This thesis focuses on the issue of glare during helicopter night navigation, which is caused by the high reflectivity of cockpit instruments, displays, and windshield surfaces. This can result in pilot eye fatigue and pose a serious threat to flight safety. To address this problem, a bionic moth eye antireflection structure is designed and prepared on the windshield glass surface using a combination of self-assembly and reactive ion beam technology. The aim is to reduce the surface reflectivity of the windshield glass and prevent glare. The anti-reflective structure comprises of conical structures with a size cycle of 15 nm and a structure height of 2000 nm. The surface of both sides is microstructured, resulting in a reduction of surface reflectivity from 8% to 0.5% at the wavelength of 300 nm to 800 nm. The passing rate is increased from 92% to 99.5%, and the applicable angle is greater than 50°). The anti-glare ability is improved by about 16 times. This thesis proposes a solution to the problem of glare during helicopter night navigation by designing and implementing a bionic moth eye antireflection structure on the windshield glass surface using self-assembly and reactive ion beam technology. The results show a significant reduction in surface reflectivity and improved anti-glare ability, which can contribute to enhancing flight safety.
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