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Low-Cost Carbon Fibers
Andrea Forrest, Louisiana
Tech University
Jon Pierce, Alfred
University
Willie Jones, Clemson
University
Esther Hwu, Emory
University
Environmental regulations on automobile emissions
increase the need for lighter automobiles. One way to reduce
vehicle weight without losing any structural and mechanical
strength is to use carbon fiber reinforced composites. Unfortunately,
high production costs have limited the widespread use of carbon
fibers. The current cost of carbon fibers is approximately
$15/pound. In order for carbon fibers to be used widely, the
costs need to be lowered to $5/pound or less. To reach this
goal, alternate precursors need to be explored and the heat
treatments involved in stabilizing and carbonizing the fibers
need to be optimized. Therefore, the goal of this research
was to explore alternate, potentially low-cost routes for
carbon fiber production.
Currently 90% of all commercial carbon fibers
are produced by the thermal conversion of a polyacrylonitrile
(PAN) precursor fiber (1, 2). In these processes a solution
of 10 to 30% by weight of a PAN copolymer in a highly polar
solvent such as sodium thiocyanate or dimethylacetamide is
extruded through a multihole spinneret into a coagulation
bath. As the solution exits the multihole spinneret and enters
the bath it precipitates forming a multifilament bundle. The
bundle is washed to remove excess solvent, stretched to increase
the molecular orientation within the filaments, and finally
wound onto a takeup bobbin. Next the PAN precursor fiber is
heated in air to temperatures ranging from 230 to 280°C
for times ranging from 30 minutes to two hours. During this
step oxygen diffuses into the fibers and crosslinking occurs.
Finally, the crosslinked fibers are heated in an inert environment
to approximately 1300°C. This drives off the non-carbon
elements, yielding a carbon fiber.
One obvious method for reducing the price
is to utilize melt-spinning rather than solution spinning
to produce the precursor fiber. Melt-spinning is inherently
less expensive than solution-spinning because it eliminates
the extra cost of solvent handling and it also operates at
much higher throughputs. Another possible approach is to employ
a precursor that contains more carbon. PAN precursor fiber
actually contains only 68% carbon. Therefore, two pounds of
PAN precursor fiber normally yield about a pound of carbon
fiber. By comparison, potential carbon fiber precursors such
as pitch and high carbon content polymers contain between
80 to 90% carbon. If one of these materials could be melt
spun and successfully converted into carbon fibers, the overall
process conversion could be substantially increased. In this
preliminary study, both approaches were explored and both
appear to offer promise for reducing process costs.
The materials investigated in our experiments
were a Mitsubishi® PAN (95% PAN, 5% methyl acrylate)
pre-spun fiber, and isotropic pitch, and Amlon® (80%
PAN, 20% methylacrylate) precursors. The Mitsubishi®
PAN is a commercial precursor fiber that is solution-spun.
This fiber served as a control for comparing the final carbonized
properties of the melt-spun fibers produced in our study.
The Amlon® PAN copolymer was supplied by BP-Amoco, and
the isotropic pitch was supplied by Conoco, Inc. These two
precursors melt below their degradation temperatures (the
prerequisite for melt-spinning). Also, the carbon content
of the isotropic pitch was greater than 85%. Thus, the Amlon®
precursor allowed us to explore the advantages, as well as
evaluate the problems, associated with producing carbon fiber
using a melt-spinnable PAN precursor. By contrast, the isotropic
pitch allowed us to evaluate the benefits as well as penalties
of producing carbon fiber with a high-carbon content precursor.
A Haake rheometer was used to determine
the optimum spinning temperature for the Amlon® and
the isotropic pitch precursors. Then, a batch melt spinning
apparatus was used to melt-spin fibers from the two precursors
(Figure 1). This involved first attaching a multihole spinneret
to the bottom of the melting chamber of the apparatus. Then,
solid pellets of each precursor were loaded into the chamber.
Next, the extrusion piston was inserted and the chamber was
purged with nitrogen. An electrical heating system was then
attached, and the chamber heated to the optimum spinning temperature.
After the precursor temperature reached equilibrium, the piston
drive motor was turned on and set to a predetermined speed.
This lowered the piston at a fixed speed, forcing the precursor
through the multihole spinneret at a fixed rate. The surrounding
air-cooled the molten precursor as it emerged from the spinneret
capillaries, forming fibers. These fibers were collected on
a takeup roll that was set to a predetermined rotation rate.

Figure 1. Batch melt-spinning apparatus.
A two-step process was used in our initial
attempts to convert these melt-spun precursor fibers into
carbon fibers. As a control, the Mitsubishi® PAN (95%
PAN, 5% methyl acrylate) pre-spun fiber was also converted
to carbon fibers using the same two-step process. This allowed
us to compare the final properties of carbon fibers produced
from the two melt-spun precursors with those of a commercial
solution-spun precursor fiber that had been subjected to a
similar conversion process.
In the first step of this thermal treatment
process, the precursor fibers were inserted in an oven with
air circulation, heated to just below their softening point,
and held at this temperature for a set amount of time. A flame
test was used as a measure of complete stabilization. This
involved placing the stabilized fibers in a flame. If the
fibers glowed red and did not melt, stabilization was considered
to be successful. In the second and final step of the thermal
treatment process, the stabilized fibers were placed in an
Astro furnace, purged with helium and heated to either 1200°C
or 1500°C for 30 minutes.
Once the fibers were carbonized, they were mounted
individually on tabs and tested using the MTI for tensile
properties. Fibers were mounted on glass slides for Raman
spectroscopy analysis. Also, fibers were mounted on cartridges
for the S-4700 scanning electron microscope.
The Mitsubishi® PAN-based pre-spun fibers
were used as a control in our experiments. The fibers were
stabilized for two hours at 230°C, 240°C, or 250°C.
Then they were carbonized at 1200°C and 1500°C for
30 minutes. The mechanical testing results for the Mitsubishi®
PAN fibers are shown below in Figures 2 and 3.
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| Figure 2:
Strength of Mitsubishi® Pan |
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Figure 3:
Modulus of Mitsubishi® Pan |
Isotropic pitch-based fibers were spun at 250°C, and then
were chemically and thermally stabilized. The fibers were
chemically stabilized by soaking them in a 15wt% to 70wt%
nitric acid solution for various lengths of time. These fibers
were then carbonized but could not be tested because they
were stuck together. Thermal stabilization followed a four-day
heating schedule: 180°C for 24hrs, 200°C for 24hrs,
220°C for 24hrs, and 240°C for 24hrs. Some fibers
were heated at either 260°C or 270°C for two additional
hours. These fibers were then carbonized at 1200°C and
1500°C for 30 minutes. Isotropic pitch fibers that were
stabilized at 260°C and 1200°C had a tensile strength
and modulus close to those of commercially produced pitch
fibers. The mechanical testing results for isotropic pitch
are shown in Figures 4 and 5.
Amlon® fibers were spun at 230-235°C, and then stabilized
using the following schedule: 180°C for 24hrs, then 230°C
for 2hrs, and then some of the fibers were ramped to 250°C
for an additional 2hrs. After being stabilized at these conditions,
the Amlon® fibers were carbonized. After carbonization
a visual inspection showed that some sticking had occurred
between the fibers. This indicated that these stabilization
conditions were not ideal.
Amlon® PAN and the isotropic pitch were
both successfully melt spun into precursor fibers. Melt spinning
carbon fibers from an Amlon® PAN precursor could lower
the production costs because it eliminates the solvents used
in wet spinning. However, heat treatment trials showed that
standard oxidative stabilization of a melt-spun PAN is likely
to require process times on the order of days. Obviously,
alternate stabilization methods will need to be developed
if this melt-spinnable PAN copolymer is to be commercially
practical. The isotropic pitch precursor offers the additional
potential advantage of high process conversions. This precursor
also required long stabilization times. Nevertheless, stabilization
was successful and fibers could be carbonized and mechanically
tested. Although isotropic pitch-based carbon fibers display
strengths approximately one third that of PAN-based fibers,
the precursors cost much less than PAN precursors. Slight
modifications of the chemical compositions of isotropic pitch
and Amlon® PAN are likely to make them practical for
industrial applications. Also, alternate methods of stabilization
should be evaluated in future research.
The authors wish to thank Jane Jacobi, director
of the Center for Advanced Engineering Fibers and Films National
Science Foundation Research Experiences for Undergraduates
program. We also would like to thank our faculty advisor,
Dr. Dan Edie, of Clemson University as well as our industrial
advisors, Mark Southard and Ernie Romine, of Conoco, Inc.
This work was supported primarily by the ERC Program of the
National Science Foundation under Award Number EEC-9731680.
1. Edie, D. D., "Carbon Fiber Processing
and Structure/Property Relations," in Design and Control
of Structure of Advanced Carbon Materials for Enhanced Performance,
B. Rand et al. (eds.), Kluwer Academic Publishers, Netherlands
(2001) pp. 163-181.
2. Edie, D. D. "The Effect of Processing
on the Structure and Properties of Carbon Fibers," Carbon,
36(11), pp. 345-362 (1998).
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