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中国航空科学基金(2011ZF77010)

作品数:2 被引量:37H指数:2
相关作者:杨宇明杨宏林谭惠丰刘宇艳刘羽熙更多>>
相关机构:哈尔滨工业大学中国航天科工集团公司中国科学院更多>>
发文基金:中国航空科学基金教育部“新世纪优秀人才支持计划”国家自然科学基金更多>>
相关领域:航空宇航科学技术一般工业技术理学更多>>

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Thermal Stability,Thermal Decomposition and Mechanism Analysis of Cycloaliphatic Epoxy/4,4'-dihydroxydiphenylsulfone/Aluminum Complexes Latent Resin Systems被引量:2
2012年
The thermal stability of latent resin systems, cycloaliphatic epoxy/4,4'- dihydroxydiphenylsulfone/aluminum complexes, was investigated by dynamic differential scanning calorimetry (DSC) analysis. Experiments were conducted under non-isothermal condition in a nitrogen atmosphere at the heating rate of 10, 20, 30 and 40 ℃/min, respectively. TG curves showed that, in the temperature range of 25 to 600 ℃, the stability of the resin systems could be enhanced by increasing the length of the aliphatic chain in the initiator. Both the Kissinger method and the Ozawa-Flyrm-Wall method were employed to calculate activation energies of the decomposition reaction, and the values obtained from the two methods were compared. Moreover, the corresponding reaction mechanism was identified by the Achar differential method and the Coats- Redfem integral method. The experimental results showed that these four methods were reliable and effective to study the kinetics of the thermal decomposition reaction; and the most probable thermal decomposition mechanism of the resin systems we proposed was found to comply with Mampel power law (m=1).
吴松全LIU Shaozhu刘宇艳ZHU QiWEI Huige
临近空间飞艇蒙皮材料研究进展和需求分析被引量:35
2012年
临近空间飞艇具有大范围不间断的高效信息获取与传输能力,是近期国际上竞相发展的未来信息平台。蒙皮材料是临近空间飞艇的主要材料,其质量和性能决定了飞艇的大小、寿命和成本,是发展临近空间飞艇的基础。本文中针对临近空间飞艇蒙皮材料选取和应用存在的若干困难,从蒙皮材料工程需求出发,对蒙皮材料的强度、耐候性、阻隔性和试验评价方法等方面的研究现状进行总结和分析,讨论未来高性能临近空间飞艇蒙皮材料的研究发展方向。
谭惠丰刘羽熙刘宇艳杨宏林杨宇明施雷
关键词:飞艇蒙皮织物复合材料平流层
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