LBO晶体上具有不同厚度过渡层的倍频增透膜的设计和制备

Design and preparation of frequency doubling antireflection coating with different thicknesses of interlayer were investigated for LiB₃O₅ (LBO) substrate. The design was based on the vector method. The thickness of the inserted SiO₂ interlayer could be changed in a wide range for the four-layer design with two zeros at 1064 and 532 nm. The coatings without any interlayer and with 0.1 quarter-wave (λ/4), 0.3 λ/4, 0.5 λ/4 SiO₂ interlayer were deposited respectively on LBO by using electron beam evaporation technique. All the prepared coatings with SiO₂ interlayer indicated satisfying optical behavior. This expanded our option for the thickness of an interlayer when coating on LBO substrate. The prepared films with SiO₂ interlayer showed better adhesion than that without any interlayer. The thickness of the interlayer affected the adhesion, the adhesion for the coating with 0.5 λ/4 SiO₂ interlayer was not as good as the other two.}

LBO晶体上1064，532nm倍频增透膜的镀制及性能分析

用电子束蒸发沉积方法在X切LBO（X-LBO）晶体上镀制了两种不同膜系结构的1064和532nm倍频增透膜，其中一种膜系结构为基底／ZrO2／Y2O3／A12O3／SiO2／空气，另一种为基底／0．5Al2O3／ZrO2／Y2O3／A12O3／SiO2／空气，两种膜系结构的主要差别在于有无氧化铝过渡层。测量了薄膜的反射率光谱曲线，发现两种增透膜在1064和532nm处的反射率均小于0．5％，实际镀制结果与理论设计曲线的差异主要是由材料折射率的变化引起的。且对样品在空气环境中进行了温度为473K的退火处理，

沉积温度对LaF3薄膜性能的影响

abstract {LaF₃ single-layer coatings were prepared by thermal boat evaporation at the deposition temperatures of 189, 255, 277 and 321°C respectively. The crystal structures of the coatings were characterized by X-ray diffraction (XRD). A spectrophotometer was employed to measure its transmittance. Moreover, refractive index, extinction coefficient and cut-off wavelength were obtained from the measured transmittance spectral curve. The residual stress was evaluated by the Stoney's equation and optical interferometer. Laser induce damage threshold (LIDT) was performed by a tripled Nd:YAG laser system. The results show that the crystallization status becomes better with the deposition temperature increasing. Correspondingly, the grain size also gets larger. Meanwhile, the coatings become more compact and the refractive index increases. However, the absorption of coatings seriously rises and the cut-off wavelength drifts to the long wave. In addition, the residual stress also increases and the intrinsic stress plays a determinant role in the coating. The LIDT of the coating also enhances at high temperature.}

渐变折射率薄膜的分层评价探讨

首先阐述了将渐变折射率薄膜细分为多层均匀薄膜的分层介质理论，接着给出了一种获得最佳分层数目的分层评价方法，最后以线性变化渐变折射率薄膜为例说明了如何优化获得渐变折射率薄膜的分层数目．研究发现：渐变折射率薄膜的分层数目与薄膜的厚度和薄膜的折射率变化快慢有关，在一定的折射率变化范围内，渐变折射率薄膜的分层数目随着薄膜厚度的增加先减小后增大．

真空室内金属杂质污染对光学薄膜性能的影响

真空室内金属粒子污染是降低激光薄膜性能的一个重要因素。采用高真空残余气体分析仪,对薄膜沉积过程中的气氛进行分析。发现由黄铜制作的加热灯架在工作时会分解出Zn,在这种条件下沉积薄膜,会使薄膜中掺入金属杂质,导致薄膜激光破坏阈值降低。采用表面分析技术对薄膜的组分进行分析,证实薄膜中锌杂质的存在。激光破坏实验证明,含有锌杂质的薄膜的破坏阈值明显降低。

沉积速率对热舟蒸发LaF3薄膜性能的影响

用热舟蒸发方法在不同的沉积速率下制备了LaF3单层膜,并对部分单层膜进行了真空退火。分别采用X射线衍射(XRD),Lambda 900 光谱仪和355 nm Nd∶YAG脉冲激光测试了薄膜的晶体结构、透射光谱和激光损伤阈值(LIDT),并通过透射光谱计算得到样品的折射率和消光系数。实验结果表明,增大沉积速率有利于LaF3薄膜的结晶和择优生长,可以提高薄膜的致密性和折射率,但薄膜的抗激光损伤能力有所下降;沉积速率太大,又会恶化薄膜的结晶性能,同时薄膜中产生大量孔洞,薄膜的机械强度降低,导致薄膜的折射率减小和

单脉冲飞秒脉冲激光对单层和高反光学薄膜的损伤

用电子柬蒸发的方法在BK7玻璃上制备了ZrO2单层膜和ZrO2／SiO2高反膜，利用掺Ti：sapphire飞秒激光系统输出的中心波长为800nm，脉宽为50fs的激光脉冲对这两种样品进行了激光损伤阈值测试．实验结果表明，ZrO2单层膜的阂值比ZrO2／SiO2高反膜的高；这与传统的纳秒脉冲激光的损伤情况相反．利用光离化和碰撞离化激发电子到导带，形成电子等离子体基本模型并对此现象进行了解释．同时，用显微镜对样品的损伤形貌进行了观测，对损伤的特点进行了表征．

低损耗193nm反射膜的设计

采用1/4规整膜系,从电场强度、吸收损耗及散射损耗的分布几个方面,对影响193 nm反射膜性能的因素进行了分析。以分析结果为基础,对低损耗193 nm反射膜的设计进行了探讨。结果表明:在空气侧的外膜层中电场强度较大,随着层数向内过渡,电场强度迅速减小;高折射率材料膜层的吸收损耗明显高于低折射率材料膜层的吸收损耗,而且靠近空气侧最外层的高折射率膜层的吸收损耗最大;按由外层向内层过渡的方向,吸收损耗迅速减小,减小的速度与高低折射率材料折射率的比值相关;表面散射损耗与两种材料的折射率比值成正比,但折射率比值减小后只能通过增加膜层数来获得一定的反射率,而这样又会使表面粗糙度增加,并且引入其它的损耗。因此,选择折射率差值适当大一些的材料对降低散射损耗是有利的。设计了27层膜堆的193 nm反射膜,设计反射率在98%以上。

Temperature fields of 355 nm HR coatings based on the interface absorption model

Temperature fields of 355 nm high-reflectance (HR) coatings were investigated based on the interface absorption model. It was found that the highest temperature in the HR coatings increased with an increase in the extinction coefficient of the interface A, B, C, Al2O3 and MgF2. The highest temperature of HR coatings that can be reached increased quickly with the increase in the extinction coefficient of interface A in particular. The temperature rises of 355 nm HR coatings at different layers and different deposition temperatures were investigated based on experiments also. The damage mechanism of 355 nm HR coatings was confirmed with temperature fields and the interface absorption model.

LiB3O5晶体上四倍频增透膜设计

采用矢量法设计了三硼酸锂（LiB3O5，LBO）晶体上1064nm、532nm、355nm和266nm四倍频增透膜．结果表明，在1064nm、532nm、355nm和266nm波长的剩余反射率分别为0．0019％、0．0031％、0．0061％和0．0047％．根据容差分析，薄膜制备时沉积速率准确度控制在＋6．5％时，基频、二倍频、三倍频和四倍频波长的剩余反射率分别增加至0．24％、0．92％、2．38％和4．37％．当薄膜材料折射率的变化控制在＋3％时，1064nm波长的剩余反射率增大为0．18％，532nm、355nm和266nm波长分别达0．61％，0．59％，0．20％．与薄膜物理厚度相比，膜层折射率对剩余反射率的影响大．对膜系敏感层的分析表明，在1064nm和266nm波长，从入射介质向基底过渡的第二层膜厚度变化对剩余反射率的影响最大，其次是第一膜层．在532nm和355nm波长，从入射介质向基底过渡的第一和第四膜层是该膜系的敏感层．误差分析也表明，薄膜材料的色散对特定波长的剩余反射率具有明显影响，即1064nm、532nm、355nm和266nm波长的剩余反射率分别增加至0．30％、0．23％、0．58％和3．13％．

引入过渡层提高介质减反膜的抗激光损伤阈值

提出了一种用于提高介质减反膜的损伤阈值的新的方法，在H2.5L (H:HfO2, L:SiO2)的膜层与基底之间引入4个1/4光学厚度的SiO2薄膜，发现抗激光损伤阈值提高了50%，并且保持1064nm处的反射率低于0.09%。本文分析了造成这一提高的机制，一定厚度的氧化硅过渡层的引入是一种提高介质减反膜的损伤阈值的灵活有效的方法。

三种不同后处理方式对ZrO_2薄膜性能的影响

采用有氧热处理、激光预处理和离子后处理三种方式对电子束蒸发(EBE)制备的单层ZrO_2薄膜进行了后处理,并分别对样品的光学性能和抗激光损伤阈值(LIDT)特性进行了研究。实验结果表明,热处理方式可以有效排除膜层内吸附的水气,弥补薄膜制备过程中的氧损失,使得光谱短移、吸收减小、损伤阈值增高;激光预处理过程可以在一定程度上减少缺陷、提高损伤阈值,但对膜层的光谱和吸收情况没有明显的改善作用;而离子后处理能够提高膜层的堆积密度、减少缺陷、降低吸收从而提高损伤阈值。由于三种方式处理机制不同,在实际应用中应根据膜层的性能选择合适的处理方式。

Influence of ZrO2 in HfO2 on reflectance of HfO2/SiO2 multilayer at 248 nm prepared by electron-beam evaporation

Influence of ZrO2 in HfO2 on the reflectance of HfO2/SiO2 multilayer at 248 nm was investigated. Two kinds of HfO2 with different ZrO2 content were chosen as high refractive index material and the same kind of SiO2 as low refractive index material to prepare the mirrors by electron-beam evaporation. The impurities in two kinds of HfO2 starting coating materials and in their corresponding single layer thin films were determined through glow discharge mass spectrum (GDMS) technology and secondary ion mass spectrometry (SIMS) equipment, respectively. It showed that between the two kinds of HfO2, either the bulk materials or their corresponding films, the difference of ZrO2 was much larger than that of the other impurities such as Ti and Fe. It is the Zr element that affects the property of thin films. Both in theoretical and in experimental, the mirror prepared with the HfO2 starting material containing more Zr content has a lower reflectance. Because the extinction coefficient of zirconia is relatively high in UV region, it can be treated as one kind of absorbing defects to influence the optical property of the mirrors. (C) 2008 Elsevier B.V. All rights reserved.

Influence of oxygen post-treatment on laser-induced damage of antireflection coatings prepared by electron-beam evaporation and ion beam assisted deposition

Antireflection coatings at the center wavelength of 1053 nm were prepared on BK7 glasses by electron-beam evaporation deposition (EBD) and ion beam assisted deposition (IBAD). Parts of the two kinds of samples were post-treated with oxygen plasma at the environment temperature after deposition. Absorption at 1064 nm was characterized based on surface thermal lensing (STL) technique. The laser-induced damage threshold (LIDT) was measured by a 1064-nm Nd:YAG laser with a pulse width of 38 ps. Leica-DMRXE Microscope was applied to gain damage morphologies of samples. The results revealed that oxygen post-treatment could lower the absorption and increase the damage thresholds for both kinds of as-grown samples. However, the improving effects are not the same. (c) 2008 Elsevier B.V. All rights reserved.

Thermal-mechanical modeling of nodular defect embedded within multilayer coatings

The initiation of laser damage within optical coatings can be better understood by thermal-mechanical modeling of coating defects. The result of this modeling shows that a high-temperature rise and thermal stress can be seen just inside the nodular defect compared to surrounding coating layers. The temperature rise and thermal stress tend to increase with seed diameter. Shallower seed tend to cause higher temperature rise and greater thermal stress. There is a critical seed depth at which thermal stress is largest. The composition of the seed resulting from different coating-material emission during evaporation can affect the temperature rise and thermal stress distribution.