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Predictive Modeling of Aerospace Fuel Properties Using Comprehensive Two-Dimensional Gas Chromatography with Time-Of-Flight Mass Spectrometry and Partial Least Squares Analysis

机译:航空航天燃料特性的预测模型,采用综合二维气相色谱法与飞行时间质谱与局部最小二乘分析

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摘要

Increasingly stringent requirements for aerospace propulsion system performance, reliability, and operability motivate quantitative connections between fuel composition, physical characteristics, and system performance. Chemically accurate assessment of aviation turbine fuels (Jet-A, JP-8, etc.) and kerosene-based rocket propellants (RP-1 and RP-2) is requisite to mature these models. Comprehensive two-dimensional gas chromatography with time-of-flight mass spectrometry (GC x GC-TOFMS) is an excellent analytical tool for measuring detailed chemical information contained in complex fuels. Additionally, multivariate data analysis methods, referred to as chemometrics, are ideally suited to relate detailed chemical information contained within the GC x GC-TOFMS data to fuel properties and performance in a predictive manner. Herein, we apply these techniques to a chemically diverse set of 74 distillate and multicomponent aerospace fuels, resulting in an improved understanding of the chemical compositional basis for physical and thermochemical behavior. Informed by GC x GC-TOFMS data, highly reliable partial least squares (PLS) models are developed and employed in the prediction of physical properties (measured separately using conventional test methods). Root-mean-square errors of cross-validation (RMSECV) were relatively low: values of 0.0450 cSt, 41.3 Btu/lbm, 0.130 mass %, and 0.0064 g/mL were obtained for viscosity, heat of combustion, hydrogen content, and density, respectively. The corresponding normalized root-mean-square errors of cross-validation (NRMSECV) were 6.01, 10.3, 8.71, and 7.12%, respectively. Investigation of the linear regression vectors (LRVs) provides valuable insight into the relationship between the chemical composition and physical properties, enabling, in principle, the model-informed selection of fuel chemical composition to achieve desired performance criteria.
机译:对航空航天推进系统性能,可靠性和可操作性的越来越严格的要求激励燃料组合物,物理特性和系统性能之间的定量连接。进而准确评估航空涡轮燃料(Jet-A,JP-8等)和基于煤油的火箭推进剂(RP-1和RP-2)是成熟这些模型的必要条件。具有飞行时间质谱(GC X GC-TOFMS)的综合二维气相色谱法是用于测量复杂燃料中包含的详细化学信息的优异分析工具。另外,称为化学计量学的多变量数据分析方法非常适合以预测的方式将包含在GC X GC-TOFM数据中的详细化学信息涉及燃料性能和性能。在此,我们将这些技术应用于化学多样化的74馏分和多组分航空航天燃料,从而改善了物理和热化学行为的化学成分基础的理解。 GC X GC-TOFMS数据通知,高度可靠的局部最小二乘(PLS)模型在物理性质的预测中开发并采用(使用常规测试方法单独测量)。交叉验证(RMSECV)的根均方误差相对较低:0.0450CST的值,41.3 BTU / LBM,0.130质量%和0.0064g / ml的粘度,燃烧热,氢含量和密度。 , 分别。交叉验证(NRMSECV)的相应归一化的根均方误差分别为6.01,10.3,8.71和7.12%。线性回归向量(LRV)的研究提供了有价值的洞察化学成分和物理性质之间的关系,原则上实现了燃料化学组合物的模型信息,以实现所需的性能标准。

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  • 来源
    《Energy & fuels》 |2020年第4期|4084-4094|共11页
  • 作者单位

    Univ Washington Dept Chem Seattle WA 98195 USA;

    Univ Washington Dept Chem Seattle WA 98195 USA;

    Air Force Res Lab RQRC Edwards Afb CA 93524 USA;

    Univ Washington Dept Chem Seattle WA 98195 USA;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);美国《生物学医学文摘》(MEDLINE);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
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