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Effects of different thermal-oxidative environments on mechanical properties of T800 carbon fiber/epoxy resin composites |
Yaoxiong JIA1, Liang XU2,*( ), Qingyang AO1, Wenzheng ZHANG1, Tao WANG1, Juan WEI1 |
1 Aviation Industrial Chengdu Aircraft Industrial (Group) Co., Ltd., Chengdu 610091, China 2 College of Electromechanical Engineering, Shenyang Aerospace University, Shenyang 110136, China |
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Abstract Different thermal-oxidative environments (70, 130 ℃ and 190 ℃) have important effects on the properties of carbon fiber composites. The mass loss characteristics of T800 carbon fiber/epoxy resin composites under different thermal-oxidative environments were analyzed, and the surface morphology, infrared spectra, dynamic mechanical properties and interlaminar shear properties of T800 carbon fiber/epoxy resin composites before and after aging were compared. The results show that in the initial stage of thermal-oxidative aging, the mass loss rate is increased rapidly, and the higher the aging temperature, the faster the mass loss. The extent of damage sample surface morphology is gradually increased with the increasing of thermal-oxidative temperature, after aging at 190 ℃, the resin on the fiber surface falls off seriously, the cracks and gaps appear between the fibers, and there is no resin filling, at this aging temperature, the sample has an irreversible chemical change. The glass transition temperature of the sample is increased with the increase of aging temperature, but the internal friction is decreased at first, then increased and then decreased. After thermal-oxidative aging at 70, 130 ℃ and 190 ℃, the shear strength of the samples is increased by 6.0%, 13.7% and 2.1%, respectively. The relevant test results and phenomena can provide data reference for the follow-up study of the new domestic T800 carbon fiber/epoxy composites.
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Received: 21 July 2021
Published: 18 April 2022
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Corresponding Authors:
Liang XU
E-mail: sysyxu@163.com
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Quality change curves under different aging environments
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SEM images under different aging environments (a)unaged; (b)70 ℃; (c)130 ℃; (d)190 ℃
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Infrared spectra of T800 carbon fiber/epoxy composites under different aging environments
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DMA curves under different aging environments
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Aging environment | Maximumbreaking load/N | Shear strength/MPa | Unaged | 854 | 62.1 | 70 ℃ thermal-oxidative aging | 906 | 65.8 | 130 ℃ thermal-oxidative aging | 972 | 70.6 | 190 ℃ thermal-oxidative aging | 872 | 63.4 |
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Influence of different aging environments on interlayer shear property of T800 carbon fiber composites
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