journal article·2018-06Open access

Effect of polyamide-6,6 (PA 66) nonwoven veils on the mechanical performance of carbon fiber/epoxy composites

Bertan Beylergil, Metin Tanoğlu, Engin Aktaş

Abstract

Abstract In this study, carbon fiber/epoxy (CF/EP) composites were interleaved with polyamide-6,6 (PA 66) nonwoven veils at two different areal weight densities (17 and 50 gsm) to improve their delamination resistance against Mode-I loading. Mode-I fracture toughness (DCB), tensile, open hole tensile (OHT), flexural, compression, short beam shear (ILSS) and Charpy-impact tests were performed on the reference and PA 66 interleaved composite specimens . The DCB test results showed that the initiation and propagation Mode-I fracture toughness values of the composites were significantly improved by 84 and 171% using PA 66-17 gsm veils respectively, as compared to reference laminates. The use of denser PA 66-50 gsm veils in the interlaminar region led to higher improvement in fracture toughness values (349% for initiation and 718% for propagation) due to the higher amount of veil fibers involved in fiber bridging toughening mechanism. The incorporation of PA 66-50 gsm nonwoven veils also increased the ILSS and Charpy impact strength of the composites by 25 and 15%, respectively. On the other hand, the PA 66 veils reduced in-plane mechanical properties of CF/EP composites due to lower carbon fiber volume fraction and increased thickness.
Source: openaire · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: Mechanical Behavior of Composites · Fiber-reinforced polymer composites · Natural Fiber Reinforced Composites

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

References (43)

Show source-provided references
1. Fractographic observations on delamination growth and the subsequent migration through the laminate10.1016/j.compscitech.2009.01.034 ↗
2. Greenhalgh · 2009
3. Kuwata · 2010
4. Steeves C, Fleck NA. Z-pinned composite laminates: knockdown in compressive strength. In: Proceedings of the 5th Conference of Delamination and Fracture of Composites, London; 18–19 March 1999, p. 60–68.
5. Stitching vs. a toughened matrix: compression strength effects10.1177/002199839502901805 ↗
6. Effect of stitching on the mechanical and impact properties of woven laminate composite10.1177/002199839402801604 ↗
7. FEM simulation of a modified DCB test for 3-D orthogonal interlocked fabric composites10.1016/S0266-3538(01)00003-3 ↗
8. Mechanical performance of composites based on various three-dimensional woven-fibre performs10.1016/0266-3538(95)00135-2 ↗
9. Fracture toughness improvement of CFRP laminates by dispersion of cupstacked carbon nanotubes10.1016/j.compscitech.2008.12.017 ↗
10. Epoxy–silica particulate nanocomposites: chemical interactions, reinforcement and fracture toughness10.1016/j.polymer.2005.08.028 ↗
11. Effect of selective adhesive interleaving on interlaminar fracture toughness of graphite/epoxy composite laminates10.1016/0010-4361(88)90543-5 ↗
12. The effect of adhesive thickness on interlaminar fracture toughness of interleaved CFRP specimens10.1016/0010-4361(89)90341-8 ↗
13. Optimal use of adhesive layers in reducing impact damage in composite laminates10.1177/073168449000900604 ↗
14. Impact resistance and tolerance of interleaved tape laminates10.1016/S0263-8223(00)00049-0 ↗
15. Effect of interleaved non-woven carbon tissue on interlaminar fracture toughness of laminated composites: Part I - Mode I10.1177/0021998302036018981 ↗
16. Interlaminar toughness of interleaved CFRP using non-woven veils: Part 1. Mode-I testing10.1016/j.compositesa.2011.07.016 ↗
17. Interlaminar toughness of interleaved CFRP using non-woven veils: Part 2. Mode-II testing10.1016/j.compositesa.2011.07.017 ↗
18. Effect of thermoplastic veils on interlaminar fracture Toughness of a Glass Fiber/Vinyl Ester Composite
19. PET interleaving veils for improved fracture toughness of glass fibre/low-styrene-emission unsaturated polyester resin composites10.1002/app.42877 ↗
20. Mode I interlaminar fracture toughness of Nylon 66 nanofibrilmat interleaved carbon/epoxy laminates10.1002/pc.21210 ↗
21. Toughening effects of interleaved nylon veils on glass fabric/low-styrene-emission unsaturated polyester resin composites10.1002/app.41462 ↗
22. Miller SG, Roberts GD, Kohlman LW, Heimann PJ, Pereira JM, Ruggeri CR, 1, Martin RE, McCorkle LS. Impact behavior of composite fan blade leading edge subcomponent with thermoplastic polyurethane interleave. In: Proceedings of 20th International Conference on Composite Materials, Denmark; 19–24 Jul. 2015.
23. Load bearing enhancement of pin joined composite laminates using electrospun polyacrylonitrile nanofiber mats10.1016/j.arabjc.2015.03.019 ↗
24. Phase morphology of nanofibre interlayers: critical factor for toughening carbon/epoxy composites10.1016/j.compscitech.2011.11.010 ↗
25. Inhomogeneous toughening of carbon fiber/epoxy composite using electrospun polysulfone nanofibrous membranes by in situ phase separation10.1016/j.compscitech.2007.07.010 ↗
26. The influence of solvent type and polymer concentration on the physical properties of solid state polymerized PA66 nanofiber yarn10.1002/app.36871 ↗
27. Mode I and Mode II interlaminar fracture toughness of composite laminates interleaved with electrospun nanofibre veils10.1016/j.compositesa.2015.01.028 ↗
28. Enhancement of interlaminar fracture toughness of carbon fiber – epoxy composites using polyamide-6,6 electrospun nanofibers
29. Electrospun nanofibers as reinforcement for composite laminates materials-a review10.1016/j.compstruct.2017.09.021 ↗
30. Inclusion of a thermoplastic phase to improve impact and post-impact performances of carbon fibre reinforced thermosetting composites-a review10.1016/j.matdes.2015.07.001 ↗
31. On the tension–tension fatigue behaviour of a carbon reinforced thermoplastic part I: limitations of the ASTM D3039/D3479 standard10.1016/j.polymertesting.2011.05.004 ↗
32. On the tension–tension fatigue behaviour of a carbon reinforced thermoplastic part II: evaluation of a dumbbell-shaped specimen10.1016/j.polymertesting.2011.05.005 ↗
33. Jones · 1998
34. Barbero · 2011
35. ASTM D5528-13. Standard Test Method for Mode I Interlaminar Fracture Toughness of Unidirectional Fiber-Reinforced Polymer Matrix Composites, ASTM International, West Conshohocken, PA; 2013.
36. Effect of interleaved non-woven carbon tissue on interlaminar fracture toughness of laminated composites: Part II – Mode I10.1177/0021998302036018981 ↗
37. ASTM D4065-12. Standard Practice for Plastics: Dynamic Mechanical Properties: Determination and Report of Procedures. ASTM International, West Conshohocken, PA; 2012.
38. The influence of the nonwoven veil architectures on interlaminar fracture toughness of interleaved composites10.1016/j.compscitech.2015.01.016 ↗
39. The reversibility of Mode-I and -II interlaminar fracture toughness after hydrothermal aging of carbon/benzoxazine composites with a thermoplastic toughening interlayer10.1016/j.compstruct.2016.05.086 ↗
40. Armstrong-Carroll, Eileen, Cochran, Roland, Improvement of delamination resistance with carbon nonwoven mat interleaves, ASTM Special Technical Publication (1230); 1995, pp. 124–131.10.1520/STP14011S ↗
41. Nanofibre bridging as a toughening mechanism in carbon/epoxy composite laminates interleaved with electrospun polyamide nanofibrous veils10.1016/j.compscitech.2015.06.021 ↗
42. Mode I interlaminar fracture toughness on Nylon 66 nanofibreilmat interleaved carbon/epoxy laminates10.1002/pc.21210 ↗
43. An investigation of the damage tolerance of carbon/benzoxazine composites with a thermoplastic toughening interlayer10.1016/j.compstruct.2016.03.015 ↗