双级液气喷射器喉管的特性

对双级液气喷射器喉管进行系统测试，建立了一系列经验特性方程。     

高含硫天然气引射增压的数值模拟及硫析出分析

针对普光气田高含硫且井口压力不断降低的特点,提出了使用喷射器来将低压天然气增压输送的方案。高含硫天然气在引射增压过程中由于温度压力的变化,在喷射器内可能出现硫析出,单质硫的沉积会造成堵塞,还会加剧设备的腐蚀。建立了高含硫天然气引射增压数学模型,数值模拟了喷射器中天然气的压力、温度、速度分布特征。分析了引射系数的影响因素及引射增压过程中的硫析出的可能性.研究发现温度对喷射器内硫析出有重要的影响,所以可以提高工作流体入口温度来提高喷射器内的整体温度,从而减少硫的析出。     

湿法液柱喷射烟气脱硫反应的实验研究

湿法液柱烟气脱硫技术是基于简易湿法石灰-石膏烟气法开发的新型湿法脱硫技术,本套设备在2000-2001年问进行了工业级示范实验运行,得到了湿法液柱脱硫反应的一些基本数据与规律。本文主要探讨了湿法液柱脱硫系统中液气比、吸收塔浆液pH值、烟气温度和烟气中SO2含量等工艺参数对系统脱硫效率的影响规律,并进行了初步的机理分析,为进一步的改进湿法液柱烟气脱硫系统的工艺奠定了基础。     

纳秒脉冲下变压器油两相流注放电仿真研究

为揭示液体电介质击穿过程中形成的气体放电通道对液体电介质放电过程的影响,以针—板电极间隙变压器油为研究对象,基于等离子体流体力学模型,引入了液体电介质放电过程中气相放电通道对电离机制及自由电荷迁移率的影响,建立了用于模拟脉冲电压下液体电介质放电过程的两相流体模型,仿真研究了纳秒脉冲下针板电极流注放电的起始与发展过程。仿真结果表明:采用Heaviside方程可以在模型的不同区域同时实现气相物理过程和液相物理过程的模拟与计算。气相物理过程的引入导致流注尾部电场显著降低,流注头部电场进一步增强,使流注通道的发展速度要高于传统液相模型,有助于加深对纳秒脉冲下液体电介质中预击穿流注的起始、发展过程的认识和理解。     

Realization of an advanced nozzle concept for compact chemical oxygen iodine laser

Conventional supersonic chemical oxygen–iodine lasers (SCOIL) are not only low-pressure systems, with cavity pressure of 2–3 Torr and Mach number of approximately 1.5, but also are high-throughput systems with a typical laser power per unit evacuation capacity of nearly 1 J/l, thus demanding high capacity vacuum systems which mainly determine the compactness of the system. These conventional nozzle-based systems usually require a minimum of a two-stage ejector system for realization of atmospheric pressure recovery in a SCOIL. Typically for a 500 W class SCOIL, a first stage requires a motive gas flow (air) of 120 gm/s to entrain a laser gas flow of 3 g/s and is capable of achieving the pressure recovery in the range of 60–80 Torr. On the other hand, the second stage ejector requires 4.5 kg/s of motive gas (air) to achieve atmospheric pressure recovery. An advanced nozzle, also known as ejector nozzle, suitable for a 500 W-class SCOIL employing an active medium flow of nearly 12 g/s, has been developed and used instead of a conventional slit nozzle. The nozzle has been tested in both cold as well as hot run conditions of SCOIL, achieving a typical cavity pressure of nearly 10 Torr, stagnation pressure of approximately 85 Torr and a cavity Mach number of 2.5. The present study details the gas dynamic aspects of this ejector nozzle and highlights its potential as a SCOIL pressure recovery device. This nozzle in conjunction with a diffuser is capable of achieving pressure recovery equivalent to a more cumbersome first stage of the pressure recovery system used in the case of a conventional slit nozzle-based system. Thus, use of this nozzle in place of a conventional slit nozzle can achieve atmospheric discharge using a single stage ejector system, thereby making the pressure recovery system quite compact.     

ALADIN热曲线的微正则系综分析

用微正则瞬时多碎裂统计模型分析了ALADIN热曲线.结果表明落在ALADIN热曲线温度平台(温度扭曲)附近的弹剩余核(热核)的理论代表点,并不落在相应弹剩余核热曲线的温度平台(扭曲)范围内,从而对ALADIN热曲线是否可作为核液气相变的证据提出质疑.     

Experimental study of the performance characteristics of a steam-ejector refrigeration system

Conventional compression-refrigeration systems not only consume a large amount of electric power, but also cause serious environmental pollution. Among the various possible approaches in overcoming these two problems, a steam-ejector refrigeration system is believed to be most effective. This paper experimentally investigates the controlling parameters of a steam ejector, including operating conditions and the exit Mach number of the primary nozzle. Operation maps useful to the practical design are constructed from experimental results, and the empirical equations are correspondingly derived. Excessively increasing the exit Mach number of primary nozzle is unnecessary, and 4.35 should be a moderate value. With regard to the performance characteristics of the ejector itself, a steam ejector is better than an R114 ejector and is comparable to an R113 ejector. Moreover, with the use of a two-stage ejector, the required pressure to drive a steam ejector is reduced, and the low-grade heat source can be efficiently used. The results of primitive observation of the flow field are also discussed in this work.     

Global classical solution for a three-dimensional viscous liquid-gas two-fluid flow model with vacuum

This is a continuation of the paper （J. Math. Phys., 52（2011）, 093102）. We consider the Cauchy problem to the three-dimensional viscous liquid-gas two-fluid flow model. The global existence of classical solution is proved, where the initial vacuum is allowed.     

引射式加热器替代低压回热系统等效焓降分析

火电机组低压回热系统中的面式加热器普遍存在较大损。应用等效焓降方法,深入分析采用引射式加热器替代面式低压加热器下机组热经济性的变化,并得到各个变化因素的数学计算式。在此基础上,对N600-165/535/535型机组低压回热系统进行实例计算,并与常规热平衡法计算进行了比较,结果表明：引射式加热器替代面式低压加热器,可以有效减小损,替代全部四级面式低压加热器,可使机组经济性提升最大,达0.263%;文中分析推导得出的计算表达式可用于机组热经济性分析计算。     

不同进料方式下气液喷射器内流体流动和混合特征

利用Fluent模拟了喷射器内气液两相在不同进料方式下（气体进口中心线与液体进口中心线偏移量不同）的流体力学和混合特征。其中A方式偏移2.5 mm;B方式偏移0 mm;C方式偏移4.0 mm,此时气体与液体完全相切进料。结果表明：在相同的喷嘴速度时,A方式下喷射器压力降与空气卷吸量最大,C方式下气体和液体的碰撞机会少于其他进料方式,压力和空气卷吸量最小,B方式下喷射器压力降与空气卷吸量居中;而混合效果随着偏移量由大到小（C、B、A）依次增强,但是增强效果不很明显。同时,还以C方式为例讨论了喷射器内喷嘴速度与压力降及空气卷吸量的关系,两者都随着喷嘴速度的增大而增大,且喷射器的压力降与空气卷吸量呈显著的线性相关,相关系数高达0.984。根据模拟结果分析,当3种进料方式压力降相同时,C方式气体卷吸量最大,即相同喷射性能时C方式的能量损失最小。