Fatigue characteristics of jagged steel pin-reinforced composite hat-joints under pull-off loading

被引:1
作者
Noh, Ji-Sub [1 ]
Kim, Dong-Gwan [2 ]
Nam, Young-Woo [3 ,4 ]
Kwak, Byeong-Su [1 ]
机构
[1] Gyeongsang Natl Univ, Composite Struct LabJinju daero, 501 Jinju Daero, Jiuju Si, Gyeongnam Do, South Korea
[2] LX Hausys, Automot Mat & Components Div, 30 Magokjungang 10 Ro, Seoul, South Korea
[3] Korea Aerosp Univ, Grad Sch Aerosp & Mech Engn, 76 Hanggongdaehak Ro, Goyang Si, Gyeonggi Do, South Korea
[4] Korea Aerosp Univ, Dept Smart Drone Engn, 76 Hanggongdaehak Ro, Goyang Si, Gyeonggi Do, South Korea
基金
新加坡国家研究基金会;
关键词
Composite hat-joint; Z-pining; reinforcement; fatigue strength; jagged steel pin; MODE-I DELAMINATION; SINGLE-LAP JOINTS; T-JOINTS; RESISTANCE; STRENGTH; MECHANISMS; BEHAVIOR;
D O I
10.1080/09243046.2024.2324566
中图分类号
TB33 [复合材料];
学科分类号
摘要
This study focuses on the reinforcement effect provided by surface-treated jagged pins on the pull-off fatigue strength of composite hat-joint structures intended for the joining area of stiffened sections in aircraft composite fuselages under at room temperature. The study utilizes pin diameters of 0.3 mm, 0.5 mm, and 0.7 mm, along with pin-areal-densities of 0.5% and 2%, as the test parameters. The investigation involved subjecting the joints to cyclic pull-off loading. Additionally, to evaluate the reinforcing impact of jagged pins, a comparison was made with a hat-joint reinforced by a standard, untreated pin. The results revealed a significant enhancement in pull-off fatigue strength compared to non-reinforced hat-joints. At a pin diameter of 0.3 mm and a pin-areal-density of 2%, the maximum improvement observed was 141%. Furthermore, the pull-off fatigue strength achieved by the jagged pins was 52% higher than that of regular pins. These test outcomes lead to the conclusion that the implementation of jagged pin reinforcement can substantially improve the pull-off fatigue strength of composite hat-joint structures.
引用
收藏
页码:1145 / 1159
页数:15
相关论文
共 36 条
[1]   A Method of Metallisation of Carbon Fibre-Reinforced Plastic (CFRP) Sandwich Antenna Reflector Dish for High-Frequency Applications [J].
Agarwal, Pankaj ;
Viswanath, Vinu ;
John, Ani K. ;
Sebastian, Mathew ;
Harikrishna, S. ;
Pandya, Jigar ;
Kumar, Sagi Sravan .
INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2023, 24 (02) :430-437
[2]   Investigation of knitting architecture on the impact behavior of glass/epoxy composites [J].
Aktas, Alaattin ;
Tercan, Mevlut ;
Aktas, Mehmet ;
Turan, Fatih .
COMPOSITES PART B-ENGINEERING, 2013, 46 :81-90
[3]   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
[4]  
ASTM E739-91, 2006, STANDARD PRACTICE ST
[5]   Determination of shift factor for long-term life prediction of carbon/fiber epoxy composites using the time-temperature superposition principle [J].
Cha, Jaeho ;
Yoon, Sungho .
FUNCTIONAL COMPOSITES AND STRUCTURES, 2022, 4 (01)
[6]   Elevated temperature properties of pinned composite lap joints [J].
Chang, P. ;
Mouritz, A. P. ;
Cox, B. N. .
JOURNAL OF COMPOSITE MATERIALS, 2008, 42 (08) :741-769
[7]   Properties and failure mechanisms of pinned composite lap joints in monotonic and cyclic tension [J].
Chang, P. ;
Mouritz, A. P. ;
Cox, B. N. .
COMPOSITES SCIENCE AND TECHNOLOGY, 2006, 66 (13) :2163-2176
[8]   Effects of ferromagnetic & carbon-fibre Z-Pins on the magnetic properties of composites [J].
Chen, Mudan ;
Zhang, Bing ;
Friedemann, Sven ;
Allegri, Giuliano ;
Hallett, Stephen R. .
COMPOSITES SCIENCE AND TECHNOLOGY, 2021, 207
[9]   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
[10]   Micro-CT based trans-scale damage analysis of 3D braided composites with pore defects [J].
Ge, Lei ;
Li, Huimin ;
Zhong, Jiehua ;
Zhang, Chun ;
Fang, Daining .
COMPOSITES SCIENCE AND TECHNOLOGY, 2021, 211 (211)