铝合金板与混凝土的粘结性能

铝合金材料具有强度高、变形性能好、耐腐蚀等优点,是沿海侵蚀环境中钢筋混凝土结构加固工程的理想材料;而铝合金板与混凝土的粘结性能是铝合金板加固钢筋混凝土梁能否协同工作的关键问题。基于此,对铝合金板与混凝土的粘结性能进行试验和理论研究。考虑混凝土强度、铝合金板宽度和厚度、粘贴长度及界面处理等因素对铝合金板和混凝土块体粘结性能的影响,设计了一套试件固定装置,采用万能试验机对105个铝合金板与混凝土棱柱体的粘贴试件进行了面内单剪试验。根据试验结果,结合理论分析,得到了铝合金板和混凝土连接的粘结破坏典型特征、剪应力分布曲线和粘结滑移曲线。研究表明,试件存在两种破坏形式:界面剥离破坏和混凝土层剥离破坏。界面处理对粘结性能有重要的影响,粘贴界面没有进行糙化处理的试件发生了界面剥离破坏,其他试件发生了混凝土层剥离破坏;随着混凝土强度的提高、铝合金板宽度和厚度的变小,粘结性能提高;存在一个有效粘贴长度,当粘贴长度大于有效粘贴长度后,增大粘贴长度并不能提高连接的极限荷载。     

玄武岩纤维编织网的网格尺寸对混凝土拉伸性能的影响

为研究网格尺寸对玄武岩纤维编织网增强混凝土(BTRC)拉伸性能的影响,进行了不同网格尺寸的4组48个试件的BTRC薄板单轴拉伸试验,分别从宏观和细观尺度分析BTRC薄板的破坏模式。在分析过程中采用ACK模型验证BTRC薄板拉伸的本构关系方程,并通过有限元模拟对结果进行对比验证。结果表明:BTRC薄板在拉伸荷载下呈明显的应变硬化特点;BTRC薄板的破坏模式为典型的脱黏破坏,且网格尺寸越小,纤维编织网与混凝土之间的黏结性能越好,单裂缝开展的细小裂纹越多;玄武岩纤维编织网不会改变混凝土的开裂强度,却能明显地提高其极限抗拉强度;编织网的网格尺寸越小,有效受力纤维束越多,抗拉强度越高。     

双组分聚氨酯人造草背胶的研制

介绍了一种双组分聚氨酯人造草背胶的制备方法,以聚醚多元醇、异氰酸酯为主体原料,3,3'-二氯-4,4'-二氨基二苯基甲烷(MOCA)为扩链剂,研究了不同聚醚多元醇质量比、扩链剂用量、异氰酸酯质量比、异氰酸酯指数对人造草背胶操作时间、脱粘时间及力学性能的影响。结果表明,当异氰酸根指数为0.99,A组分中聚醚多元醇MN-3050与DL-1000质量份数分别为80、20,A组分中扩链剂MOCA用量为4份,B组分中MDI-50与PM-200质量比为1∶1,当A、B组分按质量比2∶1混合时,操作时间及脱粘时间最佳,人造草背胶的综合力学性能达到最好。     

TiO2纳米管薄膜的脱层现象（英文）

分别通过曲率法和基体拉伸应变测试方法研究TiO2纳米管薄膜的残余应力和脱层行为。结果表明:TiO2纳米管薄膜的内残余应力为-54MPa。TiO2纳米管薄膜室温样、250°C退火样和400°C退火样的脱层出现点的应变依次为2.6%、5.1%和8.6%,半径依次为27.5、17.1和19.4μm。TiO2纳米管薄膜室温样、250°C退火样和400°C退火样的真实临界脱层应力为220.4、394.5和627.9MPa。在脱层条件下,对界面剪滞模型进行修订,并对TiO2纳米管薄膜界面剪切强度进行多项式拟合。由于拟合结果与裂纹密度的分析结果能很好吻合,因此界面剪滞模型的修订方程和多项式拟合方程均为可信的。     

Elastic Wave Scattering From a Partially Debonded Elastic Cylindrical Inclusion

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Dual-stage tertiary creep of a ceramic matrix composite

The creep behaviour of an alumina fibre/silicon carbide matrix composite has been studied. The creep curves are characterised by a short primary stage followed by one or two tertiary stages. The secondary regime of this composite is limited to a single point. The occurrence of one or two tertiary stages in the creep behaviour is discussed, and some theoretical considerations are invoked to explain this behaviour. Creep in this composite is controlled by two mechanisms, namely viscoplastic creep of the alumina fibres and damage accumulation within the composite. The two tertiary stages differ in the damage mechanisms occurring, the first one being related to fibre–matrix debonding only, whereas successive fibre failure dominates in the second part. The second tertiary regime occurs only at low creep stresses, for which a non-catastrophic rupture of the composite is observed.     

Role of controlled debonding along fiber/matrix interfaces in the strength and toughness of metal matrix composites

In metal matrix composites toughness is derived primarily from the plastic work of rupture of ductile matrix ligaments between the fractured fibers and from the plastic work of simple shear separation along steps connecting major fracture terraces. In the optimization of tensile strength in the longitudinal and transverse directions together with the respective works of fracture the most important factor is the control of the extent of debonding along interfaces between the fibers and the matrix, which develops locally in the course of deformation in a continuously changing mix of modes. In Al alloy matrix composites reinforced with Al₂O₃ fibers an effective means of controlling the key interface fracture toughness is through coarsening of Al₂Cu intermetallic interface precipitates which prescribe a ductile fracture separation layer. A combined experimental approach and micromechanical modeling, utilizing a specially tailored novel tension/shear: traction/separation law provides the means for further optimization of overall behavior. This revised version was published online in July 2006 with corrections to the Cover Date.     

Defect propagation at a circular interface

In this paper a nonlinear, nonuniform cohesive zone is employed to study the detailed features of quasi-static defect evolution in a simple, planar elastic system consisting of a circular inclusion embedded in an unbounded matrix subject to different remote loading configurations. The inclusion–matrix interface is assumed to be described by Needleman-type force-separation relations characterized by an interface strength, a characteristic force length and a shear stiffness parameter. Interface defects are modeled by an interface strength which varies with interface coordinate. Infinitesimal strain equilibrium solutions, which allow for rigid body inclusion displacement, are sought by eigenfunction approximation of the solution of the governing interfacial integral equations. For equibiaxial tension, quasi-static defect initiation and propagation occur under increasing remote load. For decreasing characteristic force length, a transition occurs from more or less uniform decohesion along the bond line to propagation of a crack-like defect. In the later case a critical failure load is well defined and interface failure is shown to be defect dominated (brittle decohesion). For interfaces with large characteristic force length, the matrix “lifts off” the inclusion accompanied by a delay in defect propagation (ductile decohesion). The decohesion modes ultimately give rise to a cavity with the inclusion situated within it on the side opposite to the original defect. Results for small characteristic force length show consistency with England’s results for the sharp arc crack on a circular interface (England AH (1966) ASME J Appl Mech 33:637–640) Stress oscillation and contact at the tip of the defect are observed primarily for small characteristic force lengths under extremely small loading. Results for remote tension, compression and pure shear loading are discussed as well. In the final section of the paper the results obtained in the first part are utilized to estimate the plane effective bulk response of a composite containing a dilute distribution of inclusions with randomly oriented interface defects.     

Effects of the surface treatments of lignocellulosic fibers on their debonding stress

This paper presents some results on the surface treatments given to natural fibers, namely coir, banana, and sisal fibers, using γ-methacryloxypropyltrimethoxysilane (MEMO), y-aminopropyltriethoxysilane (AMEO), sodium alginate (NaAl), and sodium hydroxide (NaOH) solutions. The cleaned, washed, and dried fibers were dipped in these solutions separately for a given time and dried. Treated and untreated fibers were tested for strength properties including debonding stress, and structural analysis of the fibers was carried out. It was found that a 3-11% increase in debonding stress was observed for all the treated fibers; and about 30% increase in the ultimate tensile strength (UTS), 9% in initial modulus for silane-treated coir, and only 18% increase in UTS for NaAl-treated coir and sisal fibers were also observed. No significant improvement was observed in the case of surface-treated banana fibers.     

Interfacial damage in fibre‐reinforced composites subjected to tension fatigue loading

ABSTRACT The interfacial behaviour of fibre‐reinforced composites subjected to tension fatigue loading is studied based on the shear‐lag model. The governing equations of this problem are obtained and solved. In order to describe the interfacial debonding, the Paris fatigue crack growth formula as well as a modified degradation model for the coefficient of friction is adopted. Finally some important values related to interfacial debonding are obtained. In the present investigation, Poisson's contraction is considered.