齿槽增强泡桐木夹层结构界面性能试验

采用在芯材表面开槽并注入树脂的方法,可以有效提高泡桐木夹层结构的玻璃纤维树脂面板与泡桐木芯材之间的黏结性能.为比较齿槽的界面增强效果,使用真空导入工艺制备了多个不同槽宽、槽深及间距的试件,应用双悬臂梁(DCB)方法,测试了夹层梁发生层间断裂时的能量释放率,发现齿槽构造可以显著地提高泡桐木夹层结构的界面性能.同时,分析了影响夹层结构界面性能的关键因素,齿槽的增强作用可体现在工艺和界面构造两方面.     

夹层结构用几种芯子力学性能研究

本文介绍了几种常用于夹层结构的芯子,如巴尔沙(Balsa)、蜂窝、泡沫塑料的基本力学性能与密度的关系,配成了试验曲线,这些曲线可供性能比较及产品设计时应用。     

Z向增强泡沫夹层结构复合材料

从应用领域、制造工艺及力学性能等方面论述了国内外关于z向增强泡沫夹层结构复合材料的研究成果。研究了其开发研制和应用中的主要问题，并对此材料力学性能研究前景作出了预测。     

湿热环境下泡桐木复合材料夹芯结构Ⅰ型界面剥离试验研究

采用人工加速老化的方法模拟湿热环境,通过泡桐木玻璃纤维增强复合材料夹芯结构的双悬臂梁拉伸剥离试验,研究湿热环境对玻璃纤维增强复合材料(GFRP)面板和泡桐木芯材的粘结性能的影响。试验结果表明,90 d湿热加速老化后泡桐木复合材料夹芯结构的能量释放率下降了32.3%,芯材泡桐木顺纹抗拉强度下降了11.6%,GFRP面板拉伸模量下降了11.0%。     

复合材料夹层结构在汽车上的应用

本文介绍了复合材料夹层结构的特点及其在汽车上的应用。     

汽车制造商偏爱夹层结构地板

<正> 轻量化复合材料夹层结构正在Audi A4和Daimler Chrysler E Class旅游车车箱地板应用中替代木材。该承载的刚性结构地板是用Baypreg~((R))F聚氨酯树脂和Bayer Polymers AG公司提供的连续玻璃纤维毡作蒙皮和一层纸蜂窝芯制成。用一简单的压力成型工艺模塑该结构件。据Bayer公司介绍,该部件的重量比木材和钢材相应产品大大降低,将有助于降低动力车燃料的消耗。参与了Bayer公司轻量化复合材料开发工作的Reiner Paul先生介绍说:"用Baypreg F     

格构增强型复合材料夹层结构的制备与受力性能

真空导入成型工艺是一种新型的适合大型/异型复合材料结构件成型的技术.选用H-60 PVC泡沫、四轴向玻璃纤维布以及乙烯基酯树脂,通过在泡沫芯材上、下表面开槽,同时沿芯材厚度方向剖开,采用真空导入成型工艺制备出在结构上具有创新构型的格构增强型复合材料夹层结构.研究结果表明,真空导入成型工艺充模速度快、成型效益高;格构增强型复合材料夹层结构的剪切、平压与抗弯性能均较传统夹层结构得以提高;其格构腹板可有效抑制泡沫芯材剪切裂纹的扩展,避免面板与芯材的剥离破坏;阐明了格构增强型复合材料夹层结构的受弯极限承载能力.     

复合材料蜂窝夹层结构计算的一般方法和进展

本文对目前蜂窝夹层结构有限元分析的方法进行旭纳；对每一种计算模型中所包含的假设作一讨论；指出其适用范围，供设计和强度计算时参考。     

固化压力对夹层结构力学性能的影响

通过测试不同固化压力下的Nomex蜂窝夹层结构的力学性能，讨论了固化压力对蜂窝夹层结构性能的影响。结果表明，在固化压力0．2－0．5MPa下，夹层结构的平拉强度、平压强度、剪切强度无明显变化，而侧压强度与弯曲刚度则随压力的增大而发生明显的变化。     

复合材料夹层结构产品固化变形分析

本文讨论产生复合材料产品固化变形的主要原因是树脂收缩引起的各方向上不同的线膨胀系数具体分析了复合材料夹层结构的的固化变形，经技术上的改进解决了固化变形，以满足产品的设计要求。     

Determination of core shear properties of three-dimensional woven sandwich composites

Abstract

The core shear characteristics of a relatively new material have been investigated by two methods: three point bending tests and a shear test. The material is based on woven sandwich fabric preform, which offers important advantages related to the integral core–skin structure. The core shear moduli results from the block shear test and ASTM three point bending tests show very little difference. The results from the shear test obtained by measuring the crosshead displacement were verified by conducting additional shear tests, in which two linear variable differential transformers were used for strain measurement in the longitudinal and transverse directions. The ASTM block shear test and three point bending test were used to determine the core shear strength of the material. To obtain pure core shear failure leads to a correct core shear strength result; the three point bending test was modified by increasing the skin thickness and stiffness of the panel.     

Fabrication process and mechanical properties of C/SiC corrugated core sandwich panel

Carbon fiber reinforced SiC composite is a kind of promising high-temperature thermal protection structural material owing to the excellent oxidative resistance and superior mechanical properties at high temperatures. In this work, a novel design and fabrication process of lightweight C/SiC corrugated core sandwich panel will be proposed. The compressive and three-point bending of the C/SiC corrugated sandwich panels are conducted by experiment and numerical simulation. The relative density of as-prepared C/SiC sandwich panel and the density composite material are 1.1 and 2.1 g/cm³, respectively. As the density of the C/SiC sandwich panel is only 52.3% of the bulk C/SiC, suggesting that lightweight characteristic is realized. Moreover, the C/SiC sandwich panel manifests itself as linear-elastic behavior before failure in compression and the strength is as high as 15.1 MPa. The failure mode is governed by the core shear failure and panel interlayer cracking. The load capacity under the three-point bending C/SiC composite sandwich panel is 1947.0 N. The main failure behavior is core shear failure. The stress distribution under the compression and three-point bend was simulated by FE analysis, and the results of numerical simulations are in accordance with the experimental results.     

Foam sandwich composites with cyanate ester based syntactic foam as core and carbon‐cyanate ester as skin: Processing and properties

Foam sandwich composites were processed using cyanate ester‐based syntactic foam as core and carbon fabric‐cyanate ester composite as skin. They were processed by a one‐step compression‐molding technique. The mechanical performance of the sandwich composites was evaluated in terms of flatwise tensile strength (FTS), flatwise compressive strength, and edgewise compressive strength. The dependency of these properties on the core composition was investigated. FTS initially increased with the increase in resin content of the syntactic foam core. However, higher resin content in the core led to a diminution in FTS due to high void content. The flatwise compressive strength and edgewise compressive strength and the corresponding moduli values showed an increasing trend with increase in resin content of the core despite the presence of voids at high resin content. The failure modes of the composites under different loading conditions have been examined. © 2008 Wiley Periodicals, Inc. J Appl Polym Sci, 2008     

VARI成型泡沫夹层复合材料界面质量控制方法研究

采用本体树脂涂覆、胶膜和辅助织物粘贴在泡沫加工表面的方法分别改善胶接界面,解决了真空树脂浸渗工艺(VARI)制备的非屈曲碳纤维织物(NCF)/聚甲基丙烯胺(PMI)泡沫夹芯复合材料中泡沫与蒙皮的脱粘问题。结果表明,在相同VARI工艺参数条件下,采用890树脂涂覆的方法可以达到大约80%区域面积的良好粘接界面,对应的抗平拉强度提高了30%;同时胶膜和辅助织物粘贴方法则可达到接近100%改善胶接界面质量的效果,其对应的抗平拉强度则分别提高了76%和56%。     

Evaluating the heat resistance of thermal insulated sandwich composites subjected to a turbulent fire

The fire structural response of sandwich composite laminates incorporating bio‐derived constituents subjected to a turbulent flaming fire was investigated. Fire structural tests were conducted on thermal insulated sandwich composites incorporating a thin surface‐bonded non‐woven glass fibre tissue impregnated with char‐forming fire retardant, ammonium polyphosphate. The sandwich composite laminates were loaded in compression at 10%, 15% or 20% of the ultimate compressive strength while simultaneously subjected to turbulent flames imposing an incident heat flux of 35 kW/m². Generally, the failure time increased with the reduced applied compressive load. The thermal insulated sandwich composite laminates had considerably improved fire resistance in comparison to their unmodified counterparts. The unmodified composites failed 96 s earlier than the thermal insulated specimens when the compression load was 10% of the ultimate compressive strength. The presence of ammonium polyphosphate at the heat‐exposed surface promoted the formation of a consolidated char layer, which slowed down heat conduction into composite laminate substrate. The fire reaction parameters measured via the cone calorimeter provided insights into the thermal response hence fire structural survivability of sandwich composite laminates. Copyright © 2015 John Wiley & Sons, Ltd.     

纸质蜂窝夹芯的粘接技术

按纸质蜂窝夹芯材料的生产过程，较为详细地介绍了它的生产工艺和关键工序应掌握的技术以及各项工艺参数。     

Graphene added multilayer ceramic sandwich (GMCS) composites: Structure,preparation and properties

The multilayer ceramic composites (MLC) consist of two ceramic materials insoluble in each other and sequentially piled in a symmetric manner whereas they can be divided into two groups: multilayer composites with weak interfaces and composites with strong interfaces. The graphene added multilayer ceramic sandwich (GMCS) composite was developed. The multilayer stack of Si₃N₄ with 5 and 30 wt% graphene addition were stratified in sandwich structure. So formed multilayer stacks with 5 and 7 layers were sintered by hot issostatic pressing (HIP). The homogenity of graphene addition, the effect of layered structures and the position of layers with lower and higher graphene content on the final properties were studied.     

O＇－Sialon－ZrO_2复合材料的显微结构与力学性能的研究

研究了Ｏ＇－Ｓｉａｌｏｎ－ＺｒＯ２复合材料的显微结构与力学性能的关系。结果表明，Ｏ＇－Ｓｉａｌｏｎ形成连续网络编织状结构。ＺｒＯ２加入量较少时充当填充结构骨架的作用；ＺｒＯ２加入量增多时（至４０％），会有更多的ＺｒＯ２形成聚集体。随着ＺｒＯ２引入量的增加，材料的常温抗折强度提高，但高温抗折强度下降。Ｏ＇－Ｓｉａｌｏｎ的编织状结构可能阻碍晶界滑移。这种复合材料的高温抗折强度在１４００℃为１１２～１７３ＭＰａ。     

A comparative study on some properties of wood plastic composites using canola stalk,Paulownia, and nanoclay

In this research, the reinforcing effect of fillers including canola stalk, paulownia and nanoclay, in polypropylene (PP) has been investigated. In the sample preparation, 50 wt% of lignocellulosic materials and 0, 3, and 5 wt% of nanoclay particles were used. The results showed that while flexural and tensile properties were moderately enhanced by the addition of nanoclay in the matrix, notched Izod impact strengths decreased dramatically. However, with increase in the nanoclay content (5 wt%), the flexural and tensile properties decreased considerably. The mechanical properties of composites filled with paulownia are generally greater than canola stalk composites, due to the higher aspect ratio. The thickness swelling and water absorption of the composites significantly decreased with the increase in nanoclay loading. Except tensile modulus, the differences between the type of fibrous materials and nanoclay contents had significant influence on physicomechanical properties. Morphologies of the composites were analyzed using transmission electron microscopy (TEM) and X‐ray diffraction (XRD), and the results showed increased d‐spacing of clay layers indicating enhanced compatibility among PP, clay, and lignocellulosic material. TEM micrographs also confirmed that the composites containing 3 wt% nanoclay had uniform dispersion and distribution of clay layers in the polymer matrix. © 2012 Wiley Periodicals, Inc. J. Appl. Polym. Sci., 2013