• 한국항공우주학회지
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• 제37권11호
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• pp.1096-1103
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• 2009

연소기 헤드부는 극저온 유체인 액체산소가 고압으로 작동하고, 동시에 연소기의 추력으로 인한 하중을 받기 때문에, 극저온에서의 헤드의 구조 안정성 해석을 위한 재료의 변형 거동 예측은 매우 중요하다. 헤드부의 변형 거동을 예측하기 위해 재료의 저온에서의 인장 변형 거동을 묘사할 수 있는 구성 방정식을 Kocks의 전위 에너지 장벽 모델을 바탕으로 열적 요소와 비열적 요소의 결합으로 구성하였으며, 극저온에서 장애물들의 증가로 인한 응력의 열적 요소의 증가를 묘사하기 위해서, 장애물로 인해 발생하는 응력 요소를 Ramberg-Osgood 형태의 식으로 구성하였다. 본 모델은 극저온과 상온의 넓은 온도 영역에서 재료의 변형 거동을 잘 예측하였다.

• 한국진공학회지
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• 제17권4호
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• pp.270-277
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• 2008

진공이란 공간의 기체압력이 대기압보다 낮은 상태, 즉 분자밀도가 약 $2.5{\times}10^{19}$분자/$cm^3$ 보다 적은 상태를 의미하며, 극청정환경 제공, 단열효과, 입자의 장거리 비행가능, 증발과 승화작용, 안정된 플라즈마를 유지, 생화학 반응 억제, 우주환경 제공 등의 특성으로 인해 오늘날 전 산업분야 및 과학기술 분야에 응용이 되고 있다. 우주환경은 이러한 고진공 환경과 태양 복사열에 의한 고온 환경 및 극저온이 반복되는 가혹한 환경으로 특징지어지는데, 위성체는 지상에서 발사되어 우주궤도에 진입한 순간부터는 계속해서 우주환경에 노출된다. 위성체가 이러한 가혹한 우주환경에 노출될 경우 주요부품에 기능장애가 초래되기도 하며 이는 결국 임무의 실패로 이어지기도 한다. 따라서 위성체는 지상에서 우주환경시험을 거쳐 기능 및 작동상태를 점검해야 하며, 이를 위해서는 우주환경을 모사 할 수 있는 우주환경 모사장비가 필요하다. 우주환경모사장비라 함은 우주환경의 주특징인 고진공상태와 극저온 환경을 모사할 수 있는 지상장비를 말하며, 장비의 설계 및 제작에는 기본적으로 진공기술이 응용되게 된다. 본 논문에서는 한국항공우주연구원이 보유하고 있는 인공위성의 개발에 필수 장비인 우주환경모사장치들을 소개하고, 최근 발달된 국내 진공기술로 국산화 제작에 성공한 유효제원 ${\varphi}8m{\times}L10\;m$ 급의 대형열진공챔버를 통하여 우주개발에 응용되는 진공기술을 소개하고자 한다.

• 한국수소및신에너지학회논문집
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• 제24권1호
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• pp.44-49
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• 2013

Hydrogen penetration into a metal leads to damages and mechanical degradations and its content measurement is of importance. For a precise measurement, a sample preparation procedure must be optimized through a series of studies on sample washing and drying. In this study, two-step washing with organic solvents and thermal soaking in inert gas were tried with a rod-shaped, API X65 steel sample. The samples were machined from a steel plate and then washed in acetone and etyl-alcohol for 5 minute each and dried with compressed air. After then, the samples were thermally soaked in a home-made nitrogen gas chamber during 10 minute at different heat gun temperatures from 100 to $400^{\circ}C$ and corresponding temperature range in the soaking chamber was from 77 to $266^{\circ}C$ according to the temperature calibration. Hydrogen residue in the samples was measured with a hot extraction system after each soaking step; hydrogen residue of $0.70{\pm}0.12$ wppm after the thermal soaking at $77^{\circ}C$ decayed with increase of the soaking temperature. By adopting the heat transfer model, decay behavior of the hydrogen residue was fitted into an exponential decay function of the soaking temperature. Saturated value or lower bound of the hydrogen residue was 0.36 wppm and chamber temperature required to lower the hydrogen residue about 95% of the lower bound was $360^{\circ}C$. Furthermore, a thermal desorption spectroscopy was done for the fully soaked samples at $360^{\circ}C$. Weak hydrogen peak was observed for whole temperature range and it means that hydrogen-related contaminants of the sample surface are steadily removed by heating. In addition, a broad peak found around $400^{\circ}C$ means that parts of the hydrogen residue are irreversibly trapped in the steel microstructure.

• 한국진공학회지
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• 제6권4호
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• pp.298-307
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• 1997

CRT부품 탈가스(outgassing)를 온도를 변화 시켜가며 측정할 수 있고 시료의 열탈착 특성을 측정할 수 있는 TDS(Thermal Desorption Spectroscopy) 측정 장치를 설계 제작하였다. 제작된 시스템은 유효 배기속도를 조절할 수 있는 진공 장치와 시료의 온도조절 장치, 탈가스 측정 가치로 구성되어 있다. 제작된 시스템의 최저 도달 진공도는 $1{\times}10^{-7}$Pa 이하였고 가변 콘덕탄스(conductance)를 채택하여 유효 배기 속도를 조절 할 수 있도록 제작되었다. 가변 콘덕탄스 조절에 따른 시료위치에서의 유효 배기 속도 변화를 측정하였다. 텅스텐 히터와 온도조절기를 이용하여 시료의 온도는 600℃까지 ±1℃ 이내 오차로 조절 할 수 있었으며 온도 상승률도 조절할 수 있었다. 측정계기로 사용한 이온 진공계(ion gauge)와 사중극 질량분석기(quadrupole mass spectrometer)의 감도를 측정하여 정량적인 측정을 할 수 있도록 하였다. 제작된 시스템을 이용하여 CRT 공정에서의 부품별 온도별 측정 예와 공정분석에의 적용 예를 보였다.

• Journal of Advanced Marine Engineering and Technology
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• 제27권5호
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• pp.624-632
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• 2003

In the gasoline engine industry. there has been a trend towards the development of high performance engines with improved fuel efficiency, reduced weight and smaller sizes. These trends help to solved engine problems related to thermal load and abnormal combustion. In order to investigate these Problems, a thin film-type probe for instantaneously measuring temperatures has been suggested. A method for manufacturing such a probe was established in this study. The instantaneous surface temperature of a constant volume combustion chamber was measured by this probe and the heat flux was obtained through Fourier analysis. A peak instantaneous temperature was obtained after 55∼60 ms from ignition and the temperature increased according to an equivalence ratio and varied differently according to the position of the probe. Total heat loss during combustion period was affected by the equivalence ratio and differed widely in accordance to the position of the probe.

• 대한기계학회논문집
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• 제3권1호
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• pp.1-9
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• 1979

Methanol was examined as supplemental fuel for open chamber type and pre-combustion chamber type diesel engine. Pre-determined quantities of diesel oil were injected as ordinary diesel engines and methanol was added at inlet pipe using venturi, nozzel and and float chamber for the rest of the charge. In this mode of operation, addition of methanol reduced inlet and exhaust temperature. Inlet air quantities were essentially unchanged in spite of lower inlet temperature. Exhaust smoke was significantly reduced At light load when both diesel oil and methanol were introduced with small quantities, specific heat consumption was considerably increased. However, with the increase of the quantity of methanol or diesel oil, specific heat consumption was improved. With sufficient quantities of diesel oil enough to produce the power above 3/4 load, addition of methanol showed better thermal economy.

• 대한기계학회논문집
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• 제17권1호
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• pp.153-161
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• 1993

본 연구에서는 각 운전모드별 열특성을 전체적으로 고려하여 양질의 MHD발전 용 작동플라즈마를 얻기 위하여 필요한 효과적인 방책에 관하여 집중적으로 고찰하고 자 한다.

• 한국자동차공학회논문집
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• 제9권4호
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• pp.103-111
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• 2001

In the present study, the internal combustion engine tends to high performance, fuel economy, small-sized. Therefore, it is necessary to solve the problems on thermal load, abnormal combustion, etc in the engine. Thin film instantaneous temperature probe was made, and the measuring system was established. The instantaneous surface temperatures in the constant volume combustion chamber were measured with this system and the heat flux was obtained by Fourier analysis. Maximum instantaneous temperatures were obtained after 55∼60ms from ignition and they increased as equivalence ratio and varied differently as the position of probe. Total heat loss during combustion time was affected by the equivalence ratio and differed widely as the position of probe.

• 항공우주시스템공학회지
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• 제2권2호
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• pp.28-34
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• 2008

This paper describes the performance characteristics of flow and structure in the post-chamber and nozzle. Using the computational fluid dynamics (CFD) technique, the stress and compressible flow fields in the downstream of the post chamber and nozzle were numerically calculated. Besides, the stress characteristics at the wall of post-chamber and nozzle were investigated under different thickness (2mm, 5mm and 10mm) of the nozzle wall. The stress pattern demonstrates that the strength of nozzle wall having 10mm is safer than that of 5mm or 2mm according to von Mises stress irrespective to the pressure field

• 한국철도학회:학술대회논문집
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• 한국철도학회 2005년도 추계학술대회 논문집
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• pp.941-946
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• 2005

Kinds of Sound & Thermal Insulator are being used for materials of railroad vehicles as a barrier of beat and noise. Glass Wool, PE foam, PP foam are such kinds of materials. In case of fire, it shows various combustion properties. In this study, we compared the Smoke Density of the Rubber Foam Insulator by test between Cone-Calorimeter and Smoke Density-Chamber. The results showed that the Rubber Foam Insulator had an important role in the insulator thickness and the test method, We forecast the smoke density by test between Cone-Calorimeter and Smoke Density-Chamber.