王荣华,王小燕,李 晖,刘亚平,王新波,李倩倩,孙 岩.白炭黑补强氟硅橡胶热空气老化机理研究[J].装备环境工程,2015,12(2):10-14,38. WANG Rong-hua,WANG Xiao-yan,LI Hui,LIU Ya-ping,WANG Xin-bo,LI Qian-qian,SUN Yan.Study on the Hot Air Aging Mechanism of Silica Reinforced Fluorosilicone Rubber[J].Equipment Environmental Engineering,2015,12(2):10-14,38.
白炭黑补强氟硅橡胶热空气老化机理研究
Study on the Hot Air Aging Mechanism of Silica Reinforced Fluorosilicone Rubber
投稿时间:2014-12-30  修订日期:2015-04-15
DOI:10.7643/issn.1672-9242.2015.02.003
中文关键词:  白炭黑补强氟硅橡胶  热空气老化  微观结构  老化机理
英文关键词:silica reinforced fluorosilicone rubber  hot air aging  microcosmic structure  aging mechanism
基金项目:国防科技工业技术基础科研项目 (JSHS2014208B003;H092012C002)
作者单位
王荣华 中国兵器工业集团第五三研究所,济南 250031 
王小燕 西北大学,西安 710127 
李 晖 中国兵器工业集团第五三研究所,济南 250031 
刘亚平 中国兵器工业集团第五三研究所,济南 250031 
王新波 中国兵器工业集团第五三研究所,济南 250031 
李倩倩 中国兵器工业集团第五三研究所,济南 250031 
孙 岩 中国兵器工业集团第五三研究所,济南 250031 
AuthorInstitution
WANG Rong-hua Norinco Group Institute 53, Jinan 250031, China 
WANG Xiao-yan Northwest University, Xi′ an 710127, China 
LI Hui Norinco Group Institute 53, Jinan 250031, China 
LIU Ya-ping Norinco Group Institute 53, Jinan 250031, China 
WANG Xin-bo Norinco Group Institute 53, Jinan 250031, China 
LI Qian-qian Norinco Group Institute 53, Jinan 250031, China 
SUN Yan Norinco Group Institute 53, Jinan 250031, China 
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中文摘要:
      目的 研究热空气老化过程中白炭黑补强氟硅橡胶的老化机理。方法 开展不同加速老化温度点下白炭黑补强氟硅橡胶热空气老化试验, 对老化过程中材料的力学性能进行研究, 同时采用热重分析、 衰减全反射红外光谱、 交联密度分析以及固体核磁等技术, 对200 ℃热空气老化过程中材料的微观结构变化进行分析。结果 低温环境中白炭黑氟硅橡胶拉伸强度和扯断伸长率变化较小, 高温环境中变化趋势增大, 邵尔A硬度在整个老化过程中没有明显变化。结论 白炭黑补强氟硅橡胶的老化机理主要是交联键的断裂和侧链三氟丙基的分解, 同时还可能伴随有部分主链的破坏。
英文摘要:
      Objective To study the hot air aging mechanism of silica reinforced fluorosilicone rubber. Methods Hot air aging experiments of silica reinforced fluorosilicone rubber were conducted at different accelerated aging temperature, and the mechanical properties of the material during the aging process were studied. Meanwhile, thermal analysis, ATR-FTIR, XPS, and crosslink density tester were used to investigate the microstructure changes of fluorosilicone rubber during the 200℃ hot air aging process. Results The tensile strength and elongation retention rate at break changed slightly in low-temperature environment, while the changing trend increased in high-temperature environment. The Shore A hardness did not show significant changes during the whole aging process. Conclusion The possible aging mechanism of fluorosilicone rubber could be crosslink destruction, trifluoropropyl decomposition in side chain and partial fracture in main chain.
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