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다양한 형상을 갖는 마이크로 히터의 열특성에 관한 실험 및 전산해석적 연구
김진우(Jin Woo Kim),김재춘(Jae Choon Kim),이준엽(Jun Yub Lee),정진택(Jin Taek Chung) 대한기계학회 2008 대한기계학회 춘추학술대회 Vol.2008 No.11
As a field of MEMS, micro-heater fabricated by Au is being introduced and developed in recent years. Previous studies about thermal properties of various forms of micro-heater were not sufficient. In this work, numerical and experimental analysis of the heat generation and the temperature distribution of micro-heater packages for 8 different geometric cases were studied. We fabricated a micro-heater package with silicon wafer, on which Cr/Au layer was laminated before 8 geometric forms of micro-heater were patterned. In each cases, temperature distribution was measured with IR thermal camera. According to the experimental results, which show a good agreement with the results analyzed by CFD, it was found that at 0.5W, the temperature of micro-heater chip which contained 20000㎛-long, serpentine shaped micro-heater was elevated to a relatively high temperature of 78℃. Consequently, we proposed a geometry of micro-heater which has effective thermal characteristics.
마이크로 채널을 이용한 LED 냉각 방법에 관한 전산 해석적 연구
김진우(Jin Woo Kim),김재춘,민재홍(Jae Hong Min),정진택(Jin Taek Chung) 대한기계학회 2009 대한기계학회 춘추학술대회 Vol.2009 No.11
The object of this paper is to propose a method to lower the junction temperature of LED using micro-channel by numerical method. To use LED for lighting, the chip needs to have a large capacity, resulting in concentrate heat in P-N connection area. To solve this problem, micro-channels were merged in PCB. Additionally, the characteristics of heat transfer in substrate including micro-channel were analyzed by CFD according to Re number, aspect ratio of micro-channel, and dimension of substrate. As a result, the parameters which were considered were important factor which influenced the characteristics of LED place on PCB. The junction temperature of LED chip could be lowered under the working temperature.
대체냉매 공기조화기용 로터리 압축기의 성능향상을 위한 최적 토출계에 관한 실험적 연구
윤영,정진택,민만기,Youn, Young,Chung, Jin-Taek,Min, Man-Ki 대한설비공학회 2001 설비공학 논문집 Vol.13 No.2
R410a which is one of HFC refrigerants is being considered to be a promising replacement for R22 widely used in domestic air conditioners. The rolling piston type rotary compressors for R410a have lower energy efficiency than those for R22 because of the high pressure difference between a suction chamber and a discharge chamber in the compression mechanism. in addition, the re-expansion gas loss of the rotary compressor for R410a which occurs a ta clearance volume in a discharge port becomes larger than that for R22 due to high density of R410a refrigerant. Therefore, Pressure-Volume analyses for various design parameters of a discharge system were carried out to improve efficiency of a R410a rotary compressor. The results such as performance dta, over-compression loss, and re-expansion loss were acquired by P-V analyses and analyzed quantitatively. As a conclusion, the optimal specifications of several design parameters of a discharge system were obtained by analyzing P-V diagrams.
날개 길이방향 유동과 날개 회전이 날개짓 운동의 공기역학적 특성에 미치는 효과
오현택(Hyun-Taek Oh),최항철(Hang-Cheol Choi),김광호(Kwang-Ho Kim),정진택(Jin Taek Chung) 한국항공우주학회 2007 韓國航空宇宙學會誌 Vol.35 No.9
3-D 날개짓 운동은 왕복운동과 회전운동으로 구성된다. 3-D 날개짓 운동은 왕복운동하는 동안 날개 길이방향의 유동이 발생된다. 또한 각각의 왕복운동의 끝에서 날개 회전에 의하여 회전에 의한 순환이 발생한다. 본 연구에서는 날개 길이방향 유동과 날개 회전이 3-D 날개짓 운동의 공기역학적 특성에 미치는 영향을 알아보기 위하여 3-D 날개짓 운동과 2-D 병진운동을 비교하였다. 각각의 날개짓 운동에서 받음각과 레이놀즈수에 따라 공력을 측정하였다. 2-D 병진운동의 공력이 3-D 날개짓 운동의 공력 보다 크다. 하지만 3-D 날개짓 운동시 발생되는 양력은 왕복운동의 중반부에서 받음각 50˚까지 증가하였고 2-D 병진운동시 발생되는 양력은 받음각 30˚이상에서 감소하였다. 또한 각각의 왕복운동의 끝에서 날개 회전에 의하여 공력이 급격하게 증가하였다. In a 3-D flapping motion, the spanwise flow is generated while the wing is moved on the stroke plane. And at the end of each stroke, the rotational circulation is generated due to a wing rotation. In this study, to evaluate the effect of spanwise flow and wing rotation on the aerodynamic characteristics in 3-D flapping motion, a 3-D flapping motion was compared with a 2-D translating motion. In each flapping motion, the aerodynamic forces were measured with respect to the angles of attack and Reynolds number. The aerodynamic forces generated by 2-D translating motion were higher than those generated by 3-D flapping motion. While the lift of 3-D flapping motion was increased until the angle of attack 60˚ at mid-stroke, the lift generated by 2-D translating motion was decreased above the angle of attack 40˚ at mid stroke. Also, at the end of each stroke, the aerodynamic forces were increased rapidly due to wing rotation.
날개 길이방향 유동이 날개짓 운동의 공기역학적 특성에 미치는 효과
오현택(Hyun-Taek Oh),최항철(Hang-Cheol Choi),김광호(Kwang-Ho Kim),정진택(Jin Taek Chung) 한국유체기계학회 2006 유체기계 연구개발 발표회 논문집 Vol.- No.-
Flight performance of birds and insects is superior to conventional fixed wing aircrafts at low Reynolds number regime. While they flap their wings, aerodynamic characteristics such as span-wise flow and rotational circulation are appeared on the wing. To study on the effect of span-wise flow, 3-D flapping motion was compared with 2-D flapping motion. In 3-D flapping motion, the measured lift forces were increased until the angle of attack 50° at mid-stroke. But in 2-D flapping motion, the lift forces were decreased above the angle of attack 30° at mid-stroke. Also, the mean lift to drag ratio of 3-D flapping motion is higher than that of 2-D flapping motion.
날개의 모서리 형상이 플래핑 운동의 공기역학적 특성에 미치는 영향
오현택(Hyun-Taek Oh),최항철(Hang-Cheol Choi),김광호(Kwang-Ho Kim),정진택(Jin Taek Chung) 대한기계학회 2006 대한기계학회 춘추학술대회 Vol.2006 No.6
Birds and insects have wings of rounded edge profiles. In the experiment, the wing of the square edge profiles had been employed. In this study, two wings which have different shapes of edge are used to investigate the aerodynamic characteristics. One wing has rounded edge profiles and the other has square edge profiles. Two half elliptic shaped wings were designed and scaled up according to the planform of a black-chinned hummingbird, Archilochus alexandri. While the wings were operated in the water, the aerodynamic forces were measured and the flow structures around the wings were visualized using the DPIV. The lift for the wing of rounded edge profiles was higher than that for the wing of square edge profiles. But drag for the wing of rounded edge profiles was lower than that for the wing of square edge profiles. Also the lift to drag ratio for the wing of rounded edge profiles at angle of attack from 0° to 40° was higher than that for the wing of square edge profiles.