• Journal of Biosystems Engineering
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• 제4권2호
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• pp.64-64
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• 1979

Low-temperature drying systems have been extensively used for drying cereal grain such as shelled corn and wheat. Since the 1973 energy crisis, many researches have been conducted to apply solar energy as supplemental heat to natural air drying systems. However, little research on rough rice drying has been done in this area, especially very little in Korea. In designing a solar drying system, quality loss, airflow requirements, temperature rise of drying air, fan power and energy requirements should be throughly studied. The factors affecting solar drying systems are airflow rate, initial moisture content, the amount of heat added to drying air, fan operation method and the weather conditions. The major objectives of this study were to analyze the effects of the performance factors and determine design parameters such as airflow requirements, optimum bed depth, optimum temperature rise of drying air, fan operation method and collector size. Three hourly observations based on the 4-year weather data in Chuncheon area were used to simulate rough rice drying. The results can be summarized as follows: 1. The results of the statistical analysis indicated that the experimental and predicted values of the temperature rise of the air passing through the collector agreed well.2. Equilibrium moisture content was affected a little by airflow rate, but affected mainly by the amount of heat added, to drying air. Equilibrium moisture content ranged from 12.2 to 13.2 percent wet basis for the continuous fan operation, from 10.4 to 11.7 percent wet basis for the intermittent fan operation respectively, in range of 1. 6 to 5. 9 degrees Centigrade average temperature rise of drying air.3. Average moisture content when top layer was dried to 15 percent wet basis ranged from 13.1 to 13.9 percent wet basis for the continuous fan operation, from 11.9 to 13.4 percent wet basis for the intermittent fan operation respectively, in the range of 1.6 to 5.9 degrees Centigrade average temperature rise of drying air and 18 to 24 percent wet basis initial moisture content. The results indicated that grain was overdried with the intermittent fan operation in any range of temperature rise of drying air. Therefore, the continuous fan operation is usually more effective than the intermittent fan operation considering the overdrying.4. For the continuous fan operation, the average temperature rise of drying air may be limited to 2.2 to 3. 3 degrees Centigrade considering safe storage moisture level of 13.5 to 14 perceut wet basis.5. Required drying time decrease ranged from 40 to 50 percent each time the airflow rate was doubled and from 3.9 to 4.3 percent approximately for each one degrees Centigrade in average temperature rise of drying air regardless of the fan operation methods. Therefore, the average temperature rise of drying air had a little effect on required drying time.6. Required drying time increase ranged from 18 to 30 percent approximately for each 2 percent increase in initial moisture content regardless of the fan operation methods, in the range of 18 to 24 percent moisture.7. The intermittent fan operation showed about 36 to 42 percent decrease in required drying time as compared with the continuous fan operation.8. Drymatter loss decrease ranged from 34 to 46 percent each time the airflow rate was doubled and from 2 to 3 percent approximately for each one degrees Centigrade in average temperature rise of drying air, regardless of the fan operation methods. Therefore, the average temperature rise of drying air had a little effect on drymatter loss. 9. Drymatter loss increase ranged from 50 to 78 percent approximately for each 2 percent increase in initial moisture content, in the range of 18 to 24 percent moisture. 10. The intermittent fan operation: showed about 40 to 50 percent increase in drymatter loss as compared with the continuous fan operation and the increasing rate was higher at high level of initial moisture and average temperature rise.11. Year-to-year weather conditions had a little effect on required drying time and drymatter loss.12. The equations for estimating time required to dry top layer to 16 and 1536 wet basis and drymatter loss were derived as functions of the performance factors. by the least square method.13. Minimum airflow rates based on 0.5 percent drymatter loss were estimated.Minimum airflow rates for the intermittent fan operation were approximately 1.5 to 1.8 times as much as compared with the continuous fan operation, but a few differences among year-to-year.14. Required fan horsepower and energy for the intermittent fan operation were3. 7 and 1. 5 times respectively as much as compared with the continuous fan operation.15. The continuous fan operation may be more effective than the intermittent fan operation considering overdrying, fan horsepower requirements, and energy use.16. A method for estimating the required collection area of flat-plate solar collector using average temperature rise and airflow rate was presented.

• 대한핵의학회지
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• 제38권1호
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• pp.74-84
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• 2004

목적:. I-125는 저에너지(27-35 keV) 방사선을 방출하기 때문에 두께가 얇은 섬광결정과 조준기를 사용할 수 있어 고분해능, 고민감도 영상획득에 유리한 물리적 특성을 가지고 있다. 이 연구의 목적은 새로운 시뮬레이션 도구인 GATE (Geant4 Application for Tomographic Emission)를 사용하여 최적의 I-125 SPECT 시스템 파라미터를 도출하는 것이다. 대상 및 방법: 시뮬레이션 방법의 신뢰성을 검증하기 위해, Weisenberger 등이 개발한 감마 카메라 시스템을 모사하였다. 섬광체로 평판형 Nal(T1)을 사용하였으며, 두께는 검출효율을 계산해서 결정하였다. 평행구멍조준기와 바늘구멍조준기의 여러 파라미터가 공간분해능과 민감도에 미치는 영향을 평가하였다. 그리고 최적화된 조준기를 결합한 I-125 SPECT의 성능을 평가하였다. 결과: 시뮬레이션에 대한 신뢰성 검증연구 결과, 측정과 시뮬레이션에서 공간분해능(4%)과 민감도(3%)가 유사함을 확인하였다. Nal(T1) 두께는 I-125 감마선을 98% 검출할 수 있도록 1 mm로 결정하였다. 시뮬레이션 결과 고분해능 평행구멍조준기로 구멍크기가 0.2 mm이고 길이가 5 mm인 사각구멍조준기를 선택하였고, 범용 평행구멍조준기로 구멍크기가 0.5 m이고, 길이가 10 mm인 육각구멍조준기를 선택하였다. 바늘구멍조준기는 구멍지름이 0.25 mm이고 채널높이가 0.1 mm이며, 허용각도가 90도인 조준기를 선택하였다. 최적화된 고분해능 평행구멍조준기, 범용 평행구멍조준기, 바늘구멍조준기를 결합한 I-125 SPECT의 재구성 영상 공간분해능은 각각 1.2 mm, 1.7 mm, 0.8 mm였으며, 민감도는 39.7 cps/MBq, 71.9 cps/MBq, 5.5 cps/MBq이었다. 결론: GATE 시뮬레이션으로 I-125 영상에 적합한 섬광결정 파라미터 및 조준기 파라미터를 도출하였다. 이 연구결과는 I-125 SPECT로 탁월한 고분해능, 고민감도 영상을 얻을 수 있음을 보여준다.

• 한국농공학회지
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• 제26권1호
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• pp.52-72
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• 1984

This study was performed to obtain the basic data which can be applied to the use of epoxy resin mortars. The data was based on the properties of epoxy resin mortars depending upon various mixing ratios to compare those of cement mortar. The resin which was used at this experiment was Epi-Bis type epoxy resin which is extensively being used as concrete structures. In the case of epoxy resin mortar, mixing ratios of resin to fine aggregate were 1: 2, 1: 4, 1: 6, 1: 8, 1:10, 1 :12 and 1:14, but the ratio of cement to fine aggregate in cement mortar was 1 : 2.5. The results obtained are summarized as follows; 1.When the mixing ratio was 1: 6, the highest density was 2.01 g/cm$^3$, being lower than 2.13 g/cm$^3$ of that of cement mortar. 2.According to the water absorption and water permeability test, the watertightness was shown very high at the mixing ratios of 1: 2, 1: 4 and 1: 6. But then the mixing ratio was less than 1 : 6, the watertightness considerably decreased. By this result, it was regarded that optimum mixing ratio of epoxy resin mortar for watertight structures should be richer mixing ratio than 1: 6. 3.The hardening shrinkage was large as the mixing ratio became leaner, but the values were remarkably small as compared with cement mortar. And the influence of dryness and moisture was exerted little at richer mixing ratio than 1: 6, but its effect was obvious at the lean mixing ratio, 1: 8, 1:10,1:12 and 1:14. It was confirmed that the optimum mixing ratio for concrete structures which would be influenced by the repeated dryness and moisture should be rich mixing ratio higher than 1: 6. 4.The compressive, bending and splitting tensile strenghs were observed very high, even the value at the mixing ratio of 1:14 was higher than that of cement mortar. It showed that epoxy resin mortar especially was to have high strength in bending and splitting tensile strength. Also, the initial strength within 24 hours gave rise to high value. Thus it was clear that epoxy resin was rapid hardening material. The multiple regression equations of strength were computed depending on a function of mixing ratios and curing times. 5.The elastic moduli derived from the compressive stress-strain curve were slightly smaller than the value of cement mortar, and the toughness of epoxy resin mortar was larger than that of cement mortar. 6.The impact resistance was strong compared with cement mortar at all mixing ratios. Especially, bending impact strength by the square pillar specimens was higher than the impact resistance of flat specimens or cylinderic specimens. 7.The Brinell hardness was relatively larger than that of cement mortar, but it gradually decreased with the decline of mixing ratio, and Brinell hardness at mixing ratio of 1 :14 was much the same as cement mortar. 8.The abrasion rate of epoxy resin mortar at all mixing ratio, when Losangeles abation testing machine revolved 500 times, was very low. Even mixing ratio of 1 :14 was no more than 31.41%, which was less than critical abrasion rate 40% of coarse aggregate for cement concrete. Consequently, the abrasion rate of epoxy resin mortar was superior to cement mortar, and the relation between abrasion rate and Brinell hardness was highly significant as exponential curve. 9.The highest bond strength of epoxy resin mortar was 12.9 kg/cm$^2$ at the mixing ratio of 1:2. The failure of bonded flat steel specimens occurred on the part of epoxy resin mortar at the mixing ratio of 1: 2 and 1: 4, and that of bonded cement concrete specimens was fond on the part of combained concrete at the mixing ratio of 1 : 2 ,1: 4 and 1: 6. It was confirmed that the optimum mixing ratio for bonding of steel plate, and of cement concrete should be rich mixing ratio above 1 : 4 and 1 : 6 respectively. 10.The variations of color tone by heating began to take place at about 60˚C, and the ultimate change occurred at 120˚C. The compressive, bending and splitting tensile strengths increased with rising temperature up to 80˚ C, but these rapidly decreased when temperature was above 800 C. Accordingly, it was evident that the resistance temperature of epoxy resin mortar was about 80˚C which was generally considered lower than that of the other concrete materials. But it is likely that there is no problem in epoxy resin mortar when used for unnecessary materials of high temperature resistance. The multiple regression equations of strength were computed depending on a function of mixing ratios and heating temperatures. 11.The susceptibility to chemical attack of cement mortar was easily affected by inorganic and organic acid. and that of epoxy resin mortar with mixing ratio of 1: 4 was of great resistance. On the other hand, when mixing ratio was lower than 1 : 8 epoxy resin mortar had very poor resistance, especially being poor resistant to organicacid. Therefore, for the structures requiring chemical resistance optimum mixing of epoxy resin mortar should be rich mixing ratio higher than 1: 4.

• 한국식품과학회지
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• 제14권4호
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• pp.342-349
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• 1982

송풍식건조과정(送風式乾燥過程) 중의 말쥐치육의 건조기구(乾操機構)와 수분활성(水分活性)과의 관계를 검토하기 위하여 $47.5^{\circ}C$에서 풍속과 공기의 상대습도를 달리하여 실험한 결과를 요약하면 다음과 같다. 전체 건조과정은 정속건조기(定速乾燥期)와 감속건조기(減速乾燥期)로 구분되었다. 정속건조기(定速乾燥期)는 건조표면(乾燥表面)이 수분활성(水分活性) 1.0을 유지하는한 계속되었으며, 온도와 상대습도가 일정할 때 정속건조속도(定速乾燥速度)는 공기의 속도(速度)의 제곱근에 비례하였다. 감속건조기(減速乾燥期)는 건조기구(乾操機構)가 서로 다른 제(第)1 및 제(第)2감속건조기(減速乾燥期)로 구분되었다. 제(第)1감속건조기(減速乾燥期)는 모세관 응축수의 건조표면(乾燥表面)으로의 이동이 불충분한 불포화표면건조기(不飽和表面乾燥期)였으며, 이 때의 건조속도(乾燥速度)는 공기의 온도가 일정할 때 상대습도에 크게 좌우되었다. 제(第)1감속건조기(減速乾燥期)와 제(第)2감속건조기(減速乾燥期)의 변환점에서 표면경화현상(表面硬化現象)이 시작되었다. 상대습도의 변화에 따라 제(第)2감속건조기(減速乾燥期)가 시작될 때의 수분활성(水分活性)과 수분함량(水分含量)은 각각 다른 값을 나타내었다. 제(第)2감속건조기(減速乾燥期)는 다시 건조기구(乾操機構)를 달리하는 두 개의 건조기(乾燥期)로 구분되었다. 제(第)2감속건조기(減速乾燥期)의 1단계는 말쥐치육 내부의 모세관 응축수가 건조표면(乾燥表面)으로 확산, 증발하여 건조가 진행되었으며, 이때의 수분의 확산계수는 $47.5^{\circ}C$에서 $2.89{\cdot}10^{-10}m^2/sec$였다. 표면경화현상(表面硬化現象)은 말쥐치육의 수분활성(水分活性)이 0.7에 이를때까지 계속되었다. 제(第)2감속건조기(減速乾燥期)의 2단계는 수분활성(水分活性) 0.45에서 시작되었다. 이 때의 건조는 말쥐치육 내부에 다분자층(多分子層)으로 흡착(吸着)한 결합수의 건조표면(乾燥表面)으로의 확산, 증발에 의하여 진행되었다. 흡착수분(吸着水分)의 분자층(分子層)의 수는 4였으며, $47.5^{\circ}C$에서의 확산계수는 $4.38{\cdot}10^{-11}m^2/sec$였다.

• 한국표면공학회:학술대회논문집
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• 한국표면공학회 2000년도 추계학술발표회 초록집
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• pp.3-4
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• 2000

Many researchers are interested in the synthesis and characterization of carbon nitride and diamond-like carbon (DLq because they show excellent mechanical properties such as low friction and high wear resistance and excellent electrical properties such as controllable electical resistivity and good field electron emission. We have deposited amorphous carbon nitride (a-C:N) thin films and DLC thin films by shielded arc ion plating (SAIP) and evaluated the structural and tribological properties. The application of appropriate negative bias on substrates is effective to increase the film hardness and wear resistance. This paper reports on the deposition and tribological OLC films in relation to the substrate bias voltage (Vs). films are compared with those of the OLC films. A high purity sintered graphite target was mounted on a cathode as a carbon source. Nitrogen or argon was introduced into a deposition chamber through each mass flow controller. After the initiation of an arc plasma at 60 A and 1 Pa, the target surface was heated and evaporated by the plasma. Carbon atoms and clusters evaporated from the target were ionized partially and reacted with activated nitrogen species, and a carbon nitride film was deposited onto a Si (100) substrate when we used nitrogen as a reactant gas. The surface of the growing film also reacted with activated nitrogen species. Carbon macropartic1es (0.1 -100 maicro-m) evaporated from the target at the same time were not ionized and did not react fully with nitrogen species. These macroparticles interfered with the formation of the carbon nitride film. Therefore we set a shielding plate made of stainless steel between the target and the substrate to trap the macropartic1es. This shielding method is very effective to prepare smooth a-CN films. We, therefore, call this method "shielded arc ion plating (SAIP)". For the deposition of DLC films we used argon instead of nitrogen. Films of about 150 nm in thickness were deposited onto Si substrates. Their structures, chemical compositions and chemical bonding states were analyzed by using X-ray diffraction, Raman spectroscopy, X-ray photoelectron spectroscopy and infrared spectroscopy. Hardness of the films was measured with a nanointender interfaced with an atomic force microscope (AFM). A Berkovich-type diamond tip whose radius was less than 100 nm was used for the measurement. A force-displacement curve of each film was measured at a peak load force of 250 maicro-N. Load, hold and unload times for each indentation were 2.5, 0 and 2.5 s, respectively. Hardness of each film was determined from five force-displacement curves. Wear resistance of the films was analyzed as follows. First, each film surface was scanned with the diamond tip at a constant load force of 20 maicro-N. The tip scanning was repeated 30 times in a 1 urn-square region with 512 lines at a scanning rate of 2 um/ s. After this tip-scanning, the film surface was observed in the AFM mode at a constant force of 5 maicro-N with the same Berkovich-type tip. The hardness of a-CN films was less dependent on Vs. The hardness of the film deposited at Vs=O V in a nitrogen plasma was about 10 GPa and almost similar to that of Si. It slightly increased to 12 - 15 GPa when a bias voltage of -100 - -500 V was applied to the substrate with showing its maximum at Vs=-300 V. The film deposited at Vs=O V was least wear resistant which was consistent with its lowest hardness. The biased films became more wear resistant. Particularly the film deposited at Vs=-300 V showed remarkable wear resistance. Its wear depth was too shallow to be measured with AFM. On the other hand, the DLC film, deposited at Vs=-l00 V in an argon plasma, whose hardness was 35 GPa was obviously worn under the same wear test conditions. The a-C:N films show higher wear resistance than DLC films and are useful for wear resistant coatings on various mechanical and electronic parts.nic parts.