DAMAGE ANALYSIS ON THE SURFACE OF EPOXY ADHESIVE CONNECTIONS IN COMPOSITE MATERIALS USED IN WIND TURBINE ENERGY SYSTEMS


Mertgenç Yoldaş D., Yalçınkaya S., Yoldaş M. F.

16th INTERNATIONAL CONGRESS ON ENGINEERING, ARCHITECTURE AND DESIGN , İstanbul, Türkiye, 20 - 22 Aralık 2025, ss.1-12, (Tam Metin Bildiri)

  • Yayın Türü: Bildiri / Tam Metin Bildiri
  • Basıldığı Şehir: İstanbul
  • Basıldığı Ülke: Türkiye
  • Sayfa Sayıları: ss.1-12
  • Dokuz Eylül Üniversitesi Adresli: Evet

Özet

To mitigate the global impact of climate change, efforts to identify cleaner and more efficient renewable energy alternatives for energy production are rapidly progressing. The emergence of new technologies such as new oil and gas reserves and shale gas is increasing the use of fossil fuels, while simultaneously increasing their harmful consequences. Therefore, it is necessary to develop environmentally friendly and sustainable resources that can replace renewable energy sources. In this regard, wind energy is one of the fastest-growing forms of electricity generation, with an annual production of over one million gigawatt-hours. According to an IRENA report, wind energy is expected to account for more than 30% of global electricity production by 2050. Today, wind turbine blades are mostly manufactured from composite materials. Among these materials, carbon fiber-reinforced polymer (CFRP) is the most preferred composite material. CFRP has many mechanical properties, such as high strength-to-weight ratio, stiffness, damping properties, and resistance to corrosion and abrasion. For this study, 12 samples were cut from a CFRP composite plate. These cut specimens were prepared using the adhesive bonding method on solvent-cleaned surfaces. Bonding was performed using Loctite Hysol-9466, a two-component epoxy adhesive that cures at room temperature and is mixed at a 2:1 ratio in an applicator gun. Nine of the 12 bonded specimens were stored in separate containers in 21°C seawater for one, two, or three months. The dry-surface specimens and the specimens exposed to seawater were subjected to four-point bending tests to examine the damage occurring on the adhesive bond surface. Adhesion and cohesion separations occurred on all CFRP specimens. These separations on the bond surface were caused by the maximum bending stress occurring in the constant moment region where the loads were applied in the four-point bending test. The damage was concentrated in the bending region centered between the load application points, and the integrity of the specimen body was largely preserved. This indicates that the fracture behavior initiated in this region, where the highest bending stress was effective.