K-cor夹层结构湿热环境力学性能及其影响研究
[Abstract]:K-cor structure is a new type of high performance sandwich structure strengthened by Z-pin technology, which better satisfies the requirements of aerospace lightweight and high strength. At present, there are few reports at home and abroad on the influence of wet-heat environment of K-cor structure in engineering application. In this paper, the mechanical properties of K-cor structure under wet-heat, low-speed impact and low-speed impact are studied, and the strengthening mechanism, damage mechanism and failure mode of Z-pin structure are studied. In order to design K-cor sandwich structure with excellent comprehensive performance. The effect of Z-pin implantation and overlay angle on the hygroscopicity of K-cor structure was studied. The results showed that Z-pin implantation did not affect the hygroscopicity of K-cor structure, but increased the interfacial bonding strength and dimensional stability of the structure. In the case of large water vapor concentration, the smaller the change of the laminate angle is, the lower the moisture absorption and weight gain rate of the structure is. Three-point bending and compression tests were used to study the changes of mechanical properties of K-cor core after hot and humid conditions. The results showed that the increase of Z-pin implant density could significantly increase the three-point bending strength and compressive strength of samples before and after wet-heat treatment. The three-point bending strength of the K-cor sandwich structure with Z-pin density of 12mm 脳 12mm is 11.1% higher than that of the blank sample without wet heat treatment. The compressive strength of 8mm 脳 8mm K-cor wet-heat treated specimen is 17.5% higher than that of non-wet-heat treated blank sandwich structure, which shows the excellent hygrothermal resistance of K-cor sandwich structure. The reduction of Z-pin implantation angle can obviously improve the compressive strength of the samples before and after wet-heat treatment. The compressive strength of the core of the K-cor samples implanted in 0 掳after wet-heat treatment is basically the same as that of the K-cor samples implanted in 40 掳without wet-heat treatment. However, the implantation angle has little effect on the three-point bending strength. The low-speed impact test of K-cor sandwich structure was carried out by means of drop hammer impact, and the impact resistance of K-cor structure was studied by means of infrared nondestructive test and residual compressive strength (CAI) test. The results show that the thicker the core of K-cor sandwich structure is, the larger the impact damage area is, but the higher the retention rate of residual strength is. With the increase of bending length of Z-pin, the damage area of K-cor structure after impact can be significantly reduced and the residual compressive strength can be improved by increasing the bending length without exceeding the distance between implants. Under the condition of the same core density, increasing the bending length of Z-pin is more beneficial to reduce the damage area of K-cor specimen after impact than to increase the implant density, and improve the residual compressive strength and the strength retention rate of the sample. In addition, the impact damage of the K-cor structure caused by the drop hammer with the punch parameter of 10mm/1.28Kg is more serious than that of the drop hammer with the punch parameter of 12.5mm/2Kg. Considering the influence of wet-heat environment and low-speed impact on the performance of K-cor structure, the falling hammer impact of K-cor structure after wet-heat treatment is designed, and the damage area, damage depth and CAI are measured. The results show that the increase of Z-pin implant density effectively reduces the negative effect of wet-heat environment on the impact damage area and damage depth of K-cor sandwich structures. The residual strength caused by the change of failure mechanism under lateral pressure mode is alleviated and the impact resistance of K-cor structure is more stable.
【学位授予单位】:南京航空航天大学
【学位级别】:硕士
【学位授予年份】:2016
【分类号】:TB383.4
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