Tesi etd-04232024-160228 |
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Tipo di tesi
Tesi di laurea magistrale
Autore
LAZZINI, CAMILLA
URN
etd-04232024-160228
Titolo
Titanium/Composite Adhesive Joints for Aero-Engines Applications: Characterization of Damage Onset and the Effect of Thermal Cycling
Dipartimento
INGEGNERIA CIVILE E INDUSTRIALE
Corso di studi
INGEGNERIA AEROSPAZIALE
Relatori
relatore Prof. Fanteria, Daniele
supervisore Prof. Gigliotti, Marco
supervisore Dott. Bousses, Yoan
supervisore Prof. Gigliotti, Marco
supervisore Dott. Bousses, Yoan
Parole chiave
- adhesive joint
- composite materials
- thermal cycling
- thermal oxidation
- titanium
Data inizio appello
29/05/2024
Consultabilità
Non consultabile
Data di rilascio
29/05/2094
Riassunto
In the field of aero-engine applications, the integration and the synergy of titanium and composite materials stand as an innovative area of study. In this investigation, we examine the characterization of damage onset within the adhesive joints in the interface between the two materials and explore the consequential effects of the environmental and the particular conditions these material suffer from. As the demand for high-performance aircraft components continues to increase, through tests and analysis, this study aims to clarify the behaviors of these materials under varying thermal conditions, revealing potential advancements in durability and performance within the aerospace industry.
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