• Title/Summary/Keyword: 소형 히트 파이프

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Application of Miniature Heat Pipe for Notebook PC Cooling (노트북 PC CPU 냉각용 소형 히트파이프 Packaging 연구)

  • Moon, Seok-Hwan;Hwang, Gunn;Choy, Tae-Goo
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.25 no.6
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    • pp.799-803
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    • 2001
  • Miniature heat pipe(MHP) with woven-wired wick was used to cool the CPU of a notebook PC. The pipe with circular cross-section was pressed and bent for packaging the MHP into a notebook PC with very limited compact packaging space. A cross-sectional area of the pipe is reduced about 30% as the MHP with 4mm diameter is pressed to 2mm thickness. In the present study a performance test has been performed in order to review varying of operating performance according to pressed thickness variation and heat dissipation capacity of MHP cooling module that is packaged on a notebook PC. New wick type was considered for overcoming low heat transfer limit when MHP is pressed to thin-plate. The limiting thickness or pressing is shown to be within the range of 2mm∼2.5mm through the performance test with varying the pressing thickness. When the wall thickness of 0.4mm is reduced to 0.25mm for minimizing conductive thermal resistance through the wall of heat pipe, heat transfer limit and thermal resistance of MHP were improved about 10%. In the meantime, it is shown that the thermal resistance and heat transfer limit for the MHP with central wick type are higher than those of MHP with existing wick types. The results of performance test for MHP cooling modules with woven-wired wick to cool a notebook PC shows the stability as cooling system since T(sub)j(Temperature of Processor Junction) satisfy a demand condition of 0∼100$\^{C}$ under 11.5W of CPU heat.

Performance and Availability of Seawater Distiller with Heat Pipe Utilizing Low-Grade Waste Heat (저급 폐열 이용 히트파이프 해수담수기의 성능과 유용성)

  • Park, Chang-Dae;Chung, Kyung-Yul;Tanaka, Hiroshi
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.37 no.1
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    • pp.81-86
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    • 2013
  • Exhaust gas from a small portable electric generator is simply exhausted to the surroundings because the capacity and quality of the waste heat of this gas is generally not sufficient to recover and utilize. We have proposed a seawater distiller utilizing the thermal energy of waste gas from an electric generator. The distiller recovers heat from the waste gas by means of a heat pipe and uses it effectively through a multiple-effect diffusion-type structure. We constructed an experimental apparatus with a vertical single-effect still having a 4-stroke 50 cc generator engine and found that the experimental results for distillate productivity show good agreement with the theoretical predictions. The results show that the distiller can recover 52 W of waste heat from the gas at $171^{\circ}C$, and ~85% of the recovered heat can be utilized for distillation to produce 70 g/h of fresh water. This is equivalent to a productivity of 500 g/h in the case of a 10-effect still. Therefore, the proposed distiller should be useful in remote areas where electricity and water grids are inadequate.

Preliminary System Design of STEP Cube Lab. for Verification of Fundamental Space Technology (우주기반기술 검증용 극초소형 위성 STEP Cube Lab.의 시스템 개념설계)

  • Kwon, Sung-Cheol;Jung, Hyun-Mo;Ha, Heon-Woo;Han, Sung-Hyun;Lee, Myung-Jae;Jeon, Su-Hyeon;Park, Tae-Young;Kang, Su-Jin;Chae, Bong-Gun;Jang, Su-Eun;Oh, Hyun-Ung;Han, Sang-Hyuk;Choi, Gi-Hyuk
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.42 no.5
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    • pp.430-436
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    • 2014
  • The mission objective of STEP Cube Lab. (Cube Laboratory for Space Technology Experimental Project) classified as a pico-class satellite is to verify the technical effectiveness of payloads such as variable emittance radiator, SMA washer, oscillating heat pipe and MEMS based solid propellant thruster researched at domestic universities. In addition, the MEMS concentrating photovoltaic power system and the non-explosive holding and separation mechanism with the advantages of high constraint force and low shock level will be developed as the primary payloads for on-orbit verification. In this study, the feasibility of the mission actualization has been confirmed by the preliminary system design.