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Undirectional Carbon Nanotube Yarn/Polymer CompositesCarbon nanotubes (CNTs) are one-dimensional nanomaterials with outstanding electrical and thermal conductivities and mechanical properties at the nanoscale. With these superior physical properties, CNTs are very attractive materials for future light weight structural aerospace applications. Recent manufacturing advances have led to the availability of bulk formats of CNTs such as yarns, tapes, and sheets in commercial quantities, thus enabling the development of macroscale composite processing methods for aerospace applications. The fabrication of unidirectional CNT yarn/polymer composites and the effect of processing parameters such as resin type, number of CNT yarn layers, CNT yarn/resin ratio, consolidation method, and tension applied during CNT yarn winding on the mechanical properties of unidirectional CNT yarn composites are reported herein. Structural morphologies, electrical and thermal conductivities, and mechanical performance of unidirectional CNT yarn/polymer composites under tensile and short beam shear loads are presented and discussed. The application of higher tension during the winding process and elevated cure pressure during the press molding step afforded a compact structural morphology and reduced void content in the composite. However, the composite tensile strength was negligibly impacted by the fabrication parameters, such as cure pressure, winding tension, and resin chemistry, excepting resin content and number of CNT yarn layers. The tension winding method produced better quality and lower resin content CNT yarn composites compared to conventional prepregging methods, resulting in higher specific strength and modulus of the composites. The specific tensile strength of the CNT composite was approximately 69 % of the starting CNT yarn. Electrical and thermal conductivities of unidirectional CNT yarn/polymer composites were in the range of 1000 to 12000 S/cm and 22 to 45 W/mK, respectively.
Document ID
20180006317
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Kim, Jae-Woo
(National Inst. of Aerospace Hampton, VA, United States)
Sauti, Godfrey
(NASA Langley Research Center Hampton, VA, United States)
Wincheski, Russell A.
(NASA Langley Research Center Hampton, VA, United States)
Cano, Roberto J.
(NASA Langley Research Center Hampton, VA, United States)
Jensen, Benjamin D.
(NASA Langley Research Center Hampton, VA, United States)
Smith, Joseph G.
(NASA Langley Research Center Hampton, VA, United States)
Wise, Kristopher E.
(NASA Langley Research Center Hampton, VA, United States)
Siochi, Emilie J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
October 16, 2018
Publication Date
July 1, 2018
Subject Category
Composite Materials
Report/Patent Number
NASA/TM-2018-220081
NF1676L-30688
L-20949
Distribution Limits
Public
Copyright
Public Use Permitted.
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