
Curing Kinetics of Epoxy Resin for General Aviation Aircraft Composites
DING Zhen-yuan, CHEN Shu-xian
Curing Kinetics of Epoxy Resin for General Aviation Aircraft Composites
In order to obtain the curing kinetic equation and curing kinetic parameters of thermosetting epoxy resin for general aviation aircraft, the non-isothermal test of thermosetting epoxy resin was carried out by differential scanning calorimetry (DSC) at different heating rates, and the curing kinetic properties of thermosetting epoxy resin were obtained by fitting the numerical values of the experimental curve. The Ozawa-Wall-Flynn (OWF) and Kissinger-Akahira-Sunose (KAS) methods were used to determine the activation energy, and the change of apparent activation energy with the degree of curing was studied. Based on the Málek method, the curing reaction mechanism was analyzed, and the results showed that the curing behavior of the resin was in line with the Sestak-Berggren autocatalytic model. The pre-index factor (A) and reaction order (m, n) were determined by nonlinear fitting (LSR), and the curing kinetic model was established. The curing reaction rate-curing degree curve predicted by the model was compared with the experimental results, and the results showed that the predicted values of the model were basically consistent with the experimental values. Therefore, the curing kinetic model obtained can accurately describe the curing reaction process of the resin. The research work provides a reference for the manufacturing and repair process of composite materials for general aviation aircraft, and the formulation of curing process parameters.
Non-isothermal differential scanning calorimetry / Thermosetting epoxy resin / Curing kinetics / Self-catalytic model
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3 |
陈杰,马春柳,刘邦,等.热固性树脂及其固化剂的研究进展[J].塑料科技,2019,47(2):95-102.
|
4 |
|
5 |
|
6 |
|
7 |
|
8 |
杨帆,粟俊华,胡亚坤,等.环氧封端聚苯醚/环氧树脂共混体系的固化动力学研究[J].塑料科技,2023,51(4):54-58.
|
9 |
王哲,祖愿,胡方圆,等.含杂萘联苯结构的环氧树脂固化动力学分析[J].化工学报,2022,73(2):681-688.
|
10 |
高腾龙,余建虎,许英杰.碳纤维/环氧树脂预浸料固化动力学建模研究[J].机械科学与技术,2022,41(7):1128-1135.
|
11 |
|
12 |
|
13 |
|
14 |
|
15 |
|
16 |
|
17 |
|
18 |
|
19 |
|
20 |
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