Analysis of a moderate resolution Fourier transform imaging spectrometer

A moderate resolution Fourier transform imaging spectrometer based on a modified Michelson interferometer is presented. The moving part of the interferometer is a moving wedged prism (MWP) instead of a moving mirror. The principle of the interferometer is described and the optical path difference as a function of the displacement of the MWP is calculated. Theoretical calculation and analysis are presented for the two moveable directions (hypotenuse and right angle side) of the MWP. The modified Michelson interferometer is not so sensitive to the non-uniform variation of moving speed and the environmental vibrations compared with the conventional Michelson interferometer. It is compact and has a large numerical aperture. The interferometer facilitated by CCD camera and the accompanying digital hardware and software are becoming the imaging spectrometer with moderate resolution is applicable in ultraviolet-infrared region.     

基于洛伦兹线型极光的上层大气风场探测模式研究

从洛伦兹线型极光的干涉强度、调制度与光程差的理论公式出发,用λ/4的步进光程差即“四强度法”获得一个波长范围内的4个干涉强度值,以实现基于洛伦兹线型极光的上层大气的风速、温度、压强等物理量的探测。提出用改形萨尼亚克成像干涉仪替代迈克耳孙干涉仪实现上层大气风场,给出了基准光程差的公式,并用四面角锥棱镜镀膜技术获得4个干涉强度值来同时探测上层大气风场的模式。最后在实验室将Kr灯557.0nm调整光束到一定宽度,对称地从顶角为60°的两面镀膜角锥棱镜的顶点入射,用768pixel×576pixel的CCD照相机接收到两个光斑的成像,这两个光斑的再复制就得到镀膜四面角锥棱镜在一个周期内的4个干涉强度光斑,从而获得上层大气风场。     

折返式激光二极管侧抽运Nd:YAG激光器

提出一种明显改善激光二极管侧面直接抽运固体激光器输出光束质量的新型谐振腔——折返式谐振腔,它由三部分组成：直角棱镜、全反的腔镜以及耦合输出腔镜,采用振荡光顺次通过晶体内增益场强区的工作方式。它重叠利用不均匀增益场的对称强区,提高了晶体增益场和谐振腔基模的重叠度,达到改善器件输出光束质量和提高效率的目的。通过对受抽运晶体内的增益场分布及腔内振荡光的模拟分析以及实验测试,验证了这种谐振腔的优势。在此基础上,研制了采用准连续线阵列激光二极管抽运Nd：YAG的折返式激光器。研究比较了在不同类型谐振腔下,激光器的输出特性。例如：平-平直腔和平-平折返腔在耦合透过率为50％时的输出特性,其增益场和基模的重叠度由24％提高到53％,光-光斜效率由的20．2％提高到27．3％。     

五角棱镜制造角差及抖动对其转向角的影响

从五角棱镜的原理和特性出发,分析了在理想条件下五角棱镜的转向角不受入射角的影响,详细讨论由于五角棱镜加工角差和相对入射光束抖动对其转向角的影响,给出了相应的精确表达式。其中对于入射光在垂直于入射面抖动的情况,由于不能简单从二维几何光学关系分析,而采用了矢量分析方法,得出:当角差δβ=δθ时,入射角抖动对转向角偏差的影响可以忽略,而转向角偏差与制造角差几乎成线性关系。为五角棱镜用于计量测试误差分析提供了理论依据。结论对五角棱镜的制造也有很大理论指导的意义。     

The effect of a splitter plate on the flow around a finite prism

The effect of a wake-mounted splitter plate on the flow around a surface-mounted finite-height square prism was investigated experimentally in a low-speed wind tunnel. Measurements of the mean drag force and vortex shedding frequency were made at Re=7.4×10⁴ for square prisms of aspect ratios AR=9, 7, 5 and 3. Measurements of the mean wake velocity field were made with a seven-hole pressure probe at Re=3.7×10⁴ for square prisms of AR=9 and 5. The relative thickness of the boundary layer on the ground plane was δ/D=1.5–1.6 (where D is the side length of the prism). The splitter plates were mounted vertically from the ground plane on the wake centreline, with a negligible gap between the leading edge of the plate and rear of the prism. The splitter plate heights were always the same as the heights of prisms, while the splitter plate lengths ranged from L/D=1 to 7. Compared to previously published results for an “infinite” square prism, a splitter plate is less effective at drag reduction, but more effective at vortex shedding suppression, when used with a finite-height square prism. Significant reduction in drag was realized only for short prisms (of AR≤5) when long splitter plates (of L/D≥5) were used. In contrast, a splitter plate of length L/D=3 was sufficient to suppress vortex shedding for all aspect ratios tested. Compared to previous results for finite-height circular cylinders, finite-height square prisms typically need longer splitter plates for vortex shedding suppression. The effect of the splitter plate on the mean wake was to narrow the wake width close to the ground plane, stretch and weaken the streamwise vortex structures, and increase the lateral entrainment of ambient fluid towards the wake centreline. The splitter plate has little effect on the mean downwash. Long splitter plates resulted in the formation of additional streamwise vortex structures in the upper part of the wake.     

立方棱镜二向色分光膜消倍频反射峰的设计

立方棱镜二向色分光镜是实现多光谱共光路的重要器件.立方棱镜二向色分光镜因偏振效应而在高级次倍频处出现高反射峰,严重影响了短波区的透过率.利用虚设层概念,设计出了400 nm～900 nm波段高透过、1 064 nm激光波段高反射的立方棱镜二向色分光镜.给出了消除倍频反射峰的有效方法,并成功制作出光学性能优良的样品.采用这种设计方法获得的膜系结构简单,膜层数量少,材料选择广泛,对工艺要求简单,便于工艺实现,可重复性好.     

关于测量三棱镜顶角的两种方法比较

通过对自准法和平行光法测量三棱镜顶角的实验调节过程进行比较,对这两种方法测量的数据结果进行对比分析,得出实验中使用自准法测量顶角是一种测量精度和测量方法都更实用的方法。     

温差条件下组合色散棱镜支撑结构的实验分析

介绍了超光谱成像仪采用的组合色散棱镜的支撑结构形式,讨论了温度变化对成像的影响。根据使用需求选择了支撑座的材料,模拟了5～10℃温差条件下棱镜组件的变形情况。利用有限元法解决材料线膨胀系数不同所引起的棱镜反射面变形,并分析了采用聚四氟乙烯垫片做温度补偿后垫片的厚度及接触面积对石英棱镜面型的影响。实验结果表明,在支撑座和棱镜之间增加聚四氟乙烯垫片后,石英棱镜的面型达到了λ/6的指标要求。本文提出的优化方法为组合色散棱镜支撑结构的设计提供了参考依据。     

旋转双光楔折射特性与二维扫描轨迹的分析

 为实现旋转双光楔二维扫描的可控操作,利用几何光学和光的标量衍射理论,对双光楔的折光特性进行了数学分析。研究发现：绕固定轴以不同角速度旋转的双光楔可等效为一个折射棱角和主截面都变化的单光楔。以该双光楔系统作为衍射屏,对通过双光楔的光束在观察面的衍射光场分布作了理论分析,得到了夫琅和费衍射下,光束经转动双光楔在像平面上的衍射光斑随转角变化的规律：光斑的横坐标与两光楔转角正弦值的差成正比,纵坐标与两光楔转角余弦值的和成正比。     

可见光波段及1064nm波长处用于Glan-Taylor棱镜减反射膜

为了提高Glan-Taylor棱镜的透射率,研究了Glan-Taylor棱镜在可见光波段及1064nm波长处减反射膜膜的设计和制备．为提高薄膜和冰洲石晶体的附着力,采用沉积Al2O3为过渡层,ZrO2作缓冲层的方法,用单纯形优化的方法进行膜系优化设计．用电子束沉积和离子柬辅助沉积的方法制备了多层减反射膜,并采用石英晶体振荡法监控膜厚和沉积速率．测量结果表明,在可见光波段及1064nm波长处的剩余反射率均小于0．5％经测试薄膜与冰洲石晶体的附着力性能良好．