含泡沫铝芯的复合板弯曲疲劳行为的研究

应用表面位移原位分析技术对由泡沫金属铝芯和金属面板组成的三层复合板在循环弯曲载荷条件下的损伤行为进行了观察和研究。循环弯曲载荷条件下复合板失效的基本方式是表面凹陷（Indentation，ID）和泡沫铝内芯切断（Coreshear，CS）。凹陷型失效是与加载压头接触的复合板表面局部压缩密切相关，该处沿垂直方向的压缩应变最大。内芯切断型失效是泡沫铝内芯中切应变最大的区域发生的剪切破坏。在疲劳应力比R=0时，复合板凹陷型失效的疲劳极限高于内芯切断型失效的疲劳极限。     

Bending Response of Foldcore Composite Sandwich Beams

In order to solve bending behavior difference of corrugated structure in L andWorientation, bending response for composite sandwich beams with foldcores of three different wall thicknesses were experimentally and numerically investigated. Effect of the cell walls thickness on the strength and failure behavior of the composite sandwich beams with L and W orientations was also examined. The deformation mode was obtained by the numerical method; a constitutive law of laminated material has been incorporated into a finite element (FE) analysis program. Numerical calculations give accurate prediction to the bending response of foldcore composite sandwich beams comparing with experiments. Structural flexural stiffness, strength and failure mechanism at a given topological geometry depended on the nature of core itself: the bending stiffness and strength of the sandwich beam increased with the core wall thickness (relative density). Also, bending isotropy was shown in this study for foldcore composite sandwich beams with selected core geometry.     

Local Buckling Delamination of a Rectangular Sandwich Plate Containing Interface Embedded Rectangular Cracks and Made From Elastic and Viscoelastic Materials

A three-dimensional buckling delamination problem for a rectangular sandwich plate made from elastic and viscoelastic materials is studied. It is supposed that the plate contains interface embedded rectangular cracks and that the edge-surfaces of these cracks have initial infinitesimal imperfections. The evolution of these initial imperfections with an external bi-axial compressed force (for the case where the materials of the layers of the plate are elastic) or with duration of time (for the case where the materials of the layers of the plate are viscoelastic) is investigated. The corresponding boundary value problem is formulated within the framework of the piecewise homogeneous body model with the use of three-dimensional geometrically nonlinear field equations of the theory of viscoelastic bodies. This problem is solved by employing boundary form perturbation techniques, Laplace transform and FEM. According to the initial imperfection criterion, the values of the critical parameters are determined. Numerical results on the critical force and critical time are presented and discussed. In particular, it is established that the values of the critical forces obtained for the buckling delamination around the rectangular embedded interface cracks are significantly greater than those obtained for the corresponding edge and band cracks.     

高速机构用夹芯复合材料横板模态试验分析

针对高速机构用结构复合材料的动态性能问题,以高速织机用夹芯结构复合材料横板和碳铝横板为研究对象,在自由约束状态下,利用模态试验方法,分别沿设定的x和y方向激振,对其进行测试研究。结果表明:沿x和y方向激振时,与碳铝横板相比,夹芯结构复合材料横板对应阶数的固有频率测得值普遍较高,且沿x方向激振时,横板的固有频率测得值与其长度有很大关系。     

Experimental Investigation of Strain Concentrations Caused by Inserts in Sandwich Beams

Abstract:  This paper presents an experimental study of the strain concentrations developing across the insert–core junctions in a sandwich beam with an implanted stiff insert into its core. Strain measurements were carried out at several positions on the skins and across the insert–core junction, for several sandwich beam specimens loaded in 3-points bending and having inserts with various geometries. The materials used were typical marine glass/polyester composite and PVC foams and the specimens were manufactured with the vacuum infusion method. A full material characterization was performed for the composite skins. The experimental results demonstrated a pure linear bending response of the specimens, as well as significant strain concentration factors across the insert–core junction, reaching values up to 3.3. Strain concentration factors measured for butt inserts were lower than those measured on the tension side of the specimens with scarf inserts. Transverse strains measurements verified that all specimens were in a plane stress state.     

影响蜂窝夹层结构滚筒剥离强度主要因素的研究EI

对预浸料与蜂窝直接接触共固化成形的蜂窝夹层结构的滚筒剥离强度进行了研究，主要讨论了树脂基体、预浸料树脂含量及织物构成对滚筒剥离强度的影响。     

Bending Analysis of Curved Sandwich Beams with Functionally Graded Core

In this article, bending analysis of curved sandwich beams with transversely and functionally graded (FG) core is studied. The Euler–Bernoulli beam theory is used to model the thin face-sheets and high-order shear theory is used to analyze the core. Equilibrium/field equations, compatibility and boundary conditions are used to derive the set of governing equations. The numerical solution of the governing nonlinear differential equations is based on the series Fourier–Galerkin method. Finally, the effect of geometric properties on radial deflection of core and the effect of core radius and Young's modulus on radial deflection, circumferential displacement, and stresses are investigated.     

Localized Effects across Core Junctions in Sandwich Beams Subjected to In-Plane and Out-of-Plane Loading

The paper concerns local effects that occur across junctions between different cores in sandwich beams subjected to in-plane and out-of-plane loads. These local effects display themselves by a significant rise of the bending normal stresses in the faces of the sandwich near the core junctions. At the same time, an elevation of the transverse normal and shear stresses in the adjacent core parts is observed. The nature and intensity of the local effects is studied for sandwich beams loaded statically by axial (in-plane) and transverse (out-of-plane) forces. Two types of core junctions, namely a conventional butt junction and a reinforced butt junction, are investigated experimentally. The experimental data coincides perfectly with the numerical simulations performed using Finite Element Analysis.     

Fatigue in fibre metal laminates: The interplay between fatigue in metals and fatigue in composites

With the introduction of fibre metal laminates (FMLs) as a (fatigue) damage tolerant material concept in aeronautics, an interesting field emerged where fatigue damage interaction plays a dominant role. The hybrid concept effectively demands evaluating fatigue damage growth based on fracture phenomena typical for both metals and fibre‐reinforced composites that continuously interact with each other. This paper explains current understanding of the fatigue fracture phenomena in FMLs, and it demonstrates how this interaction limits the criticality of both the metallic and composite fracture phenomena. In addition, it explains how the laminated hybrid configuration can be further exploited scientifically to unravel the physics of the individual fatigue fracture phenomena.     

泡沫夹层复合材料耐水性能研究进展

泡沫夹层复合材料作为一种新型轻质高强材料,目前越来越受到航天、航海及能源等领域的重视,但其应用大部分仍局限于次级结构,主要是由于其可靠性评价未得到广泛深入研究。概述了其吸水性能、吸水后静态和动态力学性能及断裂韧性变化规律,最后提出了防水措施。     

常压等离子处理碳纤/玻纤间隔织物的效果表征

碳/玻纤间隔织物是一种新型结构的纤维增强材料,其纤维与树脂的结合牢度是决定其复合材料性能的主要因素。为了进一步改善碳纤维和玻璃纤维与树脂的界面结合性能,本文采用不同功率的常压低温等离子技术对整体中空织物进行处理,然后通过扫描电镜、吸光率表征、玻纤单丝微脱粘测试以及碳纤维复丝拉伸性能测试等对织物中的碳纤维与玻璃纤维进行表征。研究结果表明,经过等离子处理后,混杂织物中的面层和芯材均受到等离子体刻蚀,纤维表面的官能团增多,纤维浸润性界面结合性能得到改善。同时,研究结果还表明,等离子处理碳/玻间隔织物的改性效果随着功率的增加是先增加后降低,在功率为150w的常压低温等离子处理的效果最佳。     

水下爆炸载荷下圆管夹心板的抗冲击性能研究

防护板在舰船上的应用非常广泛，它对于提高舰船抵抗水下爆炸冲击波载荷性能、抗碰撞冲击性能等都具有重要作用。利用薄壁圆管的吸能特性设计离散型和紧密型圆管夹心板，使用大型非线性有限元软件MSC.Dytran建立水域、炸药及防护板的三维有限元模型，并进行水下爆炸数值仿真计算，从板的吸能能力、加速度响应、变形量三个方面分析两种夹心板和普通平板在水下爆炸载荷作用下的抗冲击性能，仿真计算结果表明离散型夹心板的抗爆性能优于紧密型夹心板和普通平板。     

夹层材料裂纹体疲劳载荷作用下的J积分研究

通过弹塑性有限元方法研究了裂纹平行于界面时夹层材料在平行于界面时夹层材料在Ｉ型疲劳功载荷作用下扩展裂纹的Ｊ积分的适用性，结果表明，在疲劳裂纹的起裂阶段，Ｊ积分具有良好的守恒性，而在随后的疲劳裂纹扩展过程中，由于裂纹尖端区域残留应力的影响，Ｊ积分具有明显的路径依赖性。     

瓦楞结构纸蜂窝夹层的动态性能研究

比较了瓦楞结构蜂窝夹层和普通蜂窝夹层用纸量的差别,用聚醋酸乙烯酯乳液作为黏合剂,使用不同楞型和定量的瓦楞纸板制得瓦楞结构蜂窝夹层,利用冲击实验机研究其动态性能。结果表明:瓦楞结构纸蜂窝夹层受到冲击时会产生规则的褶皱变形,从而吸收冲击能量;瓦楞结构纸蜂窝夹层所用瓦楞纸板定量越大,用纸质量越好,试样受到冲击时产生的冲击加速度值就越大;在冲击高度确定的条件下,随着冲击重锤重量的增加,不同纸板所制试样其最大冲击加速度值都会有一个极小值,该极小值与材料本身有关。     

Fatigue fracture toughness of metals

The paper considers the peculiarities of fatigue crack propagation and final fracture of metals under cyclic loading. It is shown that the value of the fatigue fracture toughness of steels in an embrittled state is appreciably lower than that of the fracture toughness under static loading. A model of the transition from stable to unstable fatigue crack propagation is justified.     

复合材料褶皱夹芯结构的制备及压缩性能研究

目的 探究复合材料褶皱芯子的一次性成型工艺,并研究浸胶量对褶皱夹芯结构压缩性能的影响。方法 以V型褶皱夹芯结构为研究对象,首先采用真空吸附成型工艺制备V型复合材料褶皱芯子,然后通过黏接工艺将碳纤维复合材料层合板与褶皱芯子进行复合,得到复合材料褶皱夹芯结构,最后通过实验测试,研究该结构在压缩载荷作用下的力学性能和失效模式,以及不同浸胶量对其压缩性能的影响。结果 采用真空吸附成型工艺能够一次性制备出褶皱芯子,其成型精度有待提高;由压缩实验可知,褶皱夹芯结构先从壁面开始失效,后逐步扩散至棱线处,最终导致芯子的整体失效;由压缩实验测试结果可知,浸胶量(质量分数)为11%、17%、22%的褶皱夹芯结构的破坏载荷分别为362.853、420.521、471.389 N。结论 采用真空吸附成型工艺可一次性成型出褶皱芯子,其制备效率较高,但存在成型尺寸精度不高问题,后续需要进一步改进;在一定范围内,复合材料褶皱夹芯结构的压缩破坏载荷与芯子的浸胶量近似成正比例线性关系。     

The Effect of Load and Geometry on the Failure Modes of Sandwich Beams

Facing compressive failure, facing wrinkling and core shear failure are the most commonly encountered failure modes in sandwich beams with facings made of composite materials. The occurrence and sequence of these failure modes depends on the geometrical dimensions, the form of loading and type of support of the beam. In this paper the above three failure modes in sandwich beams with facings made of carbon/epoxy composites and cores made of aluminum honeycomb and two types of foam have been investigated. Two types of beams, the simply supported and the cantilever have been considered. Loading included concentrated, uniform and triangular. It was found that in beams with foam core facing wrinkling and core shear failure occur, whereas in beams with honeycomb core facing compressive failure and core shear crimping take place. Results were obtained for the dependence of failure mode on the geometry of the beam and the type of loading. The critical beam spans for failure mode transition from core shear to wrinkling failure were established. It was found that initiation of a particular failure mode depends on the properties of the facing and core materials, the geometrical configuration, the type of support and loading of sandwich beams.     

纸蜂窝夹芯复合板材静态缓冲性能研究

目的为了新型纸蜂窝夹芯复合板材在运输包装中的推广应用,对新型泡状纸蜂窝夹芯复合板和纸蜂窝夹芯复合平板的缓冲性能和吸能特性进行研究。方法主要通过静态压缩实验,研究不同芯高的纸蜂窝结构类板材的应力-应变曲线、总能量吸收图、单位体积能量吸收图和缓冲系数-应变曲线,分析结构和芯高对板材静态压缩性能的影响。结果数据表明同种芯高的板材,纸蜂窝夹芯复合平板的应力峰值稍高;纸蜂窝夹芯复合平板的能量吸收、单位体积能量吸收最好;泡状纸蜂窝夹芯板由于泡结构的作用,缓冲性能大大增强。结论纸蜂窝夹芯复合平板的平压强度最好,而泡状纸蜂窝夹芯复合板的缓冲性能优于同等结构的蜂窝纸板,2种板材都有很好的应用前景。     

高空低温环境对无人机复合材料及夹芯结构性能的影响

针对高空长航时无人机UAV面临的-82℃低温环境,开展低温温度对T700/LT-03A复合材料及夹芯结构的性能影响研究。研究结果表明,低温下复合材料及夹芯结构强度均随温度降低而升高,T700/LT-03A复合材料-82℃时的拉伸强度为2 500 MPa、层间剪切强度为115 MPa、冲击损伤强度CAI保持在150 MPa。其原因是低温下碳纤维的横向收缩比树脂基体小,界面摩擦力得到增强,从而获得高的界面粘接强度。-70℃低温循环后泡沫和蜂窝夹芯结构强度剪切数据分别为2.6 MPa、2.2MPa。低温试验结果表明T700/LT-03A复合材料及夹芯结构在低温下保持了较好的整体承载能力。