• 제목/요약/키워드: 종 그루브

검색결과 5건 처리시간 0.018초

타이어 패턴의 종그루브 인자에 따른 그루브 원더링 및 소음 특성 연구 (The Study on the Characteristics of Groove Wandering and Noise Caused by the Design Parameter of Longitudinal Groove on the Tire's Pattern)

  • 한진혁;황성욱;강용구;한민현
    • 한국기계가공학회지
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    • 제10권5호
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    • pp.110-116
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    • 2011
  • Water on a road surface can lower the coefficient of friction of vehicle tires and it involves lots of risks. One way to prevent water from staying is to cut many "rain grooves" into the edges of the pavement parallel. Such grooves, however, can exert unwanted side forces, particularly on passenger tires, which cause "Groove Wander" making the drivers uncomfortable. The "Groove Wander" is somewhat related to vehicle geometry, but is more strongly related to interaction between road grooves and tire tread's longitudinal grooves. This thesis tries to examine principles to estimate "Groove Wandering" effect focusing on the design of longitudinal groove. Additionally, it studied how to reduce pipe resonance longitudinal grooves form in the contact patch.

현시적 유한차분법을 이용한 볼나사 시스템의 열해석 (Thermal Analysis of Ballscrew Systems by Explicit Finite Difference Method)

  • 민복기;박천홍;정성종
    • 대한기계학회논문집A
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    • 제40권1호
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    • pp.41-51
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    • 2016
  • 볼나사 시스템은 볼과 그루브 사이에서 발생하는 마찰에 의해 온도가 상승하며, 이에 따른 열변형이 이송계의 위치결정 정도를 저하시킨다. 이를 보상하기 위해서는 볼나사 온도분포의 우선적 예측이 필요하다. 본 논문에서는 나사축 회전속도에 따른 온도분포를 해석하기 위해 볼나사 축과 너트를 각각 실린더와 중공 실린더로 가정한다. 경계조건인 대류 열전달계수, 볼과 그루브에서 발생하는 마찰토크와 접촉열전도를 볼나사 운전 및 조립 조건에 대하여 정식화 한다. 그리고, 현시적 유한차분법을 적용한 온도 분포 예측 시뮬레이터를 개발하고 그 유용성을 검증한다.

경사 그루브를 갖는 평판 실의 압력 강하 및 누설 성능 (Pressure Drop and Leakage Performances of Flat Seals with Inclined Grooves)

  • 정진우;정권종;황성호;김태호;김어진
    • Tribology and Lubricants
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    • 제38권5호
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    • pp.213-221
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    • 2022
  • This paper presents performance measurements of pressure drop and leakage flow rate of test flat seals with asymmetric inclined grooves. This study aims to reveal the influence of groove shapes, often machined in radial film riding-face seals, in forming a hydrodynamic wedge on leakage performance. A test facility was developed, and test seals were manufactured to study the effects of the inlet pressure level, ratio of inlet to outlet pressure, seal groove length, and seal groove height on the steady-state pressure drop and leakage performance. A series of tests were conducted, and the test data were compared to the predictions from a simple and efficient mathematical model using a one-dimensional Reynolds equation. The test results revealed that an increase in the inlet pressure increased the pressure drop through the test seals. The leakage flow rate increased significantly as the inlet pressure and ratio of the inlet to outlet pressure increased. The groove shape also affects seal performance. An increase in the groove length and height resulted in an evident increase in the leakage flow rate. The simple model predictions underestimated the leakage flow rates but showed good agreement with the trend in the measurements for all test operating conditions and changes in the groove shape.

조개 표면의 종방향 그루브가 공력성능에 미치는 영향 (Effect of longitudinal grooves of the scallop surface on aerodynamic performance)

  • 김태훈;최해천
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2008년도 추계학술대회B
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    • pp.2419-2421
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    • 2008
  • Some of the scallops like Amesium balloti have an excellent level-swimming ability, i.e. they can swim about 20m by single level swimming with a maximum swimming velocity of about 1.6m/s in the sea. On the other hand, some species like Patinopecten yessoensis have longitudinal grooves on the upper and lower surfaces and others do not. Therefore, in the present study, we measure the lift and drag forces on a real scallop model (Patinopecten yessoensis) in a wind tunnel. Experiments are performed at the Reynolds number of 75,000 based on the maximum chord length, which is within the swimming condition of real scallop (Re = $30,000{\sim}300,000$). To see the effect of longitudinal grooves, we measure the aerodynamic forces on a scallop model by removing the grooves. With the grooves, the lift force increases at low angles of attack (${\alpha}<10^{\circ}$). The drag force increases slightly at all the attack angles considered. The lift-to-drag ratio is increased by about 10% at ${\alpha}<10^{\circ}$.

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