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Digital archive of theses discussed at the University of Pisa

 

Thesis etd-11012021-153930


Thesis type
Tesi di laurea magistrale
Author
BERNARDI, MATTEO
URN
etd-11012021-153930
Thesis title
Refill Friction Stir Spot Welding with adhesive sealant: a hybrid joining system for the aeronautical industry
Department
INGEGNERIA CIVILE E INDUSTRIALE
Course of study
INGEGNERIA AEROSPAZIALE
Supervisors
relatore Prof. Lazzeri, Luigi
Keywords
  • fatigue
  • friction stir spot welding
  • helmholtz zentrum hereon
  • residual stress
  • solid state joint
Graduation session start date
23/11/2021
Availability
Withheld
Release date
23/11/2091
Summary
Refill Friction Stir Spot Welding (refill FSSW) is a solid-state process that shows great potential to be a substitute for single-point joining processes like riveting. The main objective of this study is to investigate and the mechanical behaviour of joints obtained by refill FSSW and adhesive sealant. Overlap joints in aircraft structures require the use of sealants for corrosion protection reasons, but using a sealant with an adhesive function allows to increase the mechanical properties of the joint. The result of this study supports the European project DAHLIAS (Development and Application of Hybrid joining in Lightweight Integral Aircraft structures) which involves three different countries with several research institutes and companies; Helmholtz Zentrum Hereon holds the role of coordinator. The objectives of the study can be summarized as follow:
- Characterize refill FSSW joints with adhesive sealant in terms of microstructure and residual stress;
- Investigate the static and dynamic mechanical properties of the joint and failure mechanisms;
- Optimise, in terms of mechanical properties, the joint design;
- Investigate fatigue initiation mechanism;
- Characterize the residual stress field in multi-spot joints;
- Understand the stress and strain field in different joint configurations;
- Develop a simple numerical model to evaluate different joint configurations in terms of stress distribution;
- Produce two full-scale demonstrators of aeronautical structures.
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