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    Effective Thermal Conductivity Model of Micron Hollow Sphere or Phase Change Material/Opacifier-SiO2 Aerogel Composites

    Source: ASME Journal of Heat and Mass Transfer:;2023:;volume( 145 ):;issue: 006::page 62501-1
    Author:
    Pang, Hao-Qiang
    ,
    Fan, Ting-Hui
    ,
    Zhang, Sheng-Nan
    ,
    Gao, Yan-Feng
    DOI: 10.1115/1.4056367
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Pure SiO2 aerogel has a strong light transmittance in the infrared wavebands from 3.0 to 8.0 μm, and an opacifier could efficiently reduce aerogel's radiative thermal conductivity (λr), especially at high temperatures (>400 K). Consequently, the λr of different core/shell structured opacifiers is proposed, including micron hollow sphere opacifier (MHSOP), i.e., hollow carbon black/SiC/TiO2, and phase change material (PCM)/opacifier, i.e., VO2/SiO2, and Ge2Sb2Te5/SiC; further, their conductive λ model has also been established. The results showed that MHSOP could reduce MHSOPs-SiO2 aerogel composite's λ compared to traditional solid structure opacifiers; the effect of MHSOPs with a certain core–shell ratio on suppressing thermal radiation is equivalent to their solid structure opacifier at high-temperature. Adding SiC MHSOPs reduces aerogel composites' weight and thermal conductivity by 42.19 and 26.29%, while the shading effect of a core–shell ratio of over 0.75 is equivalent to the solid structure. Specifically, rutile-phased VO2/SiO2's λr is smaller than TiO2 MHOSP, and crystalline Ge2Sb2Te5/SiC doped aerogel exhibits good thermal insulation. The proposed micron hollow sphere opacifier and PCM/opacifier provide a novelty, lightweight, and high-efficiency method to restrain aerogel's infrared radiation and improve insulation performance at high temperatures.
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      Effective Thermal Conductivity Model of Micron Hollow Sphere or Phase Change Material/Opacifier-SiO2 Aerogel Composites

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4294374
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    contributor authorPang, Hao-Qiang
    contributor authorFan, Ting-Hui
    contributor authorZhang, Sheng-Nan
    contributor authorGao, Yan-Feng
    date accessioned2023-11-29T18:46:20Z
    date available2023-11-29T18:46:20Z
    date copyright1/12/2023 12:00:00 AM
    date issued1/12/2023 12:00:00 AM
    date issued2023-01-12
    identifier issn2832-8450
    identifier otherht_145_06_062501.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4294374
    description abstractPure SiO2 aerogel has a strong light transmittance in the infrared wavebands from 3.0 to 8.0 μm, and an opacifier could efficiently reduce aerogel's radiative thermal conductivity (λr), especially at high temperatures (>400 K). Consequently, the λr of different core/shell structured opacifiers is proposed, including micron hollow sphere opacifier (MHSOP), i.e., hollow carbon black/SiC/TiO2, and phase change material (PCM)/opacifier, i.e., VO2/SiO2, and Ge2Sb2Te5/SiC; further, their conductive λ model has also been established. The results showed that MHSOP could reduce MHSOPs-SiO2 aerogel composite's λ compared to traditional solid structure opacifiers; the effect of MHSOPs with a certain core–shell ratio on suppressing thermal radiation is equivalent to their solid structure opacifier at high-temperature. Adding SiC MHSOPs reduces aerogel composites' weight and thermal conductivity by 42.19 and 26.29%, while the shading effect of a core–shell ratio of over 0.75 is equivalent to the solid structure. Specifically, rutile-phased VO2/SiO2's λr is smaller than TiO2 MHOSP, and crystalline Ge2Sb2Te5/SiC doped aerogel exhibits good thermal insulation. The proposed micron hollow sphere opacifier and PCM/opacifier provide a novelty, lightweight, and high-efficiency method to restrain aerogel's infrared radiation and improve insulation performance at high temperatures.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEffective Thermal Conductivity Model of Micron Hollow Sphere or Phase Change Material/Opacifier-SiO2 Aerogel Composites
    typeJournal Paper
    journal volume145
    journal issue6
    journal titleASME Journal of Heat and Mass Transfer
    identifier doi10.1115/1.4056367
    journal fristpage62501-1
    journal lastpage62501-11
    page11
    treeASME Journal of Heat and Mass Transfer:;2023:;volume( 145 ):;issue: 006
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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