• Journal of Welding and Joining
• /
• 제33권1호
• /
• pp.41-48
• /
• 2015

In this study, the effect of heat input on weld metal microstructure and the effects of dissimilar weld heat affected zone in quenched and tempered ASTM A517 on the stainless steel AISI 316L is investigated through the optimization of welding parameters. For this purpose, two welding techniques are used, tungsten-conventional gas and pulsed gas with weld wire ER 309MoL with Diameter 2.4 mm. Research showed that the grain size of the heat affected zone in pulsed welding is less compared with conventional welding; weld metal structure is fully austenitic, it has a finer structure in the pulsed method. Additionally, the growth of weld metal adjacent steel A517 is different from steel 316L. Further, investigation showed that the rate of dilution is less in the pulsed method and the impact energy is increased in each three regions of the weld metal and heat affected zones in the pulsed method; the fracture in the weld metal and heat affected zone of steel 316L is quite soft and it is semi-crispy in the heat affected zone of steel A517.

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

• 한국전산구조공학회:학술대회논문집
• /
• 한국전산구조공학회 2007년도 정기 학술대회 논문집
• /
• pp.487-492
• /
• 2007

The enhancement of the service life of damaged or cracked structures is a major issue for researchers and engineers. The hierarchical void element with the integrals of Legend polynomials is used to characterize the fracture behavior of unpatched crack as well as repaired crack with bonded composite patches by computing the stress intensity factors and stress contours at the crack tip. The numerical approach is based on the v-version degenerate shell element including the theory of anisotropic laminated composites. Since the equivalent single layer approach is adopted in this study, the proposed element is necessary to represent a discontinuous crack part as a continuum body with zero stiffness of materials. Thus the aspect ratio of this element to represent the crack should be extremely slender. The sensitivity of numerical solution with respect to energy release rate, displacement and stress has been tested to show the robustness of hierarchical void element as the aspect ratio is increased up to 2000. The stiffness derivative method and displacement extrapolation method have been applied to calculate the stress intensity factors of Mode I problem.

• Steel and Composite Structures
• /
• 제39권5호
• /
• pp.543-564
• /
• 2021

In this study free vibration analysis of a cracked Goland composite wing is investigated. The wing is modelled as a cantilevered beam based on Euler- Bernoulli equations. Also, composite material is modelled based on lamina fiber-reinforced. Edge crack is modelled by additional boundary conditions and local flexibility matrix in crack location, Castigliano's theorem and energy release rate formulation. Governing differential equations are extracted by Hamilton's principle. Using the separation of variables method, general solution in the normalized form for bending and torsion deflection is achieved then expressions for the cross-sectional rotation, the bending moment, the shear force and the torsional moment for the cantilevered beam are obtained. The cracked beam is modelled by separation of beam into two interconnected intact beams. Free vibration analysis of the beam is performed by applying boundary conditions at the fixed end, the free end, continuity conditions in the crack location of the beam and dynamic stiffness matrix determinant. Also, the effects of various parameters such as length and location of crack and fiber angle on natural frequencies and mode shapes are studied. Modal analysis results illustrate that natural frequencies and mode shapes are affected by depth and location of edge crack and coupling parameter.

• 한국재료학회지
• /
• 제31권5호
• /
• pp.255-263
• /
• 2021

P91 steel has been a highly researched material because of its applicability for high-temperature applications. Considerable efforts have been made to produce experimental creep data and develop models for creep life prediction. As creep tests are expensive and difficult to conduct, it is vital to develop authenticated empirical methods from experimental results that can be utilized for better understanding of creep behavior and can be incorporated into computational models for reliable prediction of creep life. In this research, a series of creep rupture tests are performed on the P91 specimens within a stress range of 155 MPa to 200 MPa and temperature range of 640 ℃ (913 K) to 675 ℃ (948 K). The microstructure, hardness, and fracture surfaces of the specimens are investigated. To analyze the results of the creep rupture tests at a macro level, a parameter called creep work density is derived. Then, the relationships between various creep parameters such as strain, strain rate, time to rupture, creep damage tolerance factor, and creep work density are investigated, and various empirical equations are obtained.

• 한국안전학회지
• /
• 제38권2호
• /
• pp.1-7
• /
• 2023

Fiber-metal laminates (FMLs) and polymer matrix composites (PMCs) are formed in various ways. In particular, FMLs in which aluminum is laminated as a reinforced layer are widely used. Also, glass fiber-reinforced plastics (GFRPs) are generally applied as fiber laminates. The bonding interface layer between the aluminum and fiber laminate exhibits low strength when subjected to hot press fabrication in the event of delamination fracture at the interface. This study presents a simple method for strengthening the interface bonding between the aluminum metal and GFRP layer of FML composites. The surfaces of the aluminum interface layer are engraved with three kinds of patterns by using the laser machine before the hot press works. Furthermore, the effect of the laser patterns on the interfacial toughness is investigated. The interfacial toughness was evaluated by the energy release rate (G) using an asymmetric double cantilever bending specimen (ADCB). From the experimental results, it was shown that the strip type pattern (STP) has the most proper pattern shape in GFRP/Al FML composites. Therefore, this will be considered a useful method for the safety assessment of FML composite structures.

• 폴리머
• /
• 제27권3호
• /
• pp.183-188
• /
• 2003

유전체 분광계를 사용하여 불소함유 에폭시 수지, 벤조트리플루오라이드의 다이글리시딜 에테르(FER)/다이아미노다이페닐메탄 (DDM)과 비스페놀 A의 다이글리시딜 에테르 (DGEBA)DDM 시스템의 유전상수를 측정하였으며, DMA와 TGA에 의한 열분석을 통하여 유리 전이 온도 및 열분해 개시온도, 최대 무게 감량시 온도, 그리고 분해 활성화 에너지 등 열안정성 인자를 고찰하였다. 경화된 시편의 기계적 물성은 파괴 인성, 굴곡강도 및 충격강도 실험을 통하여 알아보았으며, 주사전자 현미경을 사용하여 시편의 파단 특성을 조사하였다. 실험 결과, DGEBA/DDM 시스템에 비해 FER/DDM 시스템은 낮은 유전 상수를 나타내었으며, 경화된 시편의 기계적 물성은 높은 값을 나타내었다. 이는 trifluoromethyl (CF$_3$) 기의 도입으로 인하여 전기적 특성과 기계적 물성이 증가한 것으로 사료된다.

• 대한토목학회논문집
• /
• 제13권5호
• /
• pp.19-27
• /
• 1993

파괴역학에서 최근의 연구들은 균열체의 강도를 해석함에 있어서 균열선단 주위의 탄성 에너지 해방용, 균열확장력 그리고 응력장의 특성 등에 대한 지식을 요구하고 있다. 이런 연구들의 주안점은 에너지율, 응력장 그리고 탄성이방성체의 여러가지 경우들을 설명하는 데 있다. 철근콘크리트, 목재, 박층구조 그리고 각각의 방향으로 성질을 가지는 탄성체들은 대부분 직교이방성이다. 본 연구에서는 균열선단에 특이요소를 사용하고 균열선단 부근에서 아주 세밀한 요소를 사용하여 직교이방성 탄성체의 응력확대계수를 결정 하였다. 본 연구에서 응력확대계수를 구하기 위해 변위상관법을 사용하였으며 타 논문의 결과와 잘 일치함을 알 수 있었다.

• 한국전산구조공학회논문집
• /
• 제15권3호
• /
• pp.389-398
• /
• 2002

동전모양의 균열이 이상복합 실린더 계면에 존재하는 혼합모드 조건(I, II)에 대해 유한요소법을 사용하여 에너지해방율을 구하였다. 두재료의 탄성비와 노치율을 변화시켜 상업용 FEM 프로그램인 ABAQUS로부터 얻은 결과를 가상 균열법과 J 적분법에 적용하였으며 에너지해방율을 구하여 무차원함수로 표현하였다. 모드 II의 무차원 에너지해방율($\sqrt{G_{II}E^*}/\sqrt[p]{\pi a}$)은 균열길이와 탄성비가 증가되면서 그 값이 증가됨을 알수 있었다. 반면, 모드 I의 무차원 에너지해방율($\sqrt{G_{I}E^*}/\sqrt[p]{\pi a}$)은 탄성비가 증가하면서 그 값이 감소하며, 두재료의 탄성비가 3 이상인 경우에 균열길이가 증가되면서 무차원 에너지해방율이 감소하다가 다시 증가하게 나타났다. 또한 수치해석된 결과치를 무한판 실린더의 응력확대계수에 대한 정해와 비교하여 본 해석의 신뢰성을 확보하였다.

• Composites Research
• /
• 제36권6호
• /
• pp.388-394
• /
• 2023

복합재료 제조 시 수지의 함침성을 높이는 것은 제조 공정속도와 제품의 품질을 향상시키는 핵심 방법이다. 수지 개선은 중요하지만, 간단한 섬유 표면 처리로도 수지의 흐름성을 개선할 수 있다. 본 연구에서는 탄소섬유 직물에 다양한 플라즈마 처리 시간을 적용함으로써 수지와 섬유 간의 함침성을 향상하게 하였다. 플라즈마 처리에 따라 변화된 섬유 내 수지의 분산을 평가하기 위해 전기저항 측정법을 사용했다. 섬유 표면처리가 수지 함침성에 미치는 영향을 실시간으로 관찰할 수 있었다. 수지에 탄소섬유 토우를 삽입할 때 토우에 스며든 수지의 양을 측정하여 수지 함침성을 객관적으로 비교하였다. 5분 동안의 플라즈마 처리로 복합재료의 인장과 압축 강도가 50% 이상 향상되었으며, 보이드 함유율을 감소시키고 소화점 임계열류량을 증가시켰다. 마지막으로 건축용 복합재료 부품으로 사용되는 일부분을 활용하여 동적 굴곡피로시험을 실시했고, 3 kN하중 백만 회에도 복합재료 부품은 파손되지 않았다.