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Kinetic pyrolysis of poly(methyl methacrylate) and its effects on the ignition delay time.

机译:聚甲基丙烯酸甲酯的动力学热解及其对点火延迟时间的影响。

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摘要

An experimental technique is developed in order to capture a phenomenon related to micro-gravity combustion, the piloted ignition mixing time, in normal gravity conditions. The technique is based on investigating the degradation of a large particle size material, 0.5mm diameter PMMA by Thermogravimetry (TG)/Mass Spectrometry (MS)/Differential Thermal Analysis (DTA). The experimental results were incorporated in a numerical model previously developed for determining the piloted ignition delay time of a solid combustible impulsively exposed to an incident heat flux and prescribed forced flow. The results indicated, that due to mass transport effects and a rate limiting process controlled by diffusion, the theoretical surface temperature over-predicted the experimental surface temperature, beginning at 285°C, thus, this temperature was deemed the pyrolysis temperature. The overshoot time period commencing from the pyrolysis temperature to the ignition is deemed the mixing time. The over predicted surface temperature is attributed to mass transfer reduction of the volatile fuel emanating from the surface detected by the TG/MS. The over predicted numerical surface temperature is attributed to applying the forced convection heat transfer coefficient, which corresponds to negligible mixing time.; TG/MS/DTA measurements indicate that due to the large particle size, mass transport is impacting the degradation in both inert and oxidative environments. The diffusion process has inhibiting effects on the weight loss rate and the rate of production of gases, these inhibiting effects are enhanced with the increase of oxygen content. A net reduction of 40% in the weight loss rate was experienced by enhancing the oxygen content from 5% to 21% O 2 in N2. Furthermore, in an oxidative environment compared to that of inert environment, diffusion is initiated at lower temperatures, and was shifted to higher temperatures with lowering the heating rates. The MS data showed abrupt changes in the rate of production of gases that corroborated the hypothesis that degradation is impacted by mass transport effects. DTA profiles indicated that in an inert environment the reaction is endothermic with value of 2.8 kJ/g, while in oxidative environment the reaction is exothermic.
机译:为了捕获与微重力燃烧有关的现象,即在正常重力条件下的引燃混合时间,开发了一种实验技术。该技术基于通过热重法(TG)/质谱(MS)/差热分析(​​DTA)研究直径为0.5mm的大粒径材料的降解。将实验结果并入先前开发的数值模型中,该数值模型用于确定脉冲状暴露于入射热通量和规定的强制流动的固体可燃物的引燃点火延迟时间。结果表明,由于传质效应和受扩散控制的限速过程,理论表面温度从285°C开始对实验表面温度进行了过度预测,因此该温度被认为是热解温度。从热解温度到着火的过冲时间段被视为混合时间。过高的预测表面温度归因于由TG / MS检测到的从表面散发出来的挥发性燃料的传质减少。过度预测的表面温度归因于施加强制对流传热系数,该系数对应于可忽略的混合时间。 TG / MS / DTA测量表明,由于粒径较大,在惰性和氧化环境中,传质都会影响降解。扩散过程对重量损失率和气体产生速率具有抑制作用,这些抑制作用随着氧含量的增加而增强。通过将 N <中的 O 2 中的氧含量从5%提高到21%,可以使体重减轻净减少40% sub> 2 。此外,与惰性环境相比,在氧化环境中,扩散是在较低温度下引发的,并随着加热速率的降低而转移到较高温度。 MS数据显示气体产生速率的突然变化,证实了降解受传质影响的假设。 DTA曲线表明,在惰性环境中,该反应是吸热的,值为2.8 kJ / g,而在氧化环境中,该反应是放热的。

著录项

  • 作者

    Dakka, Sam.;

  • 作者单位

    University of Maryland College Park.;

  • 授予单位 University of Maryland College Park.;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 2002
  • 页码 235 p.
  • 总页数 235
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;
  • 关键词

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