• Title/Summary/Keyword: liquid cooling

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Subcooling of cryogenic liquid by diffusion-driven evaporation (확산동기 증발에 의한 극저온 액체 과냉각)

  • Cho, Nam-Kyung;Jeong, Sang-Kwon
    • Progress in Superconductivity and Cryogenics
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    • v.9 no.3
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    • pp.72-82
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    • 2007
  • This paper relates to reducing the temperature of a cryogenic liquid by contacting it with gas bubbles, which can be characterized by diffusion-driven evaporative cooling, The characteristic of diffusion-driven evaporative cooling is thoroughly examined by theoretical. analytical and experimental methods specifically for the case of helium injection into liquid oxygen. The results reveal that if the gaseous oxygen partial pressure in helium bubbles is lower than the liquid oxygen vapor pressure, cooling occurs autonomously due to diffusion mass transfer. The method of lowering the injected helium temperature turns out to be very effective for cooling purpose.

Performance Test of Cooling System for the KEPCO HTS Power Cable (한전 초전도전력케이블 냉각시스템 성능시험)

  • Yang, H.S.;Kim, D.L.;Sohn, S.H.;Lim, J.H.;Choi, H.O.;Lee, B.S.;Choi, Y.S.;Ryoo, H.S.;Hwang, S.D.
    • Proceedings of the KSME Conference
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    • 2007.05b
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    • pp.2206-2210
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    • 2007
  • As a power transmission line supplying power to a densely populated city, the high temperature superconducting (HTS) cable is expected to one of the most effective cables with a compact size because of its high current density. The verification of HTS power cable system have been progressed by KEPRI. A cooling system for a 3-phase 100m HTS power cable with 22.9kV/1.25kA was installed and tested at KEPCO's Gochang power testing center in Korea. The system consists of a liquid nitrogen decompression cooling system with a cooling capacity of 3kW and a closed circulation system of subcooled liquid nitrogen. Several performance tests of the cable system with respect to the cooling such as cooling capacity, heat load and temperature stability, were performed at several temperatures. Thermal cycle test, cool-down to liquid nitrogen temperature and warm-up to room temperature, was also performed to investigate thermal cycle influences. The outline of the installed cooling system and performance test results are presented in this paper.

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Quantifying Architectural Impact of Liquid Cooling for 3D Multi-Core Processors

  • Jang, Hyung-Beom;Yoon, Ik-Roh;Kim, Cheol-Hong;Shin, Seung-Won;Chung, Sung-Woo
    • JSTS:Journal of Semiconductor Technology and Science
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    • v.12 no.3
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    • pp.297-312
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    • 2012
  • For future multi-core processors, 3D integration is regarded as one of the most promising techniques since it improves performance and reduces power consumption by decreasing global wire length. However, 3D integration causes serious thermal problems since the closer proximity of heat generating dies makes existing thermal hotspots more severe. Conventional air cooling schemes are not enough for 3D multi-core processors due to the limit of the heat dissipation capability. Without more efficient cooling methods such as liquid cooling, the performance of 3D multi-core processors should be degraded by dynamic thermal management. In this paper, we examine the architectural impact of cooling methods on the 3D multi-core processor to find potential benefits of liquid cooling. We first investigate the thermal behavior and compare the performance of two different cooling schemes. We also evaluate the leakage power consumption and lifetime reliability depending on the temperature in the 3D multi-core processor.

New Cooling Techniques of High Tc Superconductor Systems (고온초전도 시스템의 새로운 냉각기술)

  • Chang, Ho-Myung
    • 한국초전도학회:학술대회논문집
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    • v.9
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    • pp.7-11
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    • 1999
  • The recent progress in new cooling techniques of the high Tc superconductor(HTS) systems is reported and discussed with some practical examples. At the beginning stage of the HTS development in research laboratories, liquid nitrogen(LN$_2$) is the standard medium for an effective cooling. The success of HTS in many different application areas, however, has required a variety of need in the cooling temperature and the cooling capacity with specific design restrictions. While the utilization of alternative liquid cryogens such as liquid neon (LNe) or liquid hydrogen (LH$_2$) has been tired in some of them, even solid cryogens such as solid nitrogen (SN$_2$) or solid hydrogen (SH$_2$) may be another option in special applications. The gaseous helium cooled by a cryogenic refrigerator has also been a good candidate in many cases. One of the best cooling methods for the HTS is the direct conduction-cooling by a closed-cycle refrigerator with no cryogen at all. The refrigeration may be based on Joul-Thomson, Brayton, Stirling, Gifford-McMahon, or pulse tube cycles. The pros and cons of the newly proposed cooling methods are described and some significant design issues are presented.

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Effects of Density Change and Cooling Rate on Heat Transfer and Thermal Stress During Vertical Solidification Process (수직응고 시스템에서 밀도차와 냉각률이 열전달 및 열응력에 미치는 영향)

  • 황기영;이진호
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.19 no.4
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    • pp.1095-1101
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    • 1995
  • Numerical analysis of vertical solidification process allowing solid-liquid density change is performed by a hybrid method between a winite volume method (FVM) and a finite element method (FEM). The investigation focuses on the influence of solid-liquid density change and cooling rates on the motion of solid-liquid interface, solidified mass fraction, temperatures and thermal stresses in the solid region. Due to the density change of pure aluminium, solid-liquid interface moves more slowly but the solidified mass fraction is larger. The cooling rate of the wall is shown to have a significant influence on the phase change heat transfer and thermal stresses, while the density change has a small influence on the motion of the interface, solidified mass fraction, temperature distributions and thermal stresses. As the cooling rate increases, the thermal stresses become higher at the early stage of a solidification process, but it has small influence on the final stresses as the steady state is reached.

A Study on Refrigeration Performance of Vehicle HVAC System for Sub-Cooling Improvement (서브쿨링향상을 위한 차량공조 시스템의 냉방성능에 관한 연구)

  • 박만재
    • Transactions of the Korean Society of Automotive Engineers
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    • v.12 no.1
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    • pp.1-9
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    • 2004
  • The general method which changes sub-cooling of refrigerant is to control the expansion valve in the state of mixing with liquid and gas phase. In this study, the performance of vehicle air conditioning system is to control either changing the expansion valve or adding the sub condenser. Therefore, this research finally is tested in case of the fourth test procedure, the second test was suitable for a valve opening area due to adjusting valve slope in comparison with the other test. The other test except for the second test happened to do liquid back due to the excessively liquified refrigerant into the system. In conclusion, the second test was appeared not to be influenced upon liquid back, and it is to expect positive performance by controlling an expansion valve. Therefore, it will be also useful to research for an increase of compressor efficiency Performance improvement of an air conditioner is to reinforce the suction performance of the evaporator and increase the sub-cooling, which make use of the sub-cooling system.

Experimental Study of Liquid Oxygen Sub-cooling by Helium Injection (헬륨분사를 통한 액체산소 과냉각에 관한 실험적 연구)

  • Kwon Oh-Sung;Cho Nam-Kyung;Chung Yong-Gahp;Ha Seong-Up;Lee Joong-Youp;Kim Hyun-Joong
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • v.y2005m4
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    • pp.179-182
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    • 2005
  • Test of liquid oxygen sub-cooling by helium injection, which is one of the method of temperature conditioning of cryogenic propellant in liquid propulsion rocket, is performed. The sub-cooling effect at different He injection flow rate with the same initial liquid oxygen mass is compared. Test results showed liquid oxygen temperature decrease of $5\sim6^{\circ}C$ under test condition. And the required time for cooling is inversely proportional to He injection flow rate.

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Cooling Performance of Liquid CPU Cooler using Water/PG-based $Al_2O_3$ Nanofluids (물/PG-기반 $Al_2O_3$ 나노유체를 적용한 수냉식 CPU 쿨러의 냉각성능)

  • Park, Y.J.;Kim, K.H.;Lee, S.H.;Jang, S.P.
    • Journal of ILASS-Korea
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    • v.19 no.1
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    • pp.19-24
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    • 2014
  • In this study, the cooling performance of a liquid CPU cooler using the water/propylene glycol(PG)-based $Al_2O_3$ nanofluids is experimentally investigated. Water/PG-based $Al_2O_3$ nanofluids are manufactured by two-step method with ultrasonic energy for 10 hours. The volume fractions of the nanofluids are 0.25% and 0.35%. Thermal conductivity and viscosity of the nanofluids are measured to theoretically predict the thermal performance of the liquid CPU cooler using performance factor. Performance factor results indicate that the cooling performance of the liquid CPU cooler can be improved using the manufactured nanofluids. To evaluate the cooling performance of the liquid CPU cooler experimentally, temperature differences between ambient air and heater are measured for base fluid and nanofluids respectively. Based on the results, it is shown that performance of the liquid CPU cooler using $Al_2O_3$ nanofluids is improved maximum up to 8.6% at 0.25 Vol.%.

A Trade-off Analysis between Combustion and Cooling Performance of a Liquid Rocket Combustor with Fuel Film Cooling Scheme (연료 막냉각을 적용한 액체로켓 연소기의 연소/냉각 성능 간 Trade-off 해석)

  • Joh, Miok;Kim, Seong-Ku;Choi, Hwan-Seok
    • Journal of the Korean Society of Propulsion Engineers
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    • v.16 no.6
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    • pp.16-22
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    • 2012
  • Performance of a liquid rocket thrust chamber with regenerative cooling scheme has been numerically analyzed using in-house CFD code which can predict combustion/cooling performance and provide nozzle design parameters. This paper investigates trade-offs between combustion and cooling performance with varying amount of fuel directly injected into the chamber wall to form cooling films and mixture ratios for the peripheral injectors. Further efforts to verify/improve the simulation methodology including comparison with the firing test results are planned to make it a reliable tool to optimize the film cooling and other major design parameters.

A Trade-off Analysis between Combustion and Cooling Performance of a Liquid Rocket Combustor with Fuel Film Cooling Scheme (연료 막냉각을 적용한 액체로켓 연소기의 연소/냉각 성능 간 trade-off 해석)

  • Joh, Mi-Ok;Kim, Seong-Ku;Choi, Hwan-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2012.05a
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    • pp.35-41
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    • 2012
  • Performance of a liquid rocket thrust chamber with regenerative cooling scheme has been numerically analyzed using in-house CFD code which can predict combustion/cooling performance and provide nozzle design parameters. This paper investigates trade-offs between combustion and cooling performance with varying amount of fuel directly injected into the chamber wall to form cooling films. Also is analyzed the effect of varying mixture ratios for the peripheral injectors on combustion performance enhancement. Further efforts to verify/improve the simulation methodology including comparison with the firing test results are planned to make it a reliable tool to optimize the film cooling and other major design parameters.

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