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Combustion kinetics of alternative jet fuels, Part-Ⅰ: Experimental flow reactor study

机译:替代喷射燃料的燃烧动力学,第Ⅰ部分:实验流程反应器研究

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摘要

A comprehensive collection of technical aviation fuels enabled an experimental and numerical study on detailed combustion chemistry and pollutant formation presented in a series of 3 interlinking parts. Part-I: Experimental Flow Reactor Study focuses on the characterization of 42 technical jet fuels and provides experimental speciation data for model development presented in Part-II: Model and Surrogate Strategy. Model validation based on the presented technical fuels here is presented in Part-III: Model Application on Technical Jet Fuels. The fuels investigated in this study cover a broad range of approved SAFs (Sustainable Aviation Fuels), candidates for approval, and technical products outside the present ASTM-D7566 specification and is completed by reference fuels (ASTM-D1655). This includes SAF components such as HEFA (Hydroprocessed Esters and Fatty Acids), ATJ (Alcohol-To-Jet), SIP (Synthesized Iso-Paraffins), and Fischer-Tropsch-products as well as their blends. A systematic investigation of the soot precursor chemistry by analyzing the influence of the complex chemical fuel composition on the intermediate species pool is presented. The experimental set-up consists of an atmospheric flow reactor with coupled molecular-beam mass spectrometer (MBMS). Quantitative evolution of combustion reaction intermediates is recorded for fuel-rich (phi = 1.2) and fuel-lean (phi = 0.8) conditions at intermediate temperatures up to 1200 K including small intermediate species (e.g. ethylene, butene) and soot precursor species (e.g. benzene, naphthalene, phenanthrene). A general systematic dependency of the soot precursor concentration on the degree of unsaturation (Index of Hydrogen Deficiency) or the hydrogen content, respectively, is demonstrated. Furthermore, larger soot precursor concentrations depend on the naphthalene content of the fuel.
机译:全面收集技术航空燃料的一系列实验和数值研究,详细燃烧化学和污染物形成,呈现在一系列3个相互作用的部分。第I部分:实验流动反应器研究重点是42项技术喷气燃料的表征,并为第1部分提供的模型发展提供了实验性质数据:模型和替代战略。基于本呈现的技术燃料的模型验证在第III部分提供:技术喷射燃料上的模型应用。本研究中调查的燃料涵盖了广泛的批准的SAF(可持续航空燃料),候选人候选人,技术产品在目前的ASTM-D7566规范之外,并通过参考燃料(ASTM-D1655)完成。这包括SAF组件,例如HEFA(加氢处理酯和脂肪酸),ATJ(醇 - 射流),SIP(合成的ISO-链烷烃)和Fischer-Tropsch-产物以及它们的共混物。介绍了通过分析复杂化学燃料组合物对中间物种池中的影响来系统研究烟灰前体化学。实验装置由具有耦合分子束质谱仪(MBMS)的大气流量反应器组成。燃烧反应中间体的定量演化被记录用于富含燃料(PHI = 1.2)和燃料稀(PHI = 0.8)条件,其在中间温度高达1200 k的中间体(例如乙烯,丁烯)和烟灰前体物种(例如苯,萘,菲苯乙烯)。证实了烟灰前体浓度对不饱和度(氢缺乏指数)或氢含量的一般系统依赖性。此外,较大的烟灰前体浓度取决于燃料的萘含量。

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  • 来源
    《Fuel》 |2021年第15期|120735.1-120735.12|共12页
  • 作者单位

    German Aerosp Ctr DLR Inst Combust Technol D-70569 Stuttgart Germany;

    German Aerosp Ctr DLR Inst Combust Technol D-70569 Stuttgart Germany;

    German Aerosp Ctr DLR Inst Combust Technol D-70569 Stuttgart Germany;

    IFP Energies Nouvelles IFPEN 1&4 Ave Bois Preau F-92852 Rueil Malmaison France;

    Sasol Energy 1 Klasie Havenga Rd ZA-1947 Sasolburg South Africa;

    Sasol Energy 1 Klasie Havenga Rd ZA-1947 Sasolburg South Africa;

    Sasol Energy 1 Klasie Havenga Rd ZA-1947 Sasolburg South Africa;

    Neste Corp Keilaranta 21 Espoo 02150 Finland;

    Neste Corp Keilaranta 21 Espoo 02150 Finland;

    Neste Corp Keilaranta 21 Espoo 02150 Finland;

    German Aerosp Ctr DLR Inst Combust Technol D-70569 Stuttgart Germany;

    German Aerosp Ctr DLR Inst Combust Technol D-70569 Stuttgart Germany;

    German Aerosp Ctr DLR Inst Combust Technol D-70569 Stuttgart Germany;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-19 03:03:42

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