• 한국유체기계학회 논문집
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• 제10권6호
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• pp.32-37
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• 2007

Aerodynamic forces and moments have been used to control rocket propelled vehicles. If control is required at very low speed, Those systems only provide a limited capability because aerodynamic control force is proportional to the air density and low dynamic pressure. But thrust vector control(TVC) can overcome the disadvantages. TVC is the method which generates the side force and roll moment by controlling exhausted gas directly in a rocket nozzle. TVC is classified by mechanical and fluid dynamic methods. Mechanical methods can change the flow direction by several objects installed in a rocket nozzle exhaust such as tapered ramp tabs and jet vane. Fluid dynamic methods control the flight direction with the injection of secondary gaseous flows into the rocket nozzle. The tapered ramp tabs of mechanical methods are used in this paper. They installed at the rear in the rocket nozzle could be freely moved along axial and radial direction on the mounting ring to provide the mass flow rate which is injected from the rocket nozzle. In this paper, the conceptual design and the study on the tapered ramp tabs of the thurst vector control has been carried out using the supersonic cold flow system and schlieren system. This paper provides the thrust spoilage, three directional forces and moments and distribution of surface pressure on the region enclosed by the tapered ramp tabs.

• 한국유체기계학회 논문집
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• 제18권5호
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• pp.49-53
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• 2015

Thrust vector control is the method which generates the side force and roll moment by controlling exhausted gas directly in a rocket nozzle. TVC is classified by mechanical and fluid dynamic methods. Mechanical methods can change the flow direction by several objects installed in a rocket nozzle exhaust such as tapered ramp tabs and jet vane. Fluid dynamic methods control the flight direction with the injection of secondary gaseous flows into the rocket nozzle. The tapered ramp tabs of mechanical methods are used in this paper. They installed at the rear in the rocket nozzle could be freely moved along axial and radial direction on the mounting ring to provide the mass flow rate which is injected from the rocket nozzle. TVC of the tapered ramp tabs has the potential to produce both large axial thrust and high lateral force. We have conducted the experimental research and flow analysis of ramp tabs to show the performance and the structural integrity of the TVC. The experiments are carried out with the supersonic cold flow system and the schlieren graph. This paper provides to analyze the location of normal shock wave and distribution of surface pressure on the region enclosed by the tapered ramp tabs.

• 한국표면공학회:학술대회논문집
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• 한국표면공학회 2008년도 추계학술대회 초록집
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• pp.15-16
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• 2008

In case manufacturing COF, through hole should be made to be used for a pathway connecting the conductive layers of its both faces. In case Cu-plating inside of through hole with electroless plating way, contact between Cu and PI film gets bad to be fell apart from PI by the impact of applying to the electric devices. Therefore, after sputtering is applying on inner through hole, then a method to perform electroplating process. In this study, after changing sputtering condition to manufacture FCCL, we looked the changeability of the upper PI and inner hole Cu layers. Making use of RF Magnetron sputtering equipment, we coated Cu thin film and Cu-plated on it through electroplating. After cold-mounting the completed FCCL, we examined hole section through an optical microscope. From the result of test, with parameters deposition pressure and deposition time, both the thickness of the hole plated layer and PI plated upper layer increased at regular rate, increasing the thickness of Cu sputter layer. However, from the result of test in increasing RF-power, we could know the increment rate of hole plated layer is considerably greater than that of PI plated upper layer. Therefore, we finally acquired good result; if you want only to increase the plated layer of inner hole, it's much better to increase RF-power.

• 한국산학기술학회논문지
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• 제21권6호
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• pp.432-439
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• 2020

제동력 향상을 위해 인 보드 브레이크 시스템이 적용된 한국형 전술차량 일부 운용 부대에서 제동 시 차체 떨림 현상인 브레이크 저더가 확인되었다. 차량 제동 시 발생되는 심한 진동은 주행 안정성을 저하시키며 나아가 사고로 이어질 수 있다. 이를 방지하기 위해 본 연구에서는 브레이크 저더가 확인된 차량을 대상으로 고장 분석을 통해 근본원인을 분석하고, 나아가 진동 전달 메커니즘 분석을 통해 진동의 주요 전달 경로를 파악함으로써 개선 가능 인자를 도출하였다. 분석 결과 전술차량에서 확인된 제동 시 차체 떨림은 냉간 저더 현상으로 브레이크 디스크의 과도한 흔들림 조건에서 녹 및 이물유입에 따라 디스크 두께 변동이 증가하여 발생됨을 확인하였다. 또한 이러한 진동은 전달계에 대한 구조 개선을 통해 저감할 수 있음을 확인하였다. 이에 본 연구에서는 각각의 인자들에 대해 개선 방안을 제시하고, 비교시험을 통해 검증함으로써 그 효과성을 확인하였다. 끝으로 본 연구를 통해 도출된 개선안은 차기 군용차량 개발 시 활용할 수 있을 것으로 기대된다.

• 구강회복응용과학지
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• 제31권2호
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• pp.75-85
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• 2015

목적: 이번 연구의 목적은 FRC-포스트와 코어가 색상차이에 따라 구별되는 정도를 비교하는 것이다. 연구 재료 및 방법: 실험을 위해 유사한 크기(${\pm}0.5 mm$)와 길이(${\pm}0.5 mm$)의 발치 한 하악 소구치 9개를 근관 형성하고 충전하였다. 3개의 치근을 체온을 재현하기 위해 $37^{\circ}C$ 물이 흐르는 가는 실리콘 튜브로 감은 후 cold mounting resin에 매몰하여 각 3개의 치근이 매몰된 총 3개의 시편을 제작하였다. 개개의 시편 치근에는 3종류의 $Snowpost^{(R)}$, MACRO-$LOCK^{TM}$ POST $ILLUSION^{TM}$ $XRO^{(R)}$, FRC $Postec^{(R)}$ Plus post를 이용하여 각각의 포스트에 맞게 공간을 형성하고 포스트를 접착하였다. 3개의 시편 별로 $Luxacore^{(R)}$ Dual Blue, $Luxacore^{(R)}$ Dual A3 및 $Filtek^{TM}$ Z350 XT A1E로 코어를 축조, 시편 별로 다른 코어를 사용하였다. 각 시편에 대해 온도를 낮추기 위한 압축공기를 불 때와 안 불 때로 나누어 디지털 이미지를 촬영하였다. 치과의사 50명과 치과대학 대학생 50명 총 100명에게 어떤 포스트가 코어와 가장 구별이 잘되는 지를 설문조사 하였다. 결과: $Luxacore^{(R)}$ Dual Blue에서는 $Snowpost^{(R)}$가, $Luxacore^{(R)}$ Dual A3에서는 $Snowpost^{(R)}$가, $Filtek^{TM}$ Z350 A1E에서는 MACRO-$LOCK^{TM}$ POST $ILLUSION^{TM}$ $XRO^{(R)}$가 구별이 가장 잘되었다. 압축공기를 불어 온도를 내리면 나타나는 MACRO-$LOCK^{TM}$ $ILLUSION^{TM}$ $XRO^{(R)}$의 색은 포스트와 코어의 구별을 더 용이하게 하였다. 결론: FRC-포스트와 복합레진 코어가 구별되는 정도는 색상차이에 따라 다름을 알 수 있었다.

• 동의생리병리학회지
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• 제22권5호
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• pp.1001-1034
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• 2008

This thesis is a study composed of eight chapters from 9. to 16. of the Maek Kyoung(脈經) Vol. VIII. ; the symptom & the pulse of Jaundice(黃疸), Malarial Disease(?疾). Carbuncle(癰腫) Intestines Carbuncle(腸癰), & c. It is as follows : Chapter 9 refers to the symptom, pulse, treatment and prognosis of Jaundice(黃疸) and Malarial Disease(?疾). Chapter 10 refers to the cause, symptom, pulse and treatment of Cardialgia(胸痺), Cardiagra(心痛) and Nephric Accumulation(賁豚). Chapter 11 refers to the symptom, pulse and treatment of Abdominal Fuliness(腹滿), Cold Mounting(寒疝) and Abiding Food(宿食). Chapter 12 refers to the symptom and pulse of Accumulation and Mass of the Five Viscera(五臟積聚). Chapter 13 refers to the cause, pathogenesis, symptom, pulse, treatment and prognosis of Terror and Palpitation due to Fright(驚悸), Hematemesis(吐血), Nasal Hemorrhage(?血), Metrorrhagia(下血) and Extravasated Blood(瘀血). Chapter 14 refers to the cause, pathogenesis, symptom, pulse and treatment of Vomiting(嘔吐), Hiccough(?) and Diarrhea(下利). Chapter 15 refers to the cause, pathogenesis, symptom, pulse and treatment of Atrophy of Lung(肺?), Pulmonary Abscess(肺癰), Lung-distention(咳逆上氣) and Phlegm(痰飮). Chapter 16 refers to the cause, pathogenesis, symptom, pulse. treatment and prognosis of Carbuncle(癰腫), Intestines Carbuncle(腸癰), Wound(金瘡) and Acute Eczema(侵淫瘡). There have been abundant investigations in China. But we couldn't find a clear result yet, and they were written in archaic texts and colloquial Chinese, therefore it is needed to be translated into Korean. And there was only one inaccurate translation with insufficient annotation. So I hope this study will be useful to develope Oriental Medical Diagnostics.

• 천문학논총
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• 제24권1호
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• pp.53-64
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• 2009

MIRIS is the main payload of the STSAT-3 (Science and Technology Satellite 3) and the first infrared space telescope for astronomical observation in Korea. MIRIS space observation camera (SOC) covers the observation wavelength from $0.9{\mu}m$ to $2.0{\mu}m$ with a wide field of view $3.67^{\circ}\times3.67^{\circ}$. The PICNIC HgCdTe detector in a cold box is cooled down below 100K by a micro Stirling cooler of which cooling capacity is 220mW at 77K. MIRIS SOC adopts passive cooling technique to chill the telescope below 200 K by pointing to the deep space (3K). The cooling mechanism employs a radiator, a Winston cone baffle, a thermal shield, MLI (Multi Layer Insulation) of 30 layers, and GFRP (Glass Fiber Reinforced Plastic) pipe support in the system. Optomechanical analysis was made in order to estimate and compensate possible stresses from the thermal contraction of mounting parts at cryogenic temperatures. Finite Element Analysis (FEA) of mechanical structure was also conducted to ensure safety and stability in launching environments and in orbit. MIRIS SOC will mainly perform Galactic plane survey with narrow band filters (Pa $\alpha$ and Pa $\alpha$ continuum) and CIB (Cosmic Infrared Background) observation with wide band filters (I and H) driven by a cryogenic stepping motor.