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Flamelet Generated Manifolds Applied to Dual-Fuel Combustion of Lean Methane/Air Mixtures at Engine Relevant Conditions Ignited by n Dodecane Micro Pilot Sprays

机译:挥动产生的歧管在发动机相关条件下应用于瘦甲烷/空气混合物的双燃料燃烧,通过N十二烷微型飞行员喷雾点燃

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In this study, a novel 3D-CFD combustion model employing Flamelet Generated Manifolds (FGM) for dual fuel combustion was developed. Validation of the platform was carried out using recent experimental results from an optically accessible Rapid Compression Expansion Machine (RCEM). Methane and n-dodecane were used as model fuels to remove any uncertainties in terms of fuel composition. The model used a tabulated chemistry approach employing a reaction mechanism of 130 species and 2399 reactions and was able to capture non-premixed auto ignition of the pilot fuel as well as premixed flame propagation of the background mixture. The CFD model was found to predict well all phases of the dual fuel combustion process: I) the pilot fuel ignition delay, II) the Heat Release Rate of the partially premixed conversion of the micro pilot spray with entrained methane/air and III) the sustained background mixture combustion following the consumption of the spray plume. The test conditions on the RCEM were chosen to mimic engine relevant conditions with start of injection (SOI) pressure and temperature of 45 bar and 1000 K respectively. The reactivity of the background lean mixture was varied by changing the air to fuel ratio λ; values of 2.1, 3 and ∞ (i.e. pure diesel) were tested. The model shows considerable promise as it was able to reasonably predict the effects of changing the reactivity of the background mixture as per measured from the RCEM experiments. To the authors best knowledge, this is the first study in the open literature reporting on the application of FGM to dual-fuel combustion of lean premixed methane/air charges ignited with liquid micro pilot fuel sprays.
机译:在该研究中,开发了一种用于采用Flameelet产生的歧管(FGM)的新型3D-CFD燃烧模型用于双燃料燃烧。使用最近由光学访问的快速压缩扩展机(RCEM)的最近实验结果进行平台的验证。甲烷和N-十二烷用作模型燃料,以在燃料组合物方面消除任何不确定性。该模型采用了制表化学方法,采用130种和2399个反应的反应机理,并能够捕获试验燃料的非预混自动点火以及背景混合物的预混火焰繁殖。发现CFD模型预测双燃料燃烧过程的所有阶段:i)先导燃料点火延迟,ii)微试频喷雾与夹带甲烷/空气和III的部分预混转化的热释放速率喷雾羽流消耗后持续的背景混合燃烧。选择RCEM上的试验条件以模拟发动机相关条件,同时注射开始(SOI)压力和45巴的温度和1000 k。通过将空气改变为燃料比λ来改变背景稀合混合物的反应性;测试2.1,3和∞(即纯柴油)的值。该模型显示了相当大的希望,因为它能够合理地预测根据RCEM实验测量时改变背景混合物的反应性的影响。为了提交人的最佳知识,这是开放文学报告的第一次研究,关于瘦预混甲烷/空气电荷的双燃料燃烧应用液体微试燃料喷雾剂。

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