极限氧指数
环氧树脂
纳米复合材料
阻燃剂
材料科学
热稳定性
复合材料
动态力学分析
玻璃化转变
抗弯强度
聚合物
涂层
相容性(地球化学)
弯曲模量
化学工程
烧焦
工程类
热解
作者
Hong Zhang,Jie Mao,Min Li,Qipeng Cai,Weihang Li,Chuhong Huang,Conghui Yuan,Yiting Xu,Birong Zeng,Lizong Dai
标识
DOI:10.1016/j.compositesa.2019.105751
摘要
In this report, we develop a simple and controllable coating strategy to decorate h-BN with a cyclotriphosphazene-containing boronate polymer (CPBP), thus forming [email protected] core-shell nanoplates with different shell thicknesses. By introducing [email protected] into epoxy resin (EP), we have found that the thermal stability, flame retardant and mechanical performances of the as formed nanocomposites greatly relies on the CPBP shell thickness. Also, our design effectively improve the compatibility between h-BN nanoplates and polymer matrix and regulate the corresponding interface. The nanocomposites show the highest limiting oxygen index (LOI) of 28.7% and reach V-0 rating in the vertical burning test at loading amount of 2.5 wt%. Also the heat and smoke releases of nanocomposites during burning are significantly reduced. The flexural strengths and modulus of the nanocomposites are at most 42.12% and 27.85% higher than that of pure EP. The glass transition temperature and dynamic mechanical property of the nanocomposites are both improved.
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