• Title/Summary/Keyword: Cooling analysis

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Benefit-Cost Analysis in Accordance with Replacement of Electrical Cooling System by Gas Cooling System using the California Standard Test (캘리포니아 표준테스트 방법을 사용한 전기냉방기기의 가스냉방기기 대체에 따른 편익비용분석)

  • Park, Rae-Jun;Song, Kyung-Bin;Won, Jong-Ryul
    • The Transactions of The Korean Institute of Electrical Engineers
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    • v.61 no.12
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    • pp.1774-1781
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    • 2012
  • There are some efforts to improve the performance of electrical heat pump(EHP) and replace it with an alternative cooling equipment such as gas engine-driven heat pump(GHP), a gas cooling equipment, in order to solve the problem of summer electricity supply through reducing the summer electricity peak. This paper analyzes cost-benefit in accordance with replacement of electrical cooling system by gas cooling system using california standard test and sensitivity analysis of some scenarios.

Experimental Study of Cooling Fan Performance Analysis and Shroud Characteristics for an Excavator (굴삭기 냉각팬 성능해석 및 슈라우드 특성에 대한 실험적 연구)

  • Lee, Jae-Seok;Chung, Kyung-Nam;Kim, Jin-Young;Lee, Tae-Kyung;Kang, Jeong-Won;Shim, Jae-Koo;Son, Deuk-Kyun
    • Proceedings of the KSME Conference
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    • 2007.05b
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    • pp.2597-2602
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    • 2007
  • In this paper, the performance analysis is experimentally carried out in order to select the best cooling fan and shroud considering both cooling performance and noise reduction. 4 cooling fans have been tested in the fan tester and the real excavator. In order to obtain the performance of the cooling fans, flow capacity has been estimated by measuring flow velocity using a hot wire anemometer, and noise radiation has been also measured to estimate the fan noise. Characteristics of a box-type and a streamlined shroud have been examined by changing the immersion depth of cooling fans. Based upon the results, the best cooling fan is selected. Finally, the criterion to select the best cooling fan has been set up.

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Thermal analysis of the conduction cooling system for HTS SMES system of 600 kJ class (600kJ급 SMES용 전도냉각시스템 열해석)

  • Hong, Yong-Ju;Yeom, Han-Kil;Park, Seong-Je;Kim, Hyo-Bong;Koh, Deuk-Yong
    • Proceedings of the KSME Conference
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    • 2007.05b
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    • pp.1959-1963
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    • 2007
  • SMES systems need cryogenic cooling systems. Conduction cooling system has more effective, compact structure than cryogen. In general, 2 stage GM cryocoolers are used for conduction cooling of HTS SMES system. 1st stages of cryocoolers are used for the cooling of current leads and radiation shields, and 2nd stages of cryocoolers for HTS coil. For the effective conduction cooling of the HTS SMES system, the temperature difference between the cryocooler and HTS coil should be minimized. In this paper, a cryogenic conduction cooling system for HTS SMES is analyzed to evaluate the performance of the cooling system. The analysis is carried out for the steady state with the heat generation of the HTS coil and effects of the thermal contact resistance. The results show the effects of the heat generation and thermal contact resistance on the temperature distribution.

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The Estimation of Curvature Deformation of Steel Plates in Water Cooling Process after Line Heating (선상 가열시 수냉 효과를 고려한 강판의 변형 추정에 관한 연구)

  • HwangBo, Hyeok;Yang, Park-Dal-Chi
    • Proceedings of the Korea Committee for Ocean Resources and Engineering Conference
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    • 2006.11a
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    • pp.209-212
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    • 2006
  • Line heating with water cooling is generally adapted process in the shipyards for the forming hull surface. The purpose of this paper is to develop a model of thermal deformation in water cooling process after the line heating. In order to simulate the cooling process, heat transfer analysis was performed by assuming the effects of water cooling as a negative heat-source. Experiment for the line heating with water cooling was performed for 9 models of plates in order to verify the cooling model. By using the suggested model for the water cooling process, it could be observed that the present method predict the plate deformations in the line heating more accurately.

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Fabrication and Testing of Injection Mold for Cosmetic Container with Conformal Cooling Channels Using Vacuum Diffusion Bonding (진공확산접합을 이용한 형상적응형 냉각채널을 가진 화장품 용기용 사출금형의 제작 및 시험사출)

  • Yu, Man-Jun;Park, Jong-Cheon
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.19 no.3
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    • pp.92-98
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    • 2020
  • In this study, an injection mold with conformal cooling channels was designed and manufactured for use in the production of a thick plastic cosmetic container that required high gloss surfaces. A cooling analysis verified the design of the conformal cooling channel for the cosmetic container, and also showed that the cooling efficiency was superior to that of the straight cooling channel. Slide cores designed with the conformal cooling channel were manufactured using the Layers Parting method and vacuum diffusion bonding. Subsequent test injection and quality inspection showed no problem in the appearance and dimensional accuracy of the produced product. The cycle time for product production was about 110 seconds, sufficient for mass production.

Numerical Analysis on the Performance of a Outdoor Air Cooled Heat exchanger for Cooling Tower (외기이용 하이브리드 냉각탑 성능해석)

  • Kim, Sung-Il;Lee, Wook-Hyun;Lee, Kye-Jung;Chun, Won-Pyo
    • Proceedings of the KSME Conference
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    • 2008.11b
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    • pp.2322-2327
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    • 2008
  • This paper is to provide analysis model that can be used to investigate the improvement in energy efficiency for cooling tower by using fresh air. Numerical analysis of Air-cooled heat exchanger for single-phase flow with variations of outdoor air temperature has been performed. A complete set of correlations of the heat transfer in both refrigerant and air sides was employed for predicting the heat transfer rate. The numerical results derived from the correlations were verified with experimental results. The energy consumption for a hybrid cooling tower has been compared for variation of a outdoor air temperature. The results showed that the hybrid cooling tower in low outdoor temperature offers a significant improvement in energy efficiency. The thermal analysis aids significantly in the solution of the design problem of hybrid cooling tower.

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A Study on Cooling Performance of In-wheel Motor for Green Car (그린카용 인휠 모터의 냉각 성능에 관한 연구)

  • Jung, Jung-Hun;Kim, Sung-Chul;Hong, Jung-Pyo
    • Transactions of the Korean Society of Automotive Engineers
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    • v.20 no.1
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    • pp.61-67
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    • 2012
  • The in-wheel motor used in green car was designed and constructed for an electric direct-drive traction system. It is difficult to connect cooling water piping because the in-wheel motor is located within the wheel structure. In the air cooling structure for the in-wheel motor, a outer surface on the housing is provided with cooling grooves to increase the heat transfer area. In this study, we carried out the analysis on the fluid flow and thermal characteristics of the in-wheel motor under the effects of motor speed and heat generation. In order to check the problem of heat release, the analysis has been performed using conjugate heat transfer (conduction and convection). As a result, flow fields and temperature distribution inside the in-wheel motor were obtained for base speed condition (1250 rpm) and maximum speed condition (5000 rpm). Also, the thermo-flow characteristics analysis of in-wheel motor for vehicles was performed in consideration of ram air effect. Therefore, we checked the feasibility of the air cooling for the housing geometry having cooling grooves and investigated the cooling performance enhancement.

The Study about the Performance-Analysis of a Automotive Engine Cooling System (엔진 냉각시스템 성능해석에 관한 연구)

  • Shin, Chang-Hoon;Lee, Seung-Hee;Park, Warn-Gyu;Jang, Gi-Lyong
    • Transactions of the Korean Society of Automotive Engineers
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    • v.14 no.2
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    • pp.39-48
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    • 2006
  • An engine cooling system affects overall performances of an engine which has been recently requested higher power in more confined engine room. The design of efficient cooling system demands a great effort to effectively correlate with each components, such as water jacket, radiator, coolant pump, cooling fan, etc. Thus, the aim of this study is to provide the design tool of the cooling system in the early design stage by enabling for the designer to accurately predict the engine cooling performances. This user-friendly design tool has various ways to assemble each components and control the running condition with related database. The present design tool was simulated and compared with experimental data. As a result, the inlet and outlet temperature of the radiator agree very well with experiments. It was concluded that the present design tool could be effectively used for the design of the engine cooling system.

Structural Design of Liquid Rocket Thrust Chamber Regenerative Cooling Channel (액체로켓 연소기 재생냉각 채널 구조설계)

  • Ryu Chul-Sung;Chung Yong Hyun;Choi Hwan-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • v.y2005m4
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    • pp.134-138
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    • 2005
  • The structural analysis and water pressure test of regenerative liquid rocket thrust chamber cooling channel specimens are performed at room temperature. material properties of copper alloy are obtained by uniaxial tension test at room temperature and used of elastic-plastic structural analysis. The plate type of cooling channel specimen are manufactured and performed water pressure test in order to confirm the analysis results. The differences between results of elastic-plastic analysis and that of water pressure test of cooling channel specimen are small and find that manufacturing process affect the structural stability of cooling channel very much because cooling channel thickness is small

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Cooling Performance Analysis of Regeneratively Cooled Combustion Chamber (재생냉각 연소실의 냉각성능 해석)

  • Cho, Won-Kook;Seol, Woo-Seok;Cho, Gwang-Rae
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.32 no.4
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    • pp.67-72
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    • 2004
  • A regenerative cooling system has been designed through empirical 1-D analysis for a liquid rocket engine of 30-ton-level thrust. The hot-gas-side wall temperature from 1-D analysis shows 100K difference compared to 3D CFD analysis. Two variations of design with same cooling performance are suggested for different maximum channel widths i.e., 4mm and 2mm. The coolant pressure drop of the latter design is higher by 20%. The maximum liner temperature is about 700K when TBC and the thermal resistance of carbon deposit are considered. So film cooling is recommended to increase the cooling capacity as the present cooling capacity is insufficient