• Electrical & Electronic Materials
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• v.6 no.5
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• pp.446-453
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• 1993

초기충진압력이 서로 다른 시편에 가한 가압횟수와 열처리시간의 혼합공정이 임계전류밀도 특성에 미치는 영향을 관찰하기 위하여 power-in-tube방법으로 초전도 선재를 제조하였다. 일정 초기충진압력에서 테이프화를 위한 열처리 및 가압이 혼합공정횟수가 증가할수록 임계전류밀도가 증가하였다. 초기충진압력이 1000kg/$cm^{2}$에서 Bi-2223 고온상 체적비가 가장 높게 나타났고 결정립이 판상으로 성장되었을 뿐만 아니라 C축과 직각방향으로 잘 배양되어 있음을 관찰할 수 있었다. 특히 초기충진압력 1000kg/$cm^{2}$의 시편을 두께를 줄이기 위하여 3회 가압하고 450시간 열처리하였을때 임계전류밀도가 5800A/$cm^{2}$를 나타내었으며 이를 중심으로 500, 2500kg/$cm^{2}$이 양측단으로 가우시안분포를 보였다. 결론적으로 시편의 임계특성은 적정 초기충진압력, Bi-2223 고온상 체적비, 테이프화를 위한 가압횟수, 결정의 일방향배열, 결정립의 성장등에 강하게 의존함을 알 수 있었다.

• Journal of Energy Engineering
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• v.4 no.1
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• pp.85-94
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• 1995

본 연구에서는 최근 차량용 대체연료로서 주목받고 있는 천연가스의 연소특성을 규명하기 위해 밀폐된 정적연소실을 이용, 당량비, 초기압력 및 점화위치 변화에 따른 연소실험을 행하였으며, 그 결과 다음과 같은 결론을 얻었다. 메탄-공기 예혼합기의 화염전파과정은 이론혼합기 부근에서 구면형으로 진행되는데 반해, 과농 또는 과박 혼합기 그리고 점화위치가 연소실 벽면에 가까울수록 타원형으로 진행되며, 초기압력이 증가함에 따라 화염전파는 느려진다. 화염전파속도와 연소 속도는 초기압력이 낮고 점화위치가 연소실 중심에 가까울수록 빠르며, 당량비 1.0∼1.1 사이에서 최대치를 보인다.

• Nuclear Engineering and Technology
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• v.27 no.5
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• pp.775-783
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• 1995

This study is to assess the effects of increasing wall thickness on the safety margin of pressure tube in operating and of lowering initial hydrogen concentration on the DHC growth in respect to the improvement of the reliability of pressure tube in CANDU reactors. The pressure tube with thicker wall of 5.2 mm shows much higher safety margin for flaw tolerance by 25％ than the current 4.2mmm tube. The thicker pressure tubes have a great benefit in LBB assessment including the initial crack depth at which DHC occurs, the crack length at onset of leaking and the available time for action. The resistance for the pressure tube ballooning at LOCA accident is also increased with the thicker tube. The calculations for Heq concentration after 20 years of operation as a function of wall thickness and initial hydrogen concentration show that the 5.2 mm nil thickness tube with 5 ppm initial hydrogen concentration is the most resistant to DHC. with the lower initial hydrogen concentration, TSS temperature for the precipitation or hydride decreases and the crack growth during cooldown reduces.

• Journal of the Korean Vacuum Society
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• v.20 no.2
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• pp.141-145
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• 2011

ZnO:Al thin films were deposited by RF magnetron sputtering with various base pressure, and their structural, optical, and electrical properties were studied. The influence of the base pressure on the ZnO:Al thin film was confirmed and a high-quality thin film was obtained by controlling the base pressure. In all Al-doped ZnO thin films, the preferred orientation of (002) plane was observed and light transmittance in visible region (400 nm~800 nm) had above 85%. With decreasing of base pressure, crystallinity, resistivity, and figure of merit were improved. The improvement of resistivity with base pressure was attributed to the change of grain size.

• Journal of Energy Engineering
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• v.11 no.2
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• pp.122-129
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• 2002

The analytical models and algorithm of the SPIKE code, which has been developed by KAERI's KALIMER team to investigate the sodium-water reaction phenomena in the liquid metal reactor, were introduced with its verification calculation results. The sodium water reaction of KALIMER IHTS was evaluated. Early stage of the sodium-water reaction consists of wave and mass transfer regimes. The pressure variations were independent of specific design features in the wave transfer regime. However in the mass transfer regime, the pressure variations were strongly dependent on cover gas volume and rupture disk set pressure. The early stage SWR analysis showed that the KALIMER IHTS with an appropriate cover gas volume and rupture disk set pressure had enough margin to its design pressure.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.31 no.5
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• pp.235-241
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• 2018

The internal pressure is a critical parameter for designing a pressure vessel. The static pressure that a pressure vessel must withstand is usually determined according to the various codes and standards with simple formula or numerical simulations considering the geometric parameters such as diameter and thickness of a vessel. However, there is no specific codes or technical standards we can use practically for designing of pressure vessels which have to endure the detonation pressure. Detonation pressure is a kind of dynamic pressure which causes an impulsive pressure on the vessel wall in a extremely short time duration. In addition, it is known that the magnitude of reflected pressure at the vessel wall due to the explosion can be over twice the incident pressure. Therefore, if we only consider the reflected pressure, the design of the pressure vessel can be too conservative from the economical point of view. In this study, we suggest a practical method to evaluate the magnitude of maximum allowable pressure that the pressure vessel can withstand against the detonation inside a vessel. As an example to validate the proposed method, we consider the pressure vessel containing hydrogen gas.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2010.05a
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• pp.138-141
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• 2010

A study to reduce the ignition peak pressure of gas generator for the missile launching system was accomplished. The igniter, as the energy release device for igniting the propellant, is aimed at simultaneous ignition of bundled 3-layered propellant grain without unstable burning. In case of our gas generator which must use the double-base propellant with low ignition property, the fast ignition of propellant and reduction of initial peak pressure should be required for the satisfaction of ejection velocity and acceleration condition. By applying MTV ignition charge for the igniter of gas generator, we accomplished all system performance requirements.

• Journal of the Korean Institute of Gas
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• v.9 no.1 s.26
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• pp.38-43
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• 2005

To examine the characteristics of the explosion of city gas, the concentration of oxygen was changed with the change of initial pressure. From the result of the experiment, as the concentration of oxygen was low, the explosion limit became narrow and the minimum concentration of oxygen for the explosion was $12\%$. Furthermore, As the increase of the initial pressure, explosion ranges were a little increased. And as the change of the initial pressure, the maximum explosion pressure were $6.3 kgf/cm^2{\cdot}g,\;12.7 kgf/cm^2{\cdot}g$ and the maximum pressure rising velocity were $245.63 kgf/cm^2/s,\;427.88 kgf/cm^2/s$.

• Journal of the Korean Institute of Gas
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• v.16 no.1
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• pp.8-14
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• 2012

Hydrogen is considered to be the most important future energy carrier in many applications reducing significantly greenhouse gas emissions, but the explosion safety issues associated with hydrogen applications need to be investigated and fully understood to be applicable as the carrier. The risk associated with a explosion depends on an understanding of the impacts of the explosion, particularly the pressure-time history during the explosion. This work provides the effects of explosion parameters, such as specific heat ratio of burned and unburned gas, equilibrium maximum explosion pressure, and burning velocity, on the pressure-time history with flame growth model. The pressure-time history is dominantly depending on the burning velocity and equilibrium maximum explosion pressure of hydrogen-air mixture. The pressure rise rate increase with the burning velocity and equilibrium maximum explosion pressure. The specific heat ratio of unburned gas has more effect on the final explosion pressure increase rate than initial explosion pressure increase rate. However, the specific heat ratio of burned gas has more influence on initial explosion pressure increase rate. The flame speeds are obtained by fitting the experimental data sets. The flame speeds for hydrogen in air based on our experimental data is very low, making a transition from deflagration to detonation in a confined space unlikely under these conditions.

• Journal of Korean Society of Environmental Engineers
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• v.39 no.1
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• pp.19-25
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• 2017

In this study, a electrostatic filter which could be applicable to road environment was developed and evaluated in adsorption capacity. The evaluation were performance for removal by particle size and adsorption amount by pressure using ASERAE 52.1 and 52.2. The range of size for removal test was $0.3{\mu}m{\sim}10.0{\mu}m$ which had 12 steps. The filter showed 91.3% removal efficiency from $2.5{\mu}m$ and under the size, average 53.5% proportional to decreasing size value. The weight removal was 96.7% from 22.6 mmaq, initial pressure to 35 mmaq, end pressure with $715.9g/m^2$, the adsorption amount. The shape of isotherm was expressed as Langmuir's one. After washing saturated filter with dust to end pressure, the initial pressure and adsorption amount of the filter showed a light drop with no removal efficiency decline.