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KARBON/PP(POLİPROPİLEN)/EPOKSİ KOMPOZİTLERİN EĞİLME DAYANIMI VE YAPISAL İYİLEŞME ÖZELLİKLERİ

Year 2019, Volume: 22 - Special Issue, 41 - 47, 29.11.2019
https://doi.org/10.17780/ksujes.596200

Abstract

Karbon/PP(Polipropilen)/epoksi
hibrid kompozitlerin eğilme dayanımı ve yapısal iyileştirme özellikleri
incelenmiştir. Karbon ve PP lifleri, manuel bir dokuma tezgâhında dokunmuştur.
Burada, karbon lifleri yapıya yüksek dayanım kazandırırken, PP lifleri ise
tokluk özelliği sağlamaktadır.  İki
farklı yapısal iyileşme prosesi kullanılmıştır. Önerilen iyileşme proseslerinin
etkinliği, hem mekanik hem de mikroskobik olarak değerlendirilmiştir. Sonuçlar,
iyileşmiş kompozitlerin eğilme dayanımlarının, hem 0° hem de 90° doğrultuda
oldukça azaldığını göstermiştir. Presle iyileştirilmiş kompozitlerin artık
eğilme dayanımları, etüvde iyileştirilen kompozitlere kıyasla daha yüksektir.
Bunun nedeni, erimiş PP liflerinin boşlukları basınç altında daha etkili bir
şekilde doldurmasıdır
.

References

  • ASTM D790-17.(2017). Standard test methods for flexural properties of unreinforced and reinforced plastics and electrical insulating materials.
  • Bleay, S.M. et al. (2001). A smart repair system for polymer matrix composites. Composites: Part A, 32, 1767-1776.
  • Dutra, R.C.L., Soares, B.G., Campos, E.A., & Silva, J.L.G. (2000). Hybrid composites based on polypropylene and carbon fiber and epoxy matrix. Polymer, 41, 3841-3849.
  • Ladani, R.B., Nguyen, A.T.T., Wang, C.H., & Mouritz, A.P. (2019). Mode II interlaminar delamination resistance and healing performance of 3D composites with hybrid z-fibre reinforcement. Composites: Part A, 120, 21-32.
  • Ladani, R.B., Pingkarawat, K., Nguyen, A.T.T., Wang, C.H., & Mouritz, A.P. (2018). Delamination toughening and healing performance of woven composites with hybrid z-fibre reinforcement. Composites: Part A, 110, 258-267.
  • Li, G., Xiao, P., Hou, S., & Huang, Y. (2019). Graphene based self-healing materials. Carbon, 146, 371-387.
  • Soutis, C. (2005). Carbon fibre reinforced plastics in aircraft construction. Materials Science and Engineering, A, 412, 171-176.
  • Williams, G., Trask, R., & Bond, I. (2007). A self-healing carbon fibre reinforced polymer for aerospace applications. Composites: Part A, 38, 1525-1532.

BENDING STRENGTH AND STRUCTURAL HEALING PROPERTIES OF CARBON/PP(POLYPROPYLENE)/EPOXY COMPOSITES

Year 2019, Volume: 22 - Special Issue, 41 - 47, 29.11.2019
https://doi.org/10.17780/ksujes.596200

Abstract

Bending strength and structural healing properties of
carbon/PP(Polypropylene)/epoxy hybrid composites are investigated. Carbon and
PP fibres are woven in a manual loom in which the carbon fibres provide high
strength while the PP fibres contribute with their high strain in
hybridization.  Two different structural
healing processes are used. Effectiveness of the proposed healing processes is
evaluated by both mechanically and microscopically. The results showed that
bending strengths of healed composites incredibly decreased at both 0° and 90° directions.
Residual bending strengths of press-healed composites are higher than that of
oven-healed composites since the molten PP filled the gaps more influentially
under pressure.

References

  • ASTM D790-17.(2017). Standard test methods for flexural properties of unreinforced and reinforced plastics and electrical insulating materials.
  • Bleay, S.M. et al. (2001). A smart repair system for polymer matrix composites. Composites: Part A, 32, 1767-1776.
  • Dutra, R.C.L., Soares, B.G., Campos, E.A., & Silva, J.L.G. (2000). Hybrid composites based on polypropylene and carbon fiber and epoxy matrix. Polymer, 41, 3841-3849.
  • Ladani, R.B., Nguyen, A.T.T., Wang, C.H., & Mouritz, A.P. (2019). Mode II interlaminar delamination resistance and healing performance of 3D composites with hybrid z-fibre reinforcement. Composites: Part A, 120, 21-32.
  • Ladani, R.B., Pingkarawat, K., Nguyen, A.T.T., Wang, C.H., & Mouritz, A.P. (2018). Delamination toughening and healing performance of woven composites with hybrid z-fibre reinforcement. Composites: Part A, 110, 258-267.
  • Li, G., Xiao, P., Hou, S., & Huang, Y. (2019). Graphene based self-healing materials. Carbon, 146, 371-387.
  • Soutis, C. (2005). Carbon fibre reinforced plastics in aircraft construction. Materials Science and Engineering, A, 412, 171-176.
  • Williams, G., Trask, R., & Bond, I. (2007). A self-healing carbon fibre reinforced polymer for aerospace applications. Composites: Part A, 38, 1525-1532.
There are 8 citations in total.

Details

Primary Language English
Subjects Wearable Materials
Journal Section Research Articles
Authors

Gaye Kaya 0000-0003-1866-4799

Pınar Çam 0000-0002-3528-888X

Publication Date November 29, 2019
Submission Date July 24, 2019
Published in Issue Year 2019Volume: 22 - Special Issue

Cite

APA Kaya, G., & Çam, P. (2019). BENDING STRENGTH AND STRUCTURAL HEALING PROPERTIES OF CARBON/PP(POLYPROPYLENE)/EPOXY COMPOSITES. Kahramanmaraş Sütçü İmam Üniversitesi Mühendislik Bilimleri Dergisi, 22, 41-47. https://doi.org/10.17780/ksujes.596200