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Quantification of elemental and total carbon in combustion particulate matter using thermal-oxidative analysis

机译:使用热氧化分析定量燃烧颗粒物质中的元素碳和总碳

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摘要

The use of a two-step thermal-oxidative analysis (TOA) technique for quantification of the mass of total carbon (TC) and elemental carbon (EC) of turbine engine-borne particulate matter (PM) has been evaluated. This approach could be used in lieu of analysis methods which were developed to characterize diluted PM. This effort is of particular interest as turbine engine PM emissions typically have a higher EC content than ambient aerosols, and filter sample mass loadings can be significantly greater than recommended for existing analysis techniques. Analyses were performed under a pure oxygen environment using a two-step temperature profile; reference carbon and actual PM samples were used to identify appropriate analysis conditions. Thermal gravimetric analysis (TGA) methods were used to provide guidance on the nature of the carbon in several of the materials. This was necessary as a standard reference material does not exist for determination of the EC fraction in PM. The TGA also assisted in identifying an appropriate temperature range for the first-stage of the TOA method. Quantification of TC and EC for turbine engine PM samples using TOA was compared to results obtained using the NIOSH 5040 thermal-optical method. For first-stage TOA temperatures of 350 degrees C and 400 degrees C, excellent agreement between the techniques was observed in both the quantified TC and EC, supporting the viability for using TOA for analysis of turbine engine PM samples. A primary benefit of using TOA for these types of PM samples is that filters with relatively high PM mass loadings (sampled at the emission source) can be readily analyzed. In addition, an entire filter sample can be evaluated, as compared to the use of a filter punch sample for the NIOSH technique. While the feasibility of using a TOA method for engine PM samples has been demonstrated, future studies to estimate potential OC charring and oxidation of EC-type material may provide additional data to assess its impact on the OC/EC fractions for other carbon-type measurements. Implications: This work presents results and procedures of an analytical method for the determination of total and elemental carbon, i.e., TC and EC present in combustion source particulate matter samples. In general, it is shown that the LECO TOA methodology is as reliable and comprehensive as NIOSH 5040 for determining TC and EC carbon types in particulate matter present in turbine emission sources, and should be considered as an alternative. Principles of the methodology, differences, and corresponding agreement with the standard NIOSH 5040 method and TGA analysis are discussed.
机译:已经评估了使用两步热氧化分析(TOA)技术来量化涡轮发动机携带的颗粒物(PM)的总碳(TC)和元素碳(EC)的质量。该方法可以代替分析方法来表征稀释的PM。由于涡轮发动机的PM排放物通常比周围的气溶胶具有更高的EC含量,因此这项工作特别引人注目,并且过滤器样品的质量负载可能明显大于现有分析技术的建议值。使用两步温度曲线在纯氧环境下进行分析;参考碳和实际PM样品用于确定适当的分析条件。热重分析(TGA)方法用于为几种材料中碳的性质提供指导。这是必需的,因为不存在用于确定PM中EC含量的标准参考物质。 TGA还协助为TOA方法的第一阶段确定合适的温度范围。将使用TOA对涡轮发动机PM样品的TC和EC定量与使用NIOSH 5040热光学方法获得的结果进行比较。对于350摄氏度和400摄氏度的第一阶段TOA温度,在定量TC和EC中都观察到了技术之间的极佳一致性,这支持了使用TOA分析涡轮发动机PM样品的可行性。对这些类型的PM样品使用TOA的主要好处是,可以轻松分析具有相对较高PM质量负载(在排放源处采样)的过滤器。此外,与使用NIOSH技术的过滤器冲头样品相比,可以评估整个过滤器样品。虽然已经证明了使用TOA方法检测发动机PM样品的可行性,但未来的研究估计潜在的OC炭化和EC型材料的氧化可能会提供其他数据,以评估其对其他碳型测量对OC / EC馏分的影响。含义:这项工作介绍了一种测定总碳和元素碳(即燃烧源颗粒物样品中存在的TC和EC)的分析方法的结果和程序。总的来说,已表明,LECO TOA方法与NIOSH 5040一样可靠,全面,可用于确定涡轮机排放源中存在的颗粒物中的TC和EC碳类型,应将其视为一种替代方法。讨论了该方法的原理,区别以及与标准NIOSH 5040方法和TGA分析的相应一致性。

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  • 来源
    《Journal of the air & waste management association 》 |2019年第8期| 1003-1013| 共11页
  • 作者单位

    Univ Dayton, Res Inst, Fuels & Combust Divison, 300 Coll Pk, Dayton, OH 45469 USA;

    Univ Dayton, Res Inst, Fuels & Combust Divison, 300 Coll Pk, Dayton, OH 45469 USA;

    Univ Dayton, Res Inst, Fuels & Combust Divison, 300 Coll Pk, Dayton, OH 45469 USA;

    Univ Dayton, Res Inst, Fuels & Combust Divison, 300 Coll Pk, Dayton, OH 45469 USA;

    Univ Dayton, Res Inst, Fuels & Combust Divison, 300 Coll Pk, Dayton, OH 45469 USA;

    Air Force Res Lab, Wright Patterson Air Force Base, Dayton, OH USA;

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