• 제목/요약/키워드: Cure shrinkage

검색결과 48건 처리시간 0.022초

Effect on the Residual Stress of Cure Profiles, Fillers and Mold Constraints in an Epoxy System

  • Moon, Chang-Kwon;Nam, Ki-Woo
    • 한국해양공학회지
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    • 제23권4호
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    • pp.1-5
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    • 2009
  • A dilatometer was used to investigate the effect of cure conditions, mold types and the presence of filler in an epoxy system. These studies showed shrinkage in the cured epoxy when heating it through the glass transition temperature region. The magnitude of the shrinkage, related to stress build up in the epoxy during curing, was influenced by the processing conditions, filler presence and the nature of the mold used to contain the resin. Cure and cyclic cure at a lower temperature, prior to a post cure, decreased the magnitude of observed shrinkage. Cure shrinkage decreased with the number of cyclic cures. Post cured samples outside the mold led to less shrinkage compared with samples in the mold. Sample cured in a silicon mold represented less shrinkage than sample cured in an aluminum mold. Sample containing kaolin filler showed less shrinkage than unfilled sample.

Effect on the residual stress of cure conditions in an epoxy system

  • 유경희;서상하;김영운;문창권
    • 한국해양공학회:학술대회논문집
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    • 한국해양공학회 2006년 창립20주년기념 정기학술대회 및 국제워크샵
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    • pp.233-236
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    • 2006
  • A dilatometer was used to investigate the effect of cure conditions and the presence of filler in an epoxy system. These studies showed shrinkage in the cured epoxy when heating it through the glass transition temperature region. The magnitude of the shrinkage, related to stress build up in the epoxy during curing, was influenced by the processing conditions, filler presence and the nature of the mold used to contain the resin. Cure and cyclic cure at a lower temperature, prior to a post cure, decreased the magnitude of observed shrinkage. Cure shrinkage decreased with number of cyclic cure. Post cured samples outside the mold led to less shrinkage compared with sample in the mold. And sample containing kaolin filler showed less shrinkage than unfilled sample.

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경화도에 따른 고분자 기지 복합재의 경화 수축률 거동 (Cure Shrinkage Behavior of Polymer Matrix Composite according to Degree of Cure)

  • 권혁;황성순;최원종;이재환;김재학
    • Composites Research
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    • 제27권3호
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    • pp.90-95
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    • 2014
  • 복합재료의 경화 시 발생하는 수축 변형률은 복합재료 구조물 내에 잔류응력을 발생시키며 이러한 잔류응력은 spring-in, spring-out, warpage와 같은 구조물 변형의 원인이 된다. 본 연구에서는 Hexcel사의 "Hexply M21EV/34%/UD268NFS/IMA-12K" prepreg를 사용하였다. 시험편의 경화에 따른 cure shrinkage 변화를 DSC(differential scanning calorimetry)와 TMA(thermomechanical analyzer)를 이용하여 측정하였다. 수지의 수축률은 $140{\sim}240^{\circ}C$ 구간에서 $20^{\circ}C$ 간격으로 질소 분위기에서 측정하였다. 경화도는 dynamic과 isothermal DSC scanning을 통하여 측정된 반응열을 이용하여 산출하였으며, DSC 시험은 Argon 분위기에서 수행하였다. 시험결과, 열경화성 수지는 27~80% 경화도에서 급격한 수축이 일어났으며, 경화온도가 높을수록 더 낮은 경화도에서 수축이 시작되는 것을 알 수 있었다.

열기계적 분석법으로 측정된 레진 포뮬레이션의 경화 수축 특성 (Cure Shrinkage Characteristics of Resin Formulations by Thermomechanical Analysis)

  • 서안나;이종현
    • 대한금속재료학회지
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    • 제50권9호
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    • pp.629-636
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    • 2012
  • Volume shrinkage behavior accompanying the cure of resin formulations might be a critical factor when assembly processes using polymer materials are considered. In this study, cure shrinkage behavior with respect to resin formulation type and heating method was measured on sandwich structure samples by a thermomechanical analyzer (TMA). Quartz, used as a cover material for the sandwich structure, indicated the coefficient of thermal expansion close to $0ppm/^{\circ}C$. When a dynamic heating mode was conducted, a squeeze-out region and a cross-linking region for each resin formulation could be separated clearly with overlapping differential scanning calorimeter results on the TMA results. In addition, a cure shrinkage dominant region and a thermal expansion dominant region in the cross-linking region were distinguished. Consequently, the degree of cure at the initiation of the thermal expansion dominant region was successfully measured. Measurement of all resin formulations indicated the thermal expansion behavior exceeded cure shrinkage before full cure.

환경친화적 Spray UV-Cure 가공 기술을 이용한 물세탁 모직물(washable wool)의 개발 -광가교 고분자인 dextran-methacrylate를 이용하여- (Development of Washable Wool Using Environmental-friendly Spray UV-cure Finishing Technique - Using Photocrosslinkable Polymerr Dextran-methacrylate-)

  • 김신희
    • 한국의류학회지
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    • 제28권11호
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    • pp.1507-1515
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    • 2004
  • Washable wool was developed using environmental-friendly spray UV-cure technique. Photocrosslinkable polymer, dextran-methacrylate, was synthesized starting from natural biopolymer, dextran. The aqueous solution of dextran-methacrylate was applied to wool fabric with various concentrations to find out the optimum condition in minimizing felting shrinkage. The wool fabric subsequently cured by 365 nm UV, The effects of UV-cure time and photoinitiator concentration on felting behavior of wool were examined. As the concentration of dextran-methacrylate increased, the felting shrinkage decreased gradually. At concentration 0.5g/ml, the felting shrinkage of wool was negligible. Other properties such as air permeability, moisture content, wrinkle recovery, thickness and wettability were also evaluated. The surface coating of dextran polymer onto wool fiber was identified by SEM.

탄소섬유강화 복합재료 성형시 화학수축에 의한 변형연구 (Thermal Deformation of Carbon Fiber Reinforced Composite by Cure Shrinkage)

  • 최은성;김위대
    • Composites Research
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    • 제31권6호
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    • pp.404-411
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    • 2018
  • 복합재료는 주어진 경화 사이클(cure cycle)로 오토클레이브 공정이 진행됨에 따라 수지의 화학수축, 열팽창계수 등에 의한 제품 내 잔류응력(residual stress)이 발생한다. 이로 인해 spring-in, warpage와 같은 열 변형이 발생하고 최종 제품의 수치 정확성이 감소한다. 구조물의 정밀한 제작이 요구되는 항공우주분야에서는 열변형으로 인한 문제를 해결하는 것이 중요하다. 따라서 복합재료의 경화과정을 예측하고 이해하기 위한 연구가 활발히 이루어지고 있다. 본 연구에서는 공정과정에 따른 복합재료의 경화메커니즘을 유한요소해석을 통해 예측하였고, 공정에 의해 발생하는 열변형에 대한 화학수축의 영향을 열팽창계수와 비교하여 분석하였다.

광중합 복합레진에 대한 가열처리 피로내성 및 중합수축에 미치는 영향 (A Fatigue Toughness and Polymerization Shrinkage of Post-cure Heat Treated Composite Resins)

  • 오원만;류선열;손호현;리이치 오쿠다;다쓰오 엔도;요시유키 쿠도
    • Restorative Dentistry and Endodontics
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    • 제19권1호
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    • pp.135-147
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    • 1994
  • This study was conducted to evaluate whether the fatigue toughness of visible light cured composite resins could be improved and how much percentage of polymerzation shrinkage could be affected by additional heat treatment. 7 materials were investigated for this study: P-50, Lite-fil CR inlay, Pekafil, Clearfil CR inlay, Clearfil photo posterior, Z -100 and Progress. Diametral tensile strengths and linear shrinkages of composite resins were taken under visible light cured and additional post-cure heated condition and compared each other. A fatigue toughness of above materials was evaluated by measuring diametral tensile strength after they were repeatedly loaded with 120kgf/$cm^2$ up to 3000 cycles. The results obtained were as follows : 1. When composite resins were cured just by visible light, Lite fil CR inlay, Z -100 and Progress showed respectively higher diametral tensile strength than the other materials. Clearfil CR inlay, Clearfil photo posterior and Progress exhibited strong fatigue toughness compared to P-50 and Pekafil. 2. Post-cure heat treated composite resins had higher diametral tensile strengths than visible light cured composite resins at fatigue toughness test as well as no fatigue toughness test. 3. When Composite resins were additionally polymerized by post-cure heat treatment, P-50 showed weak fatigue toughness, on the contrary, Clearfil CR inlay, Z-100, Progress showed strong one. 4. When composite resins were cured just by visible light, percentage of polymerization linear shrinkage was the lowerest in Clearfil CR inlay, followed by, in ascending order, Clearfil photo posterior, Lite-fil CR inlay, Progress, Pekafil, P-50, and Z-100. In the case of post- cure heat treated composite resins, percentage of linear shrinkage was the lowest in Clearfil photo posterior, followed by, in ascending order, Lite-til CR inlay, Clearfil CR inlay, Progress, P-50, Pekafil and Z-100. 5. Percentage of polymerization linear shrinkage was greater in the post-cure heat treated composite resins than in the visible light cured composite resins and linear shrinkage increased significantly in Pekafil, Clearfil CR inlay, and Clearfil photo posterior between at the visible light cured and at the post-cure heat treated condition. The above results is saying that additional post-cure heat treatment on the composite resins for posterior restoration is able to affect on improvement of strength and fatigue toughness and lead to increase polymerization of composite resins.

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유전 센서 및 광섬유 센서를 이용한 EMC 유효 경화 수축 측정 (Measurement of effective cure shrinkage of EMC using dielectric sensor and FBG sensor)

  • 백정현;박동운;김학성
    • 마이크로전자및패키징학회지
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    • 제29권4호
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    • pp.83-87
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    • 2022
  • 최근 반도체 패키지 두께가 점점 얇아짐에 따라 휨(warpage) 문제가 대두되고 있다. 휨(warpage)은 패키지 구성요소들 간의 물성 차이로 인해 발생하기 때문에, 휨(warpage)을 예측하기 위해서는 주된 구성요소인 EMC(Epoxy molding compound)의 정확한 물성 파악이 필수적으로 요구된다. 특히 EMC는 경화 공정 중 경화 수축을 보이는데, 겔점 이후에 발생하는 유효 경화 수축은 휨(warpage) 발생의 핵심 요소이다. 본 연구에서는 유전 센서를 이용해 측정한 소실 계수로부터 실제 반도체 패키지 경화 공정 동안 발생하는 EMC의 겔점이 정의되었다. 유전 센서로부터 얻은 결과를 분석하기 위해 DSC(Differential scanning calorimetry) 시험과 rheometer 시험이 수행되었다. 그 결과, 유전 측정법이 EMC 경화상태 모니터링에 효과적인 방법임이 검증되었다. 유전 측정과 동시에 광섬유 센서를 이용해 EMC의 경화 공정 중 변형률 변화 추이가 함께 측정되었다. 위 결과들로부터 경화 공정 중 발생하는 EMC의 유효 경화 수축이 측정되었다.

열경화성 수지 재료를 이용한 광학 렌즈 제조공정에서 렌즈 변형에 대한 수축률이 영향에 관한 연구 (A Study on the Effect of Shrinkage on Lens Deformation in Optical Lens Manufacturing Process Using Thermosetting Resin Material)

  • 박시환
    • Design & Manufacturing
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    • 제16권3호
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    • pp.9-15
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    • 2022
  • In order to reduce the manufacturing costs of the glass lens, it is necessary to manufacture a lens using a UV curable resin or a thermosetting resin, which is a curable material, in order to replace a glass lens. In the case of forming a lens using a thermosetting material, it is necessary to form several lenses at once using the wafer-level lens manufacturing technologies due to the long curing time of the material. When a lens is manufactured using a curable material, an error in the shape of the lens due to the shrinkage of the material during the curing process is an important cause of defects. The major factors for these shape errors and deformations are the shrinkage and the change of mechanical properties in the process of changing from a liquid material during curing to a solid state after complete curing. Therefore, it is necessary to understand the curing process of the material and to examine the shrinkage rate and change of physical properties according to the degree cure. In addition, it is necessary to proceed with CAE for lens molding using these and to review problems in lens manufacturing in advance. In this study, the viscoelastic properties of the material were measured during the curing process using a rheometer. Using the results, Rheological investigation of cure kinetics was performed. At the same time, The shrinkage of the material was measured and simple mathematical models were created. And using the results, the molding process of a single lens was analyzed using Comsol, a commercial S/W. In addition, the experiment was conducted to compare and verify the CAE results. As a result, it was confirmed that the shrinkage rate of the material had a great influence on the shape precision of the final product.

Effect of tack cure time on polymerization shrinkage of dual-cure resin cement

  • Choi, Yoorina;Heo, Yu-Keong;Jung, Ji-Hye;Chang, Hoon-Sang
    • International Journal of Oral Biology
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    • 제46권4호
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    • pp.184-189
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    • 2021
  • When luting indirect restorations with dual-cure resin cement (DCRC), excess cement can be easily removed by performing tack cure of DCRC for a few seconds. The purpose of this study was to evaluate whether different tack cure times affect polymerization shrinkage (PS) of the selected DCRC. One dual-cure resin cement (G-CEM LinkAce, GC) was used for measuring PS in light-cure (LC group), self-cure (SC group), and two tack-cure modes. In the first tack-cure subgroup, tack cure was performed for 1, 2, 3, and 5 seconds, followed by light cure after 2 minutes of remnant removal time in each case (TC-LC groups). In the other tack-cure subgroup, tack cure was performed for the same lengths of time, but followed by self-cure in each case (TC-SC groups). PS was measured by a modified bonded disc method for 1,800 seconds. One-way analysis of variance followed by Duncan's post hoc test was used to determine any statistically significant differences among the test groups (α = 0.05). When the DCRC was self-cured after tack cure, PS was significantly lower than when it was only self-cured (p < 0.05); however, tack cure time did not affect PS (p > 0.05). When the DCRC was light-cured, PS was not affected by tack cure or tack cure time (p > 0.05). Therefore, tack cure within 5 seconds did not negatively affect the final PS when the DCRC was light-cured after cement remnant removal.