黄安畏,吴永鹏,李忠盛,李晓晖,吴道勋,孙彩云,舒露,花泽荟,蒋龙.内饰材料发射率对密封舱室热防护效率的影响[J].装备环境工程,2020,17(8):58-62. HUANG An-wei,WU Yong-peng,LI Zhong-sheng,LI Xiao-hui,WU Dao-xun,SUN Cai-yun,SHU Lu,HUA Ze-hui,JIANG Long.Effect of Interior Material Emissivity on Thermal Insulation Efficiency of Sealed Cabin[J].Equipment Environmental Engineering,2020,17(8):58-62.
内饰材料发射率对密封舱室热防护效率的影响
Effect of Interior Material Emissivity on Thermal Insulation Efficiency of Sealed Cabin
投稿时间:2020-02-10  修订日期:2020-03-20
DOI:10.7643/issn.1672-9242.2020.08.009
中文关键词:  辐射传热  参与性介质  发射率  平均温度
英文关键词:radiative heat transfer  participating medium  emissivity  average temperature
基金项目:
作者单位
黄安畏 西南技术工程研究所,重庆 400039 
吴永鹏 西南技术工程研究所,重庆 400039 
李忠盛 西南技术工程研究所,重庆 400039 
李晓晖 西南技术工程研究所,重庆 400039 
吴道勋 西南技术工程研究所,重庆 400039 
孙彩云 西南技术工程研究所,重庆 400039 
舒露 西南技术工程研究所,重庆 400039 
花泽荟 西南技术工程研究所,重庆 400039 
蒋龙 西南技术工程研究所,重庆 400039 
AuthorInstitution
HUANG An-wei Southwest Technology and Engineering Research Institute, Chongqing 400039, China 
WU Yong-peng Southwest Technology and Engineering Research Institute, Chongqing 400039, China 
LI Zhong-sheng Southwest Technology and Engineering Research Institute, Chongqing 400039, China 
LI Xiao-hui Southwest Technology and Engineering Research Institute, Chongqing 400039, China 
WU Dao-xun Southwest Technology and Engineering Research Institute, Chongqing 400039, China 
SUN Cai-yun Southwest Technology and Engineering Research Institute, Chongqing 400039, China 
SHU Lu Southwest Technology and Engineering Research Institute, Chongqing 400039, China 
HUA Ze-hui Southwest Technology and Engineering Research Institute, Chongqing 400039, China 
JIANG Long Southwest Technology and Engineering Research Institute, Chongqing 400039, China 
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中文摘要:
      目的 探究密封舱室热防护效率与其内饰材料表面发射率的关系,分析内饰材料发射率对其表面温度、舱室内温度的影响规律。方法 采用自行设计的小型密封舱室和加热测量装置,对内饰材料表面及舱室内温度进行测量。结果 当内饰材料发射率为0.09时,内饰表面温度为141.2 ℃,舱室内平均温度仅为90.8 ℃;内饰材料发射率为0.91时,内饰表面温度为124.4 ℃,舱室内平均温度为109.1 ℃。结论 试样表面温度随材料发射率的提高而降低,舱室内部空气平均温度随材料发射率的提高而升高;试样表面温度与舱室空气平均温度的温度差随材料发射率的提高而减小;同时,相同试样表面温度与舱室平均温度的温度差随加热温度的提高而增加。
英文摘要:
      The work aims to explore the relationship between thermal protection efficiency of sealed cabin and surface emissivity of interior materials, and analyze the influence of emissivity of interior materials on surface temperature and cabin temperature. A small sealed cabin and heating measuring device were designed to measure the surface temperature of interior materials and the interior temperature of cabin. When the emissivity of interior materials was 0.09, the interior surface temperature was 141.2 ℃, and the average temperature in the cabin was only 90.8 ℃. When the emissivity of interior materials was 0.91, the interior surface temperature was 124.4 ℃ and the average temperature in the cabin was 109.1 ℃. The surface temperature of specimen decreases with the increase of material emissivity, but the average air temperature of the cabin increases with the increase of material emissivity. The temperature difference between the surface temperature of the specimen and the average air temperature of the sealed cabin decreases with the increase of material emissivity. Meanwhile, the temperature difference between the surface temperature of the same specimen and the average temperature of the cabin increases as the heating temperature rises.
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