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Damage study of fiber-reinforced composites drilled by abrasive waterjet —challenges and opportunities
- Source :
- The International Journal of Advanced Manufacturing Technology. 119:41-55
- Publication Year :
- 2021
- Publisher :
- Springer Science and Business Media LLC, 2021.
-
Abstract
- Owing to their excellent properties such as lightweight and high strength, fiber-reinforced composite materials are widely used as ideal materials for key structural components in extreme service environments (e.g., aviation, aerospace, and nuclear power). However, due to their non-uniformity and anisotropy, they have become typical difficult-to-machine materials, which are prone to cause damage during machining, thereby reducing the service life of the entire component. This review primarily summarizes the damage (including delamination, thermal damage, tool wear, and other processing damages) and suppression strategies of scholars in the process of traditional and non-traditional machining of fiber-reinforced composite materials in the past few years. Besides reviewing the research progress, the limitations of the current research were presented. From this review, it can be seen that traditional and non-traditional (e.g., laser machining) machining methods are difficult to avoid damage. Abrasive waterjet (AWJ) machining is a green and environmentally friendly machining technology. Some key issues are expected to be furtherly solved during the AWJ drilling of fiber-reinforced composite materials with low damage.
- Subjects :
- Engineering
business.industry
Mechanical Engineering
Delamination
Abrasive
Mechanical engineering
Fiber-reinforced composite
Environmentally friendly
Industrial and Manufacturing Engineering
Computer Science Applications
Machining
Control and Systems Engineering
Service life
Tool wear
Aerospace
business
Software
Subjects
Details
- ISSN :
- 14333015 and 02683768
- Volume :
- 119
- Database :
- OpenAIRE
- Journal :
- The International Journal of Advanced Manufacturing Technology
- Accession number :
- edsair.doi...........267be7e05c42069bb0c5a46b837c72b9