Abstract

As the fibre reinforced plastic composites gain larger and larger share in industry, the problem of joining them with metal elements becomes significant. The current paper is the first part of the literature review, which gathers and evaluates knowledge about methods suitable for mechanical joining of composite and metal elements. This paper concerns bolted joining, because this method of mechanical joining is widely used for joining composite materials. The paper describes failure modes of bolted joints in composite materials, the influence of the bolt clamping torque, the clearance between the bolt and the hole and aging on the performance of the joint, drilling techniques used in composite materials in order to minimize damages, different fastener types, inspection techniques, and finally, the techniques that have been developed in order to improve the strength of the bolted joints in composites. Since the hole drilled in a composite material in order to perform bolted joining is a weak point of the structure, those techniques: bonded inserts, titanium foil internal inserts, fibre steering, additional reinforcement, and moulded holes, mainly aim to improve the strength of the hole in the composite. The techniques have been discussed in details and compared with each other in the summary section.

Highlights

  • Fibre reinforced composite materials gain progressively larger share in the structures of modern aircraft

  • Modes of failure of bolted joints focusing on the mechanisms characteristic for composite materials, the influence of the bolt clamping torque, the clearance between the bolt and the hole and aging on the performance of the joint, drilling techniques used in composite materials in order to minimize damages, different fastener types, inspection methods, techniques that have been developed in order to improve the strength of bolted joints in composites

  • Calabrese et al studied the behaviour of glass/epoxy composite subjected to bearing test after exposure to salt-spraying, foggy conditions for 30 and 60 days to evaluate the induced change on the failure mechanisms and the consequent reduction of the joint mechanical performances compared to unaged specimens [59]

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Summary

Introduction

Fibre reinforced composite materials gain progressively larger share in the structures of modern aircraft. The current works present a review which fulfils both those conditions This part of the review devoted to bolted joining reviews: modes of failure of bolted joints focusing on the mechanisms characteristic for composite materials, the influence of the bolt clamping torque, the clearance between the bolt and the hole and aging on the performance of the joint, drilling techniques used in composite materials in order to minimize damages, different fastener types, inspection methods, techniques that have been developed in order to improve the strength of bolted joints in composites. Since a hole drilled in a composite material in order to perform bolted joining is a weak point of the structure, those techniques: bonded inserts, titanium foil internal inserts, fibre steering, additional reinforcement, moulded holes mainly aim to improve the strength of the hole in the composite. As this last part is interesting from the point of view of a designer looking for new solutions to enhance the performance of composite structures, those techniques have been discussed in details and compared with each other in the summary section

Modes of Failure
Clamping Torque
Clearance
Fatigue
Viscoelastic Effects
Drilling Holes
Fastener Types
10. Non-Destructive Testing
11.1. Metal Bonded Inserts
11.2. Titanium Foil Internal Inserts
11.3. Fibre Steering Technique
11.4. Additional Reinforcement
11.5. Moulded Holes
12. Forged Composites and 3D printing
13. Cost and Installation Challenges
14. Summary
Findings
15. Conclusions
Full Text
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