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Qualitative evaluation of failure mechanisms of aluminium 6061-T6 cold spray repairs

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Abstract

Cold spray is an emerging technology that shows great promise for the repair of civil aircraft components. However, certification of such repairs requires a comprehensive evaluation of repair performance, including a detailed assessment of repair strength and the associated failure mechanisms. The present research compared the failure mechanisms of cold-spray repaired specimens manufactured from aluminium alloy 6061-T6, produced using either a high-pressure or a low-pressure cold spray system, in tensile tests. Depending on the manufacturing process used, different failure mechanisms were observed, including cohesive failure of the deposit and failure of the deposit-substrate interface. The study suggests that failure in cold spray repair is driven by competing mechanisms, with the dominant mode influenced by both the applied load and the processing parameters, as well as the characteristics of the deposited material.
Original languageEnglish
Article number109581
Number of pages18
JournalEngineering Failure Analysis
Volume175
DOIs
Publication statusPublished - 15 Jun 2025

Funding

The authors gratefully acknowledge the financial support provided by RVO Subsidy Scheme R&D Mobility Sector (RDM) under the BrightSky Project. We would also like to extend our thanks to KLM Engineering & Maintenance for their funding and provision of the specimens, which were generously supplied prior to the initiation of the BrightSky project. We sincerely thank John-Alan Pascoe, Stratos Koufis, Myron Beukelman and Mary Patrick from TU Delft for their valuable contributions and support during the early stages of this work, as well as for their insightful reviews.

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