SavedAdd your journal

Journals / Necmettin Erbakan Üniversitesi Fen ve Mühendislik Bilimleri Dergisi / 2019 / Cilt: 1 - Sayı: 1

Nano Fiber Reinforced Nanocomposite Production and Characterization

Nano Elyaf Takviyeli Nanokompozit Üretimi ve Karakterizasyonu

Mesut UYANER
Adem YAR
Pages
10–19
Publication Date
2019-04-18
DOI
—
🏛️Bibliographic metadata and full text access for this article are provided via DergiPark.
DergiPark Record ↗
✨

AI Summary & Key Takeaways

AI Insight
⚡ TL;DR(Too Long; Didn't Read)

Results reveal that PVA and PVP nanofiber mat was not adequately impregnated with epoxy.

📌 3 Key Takeaways

🎯
Objective & Hypothesis:The present study investigates the effect of various fabricated nanofiber such as poly-vinyl-alcohol (PVA) ile poly-vinyl-pyrrolidone (PVP) nanofibers mat to interlaminar features.
📊
Key Findings & Data:E-glass/epoxy composite materials are produced by Vacuum Assisted Resin Transfer Molding (VARTM) method, interleaving PVA and PVP electrospun nanofiber mat in each laminate consisted of eight ply.
💡
Conclusion & Impact:Results reveal that PVA and PVP nanofiber mat was not adequately impregnated with epoxy.
🔬Design:Research Article
📍Scope:Comprehensive Sample
⚙️Variables:Elektro eğirme · Nano elyaf · Tabakalaarası bölge

Abstract

The present study investigates the effect of various fabricated nanofiber such as poly-vinyl-alcohol (PVA) ile poly-vinyl-pyrrolidone (PVP) nanofibers mat to interlaminar features. E-glass/epoxy composite materials are produced by Vacuum Assisted Resin Transfer Molding (VARTM) method, interleaving PVA and PVP electrospun nanofiber mat in each laminate consisted of eight ply. Tensile tests are carried out for nanomodified composite materials. Also, after tensile tests, the fracture surfaces area of both composite materials are studied using scanning electron microscobe (SEM). Results reveal that PVA and PVP nanofiber mat was not adequately impregnated with epoxy.

Özet

Bu çalışma polivinilalkol (PVA) ve polivinilpirolidon (PVP) den elde edilen nano liflerin kompozitin tabakalar arasına olan etkisini incelemektedir. E-camı/epoksi kompozit malzemelerin arasına PVA ve PVP elektro eğirme nano elyaf yerleştirilerek Vakum Destekli Reçine Transferi Kalıplama (VARTM) yöntemi ile kompozit malzeme üretimi gerçekleştirilmiştir. Nano elyaf ile modifiye edilmiş kompozit malzemelerin çekme testleri yapılmıştır. Ayrıca çekme testinden sonra kompozit malzemelerin kırılma yüzeyleri SEM ile incelenmiştir. Bu çalışma, PVA ve PVP nano elyafların epoksi ile yeteri kadar ıslanmadığını göstermektedir.

🔖

Cite This Article

UYANER, M., YAR, A. (2019). Nano Fiber Reinforced Nanocomposite Production and Characterization. Necmettin Erbakan Üniversitesi Fen ve Mühendislik Bilimleri Dergisi, Cilt: 1 - Sayı: 1, 10–19. https://ajindex.com/articles/793512

📄 Full Text PDF Viewer

📄

PDF görüntüleyici hazırlanıyor...

References (6)

  1. S.S. Wicks, R.G. de Villoria, B.L. Wardle, Interlaminar and intralaminar reinforcement of composite laminates with aligned carbon nanotubes, Composites Science and Technology. 70 (2010) 20–28. doi:10.1016/J.COMPSCITECH.2009.09.001. L. Tong, A.P. Mouritz, M.K. Bannister, 3D fibre reinforced polymer composites, Elsevier, 2002. doi:10.1016/B978-0-08-043938-9.X5012-1. T.K. Tsotsis, A. Markus, AST composite wing program work Unit IV-design, analysis, and manufacturing studies, 1999.
  2. F. Larsson, Damage tolerance of a stitched carbon/epoxy laminate, Composites Part A: Applied Science and Manufacturing. 28 (1997) 923–934. doi:10.1016/S1359-835X(97)00063-8.
  3. K.A. Dransfield, L.K. Jain, Y.-W. Mai, On the effects of stitching in CFRPs—I. mode I delamination toughness, Composites Science and Technology. 58 (1998) 815–827. doi:10.1016/S0266-3538(97)00229-7.
  4. I.K. Partridge, D.D.R. Cartié, Delamination resistant laminates by Z-Fiber® pinning: Part I manufacture and fracture performance, Composites Part A: Applied Science and Manufacturing. 36 (2005) 55–64. doi:10.1016/J.COMPOSITESA.2004.06.029. S.K. Sharma, B. V. Sankar, Effect of Stitching on Impact and Interlaminar Properties of Graphite/Epoxy Laminates, Journal of Thermoplastic Composite Materials. 10 (1997) 241–253. doi:10.1177/089270579701000302. A. Mouritz, C. Baini, I. Herszberg, Mode I interlaminar fracture toughness properties of advanced textile fibreglass composites, Composites Part A: Applied Science and Manufacturing. 30 (1999) 859–870. doi:10.1016/S1359-835X(98)00197-3.
  5. J.R. Reeder, Stitching vs. a Toughened Matrix: Compression Strength Effects, Journal of Composite Materials. 29 (1995) 2464–2487. doi:10.1177/002199839502901805. X. Zhang, L. Hounslow, M. Grassi, Improvement of low-velocity impact and compression-after-impact performance by z-fibre pinning, Composites Science and Technology. 66 (2006) 2785–2794. doi:10.1016/J.COMPSCITECH.2006.02.029. C.A. Steeves, N.A. Fleck, In-plane properties of composite laminates with through-thickness pin reinforcement, International Journal of Solids and Structures. 43 (2006) 3197–3212. doi:10.1016/J.IJSOLSTR.2005.05.017. A.P. Mouritz, Review of z-pinned composite laminates, Composites Part A: Applied Science and Manufacturing. 38 (2007) 2383–2397. doi:10.1016/J.COMPOSITESA.2007.08.016. P.K. Sinha, Composite materials and structures, Composite Centre of Excellence, AR&DB, Department of Aerospace Engineering IIT Kharagpur. (2006).
  6. M. Biron, Thermosets and composites: t