Preparation of Homogeneously Dispersed Multiwalled Carbon Nanotube/Polystyrene Nanocomposites via Melt Extrusion Using Trialkyl Imidazolium Compatibilizer

Well‐dispersed multiwalled carbon nanotube (MWNT)/polystyrene nanocomposites have been prepared via melt extrusion, using trialkylimidazolium tetrafluoroborate‐compatibilized MWNTs. Quantification of the improvement is realized via transmission electron microscopy and laser scanning confocal microsc...

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Bibliographic Details
Published in:Advanced functional materials Vol. 15; no. 6; pp. 910 - 916
Main Authors: Bellayer, S., Gilman, J. W., Eidelman, N., Bourbigot, S., Flambard, X., Fox, D. M., De Long, H. C., Trulove, P. C.
Format: Journal Article
Language:English
Published: Weinheim WILEY-VCH Verlag 01-06-2005
WILEY‐VCH Verlag
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Summary:Well‐dispersed multiwalled carbon nanotube (MWNT)/polystyrene nanocomposites have been prepared via melt extrusion, using trialkylimidazolium tetrafluoroborate‐compatibilized MWNTs. Quantification of the improvement is realized via transmission electron microscopy and laser scanning confocal microscopy image analysis. Differential scanning calorimetry and Fourier‐transform infrared and X‐ray diffraction analysis show evidence for a π‐cation, nanotube–imidazolium interaction and the conversion from an interdigitated bilayer, for the imidazolium salt, to an ordered lamellar structure, for the imidazolium on the surface of the MWNTs. Well‐dispersed multiwalled carbon nanotube (MWNT)/ polystyrene nanocomposites (see Figure) are prepared via melt extrusion, using trialkylimidazolium tetrafluoroborate (DMHDIm‐TFB)‐compatibilized MWNTs. Quantification of the nanodispersion was realized via transmission electron microscopy (TEM) and laser scanning confocal microscopy image analysis. The Figure shows a TEM image of polystyrene with 1:1 imidazolium‐treated MWNT and the corresponding analysis plot.
Bibliography:ark:/67375/WNG-83JWLFP3-K
ArticleID:ADFM200400441
istex:BD03A16D8217EAD74A62406D87817DE2CA998599
The authors thank the Air Force Office of Scientific Research (AFOSR-ISSA-01-0001) and the Federal Aviation Administration (DTFA 03-99-X-9009) for funding, and thank Dr. Kalman Migler for use of the mini-extruder and Dr. Li Piin Sung for use of the LSCM facilities.
The authors thank the Air Force Office of Scientific Research (AFOSR‐ISSA‐01‐0001) and the Federal Aviation Administration (DTFA 03‐99‐X‐9009) for funding, and thank Dr. Kalman Migler for use of the mini‐extruder and Dr. Li Piin Sung for use of the LSCM facilities.
ISSN:1616-301X
1616-3028
DOI:10.1002/adfm.200400441