HIGH-FUEL LOADING IGNITION DELAY TIME CHARACTERIZATION OF HYDROGEN/NATURAL GAS/AMMONIA AT GAS TURBINE-RELEVANT CONDITIONS INSIDE A HIGH-PRESSURE SHOCK TUBE

被引:0
|
作者
Pierro, Michael [1 ]
Urso, Justin [1 ]
Kinney, Cory [1 ]
Kesharwani, Shubham [1 ]
McGaunn, Jonathan [1 ]
Dennis, Christopher [1 ]
Vasu, Subith S. [1 ]
机构
[1] Univ Cent Florida, Ctr Adv Turbomachinery & Energy Res CATER, Mech & Aerosp Engn, Orlando, FL 32816 USA
来源
PROCEEDINGS OF ASME TURBO EXPO 2022: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2022, VOL 3B | 2022年
关键词
Shock tube; ammonia; hydrogen; natural gas; stage-fill; OXYGEN-ARGON MIXTURES; CHEMICAL-KINETICS; LOW-TEMPERATURES; SELF-IGNITION; AIR MIXTURES; COMBUSTION; OXIDATION; ENGINE; MECHANISM; AMMONIA;
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This study explores the combustion characterization of highfuel percentage, air-diluted mixtures of H-2 mixed with natural gas (NG) as well as mixtures of H-2 and NH3 at temperatures and pressures relevant to turbine operating conditions (20-30 bar, 1000-1500 K). Lower temperatures (below 1070 K) exhibit preignition characteristics due to non- homogeneity. An attempt to mitigate these occurrences at high pressures is investigated using the constrained reaction volume (CRV) stage-filling technique. Due to the need to further refine the facility CRV stage-filling uncertainty, only higher temperature data will be interpreted at this time. The test conditions in this study closely replicate the temperatures, pressures, and mixtures that would be seen in hydrogen-powered gas turbines, making it the first to explore such conditions. The experimental IDTs were compared against the current state-of-the-art chemical kinetic models for mechanism validation. The current work will advance H-2-powered turbines and aims to determine the optimum molecular ratio of H2 when mixed with natural gas.
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页数:9
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