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Nox SUPPRESSION FROM A MICRO-GAS TURBINE APPROACHING THE MILD-COMBUSTION REGIME

机译：从轻度燃烧制度接近微型燃气轮机的NOx抑制

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The authors present in this paper a refined methodology, already introduced in a recent paper, aiming to find the best compromises between the need of reducing the Nox emission from a micro-gas turbine and the preservation of satisfactory efficiency and energy saving levels. The method founds on an integrated approach consisting of an advanced cycle analysis, which includes the component matching study, and the CFD based validation of the most interesting cases. The latter refer to the activation of the exhaust recirculation to the compressor inlet, in order to generate conditions close to those characterized by a mild combustion.

机译：本文存在的作者在最近的一篇论文中介绍了一种精致的方法，旨在在减少微燃气轮机中的NOx排放和保存令人满意的效率和节能水平之间的需求之间获得最佳妥协。该方法发现了一个集成方法，包括高级循环分析，包括组件匹配研究以及基于CFD的最有趣情况的验证。后者是指对压缩机入口的排气再循环的激活，以便产生靠近由温和燃烧表征的条件。

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来源
《ASME Turbo Expo》|2007年||共12页
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作者
Maria Cristina Cameretti; Fabrizio Reale; Raffaele Tuccillo;
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原文格式 PDF
正文语种
中图分类气体透平（涡轮机）;
关键词
EGR: Exhaust Gas Recirculation; f: Fuel / Air ratio; LHV: Lower Heating Value; m: Mass Flow rate; MGT: Micro Gas Turbine; p.p.m.: Parts per million; T; X_b: Recuperator by-pass ratio; X_(egr): EGR ratio; Subscri; T.I. T.: Temperature; Turbine Inlet Temp.;

机译：EGR：废气再循环;F：燃料/空气比;LHV：较低的加热值;M：质量流量;MGT：Micro燃气涡轮机;PPM：百万分之一;T;X_B：恢复器旁路比率;X_（EGR ）：EGR比率;子弹;TI t .:温度;涡轮机入口温度。;

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3. On High Suppression of NOX and CO Emissions in Gas-Turbine Plants with Combined Gas-and- Steam Cycles [J] . A. A. Ivanov, A. N. Ermakov, R. A. Shlyakhov Thermal engineering . 2010,第13期

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4. Nox SUPPRESSION FROM A MICRO-GAS TURBINE APPROACHING THE MILD-COMBUSTION REGIME [C] . Maria Cristina Cameretti, Fabrizio Reale, Raffaele Tuccillo ASME(American Society of Mechanical Engineers) Turbo Expo vol.3; 20070514-17; Montreal(CA) . 2007

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Nox SUPPRESSION FROM A MICRO-GAS TURBINE APPROACHING THE MILD-COMBUSTION REGIME

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