Araştırma Makalesi

Investigation of Mechanical Properties of Layered Composites Formed from Glass, Carbon and Aramid Fibers and Aluminum Plates

Cilt: 12 Sayı: 2 30 Aralık 2022
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Investigation of Mechanical Properties of Layered Composites Formed from Glass, Carbon and Aramid Fibers and Aluminum Plates

Öz

Technological developments and differences in application areas increase the importance of laminated composites. Laminated composites with complex properties exhibit features such as high strength, high corrosion and thermal resistance, low specific gravity, resistance to environmental conditions. These properties generally reflect components that make up laminated composite. In this study, effects of reinforcements on mechanical properties of laminated composites were investigated. In production of laminated composites, aluminum 5754 is used for metal layers, and aramid, glass and carbon fibers are used for fiber reinforcements. Epoxy was also preferred as resin. First of all, the resin was applied on the cleaned aluminum plate and the aramid fiber was added on it. By continuing the processes in this way, Arall laminated composite consisting of five layers was obtained. Similar processes were applied to carbon fiber and glass fiber materials, and Carall and Glare laminated composites were produced, respectively. In addition, by subjecting the fiber layers to a combination among themselves, Ar-Carall, Ar-Glare and Car-Glare laminated composites were produced. The produced laminated composites were subjected to tensile and bending tests and their strengths were compared. As a result of the experiments, the highest tensile and bending strength was obtained from the Carall laminated composite. The strength of the Ar-Carall and the Car-Glare laminated hybrid composites containing carbon fiber were better than the Arall and the Glare laminated composites.

Anahtar Kelimeler

Kaynakça

  1. Botelho, E. C, Silva, R. A., Pardini, L. C. and Rezende, M. C., A review on the development and properties of continuous fiber/epoxy/aluminum hybrid composites for aircraft structures, Materials Research, 9 (3), 247-256, 2006.
  2. Qaiser, H., Umar, S., Nasir, A., Shah, M. and Nauman, S., Optimization of interlaminar shear strength behavior of anodized and unanodized ARALL composites fabricated through VARTM process, International Journal of Material Forming, 8, 481–493, 2015.
  3. Khalid, M. Y., Al Rashid, A. and Sheikh, M. F., Effect of anodizing process on inter laminar shear strength of GLARE composite through t-peel test: experimental and numerical approach, Experimental Techniques, 45, 227–235, 2021.
  4. Khan, F., Quayyum, F., Asghar, W., Azeem, M., Anjum, Z., Nasir, A. and Shah, M., Effect of various surface preparation techniques on the delamination properties of vacuum infused carbon fiber reinforced aluminum laminates (CARALL): experimentation and numerical simulation, Journal of Mechanical Science and Technology, 31 (11), 5265–5272, 2017.
  5. Armatlı Kayrak, M., Düzlemsel gerilmeler etkisindeki Arall ve Glare kompozit plakaların rijitlik analizleri, Mühendis ve Makine, 47 (560), 26–32, 2006.
  6. Wu, G. and Yang, J.-M., The mechanical behavior of GLARE laminates for aircraft structures, The Journal of the Minerals, Metals & Materials Society, 57, 72–79, 2005.
  7. Asghar, W., Nasir, M. A., Quayyum, F., Shah, M., Azeem, M, Nauman, S and Khushnood, S., Investigation of fatigue crack growth rate in CARALL, ARALL and GLARE, Fatigue Fracture of Engineering Materials and Structure, 40 (7), 1086–1100, 2017.
  8. Monsalve, A., Parra, L., Baeza, D., Solis, R., Palza, H., Mechanical properties and morphological characteristics of ARALL reinforced with TRGO doped epoxy resin, RevistaMateria, v. 23, n. 4, 2018.

Ayrıntılar

Birincil Dil

İngilizce

Konular

Makine Mühendisliği

Bölüm

Araştırma Makalesi

Yayımlanma Tarihi

30 Aralık 2022

Gönderilme Tarihi

27 Mayıs 2022

Kabul Tarihi

20 Eylül 2022

Yayımlandığı Sayı

Yıl 2022 Cilt: 12 Sayı: 2

Kaynak Göster

APA
Biliz, İ., & Çelik, Y. H. (2022). Investigation of Mechanical Properties of Layered Composites Formed from Glass, Carbon and Aramid Fibers and Aluminum Plates. European Journal of Technique (EJT), 12(2), 117-122. https://doi.org/10.36222/ejt.1122360
AMA
1.Biliz İ, Çelik YH. Investigation of Mechanical Properties of Layered Composites Formed from Glass, Carbon and Aramid Fibers and Aluminum Plates. EJT. 2022;12(2):117-122. doi:10.36222/ejt.1122360
Chicago
Biliz, İbrahim, ve Yahya Hışman Çelik. 2022. “Investigation of Mechanical Properties of Layered Composites Formed from Glass, Carbon and Aramid Fibers and Aluminum Plates”. European Journal of Technique (EJT) 12 (2): 117-22. https://doi.org/10.36222/ejt.1122360.
EndNote
Biliz İ, Çelik YH (01 Aralık 2022) Investigation of Mechanical Properties of Layered Composites Formed from Glass, Carbon and Aramid Fibers and Aluminum Plates. European Journal of Technique (EJT) 12 2 117–122.
IEEE
[1]İ. Biliz ve Y. H. Çelik, “Investigation of Mechanical Properties of Layered Composites Formed from Glass, Carbon and Aramid Fibers and Aluminum Plates”, EJT, c. 12, sy 2, ss. 117–122, Ara. 2022, doi: 10.36222/ejt.1122360.
ISNAD
Biliz, İbrahim - Çelik, Yahya Hışman. “Investigation of Mechanical Properties of Layered Composites Formed from Glass, Carbon and Aramid Fibers and Aluminum Plates”. European Journal of Technique (EJT) 12/2 (01 Aralık 2022): 117-122. https://doi.org/10.36222/ejt.1122360.
JAMA
1.Biliz İ, Çelik YH. Investigation of Mechanical Properties of Layered Composites Formed from Glass, Carbon and Aramid Fibers and Aluminum Plates. EJT. 2022;12:117–122.
MLA
Biliz, İbrahim, ve Yahya Hışman Çelik. “Investigation of Mechanical Properties of Layered Composites Formed from Glass, Carbon and Aramid Fibers and Aluminum Plates”. European Journal of Technique (EJT), c. 12, sy 2, Aralık 2022, ss. 117-22, doi:10.36222/ejt.1122360.
Vancouver
1.İbrahim Biliz, Yahya Hışman Çelik. Investigation of Mechanical Properties of Layered Composites Formed from Glass, Carbon and Aramid Fibers and Aluminum Plates. EJT. 01 Aralık 2022;12(2):117-22. doi:10.36222/ejt.1122360

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