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    Effect of Direct Liquid Cooling Technology With Flow Guide Integration on Avionics Devices Thermal and Electrical Performance

    Source: Journal of Thermal Science and Engineering Applications:;2022:;volume( 015 ):;issue: 002::page 21004-1
    Author:
    Qi, Wenliang
    ,
    Liu, Tingting
    ,
    Zhang, Zichun
    ,
    Wang, Bin
    ,
    Liu, Qi
    ,
    Xu, Yingjie
    DOI: 10.1115/1.4055862
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: With the application of various high-power electronic devices to improving aircraft comprehensive performance, there has been a significant interest in the use of high heat flux dissipation technology to maintain an effective and safe operation for electronic devices. This article presents a numerical study on the thermal and electrical performance of the avionics server module by using single-phase immersion cooling technology with flow distributor and investigates the influence of heat dissipation capacity on the thermal performance of the avionics server module and DC IR-drop of printed circuit board power distribution network (PDN). The simulation results showed that a higher dielectric fluid flowrate can be provided b flow distributor with the same pumping power, and the maximum temperature of the hot spot was 4–8 °C lower than the module without a flow distributor. The result confirmed the improved flow performance and enhances heat transfer of the hot spot for the module with a flow distributor. However, the module without the flow distributor showed better comprehensive cooling performance with about 10–15% reduction in average Nusselt number with an increase in Re. The discrepancy of PDN DC IR-drop under different Re values was constant at 3% for different design geometries, which means the effect of the flow distributor on power delivery capability can be neglected.
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      Effect of Direct Liquid Cooling Technology With Flow Guide Integration on Avionics Devices Thermal and Electrical Performance

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4291404
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    • Journal of Thermal Science and Engineering Applications

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    contributor authorQi, Wenliang
    contributor authorLiu, Tingting
    contributor authorZhang, Zichun
    contributor authorWang, Bin
    contributor authorLiu, Qi
    contributor authorXu, Yingjie
    date accessioned2023-08-16T18:05:53Z
    date available2023-08-16T18:05:53Z
    date copyright11/8/2022 12:00:00 AM
    date issued2022
    identifier issn1948-5085
    identifier othertsea_15_2_021004.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4291404
    description abstractWith the application of various high-power electronic devices to improving aircraft comprehensive performance, there has been a significant interest in the use of high heat flux dissipation technology to maintain an effective and safe operation for electronic devices. This article presents a numerical study on the thermal and electrical performance of the avionics server module by using single-phase immersion cooling technology with flow distributor and investigates the influence of heat dissipation capacity on the thermal performance of the avionics server module and DC IR-drop of printed circuit board power distribution network (PDN). The simulation results showed that a higher dielectric fluid flowrate can be provided b flow distributor with the same pumping power, and the maximum temperature of the hot spot was 4–8 °C lower than the module without a flow distributor. The result confirmed the improved flow performance and enhances heat transfer of the hot spot for the module with a flow distributor. However, the module without the flow distributor showed better comprehensive cooling performance with about 10–15% reduction in average Nusselt number with an increase in Re. The discrepancy of PDN DC IR-drop under different Re values was constant at 3% for different design geometries, which means the effect of the flow distributor on power delivery capability can be neglected.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEffect of Direct Liquid Cooling Technology With Flow Guide Integration on Avionics Devices Thermal and Electrical Performance
    typeJournal Paper
    journal volume15
    journal issue2
    journal titleJournal of Thermal Science and Engineering Applications
    identifier doi10.1115/1.4055862
    journal fristpage21004-1
    journal lastpage21004-9
    page9
    treeJournal of Thermal Science and Engineering Applications:;2022:;volume( 015 ):;issue: 002
    contenttypeFulltext
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