• 대한기계학회논문집A
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• 제20권3호
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• pp.832-842
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• 1996

Fatigue life prediction and fatigue behavior of circular notched carbon fiber reinforced plastic laminates are presented. Point and average stress criteria by Whitney and Nuismer are generalized to fatigue fracture criteria for notched laminates. Residual strength degradation model and the assumptions on the stress redistribution are introduced during the derivation of prediction equations. S-N curve, Basquin's relation, and H and H's FLPE1 are chosen for evaluation of residual strength of unnotched laminates and six prediction equations are derived. Experiments are performed using Graphite/Epoxy laminates whose fiber orientation is $[0$^\circ$/+45$^\circ$/-45$^\circ$/90$^\circ$]s. Presented prediction equations are reasonably close to experimental data and proposed appoach is found to be suitable to predict fatigue life of notched composite laminates.

• 한국전기전자재료학회논문지
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• 제31권7호
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• pp.475-480
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• 2018

We investigated the tribological properties of amorphous carbon (a-C) films deposited with CrC interlayers of various thicknesses as the adhesive layer. A-C and CrC thin films were deposited using the unbalanced magnetron (UBM) sputtering method with graphite and chromium as the targets. CrC films as the interlayer were fabricated under a-C films, and various structural, surface, and tribological properties of a-C films deposited with various CrC interlayer thicknesses were investigated. With various CrC interlayer thicknesses under a-C films, the tribological properties of CrC/a-C films were improved; the increased film thickness exhibited a maximum high hardness of over 27.5 GPa, high elastic modulus of over 242 GPa, critical load of 31 N, residual stress of 1.85 GPa, and a smooth surface below 0.09 nm at the condition of 30-nm CrC thickness.

• 한국진공학회:학술대회논문집
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• 한국진공학회 2013년도 제45회 하계 정기학술대회 초록집
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• pp.292.2-292.2
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• 2013

Graphene, a two-dimensional graphite material consisting of sp2-hybridized carbons. The properties of graphene such as extremely high carrier mobility, high thermal conductivity, low resistivity, large specific make it a promising materail of divices and material. Typically, poly (methyl methacrylate) (PMMA) is used when graphene transfer to other substrates. To remove PMMA on graphene, people used to dip the graphene into the acetone. However, it is known that the remove of PMMA on the graphene is difficult to completely using the acetone. Therefore, to remove the PMMA on the graphene surface, many research groups have employed various methods such as the thermal treatment, photothermal method, and other solvent. Nevertheless, a part of PMMA still remain on graphene surface. Usually, to observe the residual PMMA on graphene surface, topography of graphene surface scanned by atomic force microscopy is used. However, in that case, we can not distinguish PMMA and other particles. In this study, to confirm the residual PMMA on graphene surface, we employed novel measurement technique which is available to distinguish PMMA and other particles by means of photothermal effect.

• 한국주조공학회지
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• 제17권6호
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• pp.577-584
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• 1997

Evaluation of rolling contact fatigue damage as well as material development for roll of rolling mill is being studied until quite recently. In this paper, a focus has been imposed on evaluating the rolling contact fatigue damage. In order for this, the accumulating process of rolling contact damage using the ferritic, pearlitic and bainitic DCI has been analyzed by X-ray diffraction technique. The main finds are; 1) The graphite in DCI is considered to be a cause of interfering in the redistribution of stress. Eventually, it results in the branching of crack. 2) The evaluation of rolling contact fatigue damage can be estimated in terms of the change of residual stress and/or a half-value breadth on surface during rolling contact.

• 대한기계학회논문집
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• 제7권4호
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• pp.404-409
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• 1983

The warping of unsymmetric laminated composites is induced by residual curing stress at the room temperature. Classical lamination theory (C.L.T.) predicts the room temperature shapes of all unsymmetric laminates to be a saddle. Experimental observations, however, indicate some unsymmetric laminated composites have cylindrical room temperature shapes. This anomalous behavior is explained by the extention of C.L.T. which involves Von Karman's large deflection theory. It is shown that, depending on the thickness, width, length, curing temperature and room temperature of the laminate, critical boundaries of the shape change are determined. Theoretical predictions are compared with experimental results of Toray Graphite/Epoxy {O$_{n}$/90$_{n}$}$_{T}$./....

• 설비공학논문집
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• 제6권4호
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• pp.406-416
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• 1994

In this study the reactor design procedure and method of solid-solid-gas chemical heat pump system using STELF technology were investigated. For manufacturing IMPEX block which is the kernel of reactor, proper salt pair should be selected, and equilibrium temperature drop and COP should be examined for selected salt pair. Moreover, apparent density, residual porosity, and graphite ratio should be calculated to give minimum block volume and mass, and maximum energy density without causing heat and mass transfer problems. Since heat exchange area can be changed with operating condition, reactor diameter, length, and stainless steel thickness should be decided for desired specifications. These procedure and method were applied to the case study of 6kW cold production and 8 hours storage capacity reactor.

• 한국구조물진단유지관리공학회 논문집
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• 제20권4호
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• pp.9-18
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• 2016

이 연구에서는 태양열 에너지 저장용도로 사용하기 위한 시멘트 기반 복합재료의 열적 및 역학적 특성을 파악하였다. 다양한 시멘트 재료의 배합이 섬유보강 시멘트 기반 복합재료의 열적 및 역학적 특성에 미치는 영향을 파악하기 위한 실험연구를 수행하였다. 시멘트 기반 복합재료의 역학적 특성으로써 열싸이클 전과 후의 압축강도 및 인장강도를 측정하였다. 또한, 섬유보강 시멘트 기반 복합재료의 열적 특성으로써 열전도율과 비열을 측정하였다. OPC와 슬래그를 포함한 배합의 잔류압축강도가 가장 크게 나타난다. 그라파이트를 혼합한 배합의 열전도율이 크게 나타나며, 이는 그라파이트가 열저장 시스템의 효율적인 축열과 방열에 유리함을 의미한다. 또한, CSA 또는 지르코늄의 첨가는 섬유보강 복합재료의 비열을 증가시킨다. 실험연구결과는 잡광형 태양열 발전소에서 고성능 복합재료를 사용하는 열저장 시스템 설계에 기초자료로 활용될 수 있다.

• 분석과학
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• 제9권1호
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• pp.43-51
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• 1996

가온 가압법에 의하여 합성된 Li-EaGICs, Li-EGICs를 자발적으로 분해시켜서 이들의 deintercalation 과정에 대하여 X-선 회절분석, 열분해분석 및 전기비저항값을 측정하여 이들 결과에 대하여 토론하였다. Intercalation에 대한 X-선 회절분석 결과에 의하면, Li-EaGICs 와 Li-EGICs는 1 stage가 완전하게 형성되지 않았고, 주로 저차 stage가 형성되었다. 또한 deintercalation 결과에 의하면, 4주 이후에는 deintercalation이 멈추었으며 Li-EGDlCs는 Li-EaGDlCs보다 층간 잔유 금속을 많이 가지고 있음을 알 수 있다. 열분해분석 결과에 의하면 두가지 하합물 모두 강한 밭열반응을 수반하였으며, 또한 $400^{\circ}C$ 이상에서는 반응이 수반되지 않는 것으로 보아 intercalants들이 완전히 deintercalation 되었음을 알 수 있다. 전기 비저항 측정 결과에 의하면 Li-EGDlCs는 상대적으로 낮은 비저항값을 가지고 있었으며, Li-EaGDICs는 이상적인 비저항 곡선을 나타내었다. 이들 결과로부터 Li-EaGICs가 Li-EGlCs 보다 2차 전지의 양극재료로서 더 좋은 성질을 가지고 있음을 알 수 있다.

• 콘크리트학회논문집
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• 제28권4호
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• pp.395-405
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• 2016

이 연구에서는 태양열 에너지 저장용도로 사용하기 위한 섬유보강 모르타르의 열적 및 역학적 특성을 파악하였다. 다양한 시멘트 복합재료의 배합이 섬유보강 모르타르의 열적 및 역학적 특성에 미치는 영향을 파악하기 위한 실험연구를 수행하였다. 섬유보강 모르타르의 역학적 특성으로서 열싸이클 전과 후의 압축강도 및 인장강도를 측정하였다. 또한, 섬유보강 모르타르의 열적 특성으로서 열전도율과 비열을 측정하였다. OPC와 그라파이트를 포함한 배합의 잔류압축강도가 가장 크게 나타난다. 알루미나 시멘트를 혼합한 배합의 비열이 크게 나타나며, 이는 알루미나시멘트가 열저장 시스템의 효율적인 축열과 방열에 유리함을 의미한다. 또한, 그라파이트의 첨가는 섬유보강 복합재료의 비열을 증가시킨다. 실험연구결과는 콘크리트를 $450^{\circ}C$ 이상의 열저장 매체로 활용하기 위한 프로토타입 시스템 설계에 실제적인 기초자료로 활용될 수 있을 것으로 사료된다.

• Steel and Composite Structures
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• 제35권3호
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• pp.439-447
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• 2020

This paper presents two sets of full three-dimensional thermoelastic finite element analyses of superimposed thermo-mechanically loaded Spar Wingskin Joints made with laminated Graphite Fiber Reinforced Plastic composites. The study emphasizes the influence of residual thermal stresses and material anisotropy on the inter-laminar delamination behavior of the joint structure. The delamination has been pre-embedded at the most likely location, i.e., in resin layer between the top and next ply of the fiber reinforced plastic laminated wingskin and near the spar overlap end. Multi-Point Constraint finite elements have been made use of at the vicinity of the delamination fronts. This helps in simulating the growth of the embedded delamination at both ends. The inter-laminar thermoelastic peel and shear stresses responsible for causing delamination damage due to a combined thermal and a static loading have been evaluated. Strain energy release rate components corresponding to the Mode I (opening), Mode II (sliding) and Mode III (tearing) of delamination are determined using the principle of Virtual Crack Closure Technique. These are seen to be different and non-self-similar at the two fronts of the embedded delamination. Residual stresses developed due to the thermoelastic anisotropy of the laminae are found to strongly influence the delamination onset and propagation characteristics, which have been reflected by the asymmetries in the nature of energy release rate plots and their significant variation along the delamination front.