• Journal of Advanced Marine Engineering and Technology
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• 제29권3호
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• pp.275-280
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• 2005

Recently there has been a growing interest in the design and manufacturing of the muffler tube due to the strict environment regulations, A muffler is an important part used to reduce noise and to purify exhaust gas in cars and heavy equipment. The shape of the muffler tube and the number of the tube hole has been made variously according to the weight and function of the car. The perforating technique of the muffler tube has a great influence on the manufacturing cost. In this study, metal forming analysis has been carried out to investigate the perforating process for the muffler tube and predict an optimal forming conditions of the muffler tube, Also its simulation results by the finite element method were reflected to the die design and the manufacturing system for the muffler tube. The perforating process is performed in the longitudinal direction of the tube. According to the simulation results, when the shear angle of punch was similar to the tube curvature, the optimal shape was obtained. Also when the clearance of die was 0.2mm, the burr was minimized and optimal shear section was obtained.

• 대한기계학회논문집B
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• 제24권9호
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• pp.1139-1147
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• 2000

This paper describes that the size of inactive zone can be directly applied to design multiblade fan/scroll system. From the experimental studies using a five hole pitot tube and smoke test, it is found that the size of inactive zone has linear relations with the mean velocity of impeller inlet and cut-off angle gives a great influences to the fan efficiency. For the practical design, a function related with geometric parameters(i.e. inner radius, cord length, cut-off clearance and cut-off angle) of fan/scroll system is suggested. By using these formulas, the size and distribution of inactive zone can be predicted without the measurements through the full domain, it can be possible to use them to know the efficiency improvement for new model designed.

• 한국자동차공학회논문집
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• 제10권1호
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• pp.162-167
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• 2002

An automotive wheel bearing is one of the most important components to guarantee the service life of a passenger car. The endurance life of a bearing is affected by many parameters such as material properties, heat treatment, lubrication conditions, temperature, loading conditions, bearing geometry, internal clearance and so on. In this paper, we analyze the relation between loads and deformations of wheel bearing units. On the basis of it, we calculate the endurance life of wheel bearing units and suggest a method to determine the initial contact angle to achieve a maximum endurance life with considering stress concentration.

• Design & Manufacturing
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• 제10권3호
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• pp.34-38
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• 2016

Roll forming is a continuous production process that is mass-produced. The roll forming process is produced in various forms. The special feature of roll forming is a continuous production. Therefore, the process of cutting the material is essential. The troubles in a shearing process affects the low productivity. Accordingly, it is important to reduce the factors that inhibit the material flow. And it is difficult to apply the common shear angle. Because it is not a simple forms, such as a progressive die. This study shows how to select the angle of a shear punch and the shape of a cutting punch in the product with a specific shape. Conclusively through three different model, it is advantageous to apply the different shear angle and clearance along the forms.

• 한국도로학회논문집
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• 제11권4호
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• pp.49-58
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• 2009

현행 우리나라의 일조규정은 공동주택 및 일반 건축물을 중심으로 되어있기 때문에 도로 및 고가 구조물의 특성을 충분히 반영하지 못하고 있다. 또한, 공동주택간의 인동간격 및 인동간격이 미치는 다양한 영향에 대한 연구는 많이 이루어지고 있으나, 도로 및 고가 구조물과 주거지역과의 이격거리 및 구조물에 의해 발생되는 일조장애들의 환경적인 요소와 그에 따른 인자에 관한 연구는 미비하다. 따라서 본 연구에서는 도로 및 고가 구조물 중 주거지역과 인접해 있는 고가구조물을 중심으로 일조환경을 검토하여, 현재 사용되는 이격거리의 적정성 여부를 검토해보고, 구조물의 방위각에 따른 방향별 특성을 분석하였다. 구조물의 특성에 따른 일영거리를 통해 높이에 따른 이격거리비율을 산정하여, 향후 건설시 발생되는 일조장애를 최소화 하기위하여 구조물에 관한 제도 정비의 필요성과 최소 이격거리산정에 필요한 기초자료를 제시하는데 주목적을 두었다.

• 대한기계학회논문집B
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• 제22권11호
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• pp.1591-1602
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• 1998

Simple spanwise distribution models of deviation angle and pressure loss coefficient due to the tip leakage flow are formulated for use in association with the streamline curvature method as a flow analysis. Combining these new models with the previous deviation and loss models due to secondary flow, a robust streamline curvature method is established for flow analysis of single-stage, subsonic axial turbines with wide ranges of turning angle, aspect ratio and blading type. At the exit from rotor rows, the flow variables are mixed radially according to a spanwise transport equation. The proposed streamline curvature method is tested against a forced vortex type turbine as well as a free vortex type one. The results show that the spanwise variations of flow angle, axial velocity and loss coefficients at rotor exit are predicted with good accuracy, being comparable to a steady three-dimensional Navier-Stokes analysis. This simple and fast flow analysis is found to be very useful for the turbine design at the initial design phase.

• 한국산학기술학회논문지
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• 제20권9호
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• pp.517-524
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• 2019

오버드라이버 허브클러치는 자동차 6단 자동 변속기 미션에 장착되어 엔진의 여유출력을 이용해 연료사용을 절감시켜주는 부품이다. 본 연구에서는 오버드라이버 허브클러치 제품에 대해 피어싱 공정 중 펀치에 가해지는 하중 및 소재 처짐량을 최소화 하고자 한다. 공정 중 펀치의 하중과 처짐량에 영향을 줄 수 있는 다이 클리어런스(die clearance)와 전단각도(shear angle) 그리고 마찰계수(friction coefficient)를 설계 변수로 설정했다. 또한 펀치의 하중과 소재 처짐량에 대해 각 설계 변수들의 영향도를 확인하기 위해 민감도 분석(sensitivity analysis)을 진행했다. 그 결과 전단 각도, 마찰 계수, 다이 클리어런스 순으로 하중 및 처짐량에 대해 민감한 것으로 조사되었다. 이를 통해 펀치의 하중과 소재 처짐량을 목적함수로 설정하고, 반응표면법(Response Surface Method)을 통해 각 설계 변수들과 목적함수의 방정식을 도출했다. 이를 통해 설정된 설계 변수들의 최적 값을 도출해 유한요소해석에 적용한 결과 펀치의 하중 및 소재의 처짐량이 기존대비 22.14% 개선됐다.

• 대한기계학회논문집B
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• 제31권4호
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• pp.349-356
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• 2007

The present study investigated local heat/mass transfer characteristics on the tip of the rotating turbine blade with various incoming flow incidence angles. The experiments are conducted in a low speed annular cascade with a single stage turbine. The blade has a flat tip with a mean tip clearance of 2.5% of the blade chord. The incoming flow Reynolds number is $1.5{\times}10^5$ at design condition. To examine the effect of off-design condition, the experiments with various incidence angles ranging between $-15^{\circ}$ and $+7{\circ}$ were conducted. A naphthalene sublimation method is used to measure detailed mass transfer coefficient on the blade. The results indicated that the incidence angle strongly affects the behavior of tip leakage flow around the blade tip and consequently plays an important role in determining heat transfer characteristics on the tip. For negative incidence angles, the heat/mass transfer in the upstream region on the tip decreases by up to 20%. On the contrary, for positive incidence angles, much higher heat transfer coefficients are observed even with small increase of incidence angle.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 1998년도 제10회 학술강연회논문집
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• pp.13-13
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• 1998

A simple model of the tip leakage flow models of the rotor downstream flow is developed, based on Lakshminarayana's theoretical concept on the tip clearance flow and the experimental data published in open literature. And new spanwise distribution models of deviation angle and pressure loss coefficient due to the tip leakage flow are formulated for use in association with the streamline curvature method as a through flow analysis. Combining these new models and previous deviation and loss models due to secondary flow, a robust streamline curvature method is established for flow analysis of single-stage, subsonic axial turbines with wide ranges of turning angle, aspect ratio and blading type. At the exit from rotor rows, the flow variables are mixed radially according to a spanwise transport equation. The proposed streamline curvature method is tested against a forced vortex type turbine as well as a free vortex type one. The results show that the spanwise variations of flow angle, axial velocity and loss coefficients at rotor exit are predicted with good accuracy, being comparable to a steady three-dimensional Navier-Stokes analysis. This simple and fast flow analysis is found to be very useful for the turbine design at the initial design phase.

• 한국소성가공학회:학술대회논문집
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• 한국소성가공학회 1995년도 춘계학술대회논문집
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• pp.170-177
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• 1995

The restraining characteristics for the single square drawbead are discussed. The drawbead restraining forces adn maximum strains by the various drawing angles are measured experimentally. During this procedure , the drawing angles are varied from 0$^{\circ}C$ to 60$^{\circ}C$. Also, the wide range of experimental data of the drawing forces and maximum strains for the various drawbead dimensions, dimensions, clearances and blank holding forces are preseted.