• Journal of Korea Foundry Society
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• v.27 no.2
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• pp.88-94
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• 2007

General criteria for the risering design of steel castings and commercial codes for the flow and solidification analysis were used to design the optimized risering in V-process. Three type of specimens were chosen including thin plates and a thick disc. Sided riser installed in the front of a plate casting was effective to prevent the shrinkage defects and to increase the casting yield ratio. Exothennic sleeve and chill were also effective. It was possible to apply the general criteria for the risering design of steel castings to V-process. Temperature of a mold surface was expected to rise over $1,000^{\circ}C$ in the temperature calculation considering radiation effect of molten metal in the mold. Since weakening temperature of the vinyl used in V-process is about $70^{\circ}C$, it should be emphasized that a proper coating of the vinyl film is necessary to prevent the possibility of burning out of the vinyl by the molten metal.

• Proceedings of the KIEE Conference
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• 2003.04a
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• pp.355-358
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• 2003

본 연구에서는 차세대 초전도 핵융합장치(KSTAR)의 가열장치인 중성입자입사장치(NBI : Neutral Beam Injection) 시스템 중 휨 전자석(Bending magnet)의 중요한 파라메타인 전류에 따른 온도상승값과 B-field의 측정을 행하고 그 결과를 나타내었다. 휨 전자석(Bending magnet)은 중성입자입사장치(NBI) 시스템 중 중성화장치(Neutralizer) 후단에 설치되어, 미처 중성화되지 못한 이온들의 케도를 변경시켜 중성입자와 분리되도록 한 후 이온덤프에서 이들 이온들의 에너지가 흡수될 수 있도록 하는 역할을 한다. 사용전원은 15[V], 1200[A]의 가변전원을 사용하였고 전류값 변화에따른 온도상승값은 thermo couple 신호선을 이용하여 측정하였으며, B-field는 3차원 Gaussmeter를 이용하여 측정을 행하였다. 측정된 결과들은 설계시의 값과 비교분석을 행하여 오차를 줄여나가고자 하였고 향후 NBI 주 진공용기에 장착하여 중성입자입사장치의 개발 수행을 행하게 될 것이다.

• Journal of the Korean Institute of Illuminating and Electrical Installation Engineers
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• v.12 no.3
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• pp.22-28
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• 1998

It is required to automate a manufacturing industry of a glasses frame, because of the inaccuracy in assembly and shortage of labor. So, in this paper, rim-lock electric welding system has been developed in order to automate a electric welding process and to increase welding quality. Rim-lock electric welding system consists of circular and linear feeder, holder for welding rim and lock, and the equipment for silver-lead provision and so forth. Main controller is a V55 microprocessor which is easy to be expanded into other function. Control program is programed using 'C' language which is easier than other language in coding, modification and adding function. At the practical welding that Rim-Lock electric welding system from this study is used, we can get such advantages as uniform quality of electric welding, continuous operation and improved productivity.

• Journal of KSNVE
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• v.8 no.2
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• pp.331-335
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• 1998

A design modification was made on the 9-th stage wheel dovetail of a high-intermediate pressure (HIP) turbine rotor for a fossil power plant that necessitates the use of new long-shank buckets for the row. A bucket vibration test is necessary to verify that the new 9-th stage buckets have adequate frequency margin from a nozzle passing frequency when running at speed. A finite element analysis (FEA) has been performed using a commercial S/W to approximately estimate bucket natural frequencies, and thus to help the vibration test. A row of the new buckets has assembled on the HIP rotor for the vibration tests using dynamic balancing facilities. The tests have been done during deceleration run with air excitation. The test results are compared with the calculation using our empirical formula, and show that the modified design meets the frequency-margin requirements.

• Journal of Korea Foundry Society
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• v.32 no.2
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• pp.65-74
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• 2012

In this paper, we present the results of our studies on optimal die design towards development of a vacuum die casting process to fabricate fuel cell bipolar plate with micro-channel array. Cavity and overflow shape is designed by computational filling analysis of MAGMA soft. Optimal die design consists of seven overflows at the end of cavity and three overflows at each side wall of cavity. The molten metal that passed the gate and reached the side wall flowed into the side overflow, no turbulent flow occurred, and the filling behavior and velocity distribution were uniform. In addition, partially solidified molten metal passing through the channel was perfectly eliminated by overflow without back-flow. When vacuum pressure, injection speed of low and high region was 300 mbar, 0.3 m/s and 2.5 m/s respectively with Silafont 36 die casting alloy, sound sample without casting defects was obtained. The experimental results are nearly consistent with simulation results.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2008.05a
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• pp.145-148
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• 2008

A 50 Newton monopropellant thruster being developed for attitude control in a variety of aerospace application systems is described in this paper. A scaled down thruster with platinum on aluminum oxide in the reaction chamber was tested to determine the catalyst capacity. A scaled up thruster, was designed and fabricated using data obtained on small scale device, was evaluated by decomposition efficiency based on temperature, efficiency of characteristic velocity, and measurement of thrust. The performance of a scaled up thruster was 42 Newton in thrust, 98 % in efficiency of characteristic velocity, and 123 sec in specific impulse at sea level.

• Journal of the Korea Convergence Society
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• v.8 no.10
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• pp.185-191
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• 2017

Recently, for such reasons as its inexpensive price and eco-friendliness, LNG has been under the limelight as an alternative fuel for vessels and is expected to grow rapidly in the industry. However, the technology level of domestic shipbuilders in manufacturing the cryogenic pump designed to supply LNG for vessels is so low that design and manufacturing technology of core parts are in urgent need. Therefore, this study describes the stepwise development procedure of cryogenic submerged centrifugal pump for ship LNG supply system. And it aims to suggest practical and specific development methods of the pump by approaching the characteristics of each step and major development items from the standpoint of engineering and management.

• 한국태양에너지학회:학술대회논문집
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• 2012.03a
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• pp.480-487
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• 2012

The application of solar energy in residential building is general and natural in today. And application methods of solar thermal energy is divided in two kind of form, single evacuated tube and flat-plate form. Then in this study, the efficiency of single evacuated tube and flat-plate system is compared by total and effective area considering the time receiving the solar radiation between 24 hours and the specific time(10:00~15:00). As a result of the experiment, single evacuated tube and flat-plate collector's efficiency is varied by the quantity of solar radiation. And especially, the flat-plate system is more affected by outdoor temperature. Therefore the application of solar thermal system should be considered the solar radiation and outdoor temperature.

• Proceedings of the Materials Research Society of Korea Conference
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• 2010.05a
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• pp.47.2-47.2
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• 2010

1980년대 이후로 등장한 Nd-Fe-B 소결자석은 뛰어난 자성특성을 나타내며, 원재료도 풍부하기 때문에 단위 자기 에너지당 가격은 비교적 저가이다. 따라서 대부분의 기존 Sm-Co와 주조 Al-Ni-Co 자석재료를 대체하며 다양한 첨단사업의 핵심소재로 적용되며, 자동차 및 의료기기 등 산업 전반에 사용되고 있다. 이러한 응용 중에서도 향후 녹색성장을 위한 신성장동력 산업인 하이브리드 자동차의 구동 모터로서 사용되는 대표적인 영구자석이다. 현재 개발된 Nd계 영구자석은 큐리온도가 낮고 높은 온도에서 자기적 성능의 열화가 심하게 진행된다는 단점이 있기 새로운 합금 설계 및 공정의 최적화를 통해 보자력을 향상 시킴으로써 사용온도를 $200^{\circ}C$ 정도로 높이는 연구가 활발히 진행되고 있다. 본 연구에서는 일반적인 제조공정을 통해 제조된 소결체의 미세구조에 변화시키기 위하여 약 $10^{-5}$ Torr의 진공분위기에서 $10^{\circ}C/min$의 승온/냉각속도로 $350^{\circ}C$부터 $450^{\circ}C$ 구간에서 2 사이클부터 8 사이클까지 승온과 냉각을 반복하는 열처리를 수행하였다. Nd-Fe-B 소결자석을 $350^{\circ}C{\sim}450^{\circ}C$ 온도구간에서 반복적인 열처리를 수행한 결과 열처리 사이클에 따라 보자력 특성이 다르게 나타내었다. 이에 승온과 냉각을 반복하며 나타난 미세구조의 변화가 자성특성에 어떠한 영향을 미쳤는지에 대해 고찰하였다.

• Journal of the Korean Society of Propulsion Engineers
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• v.12 no.3
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• pp.24-33
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• 2008

A 50 Newton monopropellant thruster being developed for attitude control in a variety of aerospace application systems is described in this paper. A scaled down thruster with platinum on aluminum oxide in the reaction chamber was tested to determine the catalyst capacity. A scaled up thruster which was designed and fabricated using data obtained from a small scale device was evaluated by its decomposition efficiency based on the temperature, the efficiency of characteristic velocity, and the measurement of thrust. The performance of a scaled up thruster was marked by a measured thrust of 42 Newton, 98 % efficiency of the characteristic velocity, a specific impulse of 123 sec at sea level.