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用于航空航天和太空应用的可持续高性能环氧热固性材料的开发。

Development of Sustainable High Performance Epoxy Thermosets for Aerospace and Space Applications.

作者信息

Dinu Roxana, Lafont Ugo, Damiano Olivier, Mija Alice

机构信息

Université Côte d'Azur, Institut de Chimie de Nice, 06108 Nice, France.

ESA, ESTEC, Keplerlaan 1, P.O. Box 299, NL-2200 AG Noordwijk, The Netherlands.

出版信息

Polymers (Basel). 2022 Dec 14;14(24):5473. doi: 10.3390/polym14245473.

Abstract

There is an imperative need to find sustainable ways to produce bisphenol A free, high performance thermosets for specific applications such as the space or aerospace areas. In this study, an aromatic tris epoxide, the tris(4-hydroxyphenyl)methane triglycidyl ether (THPMTGE), was selected to generate high crosslinked networks by its copolymerization with anhydrides. Indeed, the prepared thermosets show a gel content () ~99.9% and glass transition values ranged between 167-196 °C. The thermo-mechanical properties examined by DMA analyses reveal the development of very hard materials with ' ~3-3.5 GPa. The thermosets' rigidity was confirmed by Young's moduli values which ranged between 1.25-1.31 GPa, an elongation at break of about 4-5%, and a tensile stress of ~35-45 MPa. The TGA analyses highlight a very good thermal stability, superior to 340 °C. The Limit Oxygen Index () parameter was also evaluated, showing the development of new materials with good flame retardancy properties.

摘要

迫切需要找到可持续的方法来生产无双酚A的高性能热固性材料,用于空间或航空航天等特定领域。在本研究中,选择了一种芳香族三环氧,即三(4-羟苯基)甲烷三缩水甘油醚(THPMTGE),通过其与酸酐的共聚反应生成高度交联的网络。实际上,制备的热固性材料显示出凝胶含量()约为99.9%,玻璃化转变温度在167-196°C之间。通过DMA分析检测的热机械性能表明,所制备的材料非常坚硬,储能模量(')约为3-3.5 GPa。热固性材料的刚性通过杨氏模量值得到证实,杨氏模量值在1.25-1.31 GPa之间,断裂伸长率约为4-5%,拉伸应力约为35-45 MPa。TGA分析突出了其非常好的热稳定性,优于340°C。还评估了极限氧指数()参数,结果表明开发出了具有良好阻燃性能的新材料。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/476d/9785596/ca723f274606/polymers-14-05473-g001.jpg

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