• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2009년 춘계학술대회논문집
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• pp.142-147
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• 2009

COMS (Communication, Ocean and Meteorological Satellite) is a geostationary satellite and has been developing by KARI for communication, ocean and meteorological observations. It will be tested under vacuum condition and very low temperature in order to verify thermal design of COMS. The test will be performed by using KARI large thermal vacuum chamber, which was developed by KARI, and the COMS will be the first flight satellite tested in this chamber. The purposes of thermal balance test are to correlate analytical model used for design evaluation and predicting temperatures, and to verify and adjust thermal control concept. KARI has plan to use heating plates to simulate space hot condition especially for radiator panels such as north and south panels. They will be controlled from 90K to 273K by circulating GN2 and LN2 alternatively according to the test phases, while the shroud of the vacuum chamber will be under constant temperature, 90K, during all thermal balance test. This paper presents thermal modelling including test chamber, heating plates and the satellite without solar array wing and Ka-band reflectors and discusses temperature prediction during thermal balance test.

• 한국공간구조학회논문집
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• 제14권3호
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• pp.93-100
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• 2014

Ethylene Tetrafluoroethylene (ETFE) has been widely used in long-span buildings because of its light weight and high transparency. This paper studies the short and long term creep behaviour of ETFE foil. A series of short-term creep and recovery tests were performed, in which the residual strain was observed. A long-term creep test of the ETFE foil was also performed over 110 days. A viscoelastic-plastic model was then established to describe the short-term creep and recovery behaviour. The model contains a traditional multi-Kelvin part and an added steady-flow component to represent the viscoelastic and viscoplastic behaviour, respectively. The model successfully fit the data for three stresses and six temperatures. Additionally, time-temperature equivalency was adopted to predict the long-term creep behaviour of ETFE foil. Horizontal shifting factors were determined from the process of shifting creep-curves at six temperatures. The long-term creep behaviours at three temperatures were predicted. Finally, the long-term creep test showed that the short-term creep test at identical temperatures insufficiently predicted additional creep behaviour, and the long-term test verified the horizontal shifting factors derived from the time-temperature equivalency.

• 한국산학기술학회논문지
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• 제21권7호
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• pp.350-356
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• 2020

목적: 본 연구는 수술 후 회복실에 입실한 환자에게 가온요법 간호중재 프로그램이 미치는 효과를 파악하여 간호중재방안 개발 및 기초자료를 제시하고자 시도된 비 동등성 대조군 유사 실험연구이다. 연구방법: 연구의 대상자는 가온요법 프로그램을 적용한 실험군 31명, 대조군 31명을 대상으로 실시하였다. 가온요법은 가온기를 통해 회복실에서 38~43℃ 범위 내 가온하였다. 대상자의 일반적 특성은 실수와 백분율로 파악하였고, 실험군과 대조군의 동질성 검정은 𝑥²-test와 In-dependent t-test로 파악하였다. 실험군과 대조군의 시간에 따른 체온, 통증, 전율의 차이는 repeated measure ANOVA로 파악하였다. 실험군과 대조군의 온도 편안감의 차이는 t-test로 파악하였다. 결과: 첫째, 수술 직후 반복 측정 결과 실험군과 대조군의 체온, 통증, 전율이 유의한 차이를 보였다. 둘째, 온도 편안감은 유의한 차이를 보였다. 결론: 이와 같이 수술 후 가온요법 중재 시 환자에게 긍정적인 효과가 있는 것을 확인할 수 있었다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2003년도 춘계학술대회
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• pp.7-12
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• 2003

When the wind turbine is used in cold regions, the mechanical properties and dimension stability of the blade will be changed. The proposal of this paper is to test the durability of the blade for wind turbine. It is necessary to select the most comfortable materials and fabrication processes for more stable wind turbine blade in cold regions. To select the most comfortable materials and processes, the static strength has to know through the tensile static tests at the severe condition as cold regions. First, the tensile static specimens made by RIM (Resin injection molding) process & vacuum bagging process with reinforcement materials and resin. Tensile static tests were carried out on three laminate lay-ups (carbon prepreg, carbon fiber dry fabric and glass fiber dry fabric) at different test temperature($24^{\circ}$, $-30^{\circ}$), determining properties such as the mechanical strength, stiffness and strain to failure. At different test temperature, in order to test the tensile strengths of these specimens used the low temperature chamber. Next, the results of this test were compared with each other. Finally, the most comfortable materials and fabrication processes can select based on these results. The results show the changes in the static behavior of three laminate lay-ups at different test temperatures. At low temperatures, the static strengths are higher than the ones at room temperature.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2003년도 춘계학술발표대회 논문집
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• pp.196-201
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• 2003

When the structures are used in cold regions, the mechanical properties and dimension stability of the blade will be changed. The proposal of this study is to test the durability of the structures in cold regions. It is necessary to select the most comfortable materials and fabrication processes for more stable structures in cold regions. To select the most comfortable materials and processes, the static strength has to know through the tensile static tests at the severe condition as cold regions. First, the tensile static specimens made by RIM (Resin injection molding) process & vacuum bagging process with reinforcement materials and resin. Tensile static tests were carried out on three laminate lay-ups (carbon prepreg, carbon fiber dry fabric) at different test temperature($24^{\circ}C$, $-30^{\circ}C$), determining properties such as the mechanical strength, stiffness and strain to failure. At different test temperature, in order to test the tensile strengths of these specimens used the low temperature chamber. Next, the results of this test were compared with each other. Finally, the most comfortable materials and fabrication processes can select based on these results. The results show the changes in the static behavior of three laminate lay-ups at different test temperatures. At low temperatures, the static strengths are higher than the ones at room temperature.

• 전기전자학회논문지
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• 제17권1호
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• pp.63-70
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• 2013

본 연구에서는 차량용 연료히터의 전기적 성능검사 챔버를 구현한다. 겨울철 저온환경의 영향을 받는 디젤 엔진이 냉각될 경우 일정한 온도 이하로 내려가면 파라핀과 같은 반고체 상태인 왁싱(Waxing)물질을 형성하여 엔진 시동이 잘 걸리지 않게 하는 원인이 된다. 히터내에 센서를 안착시켜 통합한 일체형 통합히터는 시동성 평가에 중요한 요소이며, 성능평가 시험 챔버 시스템을 통해 전기적인 특성을 시험한다. 최근 CRDI(커먼레일) 엔진을 주로 사용함에 따라 연료히터로 디젤오일을 가열하여 점화성능을 향상시키기 위한 연료히터 성능시험은 엔진의 시동성을 향상시키는 중요한 요소이다. 따라서 연료히터의 전기적 성능시험 검사항목은 상온, 극저온, 극고온에서 동작검사, 시험저항 설정에 따른 저항동작 지연시간 및 전류동작 지연시간, 온도변화에 따른 바이메탈 지연시간 검사, 블록히터의 전류 및 저항 검사, 히팅 운전검사 등을 수행하도록 설계한다.

• 한국안전학회지
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• 제32권2호
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• pp.46-51
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• 2017

This paper presents classification of domestic fire detector using response time index. Response time is measured using fire detector distributed in Korea, and the response time index is estimated. Plunge test prescribed by FM is conducted to measure response time of fire detector. The detector used to test is fixed temperature type(thermistor and bimetal type) and rate of rise temperature type(thermistor and pneumatic type). The nominal operation temperature of fixed temperature type detector is $70^{\circ}C$ and rate of rise temperature is $15^{\circ}C/min$. The fixed temperature type is measured 7 products, and the rate of rise temperature type is measured 5 products. The results show that in case of fixed temperature type(thermistor) is classified "Quick" or "Standard" and fixed temperature type(bimetal) is not classified. The rate of rise temperature type(thermistor) is classified "Fast" or "Ultra Fast" and the rate of rise temperature type(pneumatic) is classified "Very Fast" or "Ultra Fast". The pneumatic type shows more fast response than thermistor type. Also these results indicate the fixed temperature type(bimetal) is not suitable for early stage fire detection.

• 한국항공우주학회지
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• 제44권10호
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• pp.871-876
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• 2016

생산 초기의 초음속 항공기는 블리드 에어 덕트에 존재하는 생산용 자재의 부가 물질이 가열될 경우 조종실에 타는 냄새와 유사한 비정상적인 냄새가 조종실로 유입된다. 조종사가 이와 같은 냄새를 엔진의 화재와 같은 비상 상황으로 오인하는 것을 방지하기 위해 비정상적인 냄새의 원인 물질은 시험 비행 전에 burn-in test를 통해 제거되어야 한다. 그러나, 현재의 절차의 최고 온도보다 고고도 비행의 최고 온도가 더 높기 때문에 냄새를 완벽히 제거 할 수 없다. 본 논문은 고고도 비행의 열적 상황을 분석하여 개선된 burn-in test 절차를 제시한다. 비연속적인 유량 조절, 단위 시간당 높은 온도 변화율, 응축기와 터빈의 한계 온도 차이 때문에 현재의 절차로는 고고도 조건을 모사하지 못하는 것이 확인되었다. 이러한 한계를 극복하기 위해 램에어 입구 제어를 통해 연속적 유량 조절이 가능한 burn-in test 절차를 제시하였다. 제시된 방법을 통해 블리드 에어 온도가 지상에서 고고도 비행 조건 이상임을 확인하였으며, 비행 시험을 통해 비정상적인 냄새를 제거할 수 있음을 검증했다.

• 한국유체기계학회 논문집
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• 제14권1호
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• pp.42-47
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• 2011

Measurement uncertainty analysis of fuel flow using turbine flowmeter was performed for the case of altitude engine test. SAE ARP4990 was used as the fuel flow calculation procedure, as well as the mathematical model for the measurement uncertainty assessment. The assessment was performed using Sensitivity Coefficient Method. 11 parameters involved in the calculation of the flow rate were considered. For the given equipment setup, the measurement uncertainty of fuel flow was assessed in the range of 1.19~1.86 % for high flow rate case, and 1.47~3.31 % for low flow rate case. Fluctuation in frequency signal from the flowmeter had the largest influence on the fuel flow measurement uncertainty for most cases. Fuel temperature measurement had the largest for the case of low temperature and low flow rate. Calibration of K-factor and the interpolation of the calibration data also had large influence, especially for the case of very low temperature. Reference temperature, at which the reference viscosity of the sample fuel was measured, had relatively small contribution, but it became larger when the operating fuel temperature was far from reference temperature. Measurement of reference density had small contribution on the flow rate uncertainty. Fuel pressure and atmospheric pressure measurement had virtually no contribution on the flow rate uncertainty.

• 한국도로학회논문집
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• 제20권3호
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• pp.19-26
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• 2018

PURPOSES : The main purpose of this study is suggest of field bond strength evaluation method for more objective evaluation method through Evaluation of Bond Strength Properties with changing aspect ratio and temperature. METHODS : The evaluation is laboratory bond strength test. Using the core machine, the pull-off test method ; the bond strength test of interface layer the universal testing machine. RESULTS : As a result of the laboratory bond strength evaluation, it was verified that the bond strength by aspect ratio decreases linearly with increasing aspect ratio and the bond strength properties by temperature change existed at high and low temperature condition relative to odinary temperature condition. CONCLUSIONS : According to the results of laboratory bond strength evaluation, the field bond strength evaluation results suggest applying the proposed correction factor (0.8, 1.0, 1.4, 1.9) according to aspect ratio(0.5, 0.1, 1.5, 2.0), For more objective evaluation of the bond strength, it is analyzed that the evaluation value is within $6{\sim}32^{\circ}C$ and the result can be obtained within 5% of the coefficient of variation.