journal article·2024-02-01Open access

On the use of selective Z-pinning in stiffened composite panels to prevent skin/stringer debonding

Bin Yan, ShengWei Zhu, YunKe Zhang, LiangJi Shen, Yuan Li, WenTao Jiang, WenLi Kang, Hu Dou

Abstract

Carbon fiber reinforced plastic (CFRP) composites have been widely used in engineering. This paper investigates the effect of composite z-pin (polyimide fiber/epoxy resin) on flexural properties of skin/stringer composite structure with different z-pin densities and diameters. Compared with unpinned specimens, the peak loading and energy absorption of z-pinned specimens are increased by 98% and 9 times, respectively. Parameterized research indicates that the optimal z-pin density is 1.35%. And thin z-pins are beneficial to improve the peak loading and energy absorption, which attributes to more total contact area of z-pins. The statistical results present that z-pin pre-hole inserted (ZPI) process can significantly reduce initial damages of z-pinned specimens compared with Ultrasonically Assisted Z-fiber (UAZ) process. Specifically, the z-pin inclination angle is decreased by 60%, and the initial damages in eye-like zone are prominently reduced. The z-pin makes the specimen exhibit the quasi-brittle behavior under flexural loading by playing a bridging role, which makes the flexural properties of specimens prominently increased. In addition, the “snubbing effect” will enhance the bridging effect of z-pins, but it will lead to inter-fibers debonding, splitting, and shear failure of z-pins.
Source: crossref · Quality: baseline

Research context

OpenAlex topics: Mechanical Behavior of Composites · Textile materials and evaluations · Structural Analysis of Composite Materials

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

Xi’an Institute of Applied Optics, Xi’an, China

School of Mechanical Engineering, Northwestern Polytechnical University, Xi’an, China

References (32)

Show source-provided references
1. 10.1016/j.compositesa.2018.08.01310.1016/j.compositesa.2018.08.013 ↗
2. 10.1016/j.compstruct.2019.11143510.1016/j.compstruct.2019.111435 ↗
3. 10.1016/j.compositesa.2008.04.01910.1016/j.compositesa.2008.04.019 ↗
4. 10.1016/j.compstruct.2022.11629410.1016/j.compstruct.2022.116294 ↗
5. 10.1007/s10443-017-9640-610.1007/s10443-017-9640-6 ↗
6. 10.1016/j.compstruct.2009.04.00110.1016/j.compstruct.2009.04.001 ↗
7. 10.3390/aerospace807017810.3390/aerospace8070178 ↗
8. 10.1016/j.jmapro.2021.03.05210.1016/j.jmapro.2021.03.052 ↗
9. 10.1016/j.compositesa.2012.02.01010.1016/j.compositesa.2012.02.010 ↗
10. 10.1016/j.compstruct.2022.11583410.1016/j.compstruct.2022.115834 ↗
11. 10.1016/j.compositesa.2020.10612810.1016/j.compositesa.2020.106128 ↗
12. 10.1016/j.compositesa.2007.08.01610.1016/j.compositesa.2007.08.016 ↗
13. 10.3390/jcs401003110.3390/jcs4010031 ↗
14. 10.1016/j.matdes.2014.08.07210.1016/j.matdes.2014.08.072 ↗
15. 10.1520/CTR10971J10.1520/CTR10971J ↗
16. 10.1016/j.compositesa.2005.11.00910.1016/j.compositesa.2005.11.009 ↗
17. Javier TV · Composites Part A · 2011 · 42 · 2082
18. 10.1016/j.compositesa.2006.06.01310.1016/j.compositesa.2006.06.013 ↗
19. 10.1016/j.compstruct.2011.03.00910.1016/j.compstruct.2011.03.009 ↗
20. 10.1177/00219983000340150210.1177/002199830003401502 ↗
21. 10.1016/j.compositesb.2017.05.05210.1016/j.compositesb.2017.05.052 ↗
22. 10.1201/9780203492901.ch310.1201/9780203492901.ch3 ↗
23. 10.1016/j.compscitech.2018.08.04210.1016/j.compscitech.2018.08.042 ↗
24. 10.1016/j.compscitech.2020.10848610.1016/j.compscitech.2020.108486 ↗
25. 10.1016/j.compositesa.2018.03.00410.1016/j.compositesa.2018.03.004 ↗
26. James KL · 2014
27. 10.1016/j.compscitech.2020.10841310.1016/j.compscitech.2020.108413 ↗
28. 10.1016/j.aiepr.2022.03.00410.1016/j.aiepr.2022.03.004 ↗
29. 10.1016/j.compositesa.2006.05.00410.1016/j.compositesa.2006.05.004 ↗
30. 10.1016/j.ijfatigue.2009.09.00110.1016/j.ijfatigue.2009.09.001 ↗
31. 10.1080/1537649049049389910.1080/15376490490493899 ↗
32. 10.1016/j.compstruct.2011.08.02610.1016/j.compstruct.2011.08.026 ↗