用原子力显微镜4π旋转技术测量靶丸表面粗糙度

原子力显微镜靶丸4π旋转装置,可以将靶丸在夹持状态下实现4π方向旋转,便于原子力显微镜对靶丸表面任一部分做扫描测量。应用该装置对各种靶丸的表面形貌进行了测量,测量结果表明,靶丸外表面粗糙度小于10nm,内表面粗糙度小于20nm。     

氧碘化学激光器中混合现象的数值模拟

给出了基于气体动力学、化学动力学和激光物理学的氧碘化学激光器理论模型,并对氧碘化学激光器中的混合现象进行了三维数值模拟,所得结果与文献上类似模拟结果一致。     

射流式单重态氧发生器的工作稳定性实验

 实验研究了BHP的化学稳定性以及射流式SOG稳定工作的判据,为射流式SOG的研究提供了实验依据。通过理论研究和实验数据的综合分析,给出了单排孔进气结构射流式单重态氧发生器稳定工作的判据vg/vj≤2。提高射流式SOG的BHP驱动压力,以提高射流的速度是提高Cl₂摩尔流量也即单重态氧发生量的有效手段。     

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.     

无缓冲气COIL扩压器流场数值模拟

 以无缓冲气化学氧碘激光器(COIL)实验器件的数据计算得到的混合喷管出口参数平均值作为光腔入口条件,对6种不同构型的扩压器从光腔入口至扩压器出口的流场进行了数值模拟,得出了各流场参数分布;对不同构型扩压器的流场特点、总压恢复性能进行了分析;研究了扩压器出口背压对流场参数的影响。结果表明：对于主流无缓冲气的COIL,等截面扩压器具有较好的压力恢复性能;增大扩压器出口背压可以使扩压器的压力恢复性能提高,然而,较高的背压使激波串向光腔方向移动,从而使光腔流场受到干扰,影响光腔的光束质量。     

COIL腔镜薄膜参数实验研究

 利用HITACHI U-4001型分光光度计和基于光腔衰荡光谱的高反射率测量仪对氧碘化学激光器（COIL）输出镜的透过率和高反镜的反射率进行了膜层均匀性、测量重复性、激光辐照等方面的测量和实验研究。实验结果显示：离子束溅射膜的性能比电子枪蒸发膜更为稳定;只要保证镜片存放于干燥处,长时间放置对其薄膜的透过率和反射率均无明显影响。     

氧碘化学激光器增益谱线的实验研究

 利用可调谐二极管激光器为探测光源, 直接测量了氧碘化学激光器的增益谱线的精细结构及其各谱线所占比例。同时用碘原子吸收池标定了六条谱线。     

氧碘激光器小信号增益时空分布的实验研究

 首次利用一台亚音速小型连续波化学氧碘激光器做探测光源，用放大法直接测量超音速化学氧碘激光器的小信号增益系数，测得了小信号增益系数随时间和气流方向的变化。     

短波长化学激光系统反射镜研制

 报道了短波长化学激光系统高反射镜的膜系设计、镀膜材料的选取、反射膜制备技术、基板加工、反射镜性能测试和各种膜系反射镜在强激光辐照下的热畸变和损伤。     

JSOG中水蒸汽含量的模拟计算

 氧碘化学激光（简称 COIL）系统中，水是影响激光功率输出的最重要的原因之一。气流中的水不仅对激发态碘原子有严重的猝灭作用，另外对碘分子解离、超音速流动特性也有很坏的负面作用。单重态氧发生器的BHP（Basic Hydrogen Peroxide ）溶液是最主要的水蒸汽源。利用传质模型对射流式单重态氧发生器（简称JSOG）中产生的水蒸汽进行了计算，所得的数值结果与实验测量结果基本相符。根据模拟结果，对发生器的设计及实验条件进行了优化。