TY - GEN
T1 - Printable epoxy carbon fiber composites and their mechanical properties
AU - Abbott, Andrew
AU - Celik, Emrah
AU - Pierson, Harry A.
AU - Koerner, Hilmar
AU - Baur, Jeffery W.
N1 - The authors would like to thank Hugh De Jarnette, Leonardo Sierra Gutierrez, and Kyle Johnson for their technical assistance. The authors would also like to thanks the AFRL Summer Faculty program and the AFRL International Cooperative Research & Development Fund for financial support.
PY - 2019
Y1 - 2019
N2 - Additive manufacturing (AM) of fiber reinforced thermosetting resins has not been well explored due to material and processing restrictions including high viscosity, poor reinforcement dispersion, dimensional tolerance, and porosity. Yet, such a process would enable tool-less and agile manufacturing of small and complex composite parts with temperature and environmental stability superior to traditional thermoplastics. Printed thermoset composites could also be combined with traditional epoxy prepregs to make complex co-cured structures. In this work, a direct write AM process for epoxy / chopped carbon fiber composites is used which has been shown to provide cured composites tensile modulus and strength values 90% and 66% of the fully aligned composite, respectively. The fibers are largely oriented in the print direction, but have sufficient localized material flow to achieve acceptable transverse properties and low porosity. Sandwich structures created with additively printed cores and co-cured prepreg face sheets were fabricated and evaluated. Rather than creating a sandwich structure by adhesively bonding standard sizes of honeycomb core to cured composite face sheets, this work examined co-curing customized additively printed core structures with prepreg face sheets. This process can be used to design and optimize properties for complex geometries while reducing the number of manufacturing steps.
AB - Additive manufacturing (AM) of fiber reinforced thermosetting resins has not been well explored due to material and processing restrictions including high viscosity, poor reinforcement dispersion, dimensional tolerance, and porosity. Yet, such a process would enable tool-less and agile manufacturing of small and complex composite parts with temperature and environmental stability superior to traditional thermoplastics. Printed thermoset composites could also be combined with traditional epoxy prepregs to make complex co-cured structures. In this work, a direct write AM process for epoxy / chopped carbon fiber composites is used which has been shown to provide cured composites tensile modulus and strength values 90% and 66% of the fully aligned composite, respectively. The fibers are largely oriented in the print direction, but have sufficient localized material flow to achieve acceptable transverse properties and low porosity. Sandwich structures created with additively printed cores and co-cured prepreg face sheets were fabricated and evaluated. Rather than creating a sandwich structure by adhesively bonding standard sizes of honeycomb core to cured composite face sheets, this work examined co-curing customized additively printed core structures with prepreg face sheets. This process can be used to design and optimize properties for complex geometries while reducing the number of manufacturing steps.
UR - https://www.scopus.com/pages/publications/85068799232
UR - https://www.scopus.com/pages/publications/85068799232#tab=citedBy
U2 - 10.33599/nasampe/s.19.1527
DO - 10.33599/nasampe/s.19.1527
M3 - Conference contribution
AN - SCOPUS:85068799232
T3 - International SAMPE Technical Conference
BT - SAMPE Conference and Exhibition
A2 - Ahlstrom, Kevin
A2 - Anderson, Jacob Preston
A2 - Beckwith, Scott
A2 - Becnel, Andrew Craig
A2 - Biermann, Paul Joseph
A2 - Buchholz, Matt
A2 - Cates, Elizabeth
A2 - Gardner, Brian
A2 - Harris, Jim
A2 - Knight, Michael J.
A2 - Reyes-Villanueva, German
A2 - Scarborough, Stephen E.
A2 - Sears, Phil
A2 - Thomas, James
A2 - Thostenson, Erik T.
PB - Soc. for the Advancement of Material and Process Engineering
T2 - SAMPE 2019 Conference and Exhibition
Y2 - 20 May 2019 through 23 May 2019
ER -