GLARE层压板力学性能试验研究
Experimental Study on Mechanical Properties of GLARE Composite Laminates
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。
Abstract:
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.
参考文献
|
[1]
|
Vlot, A., Vogelesang, L.B. and de Vries, T.J. (1999) Towards Application of Fibre Metal Laminates in Large Aircraft. Aircraft Engineering and Aerospace Technology, 71, 558-570. [Google Scholar] [CrossRef]
|
|
[2]
|
Segall, M.D., Lindan, P.J.D., Probert, M.J., et al. (2002) First-Principles Simulation: Ideas, Illustrations and the CASTEP Code. Journal of physics: Condensed Matter, 14, 2417. [Google Scholar] [CrossRef]
|
|
[3]
|
Wu, G.C. and Yang, J.M. (2005) The Mechanical Behaviour of GLARE Aminates for Aircraft Structures. Jonrnal of the Minerals. Metals and Materials, 57, 72-73. [Google Scholar] [CrossRef]
|
|
[4]
|
Volt, A. (1996) Impact Loading on Fibre Metal Laminates. In-ternational Journal of Impact Engineering, 18, 291-307. [Google Scholar] [CrossRef]
|
|
[5]
|
Frizzell, R.M., McCarthy, C.T. and McCarthy, M.A. (2008) An Experimental Investigation into the Progression of Damage in Pin-Loaded Fibre Metal Laminates. Composites Part B: Engineering, 39, 907-925. [Google Scholar] [CrossRef]
|
|
[6]
|
沈真. 国外复合材料试验标准汇编[M]. 西安: 中国飞机强度研究所, 2011.
|
|
[7]
|
白光辉. 先进复合材料力学性能测试标准图解[M]. 北京: 化学工业出版社, 2015.
|
|
[8]
|
Volt, A., Vogelesang, L.B. and de Vries, T.J. (1999) Towards Application of Fiber Metal Laminates in Larger Aircraft. Aircraft Eng. & Aerospace Technol., 71, 558-570. [Google Scholar] [CrossRef]
|
|
[9]
|
Castro, M.R.S., Nogueira, J.C., Thim, G.P., et al. (2004) Ad-hesion and Corrosion Studies of a Lithium Based Conversion Coating Film on the 2024 Aluninum Alloy. Thin Solid Films, 457, 307-312. [Google Scholar] [CrossRef]
|