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Characterization of Hybrid CNT Polymer Matrix CompositesCarbon nanotubes (CNTs) have been studied extensively since their discovery and demonstrated at the nanoscale superior mechanical, electrical and thermal properties in comparison to micro and macro scale properties of conventional engineering materials. This combination of properties suggests their potential to enhance multi-functionality of composites in regions of primary structures on aerospace vehicles where lightweight materials with improved thermal and electrical conductivity are desirable. In this study, hybrid multifunctional polymer matrix composites were fabricated by interleaving layers of CNT sheets into Hexcel® IM7/8552 prepreg, a well-characterized toughened epoxy carbon fiber reinforced polymer (CFRP) composite. The resin content of these interleaved CNT sheets, as well as ply stacking location were varied to determine the effects on the electrical, thermal, and mechanical performance of the composites. The direct-current electrical conductivity of the hybrid CNT composites was characterized by in-line and Montgomery four-probe methods. For [0](sub 20) laminates containing a single layer of CNT sheet between each ply of IM7/8552, in-plane electrical conductivity of the hybrid laminate increased significantly, while in-plane thermal conductivity increased only slightly in comparison to the control IM7/8552 laminates. Photo-microscopy and short beam shear (SBS) strength tests were used to characterize the consolidation quality of the fabricated laminates. Hybrid panels fabricated without any pretreatment of the CNT sheets resulted in a SBS strength reduction of 70 percent. Aligning the tubes and pre-infusing the CNT sheets with resin significantly improved the SBS strength of the hybrid composite To determine the cause of this performance reduction, Mode I and Mode II fracture toughness of the CNT sheet to CFRP interface was characterized by double cantilever beam (DCB) and end notch flexure (ENF) testing, respectively. Results are compared to the control IM7/8552 laminate.
Document ID
20160006103
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Grimsley, Brian W.
(NASA Langley Research Center Hampton, VA, United States)
Cano, Roberto J.
(NASA Langley Research Center Hampton, VA, United States)
Kinney, Megan C.
(NASA Langley Research Center Hampton, VA, United States)
Pressley, James
(NASA Langley Research Center Hampton, VA, United States)
Sauti, Godfrey
(National Inst. of Aerospace Hampton, VA, United States)
Czabaj, Michael W.
(NASA Langley Research Center Hampton, VA, United States)
Kim, Jae-Woo
(National Inst. of Aerospace Hampton, VA, United States)
Siochi, Emilie J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
May 13, 2016
Publication Date
May 18, 2015
Subject Category
Composite Materials
Report/Patent Number
NF1676L-20258
Report Number: NF1676L-20258
Meeting Information
Meeting: SAMPE Symposium 2015
Location: Baltimore, MD
Country: United States
Start Date: May 18, 2015
End Date: May 21, 2015
Sponsors: Society for the Advancement of Materials and Process Engineering
Funding Number(s)
WBS: WBS 713030.01.07
Distribution Limits
Public
Copyright
Public Use Permitted.
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