• Korean Journal of Optics and Photonics
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• v.3 no.3
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• pp.178-182
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• 1992

An air-cooled discharge-heated copper-vapor laser system with its inter-electrode distance of 45 cm has been developed by utilizing an alumina ceramic plasma tube of 1.6 cm in diameter and 50 cm in lengih. For operating the laser, a dc high voltage power supply with output rating of 6 kV and 500 mA, a resonant charging circuitry consisting partly of an 1.8 H inductor assembly and a 5 nF storage capacitor, and a thyratron driver operating up to 7 kHz have also been developed. The present laser system starts lasing at the tube temperature of about $1350^{\circ}C$ and an maximum average output power of 0.7 W has been obtained at 12 kV, 4.5 kHz. 50 mbar of Ne buffer gas pressure, and at the tube temperature of $1460^{\circ}C$.

• Proceedings of the KIPE Conference
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• 2007.11a
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• pp.209-211
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• 2007

본 논문에서는 회생에너지 저장시스템의 충/방전 제어를 위한 가선전압 모의 장치를 제안한다. 제안된 시뮬레이터는 실측된 가선전압 데이터를 입력으로 받아 실측 가선전압과 동일한 전압패턴으로 모사한다. 이러한 전압패턴은 회생에너지가 포함된 가선전압이며 이를 토대로 에너지 저장시스템에 연계시켜 충/방전 제어를 좀 더 효율적으로 수행할 수 있다. 제안된 시뮬레이터는 AC/DC 컨버터 타입으로 시뮬레이션과 실험을 통해 제안된 시스템의 타당성을 확인하였다.

• The Proceedings of the Korean Institute of Illuminating and Electrical Installation Engineers
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• v.11 no.2
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• pp.56-63
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• 1997

진공에서의 파괴는 파괴전구현상으로부터 개시되고, 파괴전구현장중에서 가장 중요한 과정은 Metallic Field Electron Emission과 Micro Discharge이다. 진공내에서 평등전계 갭의 전기적 파괴특성 중 전극에 흐르는 방전전구전류는 전계에 의존하고 Fowler Nordheim 식으로 나타낼 수 있다. 이 논문은 압력 760, 1.2$\times$10-3, 1.2$\times$10-5[torr]과 스테인레스 전극을 미소갭 20, 50, 75, 100[$\mu\textrm{m}$]으로 구성하여 방전전구전류에 대해서 실험적으로 연구했다. 전극갭과 압력변화에 따라 얻어진 I-V 특성곡선을 Fowler Nordheim의 전계방출 이론에 입각해서 분석한 결과, 진공중 미소갭의 전기적 파괴기구는 Metallic Field Electron Emission (M-FEE)에만 의존되었다.

• Proceedings of the KIPE Conference
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• 2012.07a
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• pp.496-497
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• 2012

전해 커패시터는 인버터 등을 포함하는 전력 변환 장치에 직류 전압 평활용으로 사용되며, 다른 구성 요소와 비교하여 고장 발생률이 가장 높다. 본 논문은 이러한 전해 커패시터의 상태를 진단하는 방법에 대한 것으로 커패시터 전압의 충, 방전을 이용한다. 전해 커패시터가 충전된 상태에서 전동기에 전류를 인가함으로써 커패시터에 충전된 에너지를 방전 시키고, 방전된 에너지로부터 커패시턴스를 추정한다. 정상 상태의 커패시터와 열화된 상태의 커패시터의 용량 변화로부터 커패시터의 상태를 판별한다. 본 논문에서 제안된 기법은 상용 인버터에 적용하는 데 추가의 하드웨어가 필요하지 않아 저가로 구현할 수 있으며, 커패시터 용량의 변화를 신뢰성 있게 추정할 수 있기 때문에 커패시터 고장진단에 효과적이다.

• Korean Journal of Materials Research
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• v.5 no.2
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• pp.178-183
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• 1995

Piezoelectric properties of sintered specimen having a tetragonal phase of $Pb_{0.9888}Sr_{0.012}(Zr_{0.52}Ti_{0.48})O_{3}$ were comparatively studied with two different poling methodes, i.e., DC field and corona discharge technique. Internal stress of poled specimens by indentation fracture toughness was analyzed to evaluate degradation phenomenon. As the results, it was confirmed that corona discharge poling technique is practicable and has merits such as low-temperature poling, slow degradation and no electric breakdown comparing to DC field poling. However, corona discharge technique showed lower Kp value than DC field poling.

• Journal of IKEEE
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• v.23 no.3
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• pp.865-872
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• 2019

We developed a one-dimensional Ar fluid model running in DC-type applied voltage with a sine and a pulse waveform at the atmosphere pressure. We investigated the light emissions and efficiencies of ${\lambda}_{128nm}$, ${\lambda}_{727nm}$, ${\lambda}_{912nm}$ and ${\lambda}_{966nm}$ from the Ar excited particles. From the results, the light emission of ${\lambda}_{128nm}$ and ${\lambda}_{727nm}$ in the applied voltage with a sine waveform were almost two times as in DC voltage type. The shorter the switching time of applied voltage was, the more the light emissions of ${\lambda}_{128nm}$ and ${\lambda}_{727nm}$ were. We discussed the power consumption and Joule heating by charged particles.

• Journal of the Korean Society of Propulsion Engineers
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• v.20 no.3
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• pp.54-62
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• 2016

Micro plasma thruster (${\mu}PT$) was studied experimentally with a dual-stage micro-hollow cathode discharge (MHCD) plasma. Electrostatic-like acceleration exhibiting more directional and elongated exhaust plume was achieved by a dual layer MHCD at the total input power less than 10 W with argon flow rate of 40 sccm. V-I characteristic indicated that there was an optimal regime for dual-stage operation where the acceleration voltage across the second stage remained constant. Estimated exhaust plume length showed a similar trend to the analytic estimate of exhaust velocity which scales with an acceleration voltage. ${\mu}PT$ with multiple holes exhibited similar performance with single-hole thruster indicating that higher power loading is possible owing to decreased power through each hole. Boltzmann plot of atomic argon spectral lines showed average electron excitation temperature of about 2.6 eV (~30,170 K) in the exhaust plume.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.34 no.3
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• pp.245-250
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• 2010

The procedure for estimating the gas (rotational) temperature of an air discharge in supersonic flows is presented in detail. Since direct measurement of the temperature in a supersonic flow is difficult, a nonintrusive measurement was performed by optical emission spectroscopy based on the emission spectra of nitrogen molecular ions. A detailed explanation, including the equations for emission line intensity, is presented in order to understand the structure of the emission spectra of nitrogen molecular ions. Using the obtained representation for emission spectrum, a synthetic spectrum of the first negative system of $N_2^+$ is obtained, and it is compared with the experimentally measured spectrum. Within a relative error of approximately 6.8% for the overall band spectra, the synthetic and measured spectra agree well. In the case of a 25-mA DC air discharge in a supersonic (Mach 3) flow, the gas temperature profile shows an approximately linear variation and a peak temperature of approximately 350 K.

• Journal of the Korean Vacuum Society
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• v.20 no.2
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• pp.114-126
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• 2011

The light propagation along a long positive column has been observed in a cold cathode fluorescent lamp. The optical signals are observed with the DC and AC voltage power during lamp operation. The light propagating is observed in the operation with the DC-rippled voltage as well as the AC-voltage. The optical signals propagate from the high voltage side to the ground. These signals show two kinds of features according to the before and after Townsend breakdown. At the dark current before Townsend breakdown, the optical intensity is damped and the propagation velocity is $10^4{\sim}10^5m/s$. At the high current of normal glow after Townsend breakdown, the propagation velocity is 1$10^5{\sim}10^6m/s$ without damping.

• Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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• 2009.11a
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• pp.265-265
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• 2009

전기이중층 커패시터 전극으로 사용하는 활성탄에 도전제로서 CNT와 super-p의 함량에 따른 이중층 커패시터의 특성을 연구하였다. CNT 함량이 4wt%까지는 도전제로서 CNT 함량이 증가할 수록 용량이 감소하는 반면 6wt%이상에서는 CNT 함량이 증가할 수록 단위 체적당 정전용량이 증가하였다. 충, 방전 특성과 직류 저항도 정전용량의 경향과 유사함을 보이고 있으며 이와 같은 결과는 비표면적이나 도전율에 의한 결과 보다는 분산성에 의한 결과로 예상된다. Super-p 10.5wt%, CNT 6.0wt%에서 단위 체적당 정전용량은 $22g/cm^3$, 직류저항 6.1[$\Omega$]의 전기이중층 커패시터 특성을 얻을 수 있었다.