一种可实现熔石英微透镜阵列CO2激光精密抛光的初始微结构临界尺寸设计方法

By establishing a simulation model of fused silica CO2 laser polishing, the initial microstructure parameters of the fused silica microlens array were determined, solving the problem of unclear surface morphology and microlens array shape control in the existing technology, and realizing efficient and precise microlens array processing.

CN116956775BActive Publication Date: 2026-07-17HARBIN INST OF TECH

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
HARBIN INST OF TECH
Filing Date
2023-07-28
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

In the existing technology, the formation mechanism of the surface morphology of fused silica CO2 laser polishing and the shape control mechanism of the microlens array are unclear. As a result, it may not be possible to obtain a target microlens array structure that meets the quality requirements by determining the structural parameters and laser parameters through trial and error, and the trial and error method is inefficient.

Method used

A simulation model of the initial microstructure of fused silica was established using CO2 laser melting and polishing based on thermodynamics and fluid mechanics theories. The relationship between the stable temperature of the fused silica surface and the laser power and laser radius was determined. By simulating the polishing process with different structural parameters, the critical size of the initial microstructure was determined to achieve the processing of high-quality microlens arrays.

Benefits of technology

It provides a clear range of initial microstructure parameters, avoiding the problems of large workload and low efficiency of trial and error methods, establishing the selection of laser parameters during CO2 laser polishing, improving processing efficiency and quality, and filling the gap in the control of surface morphology and microlens array shape in fused silica CO2 laser polishing.

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Abstract

本发明提供一种可实现熔石英微透镜阵列CO2激光精密抛光的初始微结构临界尺寸设计方法,属于光学加工领域。为解决对熔石英CO2激光抛光表面形貌的形成机制及微透镜阵列形状的控制机制不明确,试错法确定结构参数和激光参数可能无法获取满足质量要求的目标微透镜阵列结构,且试错有随机性、效率低问题。根据目标微透镜阵列设计初始微结构,基于热力学和流体力学原理建立初始微结构的仿真模型并建立温度场仿真,选择抛光半径和功率,再对不同结构参数的初始微结构抛光过程仿真,得到微透镜尺寸和形貌,最终确定初始微结构的临界尺寸。避免工艺参数试错法工作量大、效率低;为通过工艺过程中选择合适的激光参数及控制微透镜阵列形状提供了指导。
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