{"title":"Laminar Flame Speed Measurements of Hydrogen/Natural Gas Mixtures for Gas Turbine Applications","authors":"Gihun Kim, Ritesh Ghorpade, Subith S. Vasu","doi":"10.1115/gt2021-58870","DOIUrl":null,"url":null,"abstract":"\n Due to the increasingly challenging carbon emission reduction targets, hydrogen-containing fuel combustion is gaining the energy community’s attention, as highlighted recently in the U.S. Department of Energy’s (DOE) Hydrogen Program Plan [1]. Though fundamental and applied research of hydrogen-containing fuels has been a topic of research for several decades, there are knowledge-gaps and unexplored fuel blend combustion characteristics at conditions relevant to modern gas turbine combustors. Hydrogen will be burned directly or as mixtures with natural gas (NG) and/or ammonia (NH3) in these devices. Fundamental research on the combustion of hydrogen (H2) containing fuels is still essential, especially to overcome or accurately predict challenges such as nitrogen oxides (NOx) reduction and flashback and develop fuel flexible combustors for a prosperous hydrogen economy. We focused our investigation on a natural gas and hydrogen mixture. Measurements of laminar burning velocity (LBV) are necessary for these fuels to understand their applicability in the turbines and other engines. In this study, the maximum rate of pressure rise and LBV of methane (CH4), CH4/H2, natural gas, and natural gas/H2 mixture were measured in synthetic air. The experimental conditions were at an initial pressure of 1 atm and an initial temperature of 300 K. A realistic natural gas composition from the field was used in this study and consisted of CH4 and other alkanes. The experimental data were compared with simulations carried out with detailed chemical kinetic mechanisms.","PeriodicalId":129194,"journal":{"name":"Volume 6: Ceramics and Ceramic Composites; Coal, Biomass, Hydrogen, and Alternative Fuels; Microturbines, Turbochargers, and Small Turbomachines","volume":"3 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2021-06-07","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Volume 6: Ceramics and Ceramic Composites; Coal, Biomass, Hydrogen, and Alternative Fuels; Microturbines, Turbochargers, and Small Turbomachines","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1115/gt2021-58870","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 1
Abstract
Due to the increasingly challenging carbon emission reduction targets, hydrogen-containing fuel combustion is gaining the energy community’s attention, as highlighted recently in the U.S. Department of Energy’s (DOE) Hydrogen Program Plan [1]. Though fundamental and applied research of hydrogen-containing fuels has been a topic of research for several decades, there are knowledge-gaps and unexplored fuel blend combustion characteristics at conditions relevant to modern gas turbine combustors. Hydrogen will be burned directly or as mixtures with natural gas (NG) and/or ammonia (NH3) in these devices. Fundamental research on the combustion of hydrogen (H2) containing fuels is still essential, especially to overcome or accurately predict challenges such as nitrogen oxides (NOx) reduction and flashback and develop fuel flexible combustors for a prosperous hydrogen economy. We focused our investigation on a natural gas and hydrogen mixture. Measurements of laminar burning velocity (LBV) are necessary for these fuels to understand their applicability in the turbines and other engines. In this study, the maximum rate of pressure rise and LBV of methane (CH4), CH4/H2, natural gas, and natural gas/H2 mixture were measured in synthetic air. The experimental conditions were at an initial pressure of 1 atm and an initial temperature of 300 K. A realistic natural gas composition from the field was used in this study and consisted of CH4 and other alkanes. The experimental data were compared with simulations carried out with detailed chemical kinetic mechanisms.
由于碳减排目标越来越具有挑战性,含氢燃料燃烧正受到能源界的关注,最近美国能源部(DOE)的《氢计划计划》(Hydrogen Program Plan)就强调了这一点[1]。虽然含氢燃料的基础和应用研究已成为几十年来的研究课题,但在与现代燃气轮机燃烧器相关的条件下,存在知识空白和未开发的燃料混合燃烧特性。氢气将在这些装置中直接燃烧或与天然气(NG)和/或氨(NH3)混合燃烧。含氢燃料燃烧的基础研究仍然是必不可少的,特别是要克服或准确预测氮氧化物(NOx)还原和闪回等挑战,并为繁荣的氢经济开发燃料柔性燃烧器。我们的调查重点是天然气和氢气的混合物。层流燃烧速度(LBV)的测量是必要的,以了解这些燃料在涡轮机和其他发动机中的适用性。本研究测量了合成空气中甲烷(CH4)、CH4/H2、天然气和天然气/H2混合物的最大升压速率和LBV。实验条件为初始压力为1atm,初始温度为300k。本研究采用的是该气田实际天然气组成,由CH4和其他烷烃组成。将实验数据与详细化学动力学机理的模拟结果进行了比较。