• 한국건설관리학회논문집
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• 제14권5호
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• pp.153-163
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• 2013

건축물이 고층화, 대형화 될수록 수직 양중 계획 및 운영에 관한 중요성이 부각되고 있다. 이에 프로젝트 초기 단계에 실제 모델과 유사한 건설용 리프트 양중계획을 수립하려는 노력이 계속되고 있지만 프로젝트 착수 후 리프트 운행을 컨트롤 할 수 있는 시스템은 부재한 실정이다. 따라서 본 논문에서는 건설용 리프트 운영 효율증대를 위하여 센서를 사용한 리프트 운행 정보를 수집하고 실시간 분석이 가능한 건설용 리프트 최적화 운행 시스템 개발을 실시 및 검증 단계를 수행하여, 양중 효율의 지표가 되는 사용자 대기 시간의 단축을 도모하고 향후 무인 스마트 리프트의 초석이 되는 시스템을 제시하고자 한다.

• 대한전자공학회논문지
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• 제26권10호
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• pp.1535-1544
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• 1989

The overhang structure of photoresist in optical lithography was studied for the metallization of GaAs-related devices throughout lift-off method. Optical contact aligner with a dose of 8.5 m J/cm\ulcornerand with a wavelength of 300mm was used for ultraviolet exposure of single layer of S1400-27 photoresist. The overhang thickness shows a linear relationship with the soaking time in monochlorobenzene, which its magnitude becomes high at elevated softbake temperature. Such process conditions as a low softbake temperature, a long monochlorohbenzene soaking time and a little exposed energy make the development rate of photoresist lower. The optimum process conditions to obtain a target line-width, which include an appropriate overhang structure such as complete separation between the sidewall of photoresist pattern and the deposited metal edge, are determined as the softbake temperature of 64-74\ulcornerC, the monochlorobenzene soaking time of 10-15min, the ultraviolet exposure time of 70-100sec and the development time of 50-80sec.

• 대한전기학회:학술대회논문집
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• 대한전기학회 1995년도 추계학술대회 논문집 학회본부
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• pp.352-354
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• 1995

The optical and electrical properties of High Speed AlGaAs infrared LED by using metal wet etch process instead of metal lift-off process are investigated. The power out increases when metal contact is patterned by wet etch process. Forward voltage and Reverse voltage for metal wet etch process represent higher value than the metal lift-off process. The aging effect of power out also indicates good results with wet etch process. The wet etch process for metal contact reveals reliable LED device properties.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2006년 제4회 한국유체공학학술대회 논문집
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• pp.217-220
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• 2006

The lift and drag forces produced by a wing of a given cross-sectional profile are dependent on the wing planform and the angle of attack. Aspect ratio is the ratio of the wing span to the average chord. For conventional fixed wing aircrafts, high aspect ratio wings produce a higher lift to drag ratio than low ones for flight at subsonic speeds. Therefore, high aspect ratio wings are used on aircraft intended for long endurance. However, birds and insects flap their wings to fly in the air and they can change their wing motions. Their wing motions are made up of translation and rotation. Therefore, we tested flapping motions with parameters which affect rotational motion such as the angle of attack and the wing beat frequency. The half elliptic shaped wings were designed with the variation of aspect ratio from 4 to 11. The flapping device was operated in the water to reduce the wing beat frequency according to Reynolds similarity. In this study, the aerodynamic forces, the time-averaged force coefficients and the lift to drag ratio were measured at Reynolds number 15,000 to explore the aerodynamic characteristics with the variation of aspect ratio. The maximum lift coefficient was turned up at AR=8. The mean drag coefficients were almost same values at angle of attack from $10^{\circ}$ to $40^{\circ}$ regardless of aspect ratio, and the mean drag coefficients above angle of attack $50^{\circ}$ were decreased according to the increase of aspect ratio. For flapping motion the maximum mean lift to drag ratio appeared at AR=8.

• 한국콘텐츠학회논문지
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• 제15권8호
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• pp.46-52
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• 2015

공연장의 거대한 무대 세트나 장치에 움직임이 부여되면, 다양한 극적 효과를 연출할 수 있다. 본 논문에서 제안하는 프로그래밍 가능한 다축 체인 호이스트 서버 시스템은 이러한 연출의 자동화를 가능하게 한다. 본 시스템에는 PTP 기반의 임의 궤적 생성 방법, 다축 실시간 통신 제어 방법, 그리고 4 단계의 순차적인 안전 진단 알고리즘이 적용 되었으며, 호이스트들은 콘솔의 동기 제어에 의하여 시나리오의 연출 순서에 따라 자동적으로 움직인다. 12대 체인호이스트로 구성된 멀티 체인 호이스트 서버 시스템에 대한 1 ton 부하 및 대칭-비대칭 배치 부하에 대한 실험을 통해서 우수성을 검증하였다. 아울러 K-POP 공연에서 극적효과를 연출하는데 성공적으로 적용되었다.

• 한국항해항만학회지
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• 제41권2호
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• pp.33-38
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• 2017

A marine flapped rudder is designed to improve the effective lift generated by the rudder; this also improves the maneuverability of the ship. The flap is a high lift device installed at the trailing edge of the rudder to augment lift. In this paper, the characteristics of a thick flapped rudder are analyzed at a low Reynolds number with various ratios of flap chord length to total chord length and various aspect ratios, based on the computational fluid dynamics technique. The performance of the rudder with respect to lift, drag, and center of pressure are investigated, and the efficient ratio of flap chord length to total chord length and improved aspect ratio are determined. Ed: highlight - or 'superior'. As a case study, the flow on the flapped rudder of an NACA0021 section shape in free stream condition is simulated. The standard k-epsilon turbulence model is used to model the flow around the flapped rudder. The results indicate that the efficient ratio of the flap chord length to total chord length and aspect ratio are 0.3 and 1.4, respectively.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2005년도 추계 학술대회논문집
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• pp.125-129
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• 2005

Flow control has been performed using synthetic jet on NACA23012. In order to improve aerodynamic performance, synthetic jet is located near separation paint on airfoil with leading edge droop and plain flap. The flow control using synthetic jet shows that stall characteristics and control surface performance can be improved through resizing separation vortices. Stall is delayed and stall characteristics are improved when synthetic jet is applied from separation region of leading edge droop. Control surface effectiveness is increased and lift is increased when synthetic jet applied at the flap leading edge region. The results show that aerodynamic characteristics can be improved through leading edge droop with synthetic jet at near separation and plain flap with synthetic jet at the flap leading edge. The combination of synthetic jet and simple high lift device is as good as fowler flap system.

• International Journal of Aeronautical and Space Sciences
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• 제17권3호
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• pp.285-295
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• 2016

A contact strip shape of a high speed train pantograph system was optimized with CFD to increase the aerodynamic performance and stability of contact force, and the results were validated by a wind tunnel test. For design of the optimal contact strip shape, a Kriging model and genetic algorithm were used to ensure the global search of the optimal point and reduce the computational cost. To enhance the performance and robustness of the contact strip for high speed pantograph, the drag coefficient and the fluctuation of the lift coefficient along the angle of attack were selected as design objectives. Aerodynamic forces were measured by a load cell and HWA (Hot Wire Anemometer) was used to measure the Strouhal number of wake flow. PIV (Particle Image Velocimetry) was adopted to visualize the flow fields. The optimized contact strip shape was shown a lower drag with smaller fluctuation of vertical lift force than the general shaped contact strip. And the acoustic noise source strength of the optimized contact strip was also reduced. Finally, the reduction amount of drag and noise was assessed when the optimized contact strip was applied to three dimensional pantograph system.

• EDISON SW 활용 경진대회 논문집
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• 제4회(2015년)
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• pp.590-593
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• 2015

항공기 운항 중에 가장 연료가 많이 소모될 때는 순간 고출력이 필요한 이륙 순간이다. 항공기가 이륙시 보다 적은 연료를 이용하여 효율적인 비행을 위해 고양력 장치를 사용하고 있다. 본 연구에서는 항공기가 이륙 시 사용되는 고양력 발생 장치 중 하나인 Slat을 이용하여 Slat의 각도 변화에 따라 가장 효율적인 공력특성을 찾아보았다. Slat의 각도를 $15^{\circ}$, $20^{\circ}$ $25^{\circ}$, $30^{\circ}$로 변화시켜 보면서 공력 특성 값들을 확인한 결과 Slat이 있는 경우 NACA2415만 있는 경우보다 양력계수가 좋아졌으나 Slat 뒷전의 와류에 의해 항력계수가 약간 증가 하는 모습을 보였다. 본 실험 case 중에서는 Slat 각도가 $30^{\circ}$일 때 Slat 뒷전의 와류가 사라져 가장 우수한 공력 특성을 보였다.

• 한국항공우주학회지
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• 제34권8호
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• pp.55-62
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• 2006

본 논문에서는 단일층 압전 작동기로 구동되는 곤충 모방 날갯짓 기구의 실험적 평가의 결과를 제시하였다. 변위 증폭기구의 연결막대 길이와 힌지 위치를 조절하여, 말벌류 곤충의 상향 날갯짓 끝에 발생하는 날개 겹침 (clap)을 모방할 수 있도록 하였다. 또한, 실제 곤충 날개의 단면이 지그-재그형인 것을 모방한 날개를 제작하여 부착하였다. 이 두 가지 추가적인 고안으로 인하여 본 날갯짓 기구는 이전 날개에 비하여 면적이 절반 밖에 되지 않음에도 불구하고 더 큰 양력을 발생할 수 있었다. 본 연구에서는 날개의 겹침, 지그-재그형 단면, 인가전압 파형이 양력 발생에 미치는 영향을 조사하였다. 최종적으로는 디지털 고속카메라를 이용하여, 개선된 날갯짓 기구가 상향 날갯짓과 하향 날갯짓에서 와류를 발생함을 확인하였다.