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Pyrolysis, ignition and combustion of solid fuels for ramjet applications.

机译:用于冲压发动机的固体燃料的热解,着火和燃烧。

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摘要

The utilization of the most attractive metal additive, boron powder, in ramjet application still remains in the development stages. This is due mainly to the combustion efficiency problems associated with boron. On the other hand, the very popular metal additive, magnesium, has very good ignitability and high combustion efficiency, but has a low heating value. The scope of this study was concentrated on these two kinds of metal additives and three different types of polymeric binders--HTPB, PTFE, and high energy poly(BAMO/NMMO). Using various combinations of these ingredients, a total of 17 different solid fuels were investigated.; The purpose of the present research was to study the pyrolysis, ignition, and combustion characteristics of the abovementioned fuel samples, using high-powered CO{dollar}sb2{dollar} laser testing system, a windowed strand burning setup, and two cross-flow combustion facilities--a kerosene burner and a blowdown supersonic wind tunnel.; The pyrolyzed species of solid fuels were identified by a GC-MSD. The ignition characteristics of boron/HTPB fuels were determined by the CO{dollar}sb2{dollar} laser ignition system. A hypothesis based on absorptivity, thermal diffusivity, and reactivity was proposed to interpret the observed phenomena. The effects of four additives on ignition delay time of boron/HTPB fuels were measured, and CeF{dollar}sb3{dollar} was found to be the most effective one.; Several combinations of boron and magnesium/PTFE fuels were tested. A sample composed of 20% Mg/30% B/50% PTFE exhibited a highly vigorous reaction, and it appears to be very promising for improving boron combustion efficiency. Mg/PTFE/Viton A fuel only recently has been considered as a possible candidate for ramjet (solid ducted rocket) applications. This fuel exhibited a very unique burning phenomenon--ambient oxygen has an adverse effect on the ignition delay time and also on the burning rate. An explanation for this behavior was postulated and supported by several different measurements. Finally, a sample containing 30% boron and 17.6% Poly(BAMO/NMMO) were tested. Based on the experimental results, it can be concluded that with the help of a highly energetic binder, an efficient combustion of boron can be expected.
机译:在冲压喷气机应用中,最具吸引力的金属添加剂硼粉的使用仍处于开发阶段。这主要是由于与硼有关的燃烧效率问题。另一方面,非常流行的金属添加剂镁具有很好的可燃性和高燃烧效率,但发热量低。本研究的范围集中在这两种金属添加剂和三种不同类型的聚合物粘合剂上-HTPB,PTFE和高能聚(BAMO / NMMO)。使用这些成分的各种组合,共研究了17种不同的固体燃料。本研究的目的是使用高功率的CO {dollar} sb2 {dollar}激光测试系统,开窗的线束燃烧装置和两个交叉流来研究上述燃料样品的热解,着火和燃烧特性。燃烧设施-煤油燃烧器和排污超音速风洞。固体燃料的热解种类通过GC-MSD鉴定。硼/ HTPB燃料的点火特性由CO {dollar} sb2 {dollar}激光点火系统确定。提出了基于吸收率,热扩散率和反应性的假设来解释观察到的现象。测量了四种添加剂对硼/ HTPB燃料点火延迟时间的影响,发现CeF {dollar} sb3 {dollar}是最有效的添加剂。测试了硼和镁/ PTFE燃料的几种组合。由20%Mg / 30%B / 50%PTFE组成的样品表现出强烈的反应,对于提高硼燃烧效率似乎很有希望。 Mg / PTFE / Viton仅在最近才考虑将燃料用作冲压喷气发动机(固体导管火箭)的可能选择。这种燃料表现出非常独特的燃烧现象-氧气对点火延迟时间和燃烧速率都有不利影响。假定对此行为进行了解释,并得到了几种不同的测量结果的支持。最后,测试了包含30%硼和17.6%Poly(BAMO / NMMO)的样品。基于实验结果,可以得出结论,借助于高能粘合剂,可以期望硼的有效燃烧。

著录项

  • 作者

    Chen, Dah Ming.;

  • 作者单位

    The Pennsylvania State University.;

  • 授予单位 The Pennsylvania State University.;
  • 学科 Engineering Materials Science.; Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 1988
  • 页码 215 p.
  • 总页数 215
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 工程材料学;机械、仪表工业;
  • 关键词

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