Integration and optimisation of a novel industrial Fused Composite Manufacturing process for prepreg filament

Master Thesis (2019)
Author(s)

J. Driezen (TU Delft - Aerospace Engineering)

Contributor(s)

Bergsma Otto – Mentor (TU Delft - Structural Integrity & Composites)

Faculty
Aerospace Engineering
Copyright
© 2019 Jorne Driezen
More Info
expand_more
Publication Year
2019
Language
English
Copyright
© 2019 Jorne Driezen
Graduation Date
04-10-2019
Awarding Institution
Delft University of Technology
Programme
['Aerospace Engineering']
Faculty
Aerospace Engineering
Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Abstract

Since the aerospace industry is continuously looking for new strong and lightweight solutions to existing aircraft parts, Fused Composite Manufacturing has much potential for future applications as it incorporates both the freedom of design and a continuous fiber reinforcement. The current state of the technology is of low maturity as engineering thermoplastics are of use with low Fiber Volume Content and part complexity is limited due 3-axis kinematics of the used printers.
As such, the research presented in this report aims to evaluate the feasibility of such FCM process with regard to aerospace applications by the integration and optimisation of a novel print head within a 6-axis industrial robot, capable of printing high performance prepreg filament in all arbitrary directions.

Files

ThesisReport_JorneDriezen.pdf
(pdf | 119 Mb)
- Embargo expired in 31-12-2024
License info not available