首页> 外文会议>AIAA Aerospace Sciences Meeting;AIAA SciTech Forum >Mechanism of Plasma-Assisted Ignition for H_2 and C1-C5 Hydrocarbons
【24h】

Mechanism of Plasma-Assisted Ignition for H_2 and C1-C5 Hydrocarbons

机译:等离子体辅助点燃H_​​2和C1-C5烃的机理

获取原文

摘要

There are several mechanisms that affect a gas when using a discharge to initiate combustion or stabilize the flame. There are two thermal mechanisms: 1) gas heating due to energy release causes the acceleration of chemical reactions; 2) inhomogeneous gas heating generates flow perturbations, promoting turbulence and mixing. Non-thermal mechanisms include 3) the ionic wind effect (the momentum transfer from the electric field to the gas due to space charge); 4) ions and electrons drift in the electric field can cause additional fluxes of active radicals in gradient flows; 5) excitation, dissociation and ionization of the gas by e-impact leads to the production of nonequilibrium radicals and changes the kinetic mechanisms of ignition and combustion. These mechanisms combined together, or separately, can provide additional control of combustion, which is necessary for ultra-lean flames, high-speed flows, cold low-pressure conditions of high-altitude GTE relighting, detonation initiation in pulsed detonation engines, distributed ignition control in HCCI engines, and so on. The operation efficiency of a scramjet depends critically on the efficiency and completeness of the combustion process. Namely, a low efficiency of combustion restricts the upper boundary of the flight envelope. Plasma-assisted combustion is one of the very interesting possibilities for stabilizing ignition at high altitudes, and low dynamic pressures and temperatures. In addition, plasma-assisted ignition can stabilize the ultra-fast combustion required for M > 10 operations. Thus, the ultimate goal of using plasma technologies in hypersonic applications is the extension of an engine's stability region to low dynamic pressures (0.2-0.05 arm) and high Mach numbers (M = 10-20). The major difference between common combustion and plasma-assisted combustion is the extremely nonequilibrium excitation of the gas in the discharge. The external electric field accelerates electrons, and the energy exchange between electrons and the translational degrees of freedom of molecules is very slow because of the huge differences in masses. As a result of this feature, electron impact can transfer energy to the internal degrees of freedom of molecules only. If the rate of internal energy relaxation is not very high, the population distribution of the excited states of the molecules will differ greatly from the initial Boltzmann energy distribution. The overpopulation of excited states causes an increase in the system reactivity and facilitates ignition and flame propagation. From this point of view, the most important questions regarding plasma-stimulated chemistry concern the distribution of the discharge energy through the different degrees of freedom of molecules, the rate of system relaxation (thermalization) and the response of a chemically active system to this nonequilibrium excitation. Precise control of the direction of energy deposition in the plasma is possible for a relatively short time period when the multiplication of electrons (above the breakdown threshold) or recombination (below the threshold) do not have enough time to change the electron concentration and plasma conductivity significantly. When the plasma conductivity is not very high, it is possible to maintain a desired value of E in the inter-electrode gap. This approach, together in combination with a short high-voltage pulse and constant bias, allows for the selective and extremely nonequilibrium excitation of the gas. The duration of the critical high-voltage pulse depends on the gas parameters (density, composition), but for the practically important range of parameters, it is restricted to few nanoseconds. The main mechanisms of nonequilibrium gas excitation and their influence on the ignition and combustion were briefly discussed. Rotational excitation, vibrational excitation, electronic excitation, dissociation by electron impact and ionization were all analyzed, as well as the ways in which the selectivity of the gas excitation in the discharge can be controlled. Despite of some lack of knowledge of mechanism details, a nonequilibrium plasma demonstrates great potential for controlling ultra-lean, ultra-fast, low-temperature flames and is an extremely promising technology for a very wide range of applications.
机译:当使用放电引发燃烧或稳定火焰时,有几种影响气体的机制。有两种热机制:1)由于能量释放而引起的气体加热导致化学反应的加速; 2)气体加热不均匀会产生流动扰动,从而促进湍流和混合。非热机制包括3)离子风效应(由于空间电荷而将动量从电场传递到气体); 4)电场中的离子和电子漂移会引起梯度流动中活性自由基的额外通量; 5)电子碰撞激发,离解和电离气体导致产生非平衡自由基,并改变着火和燃烧的动力学机制。这些机制组合在一起或单独使用,可以提供额外的燃烧控制,这对于超稀薄火焰,高速流动,高空GTE重点燃的低温低压条件,脉冲爆震发动机中的爆震启动,分布式点火是必要的HCCI引擎中的控制,等等。超燃冲压发动机的运行效率主要取决于燃烧过程的效率和完整性。即,低燃烧效率限制了飞行包线的上限。等离子体辅助燃烧是在高海拔,低动态压力和低温度下稳定点火的非常有趣的可能性之一。此外,等离子辅助点火可以稳定M> 10操作所需的超快燃烧。因此,在高超音速应用中使用等离子技术的最终目标是将发动机的稳定区域扩展到低动态压力(0.2-0.05臂)和高马赫数(M = 10-20)。普通燃烧与等离子辅助燃烧之间的主要区别是放电气体的极不平衡激发。外部电场使电子加速,由于质量的巨大差异,电子之间的能量交换和分子的平移自由度非常慢。由于此功能,电子撞击只能将能量转移到分子的内部自由度。如果内部能量弛豫速率不是很高,则分子的激发态的总体分布将与初始玻耳兹曼能量分布大不相同。激发态的过剩引起系统反应性的增加,并促进点火和火焰传播。从这一观点出发,关于等离子体激发化学的最重要问题涉及通过不同分子自由度的放电能量分布,系统弛豫速率(热化)以及化学活性系统对此不平衡的响应。励磁。当电子的倍增(击穿阈值以上)或复合(阈值以下)没有足够的时间来改变电子浓度和等离子体电导率时,可以在较短的时间内精确控制等离子体中的能量沉积方向显着地。当等离子体电导率不是很高时,可以在电极间间隙中保持期望的E / n值。这种方法与短的高压脉冲和恒定的偏压结合在一起,可以选择性地且极度不平衡地激发气体。临界高压脉冲的持续时间取决于气体参数(密度,组成),但是对于实际重要的参数范围,它被限制在几纳秒内。简要讨论了非平衡气体激发的主要机理及其对点火和燃烧的影响。分析了旋转激发,振动激发,电子激发,电子碰撞和电离引起的离解,以及可控制放电中气体激发选择性的方法。尽管缺乏对机理细节的了解,但非平衡等离子体仍显示出控制超稀薄,超快,低温火焰的巨大潜力,并且是非常广泛应用的极有前途的技术。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号