• 한국기계가공학회지
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• 제15권4호
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• pp.109-117
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• 2016

For efficient deburring of burrs that form inside mechanical parts after drilling, new special deburring tool was developed specifically for the burr found at intersecting holes. In this paper, the process for finding ideal cutting conditions has been carried out to identify the efficient performance of deburring using a new tool. The burrs at the entrance and exit surface were analyzed for efficient removal. The surface roughness after deburring was also reviewed for better performance. In addition, the influence of the feed rate on deburring quality was analyzed for improved productivity. Through this process, a new deburring tool can be applied effectively to remove burrs formed at intersecting holes.

• 한국정밀공학회지
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• 제18권10호
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• pp.200-207
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• 2001

Burrs farmed in drilling are classified into three types, no burr, burrs with cap, teared burr. To control burr size in drilling, the second type burrs with cap are to be formed because it is small and uniform. It is necessary to understand the mechanism of cap formation to derive the burr formation into second type burr with cap. In several materials. second type burrs are formed in drilling by changing cutting conditions. It is observed that cap is formed as a result of the plastic deformation along the outside of exit hope. According to the tension behavior of the material in concentrated region between hole and drill outside edge, the geometry of burr with cap is determined. Simplified 2D FEM analysis shows good prediction for burr formation.

• 한국생산제조학회지
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• 제21권6호
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• pp.860-864
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• 2012

The contact tip is higher the wear of resistance and the longer life are demanded to GMA welding process. In this study, four different contact tips with three different compositions by two wires were evaluated their wear resistance by measuring in every one hour the area of enlarged hole at the exit side during actual wleding. Experimental results clearly showed that the Cr-containing tips strengthened by precipitation hardening have much better resistance to wear than those made by work hardening. In addition, flux cored wire is excellent abrasion resistance test results showed. Based on these results, the domestic industry, the life of the contact tip to know will be used as basic data.

• 동력기계공학회지
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• 제14권6호
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• pp.5-12
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• 2010

In this study, an analysis of evaporative diesel spray and an usefulness of a general-purpose program, ANSYS CFX release 11.0, are investigated through the comparison and investigation of the experimental results carried out under an evaporative field, in which there is phase transition, by an exciplex fluorescence method and the results analyzed by the CFX program. The diesel fuel called n-Tridecane, $C_{13}H_{28}$, is injected from a single-hole nozzle (l/d=1.0mm/0.2mm) into a constant volume chamber under a high temperature and pressure. In the same condition as the experimental condition, the analysis was carried out. Both results of the spray tip penetration were almost coincident at each time. The results have validated the usefulness of this analysis. As a result, if the ambient pressure is high, the spray tip penetration will be shortened and move toward the nozzle exit.

• 대한기계학회논문집B
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• 제20권6호
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• pp.1971-1982
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• 1996

The breakup of liquid jet is the result of competing, unstable hydrodynamic forces acting on the liquid jet as it exit the nozzle. The nozzle geometry and up-stream injection conditions affect the characteristics of flow inside the nozzle, such as turbulence and cavitation bubbles. A set of calculation of the internal flow in a single hole type nozzle were performed using a two dimensional flow simulation under different nozzle geometry and up-stream flow conditions. The calculation showed that the turbulent intensity and discharge coefficient are related to needle position. The diesel nozzle with sharp inlet under actual engine condition has possibility of cavitation, but round inlet nozzle has no possibility of cavitation.

• 대한기계학회논문집B
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• 제36권1호
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• pp.103-110
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• 2012

EV double cone 버너를 장착한 스월 예혼합 연소기를 대상으로 LES 수치기법을 적용하여 연소기내의 유동 현상과 연료/공기 혼합, 화염 거동에 대해 조사하였고, 공연비와 압력 변화에 따른 NOx, CO 농도 변화를 예측하였다. 버너에서 발생한 강한 스월로 인해 재순환 영역이 발생하였으며, 희박 예혼합 화염은 버너 출구부터 형성되어 0.2 m 이내에 존재하는 것으로 나타났다. 상압, 공연비 38.7인 해석 조건에서 NOx 발생량은 연소기 출구에서 0.59 ppm으로 예측되었고, CO는 화염면에서 다량 생성되나 출구로 갈수록 급격히 산화되어 출구에서 5.25 ppm으로 낮게 예측되었다. 또한, NOx 배출량은 공연비가 높아질수록, 압력이 감소할수록 줄어드는 것으로 나타났다. 설계 변경을 통해 다양한 연료 공급 형태에서의 NOx 배출 특성을 조사하였으며, 5 lance-hole 분사의 경우 가장 적은 NOx 배출 특성을 보였다.

• 대한기계학회논문집
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• 제12권3호
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• pp.551-560
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• 1988

본 연구에서는 해석하려는 시스템의 유동 및 열전달 현상의 개념도를 Fig.1 에 나타내었다. 고체 입자는 윗부분 홈으로부터 분사되어, 선택적 투과면을 통해서 입사되는 복사열을 흡수 하며, 기체는 아래 또는 위의 홈 부분으로부터 들어와서 고체 입자와의 대류열전달로 가열이 된다. 기차게 아래 홈에서부터 분사되는 경우 대류에 의해 가열된 기체가 역성층화로 인해 부력을 받게 되어, 고체 입자의 하강 속도가 감 소할 때 입자의 체류 시간의 증가에 따른 복사열의 흡수효과에 대하여 고찰하였으며 입자의 크기, 투사 복사량, 분사속도, 입자의 질량유량 등을 파라미터로 하여 이들의 변화에 따른 영향을 규명하였다. 2-방연계를 고려한 2-방정식 모델을 구성하고 고체 입자에 대하여는 Lagrangian 방법으로 기술하였으며 수치해석에 있어 유한차분법을 도 입하고 두 상간의 상호연계는 PSI-Cell 방법을 이용하였고 복사 열유속은 2-유속 모델 (two-flux model)을 도입하여 계산하였다.

• 대한기계학회논문집B
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• 제31권6호
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• pp.547-557
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• 2007

This study was conducted to investigate the flow and combustion characteristic of the experimental burner which was manufactured for the reflection of the oven and broil burner features. As slot shape, spacing between slots, and slot arrangement of the exit area which emits the mixing gas are different in case of oven burners and broil turners, the purpose of this study is to know the affection of the flame interaction and combustion characteristic according to the change of shape factors such as slot shape, slot arrangement, and slot-to-slot spacing. With no relation of the slot shape, as the spacing between slots became narrow, the occurrence of a lift-flame was delayed. So the combustion was possible in the leaner region, but the appearance of yellow-tip became a little fast. Slit slot port had the broadest operating range among the other slot shapes. Specially, from the side of lift-flame, as the jet that spreads downstream in the longitudinal slot was nearly circular just a few slot lengths away from the orifice, slot-to-slot spacing of the Slit port was closer than the other ports. These results could be expected through the computer numerical method and had a good agreement. As the spacing between slots increased, in case of Slit and Mix port, NOx emission rate was constant or decreased, but the NOx emission of Hole port was increased. CO emission rate of Slit and Hole port was increased as the slot-to-slot spacing was broadened.

• 한국유체기계학회 논문집
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• 제11권6호
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• pp.24-30
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• 2008

In order to enhance the heat/mass transfer, a turbulator has been installed at the exit of injection hole for the impingement/effusion cooling system. The local heat/mass transfer coefficients have been obtained by a naphthalene sublimation method. Experiments have been carried out at the fixed jet Reynolds number of 10,000. Two turbulators with different diameter have been used in the current study. The result presents that the turbulator leads to the increase in flow mixing and jet velocity, consequently enhancing the heat/mass transfer at a stagnation region. Further, the stagnation region is divided into four small areas with peak value. In the existence of initial crossflow, the stagnation regions move downstream and low heat/mass transfer regions are formed regardless of the installation of turbulator. However, the increased jet velocity by turbulator reduces the crossflow effect against the jet, resulting in decrease of low heat/mass transfer regions. Compared to the case without turbulator, the installation of turbulator yields $5{\sim}10%$ augmentation in averaged Sh value.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 춘계학술대회논문집D
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• pp.840-845
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• 2001

Development of a small gas-turbine combustor for 100kW class APU(Auxiliary Power Unit) has been performed. This combustor is a reverse-annular type and has a tangential swirler in the liner head to improve the fuel/air mixing and flame stability. Three main and three pilot fuel injectors of the simplex pressure-swirl type are used. The performance target at the design condition includes a turbine inlet temperature of 1170K, a combustion efficiency of 99%, a pattern factor of 30%, and an engine durability of 3000 hours. Under developing the combustor, we conducted performance test of our first prototype(TS1) with some variants. As a result of the test, the performance targets of the combustor are satisfied except that the pattern factor is about 4% higher than target value. So, we redesigned the second prototype(TS2) and conduct performance test with the critical focus on pattern factor and exit mean temperature. We adopted TS2 four variant to check the improvement of pattern factor. As the result, the pattern factors of several variants were satisfied with the performance target. Finally, We chose the TS2A variant as a final combustor for our APU model.