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Modeling flow effects during polymer decomposition using percolation lattice statistics.

机译:使用渗流晶格统计来模拟聚合物分解过程中的流动效应。

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Foam encapsulants are commonly used in missile systems to increase the lifetime and reliability of the missile. The safety of the missile is greatly affected by the properties of the encapsulant. The pressure rises inside the missile as the foam degrades into smaller gaseous products, since the missile housing is essentially a closed container. If the pressure is high enough the housing may burst. The two foam encapsulants studied in this project are polyurethane foam and Removable Epoxy Foam. The ultimate goal of this project was to develop a computer model that can describe foam pyrolysis as a function of time, temperature, pressure, gas composition and confinement. The effect of pressure on foam decomposition was not well understood, with minimal of confinement effects. The effect of decomposition product flow was also not well understood. A previous model was able to empirically account for the pressure effects, but was not able to incorporate the confinement or flow effect into the foam decomposition.; Reliable pyrolysis data for both foams were obtained at atmospheric and high pressures, separate from confinement effects in this project. Buoyancy effects were found to be significant. The pyrolysis data showed that as the heating rate increased, the mass loss curves for the foam were shifted to higher reaction temperatures. A shift to higher reaction temperatures with increasing pressure and decreasing orifice size was observed. Furthermore, the decomposition product distribution shifted to produce less toluene diisocyanate and more carbon dioxide.; A model, called the MTPUF (Mass Transport PolyUrethane Model), was developed for the foam decomposition to include the capability for flow in and out of the cell. A population balance theory was the main idea that allowed for the capability of modeling the flow. Kinetic parameters were fit to the atmospheric pyrolysis data through an optimization technique. The parameters were tested against the high pressure and confinement data without being changed. The MTPUF modeling results correctly predicted the observed trend with heating rate, pressure and confinement and therefore, the MTPUF model seems capable of predicting these three effects on the polyurethane foam decomposition.
机译:泡沫密封剂通常用于导弹系统,以增加导弹的寿命和可靠性。密封剂的性质极大地影响了导弹的安全性。当泡沫降解成较小的气态产物时,导弹内部的压力上升,因为导弹壳体实质上是一个封闭的容器。如果压力足够高,外壳可能会破裂。在该项目中研究的两种泡沫密封剂是聚氨酯泡沫和可移动环氧泡沫。该项目的最终目标是开发一种计算机模型,该模型可以将泡沫热解描述为时间,温度,压力,气体成分和密闭度的函数。人们对压力对泡沫分解的影响知之甚少,限制作用最小。分解产物流动的影响也没有被很好地理解。先前的模型能够凭经验解释压力效应,但无法将限制或流动效应纳入泡沫分解。两种泡沫的可靠热解数据都是在大气压和高压下获得的,与该项目中的限制作用无关。发现浮力作用是显着的。热解数据表明,随着加热速率的增加,泡沫的质量损失曲线转移到更高的反应温度。观察到随着压力增加和孔口尺寸减小,反应温度升高。此外,分解产物的分布发生变化,从而产生更少的甲苯二异氰酸酯和更多的二氧化碳。为泡沫分解开发了一种称为MTPUF(大量运输的聚氨酯模型)的模型,以包括流入和流出气泡的能力。人口平衡理论是允许对流动进行建模的主要思想。通过优化技术将动力学参数拟合到大气热解数据中。针对高压和限制数据对参数进行了测试,未进行任何更改。 MTPUF模型结果正确地预测了加热速率,压力和限制条件下的观察趋势,因此MTPUF模型似乎能够预测这三种对聚氨酯泡沫分解的影响。

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