KaydedilenlerDerginizi ekleyin

Dergiler / Politeknik Dergisi / 2020 / Cilt: 23 - Sayı: 2

Analysing Mechanical Behaviors of Carbon Fiber Reinforced Silicone Matrix Composite Materials after Static Folding

İsmail Sinan ATLI
Atilla EVCİN
Sayfa
351–359
Yayın Tarihi
2020-06-01
DOI
—
🏛️Bu makalenin bibliyografik verileri ve tam metin bağlantısı DergiPark üzerinden sağlanmıştır.
DergiPark Kaydı ↗
✨

Yapay Zeka Hızlı Bakış & Çıkarımlar

AI Insight
⚡ TL;DR(1 Cümlede Hızlı Çıkarım)

They were subjected to tensile testing afterwards, to investigate effect of number of layers, silicone type and duration of folding to mechanical behavior.

📌 3 Maddede Bu Makale

🎯
Amaç & Hipotez:Subject of this paper is to provide information about mechanical behavior of a novel material to the literature: carbon fiber reinforced silicone matrix composite (CFRS-C).
📊
Temel Bulgular & Veri:Specimens were prepared and kept folded 90º statically in various periods of time.
💡
Sonuç & Katkı:They were subjected to tensile testing afterwards, to investigate effect of number of layers, silicone type and duration of folding to mechanical behavior.
🔬Tür:Araştırma Makalesi
📍Kapsam:Genişletilmiş Akademik Örneklem
⚙️Değişkenler:Foldable materials · composite · silicone

Özet

Subject of this paper is to provide information about mechanical behavior of a novel material to the literature: carbon fiber reinforced silicone matrix composite (CFRS-C). Under a mechanical load, silicone matrix allows large elastic deformations while carbon fiber reinforcement can bear high tensile stresses. This rare behavior of CFRS-C allows us to design foldable materials without being in a bind for mechanical hinges which bring additional weights. Foldable materials are used in space structures to gain advantage of smaller volumes. In this study, CFRS-C were manufactured with two different silicone type can be found in market and one type of plain weave unidirectional carbon fiber fabric. Specimens were prepared and kept folded 90º statically in various periods of time. They were subjected to tensile testing afterwards, to investigate effect of number of layers, silicone type and duration of folding to mechanical behavior.

Abstract

Subject of this paper is to provide information about mechanical behavior of a novel material to the literature: carbon fiber reinforced silicone matrix composite (CFRS-C). Under a mechanical load, silicone matrix allows large elastic deformations while carbon fiber reinforcement can bear high tensile stresses. This rare behavior of CFRS-C allows us to design foldable materials without being in a bind for mechanical hinges which bring additional weights. Foldable materials are used in space structures to gain advantage of smaller volumes. In this study, CFRS-C were manufactured with two different silicone type can be found in market and one type of plain weave unidirectional carbon fiber fabric. Specimens were prepared and kept folded 90º statically in various periods of time. They were subjected to tensile testing afterwards, to investigate effect of number of layers, silicone type and duration of folding to mechanical behavior.

🔖

Bu Makaleye Atıf Yap

ATLI, İ. S., EVCİN, A. (2020). Analysing Mechanical Behaviors of Carbon Fiber Reinforced Silicone Matrix Composite Materials after Static Folding. Politeknik Dergisi, Cilt: 23 - Sayı: 2, 351–359. https://ajindex.com/articles/422210

📄 Tam Metin PDF Okuyucu

📄

PDF görüntüleyici hazırlanıyor...

Kaynakça (1)

  1. Referans 1. Dano M.L., Gendron G., Picard A., Mechanical Behavior of a Triaxial Woven Fabric Composite, Mechanics of Composite Materials and Structures, 7:207-224, (2000). Referans 2. Benarcyk B.A., Arnold S.M., ‘’Micromechanics-Based Modeling of Woven Polymer Matrix Composites’’, AIAA Journal, 41(9):1788-1796, (2003). Referans 3. Le Page, B.H., Guild, F.J., Ogin, S.L. and Smith, P.A., ‘’Finite Element Simulation of Woven Fabric Composites’’, Composites: Part A, 35:861 - 872, (2004). Referans 4. Hackett, R.M., ‘’Finite Elasticity’’, Hyperelasticity Primer, Springer International Publishing, USA, (2016) Referans 5. Manuel J. Garcia R., Oscar E. Ruiz S., Carlos Lopez, "Hyperelastic Material Modeling", Technical Report, Laboratorio CAD/CAM/CAE, Departamento de Ingenieria Mecanica, Universidad EAFIT, Medellin, (2005). Referans 6. T. W. Murphey, T. Meink, and M. M. Mikulas, ‘’Some micromechanics considerations of the folding of rigidizable composite materials’’ In 42nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, AIAA:2001-1418, (2001). Referans 7. W. H. Francis, M.S. Lake, and J. Steven Mayes, ‘’A review of classical _ber microbuckling analytical solutions for use with elastic memory composites’’, In 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Newport, RI,AIAA-2006:1764, (2006). Referans 8. Lopez Jimenez, F., ‘’Mechanics of thin carbon fiber composites with a silicone matrix’’, Doctoral dissertation, California Institute of Technology, (2011). Referans 9. Baier, H., L. Datashvili, and J. Hoffmann. "Mechanically reconfigurable and massively shape morphing space structures." Proceedings of the 11th European Spacecraft Structures, Materials and Mechanical Testing Conference, (2009). Referans 10. Murphey, T. W., ‘’Large Strain Composite Materials in Deployable Space Structures’’ In 17th International Conference on Composite Materials(Vol. 28). Edinburgh, UK: The British Composites Soc., (2009) Referans 11. Campbell, D., Lake, M.S. and Mallick, K., "A study of the bending mechanics of elastic memory composites." In AIAA. 45th Structures, Structural Dynamics, and Materials Conference. California: Palm Springs: 1323-1331, (2004). Referans 12. Datashvili, L., Baier, H., Wehrle, E., Kuhn, T., & Hoffmann, J.’’ Large shell-membrane space reflectors’’ In Proceedings of AIAA Structures, Dynamics, and Materials Conference, Honolulu, Hawaii, (2010). Referans 13. ‘’Tembo Deployable Structures’’: