• 한국수소및신에너지학회논문집
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• 제27권2호
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• pp.220-229
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• 2016

A numerical study on lifted flame structure in impinging jet geometry with syngas composition ratio was investigated. The numerical calculations including chemical kinetic analysis were conducted using SPIN application of the CHEMKIN Package with Davis-Mechanism. The flame temperature and velocity profiles were calculated at the steady state for one-dimensional stagnation flow geometry. Syngas mixture compositions were adjusted such as $H_2:CO=10:90(10P)$, 20 : 80 (20P), 30 : 70 (30P), 40 : 60 (40P), 50 : 50 (50P). As composition ratios are changed from 10P to 50P, the axial velocity and flame temperature increase because the contents of hydrogen that have faster burning velocity increase. This phenomenon is due to increase in good reactive radicals such as H, OH radical. As a result of active reactivity, the burning velocity is more faster and this is confirmed by numerical methods. Consequently, combustion reaction zone was moved to burner nozzle.

• 한국기계가공학회지
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• 제18권8호
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• pp.24-30
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• 2019

This study investigated the heat dissipation characteristics of a heat-sensitive LED. The results of the empirical test showed that the best temperature intensification was found at 90 with 15-fins, and the heatsink installed perpendicular to the direction of the flow of air was directly connected to the air in the largest heat shield area, leading to the best cooling, and the number of fin also resulted increase in the heat discharge area, resulting in the largest cooling action with 15 fins. It was found that the rate of air flow changed in the range of 1.5m/s to 2.5m/s, but only by a deviation of about $2^{\circ}C$ to $3^{\circ}C$ from the current state of 15 fins at 2.5m/s, and the rate of air flow increased, but the performance of the heat release was not significantly increased. As a result wind speed with minimum air flow conditions of 1.5m/s can greatly contribute to the heat dissipation performance.

• 센서학회지
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• 제29권1호
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• pp.1-6
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• 2020

Gas sensors that operate at room temperature have been extensively studied because of sensor stability, lift time, and power consumption. To design effective room-temperature gas sensors, various nanostructures, such as nanoparticles, nanotubes, nanodomes, or nanofibers, are utilized because of their large-surface-to-volume ratio and unique surface properties. In addition, two-dimensional materials, including MoS₂, SnS₂, WS₂, and MoSe, and ultraviolet-activated methods have been studied to develop ideal room-temperature gas sensors. Herein, a brief overview of state-of-the-art research on room-temperature gas sensors and their sensing properties, including nanostructured materials, two-dimensional materials, the ultraviolet-activated method, and ionic-activated gas sensors, is provided.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2005년도 춘계학술대회 논문집
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• pp.1489-1492
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• 2005

Compared to other nano-patterning techniques, Nano imprint Lithography (NIL) has some advantages of high throughput and low process cost. To imprint low temperature and pressure, UV Nano imprint Lithography, which using the monomer based UV curable resin is suggested. Because fabrication of high fidelity pattern on topographical substrate is difficult, bi-layer Nano imprint lithography, which are consist of easily removable under-layer and imprinted pattern, is being used. If residual layer is not remained after imprinting, and under-layer is removed by oxygen RIE etching, we might be able to fabricate the bi-layer pattern for easy lift-off process.

• 공업화학
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• 제7권1호
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• pp.1-8
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• 1996

자동차 엔진용 thermostat에서 냉각수 온도제어를 위해 사용되는 wax의 제조 및 성분 분석을 실시하였다. 제조된 시료에 대해 lift 실험을 실시해 본 결과, 용제 추출법에 의해 제조된 시료가 자동차 엔진용 thermostat으로 사용 가능한 범위내에 있게 됨을 볼 수 있었다. 또한, 원유의 pitch를 용제 추출한 후 감압 증류 및 산처리를 하면 보다 정밀한 wax를 제조 할 수 있음을 알 수 있었다.

• Tribology and Lubricants
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• 제31권4호
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• pp.141-147
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• 2015

Gas foil thrust bearings (GFTBs) have attractive advantages over rolling element bearings and oil film thrust bearings, such as oil-free operation, high speed stability, and high-temperature operation. However, GFTBs have lower load carrying capacity than the other two types of bearings owing to the inherent low gas viscosity. The load carrying capacity of GFTBs depends mainly on the compliance of the foil structure and the formed hydrodynamic wedge, where the gas pressure field is generated between the top foil and the thrust runner. The load carrying capacity of the GFTBs is very important for the suitable design of oil-free turbomachinery with high performance. The aim of the present study is to identify the characteristics of the load carrying performance of GFTBs. A new test rig for the experimental measurements is designed to provide static loads up to 800 N using a pneumatic cylinder. The maximum operating speed of the driving motor is 30,000 rpm. A series of experimental tests—lift-off test, static load performance test, and maximum load capacity test—estimate the performance of a six-pad GFTB, in terms of the static load, driving torque, and temperature. The maximum load capacity is determined by increasing the static load until the driving torque rises suddenly with a sharp peak. The test results show that the torque and temperature increase linearly with the static load. The estimated maximum load capacity per unit area is approximately 80.5 kPa at a rotor speed of 25,000 rpm. The test results can be used as a design guideline for GFTBs for realizing oil-free turbomachinery.

• 한국안전학회지
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• 제18권2호
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• pp.34-39
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• 2003

In this paper, when CF/PEEK laminates for high efficiency space structure are subjected to FOD(Foreign Object Damage), the effects of temperature change on the impact damages(interlaminar separation and transverse crack) of CF/PEEK laminates and the relationship between residual lift and impact damages are experimentally investigated. Composite laminates used in this experiment are CF/PEEK orthotropic laminated plates, which have two-interlaces [$0^{\circ}_4/90^{\circ}_8/0^{\circ}_4$]. A steel ball launched by the air gun collides against CF/PEEK laminates to generate impact damages. And then CF/PEEK specimens with impact damages are observed by a scanning acoustic microscope under room and high temperatures. In this experimental results, various relations are experimentally observed including the delamination area vs. temperature change, the bending strength vs. impact energy and the residual bending strength vs. impact damage of CF/PEEK laminates.

• 전기전자학회논문지
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• 제24권2호
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• pp.673-676
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• 2020

본 논문에서는 IT 기술을 접목한 초저온 순환 냉각 방식의 전신 관리 시스템을 제안한다. 제안하는 시스템은 다음과 같은 특징들을 가진다. 첫 번째로 초저온으로 냉각된 질소가스를 관리기 내부에서 순환시킴으로서 유지비용을 최소화한다. 두 번째로 온도센서와 산소농도센서로 측정된 정보를 기초로 질소가스를 공급하여 안전한 초저온 전신관리를 제공한다. 세 번째로 사용자의 신장을 입력한 후에 전자동 리프트를 이용하여 제어 가능한 편리한 초저온 전신관리를 제공한다. 네 번째로 접근이 쉽고 조작이 편리한 GUI 및 전신관리 시스템 운영을 위한 관리자 전용 웹 프로그램의 GUI를 제공한다. 제안된 시스템의 성능을 평가하기 위하여 공인시험기관에서 실험한 결과는 온도센서 정확도는 세계 최고 수준인 ±5%의 범위에서 측정이 되었고, 전신관리 온도범위는 세계 최고 수준(-110℃ ~ -140℃)보다 넓은 -110℃ ~ -150℃의 범위가 측정되었다. 또한, 습도는 세계 최고 수준인 40% 미만으로 측정이 되었고, 산소농도도 세계 최고 수준인 18% 이상으로 측정되었다. 따라서 본 본문에서 제안한 IT 기술을 접목한 초저온 순환 냉각 방식의 전신 관리 시스템의 성능이 세계 최고 수준과 동일한 결과를 산출하였기 때문에 그 효용성이 입증되었다.

• 센서학회지
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• 제9권3호
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• pp.171-176
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• 2000

반응성 스퍼터링과 고주파 마그네트론 스퍼터링으로 각각 증착된 MgO 박막과 그 위에 증착된 백금박막의 열처리 온도 및 시간에 따른 물리적, 전기적 특성을 4침 탐침기, 주사전자현미경 및 X선 회절법을 이용하여 분석하였다. $1000^{\circ}C$, 2시간의 열처리 조건하에서 MgO 박막은 백금박막과 화학적 반응없이 백금박막의 열산화막에 대한 부착특성을 개선시켰으며, 그 위에 증착된 백금박막의 면저항 및 비저항은 각각 $0.1288\;{\Omega}/{\square}$, $12.88\;{\mu}{\Omega}{\cdot}cm$이었다. Lift-off 방법을 이용하여 $SiO_2$/Si기판상에 백금 저항체를 만들었으며, 백금 와이어, 백금 페이스트 그리고 SOG를 이용하여 마이크로 열 센서용 박막형 Pt-RTD를 제작하였다. $25{\sim}400^{\circ}C$의 온도범위에서 $1.0{\mu}m$의 두께를 갖는 제작된 Pt-RTD의 저항온도계수는 벌크 백금에 가까운 $3927ppm/^{\circ}C$로 측정되었다. 측정온도범위내에서 저항값은 선형적인 변화를 보였다.

• 한국전기전자재료학회:학술대회논문집
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• 한국전기전자재료학회 1997년도 추계학술대회 논문집
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• pp.335-338
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• 1997

Platinum-Cobalt alloy thin films were deposited on A1$_2$O$_3$substrate by magnetron cosputtering for RTD temperature sensors with wide temperature ranges. We made Pt-Co alloy resistance patterns on the A1$_2$O$_3$substrate by lift-off method and fabricated Pt-Co alley RTD temperature sensors by using Pt-wire, Pt-paste. We investigated the physical and electrical characteristics of theme films under various conditions, input power, working vacuum, annealing temperature and time, and also after annealing these films. The resistivity and sheet resistivity of these films were decreased with increasing the annealing temperature. At input power of Pt : 4.4 W/cm$^2$, Co : 6.91 W/cm$^2$, working vacuum of 10 mTorr and annealing conditions of 800$^{\circ}C$ and 60 min, the resistivity and sheet resistivity of Pt-Co thin films was 15${\mu}$$\Omega$$.$cm and 0.5$\Omega$/ , respectively, and the TCR value of Pt-Co alloy thin films with thickness of 3000${\AA}$ was 3740ppm/$^{\circ}C$ in the temperature range of 25∼600$^{\circ}C$. These results indicate that Pt-Co alloy thin films hove potentiality for the RTD with wide temperature ranges.