• Title/Summary/Keyword: 3점 굽힘

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Cu Thickness Effects on Bonding Characteristics in Cu-Cu Direct Bonds (Cu 두께에 따른 Cu-Cu 열 압착 웨이퍼 접합부의 접합 특성 평가)

  • Kim, Jae-Won;Jeong, Myeong-Hyeok;Carmak, Erkan;Kim, Bioh;Matthias, Thorsten;Lee, Hak-Joo;Hyun, Seung-Min;Park, Young-Bae
    • Journal of the Microelectronics and Packaging Society
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    • v.17 no.4
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    • pp.61-66
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    • 2010
  • Cu-Cu thermo-compression bonding process was successfully developed as functions of the deposited Cu thickness and $Ar+H_2$ forming gas annealing conditions before and after bonding step in order to find the low temperature bonding conditions of 3-D integrated technology where the interfacial toughness was measured by 4-point bending test. Pre-annealing with $Ar+H_2$ gas at $300^{\circ}C$ is effective to achieve enough interfacial adhesion energy irrespective of Cu film thickness. Successful Cu-Cu bonding process achieved in this study results in delamination at $Ta/SiO_2$ interface rather than Cu/Cu interface.

Evaluation of strength according to surface abrasion of lithium disilicate glass ceramic by 3-point bending strength test (3점 굽힘강도 시험을 통한 Lithium disilicate glass ceramic의 표면 연마 정도에 따른 강도 평가)

  • Lee, Ha-Na;Kim, Eo-Bin;Kang, Seen-Young;Lee, Kyung-Eun;Kim, Ji-Hwan;Kim, Woong-Chul
    • Journal of Technologic Dentistry
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    • v.40 no.1
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    • pp.9-15
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    • 2018
  • Purpose: The purpose of this study is to investigate the effect of lithium disilicate glass ceramic polishing on the strength of the final prosthesis. Methods: Fourteen lithium disilicate glass ceramic specimens were prepared. These were randomly divided into two groups of seven(LPG: low polishing group, HPG: high polishing group). In LPG, SiC paper was sequentially polished using 300, 600, 800, 1000 grit, and the specifications of the test piece were adjusted. HPG was sequentially polished using 300, 600, 800, 1000, 1200, 1500, and 2000 grit. Two groups of specimens are executed 3- point bending test. Using the statistical program SPSS 22.0, the average values of the strengths of the two groups were compared in the Mann-Whiteney test. The significance level was set at 0.05. Results: The mean strength value of HPG was measured at $307.14{\pm}23.28MPa$ significantly higher than LPG(p<0.001). Conclusion : The final polishing of the prosthesis is aesthetically important but has proven to play an important role in the flexural strength, early fracture, and prolongation of the prosthesis.

Bonding Strength Evaluation of Copper Bonding Using Copper Nitride Layer (구리 질화막을 이용한 구리 접합 구조의 접합강도 연구)

  • Seo, Hankyeol;Park, Haesung;Kim, Gahui;Park, Young-Bae;Kim, Sarah Eunkyung
    • Journal of the Microelectronics and Packaging Society
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    • v.27 no.3
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    • pp.55-60
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    • 2020
  • The recent semiconductor packaging technology is evolving into a high-performance system-in-packaging (SIP) structure, and copper-to-copper bonding process becomes an important core technology to realize SIP. Copper-to-copper bonding process faces challenges such as copper oxidation and high temperature and high pressure process conditions. In this study, the bonding interface quality of low-temperature copper-to-copper bonding using a two-step plasma treatment was investigated through quantitative bonding strength measurements. Our two-step plasma treatment formed copper nitride layer on copper surface which enables low-temperature copper bonding. The bonding strength was evaluated by the four-point bending test method and the shear test method, and the average bonding shear strength was 30.40 MPa, showing that the copper-to-copper bonding process using a two-step plasma process had excellent bonding strength.

Estimation of Fatigue Crack Growth Behavior of Cracked Specimen Under Mixed-mode Loads (혼합모드 하중을 받는 균열시편의 피로균열진전거동 평가)

  • Han, Jeong Woo;Woo, Eun Taek;Han, Seung Ho
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.39 no.7
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    • pp.693-700
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    • 2015
  • To estimate the fatigue crack propagation behavior of compact tension shear (CTS) specimen under mixed-mode loads, crack path prediction theories and Tanaka's equation were applied. The stress intensity factor at a newly created crack tip was calculated using a finite element method via ANSYS, and the crack path and crack increment were then obtained from the crack path prediction theories, Tanaka's equation, and the Paris' equation, which were preprogrammed in Microsoft Excel. A new method called the finite element crack tip updating method (FECTUM) was developed. In this method, the finite element method and Microsoft Excel are used to calculate the stress intensity factors and the crack path, respectively, at the crack tip per each crack increment. The developed FECTUM was applied to simulate the fatigue crack propagation of a single-edge notched bending (SENB) specimen under eccentric three-point bending loads. The results showed that the number of cycles to failure of the specimen obtained experimentally and numerically were in good agreement within an error range of less than 3%.

Acoustic Emission during Crack Propagation Process of Rubber-Modified Epoxy Resin (고무변성 에폭시 수지의 균열진전과정과 음향방출 특성)

  • 이덕보;김현수;최낙삼;남기우;문창권
    • Composites Research
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    • v.16 no.4
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    • pp.44-50
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    • 2003
  • The damage zone around a crack tip occurring before the fracture is a significant domain. which affects the toughening mechanism of materials. In this study. the growth process of damage zone in the vicinity of crack tip for rubber-modified epoxy resin is investigated using an acoustic emission(AE) analysis. The weight fractions of rubber(CTBN 1300$\times$B) in rubber-modified epoxy resin are 5 wt% and 15 wt%. The fracture toughness($K_{IC}$) and the fracture energy($G_{IC}$) were measured using 3 point bending single-edge notched specimens. The damage zone and rubber particles distributed around the crack tip were observed by a polarized optical microscope and an atomic force microscope(AFM). The damage zone around crack tip of rubber-modified epoxy resin was formed at 13 % loading and developed until 57 % loading of the fracture load. The crack initiated at 57 % loading grew repeatedly in the stick-slip propagation behavior. Based on time-frequency analysis, it was confirmed that AE signals with frequency bands of 0.15~0.20 MHz and 0.20~0.30 MHz were generated from cavitation and stable/unstable cracking inside the damage zone.

A Study of Mode II Interlaminar Fracture for CFRP Laminate Composite using the 4-point Bending CNF Specimen (4점굽힘 CNF 시험편을 이용한 CFRP적층 복합재 모드 II 층간파괴)

  • Kwon, Oh-Heon;Kang, Ji-Woong;Tae, Hwan-Jun;Hwang, Yeong-Yeun;Yun, Yu-Seung
    • Journal of the Korean Society of Safety
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    • v.25 no.3
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    • pp.34-39
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    • 2010
  • Unidirectional Carbon Fiber Reinforced Plastics (CFRP) are advanced materials which combine the characteristics of the light weight, high stiffness and strength. For those reasons, the use of the unidirectional CFRP has increased in jet fighters, aerospace structures. However, unidirectional CFRP composites have a lot of problems, especially delamination, compared with traditional materials such as steels and aluminums, and so forth. Therefore, the interlaminar fracture toughness for a laminate CFRP composite is very important. In this study, The mode II interlaminar fracture toughness was measured by using center notched flexure(CNF) test specimen. The CNF specimens using unidirectional carbon prepreg were fabricated by a hot-press with the gage pressure and temperature controller. And three kinds of a/L ratio was applied to these specimens. Here, we discuss the relations of the crack growth and the mode II interlaminar fracture under the four point bending CNF test. From the results, we shows that mode II interlaminar was occurred when the more $a_0$/L ratio, the less load. And $G_{IIC}$ also were obtained as 5.33, 2.9 and $0.58kJ/m^2$ according to $a_0$/L ratio=0.2, 0.3 and 0.4.

The Effect of Abnormal Intermetallic Compounds Growth at Component on Board Level Mechanical Reliability (컴포넌트에서의 비정상적인 금속간화합물 성장이 보드 레벨 기계적 신뢰성에 미치는 영향)

  • Choi, Jae-Hoon;Ham, Hyon-Jeong;Hwang, Jae-Seon;Kim, Yong-Hyun;Lee, Dong-Chun;Moon, Jeom-Ju
    • Journal of the Microelectronics and Packaging Society
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    • v.15 no.2
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    • pp.47-54
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    • 2008
  • In this paper, we studied how and why did abnormal IMC growth at component affect on board level mechanical reliability. First, interfacial reactions between Sn2.5Ag0.5Cu solder and electrolytic Ni/Au UBM of component side were investigated with reflow times and thermal aging time. Also, to compare mechanical reliability of component level, shear energy was evaluated using the ball shear test conducted with variation of shear tip speed. Finally, to evaluate mechanical reliability of board level, we surface-mounted component fabricated with each condition on PCB side. After conducting of 3 point bending test and impact test, we confirmed solder joint crack mode using cross-sectioning and dye & pry penetration method.

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Fracture Behavior of Advanced Composite Material (첨단복합소재의 파괴거동)

  • 김윤해;김영식
    • Journal of Advanced Marine Engineering and Technology
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    • v.18 no.3
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    • pp.52-62
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    • 1994
  • 기계나 구조물 파괴의 대부분은 노치부를 기점으로 하여 발생하기 때문에 첨단복합재료를 노지부 재로서 안전하면서도 경제적으로 사용하기 위해서는 각종 조건하에 있어서 강도특성을 명확히 하는 것은 대단히 중요하다. 본 연구에서는 노치를 갖는 복합재료를 이용하여 각종조건하에서 강도특성평가실험을 행하였으 며, 얻어진 결과를 종합하면 다음과 같다. (1) 첨단복합재료 노치재는 試驗片의 幾可學的 形狀과는 관계없이 노치반경 p만에 의해 결정되는 최대탄성응력 $\sigma_{max}$일정의 條件下에서 破t짧된다. (2) 破斷時 최소단면에서의 공칭응력 $\sigma_{c}$와 응력집중계수 $K_{t}$와의 관계에 있어서,$\sigma_{c}$의 값이 $K_{t}$의 증대와 더불어 떨어지고 있는 부분과, $K_{t}$와 관계없이 거의 일정하게 되고 있는 부분으로 나누어지는 現象은 노치재의 回轉굽힘 또는 인장압축파열에서 보여지는 현상과 外觀上 對應하고 있다. 즉, 정적파괴와 피로파괴는 파괴의 양상이 비슷하다 (3) PEN수지단체의 경우, 피로균열발생은 점발생적 피로균열이 최대탄성응력에 의해 지배되며, 노치에 만감하며,균열전파수명은전수명에 비해 상당히 짧다. (4) 단탄소섬유강화복합재료의 경우, 피로균열은 섬유端에 응력이 집중하기 때문에 일반적으로 섬유端에서 아주 빠른 시기에 발생하지만, 섬유가 피로균열진전에 대해 방해물로 작용하기때문에 아주 천천히 전파한다. (5) 短탄소鐵維는 피로균열발생에 대해서는 負의 강화작용 전수명의 극히 초기단계에 피로균열 발생을, 피로균열전파에 대해서는 正의 강화작용을 한다. (6) 단탄소섬유를 PEN에 강화함으로 인해 정적강도 보다 피로강도에 더 큰 강화효과를 초래했으며, 선형노치역학의 개녀은 첨단 복합재료의 강도평가에 대단히 유효했다.

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KSTAR 진공용기 시작품 제작관련 기술분석

  • 조승연
    • Proceedings of the Korean Vacuum Society Conference
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    • 1999.07a
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    • pp.36-36
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    • 1999
  • 한국중공업(주)에서 수행한 KSTAR 진공용기 시작품 제작이 완성됨에 따라 제작과 관련된 종합기술을 분석하여 보았다. KSTAR 진공용기 시작품(그림1)은 전체의 1/4섹터인 90도 부분으로서 NBI(Neutral Beam Injection) 포트를 포함하는 45도 섹터와 축소포트(Reduced Port)를 포함하는 45도 섹터를 각각 먼저 제작한 후 두 부분을 용접하여 최종 시작품을 완성하였다. 용접은 SMAW법과 GTAW법 등 두가지 방법을 사용하였으며, 초기 용접시는 용접 면적이 작기 때문에 GTAW법을 이용하였고, 마무리 용접과 같이 용접 면적이 넓고 거친 부분에는 SMAW법을 이용하여 용접하였다. 모든 용접이 완전통과 용접이기 때문에 구조적 안전 면에서 좋으나, 진공측면에서는 다소 미흡한 점이 있다. 시작품은 상하 대칭구조로서 원통부분, 원형부분, 원추부분, 너클부분 (그림2) 등으로 나뉘어 지며 이중 원형품은 금형을 이용하여 성형하였고, 나머지 부분은 굽힘가공 후 절단적업을 하였다. 진공용기 조립은 안쪽과 바깥쪽 내벽부터 용접한 후 폴로이달 리브를 용접하고 외벽을 용접한다. 수평포트와 수직포트를 위해 스터브를 용접한 후 미리 용접해둔 NBI 포트 및 축소포트를 부착시켰다. 용접부위의 누설시험을 위한 방법으로, 용접주위 표면에서 개구하고 있는 홈에 적색 침투액을 침투시켜 침투 후 이 액을 홈의 개구로부터 빨아 내어 용접부위 표면상태에서 실제의 홈의 폭보다 확대한 홈의 지시모양으로 나타내게 하여 누설여부를 알기 쉽게 하는 액체 침투 탐상법을 적용하였다. 지시모양의 크기가 5mm 이상인 부분에 대해서는 재용접을 하였다. 누설 시험으로 초음파 탐상시험이 본제품 제작시 수행되어야 한다. 완성된 시작품에 대해 3군데의 위치에서 각각의 부분들이 용접되기 전과 후에 치수를 각각 측정하여 비교하였다. 또한 포트들에 대해서도 용접 전후 치수를 각각 측정하였다. 이러한 측정은 줄자를 사용하여 측정하였으므로 차 후 3차원 정밀 측정이 수반되어야 한다. 이상과 같이 시작품 제작을 통하여 문제점을 파악하고 개선책을 마련함으로서 향 후 KSTASR 진공용기 본 제품 제작할 때 반영코자 한다.

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Development of the Piecewisely-integrated Composite Bumper Beam Based on the IIHS Crash Analysis (IIHS 충격해석에 근거한 구간 조합 복합재료 범퍼 빔 개발)

  • Jeong, Chan-Hee;Ham, Seok-Wu;Kim, Gyeong-Seok;Cheon, Seong S.
    • Composites Research
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    • v.31 no.1
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    • pp.37-41
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    • 2018
  • The aim of the current work is to characterise a piecewisely-integrated composite bumper beam based on the IIHS bumper crash protocol. IIHS bumper crash FE analysis for an aluminium type bumper beam was carried out to get the information about the dominant loading types at several regions in the bumper beam during crash. In the meantime, robust stacking sequences against tension and compression have been searched for using FE analysis of a coupon type model. After determining most effective stacking sequences for tension and compression, three-point bending simulation was preliminarily carried out to investigate the combination performance of them. Finally, IIHS bumper crash FE analysis for the piecewisely-integrated composite bumper beam, which consisted of the combination of tension effective stacking sequence and compression efficacious stacking sequence, was conducted and the result was compared with other types of composite bumper beams. It was found that the newly suggested piecewisely-integrated composite bumper beam showed superior crashworthy behaviour to those of uni-modal stacking sequence composite bumper beams.