• 마이크로전자및패키징학회지
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• 제25권2호
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• pp.41-48
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• 2018

Fan-out wafer level packaging (FOWLP) 적용을 위한 최적의 Cu 재배선 계면접착에너지 측정방법을 도출하기 위해, 전기도금 Cu 박막과 WPR 절연층 계면의 정량적 계면접착에너지를 $90^{\circ}$ 필 테스트, 4점 굽힘 시험법, double cantilever beam (DCB) 측정법을 통해 비교 평가 하였다. 측정 결과, 세 가지 측정법 모두 배선 및 패키징 공정 후 박리가 일어나지 않는 산업체 통용 기준인 $5J/m^2$보다 높게 측정되었다. 또한, DCB, 4점 굽힘 시험법, $90^{\circ}$ 필 테스트 순으로 계면접착에너지가 증가하는 거동을 보였는데, 이는 계면파괴역학 이론에 의해 위상각 증가에 따라 이종재료 계면균열 선단의 전단응력성분 증가에 따른 소성변형에너지 및 계면 거칠기 증가 효과에 의한 것으로 설명이 가능하다. FOWLP 재배선에 대한 최적의 계면접착에너지 도출을 위해서는 시편제작 공정, 위상각 차이, 정량적 측정 정확도 및 결합력 크기 등을 고려하여 4점 굽힘 시험법 또는 DCB 측정법을 적절히 혼용 사용하는 것이 타당한 것으로 판단된다.

• 대한기계학회논문집A
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• 제34권1호
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• pp.55-60
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• 2010

틸팅형 고속열차의 차체에 적용되는 하니컴 복합재 조인트 구조물의 경우 운행중 외팔보형 굽힘하중을 받게된다. 하이브리드 복합재 조인트 구조물에 대한 굽힘시험평가를 수행하기 위해 실제 틸팅열차 차체 구조물에서 조인트부를 절단 채취하여 시험편으로 제작하였다. 굽힘시험결과 시험편의 파괴거동은 정적하중과 피로하중하에서 확연히 달라짐을 보였다. 정적굽힘하중 하에서는 하니컴 코어 영역에서 전단변형과 파괴가 발생하였으며, 피로굽힘하중 하에서는 복합재 표피층과 하니컴 코어층 사이에서 계면분리가 발생하거나, 또는 금속재 언더프레임과의 용접부에서 파괴가 발생하였다. 이러한 파괴거동은 다른 산업분야에서 사용되는 유사한 구조의 하니컴 복합재 조인트 구조물에서도 발생할 수 있기 때문에, 본 실험 결과를 하니컴 복합재 조인트 구조물의 설계변수를 개선하기 위해 이용될 수 있다.

• Journal of Welding and Joining
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• 제6권4호
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• pp.44-53
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• 1988

The mechanical strengths of buried lamellar tears located near the weld toe in the welded tee joints were evaluated in terms of the loss of load carrying capacity as a function of tear area. In static loading, the load carrying capacity was significantly reduced when tear intercepted over 10% of the cross-sectional area of the welded joints. However, the welded joints containing buried tears still failed at stresses over the yield strength of the base metal in the through-thickness direction in spite of the presence of tears up to 20-25% of the area. Fatigue strength of welded joints containing tears markedly reduced with increasing tear areas. Lehigh lamellar tearing test used in this study to produce speicmens was described in detail. The load carrying cpapacity in static loading was influenced by the reduction of supporting area whereas that in fatigue loading was influenced by the stress-concentration effects of lamellar tears and the reduction of supporting area. In bend tests, the pre-existing lamellar tears always grew up toward the weld toe. However, in fatigue loading, cracks grew up and down simultaneously form both the weld toe and the top of lamellar tears because of stress concentration. In fatigue loading, delaminations and decohesion of inclusion/matrix interface generated in multipass welds provided crack propagation paths and enhanced crack propagation because the tips of delaminations and deconhesios acted as stress raisers.

• Structural Engineering and Mechanics
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• 제74권6호
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• pp.723-735
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• 2020

This study is reported the adhesion failure in adhesive bonded composite and specifically for the T-joint structure. Three-dimensional finite element analysis has been performed using a commercial tool and the necessary outcomes are obtained via an eight noded solid element (Solid 185-element) from the library of ANSYS. The structural analysis input has been incurred through ANSYS parametric design language (APDL) code. The normal and shear stress distributions along different layers of the joint structure have been evaluated as the final outcomes. Based on the stress distributions, failure location in the composite joint structure has been identified by using the Tsai-Wu stress failure criterion. It has been found that the failure index is maximum at the interface between flange and web part of the joint (top layer) which indicates the probable location of failure initiation. This kind of failures are considered as adhesion failure and the failure propagation is governed by strain energy release rate (SERR) of fracture mechanics. The different adhesion failure lengths are also considered at the failure location to calculate the SERR values i.e. mode I fracture (opening), mode II fracture (sliding) and mode III fracture (tearing) along the failure front. Also, virtual crack closure technique (VCCT) principle of fracture mechanics steps is used to calculate the above said SERRs. It is found that the mode I SERR is more dominating compared to other two modes of failure for the joint considered. Finally, the influences of various parametric (geometrical and material) effect on SERR of the joint structure are evaluated and discussed in details.

• 비파괴검사학회지
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• 제33권2호
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• pp.198-204
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• 2013

리튬이온전지의 충/방전 열화 과정에서 발생하는 음향방출 신호를 검출하여 누적카운트, 방전용량, 미세손상 사이의 상관관계를 확인하였다. 상용 리튬이온전지를 사용하여 가속 충/방전 싸이클 실험을 하면서 음향방출 신호를 수집하였다. 다수의 음향방출 신호가 전지의 충전 및 방전 과정에서 각각 검출되었다. 충/방전 열화 싸이클이 증가함에 따라 전지 용량은 감소하였고 음향방출 신호의 누적카운트는 증가하는 경향을 보였다. 충/방전 후 전지를 분해하여 내부 전극 손상을 관찰한 결과 전극 계면 박리 및 미소균열이 다수 확인되었으며, 이러한 기계적 손상이 음향방출원인 것으로 판단된다. 전지 방전용량과 음향방출 누적카운트 사이에는 선형의 상관관계가 있었으며, 이로부터 음향방출법을 이용한 리튬이온전지 열화 평가 가능성을 제안하였다.

• 한국표면공학회지
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• 제47권2호
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• pp.75-80
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• 2014

Nanocrystalline diamond(NCD) films on steel(SKH51) has been investigated using SiC interlayer film. SiC was deposited on SKH51 or Si wafer by RF magnetron sputter. NCD was deposited on SiC at $600^{\circ}C$ for 0.5~4 h employing microwave plasma CVD. Film morphology was observed by FESEM and FIB. Film adherence was examined by Rockwell C adhesion test. The growth rate of NCD on SiC/Si substrate was much higher than that on SiC/SKH51. During particle coalescence, NCD growth rate was slow since overall rate was determined by the diffusion of carbon on SiC surface. After completion of particle coalescence, NCD growth became faster with the reaction of carbon on NCD film controlling the whole process. In the case of SiC/SKH51 substrate, a complete NCD film was not formed even after 4 h of deposition. The adhesion test of NCD/SiC/SKH51 samples revealed a delamination of film whereas that of SiC/SKH51 showed a good adhesion. Many voids of less than 0.1 ${\mu}m$ were detected on NCD/SiC interface. These voids were believed as the reason for the poor adhesion between NCD and SiC films. The origin of voids was due to the insufficient coalescence of diamond particles on SiC surface in the early stage of deposition.

• Steel and Composite Structures
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• 제23권6호
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• pp.727-736
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• 2017

The application of carbon fiber reinforced polymer (CFRP) in steel structures primarily includes two categories, i.e., the bond-critical application and the contact-critical application. Debonding failure and buckling failure are the main failure modes for these two applications. Conventional electrometric techniques may not provide precise results because of the limitations associated with single-point contact measurements. A nondestructive full-field measurement technique is a valuable alternative to conventional methods. In this study, the digital image correlation (DIC) technique was adopted to investigate the bond behavior and buckling behavior of CFRP-steel composite members. The CFRP-to-steel bonded joint and the CFRP-strengthened square hollow section (SHS) steel column were tested to verify the suitability of the DIC technique. The stereo-DIC technique was utilized to measure continuous deformation. The bond-slip relationship of the CFRP-to-steel interface was derived using the DIC data. Additionally, a multi-camera DIC system consisting of four stereo-DIC subsystems was proposed and applied to the compressive test of CFRP-strengthened SHS steel column. The precise buckling location and CFRP delamination of the CFRP-strengthened SHS steel column were identified. The experimental results confirm that the stereo-DIC technique can provide effective measurements for investigating the behaviors of CFRP-steel composite members.

• Composites Research
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• 제34권3호
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• pp.174-179
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• 2021

유체 이송에 사용되는 강재 파이프는 신설과 도장, 또는 부식과 노후화로 인한 제반 시설 보수에 거대한 규모의 시간과 비용이 요구된다. 이에 본 연구에서는 강재 파이프의 대체재로, 내부식성과 내화학성이 우수한 탄소섬유강화복합재료(Carbon Fiber Reinforced Plastic, CFRP) 파이프 구조의 최적화 설계를 수행하였다. 헬리컬 패턴 표면에 후프 패턴을 혼합적층하여 내구성을 향상시켰으며, 수분 환경에서의 에폭시 흡습 현상을 억제하기 위해, 할로이사이트 나노튜브(Halloysite Nanotube, HNT)를 첨가하였다. HNT/CFRP 파이프는 필라멘트 와인딩 공정으로 제작하였으며, 기계적 물성 시험과 70℃ 고온 증류수 환경하에서 흡습 시험을 진행하였다. 그 결과, 파이프 두께의 0.6%에 해당하는 후프 패턴의 적층 시, 가장 우수한 물성을 나타냈다. 또한 0.5 wt.% HNT 첨가 시 상대적으로 높은 내흡습성을 가졌으며, 층간 계면에서의 박리 현상이 지연되어 가장 낮은 강도 저하율을 보였다.

• Tribology and Lubricants
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• 제37권6호
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• pp.240-245
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• 2021

Ceramic coatings with high hardness and excellent chemical stability have been successfully applied to various machine elements, tools, and implants. However, in the case of monolayer coating on soft substrates, a high-stress concentration at the interface between the coating and the substrate causes delamination of the coating layer. Recently, to overcome this problem, multilayer coatings with a metal layer with a low modulus of elasticity added between the ceramic and the substrate have been widely applied. This study presents the third part of a recent study and focuses on the effect of the number of coating layers on the Brinell hardness of multilayered coating with TiN/Ti, following the two previous studies on a new Brinell hardness test method for a coated surface and on the influence of substrate and coating thickness. Indentation analyses are performed using finite element analysis software, von Mises stress and equivalent plastic strain distributions, load-displacement curves, and residual indentation shapes are presented. The number of TiN/Ti layers considerably affect the stress distributions and indentation shapes. Moreover, the greater the number of TiN/Ti layers, the higher is the Brinell hardness. The stress and plastic strain distributions confirm that the multilayer coatings improve the wear resistance. The results are expected to be used to design and evaluate various coating systems, and additional study is required.

• 풍력에너지저널
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• 제14권3호
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• pp.83-90
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• 2023

The purpose of this study is to evaluate the inter-laminar fracture toughness characteristics of CFRP pultrusion spar cap materials reinforced with non-woven glass fabric. Test specimens were fabricated by the infusion technique. A non-woven glass fabric and artificial defects were embedded on the middle surface between two pultruded CFRP panels. Double cantilever beam (DCB) and End Notched Flexure (ENF) tests were performed according to ASTM standards. Fracture toughness and crack propagation characteristics were evaluated with load-displacement curves and delamination resistance curves (R-Curve). The fracture toughness results were calculated by compliance calibration (CC) method. The initiation and propagation values of Mode-I critical strain energy release rate value G_Ic were 1.357 kJ/m2 and 1.397 kJ/m2, respectively, and Mode-II critical strain energy release rate values G_IIc were 4.053 kJ/m2 for non-precracked test and 4.547 kJ/m2 for precracked test. It was found that the fracture toughness properties of the CFRP pultrusion spar-cap are influenced by the interface between the layers of CFRP and glass fiber non-woven.