海水环境中厚截面复合材料夹芯构件吸湿-力学特性及失效行为

Moisture absorption, mechanical property and failure behavior of thick-section composite sandwich structure in seawater environment

  • 摘要: 在海洋服役环境中,海水长期浸泡会导致复合材料的性能退化,从而对相关结构耐久性或安全性造成影响。本文针对代表性的船用厚截面复合材料夹芯构件,开展了其海水吸湿-力学行为试验和数值模拟。首先,制定了材料与结构同步的加速老化试验,探究了面板复合材料在海水浸泡过程中的吸湿特性与力学演变规律,并测定不同老化时间的构件弯曲强度,揭示厚截面夹芯构件受压弯载荷的破坏机制。其次,考虑夹芯复合材料各组分(面板、芯材、胶层)海水老化的差异性,建立能有效表征构件吸湿特性与力学响应的仿真模型,利用数值模拟方法获得海水环境中复合材料夹芯构件的吸湿浓度分布、应力/变形特征和损伤演化规律。仿真给出的不同老化时间构件的弯曲失效载荷、破坏形式与试验结果吻合良好,定量的分析结果表明:海水吸湿引起的胶层性能衰减显著降低了这类厚截面夹芯复合材料的弯曲承载能力,但未改变其核心失效模式,老化前、老化后的构件失效均是以面-芯胶层脱粘为主导因素。

     

    Abstract: Long-term seawater immersion degrades the mechanical performance of composite materials in marine service, which undermines the durability and safety of related structures. In this work, the moisture absorption and mechanical behavior of a typical ship composite sandwich structure with thick-section was investigated by experiments and simulations. First, the synchronous aging tests were designed for both composite material and sandwich structure. The evolution of moisture and mechanics characteristics of the panel composite during seawater immersion were quantified. The bending strength of this kind of thick-section structure at different aging days was measured, revealing its representative failure mechanism. Second, accounting for degradation diversity of sandwich components (panel, core and adhesive) under seawater aging, a finite element model was developed to characterize the moisture diffusion and mechanical response of the specimen. Moisture concentration, stress/deformation distribution and damage propagation were numerically analyzed. Overall, the bending failure loads and modes at different aging days captured from structural model simulation have good agreement with test results. Finally, quantitative comparison demonstrated that degradation of adhesive properties due to moisture absorption substantially reduced the bearing capacity of such sandwich structure for bending loads, but could not affect its crucial damage mode. Debonding at the adhesive layer between panel composite and core material remained the key factor for the failure of investigated specimen, both before and after aging.

     

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