• 한국표면공학회지
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• 제32권6호
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• pp.647-657
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• 1999

Due to the inherently poor adhesion strength of Cu-based leadframe/EMC (Epoxy Molding Compound) interface, popcorn cracking of thin plastic packages frequently occurs during the solder reflow process. In the present work, in order to enhance the adhesion strength of Cu-based leadframe/EMC interface, black-oxide layer was formed on the leadframe surface by chemical oxidation of leadframe, and then oxidized leadframe sheets were molded with EMC and machined to form SDCB (Sandwiched Double-Cantilever Beam) and SBN (Sandwiched Brazil-Nut) specimens. SDCB and SBN specimens were designed to measure the adhesion strength between leadframe and EMC in terms of critical energy-release rate under quasi-Mode I ($G_{IC}$ ) and mixed Mode loading ($G_{C}$ /) conditions, respectively. Results showed that black-oxide treatment of Cu-based leadframe initially introduced pebble-like X$C_2$O crystals with smooth facets on its surface, and after the full growth of $Cu_2$O layer, acicular CuO crystals were formed atop of the $Cu_2$O layer. According to the result of SDCB test, $Cu_2$O crystals on the leadframe surface did not increase ($G_{IC}$), however, acicular CuO crystals on the $Cu_2$O layer enhanced $G_{IC}$ considerably. The main reason for the adhesion improvement seems to be associated with the adhesion of CuO to EMC by mechanical interlocking mechanism. On the other hand, as the Mode II component increased, $G_{C}$ was increased, and when the phase angle was -34$^{\circ}$, crack Kinking into EMC was occured.d.

• 한국세라믹학회지
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• 제35권12호
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• pp.1316-1322
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• 1998

The amount of VC and C/N ratio in Ti(CN) was varied to investigate the effect of VC addition on the mi-crostructural change in Ti(CN)-Ni system. As the amount of VC addition increases in Ti(C0.7N0.3)-20Ni sys-tem a complete solid solution was observed in Ti(C0.7N0.3)-20Ni-25VC system. It implies that the ratio of the dissolution rates of Ti(C0.7N0.3)to that of VC is nearly 2:1 at the sintering conditions used in this study. It was found from the experiments that the system composed of the Ti(C0.7N0.3) phase exhibits a rimless structure and relatively small amount of solid solution. That is among Ti(C0.7N0.3) phase exhibits a rimless structure and relatively small amount of solid solution. This is among Ti(C1-xNx) phases the dissolution rate of Ti(C0.3N0.7) is the lowest. Also fracture toughness(KIC) of the cermet was measured by indentation method. Attentions were paid to crack propagation path to look for a dominant fracture mode and to cor-relate it with fracture toughness values. The fracture toughness was relatively high with the addition of VC content. But the addition of a large VC content reduced the overall toughness of the cermet. This result is explained with the difference in fracture mode.

• 한국콘크리트학회:학술대회논문집
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• 한국콘크리트학회 2008년도 춘계 학술발표회 제20권1호
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• pp.165-168
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• 2008

본 연구에서는 철근콘크리트 구조물의 보강에 이용되는 유리섬유강화 복합재료(Glass Fiber Reinforced Polymer, GFRP) 형상에 관한 연구로서 콘크리트의 피복두께 및 FRP 보강재의 형상(Plate, Box)을 실험 변수로 하여 FRP 보강 철근콘크리트 보의 거동 평가 관한 연구를 수행하였다. 이를 위하여 본 연구에서는 T. J. Teng 등이 제안한 설계식을 이용하여 보강량을 결정하였고 기존의 FRP Plate 보강재의 성능개선을 위하여 FRP Sandwich box 보강재를 설계, 적용하여 보았다. 연구의 결과 예상과 달리 FRP Plate 보강재가 Sandwich box 보강재보다 보강효과가 우수한 것으로 조사되었으며, 이는 보강재 제작상의 한계점 및 core 재료가 너무 약하여 Sandwich box 보강재의 Top Plate와 Bottom Plate가 일체화 거동을 하지 못하여 나타난 결과로 사료된다.

• 한국안전학회지
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• 제34권6호
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• pp.1-6
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• 2019

Carbon fiber has excellent specific strength, corrosion resistance and heat resistance. And p-Aramid fiber has high toughness and heat resistance and high elasticity, and is used in various fields such as industrial protective materials, bulletproof helmets and vests, as well as industrial fields. However, carbon fiber is relatively expensive, and is susceptible to brittle fracture behavior due to its low fracture strain. On the other hand, the aramid fiber tends to decrease in elastic modulus and strength when applied to the epoxy matrix, but it is inexpensive and has higher elongation and fracture toughness than carbon fiber. Thus the twill hybrid carbonaramid fiber reinforced composite laminate composite was investigated for a delamination fracture toughness under Mode I loading by 2 kinds of MBT and MCC deduction. The specimen was fabricated with 20 hybrid fabric plies. The initial crack was made by inserting the teflon tape in the center plane with a₀/W=0.5 length. The results show that SERR(Strain Energy Release Rate) as the critical and stable delamination fracture toughness were 0.09 kJ/㎡, 0.386 kJ/㎡ by MBT deduction, and 0.192 kJ/㎡, 0.67 kJ/㎡ by MCC deduction, respectively.

• Geomechanics and Engineering
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• 제17권4호
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• pp.323-331
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• 2019

The presence of defects in nature changes the physical parameters of the rock. In this paper, by studying the rock-like specimens with conjugated fractures, the horizontal angle and length are changed, and the physical parameters and failure modes of the specimens under uniaxial compression test are analyzed and compared with the results of simulation analysis. The experimental results show that the peak strength and failure mode of the rock-like specimens are closely related to the horizontal angle. When the horizontal angle is $45^{\circ}$, the maximum value is reached and the tensile failure mode is obtained. The fracture length affects the germination and propagation path of the cracks. It is of great significance to study the failure modes and mechanical properties of conjugated fracture rock-like specimens to guide the support of fractured rock on site.

• Structural Engineering and Mechanics
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• 제86권3호
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• pp.417-430
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• 2023

As the key part in the reinforced concrete column-steel beam (RCS) frame, the beam-column joints are usually subjected the axial force, shear force and bending moment under seismic actions. With the aim to study the seismic behavior of RCS joints with and without RC slab, the quasi-static cyclic tests results, including hysteretic curves, slab crack development, failure mode, strain distributions, etc. were discussed in detail. It is shown that the composite action between steel beam and RC slab can significantly enhance the initial stiffness and loading capacity, but lead to a changing of the failure mode from beam flexural failure to the joint shear failure. Based on the analysis of shear failure mechanism, the calculation formula accounting for the influence of RC slab was proposed to estimate shear strength of RCS joint. In addition, the finite element model (FEM) was developed by ABAQUS and a series of parametric analysis model with RC slab was conducted to investigate the influence of the face plates thickness, slab reinforcement diameter, beam web strength and inner concrete strength on the shear strength of joints. Finally, the proposed formula in this paper is verified by the experiment and FEM parametric analysis results.

• 한국강구조학회 논문집
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• 제24권4호
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• pp.399-410
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• 2012

본 연구에서는 실험적 모드해석 기법을 이용하여 캔틸레버 및 양단고정 직사각형 적층복합판의 동적 테스트가 수행되었다. 균열 성장으로 인한 손상평가를 위하여 적층복합판에 인위적인 단계별 손상(균열)을 가하였으며, 충격해머 모드실험에 의해 얻어진 주파수응답함수(FRF), MAC(Modal Assurance Criterion) 값 및 모드매개변수(진동수, 모드형상, 감쇠비)의 변화를 분석하였다. 각 단계별 손상에 대한 적층복합판의 실험적 모드매개변수를 검증하기 위하여 유한요소해석으로부터 구한 고유진동수와 모드형상을 비교하였다. 손상은 벤치마크로서의 유한요소모델을 보정하는 과정으로부터 얻게 되는 적층복합판의 기하학적 특성 및 구조적 거동의 변화를 통하여 평가될 수 있음을 보여주었다.

• 터널과지하공간
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• 제11권4호
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• pp.352-361
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• 2001

저온 냉각상태 및 냉각 후 상온 해빙 상태에서 암석의 모드 I 파괴인성을 BDT와 CCNBD시험편을 사용하여 구하였다. 실험 온도 범위는 상온($25^{\circ}C$)에서 -16$0^{\circ}C$로 설정하였으며 건조 및 포화된 화강암과 사암을 사용하여 파괴인성에 대한 공극수와 공극률의 영향 정도를 조사하고자 하였다. 또한 냉각 과정에서 발생할 수 있는 열균열을 조사하기 위해서 SEM 이미지 분석도 실시하였다. 냉각된 암석의 파괴인성은 온도가 하강함에 따라 증가하였다. 이러한 증가경향은 포화시료에서 더 크게 나타났으며, 포화 시료의 경우 화강암의 증가율이 사암에 비해 크게 나타났다. 냉각 후 상온 해빙 상태에서 구한 파괴인성의 경우, 냉각을 거 치지 않은 상온 상태의 파괴인성 값의 15% 이내에서 결정되었다. 냉각-해빙을 거친 시료에 대한 SEM 분석결과 화강암의 경우 조암광물간의 열팽창 차이에 의한 열균열을 확인할 수 있었으며 냉각온도가 낮을수록 균열밀도가 증가하였다.

• 마이크로전자및패키징학회지
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• 제14권2호
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• pp.35-40
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• 2007

Sn-8Zn-3Bi 무연 솔더 페이스트의 접합부신뢰성 및 적합성을 평가하기 위해 유(SnPb) 무연(Sn, SnBi)도금된 Cu 리드프레임 QFP(Quad Flat Packager)를 사용하여 열충격 조건 하에서의 인장 강도의 변화 및 파괴 기구에 대한 분석을 실시하였다. 리드 도금의 종류에 상관없이 모든 시험 시편에서 열충격 사이클 수의 증가에 비례하여 접합부의 취성 특성이 강화되어 인장 강도가 감소하는 것을 확인하였다. 하지만, 접합부에는 열팽창 계수의 차이에 의해 야기될 수 있는 미세 균열은 발견되지 않았다. 단면 관찰 및 변위 이력 곡선 분석을 통하여 열충격 사이클 수의 증가에 따른 인강 강도의 감소는 접합부의 파괴 기구의 변화에 기인되었음을 확인하였다. 본 실험을 통해 Sn-3Zn-3Bi 솔더의 유 무연 도금 Cu 리드프레임과의 우수한 작업 특성과 열충격 환경 하에서도 우수한 기계적 접합 특성을 유지하는 것을 확인할 수 있었다.

• Carbon letters
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• 제6권2호
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• pp.106-110
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• 2005

In this work, the effects of atmospheric oxygen plasma treatment of carbon fibers on mechanical interfacial properties of carbon fibers-reinforced epoxy matrix composites was studied. The surface properties of the carbon fibers were determined by acid/base values, Fourier-transform infrared spectrometer (FT-IR), and X-ray photoelectron spectroscopy (XPS) analyses. Also, the crack resistance properties of the composites were investigated in critical stress intensity factor ($K_{IC}$), and critical strain energy release rate mode II ($G_{IIC}$) measurements. As experimental results, FT-IR of the carbon fibers showed that the carboxyl/ester groups (C=O) at 1632 $cm^{-1}$ and hydroxyl group (O-H) at 3450 $cm^{-1}$ were observed for the plasma treated carbon fibers, and the treated carbon fibers had the higher O-H peak intensity than that of the untreated ones. The XPS results also indicated that the $O_{1S}/C_{1S}$ ratio of the carbon fiber surfaces treated by the oxygen plasma led to development of oxygen-containing functional groups. The mechanical interfacial properties of the composites, including $K_{IC}$ (critical stress intensity factor) and $G_{IIC}$ (critical strain energy release rate mode II), were also improved for the oxygen plasma-treated carbon fibersreinforced composites. These results could be explained that the oxygen plasma treatment played an important role to increase interfacial adhesions between carbon fibers and epoxy matrix resins in our composite system.