FIELD OF THE INVENTION
[0001] The present invention relates to a carbon fiber manufacturing technique, and more
particularly to a carbon fiber manufacturing method and a carbon fiber manufacturing
apparatus which can greatly improve the sizing quality of a carbon fiber and effectively
reduce the cost of the carbon fiber production equipment and the working time.
BACKGROUND OF THE INVENTION
[0002] Carbon fibers are classified into carbon fibers or graphite fibers according to their
carbon contents, which have excellent mechanical properties and electrical properties
and can be widely used in various applications. A conventional carbon fiber is achieved
by bundling precursor fibers, such as polyacrylonitrile fibers, to form a carbon fiber
precursor fiber bundle, and then the carbon fiber precursor fiber bundle is calcined
(high-temperature carbonization) to form the carbon fiber.
[0003] There are various precursor fibers of carbon fibers on the market, such as rayon,
poly vinyl alcohol, vinylidene chloride, polyacrylonitrile (PAN), pitch, and the like.
In general, polyacrylonitrile (PAN) is used as the raw material of carbon fibers.
The manufacturing steps are generally as follows: PAN raw material (precursor fiber)
→ pre-oxidation → high-temperature carbonization → surface treatment → sizing.
[0004] In the carbonization step, the carbon fiber precursor fiber bundles are heated to
form carbon fibers or graphite fibers by different heating apparatuses according to
the application of the carbon fibers. In principle, the carbon content of the fibers
of graphite fibers is 90% or more, forming a two-dimensional carbocyclic planar net
structure and a graphite layer structure having parallel layers. The results show
that the crystalline region of a high-strength carbon fiber is composed of 5-6 graphite
layers, and the crystalline region of a high-strength and high-modulus carbon fiber
is composed of 10-20 graphite layers. Theoretically and practically, it is pointed
out that the larger the crystalline thickness of the graphite layer is, the higher
the tensile modulus of the carbon fiber is.
[0005] On the other hand, the surface of the carbon fiber after the high-temperature carbonization
step is usually coated with a layer of oiling agent (a resin oiling agent is generally
used, it is called as a sizing step) before it leaves the factory. The layer of oiling
agent is used to protect the fiber from breakage due to friction in the subsequent
step to affect the overall quality of the carbon fiber. The surfaces of untreated
carbon fibers adsorb impurities thereon. Since these impurities are present between
the surface of the carbon fiber and the resin oiling agent, the adhesion between the
carbon fiber and the resin oiling agent is insufficient, and the purpose of protecting
the fiber cannot be achieved
[0006] Furthermore, in the high-temperature carbonization step, the surface of the carbon
fiber is excessively finely formed due to high-temperature sintering, and there are
few functional groups on the surface. As a result, the fiber and the resin oiling
agent cannot be bonded fully in the sizing step. It is known that a heat treatment
or electrolysis technique can be applied to the surface treatment of the fiber after
the high-temperature carbonization step, and then the sizing step is performed in
order to improve the bonding of the fiber and the resin oiling agent.
[0007] However, when the surface treatment of the carbon fiber is performed by means of
heat treatment, the carbon fiber is treated at a temperature in the range of 500°C
to 800°C for 1-10 minutes. A relatively long period of time is required. Besides,
the heat treatment is always performed with a large number of fibers at a time, so
it is difficult to control the processing quality. When the surface treatment of the
carbon fiber is performed by means of electrolysis, at least one drying process is
required before the surface of the fiber is coated with the oiling agent. This also
takes more time. Moreover, a change of the electrolyte may affect the processing quality.
Even the surface of the fiber may have depositions.
[0008] Accordingly, the inventor of the present invention has devoted himself based on his
many years of practical experiences to solve these problems.
SUMMARY OF THE INVENTION
[0009] In view of the problems of the prior art, the primary object of the present invention
is to provide a carbon fiber manufacturing method which can greatly improve the sizing
quality of a carbon fiber and effectively reduce the cost of the carbon fiber production
equipment and the working time.
[0010] In order to achieve the forgoing object, the carbon fiber manufacturing method of
the present invention comprises providing a raw material step, providing a carbon
fiber precursor fiber bundle; performing a high-temperature carbonization step, the
carbon fiber precursor fiber bundle being heated to form a carbon fiber having a predetermined
carbon content; performing a plasma surface treatment step, a plasma gas flow with
a predetermined power being provided to act on the carbon fiber at a predetermined
time so that a surface of the carbon fiber is formed with a plasma-modified configuration;
performing a sizing step, the plasma-modified configuration being coated with a resin
oiling agent; and performing a drying step, the resin oiling agent coated on the plasma-modified
configuration being processed with drying so that the resin oiling agent is firmly
adhered to the surface of the carbon fiber.
[0011] In the carbon fiber manufacturing method of the present invention, through the plasma
surface treatment step, the surface of the carbon fiber is roughened and provided
with functional groups, which is beneficial to enhance the interface bonding of the
resin oiling agent and the carbon fiber in the subsequent sizing step so as to improve
the sizing quality of the carbon fiber greatly. The structure of the carbon fiber
is more stable and reliable. The plasma surface treatment belongs to a dry-type and
fast surface treatment technique to effectively reduce the cost of the carbon fiber
production equipment and the working time.
[0012] Preferably, in the high-temperature carbonization step, the carbon fiber precursor
fiber bundle is guided into a chamber. The chamber is formed with at least one microwave
field concentration area therein, and is provided with a gas supply assembly to supply
an inert gas and a microwave generating assembly to supply a high-frequency microwave.
Under the protection of the inert gas atmosphere, the electric field of the high-frequency
microwave produces a sensing current to heat up and produce a high temperature quickly
with the carbon fiber precursor fiber bundle passing through the microwave field concentration
area.
[0013] Preferably, the chamber is provided with at least one pair of microwave-sensitive
materials.
[0014] Preferably, the microwave-sensitive materials are one of graphite, carbide, magnetic
compound, nitride, and ionic compound or a combination thereof.
[0015] Preferably, the inert gas is nitrogen, argon, helium, or a combination thereof.
[0016] Preferably, the frequency of the high-frequency microwave is in the range of 300-30,000
MHz, and its microwave power density is in the range of 1-1000kW/m3.
[0017] Preferably, the chamber is an elliptic chamber.
[0018] Alternatively, the chamber is a flat panel chamber.
[0019] Preferably, in the plasma surface treatment step, the plasma gas flow with a power
of 100-10000 watts acts on the carbon fiber for 10-1000 milliseconds.
[0020] Alternatively, in the plasma surface treatment step, an atmospheric plasma gas flow
with a power of 100-10000 watts acts on the carbon fiber for 10-1000 milliseconds.
[0021] Alternatively, in the plasma surface treatment step, a low-pressure plasma gas flow
with a power of 100-10000 watts acts on the carbon fiber for 10-1000 milliseconds.
[0022] Alternatively, in the plasma surface treatment step, a microwave plasma gas flow
with a power of 100-10000 watts acts on the carbon fiber for 10-1000 milliseconds.
[0023] Alternatively, in the plasma surface treatment step, a glow plasma gas flow with
a power of 100-10000 watts acts on the carbon fiber for 10-1000 milliseconds.
[0024] Preferably, the carbon fiber precursor fiber bundle has a surface not processed with
a pre-oxidation treatment.
[0025] Alternatively, the carbon fiber precursor fiber bundle has a surface processed with
a pre-oxidation treatment in advance.
[0026] Preferably, the resin oiling agent is a thermosetting resin oiling agent.
[0027] Alternatively, the resin oiling agent is a thermoplastic resin oiling agent.
[0028] Preferably, the carbon content of the carbon fiber is in the range of 80%-90%.
[0029] In order to achieve the forgoing object, the carbon fiber manufacturing apparatus
of the present invention comprises a feeding module, a receiving module, a high-temperature
carbonization module, a plasma surface treatment module, and a sizing module. The
receiving module is disposed in the vicinity of the feeding module. The feeding module
and the receiving module constitute a carbon fiber drag route. The high-temperature
carbonization module is disposed at the carbon fiber drag route and located between
the feeding module and the receiving module for heating the carbon fiber drag route.
The plasma surface treatment module is disposed at the carbon fiber drag route and
located between the high-temperature carbonization module and the receiving module
for supplying a plasma gas flow to the carbon fiber drag route. The sizing module
is disposed at the carbon fiber drag route and located between the plasma surface
treatment module and the receiving module for coating a resin oiling agent on the
surface of a carbon fiber.
[0030] Thereby, the carbon fiber manufacturing apparatus of the present invention can be
operated in the integrated operation of the feeding module, the high-temperature carbonization
module, the plasma surface treatment module, the sizing module, and the receiving
module. A carbon fiber precursor fiber bundle released from the feeding module is
sequentially processed at a predetermined speed to perform the steps of high-temperature
carbonization, plasma surface treatment, sizing, and so on, in a relatively more active
and reliable manner. The carbon fiber precursor fiber bundle is heated to form the
carbon fiber, and then the surface of the carbon fiber is formed with the resin oiling
agent. Particularly, through the plasma surface treatment module, the surface of the
carbon fiber is roughened and provided with functional groups, which is beneficial
to enhance the interface bonding of the resin oiling agent and the carbon fiber in
the subsequent sizing procedure so as to improve the sizing quality of the carbon
fiber greatly. The structure of the carbon fiber is more stable and reliable. The
plasma surface treatment belongs to a dry-type and fast surface treatment technique
to effectively reduce the cost of the carbon fiber production equipment and the working
time.
[0031] Preferably, the high-temperature carbonization module has a chamber for the carbon
fiber drag route or the carbon fiber precursor fiber bundle to pass therethrough.
The chamber is formed with at least one microwave field concentration area and supplies
an inert gas and a high-frequency microwave. Under the protection of the inert gas
atmosphere, the electric field of the high-frequency microwave produces a sensing
current to heat up and produce a high temperature quickly with the carbon fiber precursor
fiber bundle passing through the microwave field concentration area.
[0032] Preferably, the high-temperature carbonization module has a chamber for the carbon
fiber drag route or the carbon fiber precursor fiber bundle to pass therethrough.
The chamber is formed with at least one microwave field concentration area and provided
with a gas supply assembly to supply an inert gas and a microwave generating assembly
to supply a high-frequency microwave. Under the protection of the inert gas atmosphere,
the electric field of the high-frequency microwave produces a sensing current to heat
up and produce a high temperature quickly with the carbon fiber precursor fiber bundle
passing through the microwave field concentration area. The plasma surface treatment
module is provided with at least one plasma generator.
[0033] Preferably, the plasma surface treatment module is provided with at least one plasma
generator located at upper and lower positions of the carbon fiber drag route, respectively.
[0034] Preferably, the chamber is an elliptic chamber.
[0035] Preferably, the chamber is an elliptic chamber, and the chamber is provided with
at least one pair of microwave-sensitive materials.
[0036] Alternatively, the chamber is a flat plate chamber.
[0037] Alternatively, the chamber is a flat plate chamber, and the chamber is provided with
at least one pair of microwave-sensitive materials.
[0038] Preferably, the plasma generator is able to generate the plasma gas flow having a
power in the range of 100-10000 Watts.
[0039] Alternatively, the plasma generator is able to generate an atmospheric plasma gas
flow having a power in a range of 100-10000 Watts.
[0040] Alternatively, the plasma generator is able to generate a low-pressure plasma gas
flow having a power in the range of 100-10000 Watts.
[0041] Alternatively, the plasma generator is able to generate a microwave plasma gas flow
having a power in the range of 100-10000 Watts.
[0042] Alternatively, the plasma generator is able to generate a glow plasma gas flow having
a power in the range of 100-10000 Watts.
[0043] Preferably, the sizing module is provided with at least one reservoir.
[0044] Preferably, the carbon fiber manufacturing apparatus further comprises a drying module.
The drying module is disposed at the carbon fiber drag route between the sizing module
and the receiving module for the resin oiling agent to be adhered to the surface of
the carbon fiber firmly.
[0045] Specifically, through plasma surface treatment, the surface of the carbon fiber can
be roughened and provided with the functional groups, which is beneficial to enhance
the interface bonding of the resin oiling agent and the carbon fiber in the subsequent
sizing step. The structure of the carbon fiber is more stable and reliable. By the
microwave focusing heating way, the same apparatus can be applied to a carbon fiber
precursor fiber bundle whose surface has not been processed with a pre-oxidation treatment
or a carbon fiber precursor fiber bundle whose surface has been processed with a pre-oxidation
treatment in advance. By simply adjusting the microwave power, the apparatus can be
used to produce general carbon fibers or high modulus carbon fibers (graphite fibers)
so as reduce the cost of the carbon fiber production equipment and the working time
effectively.
BRIEF DESCRIPTION OF THE DRAWINGS
[0046]
FIG. 1 is a flow diagram of a carbon fiber manufacturing method of the present invention;
FIG. 2 is a structural schematic view of a high-temperature carbonization module in
accordance with an embodiment of the present invention;
FIG. 3 is a sectional schematic view of a carbon fiber after finishing a plasma surface
treatment step of the present invention;
FIG. 4 is a sectional schematic view of a carbon fiber after finishing a sizing step
of the present invention;
FIG. 5 is a structural schematic view of a high-temperature carbonization module in
accordance with another embodiment of the present invention;
FIG. 6a illustrates a SEM image of an object to be tested without plasma treatment;
and
FIG. 6b illustrates a SEM image of an object to be tested with the plasma treatment.
FIG. 7 is a structural schematic view of a carbon fiber manufacturing apparatus in
accordance with a first embodiment of the present invention; and
FIG. 8 is a structural schematic view of a carbon fiber manufacturing apparatus in
accordance with a second embodiment of the present invention.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0047] Embodiments of the present invention will now be described, by way of example only,
with reference to the accompanying drawings.
[0048] The present invention discloses a carbon fiber manufacturing method which can greatly
improve the sizing quality of carbon fibers and effectively reduce the cost of the
carbon fiber production equipment and the working time. As shown in FIG. 1, the carbon
fiber manufacturing method of the present invention comprises providing a raw material
step, performing a high-temperature carbonization step, performing a plasma surface
treatment step, and performing a sizing step. The carbon fiber manufacturing method
further comprises performing a drying step after the sizing step. Referring to FIG.
1 through FIG. 5, the steps are described in details as below.
[0049] In the step of providing the raw material, a carbon fiber precursor fiber bundle
is provided to be processed to form a carbon fiber. In practice, the carbon fiber
precursor fiber bundle may be formed of rayon, poly vinyl alcohol, vinylidene chloride,
polyacrylonitrile (PAN), pitch, and the like. The surface of the carbon fiber precursor
fiber bundle may have not been processed with a pre-oxidation treatment or have been
processed with a pre-oxidation treatment in advance.
[0050] In the high-temperature carbonization step, the carbon fiber precursor fiber bundle
is heated to form the carbon fiber having a predetermined carbon content. In practice,
as shown in FIG. 2, the carbon fiber precursor fiber bundle 70A is guided into a chamber
31 of a high-temperature carbonization module 30. The chamber 31 is formed with at
least one microwave field concentration area 311 therein, and is provided with a gas
supply assembly 32 to supply an inert gas and a microwave generating assembly 33 to
supply a high-frequency microwave. Under the protection of the inert gas atmosphere,
the electric field of the high-frequency microwave produces a sensing current to heat
up and produce a high temperature quickly with the carbon fiber precursor fiber bundle
70A passing through the microwave field concentration area 311, enabling the carbon
fiber precursor fiber bundle to form the carbon fiber 70B having a predetermined carbon
content. The carbon content of the carbon fiber 70B is in the range of 80%-90%.
[0051] In the plasma surface treatment step, a plasma gas flow with a predetermined power
is provided to act on the carbon fiber 70B at a predetermined time, such that the
surface of the carbon fiber 70B is formed with a plasma-modified configuration 71,
shown in FIG. 3, which is rougher or has more functional groups relative to the carbon
fiber precursor fiber bundle 70A.
[0052] In the sizing step, the plasma-modified configuration 71 on the surface of the carbon
fiber 70B is coated with a resin oiling agent 80, so that the surface of the carbon
fiber 70B has the resin oiling agent 80, as shown in FIG. 4. In practice, the resin
oiling agent 80 is coated on the surface of the carbon fiber 70B by soaking or immersing.
The resin oiling agent 80 may be a thermosetting resin oiling agent or a thermoplastic
resin oiling agent.
[0053] In the drying step, a drying treatment is applied to the resin oiling agent 80 coated
on the plasma-modified configuration 71 so that the resin oiling agent 80 is firmly
adhered to the surface of the carbon fiber 70B. In practice, the drying treatment
is carried out by ultraviolet irradiation, cooling, drying or air-drying for the resin
oiling agent to be bonded to the surface of the carbon fiber.
[0054] In the plasma surface treatment step, an atmospheric plasma gas flow, a low-pressure
plasma gas flow, a microwave plasma gas flow, or a glow plasma gas flow with a power
of 100-10000 watts may be used to act on the carbon fiber 10B for 10-1000 milliseconds.
Since the plasma gas flow contains particles having energy, the impurities that originally
adhere to the surface of the carbon fiber 10B can be broken to form small molecules
by the impact of the plasma gas flow through the physical reaction (collision) of
the plasma gas flow, and then the small molecules are blown away from the surface
of the carbon fiber 70B by the air flow, so that the surface of the carbon fiber 70B
is clean. In the sizing step, the resin oiling agent 80 can be completely in contact
with the carbon fiber 70B to increase the bonding effect. In addition, the impact
of the plasma gas flow will also form the plasma-modified configuration 71 on the
surface of the carbon fiber 70B. The plasma-modified configuration 71 is rougher relative
to the carbon fiber precursor fiber bundle 70A, and is further formed with pores.
The surface of the carbon fiber 70B is roughened or formed with the pores, which is
beneficial to increase the contact area between the resin oiling agent 80 and the
carbon fiber 70B in the subsequent sizing step. The resin oiling agent 80 penetrates
into the pores, and the resin oiling agent 80 is anchored between the pores to form
an anchor effect to enhance the bonding effect of the resin oiling agent 80 and the
carbon fiber 70B.
[0055] The plasma gas flow also makes the surface of the carbon fiber 70B generate a chemical
reaction at the same time, so that at least one functional group (such as -OH, -N,
etc.) is added to the surface of the carbon fiber 70B. In the sizing step, the surface
tension of the surface of the carbon fiber 70B is increased due to the presence of
the functional group, which is beneficial to improve the wetting effect for the resin
oiling agent 80 to be coated on the carbon fiber 70B. That is, the contact angle of
the resin oiling agent 80 to the carbon fiber 70B becomes small, so that the resin
oiling agent 80 can be quickly or instantaneously coated on the carbon fiber 70B,
and the speed of the sizing step is increased, thereby accelerating the overall production
speed of the carbon fiber 70B. The presence of the functional group such as the OH
group reacts with the resin oiling agent 80, such as epoxy resin (Epoxy), to generate
hydrogen bonding, thereby increasing the bonding effect.
[0056] Thereby, in the carbon fiber manufacturing method of the present invention, through
the plasma surface treatment step, the surface of the carbon fiber 70B is roughened
and provided with functional groups, which is beneficial to enhance the interface
bonding of the resin oiling agent 80 and the carbon fiber 70B in the subsequent sizing
step so as to improve the sizing quality of the carbon fiber 70B greatly. The structure
of the carbon fiber is more stable and reliable. The plasma surface treatment belongs
to a dry-type and fast surface treatment technique to effectively reduce the cost
of the carbon fiber production equipment and the working time.
[0057] Furthermore, the foregoing inert gas may be nitrogen, argon, helium, or a combination
thereof. The frequency of the high-frequency microwave may be in the range of 300-30,000
MHz, and its microwave power density may be in the range of 1-1000kW/m3.
[0058] In the embodiment as shown in FIG. 2, the chamber 31 of the high-temperature carbonization
module 30 may be an elliptic chamber, or the chamber 31 may be a flat plate chamber
as shown in FIG. 5. As shown in FIG. 5, whatever the chamber 31 is, the chamber 31
is provided with a pair of microwave-sensitive materials 34 therein, thereby enhancing
the focusing effect on the microwave field in order to further accelerate the high-temperature
carbonization process. In practice, the microwave-sensitive materials 34 may be one
of graphite, carbide, magnetic compound, nitride, and ionic compound or a combination
thereof.
[0059] Due to the resonant effect of microwave heating, the carbonization of the carbon
fiber is enhanced rapidly and more crystalline carbons are formed and stacked, which
leads to the formation of larger graphite crystalline molecules, namely, larger graphite
crystalline thickness, while deriving a higher microwave induction heating effect
is derived. Such a cycle generates an autocatalytic reaction, enabling the carbon
fiber to be rapidly heated to the graphitization temperature (1500- 3000°C), and carbon
atoms are reconstructed and rearranged more rapidly to form a graphite layer.
[0060] In other words, the same apparatus can be applied to a carbon fiber precursor fiber
bundle whose surface has not been processed with a pre-oxidation treatment or a carbon
fiber precursor fiber bundle whose surface has been processed with a pre-oxidation
treatment in advance. It is only necessary to adjust the microwave power for the production,
the apparatus can be used to produce general carbon fibers (1000-1500°C) or high modulus
carbon fibers (graphite fibers).
[0061] In a preferred embodiment, an object to be tested that the resin oiling agent after
the drying step is firmly adhered to the surface of the carbon fiber, and the treatment
conditions in the plasma surface treatment step are shown in Table 1 below:
Table 1: the conditions of the plasma surface treatment
| plasma gas consumption |
N2 |
200 |
L/min |
| CDA |
0.4 |
L/min |
| plasma gas amount |
200.4 |
L/min |
| plasma power |
0∼1000 |
W |
| plasma surface treatment time |
0.025∼0.100 |
sec. |
| carbon fiber yarn width |
7 |
mm |
| yarn per unit time receiving capacity |
0.28 |
J/s |
| distance |
1 |
mm |
[0062] The ILSS strength (interlayer bonding force) was measured for an object to be tested
in an environment of a temperature of 23°C and a humidity of 50% RH by using an INSTRON
measuring machine according to ASTM 2344, and the results are shown in Table 2 below:
Table 2: the relationship between the plasma surface treatment power (W), the processing
time (sec.), and the interlayer bonding force (MPa) (epoxy resin used as the resin
oiling agent) of PAN carbon fiber 12K.
| plasma power (W) of surface treatment |
interlayer bonding force (ILSS)(MPa) |
| 0.025 sec. |
0.075 sec. |
0.100 sec. |
| 0(untreated) |
70 |
70 |
70 |
| 250 |
71 |
73 |
75 |
| 500 |
73 |
76 |
81 |
| 750 |
75 |
81 |
85 |
| 900 |
79 |
86 |
88 |
| 1000 |
83 |
89 |
91 |
[0063] As can be seen from Table 2, the carbon fiber without the plasma surface treatment,
the interlayer bonding force of the object to be tested is only 70MPa. With an increase
of the plasma power, for example, the processing time is 0.075 seconds and the plasma
power is increased from the untreated (0W, without plasma power) to 1000W, the interlayer
bonding force is increased from 70MPa to 89MPa. That is, the interlayer bonding force
is increased to 127%.
[0064] In the sizing step, the epoxy resin is used as the resin oiling agent, and the carbon
fiber is used as the carbon fiber 70B. FIG. 6a shows a SEM image of the object to
be tested without the plasma treatment. FIG. 6b shows a SEM image of the object to
be tested with the plasma treatment. As shown in FIG. 6a, the SEM image of the object
to be tested without the plasma surface treatment illustrates a void H between the
resin oiling agent 80 and the carbon fiber 70B because the surface of the carbon fiber
70B is smooth and doesn't have functional groups. The void H causes a decrease in
the strength of the object to be tested. That is to say, the bonding force between
the carbon fiber and the resin oiling agent is insufficient for protecting the fiber.
[0065] As shown in FIG. 6b, the SEM image of the object to be tested with the plasma surface
treatment illustrates that there is no void between the resin oiling agent 80 and
the carbon fiber 70B because the surface of the carbon fiber 70B is rough and has
functional groups (such as -OH, -N, etc.). The resin oiling agent 80 and the carbon
fiber 70B are bonded tightly, so that the strength of the object to be tested is enhanced.
That is, the adhesion between the carbon fiber and the resin oiling agent is enhanced,
so that the purpose of protecting the fiber can be achieved.
[0066] In order to implement the aforesaid carbon fiber manufacturing method, the present
invention further discloses a carbon fiber manufacturing apparatus which can greatly
improve the sizing quality of carbon fibers and effectively reduce the cost of the
carbon fiber production equipment and the working time. As shown in FIG. 7, the carbon
fiber manufacturing apparatus of the present invention comprises a feeding module
10, a receiving module 20, a high-temperature carbonization module 30, a plasma surface
treatment module 40, and a sizing module 50.
[0067] The feeding module 10 is to perform the step of providing a raw material in the carbon
fiber manufacturing method, and is used to supply a carbon fiber precursor fiber bundle
70A to be processed into a carbon fiber 70B.
[0068] The receiving module 20 is disposed in the vicinity of the feeding module 10, and
corresponds to the feeding module 10 to constitute a carbon fiber drag route. The
receiving module 20 includes a yarn winding assembly 21 to receive the carbon fiber
70B. The yarn winding assembly 21 performs a drag action on the carbon fiber 70B to
be received.
[0069] The high-temperature carbonization module 30 is to perform the high-temperate carbonization
step in the carbon fiber manufacturing method. The high-temperature carbonization
module 30 is disposed at the carbon fiber drag route between the feeding module 10
and the receiving module 20 for heating the carbon fiber precursor fiber bundle 70A,
enabling the carbon fiber precursor fiber bundle 70A to become the carbon fiber 70B
having a predetermined carbon content.
[0070] The plasma surface treatment module 40 is to perform the plasma surface treatment
step in the carbon fiber manufacturing method. The plasma surface treatment module
40 is disposed at the carbon fiber drag route between the high-temperature carbonization
module 30 and the receiving module 20 to provide a plasma gas flow with a predetermined
power to act on the carbon fiber 70B, such that the surface of the carbon fiber 70B
is formed with a plasma-modified configuration 71 which is rougher or has more functional
groups relative to the carbon fiber precursor fiber bundle 70A.
[0071] The sizing module 50 is to perform the sizing step in the carbon fiber manufacturing
method. The sizing module 50 is disposed at the carbon fiber drag route between the
plasma surface treatment module 40 and the receiving module 20 for the plasma-modified
configuration 71 on the surface of the carbon fiber 70B to be coated with a resin
oiling agent 80. The sizing module 50 is provided with at least one reservoir 51 for
storing the resin oiling agent 80.
[0072] As shown in FIG. 8, the carbon fiber manufacturing apparatus of the present invention
may further comprise a drying module 60. The drying module 60 is to perform the drying
step in the carbon fiber manufacturing method. The drying module 60 is disposed at
the carbon fiber drag route between the sizing module 50 and the receiving module
20 for the resin oiling agent 80 to be firmly adhered to the surface of the carbon
fiber 70B. In practice, the drying module 60 is provided with at least one blast furnace
61 to generate hot blast.
[0073] Thereby, the carbon fiber manufacturing apparatus of the present invention can be
operated in the integrated operation of the feeding module 10, the high-temperature
carbonization module 30, the plasma surface treatment module 40, the sizing module
50, and the receiving module 20. The carbon fiber precursor fiber bundle 70A released
from the feeding module 10 is sequentially processed at a predetermined speed to perform
the steps of high-temperature carbonization, plasma surface treatment, sizing, and
so on, in a relatively more active and reliable manner. The carbon fiber precursor
fiber bundle 70A is heated to form the carbon fiber 70B, and then the surface of the
carbon fiber 70B is formed with the resin oiling agent 80.
[0074] The plasma surface treatment module 40 is provided with at least one plasma generator
41 for generating a plasma gas flow. In an embodiment, the plasma surface treatment
module 40 is provided with at least one plasma generator 41 disposed at the upper
and lower positions of the carbon fiber drag route respectively for generating a plasma
gas flow to act on the surface of the carbon fiber 70B.
[0075] Compared to the prior art, through the carbon fiber manufacturing method and the
carbon fiber manufacturing apparatus of the present invention, the surface of the
carbon fiber can be roughened and provided with the functional groups by the plasma
surface treatment step, which is beneficial to enhance the interface bonding of the
resin oiling agent and the carbon fiber in the subsequent sizing step. The structure
of the carbon fiber is more stable and reliable to improve the quality of the carbon
fiber, thereby accelerating the overall production speed of the carbon fiber. By the
microwave focusing heating way, the same apparatus can be applied to a carbon fiber
precursor fiber bundle whose surface has not been processed with a pre-oxidation treatment
or a carbon fiber precursor fiber bundle whose surface has been processed with a pre-oxidation
treatment in advance. By simply adjusting the microwave power, the apparatus can be
used to produce general carbon fibers or high modulus carbon fibers (graphite fibers)
so as reduce the cost of the carbon fiber production equipment and the working time
effectively.
[0076] Although particular embodiments of the present invention have been described in detail
for purposes of illustration, various modifications and enhancements may be made without
departing from the spirit and scope of the present invention. Accordingly, the present
invention is not to be limited except as by the appended claims.
1. A carbon fiber manufacturing method, comprising:
providing a raw material step, providing a carbon fiber precursor fiber bundle (70A);
performing a high-temperature carbonization step, the carbon fiber precursor fiber
bundle (70A) being heated to form a carbon fiber (70B) having a predetermined carbon
content;
performing a plasma surface treatment step, a plasma gas flow with a predetermined
power being provided to act on the carbon fiber (70B) at a predetermined time so that
a surface of the carbon fiber (70B) is formed with a plasma-modified configuration
(71);
performing a sizing step, the plasma-modified configuration (71) being coated with
a resin oiling agent (80); and
performing a drying step, the resin oiling agent (80) coated on the plasma-modified
configuration (71) being processed with drying so that the resin oiling agent (80)
is firmly adhered to the surface of the carbon fiber (70B).
2. The carbon fiber manufacturing method as claimed in claim 1, wherein in the high-temperature
carbonization step, the carbon fiber precursor fiber bundle (70A) is guided into a
chamber (31), the chamber (31) is formed with at least one microwave field concentration
area (311) therein and is provided with a gas supply assembly (32) to supply an inert
gas and a microwave generating assembly (33) to supply a high-frequency microwave,
under the protection of the inert gas atmosphere, an electric field of the high-frequency
microwave produces a sensing current to heat up and produce a high temperature quickly
with the carbon fiber precursor fiber bundle (70A) passing through the microwave field
concentration area (311).
3. The carbon fiber manufacturing method as claimed in claim 2, wherein the chamber (31)
is provided with at least one pair of microwave-sensitive materials (34).
4. The carbon fiber manufacturing method as claimed in claim 3, wherein the microwave-sensitive
materials (34) are one of graphite, carbide, magnetic compound, nitride, and ionic
compound or a combination thereof.
5. The carbon fiber manufacturing method as claimed in claim 2, wherein the inert gas
is nitrogen, argon, helium, or a combination thereof.
6. The carbon fiber manufacturing method as claimed in claim 2, wherein the frequency
of the high-frequency microwave is in the range of 300-30,000 MHz, and its microwave
power density is in the range of 1-1000kW/m3.
7. The carbon fiber manufacturing method as claimed in claim 2, wherein the chamber (31)
is an elliptic chamber.
8. The carbon fiber manufacturing method as claimed in claim 2, wherein the chamber (31)
is a flat panel chamber.
9. The carbon fiber manufacturing method as claimed in claim 1, wherein in the plasma
surface treatment step, the plasma gas flow, an atmospheric plasma gas flow, a low-pressure
plasma gas flow, a microwave plasma gas flow, or a glow plasma gas flow with a power
of 100-10000 watts acts on the carbon fiber (70B) for 10-1000 milliseconds.
10. The carbon fiber manufacturing method as claimed in claim 1, wherein the carbon fiber
precursor fiber bundle (70A) has a surface not processed with a pre-oxidation treatment.
11. The carbon fiber manufacturing method as claimed in claim 1, wherein the carbon fiber
precursor fiber bundle (70A) has a surface processed with a pre-oxidation treatment
in advance.
12. The carbon fiber manufacturing method as claimed in claim 1, wherein the resin oiling
agent (80) is a thermosetting resin oiling agent.
13. The carbon fiber manufacturing method as claimed in claim 1, wherein the resin oiling
agent (80) is a thermoplastic resin oiling agent.
14. The carbon fiber manufacturing method as claimed in claim 1, wherein the carbon content
of the carbon fiber (70B) is in the range of 80%-90%.
15. A carbon fiber manufacturing apparatus, comprising:
a feeding module (10) and a receiving module (20), the receiving module (20) being
disposed in the vicinity of the feeding module (10), the feeding module (10) and the
receiving module (20) constituting a carbon fiber drag route;
a high-temperature carbonization module (30), disposed at the carbon fiber drag route
and located between the feeding module (10) and the receiving module (20) for heating
the carbon fiber drag route;
a plasma surface treatment module (40), disposed at the carbon fiber drag route and
located between the high-temperature carbonization module (30) and the receiving module
(20) for supplying a plasma gas flow to the carbon fiber drag route; and
a sizing module (50), disposed at the carbon fiber drag route and located between
the plasma surface treatment module (40) and the receiving module (20).
16. The carbon fiber manufacturing apparatus as claimed in claim 15, wherein the high-temperature
carbonization module (30) has a chamber (31), a gas supply assembly (32), and a microwave
generating assembly (33), the carbon fiber drag route passes through the chamber (31),
the gas supply assembly (32) is used to supply an inert gas, and the microwave generating
assembly (33) is used to supply a high-frequency microwave.
17. The carbon fiber manufacturing apparatus as claimed in claim 16, wherein the plasma
surface treatment module (40) is provided with at least one plasma generator (41).
18. The carbon fiber manufacturing apparatus as claimed in claim 16, wherein the plasma
surface treatment module (40) is provided with at least one plasma generator (41)
located at upper and lower positions of the carbon fiber drag route, respectively.
19. The carbon fiber manufacturing apparatus as claimed in claim 16, wherein the chamber
(31) is an elliptic chamber.
20. The carbon fiber manufacturing apparatus as claimed in claim 19, wherein the chamber
(31) is provided with at least one pair of microwave-sensitive materials (34).
21. The carbon fiber manufacturing apparatus as claimed in claim 16, wherein the chamber
(31) is a flat plate chamber.
22. The carbon fiber manufacturing apparatus as claimed in claim 21, wherein the chamber
is provided with at least one pair of microwave-sensitive materials (34).
23. The carbon fiber manufacturing apparatus as claimed in claim 17, wherein the plasma
generator is able to generate the plasma gas flow, an atmospheric plasma gas flow,
a low-pressure plasma gas flow, a microwave plasma gas flow, or a glow plasma gas
flow having a power in the range of 100-10000 watts.
24. The carbon fiber manufacturing apparatus as claimed in claim 15, wherein the sizing
module (50) is provided with at least one reservoir (51).
25. The carbon fiber manufacturing apparatus as claimed in claim 15, further comprising
a drying module (60), the drying module (60) being disposed at the carbon fiber drag
route between the sizing module (50) and the receiving module (20).
Amended claims in accordance with Rule 137(2) EPC.
1. A carbon fiber manufacturing method, comprising;
providing a raw material step, providing a carbon fiber precursor fiber bundle (70A);
performing a high-temperature carbonization step, the carbon fiber precursor fiber
bundle (70A) being heated to form a carbon fiber (70B) having a predetermined carbon
content;
performing a plasma surface treatment step, a plasma gas flow with a predetermined
power being provided to act on the carbon fiber (70B) at a predetermined time so that
a surface of the carbon fiber (70B) is formed with a plasma-modified configuration
(71);
performing a sizing step, the plasma-modified configuration (71) being coated with
a resin oiling agent (80); and
performing a drying step, the resin oiling agent (80) coated on the plasma-modified
configuration (71) being processed with drying so that the resin oiling agent (80)
is firmly adhered to the surface of the carbon fiber (70B);
wherein in the high-temperature carbonization step, the carbon fiber precursor fiber
bundle (70A) is guided into a chamber (31), the chamber (31) is formed with at least
one microwave field concentration area (311) therein and is provided with a gas supply
assembly (32) to supply an inert gas and a microwave generating assembly (33) to supply
a high-frequency microwave, under the protection of the inert gas atmosphere, an electric
field of the high-frequency microwave produces a sensing current to heat up and produce
a high temperature quickly with the carbon fiber precursor fiber bundle (70A) passing
through the microwave field concentration area (311);
wherein the chamber (31) is provided with at least one pair of microwave-sensitive
materials (34).
2. The carbon fiber manufacturing method as claimed in claim 1, wherein the microwave-sensitive
materials (34) are one of graphite, carbide, magnetic compound, nitride, and ionic
compound or a combination thereof.
3. The carbon fiber manufacturing method as claimed in claim 1, wherein the inert gas
is nitrogen, argon, helium, or a combination thereof.
4. The carbon fiber manufacturing method as claimed in claim 1, wherein the frequency
of the high-frequency microwave is in the range of 300-30,000 MHz, and its microwave
power density is in the range of 1-1000kW/m3.
5. The carbon fiber manufacturing method as claimed in claim 1, wherein the chamber (31)
is an elliptic chamber.
6. The carbon fiber manufacturing method as claimed in claim 1, wherein the chamber (31)
is a flat panel chamber.
7. The carbon fiber manufacturing method as claimed in any one of the foregoing claims,
wherein in the plasma surface treatment step, the plasma gas flow, an atmospheric
plasma gas flow, a low-pressure plasma gas flow, a microwave plasma gas flow, or a
glow plasma gas flow with a power of 100-10000 watts acts on the carbon fiber (70B)
for 10-1000 milliseconds.
8. The carbon fiber manufacturing method as claimed in any one of the foregoing claims,
wherein the carbon fiber precursor fiber bundle (70A) has a surface not processed
with a pre-oxidation treatment.
9. The carbon fiber manufacturing method as claimed in any one of claims 1 to 7, wherein
the carbon fiber precursor fiber bundle (70A) has a surface processed with a pre-oxidation
treatment in advance.
10. The carbon fiber manufacturing method as claimed in any one of the foregoing claims,
wherein the resin oiling agent (80) is a thermosetting resin oiling agent.
11. The carbon fiber manufacturing method as claimed in any one of claims 1 to 9, wherein
the resin oiling agent (80) is a thermoplastic resin oiling agent.
12. The carbon fiber manufacturing method as claimed in any one of the foregoing claims,
wherein the carbon content of the carbon fiber (70B) is in the range of 80%-90%.
13. A carbon fiber manufacturing apparatus, comprising:
a feeding module (10) and a receiving module (20), the receiving module (20) being
disposed in the vicinity of the feeding module (10), the feeding module (10) and the
receiving module (20) constituting a carbon fiber drag route;
a high-temperature carbonization module (30), disposed at the carbon fiber drag route
and located between the feeding module (10) and the receiving module (20) for heating
the carbon fiber drag route;
a plasma surface treatment module (40), disposed at the carbon fiber drag route and
located between the high-temperature carbonization module (30) and the receiving module
(20) for supplying a plasma gas flow to the carbon fiber drag route; and
a sizing module (50), disposed at the carbon fiber drag route and located between
the plasma surface treatment module (40) and the receiving module (20);
wherein the high-temperature carbonization module (30) has a chamber (31), a gas supply
assembly (32), and a microwave generating assembly (33), the carbon fiber drag route
passes through the chamber (31), the gas supply assembly (32) is used to supply an
inert gas, and the microwave generating assembly (33) is used to supply a high-frequency
microwave;
wherein the chamber (31) is a flat plate chamber and provided with at least one pair
of microwave-sensitive materials (34)
14. The carbon fiber manufacturing apparatus as claimed in claim13, wherein the plasma
surface treatment module (40) is provided with at least one plasma generator (41).
15. The carbon fiber manufacturing apparatus as claimed in claim 13 or 14, wherein the
plasma surface treatment module (40) is provided with at least one plasma generator
(41) located at upper and lower positions of the carbon fiber drag route, respectively.
16. The carbon fiber manufacturing apparatus as claimed in any one of claims 13 to 15,
wherein the chamber (31) is an elliptic chamber.
17. The carbon fiber manufacturing apparatus as claimed in any one of claims 13 to 16,
wherein the chamber (31) is provided with at least one pair of microwave-sensitive
materials (34).
18. The carbon fiber manufacturing apparatus as claimed in claim 14 or15, wherein the
plasma generator is able to generate the plasma gas flow, an atmospheric plasma gas
flow, a low-pressure plasma gas flow, a microwave plasma gas flow, or a glow plasma
gas flow having a power in the range of 100-10000 watts.
19. The carbon fiber manufacturing apparatus as claimed in any one of claims 13 to 18,
wherein the sizing module (50) is provided with at least one reservoir (51).
20. The carbon fiber manufacturing apparatus as claimed in any one of claims 13 to 19,
further comprising a drying module (60), the drying module (60) being disposed at
the carbon fiber drag route between the sizing module (50) and the receiving module
(20).