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玻璃钢-聚氨酯泡沫夹层板弯曲失效研究
引用本文:张雁,杨树兴,魏传锋. 玻璃钢-聚氨酯泡沫夹层板弯曲失效研究[J]. 航天器环境工程, 2014, 31(6): 614-619
作者姓名:张雁  杨树兴  魏传锋
作者单位:1. 北京理工大学 宇航学院,北京100081; 中国空间技术研究院 钱学森空间技术实验室,北京 100094
2. 北京理工大学 宇航学院,北京,100081
3. 中国空间技术研究院 载人航天总体部,北京,100094
基金项目:国家自然科学基金项目(编号:51105034)
摘    要:采用真空灌注方法研制了玻璃纤维-聚氨酯泡沫夹层板,通过理论推导、数值仿真及试验验证对该夹层板的弯曲失效特性进行了研究,得到了实际失效载荷以及两种失效模式。研究表明,玻璃纤维-聚氨酯泡沫夹层板的载荷变形曲线中会出现2处拐点:第一拐点对应第一失效模式,其表征为表层玻璃纤维被拉伸断裂;第二拐点对应第二失效模式,其表征为芯体泡沫被剪切开裂。

关 键 词:复合材料  夹层板  失效机理  弯曲试验
收稿时间:2014-06-11
修稿时间:2014-11-02

The bending failure of fiberglass-polyurethane foam sandwich panel
Zhang Yan,Yang Shuxing,Wei Chuanfeng. The bending failure of fiberglass-polyurethane foam sandwich panel[J]. Spacecraft Environment Engineering, 2014, 31(6): 614-619
Authors:Zhang Yan  Yang Shuxing  Wei Chuanfeng
Affiliation:1. School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China;2. Qian Xuesen Laboratory of Space Technology, China Academy of Space Technology, Beijing 100094, China;3. Institute of Manned Space System Engineering, China Academy of Space Technology, Beijing 100094, China
Abstract:In order to study the bending failure mechanism of composite sandwich panels, the fiberglass- polyurethane foam sandwich panel is designed and manufactured by vacuum infusion. A theoretical model for its failure is built and the bending test is carried out, as well as the numerical simulation. The failure load is obtained, and two failure modes are revealed during the bending process. An explanation of two inflexion points observed in the load-deflection curve of the glass fiber-polyurethane foam sandwich panel is made. It is concluded that the first inflexion point, corresponding to the first failure mode, is owing to the tensile splitting of the surface glass fiber, and the second one, corresponding to the second failure mode, is due to the shear force splitting of the middle foam.
Keywords:composite materials  sandwich panel  failure mechanism  bending test
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