喷嘴内部涡结构对自振脉冲SC-CO2射流能量转化效率影响研究

Study on effect of internal vortex structures in nozzles on energy conversion efficiency of self-excited pulsed SC-CO2 jets

  • 摘要: 利用高速射流破裂煤体,在煤层中构造煤层气流动通道,是提高煤层气采收率的重要手段。超临界二氧化碳(SC-CO2)射流自身的溶解、萃取特性可以提高煤层渗透性,并且,自振脉冲SC-CO2射流具有低破煤临界压力和高破煤效率的显著优势,在强化煤层气开采领域潜力巨大。然而,目前自激振荡射流喷嘴性能评价方法缺乏直接定量指标,导致确定最优喷嘴结构参数难度大,严重限制了其进一步推广。为此,基于喷嘴内部涡结构演化过程,提出自激振荡喷嘴能量转化效率计算方法,采用粒子图像测速技术(PIV)试验系统和大涡模拟(LES)相结合的方法捕捉喷嘴内部涡结构演化过程,分析喷嘴内部流体能量转化与分布特征。结果表明:通过分析射流开始喷射后1.75~1.79 s的射流流场拍摄图像,发现喷嘴中的涡结构主要出现在振荡腔内。振荡腔内沿剪切层运动的自激振荡脉冲SC-CO2射流与碰撞壁接触后先向上游运动,随着时间的推移,向上游运动的过程中逐渐与轴线上的射流汇合,下游喷嘴入口、上游喷嘴出口处壁面均出现强涡结构。SC-CO2射流在喷嘴入口输入的总能量转化为振荡腔内涡动能以及喷嘴出口形成的自激振荡脉冲SC-CO2射流总能量。腔径比为3.5时,射流能量转化效率高达80.80%,振荡腔内涡动能会诱导自振脉冲SC-CO2射流产生,但涡动能占比较大时会导致能量耗散,进一步,喷嘴出口处涡动能是用来调节射流集中性,喷嘴出口涡动能占比越小,喷射越集中。自振脉冲SC-CO2射流在不同喷嘴出口产生最大峰值应力排序为L3.5 > L1.5 > L2.5 > L2.0 > L3.0

     

    Abstract: The utilization of high-speed jet technology to fracture coal bodies and construct gas flow channels within coal seams is a crucial method for enhancing coalbed methane recovery efficiency. The supercritical carbon dioxide (SC-CO2) jet enhances coal-seam permeability through its inherent dissolution and extraction capabilities, while the self-excited pulsed SC-CO2 jet exhibits markedly low critical fracturing pressure and high coal-breaking efficiency, demonstrating substantial potential for strengthening coalbed methane recovery. However, the current performance evaluation methods for self-excited oscillating jet nozzles lack direct quantitative indicators, making it difficult to determine the optimal nozzle structural parameters and severely limiting their further promotion. The content is: In this paper, based on the evolution process of vortical structures inside the nozzle, a calculation method for the energy conversion efficiency of self-excited oscillation nozzles is proposed. Particle Image Velocimetry (PIV) experimental systems combined with Large Eddy Simulation (LES) are employed to capture the evolution process of vortical structures inside the nozzle, and to analyze the characteristics of fluid energy conversion and distribution inside the nozzle. Analysis of the flow-field images acquired at 1.75–1.79 s after the onset of jetting reveals that the nozzle’s vortex structures are concentrated in the oscillation chamber. The self-excited oscillation pulses of the SC-CO2 jet moving along the shear layer within the oscillation chamber initially travel upstream upon contact with the collision wall. Over time, during this upstream movement, they gradually merge with the jet along the axis. Strong vortex structures are observed at both the downstream nozzle entrance and the upstream nozzle exit. The total energy input at the nozzle inlet of the SC-CO2 jet is converted into vortex kinetic energy within the oscillation chamber and the total energy of the self-excited oscillating pulsed SC-CO2 jet formed at the nozzle outlet. When the chamber diameter ratio is 3.5, the efficiency of jet energy conversion reaches its peak at 80.80%. The eddy kinetic energy within the oscillating chamber induces the generation of self-excited oscillation pulsed SC-CO2 jets. However, when the proportion of eddy kinetic energy is significant, it can lead to energy dissipation. Furthermore, the eddy kinetic energy at the nozzle exit is utilized to regulate the jet's concentration. The smaller the dispersion of eddy kinetic energy at the nozzle exit, the more concentrated the jet becomes. The ranking of the maximum peak stress generated by self- excited pulsed SC-CO2 jets at different nozzle exits is as follows L3.5 > L1.5 > L2.5 > L2.0 > L3.0.

     

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