Insight of low flammability limit on sustainable aviation fuel blend and prediction by ANN model

IF 9.6 Q1 COMPUTER SCIENCE, ARTIFICIAL INTELLIGENCE
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Abstract

Sustainable aviation fuel (SAF) blend has been confirmed to benefit for greenhouse gases reduction, and thus the property of blend fuel should be understanded the detail to support the utilization in aircraft. Low flammability limit (LFL) is a key property of jet fuel which should be sufficiently flammable to burn in combustor of aeroengine and meanwhile should be non-flammable for safety storage in fuel tank of aircraft. LFL of fuel could be influenced by integrating effects including molecule structure, intramolecular chemical bond energy and binding energy of molecule to molecule. Three types of theoretical models, based on different individual view including LFL of every pure hydrocarbon, stoichiometric concentration, and combustion enthalpy, present unsatisfactory simulation results, which can be deduced without integrating all potential influence factors together. The artificial neural network (ANN) approaches have been involved to bridge the relationship of the complex compositions in jet fuels with LFL. For providing adequate and available composition input, the boundary of fuel compositions has been extracted based on constrains of boiling point, flash point and freeze point coupling with statistic petroleum-based jet fuels. By clustering analysis, 43 critical classes of compositions, extracted as surrogate hydrocarbons based on with similar LFL within 1 % deviation, have been deployed as input matrix. ANN-LFL model, trained by only drop-in fuel with feature of Sigmoid function as an activation function, can distinguish drop-in fuel with non-drop-in fuel. ANN LFL model can predict LFL of drop-in fuel with 0.988 accuracy. The predict output value of non-drop-in fuel could present obvious deviation with traditional jet fuel. The optimization methodologies of ANN-LFL model could be improved the understanding of LFL and extend ANN in SAF utilization.

Abstract Image

可持续航空混合燃料低易燃性限制的启示及 ANN 模型预测
可持续航空混合燃料(SAF)已被证实有利于减少温室气体排放,因此应详细了解混合燃料的特性,以支持飞机的使用。低可燃性极限(LFL)是喷气燃料的一个关键特性,它应具有足够的可燃性,以便在航空发动机的燃烧器中燃烧,同时也应具有不可燃性,以便在飞机油箱中安全储存。燃料的低燃耗系数会受到综合效应的影响,包括分子结构、分子内化学键能和分子与分子之间的结合能。三种理论模型基于不同的个人观点,包括每种纯碳氢化合物的低燃比值、化学计量浓度和燃烧焓,其模拟结果并不令人满意,因为这些结果是在没有将所有潜在影响因素综合在一起的情况下推导出来的。人工神经网络(ANN)方法被用来解决喷气燃料中复杂成分与 LFL 的关系。为了提供充分和可用的成分输入,我们根据沸点、闪点和凝固点的约束条件,并结合石油基喷气燃料的统计数据,提取了燃料成分的边界。通过聚类分析,提取了 43 种临界成分作为代用碳氢化合物,这些代用碳氢化合物的 LFL 值偏差在 1% 以内。以 Sigmoid 函数为激活函数的 ANN-LFL 模型仅由滴入式燃料训练而成,可以区分滴入式燃料和非滴入式燃料。ANN LFL 模型能以 0.988 的准确率预测滴入式燃料的 LFL。非滴入式燃料的预测输出值与传统喷气式燃料有明显偏差。ANN-LFL 模型的优化方法可以提高对 LFL 的理解,并扩展 ANN 在 SAF 中的应用。
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来源期刊
Energy and AI
Energy and AI Engineering-Engineering (miscellaneous)
CiteScore
16.50
自引率
0.00%
发文量
64
审稿时长
56 days
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