Technical Field
[0001] The present invention relates to a carbonization apparatus for carbonizing precursor
fibers of carbon fibers, and a method for producing carbon fibers.
Background Art
[0002] Carbon fibers are produced by first thermally stabilizing precursor fibers of carbon
fibers through heating at 200 to 300°C in air, and then carbonizing the thermally
stabilized precursor fibers through heating at 1000°C or higher in an inert atmosphere
such as nitrogen. For example, microwaves are used as a method for heating in the
carbonization.
Summary of Invention
Technical Problem
[0003] However, the carbonization of precursor fibers by microwave heating has been carried
out only on a small laboratory scale, and it has been difficult to commercially produce
carbon fibers.
[0004] The present invention has been made in view of the above-described circumstances,
and it is an object thereof to provide a carbonization apparatus and a method for
producing carbon fibers, which enable commercial-scale carbonization of a plurality
of precursor fibers.
Solution to Problem
[0005] In order to achieve the above-described object, an aspect of the present invention
is directed to a carbonization apparatus for carbonizing a plurality of precursor
fibers of carbon fibers through heating, including: two or more microwave generators
that generate microwaves; one or two or more cavities into which microwaves generated
by the two or more microwave generators are introduced; and two or more structures
that are arranged in series within the one or two or more cavities and inside which
the plurality of precursor fibers can move in parallel, wherein each of the two or
more structures partially absorbs microwaves introduced from the outside, and partially
transmits the microwaves inward, and the two or more structures can be irradiated
with microwaves such that a structure on a later-stage side along a movement direction
of the plurality of precursor fibers reaches a higher temperature.
[0006] Furthermore, the carbonization apparatus according to an aspect of the present invention
may be such that at least one structure of the two or more structures can be irradiated
with microwaves such that the structure reaches a temperature equivalent to a target
temperature of the plurality of precursor fibers moving inside the structure.
[0007] Furthermore, the carbonization apparatus according to an aspect of the present invention
may be such that each of the two or more structures has a hollow pillar-like shape.
[0008] Furthermore, the carbonization apparatus according to an aspect of the present invention
may be such that the one or two or more cavities are two or more cavities connected
in series, the microwaves generated by the two or more microwave generators are respectively
introduced into the two or more cavities, and the two or more structures are respectively
arranged within the two or more cavities.
[0009] Furthermore, the carbonization apparatus according to an aspect of the present invention
may be such that a discharge port is provided between adjacent cavities among the
two or more cavities to discharge gas generated in an earlier-stage cavity of the
adjacent cavities.
[0010] Furthermore, the carbonization apparatus according to an aspect of the present invention
may be such that a supply port is provided between adjacent cavities among the two
or more cavities to supply inert gas into a later-stage cavity of the adjacent cavities.
[0011] Furthermore, the carbonization apparatus according to an aspect of the present invention
may be such that a needle array circuit is provided between adjacent cavities among
the two or more cavities to prevent propagation of microwaves between the adjacent
cavities.
[0012] Furthermore, the carbonization apparatus according to an aspect of the present invention
may be such that the carbonization apparatus further includes an electrical conduction
unit that electrically interconnects the carbon fibers in the vicinity of a discharge
port of a last-stage cavity of the one or two or more cavities.
[0013] Furthermore, the carbonization apparatus according to an aspect of the present invention
may be such that a last-stage structure of the two or more structures contains silicon
nitride.
[0014] Furthermore, an aspect of the present invention is directed to a method for producing
carbon fibers by carbonizing a plurality of precursor fibers of carbon fibers through
heating, including: moving the plurality of precursor fibers in parallel inside two
or more structures that are arranged in series within the one or two or more cavities,
each of the two or more structures partially absorbing microwaves introduced from
the outside and partially transmitting the microwaves inward; and irradiating the
two or more structures with microwaves such that a structure on a later-stage side
along a movement direction of the plurality of precursor fibers reaches a higher temperature.
Advantageous Effects of Invention
[0015] With the carbonization apparatus and the method for producing carbon fibers according
to an aspect of the present invention, a plurality of precursor fibers can be simultaneously
carbonized by microwave heating, and thus it is possible to commercially produce carbon
fibers.
Brief Description of Drawings
[0016]
FIG. 1 is a schematic diagram showing the configuration of a carbonization apparatus
according to an embodiment of the present invention.
FIG. 2 is a schematic longitudinal cross-sectional view showing an internal structure
of the carbonization apparatus in the embodiment.
FIG. 3A is a perspective view showing a structure in the embodiment.
FIG. 3B is a longitudinal cross-sectional view showing a cavity and the structure
in the embodiment.
FIG. 3C is a longitudinal cross-sectional view showing the cavity and the structure
in the embodiment.
FIG. 4A is a longitudinal cross-sectional view showing a needle array circuit in the
embodiment.
FIG. 4B is a transverse cross-sectional view showing the needle array circuit in the
embodiment.
FIG. 5 is a longitudinal cross-sectional view showing an electrical conduction unit
in the embodiment.
FIG. 6 is a schematic longitudinal cross-sectional view showing another example of
the configuration of the carbonization apparatus in the embodiment.
FIG. 7 is a longitudinal cross-sectional view showing another example of the structure
in the embodiment.
FIG. 8 is a longitudinal cross-sectional view showing another example of the structure
in the embodiment.
Description of Embodiment
[0017] Hereinafter, a carbonization apparatus and a method for producing carbon fibers according
to the present invention will be described based on an embodiment. Note that constituent
elements denoted by the same reference numerals are the same as or similar to each
other in the following embodiments, and thus a description thereof may not be repeated.
With the carbonization apparatus according to this embodiment, two or more structures
that are arranged in series within a cavity are heated with microwaves, and a plurality
of precursor fibers that are arranged in parallel and move inside the two or more
structures are directly heated with microwaves transmitted through the structures,
and thus the plurality of precursor fibers are carbonized.
[0018] FIG. 1 is a schematic diagram showing an external appearance of a carbonization apparatus
1 according to an embodiment of the present invention, and FIG. 2 is a schematic longitudinal
cross-sectional view showing an internal structure of the carbonization apparatus
1. In FIG. 1, the configurations of a control unit 19 and the like are omitted. In
the examples of FIGS. 1 and 2, the carbonization apparatus 1 includes microwave generators
11-1, 11-2, and 11-3 that generate microwaves, waveguides 12-1, 12-2, and 12-3 that
respectively guide the two or more generated microwaves, cavities 13-1, 13-2, and
13-3 that are connected in series and into which the two or more guided microwaves
are respectively introduced, and structures 14-1, 14-2, and 14-3 that are respectively
arranged within the cavities 13-1, 13-2, and 13-3. If the microwave generators 11-1,
11-2, and 11-3 are not distinguished individually, any one of them may simply be referred
to as a microwave generator 11. The same applies to other constituent elements. In
this embodiment, in the configuration of the cavities 13 that are connected in series,
the upstream side along the movement direction of fibers 3 may be referred to as an
earlier-stage side, and the downstream side may be referred to as a later-stage side.
[0019] The carbonization apparatus 1 may further include, as necessary, at least one of
an inlet portion 15 for the fibers 3, which is connected to the earliest-stage cavity
13-1, connection portions 16-1 and 16-2 that each connect two adjacent cavities 13,
an outlet portion 17 for the fibers 3, which is connected to the last-stage cavity
13-3, temperature sensors 18-1, 18-2, and 18-3 that measure the respective temperatures
of the structures 14, and a control unit 19 that controls the microwave generators
11 using the temperatures measured by the temperature sensors 18. The carbonization
apparatus 1 may further include, as necessary, at least one of a discharge pipe 22
having a discharge port 21 at one end for discharging gas generated in the cavity
13, a supply pipe 24 having a supply port 23 at one end for supplying inert gas into
the cavity 13, and a needle array circuit 25 for preventing propagation of microwaves
at the inlet portion 15, the connection portion 16, and the outlet portion 17.
[0020] The carbonization apparatus 1 carbonizes precursor fibers of carbon fibers while
continuously moving them inside the cavity 13. Accordingly, the fibers 3 introduced
from the inlet portion 15 to the cavity 13-1 are precursor fibers after thermal stabilization,
and the fibers 3 discharged from the outlet portion 17 are carbon fibers. As an example,
the precursor fibers may be polyacrylonitrile (PAN). For convenience, thermally stabilized
fibers, which are precursor fibers obtained by oxidation through thermal stabilization,
are also referred to as precursor fibers. The fibers 3 may be, for example, a single
fiber, but they are typically a fiber bundle in which a plurality of fibers are bundled.
Accordingly, the fibers 3 may be, for example, a precursor fiber bundle or a carbon
fiber bundle.
[0021] The microwave generator 11 may generate microwaves, for example, using a magnetron,
a klystron, a gyrotron, a semiconductor element, or the like. The generating microwaves
using a semiconductor device may mean, for example, oscillating microwaves using a
semiconductor device or amplifying microwaves using a semiconductor device. The frequency
band of the microwaves may be, for example, in the vicinity of 433.92 MHz, 915 MHz,
2.45 GHz, or 5.8 GHz, or other frequency bands in the range of 300 MHz to 300 GHz.
As will be described later, the two or more structures 14 are irradiated with microwaves
such that a structure 14 on a later-stage side reaches a higher temperature. Accordingly,
the output (power) of the plurality of microwave generators 11 may increase in the
order of the microwave generators 11-1, 11-2, and 11-3.
[0022] The waveguide 12 guides the microwaves generated by the microwave generator 11 into
the cavity 13. The waveguide 12 may be, for example, a rectangular waveguide or a
circular waveguide. The waveguide 12 may be, for example, a hollow waveguide. For
example, a microwave-transmissive airtight window may be provided, for example, at
an end or another portion of the waveguide 12 to prevent gas or the like from the
cavity 13 from moving toward the microwave generator 11. The airtight window may be
made of, for example, a microwave-transmissive material. The microwave-transmissive
material is not particularly limited, but examples thereof may include quartz glass,
a fluororesin such as polytetrafluoroethylene, and a ceramic. For example, instead
of the waveguide 12, a microwave guide unit such as a coaxial cable may be used to
guide the microwaves. The interior of the cavity 13 may be directly irradiated with
microwaves generated by the microwave generator 11. In this case, for example, the
carbonization apparatus 1 does not have to include the waveguide 12, and an antenna
for emitting microwaves may be provided in the cavity 13.
[0023] The microwaves generated by the microwave generator 11 are introduced into the cavity
13. The shape of the internal space of the cavity 13 is not particularly limited,
but examples thereof may include a pillar-like shape extending in one direction. The
one direction may be, for example, the movement direction of the fibers 3. The pillar-like
shape may be, for example, a rectangular parallelepiped shape or a solid cylindrical
shape. In this embodiment, a case will be mainly described in which the internal space
of the cavity 13 has a rectangular parallelepiped shape.
[0024] The cavity 13 preferably has a wall made of a material that does not transmit microwaves
so as to prevent leakage of microwaves from the internal space. The material that
does not transmit microwaves may be, for example, a microwave-reflective material.
The microwave-reflective material is not particularly limited, but examples thereof
may include a metal such as stainless steel, carbon steel, nickel, a nickel alloy,
copper, and a copper alloy.
[0025] The plurality of cavities 13 are connected in series. The plurality of cavities 13
being connected in series may mean that the plurality of cavities 13 are connected
such that the fibers 3 moving inside the plurality of cavities 13 pass through the
cavities sequentially. The plurality of cavities 13 may be connected in series, for
example, via the connection portion 16. Each cavity 13 may have, for example, an introduction
port through which the fibers 3 are introduced into the internal space and a discharge
port through which the fibers 3 are discharged from the internal space. Microwave
irradiation within each cavity 13 is typically performed in a multi-mode manner. When
carbonization is performed, the interior of each cavity 13 is typically at atmospheric
pressure.
[0026] In this embodiment, a case will be mainly described in which the number of microwave
generators 11 is equal to the number of cavities 13 and microwaves generated by the
two or more microwave generators 11 are respectively introduced into the two or more
cavities 13, but there is no limitation to this. For example, microwaves generated
by two or more microwave generators 11 may be introduced into one cavity 13, or microwaves
generated by one microwave generator 11 may be branched and introduced into two or
more cavities 13.
[0027] Two or more structures 14 each having a hollow pillar-like shape (hollow pillar-like
structures) are arranged in series within the two or more cavities 13. Each hollow
pillar-like structure 14 may have, for example, a straight elongated shape. A cross-sectional
shape in a plane perpendicular to a longitudinal direction of the hollow pillar-like
structure 14 may be, for example, rectangular or another shape. Openings communicating
with the hollow portion of the hollow pillar-like structure 14 are provided at both
longitudinal ends of the structure 14. In this embodiment, a case will be mainly described
in which the cross-sectional shape of the hollow pillar-like structure 14 is rectangular,
that is, the structure 14 has a rectangular tube shape. The two or more structures
14 may be arranged in series as a result of the two or more structures 14 being respectively
arranged within the two or more cavities 13, and the two or more cavities 13 being
connected in series. In this embodiment, a case will be mainly described in which
the number of cavities 13 is equal to the number of structures 14 and one structure
14 is arranged in one cavity 13, but there is no limitation to this. As will be described
later, the two or more structures 14 may be arranged in one cavity 13.
[0028] FIG. 3A is a perspective view showing an external appearance of the structure 14,
and FIGS. 3B and 3C are longitudinal cross-sectional views of the cavity 13 and the
structure 14. FIG. 3B is a longitudinal cross-sectional view at a position where a
frame member 31 is not present, and FIG. 3C is a longitudinal cross-sectional view
at a position where the frame member 31 is present. As shown in FIGS. 3A, 3B, and
3C, the plurality of fibers 3 arranged in parallel may move inside the structure 14.
As shown in FIG. 3B, for example, a cross section in a plane perpendicular to a longitudinal
direction of the structure 14 may be rectangular, and the plurality of fibers 3 may
be arranged along a long side thereof. The distances between inner walls of the structure
14 and the plurality of fibers 3 are preferably equivalent. For example, as shown
in FIGS. 3B and 3C, distances between two inner walls of the structure 14 facing each
other and the fibers 3 may be equivalent. The distance is preferably such that heat
exchange between the inner walls of the structure 14 and the plurality of fibers 3
can occur. As shown in FIGS. 3A, 3B, and 3C, the plurality of fibers 3 may be arranged
in parallel such that a plurality of fibers 3 lie in the same plane. In this case,
spacing between the plurality of fibers 3 may be, for example, uniform. The plurality
of fibers 3 typically move at the same speed in the longitudinal direction of the
fibers 3.
[0029] The structure 14 partially absorbs microwaves introduced from the outside, and partially
transmits the microwaves inward. The structure 14 preferably has microwave transmittance
such that a temperature difference between the structure 14 and the fibers 3 becomes
small, by heating the structure 14 with microwaves absorbed by the structure 14 and
heating the fibers 3 with microwaves transmitted through the structure 14. If the
entire outer peripheral surface of the structure 14 is irradiated with microwaves
as shown in FIG. 3B, multi-mode microwave irradiation within the cavity 13 allows
the structure 14 to be heated more uniformly. The plurality of fibers 3 are also more
uniformly heated with microwaves transmitted through the wall surface of the structure
14. At least one structure 14 of the plurality of structures may be irradiated with
microwaves such that, for example, the structure 14 reaches a temperature equivalent
to a target temperature of the plurality of fibers 3 moving inside the structure 14.
Since thermally stabilized fibers at room temperature or thermally stabilized fibers
immediately after thermal stabilization treatment are introduced into the earliest-stage
cavity 13-1, a temperature difference between the fibers 3 and the earliest-stage
structure 14-1 in an upstream region in the structure 14-1 is larger than that in
the other regions in the structures 14. In the other regions, the fibers 3 and the
structure 14 can be irradiated with microwaves such that a temperature difference
therebetween becomes small.
[0030] The microwave transmittance of the structure 14 is not particularly limited, but,
for example, at a carbonization temperature, about 20% to 80% of microwaves may be
transmitted from the outside to the inside, and about 30% to 50% of microwaves may
be transmitted from the outside to the inside. As carbonization proceeds, the fibers
3 exhibit increased microwave absorption, and the fibers 3 themselves generate more
heat. Therefore, a structure 14 on a later-stage side may have a lower microwave transmittance.
The transmittance of the structure 14 may decrease, for example, in the order of the
structures 14-1, 14-2, and 14-3. The microwave transmittance can be adjusted, for
example, by changing at least one of the material of the structure 14 and the wall
thickness of the structure 14.
[0031] In the carbonization, the temperature of the fibers 3 is gradually increased. For
example, at the start of the carbonization, the temperature of the fibers 3 is about
300°C to 500°C, whereas at the end of the carbonization, the temperature of the fibers
3 reaches 1000°C or higher, such as 1100°C to 1200°C. Accordingly, two or more structures
14 are preferably irradiated with microwaves such that a structure 14 on a later-stage
side along the movement direction of the plurality of fibers 3 reaches a higher temperature.
In the example shown in FIG. 2, the structures 14 may be irradiated with microwaves
such that the temperature increases in the order of the structures 14-1, 14-2, and
14-3. For example, the structure 14-1 may be heated to 500°C, and the structure 14-3
may be heated to 1100°C.
[0032] The material of the structure 14 is not particularly limited as long as it partially
absorbs microwaves and partially transmits the microwaves, but examples thereof may
include a material containing alumina or silicon nitride. As an example, the structure
14 may be made of sialon (SiAlON) containing silicon nitride. A structure 14 containing
silicon nitride has improved heat resistance. Accordingly, a structure 14 on a later-stage
side, in particular, the last-stage structure 14-3 preferably contains silicon nitride.
Meanwhile, a structure 14 on an earlier-stage side in which the temperature does not
become high preferably contains alumina, which is less expensive than silicon nitride.
For example, the structures 14-1 and 14-2 may be made of alumina, and the structure
14-3 may be made of silicon nitride.
[0033] The structure 14 may be supported within the internal space of the cavity 13 by a
predetermined support unit or the like. For example, as shown in FIG. 3B, in the internal
space of the cavity 13, the support unit may include a pair of protrusions 32 that
are respectively provided on a pair of inner walls of the cavity facing each other
in the arrangement direction of the plurality of fibers 3, and a plate-like member
33 whose ends are supported by the pair of protrusions 32. The structure 14 may be
placed, for example, on an upper surface of the plate-like member 33. The pair of
protrusions 32 may be, for example, metal members extending along the movement direction
of the fibers 3. The plate-like member 33 may be made of, for example, a microwave-transmissive
or thermally-insulating material. The microwave-transmissive and thermally-insulating
plate-like member 33 may be made of, for example, a material containing alumina.
[0034] The structure 14 may be arranged in the internal space of the cavity 13, for example,
so as to connect an introduction port of the cavity 13 and a discharge port of the
cavity 13. That is to say, the fibers 3 introduced from the introduction port of the
cavity 13 into the internal space may move inside the structure 14 and be discharged
from the discharge port of the cavity 13. The structure 14 expands thermally when
heated with microwaves. If the degree of thermal expansion is larger than that of
the cavity 13, as shown in FIG. 2, the longitudinal length of the structure 14 may
be shorter than the length of the internal space of the cavity 13 along the movement
direction of the fibers 3 by an amount corresponding to the thermal expansion. If
gas generated by the heating of the organic fibers 3 flows out of the structure 14,
the gas condenses on the inner walls of the cavity 13 to form tar, which needs to
be removed. The reason for this is that tar absorbs microwaves. If a gap exists between
the introduction port or discharge port of the cavity 13 and the corresponding end
of the structure 14, gas generated by the heating of the fibers 3 may flow out of
the structure 14 through that gap. Therefore, as shown in FIGS. 2 and 3C, a frame
member 31 may be provided on the inner walls of the cavity 13 to surround the introduction
port and the discharge port. Furthermore, the outer peripheral surfaces of both longitudinal
ends of the structure 14 may be surrounded by the frame member 31. The frame member
31 may be made of, for example, a metal. Since the frame member 31 and the structure
14 are not fixed, the structure 14 can thermally expand along the inner peripheral
surface of the frame member 31 when the structure reaches a high temperature. In this
manner, if both longitudinal ends of the structure 14 are surrounded by the frame
member 31, it is possible to prevent gas generated by the heating of the fibers 3
from flowing out of the structure 14. If one structure 14 is arranged in one cavity
13 as shown in FIG. 2, both ends of the structure 14 may be supported by the frame
member 31 on the introduction port side and the frame member 31 on the discharge port
side. In this case, the protrusions 32 and the plate-like member 33 may not be present
in the internal space of the cavity 13.
[0035] If two or more structures 14 are arranged in series in the internal space of one
cavity 13, two adjacent structures 14 are preferably arranged such that no gap exists
therebetween. Cross sections at connection portion may have the same shape. In this
manner, by ensuring that the space inside the structure 14 and the space outside the
structure 14 do not communicate in the internal space of the cavity 13, it is possible
to prevent gas generated by the heating of the organic fibers 3 from flowing to the
space outside the structure 14. As a result, the space outside the structure 14 in
the internal space of the cavity 13 can be kept free from contamination by gas, thereby
reducing the workload associated with cleaning that space. In this embodiment, since
the structure 14 is also heated, it is possible to prevent gas generated by the heating
of the fibers 3 from condensing on the inner walls of the structure 14 and forming
tar. Consequently, tasks such as tar removal become unnecessary.
[0036] The length of the cavity 13 and the structure 14 in the direction along the fibers
3, the respective temperatures of the two or more structures 14, the movement speed
of the fibers 3, and the like are preferably determined as appropriate so that the
desired carbonization is performed within the cavity 13. The dielectric constant of
the structure 14 and the output of the microwave generator 11 that generates microwaves
for use in irradiation of the structure 14 are preferably determined as appropriate
so that the structure 14 can be heated to the desired temperature.
[0037] Hereinafter, effects of heating not only the fibers 3 but also the structures 14
with microwaves will be described. If only the fibers are directly heated with microwaves,
ambient temperature becomes lower than the fiber temperature, causing cooling of the
fiber surface and resulting in temperature non-uniformity between the inside and surface
of the fibers. Furthermore, when a plurality of fibers are arranged in parallel, that
is, moved in parallel, heating non-uniformity also occurs among the plurality of fibers.
The reason for this is that it is difficult to irradiate a plurality of fibers with
microwaves uniformly. On the other hand, when the fibers 3 are moved inside the structures
14 that are heated with microwaves, the ambient temperature in a structure 14 on a
later-stage side can be made comparable to that of the fibers 3, thereby reducing
temperature non-uniformity between the inside and surface of the fibers 3. If each
structure 14 is made of, for example, a material having thermal conductivity comparable
to or higher than that of alumina or silicon nitride, the entire structure 14 attains
a uniform temperature. Therefore, heat exchange between the plurality of fibers 3
and the inner walls of the structure 14 occurs, and thus the temperature of the plurality
of fibers 3 is made comparable to that of the structure 14, thereby reducing heating
non-uniformity among the plurality of fibers 3. In this manner, more uniform heating
of the plurality of fibers 3 can be achieved, enabling the production of more homogeneous
carbon fibers.
[0038] The inlet portion 15 is a hollow pillar-like member having one end connected to the
introduction port for the fibers 3 in the earliest-stage cavity 13-1. The fibers 3
are introduced into the carbonization apparatus 1 from the opening at the inlet portion
15's end that is not connected to the cavity 13-1, and are subjected to carbonization.
[0039] The connection portion 16 is a hollow pillar-like member that connects two adjacent
cavities 13 among the two or more cavities 13. An opening at one end is connected
to the discharge port for the fibers 3 in the cavity 13 on the earlier-stage side,
and an opening at the other end is connected to the introduction port for the fibers
3 in the cavity 13 on the later-stage side. Since the fibers 3 are not heated in the
connection portion 16, the length of the connection portion 16 in the direction along
the fibers 3 is preferably short.
[0040] The outlet portion 17 is a hollow pillar-like member having one end connected to
the discharge port for the fibers 3 in the last-stage cavity 13-3. The fibers 3 after
carbonization, that is, carbon fibers are discharged from the opening at the outlet
portion 17's end that is not connected to the last-stage cavity 13-3.
[0041] Cross-sectional shapes of the inlet portion 15, the connection portion 16, and the
outlet portion 17 in a plane perpendicular to a longitudinal direction of the fibers
3 may be, for example, rectangular. The inlet portion 15, the connection portion 16,
and the outlet portion 17 are preferably made of materials that do not transmit microwaves.
Each of the inlet portion 15, the connection portion 16, and the outlet portion 17
is preferably connected to the cavity 13 such that microwaves do not leak from each
connection portion.
[0042] For example, the temperature sensor 18 may measure the temperature of the structure
14 arranged in the cavity 13. The temperature sensor 18 may be, for example, a radiation
thermometer that measures the temperature of an outer peripheral surface of the structure
14. In this embodiment, a case will be mainly described in which the temperature of
one structure 14 is measured by one temperature sensor, but the temperature of one
structure 14 may be measured by two or more temperature sensors 18. In this case,
for example, a representative value of two or more temperatures measured by the two
or more temperature sensors 18 may be adopted as the temperature of the structure
14. The representative value may be, for example, an average value, a median value,
a maximum value, or a minimum value.
[0043] The control unit 19 may control the microwave generators 11, for example, using the
temperatures measured by the temperature sensors 18. The control unit 19 may control
the microwave generators 11 that generate microwaves introduced into the cavities
13 in which the structures 14 are arranged such that the structures 14 reach desired
temperatures. More specifically, the control unit 19 may control the microwave generator
11-1 such that the structure 14-1 reaches a desired temperature. This control may
be feedback control. As an example, the control unit 19 may perform control such that
the temperature of the structure 14 reaches a temperature equivalent to a target temperature
of the plurality of fibers 3 moving inside the structure 14. The term "equivalent
temperature" may refer to, for example, the same temperature, or a temperature close
enough to be considered substantially the same. In the latter case as well, it is
preferable that the temperature of the structure 14 is close enough to the target
temperature to reduce temperature non-uniformity within a single fiber 3 and reduce
temperature differences among the plurality of fibers 3. As described above, the temperature
of the fibers 3 is gradually increased in the carbonization, and thus the control
unit 19 may control the microwave generators 11-1, 11-2, and 11-3 such that the temperature
increases in the order of the structures 14-1, 14-2, and 14-3, that is, such that
a structure 14 on a later-stage side reaches a higher temperature.
[0044] Furthermore, at least one of the connection portions 16-1 and 16-2 and the outlet
portion 17 may be provided, for example, with a discharge port 21 for discharging
gas generated by the heating of the fibers 3 in the cavity 13 on the earlier-stage
side. The discharge port 21 may be, for example, at one end of the discharge pipe
22. In this manner, the interiors of the structure 14, the connection portion 16,
and the outlet portion 17 can be kept free from contamination by discharging gas generated
in the cavity 13 from the discharge port 21 and the discharge pipe 22 provided between
adjacent cavities 13 among the two or more cavities 13 or provided at the outlet portion
17 for the fibers 3 in the last-stage cavity 13-3. As an example, the connection portions
16-1 and 16-2 and the outlet portion 17 may be provided with two or more discharge
ports 21 and discharge pipes 22 along the arrangement direction of the plurality of
fibers 3. The diameter of the discharge port 21 and the length of the discharge pipe
22 may be determined so as to prevent leakage of microwaves via the discharge pipe
22. As an example, the diameter of the discharge port 21 may be one-quarter or less
of the wavelength of the microwaves for use in irradiation in the cavity 13.
[0045] Furthermore, at least one of the inlet portion 15 and the connection portions 16-1
and 16-2 may be provided, for example, with a supply port 23 for supplying inert gas
into the cavity 13 on the later-stage side. The supply port 23 may be, for example,
at one end of the supply pipe 24. In this manner, the fibers 3 can be heated in an
inert atmosphere by supplying inert gas into the cavity 13 from the supply pipe 24
and the supply port 23 provided at the inlet portion 15 for the fibers 3 in the earliest-stage
cavity 13-1 or provided between adjacent cavities 13 among the two or more cavities
13. The inert gas is not particularly limited, but examples thereof may include nitrogen
and argon. The position of the supply port 23 and the flow rate and orientation of
inert gas supplied from the supply port 23 may be determined as appropriate by simulation
or the like so that the inert gas is effectively supplied into the cavity 13. As an
example, the inlet portion 15 and the connection portions 16-1 and 16-2 may be provided
with two or more supply ports 23 and supply pipes 24 along the arrangement direction
of the plurality of fibers 3. The diameter of the supply port 23 and the length of
the supply pipe 24 may be determined so as to prevent leakage of microwaves via the
supply pipe 24. As an example, the diameter of the supply port 23 may be one-quarter
or less of the wavelength of the microwaves for use in irradiation.
[0046] The inlet portion 15, the connection portion 16, and the outlet portion 17 may be
provided, for example, with a needle array circuit 25 for preventing propagation of
microwaves. The needle array circuit 25 may be referred to as a needle array structure.
FIG. 4A is a longitudinal cross-sectional view of the connection portion 16 showing
the needle array circuit 25, and FIG. 4B is a transverse cross-sectional view of the
connection portion 16 showing the needle array circuit 25. FIG. 4B is a transverse
cross-sectional view taken along a plane passing through needle-like members 26. The
needle array circuit 25 may have a plurality of needle-like members 26 arranged in
parallel. The longitudinal length of each needle-like member 26 may be, for example,
one-quarter of the wavelength of the microwaves for use in irradiation in the cavity
13. The needle-like members 26 are preferably made of, for example, a conductive material.
The conductive material may be, for example, a metal. The metal is not particularly
limited, but examples thereof may include stainless steel, carbon steel, nickel, a
nickel alloy, copper, and a copper alloy. The plurality of needle-like members 26
are preferably arranged in the inlet portion 15, the connection portion 16, and the
outlet portion 17 so as not to obstruct movement of the fibers 3 and so as to prevent
propagation of microwaves. In this embodiment, a case is shown in which the needle
array circuit 25 is provided on upper inner walls of the inlet portion 15, the connection
portion 16, and the outlet portion 17, but the needle array circuit 25 may be provided
on lower inner walls. However, the needle array circuit 25 is preferably provided
on upper inner walls in order to prevent the fibers 30 from being caught on the needle
array circuit 25 when the fibers 30 are threaded through the inlet portion 15, the
connection portion 16, and the outlet portion 17. In this manner, if the needle array
circuit 25 is provided between adjacent cavities 13 among the two or more cavities
13, the propagation of microwaves between the cavities 13 can be prevented, and it
becomes easier to control the temperature of the structure 14 in each cavity 13. If
the inlet portion 15 and the outlet portion 17 are provided with the needle array
circuit 25, the leakage of microwaves to the outside of the carbonization apparatus
1 via the inlet portion 15 and the outlet portion 17 can be prevented.
[0047] Since the carbonization is completed in the last-stage cavity 13-3, the fibers 3
discharged from the last-stage cavity 13-3 are carbon fibers formed by the carbonization
of the precursor fibers and exhibit high electrical conductivity. Therefore, there
is a possibility that microwaves may leak to the outside via the conductive fibers
3 discharged from the last-stage cavity 13-3. In order to prevent such leakage of
microwaves, the carbonization apparatus 1 may further include, for example, an electrical
conduction unit that electrically interconnects the plurality of fibers 3 in the vicinity
of the discharge port for the plurality of fibers 3 in the last-stage cavity 13-3.
The electrical conduction unit may be provided, for example, in the outlet portion
17. In this manner, the plurality of carbon fibers are electrically interconnected,
and thus the potential difference therebetween is eliminated. As a result, the generation
of an electromagnetic field between the plurality of carbon fibers can be prevented,
thereby preventing radiation of microwaves from the carbon fibers into the surrounding
space.
[0048] As an example, the electrical conduction unit may be a roller 27 shown in FIG. 5.
For example, the roller 27 may be arranged in the outlet portion 17 so as to be rotatable,
and may be rotated by a drive unit such as a motor in accordance with the movement
speed of the fibers 3. The outer peripheral surface of the roller 27 is preferably
made of a conductive material. The conductive material may be, for example, a metal.
In the outlet portion 17, the roller 27 is preferably arranged such that the direction
of its rotational axis is perpendicular to the longitudinal direction of the plurality
of fibers 3 and such that the plurality of fibers 3 come into contact with its outer
peripheral surface. For example, the roller 27 may be grounded.
[0049] FIG. 5 shows a case in which the roller 27 is arranged closer to the discharge port
of the last-stage cavity 13-3 than the needle array circuit 25 is, but the roller
27 may be arranged at a different position. For example, in FIG. 5, the roller 27
may be arranged in the vicinity of the needle array circuit 25, or may be arranged
closer to the opening on the downstream side of the outlet portion 17 than the needle
array circuit 25 is. For example, the roller 27 may be arranged above the plurality
of fibers 3. The plurality of fibers 3 may be electrically interconnected by a unit
other than the roller 27.
[0050] Next, a method for producing carbon fibers using the carbonization apparatus 1 according
to this embodiment will be described. The fibers 3 to be subjected to carbonization
are thermally stabilized fibers, and, for example, they may be supplied directly from
a thermal stabilization apparatus to the carbonization apparatus 1 or unwound from
a spool or the like and supplied to the carbonization apparatus 1. In the former case,
the fibers 3 at about 250°C are supplied to the carbonization apparatus 1, and in
the latter case, the fibers 3 at room temperature are supplied to the carbonization
apparatus 1. The plurality of fibers 3 are moved in a state arranged in parallel,
for example, as indicated by the arrows in FIGS. 1 and 2. The plurality of fibers
3 may be moved, for example, by being wound up by a winding unit downstream of the
outlet portion 17. The plurality of fibers 3 are preferably moved, for example, at
a predetermined speed, such as 5 meters per minute.
[0051] The interior of each cavity 13 is irradiated with microwaves such that the structure
14 reaches a desired temperature. As described above, the structures 14 are preferably
irradiated with microwaves such that a structure on a later-stage side reaches a higher
temperature. This microwave irradiation may be performed by adjusting the output of
the microwave generators 11 using the temperatures measured by the temperature sensors
18. During the carbonization, the plurality of fibers 3 are heated in an inert atmosphere
by supplying inert gas such as nitrogen into the cavity 13 via the supply pipe 24.
Gas generated by the heating of the plurality of fibers 3 is discharged from the discharge
pipe 22. Since the inlet portion 15, the connection portion 16, and the outlet portion
17 are provided with the needle array circuit 25, the leakage of microwaves at the
inlet portion 15 and the outlet portion 17 can be prevented, and the propagation of
microwaves between the cavities 13 can be prevented as well. In this manner, carbon
fibers can be manufactured by continuously heating and carbonizing a plurality of
precursor fibers.
[0052] As described above, with the carbonization apparatus 1 according to this embodiment,
since the plurality of fibers 3 are simultaneously carbonized, it is possible to commercially
produce carbon fibers. In the case of performing the carbonization using a plurality
of cavities 13, the temperature of the structure 14 within each cavity 13 can be controlled
independently, making it easy to perform control such that the structure 14 reaches
a desired temperature.
[0053] Furthermore, since the structure 14 partially absorbs microwaves introduced from
the outside and partially transmits the microwaves, the temperature of the fibers
3 inside the structure 14 can be made comparable to that of the structure 14. As a
result, the temperature difference between the surface of the fibers 3 and the inside
of the fibers 3 can be reduced, thereby reducing temperature non-uniformity in a single
fiber 3, in the strict sense, in a single fiber bundle. If the structure 14 is mainly
made of, for example, alumina or silicon nitride, its high thermal conductivity ensures
that the entire structure 14 is heated to a more uniform temperature. Therefore, heat
exchange between the plurality of fibers 3 that are present inside the structure 14
and the inner walls of the structure 14 occurs, and thus the temperature difference
among the plurality of fibers 3 can be reduced, thereby reducing heating non-uniformity
among the plurality of fibers 3. This configuration enables the production of more
homogeneous carbon fibers.
[0054] Furthermore, since microwave irradiation within the cavity 13 is performed in a multi-mode
manner, the size of the structure 14 is not limited as in single-mode irradiation.
Accordingly, by making the structure 14 larger, it becomes possible to arrange a larger
number of fibers 3 in parallel and carbonize them collectively. In this case as well,
as described above, the temperature non-uniformity within a fiber bundle and the heating
non-uniformity among a plurality of fiber bundles are small, and thus it is possible
to mass-produce homogeneous carbon fibers.
[0055] Furthermore, if gas generated by the heating of the fibers 3 is discharged from the
discharge port 21 provided at the connection portion 16 and the outlet portion 17,
the inner walls of the structure 14 and the like can be kept free from contamination
by that gas. In particular, if the discharge port 21 is provided at the connection
portion 16, it becomes possible to discharge gas generated by the heating of the fibers
3 even during intermediate stages of the heating of the fibers 3. Since the structure
14 itself is also heated with microwaves, it is possible to prevent tar and the like
from condensing on the inner walls of the structure 14.
[0056] Furthermore, since inert gas is supplied into the cavity 13 from the supply port
23 provided at the inlet portion 15 and the connection portion 16, carbonization can
be performed in an inert atmosphere. If the gas generated by the heating of the fibers
3 is discharged and the inert gas is supplied at the connection portion 16, the atmospheric
gas can be replaced with clean inert gas during the intermediate stages of the heating
of the fibers 3.
[0057] Furthermore, since the inlet portion 15, the connection portion 16, and the outlet
portion 17 are provided with the needle array circuit 25, the leakage of microwaves
to the outside via the inlet portion 15 and the outlet portion 17 can be prevented.
Additionally, the propagation of microwaves via the connection portion 16 can be prevented
as well, making it easier to control the temperature of the structure 14 in each cavity
13.
[0058] Furthermore, when a plurality of carbon fibers are discharged from the last-stage
cavity 13-3, the plurality of carbon fibers are electrically interconnected using
an electrical conduction unit such as the roller 27, and thus the leakage of microwaves
to the outside via the plurality of carbon fibers can be prevented.
[0059] In this embodiment, the case was mainly described in which three cavities 13 and
three structures 14 are provided, but it will be appreciated that the number of cavities
13 and structures 14 need not be limited to three. For example, the number of cavities
13 and structures 14 included in the carbonization apparatus 1 may be two or four
or more. A larger number of cavities 13 and structures 14 can realize a more finely
controlled, stepwise increase in the temperature of the fibers 3, and thus from this
perspective, a larger number of cavities 13 and structures 14 is preferable. For example,
the number of cavities 13 and the number of structures 14 may be each three or more.
Furthermore, the carbonization apparatus 1 preferably includes, for example, one or
more microwave generators 11 and one or more waveguides 12 for each cavity 13.
[0060] Furthermore, in this embodiment, the case was mainly described in which one structure
14 is arranged in one cavity 13, but there is no limitation to this. For example,
two or more structures 14 may be arranged in one cavity 13. FIG. 6 is a schematic
longitudinal cross-sectional view showing an example of the carbonization apparatus
1 in which three structures 14-1, 14-2, and 14-3 connected in series are arranged
in one cavity 13. In the carbonization apparatus 1 shown in FIG. 6 as well, the temperatures
of the structures 14-1, 14-2, and 14-3 may be respectively measured by the temperature
sensors 18, and the microwave generators 11-1, 11-2, and 11-3 may be controlled using
the measured temperatures such that the structures 14-1, 14-2, and 14-3 each reach
a desired temperature. It is assumed that in the carbonization apparatus 1 shown in
FIG. 6, the outer peripheral surfaces of the structures 14-1, 14-2, and 14-3 are mainly
irradiated inside the cavity 13 respectively with the microwaves generated by the
microwave generators 11-1, 11-2, and 11-3. With this configuration, microwave irradiation
can be performed such that the temperatures of the plurality of fibers 3 increase
in a stepwise manner. Even when carbonization of precursor fibers is performed using
one cavity 13 as shown in FIG. 6, microwaves are preferably generated by two or more
microwave generators 11.
[0061] If two or more structures 14 are arranged in one cavity 13 as shown in FIG. 6, the
connection portion between two adjacent structures 14 may be configured as an expansion
joint structure to accommodate the longitudinal thermal expansion of each structure
14. FIG. 6 shows an example of an expansion joint structure. As shown in FIG. 6, the
right end of the structure 14-1 may have an enlarged inner peripheral surface, while
the left end of the structure 14-2 may have a reduced outer peripheral surface, and
the left end of the structure 14-2 may be inserted into the right end of the structure
14-1.
[0062] Furthermore, the areas in the vicinity of the introduction port and the discharge
port in the internal space of the cavity 13 are locations where temperature fluctuations
may be significant, as they are connected to the outside via the introduction port
and the discharge port of the cavity 13. Therefore, if three or more structures 14
are arranged in series in one cavity 13, the structure 14 on the introduction port
side, that is, the earliest-stage structure 14 and the structure 14 on the discharge
port side, that is, the last-stage structure 14 among the three or more structures
14 may be made of a material with high thermal shock resistance. Therefore, the structure
14 on the introduction port side and the last-stage structure 14 may contain, for
example, silicon nitride.
[0063] Furthermore, in this embodiment, the case was mainly described in which the structure
14 has a hollow pillar-like shape, but there is no limitation to this. For example,
as shown in FIG. 7, the structure 14 may have two plate-like members 14a and 14b arranged
in parallel and facing each other. That is to say, the structure 14 may be a structure
that does not include a face corresponding to the short side in the cross section
of the structure 14 shown in FIG. 3B. The plate-like members 14a and 14b each partially
absorb microwaves and partially transmit the microwaves. Accordingly, the plurality
of fibers 3 moving inside the structure 14, that is, the plurality of fibers 3 moving
between the two plate-like members 14a and 14b are irradiated with microwaves transmitted
through the two plate-like members 14a and 14b. In order to maintain a constant spacing
between the two plate-like members 14a and 14b and to prevent gas generated by the
heating of the fibers 3 from flowing out of the structure 14, a hollow pillar-like
shape may be formed by two plate-like members 34 arranged in parallel and facing each
other and the two plate-like members 14a and 14b. The plate-like members 34 may be
made of, for example, a microwave-transmissive or thermally-insulating material. The
microwave-transmissive and thermally-insulating plate-like members 34 may be made
of, for example, a material containing alumina.
[0064] Furthermore, in this embodiment, the case was mainly described in which the internal
space of the cavity 13 is irradiated with microwaves from the upper side, but there
is no limitation on the direction from which the internal space of the cavity 13 is
irradiated with microwaves. For example, the internal space of the cavity 13 may be
irradiated with microwaves from the lower side, or may be irradiated with microwaves
from both the upper side and the lower side. If the internal space of the cavity 13
is irradiated with microwaves from both the upper side and the lower side, for example,
as shown in FIG. 8, the structure 14 may include two plate-like members 14a and 14b
in which the length in the arrangement direction of the plurality of fibers 3 is equivalent
to the length in the arrangement direction of the plurality of fibers 3 in the internal
space of the cavity 13. In this case, as shown in FIG. 8, the plate-like members 14a
and 14b may be respectively supported by the protrusions 32.
[0065] Furthermore, in the carbonization apparatus 1 according to this embodiment, a member
that has a higher microwave transmittance than the structure 14 and a higher thermal
insulation than the structure 14 may be provided so as to cover at least a portion
of the outer surface of the structure 14, thereby reducing the transfer of heat from
the structure 14 to the internal space of the cavity 13 without obstructing the microwave
irradiation onto the structure 14. The member provided on the outer surface of the
structure 14 may be arranged, for example, so as to cover all of the outer surface
of the structure 14 having a hollow pillar-like shape shown in FIG. 3B, the outer
surfaces of the structure 14 included in the hollow pillar-like shape shown in FIG.
7, and the outer surfaces of the structure 14 forming surfaces on the opposite side
to the fibers 3 shown in FIG. 8, or so as to cover a portion of the outer surfaces.
The shape of this member is not particularly limited, but examples thereof may include
a plate-like shape. This member preferably has a lower specific heat capacity (heat
storage capacity) per unit volume than the structure 14. For example, if the specific
heat capacity per unit volume of the member provided on the outer surface of the structure
14 is larger than that of the structure 14, when lowering the temperature of the structure
14, even if the microwave output is reduced, the temperature of the structure 14 will
be difficult to lower due to the influence of that member. Furthermore, when starting
microwave irradiation to raise the temperature of the structure 14, it will take longer
to bring the temperature of the structure 14 to the desired temperature. On the other
hand, such issues can be avoided by using a material with a lower specific heat capacity
per unit volume than that of the structure 14. The member provided on the outer surface
of the structure 14 may be constituted by, for example, a material formed by compacting
alumina fibers.
[0066] Furthermore, in this embodiment, the case was mainly described in which the movement
direction of the plurality of fibers 3 is horizontal, but there is no limitation to
this. The plurality of fibers 3 may be moved in directions other than the horizontal
direction, such as the vertical direction. For example, when the plurality of fibers
3 are moved in the vertical direction, the plurality of fibers 3 are preferably moved
upward from the lower side. The reason for this is that during the carbonization,
the temperature of the fibers 3 has to be gradually increased, and gases at higher
temperatures rise upward.
[0067] Furthermore, the foregoing embodiment is an example for specific implementation of
the present invention and is not intended to limit the technical scope of the invention.
The technical scope of the invention is indicated by the claims rather than by the
foregoing description, and changes which come within the wording and equivalent meanings
of the scope of the claims are intended to be encompassed therein.