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High temperature spectroscopic measurements of aluminum combustion in a heterogeneous shock tube

机译:高温光谱测量异质激波管中铝的燃烧

摘要

Aluminum is an important energetic material that burns with a variety of oxidizers with a high reaction enthalpy. It is a top performer for energy density if oxidizer mass is considered as well as the fuel. Because of this, it is often used as an energetic additive in anaerobic conditions because it reacts in what typically are products of primary fuels and oxidizers and further increases chamber temperatures in solid rocket motors or blast overpressure in enhanced blast weapons. Despite decades of research, gaps still exist in the knowledge of how aluminum burns, especially with the recent trend of using smaller particles (10 micron and below). While aluminum is a very energetic material, its rate of oxidation is relatively low, and efforts are made to not only increase the heat release rate of particles reacting with oxidizer, but also to increase peak combustion temperature. Experimental studies were performed measuring the combustion characteristics of aluminum in the heterogeneous shock tube. The heterogeneous shock tube provides unmatched control of temperature, pressure, oxidizer concentration, etc., in which to test energetic materials of different particle sizes. The burning time diameter exponent, n as in t_b ~ d^n, in aluminum particle combustion was measured to be as low as, or lower than 0.3, in conditions in the transition regime between kinetic and diffusion limited particles. This anomalous result, as well as observed increases of burn time with pressure when using water vapor as an oxidizer had been attributed to a pressure dependence on ignition of particles in these conditions or broad overlapping size distributions. Both theories were tested and rejected.Furthermore, an acrylic end section was implemented on the shock tube which provides complete optical access to the final 61 cm of the shock tube. This optical access allowed high speed images (50k fps) of the particle motion, ignition, and combustion. Results are presented which give a more complete understanding of burntime variability in the heterogeneous shock tube, owing to the contribution of initially wall-bound particles vs. those that are in the free stream upon the passage of the incident shock, bright clusters of rapidly moving burning particles, and non-uniform cloud distributions in the tube, all previously undifferentiated by shock tube burntime methods. Absorption spectroscopy was used to probe the ground state of Aluminum monoxide (AlO), a gas phase combustion intermediate, and Al vapor in order to quantify the amount of Al and AlO present under conditions where these species were not observed in emission previously, notably in most conditions with nano-aluminum particles. At least three regimes of combustion were observed for nano-aluminum combustion. At temperatures above 2000 K, particles burn with AlO and Al vapor present. Between 1500 K and 2000 K, particles burn with Al vapor present, but without detectable AlO. Between 1200 K and 1500 K, particles burn without either vapor phase component present. These results had important implications for two proposed mechanisms for nano-aluminum ignition and combustion.Optical measurements of the peak combustion temperature from AlO consistently measure near 3200 K in micro-Al combustion, even though higher temperatures are seen near larger particles. One proposed limiting factor was the volatilization temperature of alumina. The reference literature is divided on this temperature, which previously was measured with large extrapolations. The volatilization temperature was measured by measuring the extinction cross-section of nano- and micro-alumina at non-resonant wavelengths at different ambient temperatures. The volatilization temperature at 1 atm appears to be at least as high as 4000 K and does not appear to be a limiting temperature in micro-Al combustionFinally, two other sets of measurements were made to support high temperature measurements of aluminum combustion, especially in the optically thick conditions commonly observed in propellant plumes or explosive fireballs. The first was a measurement of the alumina emissivity spectral dependence, which is absolutely necessary to make pyrometric measurements. A significant temperature dependence was observed in the emissivity spectral dependence. Additionally, spatially resolved fiber optic emission probing was used in the optically thick fireballs from aluminized explosives. Using the probes allowed observations inside the fireball and avoided biases from temperature inhomogeneity and ambient air interactions in these explosive fireballs.
机译:铝是一种重要的高能材料,可与多种具有高反应焓的氧化剂一起燃烧。如果考虑氧化剂的质量以及燃料,它在能量密度方面是表现最好的。因此,它通常在厌氧条件下用作高能添加剂,因为它会在主要燃料和氧化剂的产物中发生反应,并进一步增加固体火箭发动机的燃烧室温度或增强爆炸武器中的爆炸超压。尽管进行了数十年的研究,但是铝燃烧的知识仍然存在差距,特别是在最近使用较小颗粒(10微米及以下)的趋势中。尽管铝是一种非常高能的材料,但是其氧化速率相对较低,并且不仅努力提高与氧化剂反应的颗粒的放热速率,而且还努力提高峰值燃烧温度。进行了实验研究,以测量异质激波管中铝的燃烧特性。异质冲击管可提供对温度,压力,氧化剂浓度等的无与伦比的控制,可在其中测试不同粒径的高能材料。在动力学和扩散受限的颗粒之间的过渡状态下,在铝颗粒燃烧中的燃烧时间直径指数n(t_b〜d ^ n)被测量为低至或低于0.3。这种异常结果,以及在使用水蒸气作为氧化剂时观察到的燃烧时间随压力而增加的现象,都归因于在这些条件下或颗粒尺寸分布重叠时,压力取决于颗粒的着火。两种理论都经过了测试和否定。此外,在冲击管上使用了丙烯酸树脂端部,可以通过光学方式完全接触到冲击管的最后61厘米。这种光学访问方式允许粒子运动,点火和燃烧的高速图像(50k fps)。给出的结果可以更全面地了解非均质激波管中的燃烧时间变异性,这归因于初始撞击时壁壁结合的粒子与自由流中自由流动的粒子的贡献,快速移动的明亮簇燃烧粒子,以及管道中不均匀的云分布,这些都是以前通过激波管燃烧时间方法无法区分的。吸收光谱法用于探测一氧化铝(AlO),气相燃烧中间体和Al蒸气的基态,以便量化在以前未观察到这些物种的排放的条件下(尤其是在燃烧中)存在的Al和AlO的量。大多数情况下使用纳米铝颗粒。对于纳米铝燃烧,观察到至少三种燃烧方式。在高于2000 K的温度下,存在AlO和Al蒸气的情况下燃烧颗粒。在1500 K和2000 K之间,存在Al蒸气但没有可检测到的AlO的情况下燃烧颗粒。在1200 K和1500 K之间,粒子燃烧时不存在任何气相成分。这些结果对提出的两种用于纳米铝点火和燃烧的机制具有重要意义.AlO的峰值燃烧温度的光学测量在微Al燃烧中始终测量在3200 K附近,即使在较大的颗粒附近发现较高的温度也是如此。提出的一个限制因素是氧化铝的挥发温度。参考文献在此温度上有所不同,该温度以前是通过大量外推法测量的。通过在不同的环境温度下在非共振波长下测量纳米氧化铝和微米氧化铝的消光截面来测量挥发温度。在1个大气压下的挥发温度似乎至少高达4000 K,并且似乎不是微Al燃烧的极限温度。最后,进行了另外两组测量以支持铝燃烧的高温测量,尤其是在铝燃烧中。通常在推进剂羽流或爆炸性火球中观察到的光学上较厚的情况。首先是对氧化铝发射率光谱依赖性的测量,这对于进行高温测量是绝对必要的。在发射率光谱依赖性中观察到显着的温度依赖性。另外,空间分辨的光纤发射探测被用于镀铝炸药的光学厚度的火球中。使用探头可以观察火球内部,并避免了这些爆炸性火球中温度不均匀性和环境空气相互作用造成的偏差。

著录项

  • 作者

    Lynch Patrick T.;

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  • 年度 2010
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  • 原文格式 PDF
  • 正文语种 {"code":"en","name":"English","id":9}
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