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EXPERIMENTAL STUDY ON LOW LOAD OPERATION RANGE EXTENSION BY AUTOTHERMAL ON-BOARD SYNGAS GENERATION

机译:自热车载信号发生器在低负荷运行范围内扩展的实验研究

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Volatile renewable energy sources induce power supply fluctuations. These need to be compensated by flexible conventional power plants. Gas turbines in combined cycle power plants adjust the power output quickly but their turn-down ratio is limited by the slow reaction kinetics which lead to CO and unburned hydrocarbon (UHC) emissions. To extend the turn-down ratio, part of the fuel can be converted to syngas, which exhibits a higher reactivity. By an increasing fraction of syngas in the fuel, the reactivity of the mixture is increased and total fuel mass-flow and the power output can be reduced. An Autothermal On-board Syngas Generator in combination with two different burner concepts for natural gas/syngas mixtures was presented in a previous study. The study at hand shows a mass-flow variation of the reforming process with mass-flows which allow for pure syngas combustion and further improvements of the two burner concepts which result in a more application-oriented operation. The first of the two burner concepts comprises a generic swirl stage with a central lance for syngas injection. Syngas is injected with swirl to avoid a negative impact on the total swirl intensity and non-swirled. The second concept includes a central swirl stage with an outer ring of jets. For this burner, syngas is injected in both stages to avoid NOx emissions from the swirl stage. Increased NOx emissions produced by natural gas combustion of the swirl pilot was reported in last year's paper. For both burners, combustion performance is analyzed by OH*-chemiluminescence and gaseous emissions. The lowest possible adiabatic flame temperature without a significant increase of CO emissions was 170 K - 210 K lower for the syngas compared to low load pure natural gas combustion. This corresponds to a decrease of 15 - 20 % in terms of thermal power.
机译:挥发性可再生能源诱导电源波动。这些需要通过灵活的传统发电厂进行补偿。组合循环发电厂中的燃气轮机快速调节功率输出,但其匝间比受到导致CO和未燃烧的烃(UHC)排放的缓慢反应动力学的限制。为了延长旋转率,部分燃料可以转化为合成气,这表现出更高的反应性。通过燃料中增加的合成气部分,增加了混合物的反应性,并且可以减少总燃料质量流量和功率输出。在先前的研究中,提出了一种与天然气/合成气混合物的两种不同的燃烧器概念组合的自动燃烧器概念。手的研究表明,具有质量流量的重整过程的质量流量变化,其允许纯合成气燃烧以及两种燃烧器概念的进一步改进,从而导致更具应用导向的操作。两个燃烧器概念中的第一个包括一种通用旋流阶段,具有用于合成气注射的中央矛盾。合成气被旋转注射,以避免对总旋流强度和无旋转的负面影响。第二概念包括带有射流外圈的中央旋流阶段。对于该燃烧器,合成气在两个阶段注入,以避免旋流阶段的NOx排放。去年的纸质报告了漩涡飞行员天然气燃烧产生的NOx排放量增加。对于两个燃烧器,通过OH * - 升级和气态排放分析燃烧性能。与低负荷纯天然气燃烧相比,合成气的不显着增加的绝热性火焰温度的最低可能是170 k - 210k。这对应于导热功率而降低15-20%。

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