• 제목/요약/키워드: Adherend

검색결과 76건 처리시간 0.021초

경계요소법에 의한 이종재료 접합 잔류열응력의 해석 (A Study on the Bonding Residual Thermal Stress Analysis of Dissimilar Materials Using Boundary Element Method)

  • 이원;유영철;정의섭;윤인식
    • 비파괴검사학회지
    • /
    • 제15권4호
    • /
    • pp.540-548
    • /
    • 1996
  • 전자 부품의 일종인 LSI 패키지의 제조 과정에서 절연 방진 방습 등을 목적으로 수지 몰딩이 널리 사용되고 있는데, 냉각과정에서 금속과 수지의 계면에 접합 잔류열응력이 발생하여 파괴의 원인이 되고 있다. 접합 잔류열응력의 측정에는 X선 회절법등이 사용되지만 측정상의 어려움과 계면단 응력특이성에 대한 해석의 곤란함 때문에 적절한 모델링에 따른 수치해석적 연구가 새로이 주목을 받고 있다. 본 연구에서는 Al/Epoxy를 몰딩 접합한 세가지의 대표적인 계면 형상을 선정하여 계면에서의 잔류열응력을 경계요소 수치해석 및 스트레인 게이지를 이용한 실험을 통하여 각각 해석하였다. 수치해석과 실험결과는 정성적으로 잘 일치하였으며, 서브 요소를 사용하므로써 계면단 응력 특이성의 해석 정밀도를 향상시킬 수 있었다. 또한 접합 잔류열응력의 해석결과로부터 수직응력에 의한 계면 박리가 예상되고, 피착체의 두께가 증가할수록 응력 특이성이 강하게 나타남을 확인하였다.

  • PDF

유한요소 모델에 따른 복합재 단일겹치기 접착 조인트부의 거동 평가 (Evaluation of Behavior of Composite Single Lap Joints with Different Finite Element Models)

  • 김정석;윤혁진;황재연;윤지유;이승훈
    • 한국철도학회논문집
    • /
    • 제13권6호
    • /
    • pp.546-551
    • /
    • 2010
  • 본 연구에서는 단일겹치기 접착 체결부에 대한 유한요소해석을 통해 요소의 조밀도 및 유한요소의 종류에 따른 접착 층의 변형률 분포를 Tsai의 시험치 와 비교하여 분석하였다. 이를 위해 접합부재의 길이방향, 접착체결부의 길이방향, 접합부재의 두께방향, 접착 층의 두께방향 및 조인트의 폭방향의 요소 조밀 도를 변화시켰다. 또한, 솔리드, 쉘 및 평면 변형률 요소에 따른 효과도 분석하였다. 해석은 단일 겹치기 접착 체결부의 대변형을 고려하기 위한 기하학적 비선형 해석을 수행하였다. 이를 통해 솔리드 요소를 적용할 경우 접착부재의 길이방향으로의 요소 수는 최소 2개 이상이면 해석의 신뢰도를 확보할 수 있음을 확인할 수 있었다. 쉘 요소의 겨우 x/c=1에서 수직 변형률의 시험결과와 22.8%의 오차를 보였으나, 전단응력의 경우에는 1.67%로 시험치와 거의 일치하였다.

GFRP/Mg 단일겹치기 접착 체결부의 응력집중 저감에 관한 연구 : 유한요소해석 (Stress Reduction Methods of GFRP/Mg Single Lap Bonded Joints : Finite Element Analysis)

  • 김정석;윤혁진;황재연
    • 한국철도학회논문집
    • /
    • 제14권2호
    • /
    • pp.94-99
    • /
    • 2011
  • 본 연구에서는 GFRP/Mg 단일겹치기 접착 조인트의 접착부재 형상에 따른 응력집중 완화효과를 평가하였다. 이를 위해 6가지 서로 다른 접착부재의 끝단부 형상에 대해 비선형 유한요소 해석을 수행하였다. 또한, 서로 다른 끝단부 형상에 따른 접착층내 응력의 3차원 구 배를 고찰하였다. 해석결과, 접착부재가 순방향 테이퍼를 갖고 필렛이 없는 모델 (모델 2번)이 가장 높은 응력 값을 보였다. 반면, 사각형 접착부재에 필렛이 부과된 모델 (모델 3번)과 역방향 테이퍼를 갖고 필렛이 부과된 모델 (모델 5번)은 기준모델에 비해 65.7%와 65.6%의 응력저감 효과가 있었다.

Numerical analysis of the combined aging and fillet effect of the adhesive on the mechanical behavior of a single lap joint of type Aluminum/Aluminum

  • Medjdoub, S.M.;Madani, K.;Rezgani, L.;Mallarino, S.;Touzain, S.;Campilho, R.D.S.G.
    • Structural Engineering and Mechanics
    • /
    • 제83권5호
    • /
    • pp.693-707
    • /
    • 2022
  • Bonded joints have proven their performance against conventional joining processes such as welding, riveting and bolting. The single-lap joint is the most widely used to characterize adhesive joints in tensile-shear loadings. However, the high stress concentrations in the adhesive joint due to the non-linearity of the applied loads generate a bending moment in the joint, resulting in high stresses at the adhesive edges. Geometric optimization of the bonded joint to reduce this high stress concentration prompted various researchers to perform geometric modifications of the adhesive and adherends at their free edges. Modifying both edges of the adhesive (spew) and the adherends (bevel) has proven to be an effective solution to reduce stresses at both edges and improve stress transfer at the inner part of the adhesive layer. The majority of research aimed at improving the geometry of the plate and adhesive edges has not considered the effect of temperature and water absorption in evaluating the strength of the joint. The objective of this work is to analyze, by the finite element method, the stress distribution in an adhesive joint between two 2024-T3 aluminum plates. The effects of the adhesive fillet and adherend bevel on the bonded joint stresses were taken into account. On the other hand, degradation of the mechanical properties of the adhesive following its exposure to moisture and temperature was found. The results clearly showed that the modification of the edges of the adhesive and of the bonding agent have an important role in the durability of the bond. Although the modification of the adhesive and bonding edges significantly improves the joint strength, the simultaneous exposure of the joint to temperature and moisture generates high stress concentrations in the adhesive joint that, in most cases, can easily reach the failure point of the material even at low applied stresses.

외면 및 양면겹치기 동시경화조인트의 인장하중 전달용량에 관한 연구 (Tensile load bearing capacities of co-cured single and double lap joints)

  • 신금철;이정주
    • 한국복합재료학회:학술대회논문집
    • /
    • 한국복합재료학회 2001년도 추계학술발표대회 논문집
    • /
    • pp.95-98
    • /
    • 2001
  • Co-cured joining method is an efficient joining technique because both curing and bonding processes for the composite structures can be achieved simultaneously. It requires neither an adhesive nor a surface treatment of the composite adherend because the excess resin, which is extracted from composite materials during consolidation, accomplishes the co-cured joining process. In this paper, we considered three bond parameters, affecting tensile load bearing capacity of the co-cured single and double lap joints. Filially, we nave presented optimal bonding conditions for co-cured single and double lap joints with steel and composite adherends under tensile loads.

  • PDF

금속-복합재 하이브리드 체결부의 강도 특성 연구 (A Study on the Strength of Metal-Composite Hybrid Joints)

  • 정재우;송민환;권진회;최진호
    • 한국복합재료학회:학술대회논문집
    • /
    • 한국복합재료학회 2005년도 춘계학술발표대회 논문집
    • /
    • pp.94-97
    • /
    • 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.

  • PDF

동시경화법으로 제조된 복합재료 조인트의 강도 및 파괴모드 연구 (A Study on the Strength and Failure Mode of Co-cured Composite Joints)

  • 최진호;이대길
    • 대한기계학회논문집A
    • /
    • 제21권3호
    • /
    • pp.385-392
    • /
    • 1997
  • The joint design and manufacture of the composite structure have become an important research area because the structural efficiency of the composite structure is often determined by its joint not by its basic structure. The co-cured joint is an efficient joint technique because both curing and jointing for composite structures are achieved simultaneously. In this paper, the torque capacities of the co-cured tubular lap joint with and without knurling of the pyamid type were experimentally measure. From the experimental resuts, it was found that the excess resin played a role as an adhesive in the co-cured tubular lap joint whose steel adherends were not knurled. Also, it was found that the torque capacity of the co-cured joint was increased as the knurling size of the pyramid type on the surface of the steel adherend was increased.

접착제로 접합된 복합재료 구동축의 토크 전달특성에 관한 연구 (A Study on the Torque Transmission Characteristics of Adhesively Bonded Composite Drive Shafts)

  • 김원태;김기수;이대길
    • 대한기계학회논문집
    • /
    • 제17권8호
    • /
    • pp.1980-2000
    • /
    • 1993
  • The stresses and torque transmission capabilities of adhesively bonded circular, hexagonal and elliptical lap joints were analyzed by the finite element and compared with the experimental results. The adherends of the joints were composed of carbon fiber/epoxy composite shafts and steel shafts. In calculating the torque transmission capabilities, the linear laminate properties of the composite material and the nonlinear shear properties of the adhesive were used. Using this method, the torque transmission capabilities of adhesively bonded lap joints could be obtained within 10% error compared to the experimental results except some single lap joints. The experiments revealed that the hexagonal joint had the best torque transmission capability from the single lap joints and the double lap joint had better torque transmission than the single lap joint.

복합재료 Single Lap 접합 조인트의 파손 예측 (Failure Prediction of Composite Single Lap Bonded Joints)

  • 김광수;장영순;이영무
    • 한국복합재료학회:학술대회논문집
    • /
    • 한국복합재료학회 2004년도 추계학술발표대회 논문집
    • /
    • pp.73-77
    • /
    • 2004
  • Failure predictions of composite single-lap bonded joints were performed considering both of composite adherend failure and bondline failure. An elastic-perfectly plastic model of adhesive and a delamination failure criterion are used. The failure prediction results such as failure mode and strength have very good agreements with the test results of joint specimens with various bonding methods and parameters. The influence of variations in the effective strength (that is, adhesion performance) and plastic behavior of adhesive on the failure characteristics of composite bonded joints are investigated numerically. The numerical results show that optimal joint strength is archived when adhesive and delamination failure occur in the same time.

  • PDF

알루미늄 단순겹치기 접착이음의 에지계면균열에 대한 연구 (Analysis on the Interface Edge Crack in Aluminum Bonded Single Lap-joint)

  • 유영철;박정환;정의섭;이원
    • 한국정밀공학회:학술대회논문집
    • /
    • 한국정밀공학회 1997년도 춘계학술대회 논문집
    • /
    • pp.655-659
    • /
    • 1997
  • The analysis of cracks at the interface between dissimilar materilar has received a great deal of attention in recent years. In this paper we conducted the static tensile test for the aluminum bonded single lap-joint with the interface edge crack. Comparing this results, that is ultimate load and strain value of aluminum adherend by strain gauge with the fracture mechanics parameters, compliance and stress intensity factors acquied from the boundary element analysis, we concluded that there are critical value of crack length to provoke the interface fracture.

  • PDF