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Tesi etd-01272026-193843


Tipo di tesi
Tesi di laurea magistrale
Autore
BASILI, DARIO
URN
etd-01272026-193843
Titolo
Next-Generation Alloys for Aerospace Manufacturing: Assessing Sustainability, Mechanical Performance and Advanced Manufacturing Methods
Dipartimento
INGEGNERIA DELL'ENERGIA, DEI SISTEMI, DEL TERRITORIO E DELLE COSTRUZIONI
Corso di studi
INGEGNERIA GESTIONALE
Relatori
relatore Prof. Zerbino, Pierluigi
supervisore Prof. Pagone, Emanuele
supervisore Prof. Eimer, Eloise
Parole chiave
  • additive manufacturing
  • aerospace
  • life cycle assessment
  • next generation alloys
  • supply chain criticality
  • sustainability
Data inizio appello
26/02/2026
Consultabilità
Non consultabile
Data di rilascio
26/02/2029
Riassunto (Inglese)
Riassunto (Italiano)
The rapid expansion of commercial aviation has intensified demand for lightweight, high-performance materials while increasing environmental pressures. Next-generation alloys such as Scalmalloy®, Ti-5553, and ZK60 offer improved strength, corrosion resistance, and design flexibility - especially when combined with advanced methods like Wire Arc Additive Manufacturing (WAAM). However, their environmental sustainability, lifecycle costs, and supply-chain implications remain insufficiently explored.
This project aims to develop an evaluation framework to guide material selection by assessing alloy-route combinations across four key dimensions: mechanical performance, sustainability, cost, and supply-chain criticality. Informed by a systematic literature review, the framework was applied to two case studies: an Airbus A320 main wheel and a Boeing 787 landing-gear forging. The methodology integrates cradle-to-cradle Life Cycle Assessment, cost analysis, mechanical benchmarking, and a novel supply-chain criticality index.
Findings show that although additive manufacturing consumes more energy during production, its lower buy-to-fly ratio reduces total lifecycle energy use and emissions. Since the use phase dominates environmental and cost impacts, lighter materials are generally preferred. Scalmalloy® via WAAM achieved the best overall balance of sustainability and performance, though Ti-5553 emerged as the preferred option when mechanical performance is prioritised in safety-critical applications. These results highlight the importance of integrating mechanical, environmental, economic, and supply-chain factors to enable informed aerospace material choices and provide a practical tool for evaluating trade-offs associated with next-generation alloys.
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