• Title/Summary/Keyword: 고온실린더

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Numerical Study of Natural Convection in a Square Enclosure with an Inner Circular Cylinder for Rayleigh Number of 107 (107의 Rayleigh 수에서 원형 실린더가 존재하는 사각형 실린더 내부의 자연대류에 관한 수치적 연구)

  • Yu, Dong-Hun;Yoon, Hyun-Sik;Ha, Man-Yeong
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.34 no.8
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    • pp.739-747
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    • 2010
  • Numerical calculations are carried out for evaluating the natural convection induced by the temperature difference between a hot inner circular cylinder and a cold outer square enclosure. A two-dimensional solution for unsteady natural convection is obtained by using the finite volume method to model an inner circular cylinder that was designed by using the immersed boundary method (IBM) for a Rayleigh number of $10^7$. In this study, we investigate the effect of the location ($\delta$) of the inner cylinder, which is located along the vertical central axis of the outer enclosure, on the heat transfer and fluid flow. The natural convection changes from unsteady to steady state depending on the $\delta$. The two critical lower bound and upper bound positions are ${\delta}_{C,L}$ = 0.05 and ${\delta}_{C,U}$ = 0.18, respectively. Within these defined bounds, the thermal and flow fields are in steady state.

Non-uniform wall temperature effect of the flow and heat transfer of a hot circular air jet impinging on a circular cylinder (비균일 벽면 온도가 원형 실린더에 충돌하는 고온 제트 유동 및 열전달에 미치는 영향)

  • Hong, Gi-Hyeok;Gang, Sin-Hyeong
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.21 no.7
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    • pp.882-890
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    • 1997
  • A buoyant jet flow impinging on a circular cylinder is investigated including heat conduction through the cylinder. Temperature and flow fields are obtained by an iterative method, and the effects of the non-uniform wall temperature on the flow and heat transfer are analyzed. Effects of three-dimensionality and the traversing of the jet are also included. Nusselt number over the cylinder surface for the conjugate case is relatively small as compared with the constant wall temperature case due to the small temperature gradient. As the conductivity of the cylinder becomes lower, Nusselt number decreases due to the reduced temperature gradient. Increasing jet traversing speed causes the surface temperature of the cylinder to decrease, which increases local Nusselt number over the surface.

Three-dimensional flow characteristics and heat transfer to a circular cylinder with a hot circular impinging air jet (원형 실린더에 충돌하는 고온 제트의 3차원 유동 특성 및 열전달)

  • Hong, Gi-Hyeok;Gang, Sin-Hyeong
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.21 no.2
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    • pp.285-293
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    • 1997
  • Numerical calculations has been performed for the flow and heat transfer to a circular cylinder from a hot circular impinging air jet. The characteristics of the flow and heat transfer are investigated and compared with the two-dimensional flow. The present study lays emphasis on the investigation on the flow and heat transfer of the three-dimensionality. The effects of the buoyancy force and the size of jet are also studied. The noticeable difference between the three and the two-dimensional cases is that there is axial flow of low temperature into the center-plane of the cylinder from the outside in the recirculation region. Local Nusselt number over the cylinder surface has higher value for the large jet as compared with that of the small jet since the energy loss of hot jet to the ambient air decreases with increase of the jet size. As buoyancy force increases the flow accelerates so that the period of cooling by the ambient air is reduced, which results in higher local Nusselt number over the surface.

Mist Cooling of High-Temperature Cylinder Surface (고온 실린더의 미스트 냉각)

  • Kim, Mu-Hwan;Lee, Su-Gwan;Park, Ji-Man;Lee, Pil-Jong
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.26 no.3
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    • pp.448-457
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    • 2002
  • Heat treatment such as quenching of a high-temperature cylinder is being used on steel to produce high strength levels. Especially, the mist cooling with the high and uniform surface heat flux rate s expected to contribute for better products. The experimental mist cooling curve is produced for better understanding, and two distinct heat transfer regions are recognized from the cooling curve produced. It is shown that the liquid film evaporation dominated region follows the film boiling-dominated region as decreasing the temperature of test cylinder by mist flow. Based on the intuitive view from some previous investigations, a simplified model with some assumptions is introduced to explain the mist cooling curve, and it is shown that the estimation agrees well with our experimental data. In the meanwhile, it is known that the wetting temperature, at which surface heat flux rate is a maximum, increases with mass flow rate ratio of water to air ($\varkappa$ < 10). However, based on our experimental data, it is explained that there exists a critical mass flow rate ratio, at which the wetting temperature is maximum, in the range of 3 < $\varkappa$ < 130. Also, it is described that despite of the same value of $\varkappa$, the wetting temperature may increase with mist velocity.

Review on Shock Absorber for Spacecraft Lander (착륙선용 충격 완충장치에 대한 고찰)

  • Lee, Chun-U
    • The Bulletin of The Korean Astronomical Society
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    • v.37 no.2
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    • pp.193.2-193.2
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    • 2012
  • 달착륙선 등과 같은 특수 목적을 위해 제작된 우주용 착륙선에는 착륙 시 전달되는 충격하중이 탑재장비로 전달되지 못하도록 연착륙(soft-landing)을 위한 충격흡수 메커니즘이 구현되어 있어야 한다. 일반적으로 자동차 및 항공기에서는 실린더와 피스톤으로 구성된 유공압식 완충장치를 주로 사용하여, 피스톤 압축으로 실린더 내부 오일 또는 압축공기가 오리피스를 통하여 분출됨에 따라 유체마찰 에너지를 활용한 충격 흡수장치가 일반적이다. 그러나 이와 같은 지상 장비용 유공압식 충격흡수 메커니즘은 진공 및 무중력 우주 환경하에서 오리피스 기능 상실, 유압유 기화 현상 및 극저온/고온 환경에서의 성능저하 등의 문제점으로 인하여 우주용 착륙선 충격완충장치로 적용이 불가능하다. 따라서 기존의 우주용 착륙선의 대부분은 충격에너지를 기계적인 좌굴 소성 변형에너지로 변환하여 충격을 흡수할 수 있도록 알루미늄 허니콤을 주로 많이 사용하여 왔다. 본 연구에서는 진공 및 무중력 우주환경에서 착륙선 충격완충 장치로 적용이 가능하도록 실리콘 포옴과 스프링을 조합하여 구성하였으며, 충격완충 매체로 유압유 및 공압을 대체할 수 있도록 실리콘 포옴을 후방 사출 성형 방식으로 적용하여 오리피스를 통과한 실리콘 포옴의 변형에너지로 충격에너지를 흡수하게 함으로서 착륙 완충효율을 극대화 할 수 있도록 검토하였다.

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Simulation of the Particle Deposition on a Circular Cylinder in High-Temperature Particle-Laden Flow (원형 실린더 주위의 고온 유동에서 입자의 부착 해석)

  • Jeong, Seok-min;Kim, Dongjoo
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.18 no.2
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    • pp.73-81
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    • 2019
  • Numerical simulations are performed for the thermal fluid flow around a circular cylinder, and the particle trajectories are calculated to investigate the particle motions and deposition characteristics. We aim to understand the effects of three important parameters (particle Stokes number, temperature difference in the flow and on the cylinder surface, and thermal conductivity ratio between the fluid and the particles) on the deposition efficiency. The results show that the thermophorectic effect is insignificant for particles with large Stokes numbers, but it affects particles with small Stokes numbers. The deposition efficiency increases with the increase in temperature difference between the flow and the cylinder or the decrease in ratio of thermal conductivity of the particles to the fluid. When thermophoresis becomes significant, the particles are deposited even on the back side of the cylinder.

Wear Characteristics of Cylinder-Liner Materials for Diesel Engine at Elevated Temperature (디젤엔진용 실린더 라이너 소재의 고온 마모특성)

  • Kim, Jin-Yeol;Kim, Jae-Hoon;Oh, Kwang-Keun;Lee, Seung-Hak;Chang, Joon-Yong
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.39 no.11
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    • pp.1131-1136
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    • 2015
  • In a diesel engine, the wear of the cylinder liner occurs because of the continuous reciprocating motion of the piston ring. This wear reduces the performance of the diesel engine and shortens its service life. This study evaluated the wear characteristics of GT metal and a conventional metal used for cylinder liners using a ship's diesel engine. Wear tests were performed at temperatures of $25^{\circ}C$, $175^{\circ}C$, and $325^{\circ}C$, and under loads of 10 N, 30 N, and 50 N. The amount of wear, specific wear rate, and friction coefficient were evaluated for each condition. To analyze the wear mechanism, observations were made on an SEM. In the case of both metals, abrasive and adhesion wear occurred on the wear surfaces at room temperature, and corrosion wear was observed at high temperatures. The amount of wear and the specific wear rate of the GT metal were lower than those of the conventional metal at all temperatures, and hence it can be concluded that the wear characteristics of the GT metal are much better.

Condebelt 공정변수에 따른 국산 라이너지의 물성 변화

  • 이학래;정태민;윤혜정;허용성;김진두
    • Proceedings of the Korea Technical Association of the Pulp and Paper Industry Conference
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    • 1999.04a
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    • pp.43-43
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    • 1999
  • 98년말 동일제지에 도입 설치된 Condebelt 설비는 세계 최초의 대형생산설비로 국제적 인 관심을 모으고 있다. 이러한 첨단 Condebelt 기술의 국산화를 위해서는 국내 원료 특성 에 적합하도록 공정최적화가 요청된다. 본 연구에서는 KOCC를 원료로 이용한 라이너지를 C Conde belt를 이용하여 생산할 경우 주요 공정변수에 따른 물성 변화를 평가하고, 이를 통하 여 Condebelt 공정을 최적화하고자 실험실용 파일로트 건조기를 이용하여 Condebelt 공정의 주요 변수가 지질에 미치는 영향을 검토하였다. 실험용 Condebelt 건조장치의 상부플레이트는 18WC까지, 하부플레이트는 냉각수를 이용 하여 40-80'C까지 조절이 가능하도록 설계하였으며, 유압을 이용하여 압체 압력과 시간을 변화시킬 수 있도록 하였다. 구축된 실험장치를 이용하여 Conde belt 공정의 주요 변수인 온도, 압력, 압체시간, 유입 지필의 건조도 변화에 따른 라이너지의 물성 변화를 평가하고 이를 실린더 건조된 종이의 물성과 비교하였다. 그 결과 본 연구에서 검토된 모든 건조조건에서 Conde belt 건조된 종이가 실린더 건조 된 종이보다 높은 강도를 나타내었으며, 투기저항성과 광택도 역시 향상되었다. 투기저항성 과 광택도는 강도적 성질과 달리 유입지 건조도가 높을수록, 상부플레이트의 온도가 높을수 록 그 효과가 저하되었다. 일반적으로 KOCC를 원료로한 라이너지를 Conde belt로 제조할 경우 상부 고온챔버의 온도를 160'C, 압체압력을 5 bar로 조절하는 것이 가장 좋을 것으로 판단되었다. 원료펄프의 조성에 따른 Condebelt 공정의 건조효과를 연구한 결과 모든 펄프에서 공히 C Condebelt 건조방법이 실린더 건조방법에 비하여 물성 향상 효과가 있는 것으로 나타났으 며, 그 효과는 펼프의 리그닌 함량이 높을수록 크게 나타났다. 또 Condebelt의 물성개선 특 성을 이용한 원료비 절감 가능성을 평가하기 위해 AOCC와 KOCC를 이용하여 단층지와 이 층지를 제조하고 물성을 비교평가하였다. 그 결과 Condebelt를 이용하면 KOCC의 비율을 증가시키더라도 AOCC만을 이용하여 실린더 건조한 종이보다 우수한 물성을 얻을 수 있었다. 이러한 연구를 통하여 Condebelt 공정이 국내 저급원료로 제조된 종이의 강도 저하를 극복할 수 있는 기술임을 확인하였다.

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Factors Influencing Characteristics of Sand Core for Water Jacket in Automotive Cylinder Blocks Casting (자동차 실린더 블록 주조에서 워터 자켓용 샌드 코어 특성에 영향을 미치는 인자)

  • Kim, Ki-Jun
    • Journal of the Korea Convergence Society
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    • v.12 no.2
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    • pp.185-191
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    • 2021
  • The characteristics of the foundry sand were analyzed for water jacket core required to prevent structural deformation from the heat generated in the cylinder bore during the casting of the cylinder block of an automobile. The sand core tensile strength tester, AFS-GFN, and optical microscope were used to evaluate the its properties. If the SiO2 content is high in the foundry sand, the dimensional defects and veining defects occur due to high temperature expansion. Also, if it is too low, the core breakage, porosities, chemical burn-on defects occur. The particle size index and grain shape influenced the core strength and resin consumption, resulting in fluctuations in defect types. The higher the alkalinity of the dried sand, the lower the core strength. And the more basic, the lower the core strength. At the resin content of 1.6~1.8%, the increase in core strength after 1 hour curing was approximately at its maximum.

Effect of Prandtl Number on Natural Convection in Tilted Square Enclosure with Inner Circular Cylinder (Prandtl 수 변화가 내부 원형 실린더가 존재하는 기울어진 정사각형 밀폐계 내부의 자연대류 현상에 미치는 영향)

  • Mun, Gi Su;Choi, Changyoung;Ha, Man Yeong;Yoon, Hyun Sik
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.38 no.11
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    • pp.935-942
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    • 2014
  • A numerical analysis of the effect of the Prandtl number on the natural convection in a cold outer tilted square enclosure with an inner hot circular cylinder is presented. Several Prandtl numbers (Pr=0.1, 0.7, 7) are considered, with different angles($0^{\circ}$, $15^{\circ}$, $30^{\circ}$, $45^{\circ}$) for the enclosure and Rayleigh numbers ($Ra=10^3$, $10^4$, $10^5$). The effect of the Prandtl number on the natural convection is analyzed using isotherms and streamline and surface-averaged Nusselt numbers. The flow and heat transfer characteristics are found to be dependent on the time for $Ra=10^5$ and Pr=0.1 at angles of $0^{\circ}$ and $45^{\circ}$. However, in the other cases, the flow and heat transfer characteristics are independent of the time.The surfaceaveraged Nusselt number increases with an increase in the Prandtl number. As the Prandtl number increases, the Nusselt number becomes larger regardless of the angle for $Ra=10^5$. In particular, the Nusselt number steeply increases when the angle is $45^{\circ}$ for $Ra=10^5$ and Pr=0.1.