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Physical properties and spray pattern of tailored fuels: Liquid fuels containing suspended nanoparticles.

机译:量身定制的燃料的物理特性和喷雾方式:包含悬浮纳米颗粒的液体燃料。

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摘要

Physical properties such as density, viscosity and colloidal stability, and spray pattern of tailored fuels (ethanol and n-decane containing 20-30nm aluminum oxide) are investigated. Density is determined using a simple fixed volume experiment and is found to increases linearly with the percentage of nanoparticles by mass in the suspension. Viscosity of ethanol and its suspensions is determined using a rotational rheometer. Viscosity shear rate relationship shows that with increase in particle concentration, the viscosity of the suspension increases. It was also observed that suspension with 5% or higher particle concentrations showed shear thinning behavior, deviating from the Newtonian behavior of pure solvents such as ethanol. Ethanol and n-decane/Span80 (surfactant) suspensions showed good colloidal stability for up to 10-12 minutes with very little sedimentation for low particle concentrations of up to 5%. Pure n-decane suspensions did not maintain stability for more than 5 seconds and immediate sedimentation was observed. 5% aluminum oxide and n-Decane/span80 suspensions did not clog the 267microm orifice nozzle after 10 minutes of operation with a nitrogen driven fuel supply system operating at 50-80psi pressure. Ethanol suspensions (without surfactant) with 5% aluminum oxide clogged the nozzle after ~5 minutes of operation. Both fuels carried lower percentage of particles (1-4%) well through the nozzle causing no clogging for a 10-12minute operation time. A SETScan OP-200 patternator is used to characterize the spray. Results show that particle addition of up to 4% nanoparticles has little effect on spray angle and the spray pattern. However, as the particle concentration is increased the total surface area of the spray is slightly reduced. To study the spray combustion, a vitiated coflow spray burner was designed and built. The air and coflow fuel supply systems will be finalized in the near future.
机译:研究了物理性能,如密度,粘度和胶体稳定性,以及定制燃料(乙醇和正癸烷,含20-30nm氧化铝)的喷雾模式。使用简单的固定体积实验确定密度,发现密度随悬浮液中纳米颗粒的质量百分比线性增加。使用旋转流变仪测定乙醇及其悬浮液的粘度。粘度剪切速率关系表明,随着颗粒浓度的增加,悬浮液的粘度增加。还观察到颗粒浓度为5%或更高的悬浮液表现出剪切稀化行为,这与纯溶剂(如乙醇)的牛顿行为有所不同。乙醇和正癸烷/ Span80(表面活性剂)悬浮液在长达10-12分钟的时间内表现出良好的胶体稳定性,对于高达5%的低浓度颗粒,几乎没有沉淀。纯正癸烷悬浮液不能保持稳定性超过5秒,并且观察到立即沉淀。用氮气驱动的燃料供应系统在50-80psi的压力下运行10分钟后,5%的氧化铝和正癸烷/ span80悬浮液不会堵塞267微米的孔口喷嘴。操作约5分钟后,含5%氧化铝的乙醇悬浮液(不含表面活性剂)堵塞喷嘴。两种燃料都通过喷嘴很好地运送了较低百分比的颗粒(1-4%),在10-12分钟的运行时间内没有堵塞。 SETScan OP-200图案形成器用于表征喷雾。结果表明,最多添加4%的纳米颗粒会影响喷雾角度和喷雾方式。但是,随着颗粒浓度的增加,喷雾的总表面积会略有减少。为了研究喷雾燃烧,设计并制造了一个通风的同流喷雾燃烧器。空气和同流燃料供应系统将在不久的将来完成。

著录项

  • 作者

    Tanvir, Saad.;

  • 作者单位

    Purdue University.;

  • 授予单位 Purdue University.;
  • 学科 Engineering Aerospace.
  • 学位 M.S.A.A.
  • 年度 2011
  • 页码 139 p.
  • 总页数 139
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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