• 제목/요약/키워드: Uniform Heating

검색결과 278건 처리시간 0.023초

PDP용 배기로내 열전달 현상에 관한 해석 (The Analysis of the Heat Transfer Characteristic in a PDP Ventilation Chamber)

  • 박형규;정재동;김찬중;이준식;박희재;조영만;조해균;박득일
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2000년도 춘계학술대회논문집B
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    • pp.385-391
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    • 2000
  • An analysis of the heat transfer in a PDP ventilation chamber has been conducted to investigate the required heat curve and temperature uniformity of the panels. Firstly, experiment in a test chamber has been carried out and compared with the unsteady 3D numerical simulation. Reasonable agreement was found, which suggested that the employed numerical model had its credibility in an actual PDP ventilation process. On this ground, tact-type heating/cooling system was analyzed. The panel temperature was more uniform in the $40^{\circ}C$ tact-type system than in the $80^{\circ}C$ one. Comparison of full simulation of a cart and simplified simulation of one panel shows the panel pitch, which is closely related to a production rate, can be also predicted.

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Local transport properties of coated conductors by laser-scan imaging methods

  • Kim, Gracia;Jo, William;Nam, Dahyun;Cheong, Hyeonsik;Moon, Seoung Hyun
    • 한국초전도ㆍ저온공학회논문지
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    • 제18권2호
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    • pp.1-4
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    • 2016
  • To observe the superconducting current and structural properties of high critical temperature ($T_c$) superconductors (HTS), we suggest the following imaging methods: Room temperature imaging (RTI) through thermal heating, low-temperature bolometric microscopy (LTBM) and Raman scattering imaging. RTI and LTBM images visualize thermal-electric voltages as different thermal gradients at room temperature (RT) and superconducting current dissipation at near-$T_c$, respectively. Using RTI, we can obtain structural information about the surface uniformity and positions of impurities. LTBM images show the flux flow in two dimensions as a function of the local critical currents. Raman imaging is transformed from Raman survey spectra in particular areas, and the Raman vibration modes can be combined. Raman imaging can quantify the vibration modes of the areas. Therefore, we demonstrate the spatial transport properties of superconducting materials by combining the results. In addition, this enables visualization of the effect of current flow on the distribution of impurities in a uniform superconducting crystalline material. These imaging methods facilitate direct examination of the local properties of superconducting materials and wires.

비전도 반평판 사이에서 미끄럼 운동하는 평판 층의 열탄성 불안정성 (Thermoelastic Instability of the Layer Sliding between Two Non-conducting Half-planes)

  • 하태원;조용구;김흥섭;이정윤;오재응
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2003년도 춘계학술대회논문집
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    • pp.483-488
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    • 2003
  • Frictional heating in brakes causes thermoelastic distortion of the contacting bodies and hence affects the contact pressure distribution. The resulting thermo-mechanical coupling can cause thermoelastic instability (TEI) if the sliding speed is sufficiently high, leading to non-uniform heating called hot spots and low frequency vibration known as hot judder. The vibration of brakes to the known phenomenon of frictionally-excited thermoelastic instability is estimated studying the interface temperature and pressure evolution with time. A simple model has been considered where a layer with half-thickness ${\alpha}$ slides with speed V between two half-planes which are rigid and non-conducting. The advantage of this properly simple model permits us to deduce analytically the critical conditions for the onset of instability, which is the relation between the critical speed and the growth rate of the interface temperature and pressure. Symmetrical component of pressure and temperature distribution at the layer interfaces can be more unstable than antisymmetrical component. As the thickness ${\alpha}$ reduces, the system becomes more apt to thermoelastic instability. Moreover, the evolution of the system beyond the critical conditions has shown that even if low frequency perturbations are associated with low critical speed, it might be less critical than high frequency perturbations if the working sliding speed is much larger than the actual critical speed of the system.

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모세관을 이용한 멀티형 열펌프의 신뢰성에 관한 실험적 연구 (An Experimental Stuff on the Performance of Multi-type Heat Pump using Capillary Tubes)

  • 권영철;장근선;이윤수;김대훈;전용호;이상재
    • 설비공학논문집
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    • 제14권9호
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    • pp.749-755
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    • 2002
  • In order to develop a multi-type heat pump system with two indoor units of non-uniform capacities, the optimum refrigerant circuit was developed using capillary tubes. The refrigerant circuit was composed of four main parts, a heating circuit, a cooling circuit, a by-pass circuit and a balance circuit. The system characteristics of multi-type heat pump was investigated through the rating test and the reliability test, using the multi-type psy-chrometric calorimeter. The results of the rating test showed that the capacity of the multi-type heat pump was about 93% of the design value. In particular, the capacity of cooling single mode was about 13% higher than the design value, and the capacity of heating multi mode was about 5% higher than the design value. The reliability of the multi-type heat pump was verified by various reliability tests (overload, extension tube, freeze up, under/over charging, sweat, flood back). The optimal amount of refrigerant charge and compressor capacity were determined from the present work.

온도 구배열자극측정법의한 XLPE하전입자의 극성판정 (Polarity of Charged Particles n XLPE Measured by Temperature Gradient Thermally Stimulated Surface Potential)

  • 국상훈
    • 대한전기학회논문지
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    • 제34권4호
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    • pp.144-152
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    • 1985
  • This paper temperature gradient thermally stimulated surface potentian (TG-TSSP) in measurements are applied to the study of the polarity of trapped and ionic carriers in cross-linked polyethylene (XLPE) filsm. In the thermally stimulated current in uniform temperature (TSC) of XLPE five peaks appear as indicated of the A B C D and E. In this paper A (at about -120$^{\circ}C$) D (at about 70$^{\circ}C$) and E (at about 110$^{\circ}C$) peaks are investigated. A peak is due to the biassing voltage and biassing temperature. Appear in to the glass transition temperature territory and caused in to the polarization of dipole. D peak is due to the depolarization of ionic space charge and E peak due to the detrapping of carriers injected from the electrodes. TG-TSSP and TSSP are measured to study the polarity of ionic carrier (D peak). In the unsatureated region of ionic space charge polarization, TG-TSSP is lower than TSSP during the initial stage of heating. Result of the experiment for E peak, TG-TSSP is higher than TSSP during the initial stage of heating and these results do not depend on the polarity of biassing voltage, and E peak is concerned with positive carriers (Holes).

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단단한 비전도 반평판 사이에서 미끄럼 운동하는 평판층의 열탄성 불안정성 (Thermoelastic Instability of the Layer Sliding between Two Rigid Non-conducting Half-planes)

  • 오재응;하태원;조용구;김흥섭;이정윤
    • 한국자동차공학회논문집
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    • 제12권1호
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    • pp.114-121
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    • 2004
  • Frictional heating in brakes causes thermoelastic distortion of the contacting bodies and hence affects the contact pressure distribution. The resulting thermo-mechanical coupling can cause thermoelastic instability (TEI) if the sliding speed is sufficiently high, leading to non-uniform heating called hot spots and low frequency vibration known as hot judder. The vibration of brakes to the known phenomenon of frictionally-excited thermoelastic instability is estimated studying the interface temperature and pressure evolution with time. A simple model has been considered where a layer with half-thickness$\alpha$slides with speed V between two half-planes which are rigid and non-conducting. The advantage of this properlysimple model permits us to deduce analytically the critical conditions for the onset of instability, which is the relation between the critical speed and the growth rate of the interface temperature and pressure. Symmetrical component of pressure and temperature distribution at the layer interfaces can be more unstable than antisymmetrical component. As the thickness $\alpha$ reduces, the system becomes more apt to thermoelastic instability. For perturbations with wave number smaller than the critical$m_{cr}$ the temperature increases with m vice versa for perturbations with wave number larges than $m_{cr}$ , the temperature decreases with m.

PDP용 배기로내 열전달 현상 해석 (Heat Transfer Analysis in a PDP Ventilation Chamber)

  • 박형규;정재동;김찬중;이준식;박희재;조영만;조해균;박득일
    • 대한기계학회논문집B
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    • 제25권3호
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    • pp.347-355
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    • 2001
  • A heat transfer analysis in a ventilation chamber of Plasma Display Panel(PDP) has been conducted. The process requirement is to precisely follow prescribed temperature trajectory while maintaining temperature uniformity for each panel. Firstly, experiment in a test chamber has been carried out and the results are compared with the unsteady 3D numerical data. Reasonable agreement was found, which suggested that the employed numerical model had its credibility in actual PDP ventilation processes. On this ground, a tact-type heating/cooling system was analyzed. The panel temperature in the 40$^{\circ}C$ tact-type system was more uniform than that in the 80$^{\circ}C$ one. For improving the uniformity of panel temperature, relocation of ventilation head to the rear part and inlet flow control are required. Comparison of full simulation of a cart and simplified simulation of one panel indicates the optimized panel pitch can also be predicted.

열전달 향상을 위한 새로운 MCFC 연료전지용 프리컨버터의 수치해석 (Numerical Analysis of New Proposals to Enhance Heat Transfer in MCFC'S Preconverter)

  • 손창현
    • 대한기계학회논문집B
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    • 제37권8호
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    • pp.753-758
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    • 2013
  • 본 연구는 MCFC용 벽면가열 방식 프리컨버터의 낮은 열전도율 때문에 발생하는 벽면 고온 발생 문제를 해결하기 위한 두 가지 방안을 수치해석을 통해 연구하였다. 프리컨버터 내부에 열전도율이 높은 다공성판을 설치한 경우 벽면에서 중심부위로 열전달이 향상되어 수소 생성이 벽면부위에 국한되지 않고 촉매내부에 좀 더 균일하게 발생되는 것을 확인하였다. 그리고 촉매 내부에 일정한 두께의 빈 공간을 중심, 1/2 그리고 4/5 위치에 두고 해석하여 결과를 비교하였고, 1/2위치의 빈 공간이 다른 경우에 비해 연료전환이 보다 이상적인 경우에 근접하지만 열전도율이 높은 다공성판의 설치가 보다 효과적임을 확인하였다.

An Investigation of Heat Transfer Characteristics of Swirling Flow in a 180$^{\circ}$ Circular Section Bend with Uniform Heat Flux

  • Chang, Tae-Hyun
    • Journal of Mechanical Science and Technology
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    • 제17권10호
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    • pp.1520-1532
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    • 2003
  • An experiment was performed to obtain the local heat transfer coefficient and Nusselt number in a circular duct with a 180$^{\circ}$ bend for Re=6 x 10$^4$, 8 x 10$^4$ and 1 x 10$\^$5/ under swirling flow and non-swirling flow conditions. The test tube with a circular section was made from stainless steel having a curvature ration of 9.4. Current heat flux of 5.11 kW/㎡ was applied to the test tube by electrical power and the swirling motion of air was produced by a tangential inlet to the pipe axis at 180$^{\circ}$. Measurements of local wall temperatures and the bulk mean temperatures of air were made at four circumferential positions at 16 stations. The wall temperatures showed a reduced distribution curve at the bend for the non-swirling flow, but this effect did not appear for the swirling flow. The Nusselt number distributions for the swirling flow, which was calculated from the measured wall and the bulk temperatures, were higher than that of the non-swirling flow. The average Nusselt number of the swirling flow increased by about 90-100%, compared to that of the non-swirling flow. The Nu/Nu$\_$DB/ values at the 90$^{\circ}$ station for non-swirling flow and swirling flow were approximately 2.5 and 4.8 at Re=6x10$^4$ respectively. The values agree well with Said's results for non-swirling flow.

Thermal Analysis of Silicon Carbide Coating on a Nickel based Superalloy Substrate and Thickness Measurement of Top Layers by Lock-in Infrared Thermography

  • Ranjit, Shrestha;Kim, Wontae
    • 비파괴검사학회지
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    • 제37권2호
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    • pp.75-83
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    • 2017
  • In this paper, we investigate the capacity of the lock-in infrared thermography technique for the evaluation of non-uniform top layers of a silicon carbide coating with a nickel based superalloy sample. The method utilized a multilayer heat transfer model to analyze the surface temperature response. The modelling of the sample was done in ANSYS. The sample consists of three layers, namely, the metal substrate, bond coat and top coat. A sinusoidal heating at different excitation frequencies was imposed upon the top layer of the sample according to the experimental procedures. The thermal response of the excited surface was recorded, and the phase angle image was computed by Fourier transform using the image processing software, MATLAB and Thermofit Pro. The correlation between the coating thickness and phase angle was established for each excitation frequency. The most appropriate excitation frequency was found to be 0.05 Hz. The method demonstrated potential in the evaluation of coating thickness and it was successfully applied to measure the non-uniform top layers ranging from 0.05 mm to 1 mm with an accuracy of 0.000002 mm to 0.045 mm.