一种新型蜂窝夹层结构防热材料
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航天材料及工艺研究所

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Novel Honeycomb Sandwich Thermal Protection Materials
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    摘要:

    针对实际使用的热环境要求,提出了多种防热结构材料及结构方案。通过石英灯加热试验对其
    防热性能进行了考核验证。考察了防热涂层、样件结构形式以及材料种类对试验件防热性能的影响。结果表
    明,防热涂层可显著降低防热试验件的背温,最高降幅达241益;相对于传统的玻璃纤维/ 酚醛层压板结构,在
    满足防热要求的同时,新型蜂窝夹层结构的面密度较低,仅为层压板的50% 左右,具有明显的减重优势,其中
    聚酰亚胺面板的蜂窝夹层结构的面密度仅为酚醛玻璃钢面板夹层结构的80%,其表面加防热涂层样件的背温
    仅为246益。

    Abstract:

    Several thermal protection methods were proposed according to the thermal environment requirements
    in application. The thermal insulation property of different thermal protection materials and structures was tested by
    the quartz radiation heating method. The effects of thermal protection coating, structure and material on the thermal
    insulation property were investigated. Results show that the thermal protection coating can significantly lower the back
    temperature of the sample. Compared to the general glass fabric reinforced phenolic resin laminate panel, the sand鄄
    wich test panel prepared by glass fabric honeycomb and polyimide composite panel has lighter weight and good thermal
    insulation property. The area weight of honeycomb sandwich was only 50% of the laminate panel. And the area
    weight of sandwich with polyimide composite panel was about 80% of sandwich with phenolic composite panel. The
    back temperature of sandwich with polyimide panel covered by the thermal protection coating was only 246益.

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潘玲英.一种新型蜂窝夹层结构防热材料[J].宇航材料工艺,2012,42(5).

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  • 在线发布日期: 2016-11-28
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