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Prediction of NOx emissions for an RQL combustor using a stirred reactor modelling approach

机译:使用搅拌反应器建模方法预测RQL燃烧器的NOx排放

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摘要

In an effort to reduce NOX emissions both in the landing and take-off (LTO) cycle as well as in cruise, significant research has been conducted on novel aero-engine low emissions combustor design concepts. Preliminary combustor design and emissions prediction software tools are becoming increasingly important during the conceptual design phase of aero-engine combustors. They allow a large number of designs to be explored, in a relatively short amount of time, thereby identifying the most promising designs to consider for further development.There are three methods for NOX emission prediction; correlations, stirred reactor models and CFD models. Correlation methods are derived from experimental results and are therefore only applicable for combustors for which data is available. The stirred reactor modelling approach provides a reasonably good compromise with respect to computational time and robustness relative to correlation and CFD based methods. The stirred reactor method assumes finite rate chemistry inside the combustor using simplified chemical kinetic models. The basic concept of the reactor-based method is to split the combustor into a number of reactors (perfectly or partially stirred) to compute the overall emissions.The primary objective of this doctoral research was to assess the suitability and limitations of the stirred reactor modelling approach to predict NOX emissions of a Rich-Burn Quick-Quench and Lean-Burn (RQL) combustor concept. The geometry of the RQL combustor and the model constraints were assumed from a NASA test rig experiment. The stirred reactor emission prediction model developed was verified using this test data. The results suggest that, based on the modelling assumptions made, the stirred reactor modelling approach is able to capture the trends of emissions (with changing boundary conditions) even though there are discrepancies in the absolute values. This suggests that the stirred reactor model is a useful tool during the preliminary design phase to quantify the impact of changes in boundary conditions/design parameters on changes in NOX emissions ... [cont.].
机译:为了减少着陆和起飞(LTO)循环以及巡航中的NOX排放,已经对新颖的航空发动机低排放燃烧室设计概念进行了大量研究。在航空发动机燃烧器的概念设计阶段,燃烧器的初步设计和排放预测软件工具变得越来越重要。它们允许在相对较短的时间内探索大量设计,从而确定最有希望的设计以供进一步开发。NOX排放预测有以下三种方法:相关性,搅拌反应器模型和CFD模型。相关方法是从实验结果中得出的,因此仅适用于可获得数据的燃烧器。搅拌反应器建模方法相对于基于关联和CFD的方法,在计算时间和鲁棒性方面提供了合理的折衷。搅拌反应器方法使用简化的化学动力学模型,假设燃烧室内部的化学反应速率有限。基于反应器的方法的基本概念是将燃烧器分成多个反应器(完全或部分搅拌)以计算总排放量。本博士研究的主要目的是评估搅拌反应器建模的适用性和局限性富燃快速熄灭和贫燃(RQL)燃烧器概念的NOx排放预测方法。 RQL燃烧室的几何形状和模型约束条件是根据NASA试验台实验得出的。使用该测试数据验证了开发的搅拌反应器排放预测模型。结果表明,基于所做的建模假设,即使绝对值存在差异,搅拌反应器建模方法也能够捕获排放趋势(边界条件不断变化)。这表明搅拌反应器模型在初步设计阶段是量化边界条件/设计参数变化对NOx排放变化的影响的有用工具……[续]。

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    Prakash Atma;

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  • 年度 2015
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