• Proceedings of the Korean Institute of Surface Engineering Conference
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• 2001.06a
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• pp.54-54
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• 2001

End hall type 이온건을 이용하여 다층 다이아몬드상 차본(DLC) 필름을 M2 steel 기판 위에 합성하였다. 다충 다이아몬드상 카본 필름은 순수 DLC 필름과 실라콘 함유 D DLC 필름의 조합으로 구성되어 있으며, $C_6H_6$ 및 수소 희석된 30% 를 사용하여 증착 하였다. 생성된 DLC 박막의 조성은 $C_6H_6$과 $SiH_4$ 가스의 비를 조절함으로써 변화시켰으며, 250 kHz의 고주파 전원을 바이어스 전원으로 사용하여 박막의 물성을 변화시켰다. DLC 박막의 두께와 다층의 구조 및 종류(2충, 4충)는 코팅 공정의 실험 변수로서 변화시켰다. 직경 3 mm의 루비볼을 사용하여 ball-on-disk 방식으로 마모 시험을 행하였으며, 하중은 490 g, 500 rpm에서 상대습도를 5 % 이하와 80 % 이상으로 변화시켜가며 시행하였다. 100,000 cycle 회전 후 측정된 시편의 마모상태는 5 % 이하의 습 도에서 4층 구조의 박막이 2충 구조의 박막보다 2배 이상 낮은 마모률을 보였으며 그 값은 각각 $2~3{\times}\;10^{-8}\;\textrm{mm}^3/rev$와 $1~2{\times}\;10^{-7}\;\textrm{mm}^3/rev$로 나타내었다. 80% 이상의 습도에서도 마모률의 변화는 저습에서의 경우와 유사하였다. 또한 Si함유 DLC 다층 박막이 저습 및 고습에서 더욱 안정한 마찰 마모 거동을 보였다.

• Tribology and Lubricants
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• v.9 no.1
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• pp.62-69
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• 1993

Friction and wear behavior of a carbon/carbon composite material for aircraft brake material was experimentally investigated. Friction and wear test setup was designed and built for the experiment. Friction and wear tests were conducted under various sliding conditions. Friction coefficients were measured and processed by a data acquisition system and amount of wear measured by a balance. Stainless steel disk was used as the counterface material. Temperature was also measured by inserting thermocouple 2.5 mm beneath the sliding surface of the carbon/carbon composite specimen. Wear surfaces were observed by SEM, and analyzed by EDAX. The experimental results showed that sliding speed and normal force did not have significant effects on friction coefficient and wear factor of the composite. Temperature increase just below the surface was not large enough to cause any thermal degradation or oxidation which occurred at higher temperature when tested by TGA. Wear film was generated both on the specimen and on the counterface at relatively low sliding speed but cracks, grooves, and wear debris were observed at high sliding speed. Friction coefficient remained almost constant when the sliding speed or normal load was varied. It is believed that the adhesive and abrasive components contributed mainly to the friction coefficient. Wear behavior at low sliding speed was governed by wear film formation and adhesive wear mechanism. At high speed, fiber orientation, ploughing by counterface asperities, and fiber breakage dominated wear of the carbon/carbon composite.

• Tribology and Lubricants
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• v.29 no.6
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• pp.372-377
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• 2013

This study investigated the interface temperatures for the sliding friction of three types of pins fabricated with thermocouple wires by the suction casting method. Optical microscopy was used to examine the surrounding material state at the bonding interface with the thermocouple wires. Friction tests were performed under dry sliding conditions against stainless steel 304 at nominal stresses of 1.42-4.25 MPa and sliding speeds of 0.5-1.25 m/s. Tribological data were collected using a custom-made pin-on-disk apparatus that measured the interface temperature and corresponding friction coefficient. Static tests were performed to demonstrate the functionality and reliability of the thermocouple wires-combined temperature sensor (TCTS). Each TCTS showed good linearity and sensitivity and very similar response times for the thermocouple and critical temperature during sliding friction.

• Journal of Power System Engineering
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• v.18 no.5
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• pp.94-99
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• 2014

In this study, AISI M2 powder was selected primarily through various literature in order to improve the hardness and wear resistance. Among the laser metal deposition parameters, laser power was studied to improve the deposition efficiency in the laser metal deposition using a diode pumped disk laser. SKD61 hot work steel plate and AISI M2 powder were used as a substrate and powder for laser metal deposition, respectively. Fixed parameters are CTWD, focal position, travel speed, powder feed rate, etc. Experiments for the laser metal deposition were carried out by changing laser power. Through optical micrographs analysis of cross-section in LMD track, effect of the major parameters were predicted by track pitch. As the track pitch increased, so the reheated zone width, the overlap width and the minimum thickness was decreased. The hardness was decreased in the HAZ area, the hardness in the reheated HAZ area was decreased significantly and regularly in particular.

• KSTLE International Journal
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• v.3 no.1
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• pp.38-42
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• 2002

Diamond-like Carbon(DLC) films were deposited on Si wafers by an RF-plasma-assisted CVD using CH$_4$gas. Tribological tests were conducted with the use of a rotating type ball on a disk friction tester with dry air. This study made use of four kinds of mating balls that were made with stainless steel but subjected to different annealing conditions in order to achieve different levels of hardness. In all load conditions, testing results demonstrated that the harder the mating materials, the lower the friction coefficient was. The friction coefficients were fecund to be lower with austenite mating balls than with fully annealed martensite balls. Conversely, the high friction coefficient found in soft martensite balls appeared to be caused by the larger contact area between the DLC film and the ball. The wear tracks on DLC films and mating balls could prove that effect. Measuring the wear track of both DLC films and mating balls revealed a similar tendency compared to the results of friction coefficients. The wear rate of austenite balls was also less than that of fully annealed martensite balls. Friction eoefficients decrease when applied leads exceed critical amount. The wear track on mating balls showed that a certain amount of material transfer occurs from the DLC film to the mating ball during a high friction process. Raman Spectra analysis Showed that the transferred materials were a kind of graphite and that the contact surface of the DLC film seemed to undergo a phase transition from carbon to graphite during the high friction process.

• Proceedings of the KIEE Conference
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• 2008.07a
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• pp.1476-1477
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• 2008

This paper reports on a flexible flap valve actuated by electromagnetic force under a constant pressure source. The flexible flap valve consists of the three main components: a flexible flap with a steel disk embedded in PDMS, an electromagnetic actuator and two glass plates with inlet and outlet. Sealing lip structures for improving the valve characteristics are added on the outlet of the bottom glass substrate. The flap valve is fabricated by the spin-coating process, the EDM process, SU-8 mold process and oxygen plasma treatment. The dimension of an assembled flap valve is $12mm{\times}20mm{\times}28mm$. The stroke volume of the flap valve is measured for various pressures and open times. When the input voltage of 30 V is applied for 0.33 s, the minimum stroke volume of the flap valve is 70 ${\mu}L$ at 50 kPa.

• Proceedings of the Korean Vacuum Society Conference
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• 2010.08a
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• pp.62-62
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• 2010

인공관절은 노인성 질환이나 자가 면역질환, 신체적인 외상 등에 의한 관절의 손상 부위를 대체하기 위해 고안된 관절의 인공대용물로써 최근 인구의 고령화와 질병, 사고의 증가에 따라 그 수요가 급격히 증가하는 추세를 보이고 있다. 인공관절의 소재로는 현재 metal-on-polymer(MOP) 소재가 가장 많이 사용되고 있는데, metal 소재로서는 Co-Cr계 합금이, polymer 소재로서는 초고분자량 폴리에틸렌 (ultra high molecular weight polyethylene) 이 주로 사용되고 있다. MOP 소재의 경우 충격흡수의 장점이 있는 반면 wear debris에 의한 골용해로 인해 관절이 느슨해지는 문제점이 발생하여 재시술의 주요 원인이 되고 있다. 또한 metal 소재로 주로 사용되고 있는 Co-Cr계 합금의 경우 인공관절의 마모, 부식 현상에 의해 Co, Cr등이 체내에 용출되어 세포독성의 문제를 일으킬 수 있다는 단점을 가지고 있다. 본 연구에서는 고체원소 이온주입 기술을 이용하여 316L stainless steel 기판에 niobium을 이온 주입 한 후 niobium nitride (NbN) 박막을 증착하여 counterpart 소재인 초고분자량 폴리에틸렌(UHMWPE) 의 마모를 줄이는 실험을 진행하였다. Pin-on-disk tribometer를 통해 마모 테스트를 진행하여 NbN 박막의 내마모특성을 평가하였으며, 박막의 결정구조 및 화학적 특성을 평가하기 위해 XRD, AES 분석을 수행하였다. 또한 박막의 경도와 표면조도를 측정하기 위해 micro hardness tester, AFM을 이용하였다.

• Tribology and Lubricants
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• v.11 no.5
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• pp.59-65
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• 1995

Tribological behaviors of nitrogen incorporated amorphous diamond-like carbon films were experimentally measured under a vacuum ($3 \times 10^{-5}$ Torr) using a ball (AISI 52100 steel)-on-disk wear-rig. Nitrogen incorporated DLC films were deposited by r.f. plasma assisted chemical vapor deposition method. Mixtures of benzene and ammonia or nitrogen gases were used as the reaction gases for the r.f. PACVD, and Si (100) wafer was used as the substrate. In the tribo-test, effects of DLC film thickness and normal load in friction were measured and discussed. Results showed that friction of nitrogen incorporated DLC films from a mixture gas of benzene and ammonia was lower than that of 100% benzene, specially in the measurement of minimum coefficient of friction. Differences in frictional characteristics of nitrogen incorporated DLC films were explained with the changes in chemical structures of the films. Result also showed that friction of DLC films increased with the sliding contact cycle, which remarkably accompanied with roll-shaped wear debris. Mechanisms and roles of the polymer-like wear debris were presented and discussed.

• Journal of the Korean Society for Heat Treatment
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• v.20 no.2
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• pp.78-83
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• 2007

CrN coatings were deposited by cathodic arc ion plating method on the SKD11 steel substrates. Atmosphere temperature of $350^{\circ}C$, arc current of 90 A, nitrogen partial pressure of 1.0-5.3 Pa, and negative bias voltage of 30-135 V were selected. The characteristics of microstructure were investigated with XRD. Hardness, adhesion and friction coefficient measured by microhardness tester, scratch tester, and ball on disk tribometer. Microstructures depended on nitrogen partial pressure and bias voltage. The preferred orientation of the films was changed from (200) to (111) with decreasing pressure and increasing bias voltage. Adhesion properties related with microstructure, but microstructure changes slightly influenced on hardness and friction properties. The critical load.($Lc_1$) and hardness of CrN films deposited at 5.3 Pa, -30 V condition were 55 N(HF1), $2157{\pm}47\;Hk_{0.025}$. The friction coefficient were about 0.5 under dry condition.

• Transactions of Materials Processing
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• v.13 no.8
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• pp.716-722
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• 2004

Effects of sliding speed, applied load, and thickness of PMMA (Poly Methyl Methacrylate) coating layers on their dry sliding frictional and wear behavior were investigated. Sliding wear tests were carried out using a pin-on-disk wear tester. The PMMA layer was coated on Si wafer by a spin coating process with two different thicknesses, $1.5\mu\textrm{m}$ and $0.8\mu\textrm{m}$. AISI 52100 bearing steel balls were used as a counterpart of the PMMA coating during the wear. Normal applied load and sliding speed were varied. Wear mechanisms of the coatings were investigated by examining worn surfaces using an SEM. Friction coefficient of the coatings decreased with the increase of the applied load. Both adhesion and deformation of the coating determined the coefficient. The thicker PMMA layer with the thickness of $1.5mutextrm{m}$ showed lower friction coefficient than the thinner layer under most test conditions. Effects of sliding speed and applied load on the frictional behavior were varied depending on the thickness of the coating layer.