民机蒙皮激光除漆工艺机理与关键技术
批准号:
U2033211
项目类别:
联合基金项目
资助金额:
216.0 万元
负责人:
林学春
依托单位:
学科分类:
电子学与信息系统
结题年份:
2024
批准年份:
2020
项目状态:
已结题
项目参与者:
林学春
中文摘要
我国民航运输发展迅猛,民机蒙皮除漆需求剧增,目前蒙皮除漆以人工打磨与化学褪漆为主,可控性差,环境污染严重,亟待绿色自动化除漆技术。激光除漆具有绿色、高精度、易自动化等优点,但民机蒙皮激光除漆仍面临以下技术瓶颈:脉冲激光难以同时满足除漆效率与光纤传输要求、多物理场交互作用、基材损伤与质量控制。项目围绕激光除漆瞬态烧蚀气化、热膨胀应力及等离子体冲击波耦合作用的关键科学问题,提出双脉冲模式激光控制技术,获得能够强化等离子体冲击效应,且光纤传输的脉冲激光;分层次建立高重频纳秒激光瞬态烧蚀气化微-细观模型、温度-应力-冲击载荷耦合作用下漆层响应宏-细观模型及基材热力响应宏观模型,揭示激光除漆多尺度物理机制;开展民机蒙皮激光除漆多目标工艺优化与质量评估研究,建立多输入参数与除漆质量对应关系。项目研究成果将发展激光除漆基础理论,解决民机蒙皮激光除漆亟待突破的工程难题,提升我国民航自主维修技术核心竞争力。
英文摘要
Civil aviation transportation developed rapidly and the demand of paint removal of civil aircraft skins increased sharply. At present, the paint removal of civil aircraft skins is mainly based on manual sanding and chemical method, which have poor controllability and pollute the environment seriously. Thus, the pollution-free and automated paint removal technology is urgently needed. Laser paint removal has the advantages of pollution-free, high precision, and easy to automate, however, the following technical bottlenecks during laser stripping of civil aircraft skin need to be solved: it is difficult for pulsed laser to meet the requirements of paint removal efficiency and optical fiber transmission at the same time, interaction between the multiple physical effects such as transient ablation, thermal expansion stress, plasma shock wave during laser paint removal process, and the micro-damage of substrates and quality controlling. This project focuses on the key issues of the coupling mechanism of transient ablation, thermal expansion stress and plasma shock wave during laser paint removal process, the theoretical model and controlling method of the dual pulse mode laser is proposed to obtain a dual-pulse laser beam that not only strengthening the plasma shock effect but also could be transmitted by optical fiber; a micro-meso model of high-frequency nanosecond laser transient ablation, a macro-meso response model of paint layer under the temperature-stress-impact load, and a macro thermal-mechanical response model of substrate are established by scale to reveal the multi-scale physical mechanism of laser paint removal; multi-objective parameter optimization and quality assessment of laser paint removal of civil aircraft skin are carried out to establish a corresponding relationship between multi-process parameters and paint removal quality. Research results of this project will develop the theory of laser paint removal, sovle the engineering problems of laser paint removal of civil aircraft skin, and enhance the core competitiveness of our civil aviation maintenance technology.
飞机蒙皮除漆以人工打磨与化学褪漆为主,可控性差,环境污染严重,亟待绿色自动化除漆技术。激光除漆具有绿色、高精度、易自动化等优点,但民机蒙皮激光除漆仍面临脉冲激光模式调控、多物理场交互作用、基材损伤与质量控制等关键问题。本项目提出了利用阶梯状的模拟信号控制衍射损耗分段降低以实现反转粒子数逐级释放的方法,完成了1036W@5kHz的双脉冲激光清洗机样机研制,在激光清洗和激光诱导击穿光谱实验中得到了应用验证。建立温度-应力-冲击载荷作用激光除漆耦合模型,模拟了激光除漆过程中的温度场和应力场,采用生死单元对激光烧蚀形貌进行了模拟,结合本构方程对激光单脉冲作用产生的应力分布进行了计算。建立了激光烧蚀聚合物漆层的动力学模型,模拟了激光能量的沉积、材料表面的凹陷以及高温热解气体羽流的生成过程,与实验相比,数值计算准确地反映了脉冲激光作用后环氧树脂的动力学行。搭建了激光除漆高速阴影成像系统,采集了不同激光功率、脉宽、重频条件下不同作用材料的瞬态阴影图像,结合扫描电镜和热重-红外联用等表征方法,明确激光除漆的机理为烧蚀、热应力以及热解气体羽流的反冲压力作用。基于无量纲分析方法,获得了碳纤维复合材料基材烧蚀热影响区的关键参量与烧蚀阈值预测模型,建立起热影响区尺寸和特征与工艺参数之间的定性和定量关系。研究了激光器脉宽-重频组合模式对激光除漆的影响,对比了不同激光参数组合条件下的除漆效果,实现激光除漆的工艺参数优化,对激光除漆质量及基材力学性能进行综合评价,并在飞机雷达罩除漆等领域开展应用验证。
基于LCB晶体的355nm高功率皮秒紫外激光特性研究
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批准号:51672263
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项目类别:面上项目
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资助金额:62.0万元
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批准年份:2016
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负责人:林学春
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依托单位:
国内基金
海外基金