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Solid-state laser ablation effect on laser-proof composite coating applied in aerospace material

机译:固态激光烧蚀对航空航天材料应用的耐激光复合涂层的影响

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This paper concentrates on the measurement and analysis of laser ablation effect of particularly prepared aerospace material, polycarbosilane (PCS). Laser ablation experiment setup is designed and built, based on a continuous-wave high-power solid-state laser (CWHPSSL). Steel samples with composite PCS coating are prepared. After that, a group of laser ablation experiment is performed. The samples are shot by laser beam with thousands W/cm~2 fluence. The results, including the ablation morphology and temperature data, is shown and discussed. Temperature data gives a good demonstration of thermal protection effect of composite coating, and in the meanwhile the morphological features in the ablated region reveal the principle of PCS laser-proof effect. Theoretical investigation has also been carried out. The temperature field is simulated based on Fourier equation of heat conduction, and the simulation result provides a good demonstration on thermal-proof effect of PCS coating layer during laser ablation process.
机译:本文着重于特别制备的航空航天材料聚碳硅烷(PCS)的激光烧蚀效果的测量和分析。基于连续波高功率固态激光器(CWHPSSL),设计并构建了激光烧蚀实验装置。准备了具有复合PCS涂层的钢样品。之后,进行一组激光烧蚀实验。样品由具有数千个W / cm〜2通量的激光束拍摄。显示并讨论了包括烧蚀形态和温度数据在内的结果。温度数据很好地证明了复合涂层的热防护效果,同时在烧蚀区域的形貌特征揭示了PCS防激光作用的原理。理论研究也已经进行。利用傅里叶热传导方程对温度场进行了仿真,仿真结果很好地证明了PCS涂层在激光烧蚀过程中的隔热效果。

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