GLARE层压板力学性能试验研究  

Experimental Study on Mechanical Properties of GLARE Composite Laminates

作　　者：杨梦粤 杨胜春[1] 

机构地区：[1]中国飞机强度研究所,陕西 西安

出　　处：《材料科学》2020年第10期824-832,共9页Material Sciences

摘　　要：新型纤维金属层板GLARE因其优异的静强度、抗疲劳和抗冲击等性能,已经广泛应用于飞机的机身蒙皮、水平尾翼和垂直尾翼前缘以及货舱地板。本文对国产GLARE层板力学性能进行试验研究,获得国产GLARE材料的基本力学性能及失效模式,并与国外GLARE层板力学性能进行对比。结果表明,国产GLARE性能优越,可以应用于我国飞机机身蒙皮、尾翼等部位。Due to its excellent static strength, fatigue resistance and impact resistance, glass has been widely used in fuselage skin, leading edge of horizontal and vertical tail and cargo floor. In this paper, the mechanical properties of domestic glare laminates were studied, and the basic mechanical prop-erties and failure modes of domestic glare laminates were obtained, and the mechanical properties of domestic glare laminates were compared with those of foreign glare laminates. The results show that the performance of domestic glare is superior, and it can be used in fuselage skin, tail wing and other parts of Chinese aircraft.

关 键 词：GLARE层板 新型混合体复合材料 基本力学性能 

分 类 号：V21[航空宇航科学与技术—航空宇航推进理论与工程]