• 한국지반공학회논문집
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• 제38권2호
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• pp.29-38
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• 2022

마찰 방향에 따른 전단 저항의 이방성을 지반 구조물에서 선택적으로 이용할 수가 있다. 예를 들어서, 축방향으로 하중을 가하는 깊은 기초, 소일 네일링, 타이백 등은 큰 전단 저항이 유발되므로 하중 전달 능력을 증가시키지만, 이와 반대로 말뚝 관입과 흙 시료 채취 등은 최소화된 전단 저항만 유발된다. 기존 연구는 뱀 비늘의 기하학적 형상과 유사한 표면 돌출부를 갖는 플레이트와 흙 경계면에서 유발되는 전단 저항 변화를 확인하였다. 본 논문에서는 표면 돌출부의 형상에 따른 경계면 마찰각의 변화를 정량적으로 평가하였다. 수정된 직접 전단 시험기를 이용하여 상대 밀도가 40%로 조성된 모래 시료에 대해 9개의 플레이트, 2개의 전단 방향(전단 시 돌출부 높이가 증가와 감소하는 방향), 그리고 3개의 초기 수직 응력(100kPa, 200kPa, 300kPa) 조건으로 총 51가지 경우를 실험 하였다. 실험 결과, 전단 응력은 돌출부 높이가 높을수록, 돌출부 길이가 짧을수록, 돌출부 높이가 증가하는 전단 방향에서 크게 나타났다.

• International Journal of Safety
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• 제5권1호
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• pp.10-16
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• 2006

A suspended hemispherical silicon asperity moving over a silicon plate was simulated. The simulation results on friction and wear in the interface between the two can help obtain more durable miscroscale structures. Silicon structures were constructed with Tersoff three-body potential. Dependence of friction and wear of the asperity on both the atomic arrangement in the plate and the moving direction was investigated under the condition that the asperity is subject to the attractive normal force due to the plate. The results show that the variation of friction force with the movement of asperity, and the occurrence of adhesive wear are attributed to the formation and rupture of asperity, junction between the asperity and the plate. The friction force and wear are smaller when the asperity is incommensurate with the plate, and they also depend on the moving direction of the asperity over the plate.

• 터널과지하공간
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• 제23권5호
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• pp.401-412
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• 2013

전단거동에 의한 절리면의 거칠기 변화가 전단강도에 미치는 영향을 조사하기 위하여 절리면 강도가 상이한 편마암, 화강암 및 셰일 시료를 이용하여 순차적 다단계 전단시험을 수행하였다. 시험단계별로 절리면 프로파일의 고도를 측정하여 거칠기 계수를 산정하고 미세 거칠기 빈도 변화를 조사하였다. 거칠기 감쇠에 대한 최적의 거칠기 계수를 산정하여 반복된 전단거동에 의한 순차적 거칠기 감쇠특성을 고찰하였다. 전단강도식을 산정하여 점착력과 마찰각의 차별적 변화양상을 도출하였으며, 표면 거칠기의 마모, 파쇄 및 재형성에 의한 미세 거칠기 빈도변화를 조사하여 강도계수 변화의 원인적 요인을 분석하였다. 또한, 미세 거칠기 변화양상이 전단강도에 미치는 영향을 절리면 강도를 고려하여 분석하였다.

• 한국터널지하공간학회 논문집
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• 제15권4호
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• pp.431-442
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• 2013

기존의 연구에서 삼각형 돌출부의 크기 즉 돌출부 길이 및 돌출부 경사각 변화에 따른 전단거동 및 파괴 형상 특성에 대한 광범위한 실험적 연구는 부족하였다. 본 연구에서는 직접전단시험기를 사용하여 삼각형 돌출부의 전단거동에 있어서 돌출부의 길이 및 경사각 특성이 표면 돌출부의 파괴 형상 특성에 미치는 영향을 규명하고자 한다. 이를 위하여 돌출부 길이는 4가지로 변환하였고, 수직응력은 3가지로, 그리고 돌출부 경사각은 3개의 각도로 변환하면서 총 36회의 시험을 수행하였다. 시험을 수행한 시편은 3차원 형상측정기를 사용하여 파괴 형상 특성을 정량적으로 분석하였다. 이러한 시험을 통하여, 수직응력 변화에 따른 돌출부의 파괴 형상 특성을 조사하였다. 또한 각각의 경사각에서 돌출부의 길이를 변화시켜 시험을 수행함으로써, 특정 수직응력 하에서 돌출부가 파괴되는 길이 및 높이를 정의하였다.

• Tribology and Lubricants
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• 제21권6호
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• pp.289-295
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• 2005

Most machine element, such as gears and bearings, are operated in the mixed lubrication region. Contact between two asperities has an effect on machine life by increasing local pressure. To estimate fatigue life exactly, asperity contact should be considered as a factor of fatigue life because this happening produce friction, abrasion and make flash temperature. In this paper, asperity contact is considered as a result of film breakdown when lubricant pressure is not enough to separate two asperities. Contact pressure is calculated to asperity overlap region and added to lubricant pressure. For this model, numerical procedure is introduced and the result on surface roughness and velocity for wheel bearing is presented. Results of EHL analysis for wheel bearing show that asperity contact is occurred at the edge ofEHL conjunction where has a insufficient lubricant pressure to separate two surface.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2005년도 추계학술대회 논문집
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• pp.616-621
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• 2005

Most machine element, such as gears and bearings, are operated in the mixed lubrication region. Contact between two asperities has an effect on machine life by increasing local pressure. To estimate fatigue lift exactly, asperity contact should be considered as a factor of fatigue liff because this happening produce friction, abrasion and make flash temperature. In this paper, asperity contact is considered as a result of film breakdown when lubricant pressure is not enough to separate two asperities. Contact pressure is calculated to asperity overlap region and added to lubricant pressure. For this model, numerical procedure is introduced and the result on surface roughness and velocity for wheel bearing is presented. Results of EHL analysis for wheel bearing show that asperity contact is occurred at the edge of EHL conjunction where has a insufficient lubricant pressure to separate two surface.

• 한국윤활학회:학술대회논문집
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• 한국윤활학회 2000년도 제31회 춘계학술대회
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• pp.34-41
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• 2000

Surface roughness plays a significant role in friction, wear, and lubrication in machine components. Most engineering surfaces have the nongaussian distrubution. So, in this study, contact simulation are conducted for not only gaussian surfaces but also nongaussian surfaces. Nongaussian rough surface censidering the kurtosis is generated numerically, And the effects of kurtosis on real contact area fraction, average gap, and mean asperity contact pressure are studied. It will be shown that the real contact area fraction and the mean asperity contact pressure are sensitive to the characteristics of surface geometry according to kurtosis.

• 한국정밀공학회지
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• 제18권10호
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• pp.53-60
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• 2001

Surface roughness plays a significant role in friction, wear, and lubrication in machine components. Most engineering surfaces have the nongaussian height distribution. So, in this study, contact simulations are conducted for not only gaussian surfaces but also nongaussian surfaces. Nongaussian rough surface considering the kurtosis is generated numerically And the effects of kurtosis on real contact area fraction, average gap, and mean asperity contact pressure are studied. It will be shown that the real contact area fraction and the mean asperity contact pressure are sensitive to the characteristics of surface geometry according to kurtosis.

• Journal of Mechanical Science and Technology
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• 제15권7호
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• pp.859-865
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• 2001

This paper reports on the theoretical analysis of mixed lubrication for the piston ring. The analytical model is presented by using the average flow and asperity contact model. The cyclic variations of the nominal minimum oil film thickness are obtained by numerical iterative method. The total friction is calculated by using the hydrodynamic and asperity contact theory. The effect of the roughness height, pattern, and engine speed on the nominal minimum film thickness, friction force, ad frictional power losses are investigated. As the roughness height increases, the nominal oil film thickness and total friction force increase. Also, the effect of the surface roughness on the boundary friction is dominant at low engine speed and high asperity height. The longitudinal roughness pattern shows lower mean oil film pressure and thinner oil film thickness compared to the case of the isotropic and transverse roughness patterns.

• Tribology and Lubricants
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• 제15권4호
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• pp.335-342
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• 1999

Corrosion of the disk has been an ongoing concern for the manufacturers of hard disk drives. With the advent of magnetoresistive (MR) head, very low levels of corrosion and contamination become more critical since the raised defects and corrosion products on the disk surface-anything that heats the MR sensor due to the contact-can distort the output signal of the head. This phenomenon is called as thermal asperity. In this paper, the effect of corrosion as a form of Co migration on the occurrence of thermal asperity in MR drives was investigated. The corrosion test at high temperature (60$^{\circ}C$) and high relative humidity (80%) was emphasized in this study and the testing results at ambient condition were compared. The corrosion on the disks was characterized as the amount of Co ion migration using an ion chromatography (IC) and a time-of-flight secondary ion mass spectroscopy (TOF-SIMS). It is proved that corrosion on the disk surface after storage testing is closely correlated to the amount of Co ions migration from the magnetic layer to disk surfaces and higher Co migration causes more thermal asperities in the drive. In order to reduce Co migration, several methods such as burnishing process and structure of the carbon overcoat were investigated. It is found that the hydrogenated carbon overcoat shows the least Co migration among different types of overcoat layer. However, the most effective way to reduce Co migration is the application of Cr layer between the overcoat and the magnetic alloy layer.