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Licensed Unlicensed Requires Authentication Published by De Gruyter August 30, 2019

Hygrothermal environment effects on mechanical properties of T700/3228 CFRP laminates

  • Zhenyu Feng , Haolei Mou , Jiang Xie and Tianchen Gong
From the journal Materials Testing

Abstract

Exposure to a hygrothermal environment would cause severe degradation of the mechanism properties of carbon fiber reinforced polymer (CFRP) laminates. The moisture absorption characteristics of T700/3228 CFRP laminates was studied through moisture absorption tests. The effects on the tensile and compression properties of [0]16 and [90]16 specimens under various hygrothermal conditions were comparative analyzed, and the degradation mechanisms of tensile and compression properties were further researched by microstructure characterization. The results show that under dry conditions, matrix strength increases with rising of temperature because of post-curing of epoxy at high temperatures. At 85 % RH (relative humidity), the strength of CFRP laminates decrease entirely with rising temperature because of the thermal and moisture stress generated at the interface. At a water temperature of 70 °C, the proprieties of CFRP laminates decrease severely.


Correspondence Address, Prof. Dr. Zhenyu Feng, Key Laboratory of Civil Aircraft Airworthiness Technology, CAAC, No. 2898, Jinbei Road, Dongli District, Tianjin 300300 P. R. China, E-mail:

Prof. Zhenyu Feng, Ph.D., born in 1966, received his Ph.D. in Solid Mechanics at the Northwestern Polytechnical University in 1995. He is currently working on structural strength and fatigue fracture mechanics at the Key Laboratory of Civil Aircraft Airworthiness Technology, CAAC, Tianjin, China.

Jiang Xie, Ph.D., born in 1982, received his Ph.D. in Solid Mechanics at the Northwestern Polytechnical University in 2012. He is currently working on impact dynamics as Associate Researcher at the Key Laboratory of Civil Aircraft Airworthiness Technology, CAAC, Tianjin, China.

Haolei Mou, MSc., born in 1987, received his Master's degree in Aircraft Design at the Civil Aviation University of China in 2013 and is currently engaged in structure and material related research at the Key Laboratory of Civil Aircraft Airworthiness Technology, CAAC, Tianjin, China.

Tianchen Gong, MSc-, born in 1990, received her Master's degree in Aircraft Design at the Civil Aviation University of China in 2017. She is currently engaged in structure and material related research at the Key Laboratory of Civil Aircraft Airworthiness Technology, CAAC, Tianjin, China.


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Published Online: 2019-08-30
Published in Print: 2019-08-30

© 2019, Carl Hanser Verlag, München

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