• 한국해양공학회:학술대회논문집
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• 한국해양공학회 2000년도 추계학술대회 논문집
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• pp.47-52
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• 2000

F.R.P specimens were made by mixture CM(chopped mat) 450-104 matrix & RC(roving clothes)570-100 Roving, the mixture ratio Resin: hardener (92:8) for tensile test. It was also made of plates by hand lay-up method and was been cured for 24 hours and then was cut tensile specimens in accordance with ASTM D638 Type 3. Knowing exact behavior of bonded area's stress and strain when the tensile test was going on, the test specimens were made of 2 plies laminae of F.R.P in each for supporting cut part in middle of specimen length. And in middle part also were covered of F.R.P plies of 1/2, 2/3 length of specimen in each as well. Also we consider shear stress in adhered area. This study reveals that as plys length is more longer, rupture stress grows remarkably larger.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2005년도 추계학술발표대회 논문집
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• pp.57-60
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• 2005

Composite-to-aluminum joins were tested to get failure loads and modes for three types of joins; adhesive bonding, bolt fastening, and adhesive-bolt hybrid joining. Film type adhesive FM73 and paste type adhesive Cytec EA9394S were used for aluminum and composite bonding to make a double-lap joint. A digital microscope camcorder was used to monitor the failure initiation and propagation. It was found that the hybrid joining is an effective method to strengthen the joint when the mechanical fastening is stronger than the bonding as in the case of using the paste type adhesive. On the contrary, when the strength of the bolted joint is lower than the strength of the bonded joint as in the joint with the film type adhesive, the bolt joining contribute little to the hybrid joint strength.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2004년도 추계학술발표대회 논문집
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• pp.78-82
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• 2004

The co-cured joint has been widely used in joining process of composite structures due to its simple and easy manufacturing process. In this paper, the effect of stacking sequence of the carbon epoxy prepreg, bonding length and thickness of the aluminum plate on the static tensile load capability of the co-cured aluminum-composite double lap joint were experimentally investigated. From experimental results, the optimum EA ratios with respect to stacking sequence and bonding length of the co-cured joint were obtained, which may be useful for the joining of hybrid structures.

• 대한기계학회논문집A
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• 제28권6호
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• pp.783-790
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• 2004

Adhesive-bonded joints are widely used in the industry. Recently, applications of adhesive bonding joints have been increased extensively in automobile and aircraft industry. The strength of adhesive joints is influenced by the surface roughness, adhesive shape, stress distribution, and etc. However, the magnitude of the influence has not yet been clarified because of the complexity of the phenomena. In this study, as the fundamental research of adhesive bonding joints, the effects of adhesive shape and loading speed on bonding strength properties and durability of aluminum to polycarbonate single-lap joints were studied. To evaluate the effect of adhesive shape, several modified shapes were used, and loading speeds were varied from 0.05 to 5 mm/min. As a result, the load-displacement distribution was shown a brittle fracture tendency. The trigonal edged single lap and bevelled lap joints showed the higher strength than the plain single lap, trigonal single lap, joggle lap and double lap joints in same adhesive area. The fractures of trigonal single lap and trigonal edged single lap joints that had the higher strength level were shown as the mixture type of the cohesive and interfacial-failure, mostly joggle lap joints that had the lower strength level were shown as the adhesive-failure.

• 한국항공우주학회지
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• 제41권3호
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• pp.194-200
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• 2013

복합재료 적층판 기계적 체결부 표준시험(ASTM D5961) 결과에 대하여 이론적 강도 계산 및 유한요소 해석결과를 비교한다. 응력집중계수를 산출하기 위하여 ASM Handbook의 금속 및 복합재료에 대한 산출식을 이용하여 실험 결과값과 비교한다. 형상학적 인자들과 체결방식(단일/이중 겹칩)에 따른 체결강도의 차이도 비교한다. 유한요소 해석에 있어, 복합재료 적층판의 기계적 체결부의 효율적인 유한요소 모델을 찾기 위해 몇 가지 유한요소 모델들과 실험 결과들을 비교한다.

• Composites Research
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• 제19권4호
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• pp.15-22
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• 2006

구조물 설계에 복합재료-금속 접착제 결합 조인트의 개발 및 사용을 제한하는 가장 큰 요인은 접착 조인트의 하중지지 능력 예측을 위한 접착 계면의 강도 평가 방법의 부재이다. 본 연구에서는 복합재료-탄소강의 접착 강도를 계면 모서리에서의 응력강도계수와 파괴 인성 값으로 평가하였다. 구체적으로 동시 경화 성형법으로 제작된 복합재료-탄소강 양면 겹치기 접착조인트의 하중지지 능력을 파괴 역학적 분석 방법을 통하여 결정하였다. 이종재료 계면 모서리 첨단의 응력 특이성과 그 지수를 제시하고 최종적으로 응력강도계수와 실험을 통한 계면의 파괴인성 값을 획득하였다. 서로 다른 접합 길이를 갖는 조인트의 하중지지 능력 비교를 통하여 양면 겹치기 접착 조인트의 파괴 인성치와 혼합 모드에서의 균열 진전 기준을 $K_1-K_{11}$ 평면 내에 도시하였다.

• Journal of the Korean Wood Science and Technology
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• 제46권1호
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• pp.85-92
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• 2018

소경각재를 이용한 소경각재 적층목을 기둥-보 목조건축 구조재로 이용하기 위해선 장대재 제작이 가능하여야 한다. 본 연구에서는 낙엽송 소경각재의 종접합 성능평가를 실시하였다. 시험편들은 종접합 방법에 따라 6가지 형상으로 제작하였으며 인장 및 휨 강도시험으로 종접합성능을 검토하였다. 종접합 접합부의 인장시험에서 Lap 시험편의 인장강도는 Double Lap 시험편보다 양호하였으며, Scarf 시험편의 인장강도는 Hooked scarf 시험편보다 양호하였다. Rod 시험편의 인장강도는 3.6 MPa로 가장 양호하였다. 종접합 접합부의 휨 시험결과 봉형 GFRP를 삽입 접착한 시험편들은 평균 29 MPa의 휨 파괴계수가 측정되었으며, 타 접합부 시험편들은 11 MPa 이하의 휨 파괴계수 값이 관찰되었다. 봉형 GFRP (Glass Fiber Reinforced Plastic)를 삽입 접착한 시험편들은 인성파괴가 관찰되었고 나머지 시험편들은 취성파괴가 발생하였다. Rod + Lap 시험편의 평균 휨 파괴계수가 30.5 MPa로 종접합한 시험편 중 가장 양호한 성능을 발휘하였다. Rod + Lap 시험편의 휨 강도는 종접합하지 않은 대조군 시험편 휨 파괴계수의 66%에 해당되었다. 낙엽송 소경각재 종접합 방법으로 봉형 GFRP 삽입 접착이 가장 유효한 강도를 나타내는 것을 확인하였다.

• 한국전기전자재료학회논문지
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• 제16권10호
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• pp.923-930
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• 2003

We jointed Bi(Pb)-Sr-Ca-Cu-O multifilament tapes and evaluated their electrical and mechanical properties. In order to improve connectivity of multifilaments, one or two single-filament tape was inserted between two multifilament tapes. The critical current ratio(CCR) and n-value of the jointed tapes were evaluated as a function of uniaxial pressure. It was observed that critical current ratio and n-value were 24.8-29.0% and 2.5-2.8 for MM lap-jointed tape. On the other hand, the corresponding values were improved to 24.7-53.9% and 3.1-4.2 for MSM jointed tape, and 63.4-76.0% and 3.4-5.1 for double MS:vr lap-jointed tape, respectively. The highest electrical properties of double MSM lap-jointed tape are considered to be owing to the presence of single core, causing better interconnections of multifilaments between the two tapes. The mechanical property of jointed tape was evaluated and correlated to the microstructural evolution. The strength of jointed tapes was 44-64% less than that of the unjoined tape. The strain tolerance of jointed tape was also reduced compared to that of the unjoined tape. These lower mechanical properties of jointed tape are probably due to the induced nonuniform microstructure such as the existence of cracks and Ag-intrusion in the joined region.

• 한국초전도학회:학술대회논문집
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• 한국초전도학회 1999년도 High Temperature Superconductivity Vol.IX
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• pp.373-377
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• 1999

HTS magnet operated at 20${\sim}$40 K was fabricated using three pieces of 100 m Bi-2223 high temperature superconductors fabricated by powder-in-tube process. It was composed of 6 double pancakes with 75 ID. and 113 OD. connected by lab splice. Coil I$_c$ of each DP.(double pancake) obtained for a 140 turn, fabricated using react and wind procedure was 6${\sim}$8 A at 77 K, self field. The maximum field was measured 0.06 T at lop = 5 A, 77 K. The joint resistance due to lap splice of HTS tapes affect badly to operate HTS magnet with persistent current mode, total effective magnet resistance included lap splice was 55 ${\mu}$ ${\omega}$ at 77 K.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2005년도 춘계학술발표대회 논문집
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• pp.94-97
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• 2005

The strength of aluminum 7075 and carbon composite hybrid joints was studied for adhesive, bolt, and the adhesive-bolt combined joints. Several hybrid joint specimens were tested to get the failure load and modes for three types of the joints. Adhesive Cytec EA9394S was used for aluminum and carbon bonding. Failure load of the adhesive-bolt combined joint was 94 % of the sum of the failure load of the separately bonded and bolted joints. Hybrid joint also showed more stable failure behavior than the simple adhesive or bolted joint.