• 제목/요약/키워드: adhesive material

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다층구조형 아크릴 점착제의 분자량 및 피착재 종류에 따른 접착특성 (Adhesion Properties on the Molecular Weight and Various Substrates of Multi-layered Structural Acrylic Adhesive)

  • 김동복
    • 폴리머
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    • 제39권3호
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    • pp.514-521
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    • 2015
  • 본 연구는 자동차, 건축, 디스플레이 부품 접합 등에 사용되는 다층구조형 양면 점착테이프에 대한 것으로 UV 경화에 의해 제조된 아크릴폼 기재에 용제 건조형 점착제(AD)를 양면에 붙이고 피착제 종류에 따른 박리강도와 전단접착강도를 고찰하였다. AD 종류와 기재 조성에 따른 접착력 변화 및 피착재로 사용한 플라스틱에 대한 접착력을 고찰한 결과, AD의 분자량(MW)이 증가할수록 박리강도 및 전단접착강도가 증가하였으나 약 65만 이상의 MW를 가진 AD는 접착력이 감소하는 거동을 보였다. 양면 점착테이프에 사용된 AD층 두께가 얇을수록 온도감소와 함께 높은 물성 값을 보였다. 기재와 AD와의 계면접합 특성은 MW 615000(AD-4)을 사용한 것이 가장 우수하였으며, MW가 615000보다 낮으면 기재인 아크릴 폼과의 계면이 분리되는 결과를 보였다. 따라서 본 연구에서 검토한 다층구조형 양면 점착테이프는 표면에너지가 낮은 플라스틱 부품 및 곡면 부위에 적용가능한 산업분야에 유용하게 사용될 수 있을 것으로 판단된다.

Effect of adhesive primers on bonding strength of heat cure denture base resin to cast titanium and cobalt-chromium alloy

  • Kim, Su-Sung;Vang, Mong-Sook;Yang, Hong-So;Park, Sang-Won;Lim, Hyun-Pil
    • The Journal of Advanced Prosthodontics
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    • 제1권1호
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    • pp.41-46
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    • 2009
  • STATEMENT OF PROBLEM. The poor chemical bonding of a denture base resin to cast titanium framework often introduces adhesive failure and increases microleakage. PURPOSE. This study evaluated the shear bond strengths of a heat cure denture base resin to commercially pure titanium, Ti-6Al-4V alloy and a cobalt-chromium alloy using two adhesive primers. MATERIAL AND MATHODS. Disks of commercially pure titanium, Ti-6Al-4V alloy and a cobalt-chromium alloy were cast. Specimens without the primer were also prepared and used as the controls. The shear bond strengths were measured on a screw-driven universal testing machine. RESULTS. The primers significantly(P < .05) improved the shear bond strengths of the heat cure resin to all metals. However, the specimens primed with the Alloy $primer^{(R)}$(MDP monomer) showed higher bond strength than those primed with the MR $bond^{(R)}$(MAC-10 monomer) on titanium. Only adhesive failure was observed at the metal-resin interface in the non-primed specimens, while the primed specimens showed mixed failure of adhesive and cohesive failure. CONCLUSIONS. The use of appropriate adhesive metal primers makes it possible not only to eliminate the need for surface preparation of the metal framework before applying the heat cure resins, but also reduce the need for retentive devices on the metal substructure. In particular, the Alloy $primer^{(R)}$, which contains the phosphoric acid monomer, MDP, might be clinically more acceptable for bonding a heat cure resin to titanium than a MR $bond^{(R)}$, which contains the carboxylic acid monomer, MAC-10.

LNG 화물창 정밀 구조해석을 위한 에폭시와 폴리우레탄 접착제 기계적 물성치 분석 (Mechanical Properties Analysis of Epoxy and Polyurethane Adhesive for Accurate Structural Analysis of LNG Cargo Hold)

  • 정용철;정연제;김정대;박성보;김용태;오훈규;이제명
    • 대한조선학회논문집
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    • 제58권2호
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    • pp.66-72
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    • 2021
  • As the demand for natural gas that satisfies environmental regulations increases, the quantities of natural gas cargo that carrier can load is also increasing. Natural gas is transported in a liquefied state at -163 ℃ to increase loading efficiency. Among several LNG CCS types, MARK-III types are generally adopted in terms of loading efficiency. The secondary barrier adhesives of the MARK-III, nevertheless, is subjected to tensile stress due to thermal contraction and tension in the environment. In terms of these reasons, local analysis of the adhesive to evaluate the stress state must be carried out. According to previous studies, local analysis is unavailable since material properties for secondary barrier adhesives have not been reported. Thus, in this study, the cryogenic tensile test and coefficient of thermal expansion of epoxy and polyurethane (PU15, PU45), which are most widely used at cryogenic temperatures, were experimentally analyzed. At cryogenic temperature, the mechanical behavior of the polyurethane adhesive was better than epoxy of the adhesive. the joint of FSB and epoxy adhesive of the secondary barrier has the maximum coefficient of thermal expansion difference at 25 ℃ and minimum at -150 ℃, respectively.

Effect of modifying the thickness of the plate at the level of the overlap length in the presence of bonding defects on the strength of an adhesive joint

  • Attout Boualem;Sidi Mohamed Medjdoub;Madani Kouider;Kaddouri Nadia;Elajrami Mohamed;Belhouari Mohamed;Amin Houari;Salah Amroune;R.D.S.G. Campilho
    • Advances in aircraft and spacecraft science
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    • 제11권1호
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    • pp.83-103
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    • 2024
  • Adhesive bonding is currently widely used in many industrial fields, particularly in the aeronautics sector. Despite its advantages over mechanical joints such as riveting and welding, adhesive bonding is mostly used for secondary structures due to its low peel strength; especially if it is simultaneously exposed to temperature and humidity; and often presence of bonding defects. In fact, during joint preparation, several types of defects can be introduced into the adhesive layer such as air bubbles, cavities, or cracks, which induce stress concentrations potentially leading to premature failure. Indeed, the presence of defects in the adhesive joint has a significant effect on adhesive stresses, which emphasizes the need for a good surface treatment. The research in this field is aimed at minimizing the stresses in the adhesive joint at its free edges by geometric modifications of the ovelapping part and/or by changing the nature of the substrates. In this study, the finite element method is used to describe the mechanical behavior of bonded joints. Thus, a three-dimensional model is made to analyze the effect of defects in the adhesive joint at areas of high stress concentrations. The analysis consists of estimating the different stresses in an adhesive joint between two 2024-T3 aluminum plates. Two types of single lap joints(SLJ) were analyzed: a standard SLJ and another modified by removing 0.2 mm of material from the thickness of one plate along the overlap length, taking into account several factors such as the applied load, shape, size and position of the defect. The obtained results clearly show that the presence of a bonding defect significantly affects stresses in the adhesive joint, which become important if the joint is subjected to a higher applied load. On the other hand, the geometric modification made to the plate considerably reduces the various stresses in the adhesive joint even in the presence of a bonding defect.

항공기 브레이크 재료용 탄소/탄소 복합재료의 마찰 및 마모 거동 (Friction and Wear Behavior of Carbon/Carbon Composites for Aircraft Brake Material)

  • 우성택;윤재륜
    • Tribology and Lubricants
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    • 제9권1호
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    • pp.62-69
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    • 1993
  • Friction and wear behavior of a carbon/carbon composite material for aircraft brake material was experimentally investigated. Friction and wear test setup was designed and built for the experiment. Friction and wear tests were conducted under various sliding conditions. Friction coefficients were measured and processed by a data acquisition system and amount of wear measured by a balance. Stainless steel disk was used as the counterface material. Temperature was also measured by inserting thermocouple 2.5 mm beneath the sliding surface of the carbon/carbon composite specimen. Wear surfaces were observed by SEM, and analyzed by EDAX. The experimental results showed that sliding speed and normal force did not have significant effects on friction coefficient and wear factor of the composite. Temperature increase just below the surface was not large enough to cause any thermal degradation or oxidation which occurred at higher temperature when tested by TGA. Wear film was generated both on the specimen and on the counterface at relatively low sliding speed but cracks, grooves, and wear debris were observed at high sliding speed. Friction coefficient remained almost constant when the sliding speed or normal load was varied. It is believed that the adhesive and abrasive components contributed mainly to the friction coefficient. Wear behavior at low sliding speed was governed by wear film formation and adhesive wear mechanism. At high speed, fiber orientation, ploughing by counterface asperities, and fiber breakage dominated wear of the carbon/carbon composite.

폐콘크리트 순환자원을 이용한 건설재료의 특성연구 (A Experimental Study on the Construction Material Using the Circulation Resources)

  • 홍세화;손기상;최재남
    • 한국안전학회지
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    • 제25권2호
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    • pp.41-46
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    • 2010
  • This is to show some basic data for introducing both circulated aggregate and recycled powder producing waste concrete. Standard-mixing design for 24MPa has been basically used and added and replaced normal aggregate with recycled powder made of waste concrete. In addition, polycarboxylate high-range water reducing agent has been used because recycled powder is missing adhesive strength and it is not compare with cement's adhesive strength. Compressive strength with powder mixture of 2%, 4%, 6%, 8%, and 10% has been decreased down to 80% of normal concrete material strength without recycled powder mixture. This result has same decreasing proportion to tensile strength of the material. Resistant capacity change of beam varying with recycled powder mixture has been decreased down to 60% of normal concrete bean capacity, while there are 80% decrease of material strength. But strength and capacity change has same consistent decrease ratio. It is found that recycled powder with approximately 15% unit concrete volume can be replaced with cement in reasonable admixture mixing condition.

Composite 부싱의 기밀 특성을 위한 최적의 압착에 관한 연구 (A Study on Optimal Fitting for Tightness Characteristics of Composite Bushing)

  • 조한구;강형경;유대훈
    • 한국전기전자재료학회:학술대회논문집
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    • 한국전기전자재료학회 2009년도 하계학술대회 논문집
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    • pp.390-391
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    • 2009
  • Recently, composite hollow bushings have been increasingly employed mainly from the various characteristics. Composite bushings are superior to porcelain bushings in several respects, including lighter weight, better anti-pollution and anti-explosion properties, and easer manufacturing. This paper deals with the optimal thermal fitting for improved tightness characteristics of composite bushing. Two types of composite bushings were fabricated. For optimal fitting process, it is necessary using adhesive and designed internal structure of flange and FRP tube. In this study, for improved tightness characteristics of composite bushing has prominence and interface tolerance of flange and FRP tube. From FE-SEM analysis the adhesive layers were different with interface tolerance, sample 1 and 2 which have respective about $120{\mu}m$ and $50{\mu}m$.

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A Case-based Decision Support Model for The Semiconductor Packaging Tasks

  • Shin, Kyung-shik;Yang, Yoon-ok;Kang, Hyeon-seok
    • 한국지능정보시스템학회:학술대회논문집
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    • 한국지능정보시스템학회 2001년도 The Pacific Aisan Confrence On Intelligent Systems 2001
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    • pp.224-229
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    • 2001
  • When a semiconductor package is assembled, various materials such as die attach adhesive, lead frame, EMC (Epoxy Molding Compound), and gold wire are used. For better preconditioning performance, the combination between the packaging materials by studying the compatibility of their properties as well as superior packaging material selection is important. But it is not an easy task to find proper packaging material sets, since a variety of factors like package design, substrate design, substrate size, substrate treatment, die size, die thickness, die passivation, and customer requirements should be considered. This research applies case-based reasoning(CBR) technique to solve this problem, utilizing prior cases that have been experienced. Our particular interests lie in building decision support model to aid the selection of proper die attach adhesive. The preliminary results show that this approach is promising.

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광섬유 센서를 이용한 복합 섬유 재료로 보강된 철근 콘크리트 보의 모니터링 (Monitoring of Retrofitted Reinforced Concrete Beams with Hybrid Fiber Reinforced Polymer)

  • 이옥기;신영수;김기수;김종우
    • 한국콘크리트학회:학술대회논문집
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    • 한국콘크리트학회 2001년도 가을 학술발표회 논문집
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    • pp.509-514
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    • 2001
  • The Fibre-optic Bragg grating (FBG) sensor is broadly accepted as a structural health monitoring device for Fibre reinforced plastic (FRP) materials by either embedding into or bonding onto the structures. The accuracy of the strain measured by using the FBG sensor is highly dependent on the bonding characteristics among the bare optical fibre, protective coating, adhesive layer and host material. In general, the signal extracted from the embedded FBG sensor should reflect the straining condition of the host structure. This paper presents a theoretical model to evaluate the differential strains between the bare fibre and host material with different adhesive thickness and modulus of the protective coating of the embedded FBG sensor.

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