Low velocity impact resistance of woven fabric reinforced T-shaped composites

被引：0

作者：

Qin Z. ^{[1
]}

Wei X. ^{[1
]}

Hu H. ^{[1
]}

Ouyang Y. ^{[1
]}

Xie J. ^{[2
]}

Gong X. ^{[1
]}

机构：

[1] College of Textile Science and Engineering, Wuhan Textile University, Wuhan

[2] Ministry of Education Key Laboratory for Advanced Textile Composite Material, Tiangong University, Tianjin

来源：

Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinica | 2023年 / 40卷 / 06期

关键词：

composites; finite element method; low velocity impact; T-shaped stiffened plate; three-dimensional fabric;

D O I：

10.13801/j.cnki.fhclxb.20220907.006

中图分类号：

学科分类号：

摘要：

In order to solve the problem of weak interlaminar shear resistance of T-shaped laminate composites, the weaving process of composite preform was reasonably designed, and the T-shaped fabric was woven by SGA598 small sample loom. The T-shaped fabric was prepared by vacuum assisted resin transfer molding (VARTM) process, and its impact resistance under low velocity impact was studied. The geometric and material models were established by using the finite element software ABAQUS to simulate the impact response process under different impact energies. The results show that the T-shaped stiffened plate has high impact resistance, and the simulation results are in good agreement with the experimental results. The finite element model has good reliability. © 2023 Beijing University of Aeronautics and Astronautics (BUAA). All rights reserved.

引用

页码：3673 / 3682

页数：9

共 22 条

[1]

XIAO Yao, LI Dongsheng, JI Kang, Et al., Research and application progress of curing tooling technology for large composite aeronautical components[J], Acta Materiae Compositae Sinica, 39, 3, pp. 907-925, (2022)

[2]

MA Quansheng, LI Xuezhen, WANG Yulin, Et al., Rescarch and progress of 3D stereo fabric composite[J], New Chemical Materials, 49, S1, pp. 279-282, (2021)

[3]

WANG C Z, SU D D, XIE Z F, Et al., Low-velocity impact response of 3D woven hybrid epoxy composites with carbon and heterocyclic aramid fibres[J], Polymer Testing, 101, (2021)

[4]

WEI Fengsheng, Design and application of composite materials in aircraft, Dual Use Technologies & Products, 8, (2015)

[5]

WU Chengsi, LI Qingfei, Study about choice of stiffened structure configuration of laminated composite fuselage, Fiber composites, 33, 2, pp. 3-5, (2016)

[6]

CHEN X, TAYLOR L W, TSAI L J., Three-dimensional fabric structures. Part 1− An overview on fabrication of three-dimensional woven textile preforms for composites, pp. 285-304, (2016)

[7]

CHOU S, CHEN H E., The weaving methods of three-dimensional fabrics of advanced composite materials[J], Composite Structures, 33, 3, pp. 159-172, (1995)

[8]

OUYANG Tian, GUAN Zhidong, TAN Riming, Et al., Experimental study on stiffener impact damage and compression after impact behavior of T-stiffened composite panels, Acta Materiae Compositae Sincia, 35, 10, pp. 2689-2697, (2018)

[9]

CUI Yongjiang, WANG Bintuan, ZHAO Zhanwen, Research on the post-buckling bearing capacity of T-type composite stiffened panel, Composites Science and Engineering, 2021, 7, pp. 22-27

[10]

JIA Jiale, Investigation on low velocity impact and residual compressive properties of reinforced composite skin, (2021)

← 1 2 3 →