• 제목/요약/키워드: Sliding Mechanism

검색결과 348건 처리시간 0.03초

미세조직 변화에 따른 AISI 52100 강의 미끄럼마멸 특성 (Sliding Wear Behavior of AISI 52100 Steel with Pearlitic and Bainitic Microstructures)

  • 윤나래;김용석
    • 소성∙가공
    • /
    • 제20권7호
    • /
    • pp.479-484
    • /
    • 2011
  • Dry sliding wear behavior of AISI 52100 steel that has a pearlite or bainite microstructure was characterized to explore the effect of microstructure on the wear of the steel. Isothermal heat treatments were employed to obtain the different microstructures. Pin-on-disk type wear tests of the steel disk were performed at loads of 25~125N in air against an alumina ball. Sliding speed and wear distance used were 0.1m/sec and 300m, respectively. Worn surfaces, wear debris and cross-sections of the worn surfaces were examined with SEM to investigate the wear mechanism of the steel. Hardness of the steel was also evaluated. Wear rate of the steel was correlated with the hardness and the microstructure. On the whole, wear resistance increased with an increase in hardness. However, the pearlite microstructure showed superior wear resistance as compared to the bainite microstructure with a similar hardness. The effect of the microstructure on the wear rate was attributed to the morphological differences of the carbide in the microstructure, which was found to have a significant effect on strain hardening during the wear.

차별서비스 네트워크에서 보장형 서비스의 공평성 향상을 위한 이중 윈도우 기반 마킹 알고리즘 (The Two Window-Based Marking Algorithm For Enhancing Fairness of Assured Services in a Differentiated Services Network)

  • 조병규;이성근;강의성
    • 정보처리학회논문지C
    • /
    • 제9C권5호
    • /
    • pp.743-748
    • /
    • 2002
  • 최근 인터넷에서 QoS(Quality of Service)를 제공하는 방법인 차별 서비스에 대해 많은 연구가 진행중이다. 차별화 서비스에서 보장형 서비스는 2등급 패킷 폐기 우선순위 방법과 RIO(RED with In and Out)를 일반적으로 사용한다. 하지만 이 방법만으로는 대역폭을 만족할 만큼 공평하게 사용자에게 제공하지 못한다. 본 논문에서는 공평성을 개선하기 위한 방법으로 TSW(Time Sliding Window) marking algorithm을 개선하여 TS2W3C(Time Sliding Two Window Three Color)marking algorithm을 제안한다. ns-2를 이용하여 제안된 메커니즘을 모의 실험을 통해 성능을 분석한 결과, 제안한 방법이 기존의 방법에 비해 공평하게 대역폭을 분배하는 것으로 나타났다.

Fe-10Mn-3.5Si 합금의 초소성에 미치는 반복 냉연 및 소둔의 영향 (Effect of Repetitive Cold Rolling and Annealing on the Superplasticity of Fe-10Mn-3.5Si Alloy)

  • 정현빈;최석원;이영국
    • 열처리공학회지
    • /
    • 제35권4호
    • /
    • pp.211-219
    • /
    • 2022
  • It is known that superplastic materials with ultrafine grains have high elongation mainly due to grain boundary sliding. Therefore, in the present study we examined the influence of grain refinement, caused by a repetitive cold rolling and annealing process, on both superplastic elongation and superplastic deformation mechanism. The cold rolling and annealing process was repetitively applied up to 4 times using Fe-10Mn-3.5Si alloy. High-temperature tensile tests were conducted at 763 K with an initial strain rate of 1 × 10-3 s-1 using the specimens. The superplastic elongation increased with the number of the repetitive cold rolling and annealing process; in particular, the 4 cycled specimen exhibited the highest elongation of 372%. The primary deformation mechanism of all specimens was grain boundary sliding between recrystallized α-ferrite and reverted γ-austenite grains. The main reason for the increase in elongation with the number of the repetitive cold rolling and annealing process was the increase in fractions of fine recrystallized α-ferrite and reverted γ-austenite grains, which undergo grain boundary sliding.

Nanoscale Processing on Silicon by Tribochemical Reaction

  • Kim, J.;Miyake, S.;Suzuki, K.
    • 한국윤활학회:학술대회논문집
    • /
    • 한국윤활학회 2002년도 proceedings of the second asia international conference on tribology
    • /
    • pp.67-68
    • /
    • 2002
  • The properties and mechanism of silicon protuberance and groove processing by diamond tip sliding using atomic force microscope (AFM) in atmosphere were studied. To control the height of protuberance and the depth of groove, the processed height and depth depended on load and diamond tip radius were evaluated. Nanoprotuberances and grooves were fabricated on a silicon surface by approximately 100-nm-radius diamond tip sliding using an atomic force microscope in atmosphere. To clarify the mechanical and chemical properties of these parts processed, changes in the protuberance and groove profiles due to additional diamond tip sliding and potassium hydroxide (KOH) solution etching were evaluated. Processed protuberances were negligibly removed, and processed grooves were easily removed by additional diamond tip sliding. The KOH solution selectively etched the unprocessed silicon area. while the protuberances, grooves and flat surfaces processed by diamond tip sliding were negligibly etched. Three-dimensional nanofabrication is performed in this study by utilizing these mechanic-chemically processed parts as protective etching mask for KOH solution etching.

  • PDF

미닫이 천정판 구조 (Sliding Ceiling Panel Structure)

  • 국승욱
    • 한국철도학회:학술대회논문집
    • /
    • 한국철도학회 2011년도 정기총회 및 추계학술대회 논문집
    • /
    • pp.1478-1485
    • /
    • 2011
  • 이 기술은 지하철 역사 특성상 천정판 개방이 수반되는 보수공사와 각종점검이 수시로 이루어지고 있는 바, 잦은 탈 부착으로 천정판이 쉽게 탈락 및 훼손되어 역사 유지관리에 어려움이 발생되고 있는 문제를 해결하기 위해 천정판의 설치 방법을 고정방식에서 탈피하여, 일부분을 미닫이 방식으로 개폐할 수 있도록 설치함으로서 천정판의 탈 부착으로 인한 훼손을 방지하고 내구성을 증대시켜 역사 천정판 교체공사 주기를 연장시키고 이에 따른 유지관리 비용 절감 효과가 있는 천정판 시공방법을 제시코자 함.

  • PDF

반복 미끄럼 접촉에 의한 표면층의 경화에 대한 해석 (The Analysis for Surface Hardening by Repeated Sliding Contact)

  • 박준목;김석삼
    • Tribology and Lubricants
    • /
    • 제13권4호
    • /
    • pp.71-78
    • /
    • 1997
  • Wear is affected by numerous factors-contact load, sliding velocity and distance, friction coefficient, material properties and environmental conditions. Among these wear factors, surface hardness is one of very important factors to determine wear. But surface hardness is varied by work hardening during repeated sliding contact. In this reason wear rate is increased or decreased with varying surface hardness, and transition of wear mechanism is happened. In this study, the surface hardening by accumulating residual stress was analyzed by considering the repeated sliding Hertzian contact model. The results showed that surface hardness was increased with increasing contact load, friction coefficient and contact number. And the depth of hardening layer, plastic layer and elastic layer depended upon contact load and number, but they didn't depend upon friction coefficient. The predicted surface hardness was about 1.5-1.8 times as hard as the material.

A Robust Control Approach for Maneuvering a Flexible Spacecraft

  • Sung, Yoon-Gyeoung;Lee, Jea-Won;Kim, Hunmo
    • Journal of Mechanical Science and Technology
    • /
    • 제15권2호
    • /
    • pp.143-151
    • /
    • 2001
  • In the paper, a robust control mechanism is presented to maneuver a flexible spacecraft with the deflection reduction during large slewing operation at the same time. For deflection reduction and maneuvering of the flexible spacecraft, a control mechanism is developed with the application of stochastic optimal sliding-mode control, a linear tracking model and input shaping technique. A start-coast-stop maneuver is employed as a slewing strategy. It is shown that the control mechanism with he strategic maneuver results in better performance and is more efficient than rigid-body-like maneuver, by applying to the Spacecraft Control Laboratory Experiment (SCOLE) system in a space environment.

  • PDF

암반 사면의 복합 파괴 메커니즘 규명 (Complex failure mechanism of rock slopes)

  • 윤운상;정의진;박성욱;최재원
    • 한국지반공학회:학술대회논문집
    • /
    • 한국지반공학회 2006년도 추계 학술발표회
    • /
    • pp.268-273
    • /
    • 2006
  • Slope failures can be occurred by complex mechanism. In this cases, failures shows characteristics of complex failure mechanism during progressive mass movements. A case is a merged large slide with two sliding events triggered by slip on fault plane. Another case shows extension of failure area by sliding or subsidence at backyards of toppling areas. Generally, areas of progressive failures have wider than them of simple events.

  • PDF

항공기 브레이크 재료용 탄소/탄소 복합재료의 마찰 및 마모 거동 (Friction and Wear Behavior of Carbon/Carbon Composites for Aircraft Brake Material)

  • 우성택;윤재륜
    • Tribology and Lubricants
    • /
    • 제9권1호
    • /
    • pp.62-69
    • /
    • 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.

입방정계 순 금속 Fe, Cu의 미끄럼 마멸 거동 (Sliding Wear Behavior of Pure Metal, Fe and Cu Having a Cubic Crystal System)

  • 이슬기;김용석
    • 소성∙가공
    • /
    • 제19권6호
    • /
    • pp.357-362
    • /
    • 2010
  • Dry sliding wear behavior of pure Fe and Cu which have BCC and FCC crystal structure, respectively, was investigated. The wear characteristics of the pure metals with different crystal structure were compared. Dry sliding wear tests were carried out using a pin-on-disk wear tester at various loads under the constant sliding speed condition of 0.15 m/s against a silica ball at room temperature. Sliding distance was fixed as 600 m for all wear tests. Wear rate of a specimen was calculated by dividing the weight loss of the specimen after the test by the specific gravity and sliding distance. Worn surfaces and wear debris were analyzed by SEM. The wear of both pure Fe and Cu proceeded with surface deformation, resulting in similar wear rates despite of their structure difference under the current test conditions. Wear rates of both metals were low if the surface deformation due to wear forms thick surface-deformation layer that is strain hardened beneath the wearing surface. The pure Cu specimens showed a lot of oxides on the worn surface when tested at low loads less than 5 N, which resulted in very low wear rate.