• 한국항해항만학회지
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• 제29권4호
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• pp.335-339
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• 2005

The superconducting electromagnetic propulsion system has been proposed as one of new alternative propulsion systems. Especially, the helical-type propulsion system has the greatest merit that is able to use the solenoid-type superconducting magnets with high magnetic fields. In this study, calculations of characteristics of the large scale helical-type thruster are carried out on the basis of our experimental results. As a couple of results of calculations, it is found that the thruster efficiency quickly increases with the length of electrode up to about 5 m and then goes up to about 0.9. The thruster efficiency peaks at a certain point ($^{\sim}0.6\;m$) and then falls as length of pitch increases.

• Journal of Biosystems Engineering
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• 제33권6호
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• pp.371-378
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• 2008

Bio-diesel applications seem to be extended due to bio-diesel policies and changes of agricultural environment. This study was conducted to develop a rapeseed reaping equipment attachable to the conventional combine. This paper was intended to report concept design, process and manufacturing of the prototype rapeseed reaping equipment. For concept design, physical properties of "SUNMANG", which is a typical rapeseed as bio-diesel materials, were considered. The designed prototype rapeseed reaping equipment consisted of wide-width plates, finger type knifes, side cutter knifes and drive equipments. The wide-width plate is 2.1 m wide, 0.7 m long, and 0.002 m thick. The finger type cutter knifes have 14.5 fingers, 30 knifes, and the specification was 7.6 cm of pitch, 8.3 cm of length and $21^{\circ}$ of cutting angle. The side cutter knifes consisted of a hydraulic pump, a hydraulic motor, a flow control and a relief valve, a hydraulic hose, a driving equipment and a reciprocating cutter knife. The 18 reciprocating cutter knifes were 137 cm long and knife pitch, knife length and cutting angle were 7.7 cm, 10.5 cm, and $18^{\circ}$. Prototype weight of the rapeseed reaping equipment was heavier by 272 kg when compared with the manual reaping equipments. Load distributions of left and right side showed 50% and 49%, and those of front and rear side showed 64% and 36%. Static turn-over angles in left and right of the prototype were $38.1^{\circ}$ and $38.7^{\circ}$, respectively. The designed prototype rapeseed reaping equipment was properly mounted at the front of a conventional combine.

• 에너지공학
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• 제12권2호
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• pp.84-92
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• 2003

구리밀봉 증기발생기의 열적크기 계산을 위한 1차원 열수력코드를 개발하였다. 고온 및 저온측 전열관사이의 구리의 열전도는 1차원으로 가정하고, 전열관 피치의 함수로 열저항을 구하였다 물/증기측 유동영역은 아냉, 포화핵비등, 포화막비등, 과열영역의 4 구간으로 구분하였다. 매개변수 연구를 위한 전열관 갯수는 250에서 3500이며, P/D비율은 각각1.4, 1.6, 1.8로 하였다. 계산결과, 전열관 갯수가 2500일 때 전열관 길이는 약 12 m, 직경은 약 3 m이다. P/D를 증가시키면 구리에 의한 열저항 성분이 증가하지만 전열관 길이는 큰 차이가 없음을 알 수 있었다.

• 한국지반공학회논문집
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• 제28권1호
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• pp.5-15
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• 2012

본 논문에서는 지하굴착 혹은 절토사면에 적용할 수 있는 스크류 앵커 파일의 인발저항 특성에 관한 연구내용을 제시하였다. 이를 위해 스크류의 크기(직경) 및 피치길이 등 스크류 앵커 파일의 기하적 특성을 달리하는 모형 스크류 앵커 파일을 이용하여 모형실험을 수행하였다. 실험 결과 분석내용을 토대로 할 때 일정한 스크류 크기를 갖는 스크류 앵커 파일의 인발 저항력은 피치길이가 감소할수록 증가하는 것으로 검토 되었다. 또한 일정한 피치길이의 조건에서 스크류 앵커 파일의 인발저항력은 스크류 크기가 증가하면 일정 크기까지는 선형적으로 증가하나 일정 크기 이상에서는 증가량이 거의 일정해지는 것으로 검토 되었다. 본 논문에서는 실험결과를 스크류 앵커 파일의 다양한 제원과 인발저항 특성에 대한 상관관계를 파악할 수 있도록 제시하였으며 연구결과의 실무적 관점에서의 검토 내용을 기술하였다.

• 대한기계학회논문집B
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• 제39권8호
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• pp.693-702
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• 2015

본 논문은 NACA 익형의 블레이드를 가지는 다리우스 수직축 풍력발전기(VAWT)의 성능특성에 대한 연구이다. 다양한 설계변수를 이용한 다리우스 VAWT 의 최적 형상을 예측하기 위해서 블레이드 근처에서 나타나는 공력특성 및 박리유동, 유동과 블레이드 간의 상호작용, 이로 인해 유도되는 토크 및 출력특성 등을 분석하였다. 블레이드의 최적 형상 설계 및 주변 유동과의 상호작용 특성을 보기 위하여 다양한 인자들 (즉, 코드길이, 로터직경, 피치각, 블레이드의 두께비 및 비틀림각 등)을 고려하였다. 본 연구에서 연구결과로는 TSR 가 낮은 영역에서는 솔리디티가 큰 로터가 높은 출력계수를 가지는 반면, TSR 이 높은 영역에서는 솔리디티가 작은 로터가 높은 출력계수를 가진다. 블레이드의 익형이 안쪽으로 향하는 피치각은 $-2^{\circ}$와 비틀림각이 $0^{\circ}$ 일 때, 다리우스형 VAWT 가 최대 출력을 발생하였다.

• 대한조선학회지
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• 제12권2호
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• pp.59-66
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• 1975

Recently, as the dimensions of energy carriers increase, especially in draft, a reliable prediction of the ship motions at finite depths of water becomes necessary. The purpose of this paper is to probe the effect of finite water depth on the hydrodynamic forces and ship motions, particularly heave and pitch, in longitudinal regular head waves, by comparing the experimental value of Freakes and Keay with the author's theoretical value obtained by applying the modified strip theory to the Mariner class ship. It is confirmed that generally the hydrodynamic coefficients in the equations of motion increase with decreasing water depth, and the wave exciting forces and moments decrease with decreasing water depth. Amplitudes of heave and pitch in longitudinal regular head waves decrease as the water depth in the range where the length of the incident wave is comparatively long. The effects of Froude Number on the hydrodynamic coefficients increase with decreasing water depth and is more noticeable in the case of heave than pitch. In heave, generally the discrepancy between the experimental value and the theoretical value is relatively small in the case of $F_n=O$, but it is very large in the case of $F_n=0.2$. It is considered that the trend stems from the ignorance of the three dimensional effect and the other effects due to shallowness of water on the hydrodynamic coefficients in the theoretical calculation. An extension of methods for calculating the two dimensional hydrodynamic forces to included the effect of forward speed should be recommended. It is required that more experimental works in finite water depths will be carried out for correlation studies between the theoretical calculation, according tp modified strip theory, and model experiments.

• 한국전기전자재료학회:학술대회논문집
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• 한국전기전자재료학회 2007년도 하계학술대회 논문집 Vol.8
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• pp.183-184
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• 2007

A 40 Gb/s transimpedance amplifier IC was designed and fabricated with a InP/InGaAs HBTs technology. In this study, we interconnect 40Gbps trans impedance amplifier IC to a duroid substrate by a flip chip bonding instead of conventional wire bonding for interconnection. For flip chip bonding, we developed fine pitch bump with the $70{\mu}m$ diameter and $150{\mu}m$ pitch using WLP process. To study the effect of WLP, electrical performance was measured and analyzed in wafer and package module using WLP. The Small signal gains in wafer and package module were 7.24 dB and 6.93dB respectively. The difference of small signal gain in wafer and package module was 0.3dB. This small difference of gain is due to the short interconnection length by bump. The characteristics of return loss was under -10dB in both wafer and module. So, WLP process can be used for millimeter wave GaAs MMIC with the fine pitch pad and duroid substrate can be used in flip chip bonding process.

• Wind and Structures
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• 제32권5호
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• pp.471-485
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• 2021

Onshore wind turbines may experience substantially different wind loads depending on their working conditions, i.e. rotation velocity of rotor blades, incoming freestream wind velocity, pitch angle of rotor blades, and yaw angle of the wind-turbine tower. In the present study, aerodynamic loads acting on a horizontal axis wind turbine were accordingly quantified for the high tip speed ratio (TSR) at high yaw angles because these conditions have previously not been adequately addressed. This was analyzed experimentally on a small-scale wind-turbine model in a boundary layer wind tunnel. The wind-tunnel simulation of the neutrally stratified atmospheric boundary layer (ABL) developing above a flat terrain was generated using the Counihan approach. The ABL was simulated to achieve the conditions of a wind-turbine model operating in similar inflow conditions to those of a prototype wind turbine situated in the lower atmosphere, which is another important aspect of the present work. The ABL and wind-turbine simulation length scale factors were the same (S=300) in order to satisfy the Jensen similarity criterion. Aerodynamic loads experienced by the wind-turbine model subjected to the ABL simulation were studied based on the high frequency force balance (HFFB) measurements. Emphasis was put on the thrust force and the bending moment because these two load components have previously proven to be dominant compared to other load components. The results indicate several important findings. The loads were substantially higher for TSR=10 compared to TSR=5.6. In these conditions, a considerable load reduction was achieved by pitching the rotor blades. For the blade pitch angle at 90°, the loads were ten times lower than the loads of the rotating wind-turbine model. For the blade pitch angle at 12°, the loads were at 50% of the rotating wind-turbine model. The loads were reduced by up to 40% through the yawing of the wind-turbine model, which was observed both for the rotating and the parked wind-turbine model.

• 한국정밀공학회지
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• 제29권8호
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• pp.920-926
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• 2012

Wrinkling is a common phenomenon in nature and the shape of a wrinkle can be defined using characteristic dimensions such as pitch, length, amplitude, and density etc. Wrinkle structure can be utilized in various research fields, and especially it has special characteristics when it used in applications of heat transfer; a wrinkly surface has the effect to promote turbulent flow and increasing surface area. However, the generation of wrinkle structures in somewhat regular is not easy. Till now, there are some research works focused on realization of wrinkles in micro scale. However, most of the processes generally requires high precision equipments and high costs, and also there is a limitation to generate the wrinkles in a large area. In this study, we propose a novel method named as a RCO (repetitive contact-and-open) process to fabricate wrinkle structure with low cost and relative easy way. Using the RCO, we fabricated micro-corrugate structures successfully. From the experimental results, we found out the process parameters of RCO, and showed the possibility of RCO to be used in real applications.

• 한국생산제조학회지
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• 제26권1호
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• pp.137-143
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• 2017

An axial fan has competitive advantages that can make air flow more straight and longer and produce larger air volume than the other kinds of fans. In those reasons, axial fans are widely used for ventilator, 4D cinema, duct, and so on. But, as it was designed and manufactured without any mathematical analysis or computer simulations, it is difficult to develop the performance of axial fans. Actually the axial fan is designed and manufactured in industry by imitation or traditional method. Flow velocity and volume of axial fan are changed by pitch angle, frame, the number of blade, camber angle, and chord length. In this paper, the performance of axial fan was analyzed and by computer program known as CFD. Finally, we have designed a new axial fan whose velocity and volume is improved. The performance of new axial fan is also compared with the of conventional fans experimentally.