• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 1993년도 춘계학술대회 논문집
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• pp.108-113
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• 1993

The material for the machine tool structure should have high static stiffiness and damping in its property to improve both the static and dynamic performances. The static stiffness of a machine tool can be inceased by using either higher modulus material in the structure of a machine tool. However, the machine tool structrue with high stiffness but low damping is vulnerable to vibration at the resonance frequencies of the structure . For the high precision and highsped machine tool structure, therefore, the high damping capacity is most important in order to suppress vibration. The damping of a machine tool can not be increased by increasing the static stiffness. The best way to increase the damping capacity of the machine tool structure is to use a composite material which is composed of on material with high stiffness with low damping and another material with low stiffness with high damping. Therefore, in this paper, the bed of the ultra high precision grinding machine for mirror surface machining of brittle materials such as ceramics and composite materials was designed and manufactured with the epoxy concrete material. The epoxy concrete material was prepared by mixing epoxy resin with different size sands and gravels. The modulus, compressive strength, coefficient of thermal expansion, specific heat, and damping factor were measured by varying the compaction ratio, sizes and contents of the ingredients to assess the effect of the processing parameters on the mechanical properties of the material. Based of the measured properties, the prototype epoxy resin concrete bed for the mirror surface CNC grinding machine was designed and manufactured.

• Carbon letters
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• 제13권4호
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• pp.191-204
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• 2012

Carbon nanotubes (CNTs) have exceptional mechanical, electrical, and thermal properties compared with those of commercialized high-performance fibers. For use in the form of fabrics that can maintain such properties, individual CNTs should be held together in fibers or made into yarns twisted out of the fibers. Typical methods that are used for such purposes include (a) surfactant-based coagulation spinning, which injects a polymeric binder between CNTs to form fibers; (b) liquid-crystalline spinning, which uses the nature of CNTs to form liquid crystals under certain conditions; (c) direct spinning, which can produce CNT fibers or yarns at the same time as synthesis by introducing a carbon source into a vertical furnace; and (d) forest spinning, which draws and twists CNTs grown vertically on a substrate. However, it is difficult for those CNT fibers to express the excellent properties of individual CNTs as they are. As solutions to this problem, post-treatment processes are under development for improving the production process of CNT fibers or enhancing their properties. This paper discusses the recent methods of fabricating CNT fibers and examines some post-treatment processes for property enhancement and their applications.

• 열처리공학회지
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• 제21권3호
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• pp.131-136
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• 2008

The fatigue characteristics of the carbon fiber reinforced carbon composites (CFRC) material are necessary for the advanced industries requiring the thermal resistance. The research and development of CFRC have been in progress in the field of aerospace and defense industry. In this paper, we investigated the fatigue characteristics of CFRC by using an aircraft brake disk system. As the results of a series of tensile tests, the tensile strengths of CFRC were appeared 102.8 MPa ($0^{\circ}$), 98.6 MPa ($60^{\circ}$), and 95.5 MPa ($90^{\circ}$), respectively. It was showed that CFRC had better tensile property than the usual composite materials. As the results of fatigue tests, the fatigue limit was ~ 77 MPa, which is under the 75% of the maximum tensile load. CFRC is recommended as a strong potential composite materials because the carbon fibers are closely packed and strongly bonded between the carbon fibers.

• Nuclear Engineering and Technology
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• 제52권11호
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• pp.2607-2612
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• 2020

The present work was aimed to show the possibility of using hydrogel (acrylic/boric acid) for evaluation of the neutron radiation shielding. The influence of acrylic acid concentration, different gamma doses and relative contents of boric acid were studied. The physical properties and the thermomechanical stability of the studied samples were investigated. The shielding property of the composite for neutron was tested by Pu-Be neutron source (5 Ci) under room temperature. The neutron fluence rates and gamma fluxes were measured using a stilbene organic scintillator. The macroscopic effective removal cross-section Σ_R (cm^-1) of fast neutrons and total attenuation coefficient μ (cm^-1) of gamma rays has been studied experimentally. The transmission parameters, the relaxation length (??) and the half-value layer (HVL) were obtained. The obtained results indicated that the addition of boric acid to acrylic acid tends to increase the macroscopic effective removal cross-section Σ_R (cm^-1) to 0.141 compared to 0.094 of ordinary concrete.

• Composites Research
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• 제26권5호
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• pp.303-308
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• 2013

탄소섬유(CF) 강화 폴리프로필렌(PP) 복합재료의 수요는 증가되고 있다. 본 연구에서는 재활용 횟수에 따라 변화되는 복합재료의 물성 변화를 관찰하였다. CF 함량을 20% 함량으로 조성한 복합재료에 대해서 재활용 횟수에 따른 기계적 물성 평가를 진행하였다. 인장, 굴곡, Izod 동적 피로 실험에 따른 영향을 확인하였다. CF/PP 복합재료의 계면 물성을 평가하기 위해 젖음성 평가와 파단면을 FE-SEM으로 확인하였다. 재활용 횟수에 따라 섬유와 기지는 변화된다. CF/PP 복합재료는 재활용 할수록 섬유와 기지간의 계면에 열 데미지와 분쇄 과정에 의한 결합력 감소가 확인하였다.

• Carbon letters
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• 제28권
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• pp.9-15
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• 2018

In the aerospace field, Carbon/Cork composites have been used for rocket propulsion systems as a light weight structural component with a high bending stiffness and high thermal insulation properties. For the fabrication of a carbon composite with a heat insulation cork part, the bonding properties between them are very important to determine the service life of the Carbon/Cork composite structure. In this study, the changes in the interfacial adhesion and mechanical properties of Carbon/Cork composites under accelerated aging conditions were investigated. The accelerated aging experiments were performed with different temperatures and humidity conditions. The properties of the aged Carbon/Cork composites were evaluated mainly with the interfacial strength. Finally, the lifetime prediction of the Carbon/Cork composites was performed with the long-term property data under accelerated conditions.

• Composites Research
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• 제17권6호
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• pp.44-51
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• 2004

에폭시 경화계에서 말단 관능기가 같은 선형아민 경화제의 주쇄에 포함된 에틸기에 결합된 질소원자 개수가 반응특성 및 열적, 기계적특성에 미치는 영향을 알아보기 위하여, 빈용 에폭시수지인 DCEBF (diglycidyl ether of bisphenol F)를 DETA (diethylenetriamine), TETA (triethylenetetraamine) 그리고 TEPA (tetraethylenepentaamine)와 1:1 당량비로 경화하였다. 이 연구에서 DGEBF/아민계에서 경화제 주쇄의 질소원자 거수에 의하여 반응특성 및 열적성질, 기계적특성에 중대하게 영향을 미쳤다. 즉, 주쇄의 질소원자 개수가 작을수록 반응열이 많고 최대발열온도가 낮아졌다. 경화물의 경우 밀도와 최대반응전환률은 주쇄의 질소원자 개수와는 큰 관계가 없으나, 굴곡탄성률과 인장탄성률은 주쇄의 질소원자 개수가 작을 수록 크다. 그 외의 열안정성, 부피수축률(%), 유리전이온도, 인장강도, 굴곡강도는 주쇄의 질소원자 개수와는 일견 무관한 불규칙한 경향을 보인다. 이는 최대반응전환률(%)의 차이가 이러한 특성에 영향을 미치는 것을 나타낸다.

• 항공우주기술
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• 제13권1호
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• pp.76-85
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• 2014

본 연구에서는 다양한 열팽창계수 예측기법을 활용해서 섬유강화 복합재료 라미나 등가 열팽창계수 예측을 수행하였다. 등가열팽창계수를 예측하는 많은 식들이 제안되어 왔지만 사용대상에 따라 제약이 있거나, 예측결과가 시험결과와 잘 일치하지 않는 문제점을 갖고 있다. 본 연구에서 실제 복합재료 형상과 유사한 대표체적요소를 선정하여 유한요소 모델링을 수행하고 여기에 주기적 경계조건을 부여하여 재료의 등가열팽창계수를 예측하였다. 예측결과를 기존의 예측식 및 시험결과와 비교하여 그 성능을 검증하였으며, 별추적기 지지구조물의 열지향오차해석을 수행하고 다양한 예측물성을 따라 그 정확도를 검토하였다.

• Composites Research
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• 제18권4호
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• pp.14-20
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• 2005

방향족아민 경화제의 벤젠링 사이의 관능기 변화가 반응특성, 기계적특성 및 열적특성에 미치는 영향을 고찰하기 위하여 범용 에폭시수지인 DGEBF와 방향족아민 경화제 DDM, DDS 각각을 1:1의 당량비로 혼합하여 동일한 조건으로 경화하였다. 그 결과 에폭시수지 경화물의 특성은 경화제의 벤젠링 사이의 관능기 구조에 따라 매우 큰 영향을 받았다. 즉, 벤젠링 사이에 길이가 길고 bulky한 술폰기를 포함한 DDS는 반응성, 열안정성, 밀도, shrinkage($\%$), 선팽창계수, 인장탄성율. 인장강도, 굴곡탄성율, 굴곡강도의 값이 벤젠링 사이에 메틸기를 가지는 DDM 경화물계 보다 높게 나타났지만, epoxide기의 전환율, 유리전이온도의 값은 낮게 나타냈다. 이것은 술폰기의 강한 전기음성도와 메틸기의 전기 양성적인 repulsive한 성질의 차이에 의한 영향인 것으로 판단된다. 굴곡 파단면의 관찰 결과는 DDS 경화물계의 각개 grain이 불규칙적으로 분포되어 있음을 확연하게 보여준다.

• 한국세라믹학회지
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• 제28권1호
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• pp.11-18
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• 1991

A precipitation method, one of the most effective liquid phase reaction methods, was adopted in order to prepare high-tech Al2O3/ZrO2 composite ceramics, and the effects of stress-induced phase transformation of ZrO2 on thermal shock behavior of Al2O3-ZrO2 ceramics were investigated. Al2(SO4)3.18H2O, ZrOCl2.8H2O and YCl3.6H2O were used as starting materials and NH4OH as a precipitation agent. Metal hydroxides were obtained by single precipitation(process A) and co-precipitation(process B) method at the condition of pH=7, and the composition of Al2O3-ZrO2 composites was fixed as Al2O3-15v/o ZrO2(+3m/o Y2O3). Critical temperature difference showing rapid strength degradation by thermal shock showed higher value in Al2O3/ZrO2 composites(process A : 20$0^{\circ}C$, process B : 215$^{\circ}C$) than in Al2O3(175$^{\circ}C$). The improvement of thermal shock property for Al2O3/ZrO2 composites was mainly due to the increase of strength at room temperature by adding ZrO2. The strength degradation was more severe for the sample with higher strength at room temperature. Crack initiation energies by thermal shock showed higher values in Al2O3/ZrO2 composites than in Al2O3 ceramics due to increase of fracture toughness by ZrO2.