• Fire Science and Engineering
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• v.30 no.1
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• pp.1-5
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• 2016

Cases of cardiac arrests due to cardiovascular ailments have increased recently., portable Current portable resuscitators which can be automatically supply oxygen operated by the pressure of supplied oxygen without manual or electronic actuators are now widely used in emergency worldwide. However, reductions in Pressure drop characteristics through the extended use of this type of resuscitator, however, is are not well-known described. This paper describes the reduction in pressure loss drop performance of the various holes in within the flow control disc of with various hole size of the portable resuscitators using on breathing resistance through the CFD simulation, and suggests the an optimum optimal design of the hole shapes for the minimization of alteration in order to minimize this pressure drops.

• Journal of Korean Society of Water and Wastewater
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• v.34 no.2
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• pp.139-147
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• 2020

This paper suggests a nonlinear pressure consideration scheme through an unsteady pipe network analyzer for leakage detection with a portable pressure wave generator. In order to evaluate the performance of a proposal scheme, linear input pattern has been simulated and experiments had been carried out under both no leakage and one leakage conditions in a reservoir-pipeline-valve system. This method using portable pressure wave generator showed that a leakage can be detected from a reflection where a leakage is originated through time domain analysis. Meaningful similarity in pressure response between nonlinear input pattern and experimental results were found both no leakage and a leakage conditions.

• Journal of the Korean Society of Propulsion Engineers
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• v.3 no.3
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• pp.53-61
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• 1999

Impinging jets are observed when exhaust gases from missiles or V/STOL aircrafts impinge on the ground, flame deflector, ship deck, etc. The flow shows different patterns according to the nozzle geometry, nozzle-to-plate distance, and plate angle, for example. This paper describes experimental works on the phenomena (pressure distribution, occurrence of stagnation bubble, and so on.) when underexpanded supersonic jets impinge on a perpendicular flat plate using a supersonic cold-flow system, and compares the results with those obtained using a shock tunnel. The flow characteristics for the supersonic cold-flow system were also investigated. Surface pressure distribution of supersonic cold-flow system differed from that of shock tunnel because of water and temperature in the low-pressure chamber. Surface pressure distribution as to underexpanded ratio showed similar patterns together.

• Journal of the Korean Society of Propulsion Engineers
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• v.13 no.6
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• pp.34-40
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• 2009

The present study describes the methods and standards for the combustion stability assessment of a thrust chamber and a gas generator as parts of a liquid rocket engine. The first method uses a statistical approach through typical static combustion tests and the second one a dynamic assessment identifying decaying characteristics of pressure fluctuations excited by a pulse generating device. Based on accumulated test results, it is concluded that the maximal values for combustion stability are 3% of a chamber static pressure with a Root-Mean-Square value of pressure fluctuations, and 10 msec with a decay time.

• Journal of the Institute of Electronics Engineers of Korea SC
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• v.44 no.1
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• pp.94-99
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• 2007

Many cases of acute cardiac shock and cardiac arrest in emergency room and ICU have been increasing. In this case, ECMO with centrifugal pump has been used generally. However, due to the heavy weight and big size, the system is not adequate for emergency cases. And other defects of this system are that membrane oxygenator's pressure is high and blood are exposed to the air. There was some tries of ECMO using pulsatile pump, but it was found that the weak point of these system is high peak pressure and hemolysis. The mechanism of twin pulsatile pump is that Membrane oxygenator Outlet Pump(MOP) make negative pressure when Membrane oxygenator Inlet Pump(MIP) provides high positive pressure, and the negative pressure will decrease positive pressure of Membrane Oxygenator. Our group analyzed this advantage through In-Vitro and 12 Cases In-Vivo test.

• Journal of Korean Ophthalmic Optics Society
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• v.5 no.2
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• pp.163-165
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• 2000

We investigated visible light radiated from Plasma Focus device by time-integrated analyzed method. Plasma focus is a device that translated from electric energy into visible light by electric discharge. Spectral analysis is using Monochromator(focal length = 0.5 m). Time-integrated spectrum is analyzed with densitometer the film which developed a constant range of wavelength. The condition of visible emission was that the discharging voltage was 13 kV and the working gas were Argon and Helium.

• Proceedings of the Korean Vacuum Society Conference
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• 2012.08a
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• pp.164-164
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• 2012

저진공 (＞100 mTorr)에서 냉음극 변압기 전원 소스를 이용하여 플라즈마를 발생시키는 시스템을 개발하였다. 또한 이 장치를 이용하여 Tetraethylorthosilicate (TEOS)를 기화시켜 이산화규소 ($SiO_2$) 박막 증착 기술을 연구하였다. 공정 압력은 400~1,000 mT이었다. 증착된 박막의 박막 두께, 굴절률 등의 측정을 실시하였다. 결과를 요약하면, 플라즈마 공정 압력이 증가함에 따라 박막 증착 속도는 약 200~300 A/min이었다. 또한 전압이 1,100에서 2,100 V로 증가함에 따라 산화막의 증착 속도는 약 300에서 40 nm/min으로 증가하였다. TEOS만을 사용하였을 때 굴절률은 약 1.5~1.6정도였다. 그러나 TEOS에 산소를 추가하면 자연 산화막의 굴절률인 1.46을 쉽게 얻을 수 있었다. 초기 연구 결과를 정리하면 냉음극 변압기 플라즈마 장치는 향후 실용적인 산화막 플라즈마 증착 연구 장치로 사용될 수 있을 것으로 생각된다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.423-425
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• 2017

When many space launchers and rockets need to be separated, the pyrotechnic separators have been widely used because of their high reliability and high energy generation. However, intensive pyroshock and debris from the high-explosive type separator may cause fatal damage to the equipment inside of the space launchers or rockets. To solve this problem, a pressure-cartridge type low-impact separator has been developed. In this study, one of the low-impact separators, the split-type pyrolock, was used. We established a mathematical model for the split-type pyrolock that simulates the state of combustion gas and the separation behavior of four independent internal components and verified the mathematical model through comparing with experiment results.

• Proceedings of the Korean Institute of Surface Engineering Conference
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• 2017.05a
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• pp.93-93
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• 2017

고전력 펄스 전원공급장치를 이용한 마그네트론 스퍼터링(high-power impulse magnetron sputtering; HiPIMS)과 직류(direct current; DC) 전원공급장치를 이용한 마그네트론 스퍼터링(DC 스퍼터링)을 이용하여 제조한 티타늄 질화물(titanium nitride; TiN) 박막의 특성을 비교하였다. HiPIMS와 DC 스퍼터링 공정 중에 빗각증착을 적용하여 TiN 박막의 미세구조와 기계적 특성의 변화를 확인하였다. TiN 박막을 코팅하기 위한 기판으로 스테인리스 강판(SUS304)과 초경(cemented carbide; WC-10wt.%Co)을 사용하였다. 기판은 알코올과 아세톤으로 초음파 처리를 실시하여 기판 표면의 불순물을 제거하였다. 기판 청정 후 진공용기 내부의 기판홀더에 기판을 장착하고 $2.0{\times}10^{-5}torr$의 기본 압력까지 진공배기를 실시하였다. 진공 용기의 압력이 기본 압력에 도달하면 아르곤(Ar) 가스를 진공용기 내부로 ${\sim}10^{-2}torr$의 압력으로 주입하고 기판홀더에 라디오 주파수(radio frequency; rf) 전원공급장치를 이용하여 - 800 V의 전압을 인가하여 글로우 방전을 발생시켜 30 분간 기판 표면의 산화막을 제거하는 기판청정을 실시하였다. 기판청정이 완료되면 기본 압력까지 진공배기를 실시하고 Ar과 질소($N_2$)의 혼합 가스를 진공용기 내부로 ${\sim}10^{-3}torr$의 압력으로 주입하여 HiPIMS와 DC 스퍼터링으로 TiN 박막 제조를 실시하였다. 빗각의 크기는 $45^{\circ}$와 $-45^{\circ}$이었다. 제조된 TiN 박막은 주사전자 현미경, 비커스 경도 측정기 그리고 X-선 회절 분석기를 이용하여 특성을 분석하였다. HiPIMS로 제조한 TiN 박막은 기판 전압을 인가하지 않아도 색상이 노란색을 보이지만, DC 스퍼터링으로 제조한 TiN 박막은 기판 전압을 인가하지 않으면 노란색을 보이지 않고 어두운 갈색에 가까운 색을 보였다. TiN 박막의 경도는 HiPIMS로 제조한 TiN 박막이 DC 스퍼터링으로 제조한 TiN 박막보다 높았다. 이러한 TiN 박막의 특성 차이는 DC 스퍼터링과 비교하여 높은 HiPIMS의 이온화율에 의한 결과로 판단된다. 빗각을 적용한 TiN 박막은 미세구조 변화를 보였으며 이러한 미세구조 변화는 TiN 박막의 특성에 영향을 미치는 것을 확인하였다.

• Journal of the Korean Vacuum Society
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• v.16 no.4
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• pp.244-249
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• 2007

Deadweight piston gauge have been widely used as a fundamental instrument of precise pressure measurement because they are robust, accurate, potable, convenient to use and are able to realize the definition of pressure as farce per unit area. Basically, a deadweight piston gauge consists of a piston mounted vertically in a close-fitting cylinder filled with a gas and weights of known mass values. The pressure to be measured is applied to the base of the piston generating an upward vertical force, and is balanced by the downward gravitational force generated by weights. These instruments can be used to measure pressures above 10 kPa because of tare weights including piston. However, using a variable bell-jar pressure method and a newly developed weight loading device we can extend the application range of deadweight piston gauge to lower pressures. In this paper, we present the practical calibration results for two CDGs(Capacitance diaphragm gauge, MKS) with full-scale ranges of 1.33 kPa and 13.3 kPa, respectively.