[0001] This invention relates to a process for manufacturing carbon fiber by carbonizing
a precursor comprising a polyacrylonitrile polymer, and more particularly to the
stabilization of the precursor prior to carbonization.
[0002] Carbon fiber is useful in a variety of applications for which its mechanical, chemical
and electrical properties are uniquely suited, particularly for making lightweight
composites comprising the fiber in inorganic or organic matrices.
[0003] Although the cost of carbon fiber has been decreasing significantly even while its
properties and reliability have been improved, there are still problems in some aspects
of its production. In particular, the stabilization step in which polyacrylonitrile
polymer, in the form of a tow comprising a multitude of filaments, is heated in air
or other oxygen-containing gaseous medium prior to carbonization, adversely limits
the rate at which carbon fiber can be manufactured on a commercial scale.
[0004] Such stabilization through oxidation is rate-limiting because of the risk of fusing
the filaments or even causing an uncontrollable self-generating reaction (a "thermal
runaway") if the precursor is heated too fast or too high during the stabilization.
It is customary to use certain comonomers, such as acrylic acid, in forming the polyacrylonitrile
polymer filaments in order to permit initiation of the oxidation reaction at a temperature
lower than that otherwise required, e.g. between about 200 and 400°C. There is risk
of thermal runaway even at such lower temperatures, but the risk is less and there
is obviously less risk of fusion of the filaments.
[0005] However, to produce carbon fiber having uniform properties requires strict control
of the amounts of the comonomer that is used to permit oxidation at lower temperatures,
which presents production problems in addition to the rate limitation caused by the
need to maintain a relatively low temperature.
[0006] The problems associated with the stabilization step have been extensively studied,
for instance, in "Studies on Carbonization of Polyacrylonitrile Fibre - Part 5: Changes
in Structure with Pyrolysis of Polyacrylonitrile Fibre: by Miyamichi, et al., Journal
of Society of Fibre Science and Technology, Japan,
22, No. 12, 538 - 547 (1966).
[0007] U.S. Patent 4,104,004 suggests dividing up the stabilization step so that the precursor
is heated in separate temperature zones, and U.S. Patents 3,775,520 and 3,954,950,
while they suggest driving off residual solvent and producing controlled shrinkage
by an initial brief heating step in an inert atmosphere prior to oxidizing the precursor,
also limit the initial heating step to prevent stabilization from occurring.
[0008] There is still need for a process for manufacturing carbon fiber having uniform
properties from a polyacrylonitrile polymer carbon fiber that reduces the risk of
thermal runaway and fusion of the filaments while increasing the possible rates of
reaction. It is also desirable to permit the use of polyacrylonitrile homopolymer,
which is more economical to make than the comonomers conventionally used to reduce
the temperature of oxidation.
[0009] According to the invention, a process for manufacturing carbon fiber in which a polyacrylonitrile
polymer in the form of a multitude of filaments is heated in an oxygen-containing
atmosphere to form a stabilized and oxidized precursor that is then carbonized in
an atmosphere substantially free of oxygen, is characterized in that the polyacrylonitrile
filaments are heated in an atmosphere that is substantially free of oxygen to form
a thermally stabilized carbon fiber precursor prior to the step of heating the filaments
in an oxygen-containing atmosphere to oxidize the thermally-stabilized precursor.
[0010] By that process, the precursor is readily and safely stabilized in a form that is
capable of being oxidized for subsequent carbonization below the range of temperatures
ordinarily used for oxidation, or alternatively permits the use of conventional oxidation
temperatures or even higher temperatures to achieve a faster rate of oxidation. The
carbonization conditions after oxidation follow the conventional procedures for making
carbon fiber from polyacrylonitrile precursor.
[0011] Polyacrylonitrile polymers conventionally used as precursors for carbon fiber manufacture,
and conventional procedures for the manufacture of such precursors are well known,
for instance from U.S. Patents 4,001,382, 4,009,248, 4,397,831 and 4,452,860. While
the same polyacrylonitrile polymers are preferred as precursors for carbon fiber manufacture
according to the invention, a greater variety of polyacrylonitrile polymers may be
used. For example, polyacrylonitrile homopolymer may be used as a precursor and is
readily stabilized by the process of this invention.
[0012] Preferably, the atmosphere that is substantially free of oxygen consists essentially
of nitrogen or other inert gas, although a vacuum may be also used. The temperature
to which the precursor is heated is preferably at least about 130°C, more preferably
at least about 230°C.but may be up to 500°C or higher without risk of thermal runaway.
Typically, one or more tows each comprising a multitude of continuous filaments traveling
as a band are heated in a furnace or oven for stabilization in that inert atmosphere
according to the invention. The stabilization step takes from a few minutes up to
about an hour or more depending on the temperature chosen and may be conducted in
a series of steps, if desired.
[0013] The duration of the stabilization step may be pre-determined by a conventional technique
that measures thermal rearrangement, such as by differential scanning calorimetry
(DSC). The reduction in residual heat of reaction measured by DSC in an inert atmosphere
before and after the stabilization step is an appropriate measure of thermal rearrangement,
and preferably is from about 10% to about 35%, more preferably by about 20%.
[0014] The diameter of filaments within the tow preferably ranges between 1 and 10 microns,
although the magnitude of such diameter is not critical in accordance with this invention.
Moreover, each tow may comprise between 500 and 20,000 filaments per tow. The conventional
use of surface treatments on the filaments within the tow does not detract from the
benefits of this invention.
[0015] After being thermally stabilized, the tows are may be oxidized at temperatures ranging
surprisingly as low as room temperature or even lower, but it is preferred that oxidation
take place in a gaseous medium containing oxygen such as air at temperatures ranging
between 150°C and 300°C for a time sufficient to allow these thermally stabilized
tows to be self supporting (i.e. to retain dimensional integrity) during carbonization.
Too high a temperature during oxidation is undesirable unless such heating takes place
in apparatus for carrying away thermal decomposition products of the fiber being oxidized.
[0016] While undergoing stabilization in the non-oxidizing atmosphere or oxidation, the
band of filaments may be stretched to a length longer than its original length, held
constant in length or allowed to shrink as desired.
[0017] After oxidation, the thermally stabilized and oxidized precursor tows are carbonized
using conventional techniques for making carbon fibers. For example, the stabilized
and oxidized precursor tow is heated in an inert atmosphere or vacuum at a temperature
between about 500°C and 800°C for tar removal followed by heating at higher temperatures,
also in nitrogen or other non-oxidizing atmosphere, to yield a carbonized fiber suitable
for use with or without surface treatment according to conventional practice.
[0018] The following examples illustrate the invention, and Figures 1 - 14 graphically
display the results of tests made according to the examples. The DSC apparatus used
was a DuPont 910 DSC Module with a Model 1090 or like controller. The X-axis in Figures
1 through 11C is temperature in degrees centigrade. The Y-axis is heat flow in milliwatts.
Figures 12, 13 and 14 show load (tension) in grams per denier versus degree of reaction
in percent. The degree of reaction is determined using density.
[0019] The sample size in Figure 1 was 1.136 milligrams. The rate of temperature increase
was 10 degrees centigrade per minute and was in air. The sample size in Figure 2 was
1.110 milligrams and the rate of temperature increase was 10 degrees centigrade per
minute in nitrogen. The sample type and rate of temperature increase are set forth
below for the data in Figures 3 - 11C.
Figure |
Sample Size |
Type |
Rate |
3 |
1.332 mg |
AB |
10 |
4 |
1.396 mg |
CE |
10 |
5 |
1.369 mg |
AB |
10 |
6 |
1.320 mg |
CE |
10 |
7 |
0.243 mg |
AB |
10 |
8 |
0.791 mg |
CE |
10 |
9 |
1.246 mg |
DUP |
10 |
10 |
8.826 mg |
DUP |
10 |
11 |
4.624 mg |
DUP |
10 |
11A |
1.332 mg |
DUP |
10 |
11B |
1.327 mg |
DUP |
10 |
11C |
3.178 mg |
DUP |
10 |
[0020] In Figures 1 and 2 DSC was respectively in air and nitrogen. DSC of Figures 3 and
4 was in nitrogen. DSC was in air for Figures 5, 6 (both purge) and 7 and 8 (second
heating). Figure 9 of the DSC was in air (purge) and DSC was in nitrogen (Figure
10) and then in air in Figure 11. Figure 11A was run in nitrogen; Figure 11B run in
air; and Figure 11C is rerun in air after initial heating in nitrogen.
Examples
[0021] In the work described below "AB Precursor" and "CE Precursor, are standard carbon
fiber precursors made from acrylonitrile and methacrylic acid (2 weight %) in the
case of the AB precursor and acrylonitrile, methylacrylate and itaconic acid in case
of the CE precursor.
[0022] Several experiments were initially run with varying degrees of nitrogen (N₂) pretreatment
and then analyzed thermally. As seen in Figures 1 and 2, the amount of change in heats
of decomposition (H
D) between precursor heated in air and heated in nitrogen (N₂) were different. These
differences are typical for acrylic polymers heated in oxygen containing and oxygen
free atmospheres with the low H
D (in N₂) due to thermal rearrangement reactions and the large H
D in air due to thermal rearrangement and oxidation reactions. Table 1 shows the results
of two experiments where precursor was first pretreated in N₂ at elevated temperatures.
TABLE 1
HEATS OF DECOMPOSITION IN AIR AND N₂ |
|
Air |
HD cal/gm |
N₂ |
AB Precursor (Baseline) |
1121 |
|
165 |
Pretreatment: 235°C, 55 min in N₂ |
943 |
|
116 |
Pretreatment: 235°C, 116 min in N₂ |
844 |
|
90.8 |
[0023] The change in H
D was 178 cal/g when heated in air after pretreatment in N₂ but only 49 cal/g when
heated in N₂ after the same nitrogen pretreatment for the first sample and 277 cal/g
when heated in air after pretreatment and only 74 cal/g when heated in N₂ after pretreatment
for the second. Since the pretreatment heating was carried out in N₂, it might be
expected that the change in H
D would be the same in both air and N₂. However, from this data at least part of the
oxidation reaction is not involved with or linked to the rearrangement reaction. If
the sample 1 pretreatment (235°C/55 min) had been run in air instead of N₂, the residual
H
D, air would be 740 cal/g. The N₂ preheat generated only 49 cal/g, but lowered the
H
D, air by 178 cal/g, so it appears that 129 cal/g of reaction with oxygen was by-passed
by the N₂ preheat. The N₂ preheat for 116 min at 235°C generated 74 cal/g and lowered
the H
D, air by 277 cal/g so it by-passed 203 cal/g of the expected reaction with oxygen.
It is evident that the chemical structure of the fiber is different when preheated
in N₂ prior to air oxidation.
[0024] Samples of four different polyacrylonitrile polymers were thermally analyzed in nitrogen
and air to better define the mechanisms that were occurring. As part of the analysis,
ground precursor fiber was first analyzed in nitrogen, up to about 430°C. The results
are shown in Figure 3 (AB Precursor) and 4 (CE Precursor). The results were not unusual;
an exponentially-increasing heat evolution peaking at about 285-290°C, followed by
a rapid heat decrease to give about 100-135 cal/g evolved heat. The resultant thermally-stabilized
powder was then reweighed and reanalyzed, this time in air. Normally the air oxidation
curve will follow the route shown in Figure 5 (AB Precursor) and Figure 6 (CE Precursor).
Instead, the curve shape was markedly changed. The area under the curve was significantly
reduced, from about 1000-1100 cal/g to about 250 cal/g for AB Precursor and 335 cal/g
for CE Precursor. In addition, the oxidation-initiation temperature was reduced about
20°C, indicating that the oxidation would be more rapid than non-prestabilized fiber
(Figures 7 and 8). Additionally, the position of the two major thermal peaks shifted.
For the AB Precursor the shift was more dramatic, with the lower peak dropping from
a typical 228°C to 212°C. The position of the higher-temperature peak increased from
326°C to 360°C for AB Precursor while it decreased for CE Precursor from 330°C to
315°C.
[0025] These results suggest a major change in the oxidation reactions. There appear to
be more oxidatively-active sites after the nitrogen pretreatment as evidenced by the
decrease in initiation temperature. There also appears to be less overall oxidation,
or possibly less dehydrogenation, as evidenced by the higher temperature which may
imply more oxidative stability or may simply mean that the influence of the lower-temperature
reactions is dissipated leaving only the higher-temperature part of the response.
[0026] The thermal analysis of DuPont T-42 polymer, a commercial grade polyacrylonitrile
polymer fiber, in air (Figure 9) indicates that it would be a less suitable precursor
than AB Precursor due to its high initiation temperature and rapid heat evolution
rate. If the precursor is first prestabilized in N₂ (Figure 10) and then reheated
in air (Figure 11), the thermal response changes dramatically, similar to what has
been seen with the other acrylic polymers. The reaction initiation temperature has
decreased substantially, the single peak has split into two very distinct peaks, and
the total heat of reaction is only 34 cal/gm.
[0027] PAN homopolymer, which is typically avoided at present as a carbon fiber precursor
in commercial practice because of its slow reaction rate, high rate of that evolution
once it begins to react, and high initiation temperature was also found to undergo
dramatic changes in thermal characteristics once it was prestabillzed. Figure 11A
shows the typical DSC curve for this polymer in nitrogen with a heat of decomposition
of 124 cal/gm, while Figure 11B shows the thermal curve in air. The heat of reaction
in air (1103 cal/gm) is typical of other acrylic polymers, but the homopolymer is
characterized by a high initiation temperature (250°C) and rapid heat evolution rate
(steep slope). When the polymer is prestabilized by running the DSC in nitrogen and
then rerun in air, the changes are dramatic (Figure 11C). The initiation temperature
drops to 155°C with the single peak splitting into two distinct peaks, the rate of
heat evolution drops significantly as evidenced by a change in initial slope (note
change in y-axis range between Figures 11B and 11C), and the overall heat of reaction
has dropped to 237 cal/gm. Those results indicate the polymer may make a much more
suitable carbon fiber precursor from the standpoint of ease of processability, safety,
and potentially, economics.
[0028] These data also suggest that the fiber will be more easily oxidized after prestabilization.
As such, a fiber that has been prestabilized and oxidized for a given time at temperature
will have a higher density than a fiber that is only oxidized for the same time at
temperature. A set of experiments was run to determine if this is true; the results
are shown in Table 2 below.
TABLE 2
DU PONT T-42 PRESTABILIZATION AND OXIDATION DENSITIES |
Conditions |
Density (g/cc) |
235°C, 2 hr, air |
1.2688 |
235°C, 1 hr, N₂; then |
|
235°C, 1 hr, air |
1.2904 |
235°C, 1 hr, air |
|
235°C, 1 hr, N₂ |
1.2101 |
[0029] The fiber that has been prestabilized and oxidized does exhibit a higher density
than the fiber that has just been oxidized at the same temperature for the same amount
of time. This is believed due to the increase in reactivity after prestabilization
since prestabilization alone results in a rate of density increase that is less than
that due to oxidation in air (Table 2 and Figure 12). Looking at the density difference
between the oxidized and prestabilized/oxidized fibers and assuming kinetics similar
to the reaction kinetics of the AB Precursor for comparison purposes, the increase
in oxidized fiber density due to prestabilization corresponds to a time savings of
40 minutes at 235°C. That is, in order to reach the same oxidized density as the prestabilized/oxidized
fiber, the precursor fiber would have to be oxidized for 160 minutes at 235°C instead
of stabilized/oxidized for a total of 120 minutes at 235°C.
[0030] Another way to monitor the reaction characteristics of an acrylic based precursor
is to follow the tension that is generated as the fiber rearranges and oxidizes at
elevated temperatures. Tension vs time data were generated for AB and DuPont precursors
and prestabilized fibers to further clarify changes in oxidation reaction characteristics
that are caused by prestabilization in an inert atmosphere.
[0031] Figure 13 shows load/time data for AB precursor in air at 235°C, N₂ at 235°C, and
for AB prestabilized for varying amounts of time and then run in air at 235°C. Comparing
the samples run in air and N₂ (no stabilization), both samples shorn the characteristic
drop in tension initially followed by a tension increase as the fiber begins to react.
The tension increase due to the shrinkage of the sample run in N₂ is significantly
less than in air, the difference presumably being due to the added shrinkage of the
oxidation reactions occurring in air.
[0032] The prestabilized fibers show a sudden increase in tension when run in air possibly
indicating an initial increase in the degree of reactivity. The load build up quickly
levels out for the 60 minute prestabilized fiber, followed by 30 minute, and 5 minute
which has a final load after 60 minutes, similar to AB Precursor. These lower oxidation
loads could be due to a lower overall oxidation reactivity for the prestabilized
fibers that would agree with DTA results showing lower than expected residual heats
of reaction in air after prestabilization.
[0033] The results for the DuPont T-42 type fiber are shown in Figure 14. This fiber is
characteristically slower to react than AB as evidenced by the slow load buildup for
the AB 10 Precursor. After prestabilization, the shrinkage characteristics of the
fiber are greatly altered. The tension increase with time, while not as great as for
AB Precursor, is similar in shape, indicating the fiber may oxidize more readily after
prestabilization. As with the prestabilized AB Precursor samples, the T-42 type fibers
show a rapid initial increase in tension (the greater the degree of prestabilization,
the greater the rate of tension buildup). After 60 minutes, the more highly prestabilized
fiber has a lower load buildup than the other prestabilized fiber (similar to AB results)
but both samples are significantly higher than the baseline indicating the prestabilization
(even after as little as five minutes) results in an increase in oxidation reaction
rate, but may reduce the number of sites available for reaction. These results indicate
that prestabilization can be used to make certain precursor fibers more reactive while
also increasing the safety of the process by reducing the oxidation exotherm.
[0034] Another interesting finding from these experiments is that prestabilization changes
fiber reactively sufficiently to cause a subsequent reaction in air at room temperature.
[0035] A set of AB fibers were stabilized in N₂ at 250°C for times ranging from 5 minutes
to 6 hours. In each case, the sample was then divided in half, with half placed in
an inert atmosphere and the other half stored in air, both at room temperature. In
all cases, the sample in air continued to change color and slowly darken while the
sample in N₂ remained golden brown. It was found that this reaction could be suspended
by placing the partially darkened sample in N₂ and then reinitiated by exposing again
to air. The fibers exposed to air after prestabilization were able to oxidize at room
temperature. If oxidation type reactions were indeed occurring, it would be expected
that the residual heat of reaction would decrease with increasing time of exposure
to air at room temperature. A series of experiments was per- formed to determine if
this was indeed the case. In one set of experiments, a length of AB Precursor was
stabilized in N₂ for 2 hours at 250°C; the fiber was divided in half with half exposed
to room-temperature air for 3 hours and the other half exposed to air for 24 hours.
The samples were then restored in N₂ and submitted for thermal analysis. In all cases,
the thermal lab was careful to run the samples as quickly as possible after the N₂
seal was broken. In the second experiment, a sample of AB Precursor was stabilized
for 16 hours at 250°C in N₂ and then divided with parts exposed for 0 hours, 1 hour,
3 hours, and 24 hours in air. Samples were then restored in N₂ and thermally analyzed.
The results are shown in Table 3 below:
TABLE 3
CHANGE IN Hair OF STABILIZED FIBERS AFTER VARYING AMOUNTS OF EXPOSURE TIME IN AIR |
Stabilization Conditions in N₂ |
Air Exposure Time at Room Temperature (hr) |
Hair |
2 hours at 250°C |
3 |
684 |
2 hours at 250°C |
24 |
624 |
16 hours at 250°C |
0 |
678 |
16 hours at 250°C |
1 |
652 |
16 hours at 250°C |
3 |
605 |
16 hours at 250°C |
24 |
548 |
[0036] For both sets of these experiments, the heat of reaction decreased with time of exposure
in air, indicating a reaction occurring at room temperature which is responsible for
the color change we had noted. A stabilized fiber was also run to determine if free
radicals are present, which might be initiating the reaction at room temperature in
air. The results indicated the presence of some free radical activity, which is as
yet unidentified.
1. A process for manufacturing carbon fiber in which a polyacrylonitrile polymer in
the form of a multitude of filaments is heated in an oxygen-containing atmosphere
to form a stabilized and oxidized precursor that is then carbonized in an atmosphere
substantially free of oxygen, is characterized in that the polyacrylonitrile filaments
are heated in an atmosphere that is substantially free of oxygen to form a thermally
stabilized carbon fiber precursor prior to the step of heating the filaments in an
oxygen-containing atmosphere to oxidize the thermally-stabilized precursor.
2. A process for manufacturing carbon fiber as claimed in claim 1, further characterized
in that the temperature to which the polyacrylonitrile filaments are heated in an
atmosphere that is substantially free of oxygen is heated is preferably at least
about 230°.
3. A process for manufacturing carbon fiber as claimed in claim 1, further characterized
in that the atmosphere that is substantially free of oxygen is nitrogen.
4. A process for manufacturing carbon fiber as claimed in claim 1, 2, or 3, further
characterized in that the polyacrylonitrile filaments are heated in an atmosphere
that is substantially free of oxygen until the reduction in residual heat of reaction
as measured by differential scanning calorimetry is from about 10% to about 35%.
5. A process for manufacturing carbon fiber as claimed in claim 4, further characterized
in that the filaments are heated until the reduction in residual heat of reaction
is about 20%.
6. A process for manufacturing carbon fiber as claimed in any of the preceding claims,
further characterized in that the thermally stabilized carbon fiber precursor in the
form of a tow is heated in an oxygen-containing atmosphere at a temperature from 150°C
to 300°C for a time sufficient to allow the tow to be self supporting.
7. A process for manufacturing carbon fiber as claimed in any of the preceding claims,
further characterized in that the polyacrylonitrile filaments in the form of a band
of closely spaced tows are moved in an atmosphere that is substantially free of oxygen
through an oven maintained at a first range of temperatures to heat the filaments
to form a thermally stabilized carbon fiber precursor and then are moved at a higher
line speed in an oxygen-containing atmosphere through an oven maintained at a second
range of temperatures to oxidize the thermally-stabilized precursor.