃烧
天然气
机械工程
燃气轮机
燃烧室
航程(航空)
闪光灯(摄影)
煤气燃烧器
汽车工程
核工程
工程类
航空航天工程
废物管理
化学
物理
光学
有机化学
作者
Young‐Jun Shin,Cheahong Choi,Hanjin Jeong,Seonghwi Jo,E.-S. Cho
出处
期刊:한국연소학회지
[The Korean Society of Combustion]
日期:2023-06-30
卷期号:28 (2): 57-66
被引量:4
标识
DOI:10.15231/jksc.2023.28.2.057
摘要
Doosan is currently developing a 100% hydrogen gas turbine combustor with a micro-mixer concept multi-tube type nozzle, which has the ability to prevent flash-back phenomena during operation. This combustor is intended to replace the existing natural gas firing combustor for 5 MW, and has also been designed to achieve low NOSUBx/SUB emissions through the utilization of premixed methods. Our testing has shown that the nozzle provides an expanded operating range through lean blow off and flame holding flash back tests. Going forward, we plan to continue improving and testing the nozzle in real geometry under high-pressure conditions.
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