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Next generation of high-performance impact resistant composites with visibility of damage

Lead Research Organisation: Delft University of Technology
Department Name: Civil Engineering Faculty

Abstract

Composites are truly the materials of the future, due to their excellent properties such as high strength to weight ratio, and their use is rising exponentially, continuing to replace or augment traditional materials in different sectors such as aerospace, automotive, wind turbine blades, civil engineering infrastructure and sporting goods. A good example is the construction of large aircraft such as the Airbus A350 and Boeing 787 which are 53% and 50% composite by weight, respectively. However, while the fibre dominant properties guarantee excellent in-plane load-bearing characteristics, traditional composite materials exhibit weak resistance to out-of-plane loads, making them susceptible to barely visible impact damage (BVID) under impact loads that can happen during manufacturing or in service. BVID can drastically reduce the strength, without any visible warning. Structures that look fine can fail suddenly at loads much lower than expected. This weak impact resistance together with the complexity of the failure mechanisms typical of composite systems led in the past decade to complex and expensive maintenance/inspection procedures. Therefore, a significantly greater safety margin than other materials leads to conservative design in composite structures. Based on these premises, the need is clear for a comprehensive solution that matches the requirements of lightweight structures with the need for high impact resistance and ease of inspection. This project is aimed at the design and development of next generation of high-performance impact resistant composites with visibility of damage and improved compression after impact strength. These exceptional properties are caused with ability to visualise and control failure modes to happen in an optimised way. Energy would be absorbed by gradual and sacrificial damage, strength would be maintained, and there would be visible evidence of damage. This would eliminate the need for very low design strains to cater for BVID, providing a step change in composite performance, leading to greater reliability and safety, together with reduced design and maintenance requirements, and longer service life. This is an exciting opportunity to develop this novel proposed technology with my extensive industrial partners, a potentially transformative prospect for the UK composites research and industry.

Publications

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Fotouhi S. (2022) INVESTIGATING THE EFFECT OF INTERFACE ANGLE AND PLY THICKNESS ON MODE II DELAMINATION BEHAVIOUR OF CARBON/EPOXY LAMINATED COMPOSITES in ECCM 2022 - Proceedings of the 20th European Conference on Composite Materials: Composites Meet Sustainability

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Tabatabaeian A. (2022) ON THE OPTIMAL DESIGN OF SMART COMPOSITE SENSORS FOR IMPACT DAMAGE DETECTION in ECCM 2022 - Proceedings of the 20th European Conference on Composite Materials: Composites Meet Sustainability

Related Projects

Project Reference Relationship Related To Start End Award Value
EP/V009451/1 16/05/2021 18/06/2022 £241,210
EP/V009451/2 Transfer EP/V009451/1 20/05/2021 28/02/2024 £46,100
 
Description This project developed novel structural health monitoring (SHM) sensors to improve the detection of low energy impact damage in laminated composites. The sensors were designed and experimentally tested and the results indicate that the sensors functioned satisfactorily and provided direct correlations between visible and internal hidden damage detected by C-scan. The sensor needs to be optimized by selecting appropriate material properties and adjusting it to the in-plane dimensions of the substrate, which provide further challenges in modelling and a better understanding of how the sensors operate and can be optimized and calibrated to fit the applications such as aerospace, wind and civil.
Exploitation Route We have demonstrated that novel sensors perform satisfactorily for detecting impact damage, enabling the identification of the impact location visually, and we have established direct correlations between visible and internal hidden damage detected by C-scan. These hybrid sensing layers serve as both load-bearing components and damage indicators and are entirely wireless, providing cost-effective and straightforward solutions for damage detection. We believe that our findings will offer new insights into the development of SHM systems for impact damage detection in composite structures, and we anticipate that they will be of significant interest to both the academic and industrial communities.
Sectors Aerospace

Defence and Marine

Manufacturing

including Industrial Biotechology

 
Description Autonomous VIsion tAcTile rObots foR inspection of laminated composites (AVIATOR)
Amount € 849,211 (EUR)
Organisation Netherlands Organisation for Scientific Research (NWO) 
Sector Public
Country Netherlands
Start 01/2024 
End 06/2028