碳纤维复合材料防护门抗冲击性能研究
[Abstract]:The quality of protective engineering is of great significance to our national defense and civil air defense safety. As the core component of the protective engineering, the performance of the protective door directly affects the protection grade of the protective engineering. The impact resistance of the protective door is mainly described as the ability of the door to resist the explosion shock wave, and it is the key index to evaluate the performance of the protective door. Therefore, the impact resistance of the protective door is the focus of the study of the protection door. Conventional doors are divided into steel doors and reinforced concrete doors. Because of the need of material and resistance design, the conventional protective door is bulky, difficult to open and maintain, difficult to rush repair and construction, and inconvenient to transport and install. With the development of new weapon, it is imperative to study the new protective door. The ideal protective door material should have the characteristics of light, high strength, low cost and good technology. Carbon fiber composite has the above characteristics and has a wide prospect in the application of protective doors. In this paper, the structure design and performance evaluation of the carbon fiber composite protective door are carried out, and the design of the coating parameters of the carbon fiber composite is studied. Based on the theory of explosion shock wave propagation, the response characteristics of laminated plates under the condition of clamping around are analyzed, and the evaluation indexes of carbon fiber composite protective doors are proposed. Carbon fiber composite protective door is a new type of protective door with carbon fiber composite material characteristics and meets the requirements of the application of the door. Combined with the evaluation index of the conventional protection door and the evaluation index of the carbon fiber composite material, the evaluation index of the carbon fiber composite protection door is determined, that is, the failure principle of the initial layer of the carbon fiber composite is adopted, and the maximum stress criterion is taken as the benchmark. Combined with the mid-span displacement value of the carbon fiber composite protection door, it can be used as the evaluation index of the impact resistance of the carbon fiber composite protection door. Firstly, the damping characteristics of carbon fiber composites are measured, and the Rayleigh damping coefficients of carbon fiber composite protective panels under given structure and layer conditions are obtained, in which the Rayleigh damping coefficient-6? According to the operating condition of the protective door, the blast shock wave load model of the protective door is established in the LS-DYNA software, and the dynamic load of the protective door is analyzed under the given conditions. The load is triangular, the action time is 11 Ms, and the peak value is 2.5 脳 105 Pa. According to the Rayleigh damping coefficient and the dynamic load of the protective door, the influence of the coating parameters on the carbon fiber composite protective plate is analyzed. The results show that, based on the criterion of maximum stress, the impact performance of the protective door layer of carbon fiber composite is good when the ratio of 0 掳to 0 掳is the highest, and the optimum layer is [0 掳4 / 45 掳/ 0 掳4 / -45 掳/ 0 掳4 / 45 掳/ 0 掳4 / -45 掳] s; In this paper, the structure of carbon fiber composite protective door is designed and analyzed. The analysis shows that: 1) when the arc of the protective plate is 0 掳, that is, the plate is the plate, the stress effect is the best, 2) when the thickness of the steel skin is 1 脳 10 3m, it can resist the impact of the shrapnel. 3) when the skeleton number is 18:00, the optimum weight and maximum stress are obtained. According to the given explosion load, the failure of the protective door under the load is analyzed in this paper. Under the equivalent static load of 3 脳 105Pa, the maximum stress and displacement of the carbon fiber composite protective door are 2.14 脳 10 ~ 8 Pa and 7.488 脳 10 ~ 3 m respectively. When the equivalent static load is 3 脳 10 ~ (9) Pa, the maximum stress is 2 脳 10 ~ (9) Paa and the maximum displacement is 5.222 脳 10 ~ (2) m. The corresponding dynamic load resistance energy is 2.5 脳 106 Pa. that is, the resistance of the CFRP protective door is 2.5 脳 106 Pa. it can meet the requirements of protection.
【学位授予单位】:武汉理工大学
【学位级别】:硕士
【学位授予年份】:2015
【分类号】:TB332
【参考文献】
相关期刊论文 前10条
1 张建国;岳金;宋春生;张锦光;;碳纤维复合材料螺旋桨铺层角度研究[J];武汉理工大学学报(信息与管理工程版);2014年02期
2 王亚生;王宏伟;李智斌;李鹏;;钢管混凝土在爆炸冲击荷载作用的研究现状[J];华南地震;2014年S1期
3 王瑞斌;马婷;王丽;王敏;朱玉华;;人防工程防护门专利概况[J];建筑结构;2013年S2期
4 宋浦;杨凯;梁安定;沈飞;王辉;;国内外TNT炸药的JWL状态方程及其能量释放差异分析[J];火炸药学报;2013年02期
5 倪小军;沈兆武;杨昌德;;泡沫铝壳对水下爆炸冲击波衰减的影响[J];含能材料;2011年03期
6 史梅;;结构加固工程的质量监督控制[J];经营管理者;2009年10期
7 朱江辉;王志华;王富生;王安强;岳珠峰;;冲击载荷作用下泡沫铝材料模型的参数研究[J];强度与环境;2008年05期
8 方秦;谷波;张亚栋;;钢结构防护门结构优化的数值分析[J];解放军理工大学学报(自然科学版);2006年06期
9 王宝来;吴世平;梁军;;复合材料失效及其强度理论[J];失效分析与预防;2006年02期
10 王志华;曹晓卿;马宏伟;赵隆茂;杨桂通;;泡沫铝合金动态力学性能实验研究[J];爆炸与冲击;2006年01期
相关博士学位论文 前1条
1 孔祥韶;爆炸载荷及复合多层防护结构响应特性研究[D];武汉理工大学;2013年
相关硕士学位论文 前4条
1 洪宝剑;碳纤维复合材料传动轴的设计研究[D];武汉理工大学;2012年
2 王t@;典型结构内部爆炸波的传播规律与超压荷载模型[D];天津大学;2008年
3 李家文;爆炸冲击波作用下结构瞬态响应分析[D];国防科学技术大学;2006年
4 张铁军;板壳结构在爆炸载荷作用下的破坏分析[D];哈尔滨工程大学;2005年
,本文编号:2424959
本文链接:https://www.wllwen.com/kejilunwen/cailiaohuaxuelunwen/2424959.html