塑封组件可靠性测试中加速浸润方法的研究

在对塑封集成电路进行封装可靠性评估中,预处理过程是必经的步骤,其中的浸润测试通常在非加速条件下进行,耗时较长。在市场竞争日趋激烈的环境下,企业迫切需要缩短新产品的可靠性验证时间。针对JEDEC(电子器件工程联合委员会)和JEITA(日本电子信息技术协会)标准中涉及到的三种加速浸润条件,以组件在非加速条件下(JEDECLevel3和JEITARankE)潮气的穿透力、吸收量及由此产生的失效为参照,确定在加速条件下,组件达到同样的潮气吸收量并产生相类似的失效所需的时间;同时应用有限元分析的方法进行建模和计算,并与实际的测量结果比较验证。     

Cracking behavior and delamination mechanism of lamellar structured TBC with localized mixed oxides

Mixed oxide (MO) with localized growth feature and high growth rate remarkably affects the lifetime of thermal barrier coatings (TBCs), which indicates that clarifying the ceramic cracking mechanism induced by MO is critical for developing new coatings with high durability. Two kinds of TBC models involving spherical and layered mixed oxides are created to explore the influence of MO growth on the local stress state and crack evolution during thermal cycle. The growth of α-Al₂O₃ is also included in the model. The undulating interface between ceramic coat and bond coat is approximated using a cosine curve. Dynamic ceramic cracking is realized by a surface-based cohesive interaction. The ceramic delamination by simulation agrees with the experimental observation. The effects of MO coverage ratio and growth rate on the TBC failure are also discussed. The results show that the MO growth causes the local ceramic coat to bear the normal tensile stress. The failure mode of coating is turned from α-Al₂O₃ thickness control to MO growth control. Once the mixed oxide appears, local ceramic cracking is easy to occur. When multiple cracks connect, ceramic delamination happens. Suppressing MO formation or decreasing MO growth can evidently improve the coating durability. These results in this work can provide important theoretical guidance for the development of anti-cracking TBCs.     

Relationship Between Microstructure,Delamination Behavior,and Toughness of Steel Plates Rolled in the Intercritical Region Under Variable Deformation

Herein, the effects of microstructure on delamination behavior and toughness are discussed in detail. Steel plates have been fabricated by intercritical rolling (IR) under various strains (0.5, 0.8, and 1.1). The results show that increasing applied strain enhances the degree of laminated microstructure, and three kinds of impact fracture occur in sequence. 1) No delamination occurs in the IR0.5 steel plate with approximately equiaxed microstructure. 2) Delamination takes place in the IR0.8 steel plate with obvious laminated microstructure. But a crack parallel to the impact load direction forms beneath the delaminated crack. 3) Delamination is enhanced in the IR1.1 steel plate with enhanced laminated microstructure, and no crack forms below the delaminated crack. The delaminated crack mainly propagates along the laminated interfaces, so the laminated microstructure is the key reason for forming delamination. The more apparent laminated microstructure causes more remarkable laminated tearing at room temperature, large-scale severe plastic deformation in the microstructure below the delaminated crack at low temperatures, and longer zigzag cracks at lower temperatures. Therefore, to improve toughness, the microstructure needs enough laminated structure to inhibit the formation of cracks parallel to the impact load direction below the delaminated crack.     

含预制分层损伤复合材料层合板在压缩载荷下破坏过程和剩余强度的模拟

本文运用一种具有较高精度的高阶位移模式,结合特定的损伤判据和刚度折减方法,建立了一种含损伤有限元模型,并利用其对多个含预制分层损伤的复合材料层合板在压缩载荷下的破坏过程进行了数值模拟,并最终得到这些层合板的剩余强度。与实验结果的对比表明,该数值模拟方法具有较高的精度和有效性。     

紧缩能量分层有限Ridgelet图像去噪新方法

有限Ridgelet变换是一种为了克服Wavelet在高维信号处理中的不足而提出的图像处理新方法。通过Radon变换将图像边缘奇异性转变为点奇异性,再利用Wavelet变换针对点奇异性进行处理。根据图像经Radon变换后能量分布紧缩集中,该文提出一种新的Ridgelet改进算法,该算法在图像Ridgelet变换过程中,按能量高低分为两种能量系数矩阵再分别进行降噪处理,并在融合重构以后,再次利用Wavelet变换提取低能量图像中的细节信息并将之融合,二次加强图像细节。使得输出信噪比及图像细节保持上得到大幅度提高。仿真试验表明在受噪声干扰严重情况下,该方法的输出信噪比及视觉效果均优于其他算法。     

基于低能量冲击损伤阻抗的复合材料薄壁结构铺层顺序设计

建立了有效的复合材料层合板结构冲击损伤分析方法,层合板面内损伤采用改进的Chang/Chang 失效准则做判据,得到面内各类损伤形式。层间损伤采用与Mixed-Mode粘接元等效的TIEBREAK接触模拟。利用此分析方法,从复合材料薄壁结构设计需要出发,研究了在低能量冲击下,铺层的层间角度、铺层方向、铺层重叠对层合板结构冲击损伤阻抗的影响规律,并对它们的综合影响进行了总体分析,得到了能提高层合板结构损伤阻抗的铺层顺序设计指导。最后用该设计指导对某种铺层结构进行了重新设计和有限元模拟,验证了该设计指导的可行性和有效性。     

Flutter of delaminated three-phase nano-composite beam-plates

ABSTRACT

In this article the supersonic flutter instability of delaminated carbon nanotube reinforced three-phase composite plate is investigated. The classical laminate plate theory and piston aerodynamic theory are developed to construct the governing equation of delaminated three-phase nano-composite plates. The effective material properties are obtained using Halpin-Tsai relation and rule of mixture. The effects of different parameters including carbon nanotubes (CNTs) weight percentage, fiber volume fraction, CNTs aspect ratio and different fiber orientation on flutter pressure of delaminated reinforced composite plates are considered. According to the results, appending small amount of CNTs (4% wt) into the matrix epoxy can improve the flutter critical pressure by 33% in comparison to the neat matrix epoxy.     

Fatigue Performance of Sandwich Beams With Peel Stoppers

Abstract:  This paper concerns a newly developed peel stopper for sandwich structures, which may be embedded as a core insert or an edge stiffener. The major purpose of the peel stopper is to prevent large debonds/delaminations between face sheets and core in sandwich structures in the case of failure. Experimental investigations of conventional sandwich beams and beams furnished with peel stoppers, under static and fatigue loading conditions, and with temperature monitoring, were conducted. The experimental programme included investigation of crack initiation and propagation, as well as of fatigue endurance of conventional and modified sandwich beams. The results showed that although the peel stoppers did not significantly influence the fatigue life of the sandwich beams, they were exceptionally effective in re-routing the crack propagation away from the face–core interface. Moreover, one of the two peel stopper designs presented prevented face–core debonding/delamination and total failure of the sandwich beams.     

高强玻璃纤维复合材料的铣削加工性能研究

由于复合材料具有各向异性,在加工过程中产生的分层破坏严重影响其装配质量、降低其结合强度,因此需要对复合材料加工过程中的分层情况进行研究.从手糊成型层叠厚板高强玻璃纤维增强复合材料的铣削加工入手,通过单因素法改变切削参数测试作用在试件上的切削力和扭矩的大小来考察加工表面的分层破坏情况.利用正交回归原理建立了切削力、扭矩和分层因子的经验公式,预测了切削力、扭矩和分层因子随切削参数变化的趋势.     

水环境对热塑性复合材料层合板分层疲劳裂纹扩展的影响

本文研究了水环境对ICIAPC-2热塑性预浸料(AS4/PEEK)制成的单向复合材料层合板分层疲劳裂纹扩展的影响.用双悬臂梁试件进行了I型张开位移加载试验.试验环境为23℃水中和50℃水中.水环境未引起很大的不利影响.用电子显微镜和机理分析讨论了水环境对CF/PEEK和CF/环氧两种层合板的差异.