STUDY ON DEBONDING FAILURE MODEL OF POLYUREA-BASED COATING WITH HIGH VELOCITY WATER FLOW BASED ON COHESIVE ZONE MODEL

冲磨和空蚀破坏是水利水电设施最为常见的病害之一,严重影响水利水电设施的安全运行和效益发挥. 泄洪建筑物通常喷涂聚脲基涂层来提高抗冲耐磨性能,但在泄洪高速水流速度作用下抗冲磨聚脲基涂层的剥离破坏机理的研究尚属空白. 本文基于高速水流的流态形式,提出了高速水流对泄洪建筑物的力学作用模型,水流作用对泄洪建筑物的载荷主要包括拖曳力、冲击力、脉动力和上浮力;采用内聚力模型表征聚脲基涂层与泄洪建筑物防护体界面的剥离破坏过程,建立了高速水流聚脲涂层的剥离破坏模型, 给出了模型的有限元形式方程、本构关系以及损伤起始原则、演化原则和接触碰撞模型. 通过聚脲涂层与混凝土基底的剥离破坏试验,分析了不同剥离倾角下界面剥离破坏的拉应力与倾角之间的变化规律,得到了聚脲涂层剥离破坏过程中应力-$\!$-位移变化关系. 根据剥离破坏试验计算了界面剥离破坏断裂模型参数,采用数值方法对模型进行了验证,试验结果与模型计算结果吻合良好,为泄洪建筑物的抗冲耐磨设计提供理论依据.     

聚脲涂层的冲蚀磨损机理研究

采用高速含沙水射流冲蚀磨损试验机测试了聚脲涂层的冲蚀磨损性能,试验结果表明所制备聚脲涂层具有优异的耐冲蚀性能.根据Bitter的塑性材料冲蚀模型,应用Matlab程序进行拟合计算,探讨聚脲涂层在不同冲蚀角度和速度下的冲蚀规律,研究表明聚脲涂层在冲蚀角度30°时切削磨损量最大,而接近90°时变形磨损量最大.     

薄膜涂层材料界面纯剪破坏标准试验法的开发

界面强度是薄膜涂层材料的最重要的性能指标之一，目前尚缺乏有效的测量方法。测量界面强度的主要困难在于寻求一种便于试验的试件形状和加载方式，使得界面上能够产生不同的应力状态，即在不同的剥离应力和剪应力比的状态下发生破坏。本文采用有限元数值分析（ABAQUS），研究了几种具有简单几何形状的试件的界面应力，并基于大量的数值试验，设计了剪应力为破坏支配因素的试件形状和加载方式，并且给出了便于应用的最大界面剪应力的经验估算公式。该经验公式可以适用于各种材料组合和薄膜涂层的厚度。研究结果表明，通过对薄膜涂层材料试件的基体引入缺口以产生应力集中，进行普通的四点弯曲试验，可以进行剪应力占支配地位的界面破坏试验。利用本文提出的试件形状和相应的最大界面剪应力经验公式，可以通过破坏试验简单地得到界面的剪切强度。     

有限元模拟TIN 膜/碳钢基材体系的摩擦磨损试验

对TiN膜/碳钢基材体系摩擦磨损过程的有限元模拟表明:磨痕边缘的多种应力集中、磨痕内外的张应力、膜/基界面切应力,都将影响体系的摩擦学行为.用销/盘试验验证了有限元模拟结果,根据对膜层中裂纹的萌生、扩展和体系的损伤、破坏情况分析,摩擦磨损过程分为磨合、稳定磨损、膜层失稳、体系失效阶段.提出了小载荷摩擦磨损下过软基材的膜/基体系失效机制,即膜层在集中应力和张应力作用下发生裂纹萌生和扩展的脆性破坏,其中,由于体系变形引起的磨痕边缘应力集中对膜层早期损伤进而导致体系磨损失效具有最重要作用.     

埋入式光纤传感器界面剪切强度实验

采用实验方法对光纤与基体间界面性能进行研究.用临界断裂长度法直接测定界面的剪切强度,由于光纤拉伸强度高于树脂基的拉伸强度,出现试验时基体破坏而光纤完整地从树脂基中拔脱的现象.用单丝拔出法测量光纤与基体之间界面剪切强度,试验结果表明,光纤单丝拔出时,总是出现光纤涂层在锚入端断裂,而纤芯从涂层中拔脱的现象,说明当光纤埋入复合材料中,涂层和基体材料结合为一体,光纤涂层与纤芯之间界面剪切强度最低.承载时,若光纤所受正应力超过σ_(max),会出现光纤涂层与纤芯之间界面脱离,产生裂纹,降低整体结构力学性能.     

聚脲加固砖填充墙抗爆性能的试验和分析方法研究

为了掌握聚脲喷涂加固砖填充墙的抗爆特性,基于一种改进的大型爆炸试验装置,开展了聚脲加固框架砖填充墙的原型爆炸试验,分析了爆炸荷载作用下加固砖墙的动力响应特征和破坏过程及模式,揭示了其失效破坏机理。研究结果表明,聚脲加固可大幅提升填充墙构件的抗爆性能,显著增加填充墙构件的变形延性;加固砖墙受爆炸荷载作用发生振动的过程其体系刚度不断变化,最高相差133%;随着比例距离降低,加固砖墙的破坏模式逐渐由弯曲破坏转为剪切破坏,聚脲厚度超过6 mm可以有效限制局部剪切破坏现象;基于砖墙和聚脲涂层的抗力函数建立的理论计算模型,可以较为准确地预测爆炸作用下背爆面加固双向砖墙的正向位移响应过程。     

基于圆筒模型的热障涂层安定分析

热载荷作用下,由于热障涂层(thermal barrier coatings, TBCs) 各层材料的热不匹配以及材料参数的温度相关等因素,会使热障涂层界面区域存在复杂的应力应变场,影响系统安定性,并导致涂层开裂和剥落. 将热障涂层外凸和内凹微观界面结构简化为多层圆筒模型,借助经典机动安定定理,利用特雷斯卡(Tresca) 屈服准则和增量破坏准则处理对时间的积分问题,避免了常规安定性分析的数学规划问题,建立了热障涂层安定极限分析方法,将材料屈服强度随温度变化关系简化为双线性关系,利用补偿变换的方法简化求解过程,对典型热障涂层安定性进行了研究. 结果表明,利用基于圆筒的安定极限分析方法,能够方便求解安定极限,便于工程应用;热障涂层安定极限值明显高于弹性设计值,且界面外凸区域安定极限高于内凹区域极限值,结构首先在内凹处失效;圆筒模型基体曲率和涂层厚度越大,结构安定极限越高,分析结果与试验结果一致;所建立的热障涂层安定分析方法,对进一步研究考虑蠕变因素影响的热障涂层安定性具有重要意义.      

纤维增强陶瓷基复合材料疲劳迟滞回线模型研究

纤维增强陶瓷基复合材料初始加载到疲劳峰值应力时, 基体出现裂纹, 纤维/基体界面发生脱粘. 在疲劳载荷作用下, 纤维相对基体在界面脱粘区往复滑移使得陶瓷基复合材料出现疲劳迟滞现象. 建立了纤维陶瓷基复合材料疲劳迟滞回线细观力学模型, 采用断裂力学方法确定了初始加载纤维/基体界面脱粘长度、卸载界面反向滑移长度与重新加载新界面滑移长度, 分析了4种不同界面滑移情况的疲劳迟滞回线. 假设正交铺设与编织陶瓷基复合材料疲劳迟滞回线主要受0°铺层、轴向纱线内纤维/基体界面滑移的影响, 预测了单向、正交铺设与编织陶瓷基复合材料在不同峰值应力与不同循环的疲劳迟滞回线, 与试验结果吻合.      

涂层/基体体系的界面应力分析

针对热防护涂层的承载特征,建立了涂层、基体体系的平面应变模型.以均匀应变差比拟热膨胀失配,基于最小功原理,推导了完整涂层/基体界面应力的级数解.分析结果表明,在自由端面附近,界面应力集中明显,其峰值达到了与涂层内拉应力相当的量级.涂层膨胀或收缩,界面正应力分别呈现压应力或拉应力状态,界面剪应力也发生方向交变.     

聚脲润滑脂噪音特性的衰退机制研究

低噪音润滑脂是高速电主轴、高速电机及高端家电中高精密轴承广泛使用的润滑介质. 当前有关低噪音润滑脂的研究大都集中在基础油、稠化剂和生产工艺等因素对润滑脂噪音特性的影响,而对长期使用过程中润滑脂噪音性能的变化行为及其微观机制则缺乏足够关注. 本论文中围绕低噪音聚脲润滑脂,基于FE9轴承测试台架,结合润滑脂噪音检测技术,考察了低噪音聚脲润滑脂在使用过程中噪音特性的衰退行为. 结果表明,静音性能优异的聚脲基低噪音润滑脂在轴承试验开始的100 h内,噪音等级已由GN4级衰减为GNX级,丧失减振降噪能力. 对取样润滑脂的微观结构表征发现,润滑脂噪音等级的衰退与聚脲润滑脂内稠化剂团聚体的形成高度关联. 团聚体的形成破坏了稠化体系的结构连续性,导致稠化网络的结构保持性显著下降,失去束缚的大尺寸团聚体随基础油流入轴承运动界面,进而引发高速轴承的振动和噪声. 热分析结果表明该低噪音聚脲稠化剂可能为一种亚稳态聚脲结构,在受热条件下会向组装度更高的团聚体发展. 本论文中的研究表明低噪音润滑脂的噪音寿命与轴承试验中得到的服役寿命相关度并不高,充分评估热作用对润滑脂微观结构及噪音特性的影响,对于保障高速精密轴承的长期可靠运行具有重要意义.      

基于弹性-塑性内聚力模型的纤维拔出界面宏观行为分析

用解析法分析了单纤维从聚合物基体中的拔出过程,采用弹性—塑性内聚力模型模拟裂纹的扩展和界面失效,确定了临界纤维埋入长度,该值区分两种不同长度的纤维拔出过程. 在纤维拔出过程,界面经历不同的阶段. 纤维埋长小于临界长度时,界面的脱粘载荷与纤维的埋长成正比;超过临界长度后,界面的脱粘载荷近似为常数. 分析了界面参数对脱粘载荷的影响:增加界面的剪切强度和界面的断裂韧性,或减小界面裂纹萌生位移,均能提高界面的脱粘载荷;界面脱粘后无界面摩擦应力时,拔出载荷—位移曲线的峰值载荷等于界面的脱粘载荷;界面摩擦应力存在时,使峰值载荷大于脱粘载荷,需要较长的纤维埋入长度和较大的界面摩擦应力.      

热应力作用下层合路面结构层间剥离内力分析

温度变化会造成环氧树脂-混凝土特种路面结构边缘处产生脱层现象.基于层合结构热应力的两变量解析模型,推导了层间剥离力矩和剥离剪力.该方法避免了采用弹性理论求解局部复杂应力状态的困难,为解决层合结构边界脱层问题提供了新途径;由此,研究了环氧树脂层的厚度和弹性模量对层间剥离内力和混凝土层最大拉应力的影响.计算结果表明,通过控制环氧树脂层厚度和弹性模量,可有效降低剥离内力,避免剥离破坏.     

Debonding analysis of FRP–concrete interface between two balanced adjacent flexural cracks in plated beams

A cohesive interface modeling approach to debonding analysis of adhesively bonded interface between two balanced adjacent flexural cracks in conventional material (e.g., concrete or wood) beams strengthened with externally bonded FRP plates is presented. Both the strengthened beam and strengthening FRP are modeled as two linearly elastic Euler–Bernoulli beams bonded together through a thin adhesive layer. A bi-linear cohesive model, which is commonly used in the literature, is adopted to characterize the stress-deformation relationship of the FRP–concrete interface. Completely different from the single-lap or double-shear pull models in which only the axial pull force is considered, the present model takes the couple moment and transverse shear forces in both the substrates into account to study the second type of intermediate crack-induced debonding (IC debonding) along the interface. The whole debonding process of the FRP–concrete interface is discussed in detail, and closed-form solutions of bond slip, interface shear stress, and axial force of FRP in different stages are obtained. A rotational spring model is introduced at locations of the two adjacent flexural cracks to model the local flexibility of the cracked concrete beam, with which the relationship between the local bond slip and externally applied load is established and the real bond failure process of the FRP-plated concrete beam with the increasing of the externally applied load is revealed. Parametric studies are further conducted to investigate the effect of the thickness of adhesive layer on the bond behavior of FRP–concrete interface. The present closed-form solution and analysis on the local bond slip versus applied load relationship for the second type of IC debonding along the interface shed light on the bond failure process of structures externally strengthened with FRP composite plates and can be used effectively and efficiently to predict ductility and ultimate load of FRP-strengthened structures.     

Modelling and experimental investigation of horizontal buoyant gas jets injected into stagnant uniform ambient liquid

In this article, an experimental and theoretical study on the buoyant non-condensable gas jet that is injected horizontally into a high-density liquid ambient at different initial conditions is performed. Direct and instantaneous global measurements of the interface were performed using a high-speed photography. The position and motion of the entire gas jet were captured by a high-velocity camera and the images were processed, averaged and analyzed to extract the jet parameters and interface position. In the mathematical model, the rate of entrainment is assumed to be a function of the jet centerline velocity, the ratio of the mean jet and the ambient densities, while the entrainment coefficient depends on the local Froude number at the jet region. An interfacial shear stress acting at the interface between the jet flow and the water ambient in the opposed direction to the main jet momentum flux is considered. The results showed that the model is able to accurately predict the jet parameters: trajectory, spread, jet angles and penetration lengths as well as the jet regimes. An overall good agreement was obtained between the simulation and experimental results over a large range of Froude numbers and jet diameters. The developed model has proven to be an adequate tool to predict the different jet parameters.     

THEORETICAL MODEL ON INTERFACE FAILURE MECHANISM OF REINFORCED CONCRETE CONTINUOUS BEAM STRENGTHENED BY FRP

Fiber reinforced polymer （FRP） composites are increasingly being used for the re-pair and strengthening of deteriorated concrete structural components through adhesive bonding of prefabricated strips/plates and the wet lay-up of fabric. Interfacial bond failure modes have attracted the attention of researchers because of the importance. The objective of the present study is to analyse the interface failure mechanism of reinforced concrete continuous beam strength-ened by FRP. An analytical solution has been firstly presented to predict the entire debonding process of the model. The realistic bi-linear bond-slip interfacial law was adopted to study this problem. The crack propagation process of the loaded model was divided into four stages （elastic,elastic-softening,elastic-softening-debonded and softening-debonded stage）. Among them,elastic-softening-debonded stage has four sub-stages. The equations are solved by adding suitable stress and displacement boundary conditions. Finally,critical value of bond length is determined to make the failure mechanism in the paper effective by solving the simultaneously linear algebraic equations. The interaction between the upper and lower FRP plates can be neglected if axial stiffness ratio of the concrete-to-plate prism is large enough.     

Dislocation stability in three-phase nanocomposites with imperfect interface

Interface imperfection can significantly affect the mechanical properties and failure mechanisms as well as the strength and toughness of nanocomposites. The elastic behavior of a screw dislocation in nanoscale coating with imperfect interface is studied in the three-phase composite cylinder model. The interface between inner nanoin- homogeneity and intermediate coating is assumed as perfectly bonded. The bonding between intermediate coating and outer matrix is considered to be imperfect with the assumption that interface imperfection is uniform, and a linear spring model is adopted to describe the weakness of imperfect interface. The explicit expression for image force acting on dislocation is obtained by means of a complex variable method. The analytic results indicate that inner interface effect and outer interface imperfection, simultaneously taken into account, would influence greatly image force, equilibrium position and stability of dislocation, and various critical parameters that would change dislocation stability. The weaker interface is a very strong trap for glide dislocation and, thus, a more effective barrier for slip transmission.     

各向异性复合材料中界面屈服/脱粘对裂纹扩展的影响

本研究针对层状复合材料中正交于层合面的裂纹,研究裂纹前方层状界面发生屈服或脱粘现象对该裂纹前沿应力场的扰动。通过利用叠加原理,借用滑移型位错密度表征界面的屈服或脱粘。利用Chebyshev数值积分法求解相应的位错密度的奇异积分方程,得到沿界面屈服/脱粘区域的位错密度分布及裂端区应力场。结果表明,若层状复合材料界面为发生屈服或脱粘,将减弱独立层裂尖的应力奇异性,进而抑制独立层中裂纹的扩展。     

Mechanics of adhesive joints

Summary Taking into consideration both the pulling and bending actions of the external force, the differential equations for bending of a partly attached tape in a peeling test have been derived. The equations relating the peeling load to the adhesive force were derived under the assumption that the peeling may proceed step by step from the attached end when the adhesive force is overcome by either the tensile stress along the interface (shearing peeling) or that which is perpendicular to the interface (tensile peeling). To verify the validity of the obtained equations, the dependence of the peeling load P on the angle between the direction of the action of the load and the adhering surface has been investigated using plasticized polymer films. In view of the elementary mechanics, the results were satisfactory, while a modification was attempted by introducing the stress concentration factor.