• Title/Summary/Keyword: 표면압력

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Development of Tapered Rolling Type Strip Pressure Key for the Prevention of Scratch (스크래치 방지를 위한 테이퍼 롤링형 판재 누름키의 개발)

  • Kim, Tae-Wan
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.11 no.12
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    • pp.4715-4720
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    • 2010
  • In this study, we developed new tapered rolling type strip pressure key for the prevention of scratch in sheet metal forming line. The developed pressure key is equipped with two tapered rollers inside a conventional block pressure key. Through the scratch test, for the case of transversal movement the tapered rolling type pressure key reduces both friction and depth of scratch by the effect of tapered shape which decreases the pressure spike on edge, and for longitudinal movement the scratch on the sheet metal surface is certainly removed by the rolling contact.

Characterization of Etching profile for $LiNbO_3$ Optical Waveguide by Using Neutral Loop Discharge Plasma Dry Etching (NLD Plasma 식각 공정을 이용한 $LiNbO_3$ 광 도파로의 식각 Profile의 특성)

  • 박우정;양우석;이승태;김우경;장현수;이한영;윤대호
    • Proceedings of the Materials Research Society of Korea Conference
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    • 2003.03a
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    • pp.138-138
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    • 2003
  • 광대역 LiNbO$_3$ 광변조기의 초고속 광 변조 구현을 위해서는 RF/ optical 속도 정합 및 임피던스 매칭 조건 하에서 낮은 구동전압을 얻을 수 있는 ridge 구조의 제작이 필수적이며 이런 구조 제작하기 위해서는 식각 속도와 식각면 거칠기 식각 profile 및 식각 과정에서의 반응물의 감소 등과 같은 개선을 위한 연구가 필요하다. 본 연구에서는 LiNbO$_3$ 기판 위에 메탈 마스크를 형성한 후 비등방성 (anisotropic) 건식 식각 방법인 NLD (Neutral Loop Discharge)로 플라즈마 식각을 하였다. NLD plasma 식각은 1Pa 이하의 압력에서 낮은 전자 온도를 갖는 고밀도 플라즈마를 생성하고 이온 플라즈마를 형성하여 LiNbO$_3$ 표면의 원자와 분자를 이온충돌효과를 이용하여 물리적인 식각과 discharge로 형성된 레디칼 (radical)과의 상호작용에 의한 화학적 식각 메커니즘에 의한 방법으로 plasma에 의한 시편의 손상이 적으며 식각 속도가 또한 높은 것이 특징이다. 본 논문에서는 안테나 파워와 가스의 유량에 따른 LiNbO$_3$ 식각 profile 특성에 관하여 연구 하고자 한다.

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A Study on the Floating OWC Chamber Motion in Waves (부유기 OWC 챔버의 파중 운동해석)

  • 홍도천
    • Journal of Ocean Engineering and Technology
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    • v.16 no.3
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    • pp.19-27
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    • 2002
  • The motion of a floating OWC chamber in waves is studied taking account of fluctuating air pressure in the air chamber. An atmospheric pressure drop occurs across the upper opening of the chamber which causes not only hydrodynamic but also pneumatic added mass and damping forces to the floating chamber. A velocity potential in the water due to the free surface oscillating pressure patch is added to the conventional radiation-diffraction potential problem. the potential problem inside the chamber is formulated by making use of the Green integral equation associated with the Rankine Green function wile the outer problem with the Kelvin Green function. The two integral equations are solved simultaneously by making use of a matching boundary condition at the lower opening of the chamber to the outer water region. The chamber motion in the frequency domain is calculated for various values of parameters related to the atmospheric pressure drop. The present methods can also be sued for the analysis of air-cushion vehicle motion as well as for the design of a floating OWC wave energy absorber.

A Study on the Floating OWC Chamber Motion in Waves (부유식 OWC 챔버의 파중 운동해석)

  • Hong, Do-Chun;Hong, Sa-Young
    • Proceedings of the Korea Committee for Ocean Resources and Engineering Conference
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    • 2002.05a
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    • pp.191-197
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    • 2002
  • The motion of a floating OWC chamber in waves is studied taking account of fluctuating.air pressure in the air chamber. An atmospheric pressure drop occurs across the upper opening of the chamber which causes not only hydrodynamic but also pneumatic added mass and damping forces to the floating chamber. A velocity potential in the water due to the free surface oscillating pressure patch is added to the conventional radiation-diffraction potential problem. The potential problem inside the chamber is formulated by making use of the Green integral equation associated with the Rankine Green function while the outer problem with the Kelvin Green function. The two integral equations are solved simultaneously by making use of a matching boundary condition at the lower opening of the chamber to the outer water region. The chamber motion in the frequency domain is calculated for various values of parameters related to the atmospheric pressure drop. The present methods can also be used for the analysis of air-cushion vehicle motion as well as for the design oj a floating owe wave energy absorber.

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A Study on the Development of Dust Collection System for Hull Repair (선체 표면 공사시 발생하는 분진 수거 장치 개발에 관한 연구)

  • Yoa, S.J.
    • Journal of Power System Engineering
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    • v.8 no.2
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    • pp.31-38
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    • 2004
  • The main purpose of this study is to investigate the characteristics of hybrid collection system combined with centrifugal force of cyclone and filtration of bag filter in one unit system. The experiment and numerical simulation are executed for the analysis of collection efficiency and pressure drop characteristics of hybrid system in comparison with those of a general fabric bag filter with the various experimental parameters such as inlet velocity(filtration velocity), dust concentration and dust type, etc.. In present system, dust particles tangentially coming into the system body are controlled by the centrifugal force effect, and the next collection is made out by the filtration mechanism in the fabric filter media. Therefore, the effective first collection causes the decrease of dust loading on the fabric filter, and it presents quite a lower pressure drop of fabric filter than that of a general fabric filter. At the inlet velocity, $21{\sim}27m/sec$ and inlet concentration(fly ash) $300mg/m^3$, pressure drops through the filter media of hybrid system are shown lower as $10{\sim}22mmH_2O$ comparing to those($17{\sim}33mmH_2O$) of a general fabric bag filter.

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Movement of Liquid Metal Droplet in Channel by Continuous Electrowetting Effect (연속적 전기습윤 효과를 이용한 액체금속 액적의 채널 내 거동)

  • Baek, Seungbum;Won, Dong-Joon;Kim, Hojin;Kim, Joonwon
    • Journal of the Korean Society for Precision Engineering
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    • v.33 no.3
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    • pp.217-223
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    • 2016
  • In this paper, the movement of a liquid metal droplet in a channel by continuous electrowetting effect is analyzed. The channel is fabricated using two glass substrates and silicone rubber as spacers, and a mercury droplet and dilute sulfuric acid are added into the channel. The droplet is moved according to voltage applied at both ends of the channel through an electrolyte. According to the shape of the droplet and the applied voltage, the velocity of the droplet is changed. The velocity is proportional to the applied voltage and inversely proportional to the length of the droplet, both theoretically and experimentally. Contact angle hysteresis and a meniscus change were also found in the moving state. This implies the existence of a threshold in movement by Laplace pressure difference. The experiment indicated that the sliding angle was inversely proportional to the width of the droplet but that the voltage threshold was proportional to the width.

A Study on the Performance of Ramp Tabs Asymmetrically Installed in the Supersonic Nozzle Exit (초음속 노즐 출구에 비대칭적으로 설치한 램프 탭의 성능 연구)

  • Kim, Kyoung-Rean;Ko, Jae-Myoung;Park, Jong-Ho
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.35 no.10
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    • pp.934-939
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    • 2007
  • Thrust vector control(TVC) is the method which generates the side force and moment by controlling the exhausting gas directly from the supersonic nozzle to change the trajectory of a missile quickly. In this paper, performance study on the tapered ramp tabs asymmetrically installed in the supersonic nozzle exhaust for the thurst vector control has been carried out using the supersonic cold flow system. To study the shock wave structure and location of the oblique shock wave produced by the ramp tab, the flow field visualization using the schlieren system is conducted. This paper provides the thrust spoilage, three directional forces and moments and distribution of surface pressure on the region enclosed by the tapered ramp tabs.

마그네트론 스퍼터링을 이용하여 TiN 박막을 증착한 도전성 섬유

  • Jang, Jin-Hyeok;Mun, Seon-U;Kim, Gyeong-Hun;Kim, Seong-Min;Lee, Seung-Min;Kim, Jeong-Su;Han, Seung-Hui
    • Proceedings of the Korean Vacuum Society Conference
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    • 2013.02a
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    • pp.168-168
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    • 2013
  • 도전성 섬유(Conductive textile)는 섬유자체의 고유 특성을 유지하면서 전기적인 도전 특성을 갖는 섬유로서, Cu, Ag, Ni 등의 전기전도성이 높은 금속 박막을 증착하여 제작하고 있다. 그러나, 이러한 금속은 공기 중의 산소와 결합하여 쉽게 산화되는 특성을 지니고 있기 때문에 사용 중에 산화되어 도전 특성이 감소하는 단점이 있다. TiN은 금속 못지않은 높은 전기전도성을 지니고 있을 뿐만 아니라, 금속에 비하여 높은 경도에 따른 우수한 내마모 특성, 내부식성 및 낮은 마찰계수를 지니고 있다. 그러나, TiN은 경도가 높기 때문에 섬유의 고유 특성인 유연성이 저하되는 문제가 있다. 본 연구에서는 면(Cotton), PE (Polyester), PP (Polypropylene) 등의 섬유 위에 TiN 박막을 증착하여, 섬유의 유연성을 유지하며 전기전도성과 내마모 특성이 우수한 도전성 섬유를 제작하고자 하였다. TiN 박막 증착을 위하여 ICP-assisted pulsed-DC reactive magnetron sputtering 장비를 사용하였으며, Ar:N2 유량비(Flow rate), Ti 타겟 power, ICP RF power 등을 변화시켜 Ti와 N의 조성비를 조절하였고, 이를 통하여 섬유의 휨이나 접힘에도 도전 특성이 변하지 않고 내마모 특성이 우수한 TiN 박막을 증착하였다. TiN 박막이 증착된 섬유의 전기전도도는 일정한 압력 하에 전기전도도를 측정할 수 있는 장치를 제작하여 측정하였으며, 표면 조성 분포 및 접합력 측정을 위하여 XPS (X-ray Photoelectron Spectroscopy)와 Peel-tester를 이용하였다.

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Characterization and Emission/Absorption Study of a Grimm-type Glow discharge source in the application of high frequency Glow Discharge (고주파 글로우 방전을 이용한 GRIMM형 방전원의 특성 및 방출/흡광분석법 연구)

  • Suh, Jung-Gee;Woo, Jin-Chun
    • Analytical Science and Technology
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    • v.7 no.2
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    • pp.155-164
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    • 1994
  • A conventional Grimm-type glow discharge source was constructed and applied to radio-frequency(13.56MHz) discharge for metal and ceramic analysis. We investigated the emission spectrum for aluminium and aluminium oxide and the influence of discharge operating paramaters including argon pressure, rf-power and DC-bias voltages at the sample-side electrode. Scanning Electron Microscope(SEM) also was used to investigate the effect of rf-sputtering on the microstructure formation of the aluminium oxide. Linear analytical calibration curves were constructed for Manganese and zinc element in samples of low alloy steel(BAS 401-405) and brass(NIST 1108-1117).

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Study on the Flow Characteristics of Supersonic Air Intake at Mach 4 (마하4 초음속 공기 흡입구 유동 특성에 관한 연구)

  • ;;;;Shigeru , Aso
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.34 no.10
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    • pp.61-70
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    • 2006
  • A Supersonic air intake model was designed for the high performance ramjet and dual-mode scramjet engine to operate at Mach 4 flight condition. The air intake was tested in the blowdown-type wind tunnel of Kyushu University to identify the internal flow characteristics corresponding to the flight parameters such as the back pressure, angle of attack and angle of yaw. Flow visualization was achieved by the Schlieren and oil flow visualization techniques. The intake performance was analyzed quantitatively based on the surface pressure and total Pressure measurements. The experimental results were compared with the computational fluid dynamics results. The present study exhibits the fundamental but rarely found experimental results of the high Mach number supersonic air intake.