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Multifunctional properties of high volume fraction aligned carbon nanotube polymer composites with controlled morphology

  • Hülya Cebeci
  • , Roberto Guzman de Villoria
  • , A. John Hart
  • , Brian L. Wardle*
  • *Bu çalışma için yazışmadan sorumlu yazar
  • Massachusetts Institute of Technology
  • University of Michigan, Ann Arbor

Araştırma sonucu: Dergiye katkıMakalebilirkişi

210 Atıf (Scopus)

Özet

Advanced composites, such as those used in aerospace applications, employ a high volume fraction of aligned stiff fibers embedded in high-performance polymers. Unlike advanced composites, polymer nanocomposites (PNCs) employ low volume fraction filler-like concepts with randomly-oriented and poorly controlled morphologies due to difficult issues such as dispersion and alignment of the nanostructures. Here, novel fabrication techniques yield controlled-morphology aligned carbon nanotube (CNT) composites with measured non-isotropic properties and trends consistent with standard composites theories. Modulus and electrical conductivity are maximal along the CNT axis, and are the highest reported in the literature due to the continuous aligned-CNTs and use of an unmodified aerospace-grade structural epoxy. Rule-of-mixtures predictions are brought into agreement with the measured moduli when CNT waviness is incorporated. Waviness yields a large (∼10×) reduction in modulus, and therefore control of CNT collimation is seen as the primary limiting factor in CNT reinforcement of composites for stiffness. Anisotropic electron transport (conductivity and current-carrying capacity) follows expected trends, with enhanced conductivity and Joule heating observed at high current densities.

Orijinal dilİngilizce
Sayfa (başlangıç-bitiş)2649-2656
Sayfa sayısı8
DergiComposites Science and Technology
Hacim69
Basın numarası15-16
DOI'lar
Yayın durumuYayınlandı - Ara 2009

Finansman

This study was supported by Airbus S.A.S., Boeing, Embraer, Lockheed Martin, Saab AB, Spirit AeroSystems, Textron Inc., Composite Systems Technology, and TohoTenax Inc. through MIT’s Nano-Engineered Composite aerospace STructures (NECST) Consortium. Hülya Cebeci acknowledges support from Scientific and Technical Research Council of Turkey (TUBITAK) for a 2214-International Research Fellowship Programme. Roberto Guzman de Villoria is grateful for the support of the Ministry of Science and Education (MEC) for the award of a FPU grant (AP-2004-6264). The authors gratefully acknowledge Patrick Boisvert for SEM imaging, Peter Morley for specimen preparation assistance, Alan Schwartzmann for nanoindentation testing and Eric Verploegen and Jeremy Ng for SAXS/WAXS analysis. The authors are grateful for the donation of materials from Hexcel Corp.

FinansörlerFinansör numarası
Airbus S.A.S.
NECST
TUBITAK
TohoTenax Inc.
Boeing
Ministarstvo znanosti i obrazovanjaAP-2004-6264
Türkiye Bilimsel ve Teknolojik Araştirma Kurumu

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