Özet
Fibre-reinforced polymer (FRP) composites generally have a layered architecture and are commonly manufactured with thermosetting resins - making them susceptible to interlaminar fracture (i.e. delamination), which is often a major concern in structurally critical applications. As a result, various approaches have been explored to enhance interlaminar fracture resistance. This review focuses on third-phase toughener inclusions, which offer opportunities to create damage resistant and damage tolerant structures without significantly adding weight or reducing in-plane mechanical properties. These toughener inclusions, typically introduced in the interlaminar regions, are divided into two categories herein: particle fillers and non-woven fibre veils. The advantages and limitations of both types are discussed, and the potential of the two approaches is evaluated using published data, aiming to provide an overview of the current understanding and challenges in designing and manufacturing safe and reliable composite structures.
| Orijinal dil | İngilizce |
|---|---|
| Sayfa (başlangıç-bitiş) | 222-248 |
| Sayfa sayısı | 27 |
| Dergi | Aeronautical Journal |
| Hacim | 126 |
| Basın numarası | 1295 |
| DOI'lar | |
| Yayın durumu | Yayınlandı - 28 Oca 2022 |
| Harici olarak yayınlandı | Evet |
Bibliyografik not
Publisher Copyright:© The Author(s), 2021. Published by Cambridge University Press on behalf of Royal Aeronautical Society.
BM SKH
Bu sonuç, aşağıdaki Sürdürülebilir Kalkınma Hedefine/Hedeflerine katkıda bulunur
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SKH 9 Sanayi, Yenilikçilik ve Altyapı
Parmak izi
Progress in interlaminar toughening of aerospace polymer composites using particles and non-woven veils' araştırma başlıklarına git. Birlikte benzersiz bir parmak izi oluştururlar.Alıntı Yap
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