碳纖維復合材料防護門抗沖擊性能研究
[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 擄to 0 擄is the highest, and the optimum layer is [0 擄4 / 45 擄/ 0 擄4 / -45 擄/ 0 擄4 / 45 擄/ 0 擄4 / -45 擄] 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 擄, 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.
【學位授予單位】:武漢理工大學
【學位級別】:碩士
【學位授予年份】:2015
【分類號】:TB332
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