Impact characteristics of composite panel stitched by I-fiber process

被引:35
作者
Kim, Cheol-Hwan [1 ]
Sim, Hyung-Woo [1 ]
An, Woo-Jin [1 ]
Kweon, Jin-Hwe [1 ]
Choi, Jin-Ho [1 ]
机构
[1] Gyeongsang Natl Univ, Res Ctr Aircraft Parts Technol, Sch Mech & Aerosp Engn, 900 Gajwa Dong, Jinju 660701, Gyeongnam, South Korea
基金
新加坡国家研究基金会;
关键词
I-fiber; Stitching; Impact test; Z-pinning; LOW-VELOCITY IMPACT; T-JOINTS; COMPRESSION; RESISTANCE; STRENGTH; CFRP; PERFORMANCE; BEHAVIOR;
D O I
10.1016/j.compositesa.2019.105644
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Impact damage generated during manufacturing processes or operations are undetectable by the naked eye, hard to repair, and decrease the lifetime of a product. The damage area can be reduced by reinforcing the z-directional strength. Z-pinning and stitching are typical z-directional reinforcement methods. The I-fiber stitching process is a very promising technology that combines the advantages of Z-pinning and a conventional stitching process. In this paper, composite panels stitched by the I-fiber process were manufactured, and impact tests were performed. The damage areas and compressive strengths after impact were measured and compared with an unstitched panel. A reinforcing area of 50 x 50 mm was reinforced in a composite panel having a stacking sequence of [45/0/ - 45/90](3s), and the impact tests of six composite panels with different stitching densities and patterns were tested and evaluated.
引用
收藏
页数:8
相关论文
共 21 条
[1]   Static strength of RTM composite joint with I-fiber stitching process [J].
An, Woo-Jin ;
Kim, Cheol-Hwan ;
Choi, Jin-Ho ;
Kweon, Jin-Hwe .
COMPOSITE STRUCTURES, 2019, 210 :348-353
[2]   Characterization of fracture modes in stitched and unstitched cross-ply laminates subjected to low-velocity impact and compression after impact loading [J].
Aymerich, F. ;
Priolo, P. .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2008, 35 (07) :591-608
[3]   Damage mechanisms in thin stitched laminates subjected to low-velocity impact [J].
Aymerich, F. ;
Francesconi, L. .
INTERNATIONAL SYMPOSIUM ON DYNAMIC RESPONSE AND FAILURE OF COMPOSITE MATERIALS (DRAF2014), 2014, 88 :133-140
[4]   Ballistic impact behaviour of stitched graphite/epoxy laminates [J].
Caprino, G. ;
Lopresto, V. ;
Santoro, D. .
COMPOSITES SCIENCE AND TECHNOLOGY, 2007, 67 (3-4) :325-335
[5]   Effect of resin and fibre properties on impact and compression after impact performance of CFRP [J].
Cartié, DDR ;
Irving, PE .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2002, 33 (04) :483-493
[6]   IMPROVING THE DELAMINATION RESISTANCE OF CFRP BY STITCHING - A REVIEW [J].
DRANSFIELD, K ;
BAILLIE, C ;
MAI, YW .
COMPOSITES SCIENCE AND TECHNOLOGY, 1994, 50 (03) :305-317
[7]   Effect of Z-pinning on the impact resistance of composite laminates with different layups [J].
Francesconi, L. ;
Aymerich, F. .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2018, 114 :136-148
[8]   Compression properties of composite laminates reinforced with rectangular z-pins [J].
Hoffmann, Julian ;
Scharr, Gerhard .
COMPOSITES SCIENCE AND TECHNOLOGY, 2018, 167 :463-469
[9]   Performance of stitched/unstitched woven carbon/epoxy composites under high velocity impact loading [J].
Hosur, MV ;
Vaidya, UK ;
Ulven, C ;
Jeelani, S .
COMPOSITE STRUCTURES, 2004, 64 (3-4) :455-466
[10]   Failure strength of composite T-joints prepared using a new 1-thread stitching process [J].
Kim, Cheol Hwan ;
Jo, Dae Hyeon ;
Choi, Jin Ho .
COMPOSITE STRUCTURES, 2017, 178 :225-231