摘要
利用电子束蒸发法制备了单层HfO2膜,控制氧气流量从0 mL/min以步长5 mL/min递增至25 mL/min(标况下)。利用ZYGO干涉仪测量基片镀膜前后的面形变化,代入Stoney公式计算出残余应力,分析了不同氧压下残余应力的变化情况。随着氧压的增大,残余应力由张应力逐渐过渡到压应力,当氧压过大时,压应力减小。因此可以通过改变氧压来控制应力。应力的变化与薄膜的微观结构密切相关,分析了所有样品的X射线衍射图(XRD),发现均为非晶结构。利用Ansys建立基片-薄膜有限元模型,将应力作用下基片的形变与实验结果进行对比,验证所建立的模型,为分析HfO2/SiO2膜堆应力的匹配设计提供参考。
HfO2 films were prepared by electron beam evaporation on K9 glass. Oxygen flux was varied in the range of 0 mL/min to 25 mL/min by step of 5 mL/min （under standard condition）. The residual stress was measured by viewing the substrate deflection using ZYGO interferometer. The results show that, as the oxygen pressure increases, the residual stresses decrease gradually from tensile to compressive, and then increase. The changes may be due to the variation of the microstructure of the HfO2 films, which was inspected with X-ray diffraction（XRD）. The finite element software ansys was used to calculate the substrate deflection which was then compared with the measured data. The comparison proves that our model is right and it helps to conduct analyses on HfO2/SiO2 stack stresses.
出处
《强激光与粒子束》
EI
CAS
CSCD
北大核心
2008年第6期894-898,共5页
High Power Laser and Particle Beams
基金
国家高技术发展计划项目
关键词
电子束蒸发
HFO2薄膜
残余应力
氧分压
有限元分析
Electron beam evaporation
HfO2 thin film
Residual stress
Oxygen partial pressure
Finite element analysis
作者简介
张丽莎（1983-），女，硕士，从事高损伤阈值激光薄膜应力研究；hilarey@163．com．
