• 한국진공학회:학술대회논문집
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• 한국진공학회 2013년도 제44회 동계 정기학술대회 초록집
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• pp.367-367
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• 2013

Commercial applications of indium tin oxide (ITO) can be separated into two useful areas. As it is perceived to bear electrical properties and optical transparency at once, its chance to apply to promising fields, usually for an optical device, gets greater in the passing time. ITO is one of the transparent conducting oxides (TCO), and required to carry the relative resistance less than $10^{-3}{\Omega}$/cm and transmittances over 80 % in the visible wavelength of light. Because ITO has considerable refractive index, there exist applications for anti-reflection coatings. Anti-reflection properties require gradual change in refractive index from films to air. Such changes are obtained from film density or nano-clustered fractional void. Glancing angle deposition (GLAD) method is a well known process for adjusting nanostructure of the films. From its shadowing effects, GLAD helps to deposit well-controlled porous films effectively. In this study, we are comparing the reference sample to samples coated with controlled ITO multilayer accumulated by an e-beam evaporation system. At first, the single ITO layer samples are prepared to decide refractive index with ellipsometry. Afterwards, ITO multilayer samples are fabricated and fitted by multilayer ellipsometric model based on single layer data. The structural properties were measured by using atomic force microscopy (AFM), and by scanning X-ray diffraction (XRD) measurements. The ellipsometry was used to determine refractive indices and extinction coefficient. The optical transmittance of the film was investigated by using an ultraviolet-visible (UV-Vis) spectrophotometer.

• Asian Journal of Atmospheric Environment
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• 제5권2호
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• pp.113-120
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• 2011

Adsorbent combination studies have been carried out to remove nitrogen dioxide ($NO_2$) and volatile organic compounds (VOCs: BTEX) out of a subway environment characterized by high flow and low concentration. Optimal conditions for the high removal efficiency of the concerned target compounds were obtained through testing a series of control factors such as adsorbent sorts, thicknesses, and superficial velocity. It was found that the efficiencies increased as the specific surface area of activated carbon and its thickness increased, and external void fraction decreased. Furthermore, mixed activated carbon with granular and constructed contents was extensively tested to reduce pressure drop through the carbon bed. It was found that the performance of higher contents of granular activated carbon was better than that of higher contents of the constructed carbon. When the mixed carbon was applied to the subway ventilation system in order to eliminate $NO_2$ and VOC simultaneously, the removal efficiencies were found to be 75% and 85%, respectively.

• 한국도로학회논문집
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• 제17권6호
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• pp.1-9
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• 2015

PURPOSES : The objective of this study is to propose a quality control and quality assurance method for use during asphalt pavement construction using non-destructive methods, such as ground penetrating radar (GPR) and an infrared (IR) camera. METHODS : A 1.0 GHz air-coupled GPR system was used to measure the thickness and in situ density of asphalt concrete overlay during the placement and compaction of the asphalt layer in two test construction sections. The in situ density of the asphalt layer was estimated based on the dielectric constant of the asphalt concrete, which was measured as the ratio of the amplitude of the surface reflection of the asphalt mat to that of a metal plate. In addition, an IR camera was used to monitor the surface temperature of the asphalt mat to ensure its uniformity, for both conventional asphalt concrete and fiber-reinforced asphalt (FRA) concrete. RESULTS : From the GPR test, the measured in situ air void of the asphalt concrete overlay gradually decreased from 12.6% at placement to 8.1% after five roller passes for conventional asphalt concrete, and from 10.7% to 5.9% for the FRA concrete. The thickness of the asphalt concrete overlay was reduced from 7.0 cm to 6.0 cm for the conventional material, and from 9.2 cm to 6.4 cm for the FRA concrete. From the IR camera measurements, the temperature differences in the asphalt mat ranged from $10^{\circ}C$ to $30^{\circ}C$ in the two test sections. CONCLUSIONS : During asphalt concrete construction, GPR and IR tests can be applicable for monitoring the changes in in situ density, thickness, and temperature differences of the overlay, which are the most important factors for quality control. For easier and more reliable quality control of asphalt overlay construction, it is better to use the thickness measurement from the GPR.

• 전기학회논문지
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• 제56권6호
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• pp.1092-1098
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• 2007

Since one decade, the detection of HFPD (High frequency Partial Discharge) has been proposed as one of the effective method for the diagnosis of the power component under service in power grids. As a tool for HFPD detection, Metal Foil sensor based on the embedded technology has been commercialized for mainly power cable due to its advantages. Recently, for the on-site noise discrimination, several PA (Pulse analysis) methods have been reported and the related software, such as Neural Network and Fuzzy, have been proposed to separate the PD (Partial Discharge) signals from the noises since their wave shapes are completely different from each other. On the other hand, the relevant fundamental investigation has not yet clearly made while it is reported that the effectiveness of the current methods based on PA is dependant on the types of sensors. Moreover, regarding the identification of the vital defects introducible into the Power Cable, the direct identification of the nature of defects from the PD signals through Metal Foil coupler has not yet been realized. As a trial for solving above shortcomings, different types of software have been proposed and employed without any convincing probability of identification. In this regards, our novel algorithm 'PA Map' based on the pulse analysis is suggested to identify directly the defects inside the power cable from the HFPD signals which is output of the HFCT and metal foil sensors. This method enables to discriminate the noise and then to make the data analysis related to the PD signals. For the purpose, the HFPD detection and PA (Pulse Analysis) system have been developed and then the effect of noise discrimination has been investigated by use of the artificial defects using real scale mockup. Throughout these works, our system is proved to be capable of separating the small void discharges among the very large noises such as big air corona and ground floating discharges at the on-site as well as of identifying the concerned defects.

• 무역상무연구
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• 제49권
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• pp.283-324
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• 2011

The purpose of this paper is to research the air waybill and the carrier's liability in respect of the carriage of cargo by air under the Montreal Convention of 1999. The Warsaw Convention for the unification of certain rules for international carriage by air was adopted in 1929 and modified successively in 1955, 1961, 1971, 1975 and 1999. The Montreal Convention of 1999 modernized and consolidated the Warsaw Convention and related instruments. Under the Montreal Convention, in respect of the carriage of cargo, the air waybill shall be made out by the consignor. If, at the request of the consignor, the carrier makes it out, the carrier shall be deemed to have done so on behalf of the consignor. The air waybill shall be made out in three orignal parts. Under the Montreal Convention, the consignor shall indemnify the carrier against all damages suffered by the carrier or any other person to whom the carrier is liable, by reason of the irregularity, incorrectness or incompleteness of the particulars and statement furnished by the consignor or on its behalf. The air waybill is not a document of title or negotiable instrument. Under the Montreal Convention, the air waybill is prima facie evidence of the conclusion of the contract, of the acceptance of the cargo and of the conditions of carriage. If the carrier carries out the instructions of the consignor for the disposition of the cargo without requiring the production of the part of the air waybill, the carrier will be liable, for any damage which may be accused thereby to any person who is lawfully in possession of the part of the air waybill. Under the Montreal Convention, the carrier is liable by application of principle of strict liability for the damage sustained during the carriage of cargo by air. The carrier is liable for the destruction or loss of, or damage to cargo and delay during the carriage by air. The period of the carriage by air does not extend to any carriage by land, by sea or by inland waterway performed outside an airport. Under the Montreal Convention, the carrier's liability is limited to a sum of 17 Special Drawing Rights per kilogramme. Any provision tending to relieve the carrier of liability or to fix a lower limit than that which is laid down in this Convention shall be and void. Under the Montreal Convention, if the carrier proves that the damage was caused by the negligence or other wrongful act or omission of the person claiming compensation, or the person from whom he derives his rights, the carrier shall be wholly or partly exonerated from ist liability to the claimant to the extent that such negligence or wrongful act or omission caused the damage. Under the Montreal Convention, any action for damages, however founded, whether under this Convention or in contract or in tort or otherwise, can only be brought subject to the conditions and such limits of liability as are set out in this Convention. Under the Montreal Convention, in the case of damage the person entitled to delivery must complain to the carrier forthwith after the discovery of the damage, and at the latest, within fourteen days from the date of receipt of cargo. In the case of delay, the complaint must be made at the latest within twenty-one days from the date on which the cargo has been placed at his disposal. if no complaint is made within the times aforesaid, no action shall lie against the carrier, save in the case of fraud on its part. Under the Montreal Convention, the right to damage shall be extinguished if an action is not brought within a period of two years, reckoned from the date of arrival at the destination, or from the date on which the aircraft ought to have arrived, or from the date on which the carriage stopped. In conclusion, the Montreal Convention has main outstanding issues with respect to the carrier's liability in respect of the carriage of cargo by air as follows : The amounts of limits of the carrier's liability, the duration of the carrier's liability, and the aviation liability insurance. Therefore, the conditions and limits of the carrier's liability under the Montreal Convention should be readjusted and regulated in detail.

• 한국안전학회지
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• 제19권4호
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• pp.141-149
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• 2004

가솔린 엔진을 장착한 자동차는 고전압발생장치인 점화코일을 이용하여 고전압을 발생 연소실 내의 혼합기를 점화 및 연소시킴으로써 동력을 얻고 엔진을 구동하게 된다. 점화코일은 1차측 낮은 전압을 스위칭 작용으로 2차측 높은 전압을 발생시키고, 이를 전극으로 보내는데, 점화코일에 작은 결함이 발생하게 되면 제 성능을 발휘하지 못한다. 본 연구에서는 현재 사용하고 있는 에폭시 성형 점화코일과 절연재료인 에폭시수지를 시료로 선택하여 시료에 전압이 인가될 때 발생하는 부분방전 특성을 측정하여 전압변화에 따른 위상각, 방전전하량 및 발생빈도 수 등의 분포를 연구하고 검토한 결과를 실제 자동차점화장치에 접목시켜 점화코일의 성능향상과 전기장치의 신뢰성 확보에 기여하고자 한다.

• Nuclear Engineering and Technology
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• 제51권6호
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• pp.1487-1503
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• 2019

The methods and performance of a pin-level nuclear reactor core thermal-hydraulics (T/H) code ESCOT employing the drift-flux model are presented. This code aims at providing an accurate yet fast core thermal-hydraulics solution capability to high-fidelity multiphysics core analysis systems targeting massively parallel computing platforms. The four equation drift-flux model is adopted for two-phase calculations, and numerical solutions are obtained by applying the Finite Volume Method (FVM) and the Semi-Implicit Method for Pressure-Linked Equation (SIMPLE)-like algorithm in a staggered grid system. Constitutive models involving turbulent mixing, pressure drop, and vapor generation are employed to simulate key phenomena in subchannel-scale analyses. ESCOT is parallelized by a domain decomposition scheme that involves both radial and axial decomposition to enable highly parallelized execution. The ESCOT solutions are validated through the applications to various experiments which include CNEN $4{\times}4$, Weiss et al. two assemblies, PNNL $2{\times}6$, RPI $2{\times}2$ air-water, and PSBT covering single/two-phase and unheated/heated conditions. The parameters of interest for validation include various flow characteristics such as turbulent mixing, spacer grid pressure drop, cross-flow, reverse flow, buoyancy effect, void drift, and bubble generation. For all the validation tests, ESCOT shows good agreements with measured data in the extent comparable to those of other subchannel-scale codes: COBRA-TF, MATRA and/or CUPID. The execution performance is examined with a mini-sized whole core consisting of 89 fuel assemblies and for an OPR1000 core. It turns out that it is about 1.5 times faster than a subchannel code based on the two-fluid three field model and the axial domain decomposition scheme works as well as the radial one yielding a steady-state solution for the OPR1000 core within 30 s with 104 processors.

• 한국항행학회논문지
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• 제24권6호
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• pp.465-470
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• 2020

복합 소재는 금속보다 가벼운 특성을 가져 경량화가 필수인 항공 산업에 널리 사용되고 있다. 하지만 복합소재는 생산 공정 중 내부 보이드 형성, 접착제 혼합 불량, 미접착 부분 발생 등 결함 요소가 발생할 수 있고, 저 에너지 충격에 의한 미세균열 및 층간분리가 발생할 위험이 있다. 그러므로 구조물 손상검사가 필수적으로 요구된다. 이에 FBG를 이용한 구조 건전성 모니터링이 주목받고 있다. FBG는 기존의 전기적 센서에 비해 전기적 노이즈 영향을 받지 않고 부식에 강하며 멀티플렉싱이 가능하다는 장점이 있다. 하지만 FBG를 계측하는 인터로게이터는 대형 구조물 계측을 전제로 만들었기 때문에 가격이 고가이며, 크기가 큰 단점이 있다. 이에 본 논문에서는 광 스위치와 WDM필터, LTF를 이용해 무인항공기나 소형항공기에 사용할 수 있도록 저가형 인터로게이터를 설계하여, 기존의 고가 인터로게이터와 비교를 진행하였다.

• 한국지반공학회논문집
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• 제31권8호
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• pp.17-28
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• 2015

흙-함수특성곡선에 대한 선행 연구결과들의 경우, 정량적으로 간극수 유출입량을 측정하여 모관흡수력에 따른 체적함수비를 산정하였다. 본 연구에서는, 압력판 추출시험기(VPPE)에 Time Domain Reflectimoetry(TDR) 측정 시스템을 도입하여 불포화토의 건조과정 및 습윤과정 진행에 따른 유전상수를 측정하여 체적함수비를 산정하고자 하였다. 압력판 추출 시험기는 압력셀, 압력조절장치, 뷰렛 시스템, TDR 프로브로 구성된다. 압력셀에 초기 간극비가 다른 두 시료를 조성한 후, 압력조절장치를 이용하여 압력셀 내부에 0.1kPa - 50kPa 범위의 공기압을 가하여 모관흡수력을 조절하였다. 그리고 뷰렛시스템을 이용하여 모관흡수력 변화에 따른 시료의 체적함수비 변화를 측정하였다. 또한, 압력셀 내부에 설치된 TDR 프로브를 이용하여 프로브 양단에서 발생되는 전자기파의 반사 신호로부터 유전상수를 산정하였다. 주문진 표준사의 체적함수비 변화에 따른 유전상수 측정에 대한 보정으로 도출한 체적함수비와 유전상수관계를 이용하여 시료의 체적함수비를 산정하였다. 실험 결과, 시료의 초기 간극비와 상관없이 TDR 프로브에 의해 산정된 체적함수비는 뷰렛 시스템을 통해 정량적으로 산정된 체적함수비와 매우 유사한 것으로 나타났다. 또한, 건조과정 및 습윤과정 진행에 따라 동일한 모관흡수력에 대한 함수비의 차이가 존재하는 이력현상(Hysteresis)이 발생하였고, 건조과정 및 습윤과정의 반복에 따라 이력현상은 줄어들었다. 본 연구에서 적용된 전자기파의 시간영역반사법(TDR)을 통해 불포화토의 흙-함수특성곡선을 효과적으로 파악할 수 있을 것으로 판단된다.

• 항공우주정책ㆍ법학회지
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• 제33권1호
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• pp.261-284
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• 2018

현재의 국제법제도는 우주의 군사화와 무기화에 대한 안전장치를 제공하지 못한다. 1967년 우주조약 제4조에 명시된 "우주의 평화적 이용"이라는 용어는 정부의 공식 성명서나 다자간 우주관련조약에 표현되어 있지만, 국가 관행을 검토하면 이 용어는 여전히 권위 있는 정의를 내리지 못하고 있다. 이러한 우주조약 제4조의 무기에 대한 모호한 금지는 국가들로 하여금 우주와 천체에 핵무기나 대량파괴무기 이외에 다른 기타 무기의 배치를 허용하고 있다. 1967년 우주조약에 명시된 '우주의 평화적 이용'의 문구는 1979년 달협정에서도 발견되므로 이를 함께 분석해야 한다. 또한 특정 무기통제조치가 포함되어 있지는 않지만 1975년 등록협약도 참고해야 하는데, 등록협약은 적절하게 적용되면 신뢰구축의 역할을 상당히 수행할 수 있다. 그 이유는 동 협약 제4조가 우주물체의 일반적인 기능을 포함한 우주발사물체에 관한 정보를 유엔사무총장에게 제공할 것을 요구하고 있기 때문이다. 한편 2008년 유엔총회의 특별회기 때 군비축소팀에 중국과 러시아가 공동으로 제출하고 나중에 2014년에 개정된 "우주에서의 무기배치와 우주물체에 대한 무력의 위협이나 사용금지조약안(PPWT)"은 우주에서 사용되는 무기에 대한 정의를 제공하고 우주무기확산을 금지하려는 시도를 하고 있지만, 미국이 반대하고 있다. 그 이유는 우주 공간에는 현재 무기경쟁이 없다는 이유에서인데, 실제로 우주에서 천체는 아니고 우주공간(outer void space)은 이미 "군사화"되어 군사적 수단으로 사용되고 있으나 아직 "무기화"는 되지 못하고 있다. 즉, 인공위성이 다른 위성을 파괴하거나 우주에서 발사되어 지구표면을 공격할 수 있는 우주무기는 아직 없고, 지구표면에서 발사된 인공위성을 파괴할 수 있는 능력만 계속 시도되고 입증되고 있을 뿐이다. 우주의 군사적 이용을 규제하기 위해 모든 면에서 통합적이고 구속력 있는 법적 도구의 궁극적인 창조를 목적으로 한 구속력을 가진 법이 채택되어야 한다는 경성법(hard law) 접근법을 지지하는 사람들도 있지만, 현재 그것이 불가능하다면 임시조치로 연성법(soft)인 가이드라인이 개발되어야 할 것이다. 이는 적용시킬 법이 없어서 재판불능(non liquiet) 상태에 이르는 사태에 대비하기 위하여 매우 유용하게 이용될 수 있다. 사실 연성법은 조약의 포고에 관하여 지지를 표출하며 국제관습법을 창출하는 데 사용되기도 한다. 1963년 "우주의 탐사와 사용에 있어서 국가의 활동을 규제하는 법원칙 선언"과 1992년 " 원료사용원칙"을 그 예로 들 수 있는데, 전자의 상당 부분은 이후에 제정된 1967년 우주조약에 성문화되었고, 후자는 비록 의무적인 용어로 쓰여졌지만 경성법 못지않게 지속적으로 국가에 의해 준수될 국제관습법의 일부가 되어 가고 있다. 한편 이와 관련하여 1974년 11월 12일 유엔총회에서 채택된 결의에서 '선언'(declaration)과 '결의'(resolution)는 국제법의 발전에 반영될 수 있는 방법으로서 국제사법재판소(ICJ)에 의해서 고려되어야 한다고 권고한 점에 주목해야 할 것이다.