• 제목/요약/키워드: Delamination length

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Evaluation of Physical and Mechanical Properties of Non-certificated Laminated Veneer Lumber (LVL) Circulated in Domestic Lumber Market

  • Oh, Sei-Chang
    • Journal of the Korean Wood Science and Technology
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    • 제39권5호
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    • pp.429-436
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    • 2011
  • The selected physical and mechanical properties of non-certificated LVL circulated in domestic lumber market were investigated and compared to relevant standards. The tested LVL passed the moisture content and the soaking delamination rate limit as per domestic (KS) and Japanese standard (JAS). The evaluated mechanical properties were flatwise/edgewise bending strength, modulus of elasticity (MOE), horizontal shear and compressive strength. The 30 mm-thick LVL showed significantly higher bending strength than that of the 25 mm-thick LVL. The modulus of elasticity (MOE) showed same tendency in the results of bending strength. The edgewise bending strength and MOE were higher than that of flatwise bending strength and MOE. The horizontal shear strength values were also showed similar results to bending strength values. The tested results were compared each other and each products were graded according to JAS 701 grade specification. The failure mode of LVL in bending test showed the similar failure mode of solidwood that failed in a simple tension manner (splintery tension). The glue line failure was severe in 25 mm-thick specimens due to concentration of shear stress in layer discontinuity containing small voids and starved glue lines. In horizontal shear strength test, failure mode of LVL showed the typical horizontal shear failure. Compressive specimens failed with fiber crushing in company with apparent delamination that splitted along the length of the specimens. From the results, the complete bonding between lamination and consistency in thin veneer layer were considered as a critical factor in the mechanical properties of LVL. Moreover, the standard test procedure and specification for non-certificated LVL should be required to check the performance of uncertificated materials.

원공노치 인근에 발생한 결함의 위치변화가 균열성장률(da/dN) 및 응력확대계수범위(δK)의 관계에 미치는 영향 - 단일재 알루미늄과 Al/GFRP 적층재의 피로거동 비교 - (The Effect of Defect Location Near a Circular Hole Notch on the Relationship Between Crack Growth Rate (da/dN) and Stress Intensity Factor Range (δK) - Comparative Studies of Fatigue Behavior in the Case of Monolithic Al Alloy vs. Al/GFRP Laminate -)

  • 김철웅;고영호;이건복
    • 대한기계학회논문집A
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    • 제31권3호
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    • pp.344-354
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    • 2007
  • The objective of this study is to investigate the effect of arbitrarily located defect around the circular hole in the aircraft structural material such as Al/GFRP laminates and monolithic Al alloy sheet under cyclic bending moment. The fatigue behavior of these materials may be different due to the defect location. Material flaws in the from of pre-existing defects can severely affect the fatigue crack initiation and propagation behavior. The aim of this study is to evaluate effects of relative location of defects around the circular hole in monolithic Al alloy and Al/GFRP laminates under cyclic bending moment. The fatigue behavior i.e., the stress concentration factor($K_t$), the crack initiation life($N_i$), the relationship between crack length(a) and cycles(N), the relationship between crack growth rate(da/dN) and stress intensity factor range(${\Dalta}K$) near a circular hole are considered. Especially, the defects location at ${\theta}_1=0^{\circ}\;and\;{\theta}_2=30^{\circ}$ was strongly effective in stress concentration factor($K_t$) and crack initiation life($N_i$). The test results indicated the features of different fatigue crack propagation behavior and the different growing delamination shape according to each location of defect around the circular hole in Al/GFRP laminates.

양극산화 제어에 의한 TiO2 나노튜브의 광전기화학 특성 (Photoelectrochemical Properties of TiO2 Nanotubes by Well-Controlled Anodization Process)

  • 정다솔;김동현;정현성
    • 한국표면공학회지
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    • 제52권6호
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    • pp.298-305
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    • 2019
  • We investigated a correlation between morphology and photoelectrochemical properties of TiO2 nanotubes fabricated by well-controlled anodization processes. Anodization in an ethylene-glycol-based electrolyte solution accelerated the rapid grow rate of TiO2 nanotubes, but also cause problems such as delamination at the interface between TiO2 nanotubes and a Ti substrate, and debris on the top of the nanotube. The applied voltages for the anodization of TiO2 were adjusted to avoid the interface delamination. The heat treatment and the anodizing time were also controlled to enhance the crystallinity of the as-prepared TiO2 nanotubes and to increase the surface area with the varied length of the anodized TiO2 nanotubes. Additionally, a 2-step anodization process was utilized to remove the debris on the tube top. The photoelectrochemical properties of TiO2 nanotubes prepared with the carefully tailored conditions were investigated. By removing the debris on TiO2 nanotubes, applied bias photon-to-current efficiency (ABPE) of TiO2 nanotubes increased up to 0.33%.

아라미드 FRP 스트립과 강판 사이의 계면 부착응력에 관한 실험적 연구 (Experimental Study on Interfacial Bond Stress between Aramid FRP Strips and Steel Plates)

  • 박재우;류재용;최성모
    • 한국강구조학회 논문집
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    • 제27권4호
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    • pp.359-370
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    • 2015
  • 본 연구에서는 AFRP 스트립과 강재사이의 부착거동에 관한 실험적 연구를 수행하였다. 실험적 연구를 통해 AFRP 판과 강판사이의 계면부착거동을 관찰하고, 계면부착응력을 산정하는 것이 본 연구의 목표이다. 실험변수로는 부착길이와 AFRP의 두께를 선택하였으며, 18개의 일면전단시편 제작하여 실험을 수행하였다. 실험결과 부착길이와 AFRP 두께가 증가함에 따라 하중값을 증가하였으며, 부착길이와 AFRP 두께가 증가함에 따라 각각 63%, 86%의 하중값이 증가하였다. 끝으로 강재와 AFRP 사이의 부착응력-슬립관계를 산정하였다. 부착응력-슬립관계는 탄성선형거동을 보이고 있으며, 부착길이와 AFRP 두께는 부착응력과 파괴에너지에 영향을 덜 미치는 것으로 나타났다.

CFRP 복합재료의 충격파괴거동에 관한 연구 (A Study on the Impact Fracture Behavior of Carbon Fiber Reinforced Plastics)

  • 고성위;김학돌;엄윤성;최영근;김형진;김재동;김엄기
    • 수산해양기술연구
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    • 제38권4호
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    • pp.300-306
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    • 2002
  • 장섬유 CF/에폭시 복합재료를 사용하여-5$0^{\circ}C$에서 6$0^{\circ}C$ 사이의 범위에서 스팬길이를 변화시켜 충격시험으로 얻어진 임계파괴에너지의 거동을 고찰한 결과는 다음과 같다. 1. CF/에폭시 복합재료의 온도 변화에 따른 임계파괴에너지 GIC는 동일한 스팬길에서는 실온의 경우가 가장 높고, 6$0^{\circ}C$, -15$^{\circ}C$ 그리고 -5$0^{\circ}C$의 순으로 낮게 나타났다. 2. CF/에폭시 복합재료의 스팬길이의 변화에 대한 임계 파괴에너지 GIC는 동일한 온도조건하에서는 스팬길이가 20mm인 경우가 가장 높게 나타났으나 불안정하며, 스팬길이는 40mm인 경우 임계파괴에너지 GIC는 가장 낮게 나타났으나 실험치의 흩어짐을 고려할 때 40mm인 경우의 시험편이 더 적절한 조건이라 생각된다. 3. 본 실험에 사용한 재료의 파괴기구는 섬유의 풀아웃, 섬유와 매트릭스 사이의 디본딩 그리고 매트릭스의 변형을 관찰할 수 있었으며, 이와 같은 파괴기가구 종합적으로 상호작용한다고 생각된다.

GFRP 복합구조의 피로신뢰성 해석모형에 관한 연구 (Fatigue Reliability Analysis Model for GFRP Composite Structures)

  • 조효남;신재철;이승재
    • 한국전산구조공학회:학술대회논문집
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    • 한국전산구조공학회 1991년도 가을 학술발표회 논문집
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    • pp.29-32
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    • 1991
  • It is well known that the fatigue damage process in composite materials is very complicated due to complex failure mechanisms that comprise debounding, matrix cracking, delamination and fiber splitting of laminates. Therefore, the residual strength, instead of a single dominant crack length, is chosen to describe the criticality of the damage accumulated in the sublaminate. In this study, two models for residual strength degradation established by Yang-Liu and Tanimoto-Ishikawa that are capable of predicting the statistical distribution of both fatigue life and residual strength have been investigated and compared. Statistical methodologies for fatigue life prediction of composite materials have frequently been adopted. However, these are usually based on a simplified probabilistic approach considering only the variation of fatigue test data. The main object of this work is to propose a fatigue reliability analysis model which accounts for the effect of all sources of variation such as fabrication and workmanship, error in the fatigue model, load itself, etc. The proposed model is examined using the previous experimental data of GFRP and it is shown that it can be practically applied for fatigue problems in composite materials.

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플립 칩 전자 패키지의 피로 균열이 미치는 열적 기계적 거동 분석 (Effect analysis of thermal-mechanical behavior on fatigue crack of flip-chip electronic package)

  • 박진형;이순복
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2007년도 춘계학술대회A
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    • pp.1673-1678
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    • 2007
  • The use of flip-chip type electronic package offers numerous advantages such as reduced thickness, improved environmental compatibility, and downed cost. Despite numerous benefits, flip-chip type packages bare several reliability problems. The most critical issue among them is their electrical performance deterioration upon consecutive thermal cycles attributed to gradual delamination growth through chip and adhesive film interface induced by CTE mismatch driven shear and peel stresses. The electronic package in use is heated continuously by itself. When the crack at a weak site of the electronic package occurs, thermal deformationon the chip side is changed. Therefore, we can measure these micro deformations by using Moire interferometry and find out the crack length.

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틸팅열차 차체8 탄소섬유직물/에폭시 복합재의 모우드 II 층간파괴인성 평가 (Evaluation of Mode II Interlaminar Fracture Toughness for Carbon Fabric/Epoxy Composites for Tilting Train Carbody)

  • 윤성모;이은동;허광수;정종절;신광복
    • 한국철도학회논문집
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    • 제8권2호
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    • pp.195-201
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    • 2005
  • Mode II interlaminar fracture behaviors of carbon fabric/epoxy composites, which are applicable to tilting train carbodies, was investigated by the ENF (End notched flexure) test. The specimens were made of CF3327 plain woven fabric with epoxy and a starter delamination at one end was made by inserting Teflon film with the thickness of 12.5$mu$m or 25.0$mu$m. The equation for mode II interlaminar fracture toughness was suggested based on the effective crack length from the compliance of load-displacement curve. Mode II interlaminar fracture toughness was evaluated for several types of the specimens. Also crack propagating behaviors and fracture surfaces were examined through an optical travelling scope and a scanning electron microscope.

홀로그래피 간섭계를 이용한 복합적층판의 결함측정 (Nondestructive Inspection Method of Composite Laminated Plates by Holographic Interferometry)

  • 김석중;김재형;박현철
    • 대한기계학회논문집
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    • 제18권12호
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    • pp.3202-3218
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    • 1994
  • Mode shapes and natural frequencies of vibrating laminated composite plates are taken using real-time and time-average holographic interferometry. Debonds and delamination in the laminated plates are measured nondestructively. During holographic testing of composite plates, it has been found that the conditions for the local resonance in debonds are strongly dependent on the frequency of excitation. A membrane resonance model was proposed to describe this behavior. Relations between characteristic length according to the size, shape of debonds and membrane resonance frequency are presented. Several experiments were performed to verify the membrane resonance model. The agreements between the predicted excitation frequency and the observed resonance frequency are good. The experimental results show that higher stresses and strains due to local resonance lead to the debond detection.

Design and Simulation of Heating Rubber Roller for Laminating Process

  • Hur, Shin;Woo, Chang Su
    • Elastomers and Composites
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    • 제51권4호
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    • pp.280-285
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    • 2016
  • The purpose of this study is to get optimum design and operation conditions of the heating rubber roller for laminating process. The cause of performance degradation of heating rubber roller is delamination of rubber on metal tube, rubber aging due to high temperature. We measured the material properties of thermal expansion, thermal conductivity, specific heat and density and analyzed thermal distributions of rubber layer using finite element method. As a result of heat/flow analysis, the density distribution of heating coil must shorten the stabilization time by reducing the temperature deviation on the length direction at the temperature rising section after increasing the density of the area contacting with the laminate film at the center part which is an opposite of the current composition while enabling to maintain the temperature of heater to be consistent while maintaining the temperature deviation to be low when heat loss is created. Finally, we determined optimum heating method of heating rubber roller.