• 제목/요약/키워드: Cooling Duct

검색결과 119건 처리시간 0.025초

정사각 막냉각홀 내부에서의 열/물질전달 및 유동 특성 (II) - 비대칭 입구조건 효과 - (Heat/Mass Transfer and Flow Characteristics Within a Film Cooling Hole of Square Cross Sections (II) - Effects of Asymmetric Inlet Flow Condition -)

  • 이동호;강승구;조형희
    • 대한기계학회논문집B
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    • 제26권7호
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    • pp.937-944
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    • 2002
  • An experimental study has been conducted to investigate the heat/mass transfer characteristics within a square film cooling hole with asymmetric inlet now condition. The asymmetric inlet now condition is achieved by making distances between side walls of the secondary now duct and the film cooling hole different; one side wall is $2D_h$ apart from the center of the film cooling hole, while the other side wall is $1.5D_h$ apart from the center of the film cooling hole. The heat/mass transfer experiments for this study have been performed using a naphthalene sublimation method and the now field has been analyzed by numerical calculation using a commercial code. Swirl now is generated at the inlet region and the heat/mass transfer pattem with the asymmetric inlet now condition is changed significantly from that with the symmetric condition. In the exit region, the effect of mainstream on the inside hole now is reduced with the asymmetric condition. The average heat/mass transfer coefficient is higher than that with the symmetric condition due to the swirl now generated by the asymmetric inlet condition.

터보샤프트 엔진의 배기 이젝터 설계 및 유동해석 (THE DESIGN AND ANALYSIS OF EXHAUST EJECTOR FOR TURBOSHAFT ENGINE)

  • 이창호;김철완
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2006년도 추계 학술대회논문집
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    • pp.97-100
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    • 2006
  • An ejector is designed for the purpose of engine bay cooling and exhaust gas cooling. The primary flow of the ejector is the exhaust gas of the turboshaft engine. The mass flow of secondary flow is calculated by using the approximate analytic equation. For the purpose of verification of approximate method, comparison is made with the results of Navier-Stokes turbulent flow solution. According to the results of CFD, the mixing of two flows is incomplete due to the short length of mixing duct.

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재생냉각 유로 내의 유동에 관한 수치해석 (Numerical Analysis of Fluid Flow in a Regenerative Cooling Passage)

  • 조원국
    • 한국추진공학회지
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    • 제4권1호
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    • pp.46-52
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    • 2000
  • 축소형 액체로켓 엔진에 적용될 재생냉각유로에 대한 전산유동해석을 수행하고 결과로서 유로 내의 압력손실과 열전달률을 예측하였다. 유로의 단면적 축소/확대가 압력손실을 증가시키지만 이차유동을 유발하고 난류화를 촉진시켜 열전달률을 상승시키는 효과가 있는 것으로 밝혀졌다. 단면적 변화는 노즐목 부근에서 일어나는데 이는 열부하가 큰 노즐목을 보호하는데 효과적이다. 또한 유량 변화로 인한 재생냉각 장치의 정량적인 성능변화를 관찰하였다.

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이온풍 공랭 방식 적용을 위한 방송용 LED 조명장치의 냉각 특성 해석 (Analysis of Cooling Characteristics of Broadcasting LED Light with Ion Wind Generator)

  • 박철우;이승준;김대중
    • 설비공학논문집
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    • 제24권9호
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    • pp.693-698
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    • 2012
  • In the present work, numerical analyses of broadcasting LED light with ion wind generator have been carried out for enhancement of cooling performance. Ion wind generator is produced and experimented before analysis. With the use of result of experiments, broadcasting LED light model is computed. Ion wind velocity into LED light is varied with 0~3 m/s. Based on the numerical results, the area of duct-type ion wind generator was designed to reduce the volume flow rate of ion wind. The modified inlet geometry shows sufficient cooling capability. And, through modified ion wind generator, the volume flow rate of ion wind has been largely reduced.

인덕션 쿡탑 기구물 형상변경이 Heatsink 및 Coil 냉각성능에 미치는 영향에 대한 연구 (Study on the Cooling Performance of Heatsink for Induction Cooktop using Computational Fluid Dynamics)

  • 박동호;권명근;이동범;서응렬;박용종
    • 한국유체기계학회 논문집
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    • 제18권3호
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    • pp.33-37
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    • 2015
  • A numerical study on the IPM/Bridge Diode cooling and coil cooling has been performed. Results are presented as plots of thermal resistance, temperature drop and RPM-ratio. CFD analysis for conventional cooling system has been performed as a reference case. As the RPM-Ratio was increased, heatsink thermal resistance and coil temperature were decreased. IPM/Bridge Diode thermal resistance and temperature of the coil is tended to be trade-off. The temperature of coil closest to the AC-motor fan showed the most significant change in accordance with duct design. The temperature of coil located at the top of DC-motor fan showed the most significant variation as the cooling air passes the heatsink fin area.

터보냉동기의 소음원 파악 및 저소음화에 대한 연구 (A Study on the Identification of Noise Source and the Noise Reduction Method of a Turbo Chiller)

  • 전완호
    • 한국유체기계학회 논문집
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    • 제7권3호
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    • pp.7-13
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    • 2004
  • In this paper, we identify the noise source and the path of a chiller. This chiller is newly developed for R-l34a refrigerant and 250 RT cooling capacity. The measured overall SPL of the developed turbo-chiller is about 100 dBA. Due to the high rotating speed of the centrifugal impeller, the nun noise source of the chiller is the blade passing frequency and its higher harmonics of the centrifugal impeller. This generated soundpropagates through the duct, and then transmits and radiates to the outer field. From the experiment, it is found that the high frequency noise is mostlytransmitted and radiated through the elbow duct, but the low frequency noise is transmitted and vadiated through the condenser wall. Therefore applying the absorbing material is an effective way of reducing the high and low frequency noise simultaneously. Measurement results show that the application of the sound absorbing material to the elbow duct reduced the overall sound pressure level by 4 dB compared to the 9 dBA reduction for the case of full enclosure. In order to control the generated noise, a dissipativetype silencer is also designed and tested. The silencer reduced the radiated noise about 7.5 dBA.

스마트무인기 엔진 배기가스가 기체에 미치는 영향에 관한 수치적 연구 (Numerical Study for the Effect of Engine Exhaust Gas on the Airframe of Smart UAV)

  • 이창호;김철완;김재무
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2008년도 춘계학술대회논문집
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    • pp.464-467
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    • 2008
  • An ejector is designed for the purpose of engine bay cooling. The primary flow of the ejector is the exhaust gas of the PW206C turboshaft engine. The mass flow of secondary flow is calculated by using the approximate analytic equation. And the effect of exhaust gas flow on the fuselage surface is investigated by using the Fluent Code. Three types of exhaust duct shape were compared in the viewpoint of surface temperature and aerodynamic drag. As a result, exhaust duct shape P3 shows minimum interference of exhaust gas and fuselage and minimum increment of drag among the three candidate shapes.

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열선유속계를 이용한 $180^{\circ}$ 곡덕트 내 난류유동의 측정 (Measurements of Turbulent Flows in the $180^{\circ}$ Curved Duct by Hot-wire Anemometer)

  • 한성호;김원갑;최영돈
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2003년도 추계학술대회
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    • pp.729-734
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    • 2003
  • This paper reports the characteristics of the three dimensional turbulent flow in the rectangular-sectioned 180 degree bends by Hot-wire anemometer. Grande and Kool proposed a cooling law for the measurements of the flow through the narrow passage. The authors noticed that the calibration coefficients of original method are not constant and fairly sensitive to the flow approaching angle. Measured voltages are converted to three velocity and six Reynolds stress components using the modified method in which the coefficients are treated as a function of approaching angle.

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주상용 몰드변압기의 온도분포와 열응력 해석 (The Temperature Distribution and Thermal Stress Analysis of Pole Mold transformer)

  • 조한구;이운용;한세원;김석수
    • 한국전기전자재료학회논문지
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    • 제14권4호
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    • pp.297-301
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    • 2001
  • In this paper, the temperature distribution and thermal stress analysis of 50kVA pole cast resin transformer for power distribution are investigated by FEM program. The one body molding model (Model 1) and air duct model (Model 2) are designed and their temperature distribution are analysed. The temperature rise value is about 105.5 deg in the model 1 and 65.28 de in the model 2. The temperature change of secondary winding is more than primary winding according to load ratio. The concentration part of Von Mises Stress occurs at interface between glass fiber and epoxy.

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공랭식 열교환핀이 부착된 열전모듈의 냉각 성능에 관한 연구 (Cooling Performance of Thermoelectric Module with Air-Cooled Heat Exchanger Fins)

  • 신재훈;한훈식;김윤호;김서영;현재민
    • 설비공학논문집
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    • 제22권3호
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    • pp.171-179
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    • 2010
  • Thermal performance of louver fin and plate fin in a thermoelectric cooling system with a duct-flow type fan arrangement is analytically evaluated. The thermoelectric cooling system consists of a thermoelectric module and two heat exchanger fins. The analytic results show that the optimized louver fin has lower thermal resistance than plate fin. The COP and heat absorbed rate of the thermoelectric cooling system with optimized louver fins are 10.3% and 5.8% higher than optimized plate fins, respectively.