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Mesoscale evolution of non-graphitizing pyrolytic carbon in aligned carbon nanotube carbon matrix nanocomposites

Authors :
Brian L. Wardle
Alexander J. Constable
Luiz Acauan
Itai Y. Stein
Ashley L. Kaiser
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Massachusetts Institute of Technology. Department of Materials Science and Engineering
Massachusetts Institute of Technology. Department of Mechanical Engineering
Kaiser, Ashley Louise
Stein, Itai Y
Chichester-Constable, Alexander
Acauan, Luiz Henrique H
Wardle, Brian L
Source :
Springer US
Publication Year :
2017
Publisher :
Springer Science and Business Media LLC, 2017.

Abstract

Polymer-derived pyrolytic carbons (PyCs) are highly desirable building blocks for high-strength low-density ceramic meta-materials, and reinforcement with nanofibers is of interest to address brittleness and tailor multi-functional properties. The properties of carbon nanotubes (CNTs) make them leading candidates for nanocomposite reinforcement, but how CNT confinement influences the structural evolution of the PyC matrix is unknown. Here, the influence of aligned CNT proximity interactions on nano- and mesoscale structural evolution of phenol-formaldehyde-derived PyCs is established as a function of pyrolysis temperature (Tₚ) using X-ray diffraction, Raman spectroscopy, and Fourier transform infrared spectroscopy. Aligned CNT PyC matrix nanocomposites are found to evolve faster at the mesoscale by plateauing in crystallite size at Tₚ ∼ 800°C, which is more than 200°C below that of unconfined PyCs. Since the aligned CNTs used here exhibit ∼ 80 nm average separations and ∼ 8 nm diameters, confinement effects are surprisingly not found to influence PyC structure on the atomic-scale at Tₚ ≤ 1400°C. Since CNT confinement could lead to anisotropic crystallite growth in PyCs synthesized below ∼ 1000°C, and recent modeling indicates that more slender crystallites increase PyC hardness, these results inform fabrication of PyC-based meta-materials with unrivaled specific mechanical properties.<br />National Science Foundation (U.S.). Research Experience for Undergraduates (Program) (grant number DMR-08-19762)<br />Massachusetts Institute of Technology. Materials Processing Center<br />United States. Department of Defense (National Defense Science & Engineering Graduate Fellowship (NDSEG) Program)<br />Airbus Group<br />Boeing Company<br />Embraer<br />Lockheed Martin<br />Saab (Firm)<br />ANSYS, Inc.<br />Hexcel (Firm)<br />Toho Tenax Co., Ltd. (MIT’s Nano-Engineered Composite aerospace STructures (NECST) Consortium)

Details

ISSN :
15734803 and 00222461
Volume :
52
Database :
OpenAIRE
Journal :
Journal of Materials Science
Accession number :
edsair.doi.dedup.....17d0a473abefd2e7c26396deced1d453