[0001] This invention relates to an unwoven metal fabric which is a kind of porous metal
structure for various uses such as battery electrodes, catalysts and filters and a
method of manufacturing the same.
[0002] Conventional battery electrodes and filters are formed from ultra-fine metal fibers
entangled together. Different materials and various new techniques for forming them
have been developed.
[0003] For example, Unexamined Japanese Patent Publication 4-11058 discloses a material
made of metal fibers that are joined together so that the length of the joint portions
will be more than 0.7 time the average fiber diameter, and a method of manufacturing
the same. Unexamined Japanese Patent Publication 3-17957 proposes a material made
of metal fibers which are subjected to pre-plating treatment using precious metal
catalysts to improve the adhesion of plating to the fibers, and a method of manufacturing
the same.
[0004] Also, Unexamined Japanese Patent Publication 61-76686 proposes to provide a metal
coating on a felt member by sputtering under vacuum in order to provide an electrode
having a high porosity. But the methods disclosed in these publications require complicated
processes such as pre-plating treatment by catalysts and sputtering, so that mass-productivity
is low. Also, if the electrodes thus formed contain more than 100 ppm metallic impurities
resulting from the catalysts used, their properties will vary so widely that they
will not stand practical use.
[0005] In order to solve these problems, Unexamined Japanese Patent Publication 4-126859
proposes a metal fiber material formed by electroplating a high-conductivity carbon
fiber sheet and removing the substrate. The carbon fiber sheet used here is manufactured
by forming a mixture of carbon fibers and a substance for bonding fibers (hereinafter
referred to as "binder") into sheet form and drying it.
[0006] The carbon fibers in such a carbon fiber sheet have a resistivity of mere 10⁻³- 10⁻⁴Ω
· cm. But the binder surrounding the carbon fibers has a very high resistivity because
it is an insulating material. It is not an easy job to directly electroplate such
a sheet. It would be possible to reduce the content of the binder in order to increase
the conductivity of the entire sheet. But this will make it necessary to increase
the amount of plating to make up for the reduced adhesion between fibers. The metal
fiber product thus obtained would have a porosity of 80-90%, which is too low for
use as battery electrodes.
[0007] It is possible to reduce the resistivity of the fiber material by increasing its
firing temperature to 1000°C or higher to graphitize the fiber. But since the fibers
are joined together by the resin binder, it is impossible to electroplate such joint
portions. The metallic porous member thus formed tends to be low in mechanical strength
and unsatisfactory in its electrical properties. Also, excessive graphitization would
make it necessary to increase the temperature to 900°C or higher in removing the substrate
by thermal oxidation in the later step. This will in turn result in reduced strength
of the unwoven fabric formed.
[0008] One solution to these problems is to increase the thickness of plating to 500-1000
g/m², because such a thick plating layer provided on the carbon fiber portions overhangs
the binder portions. But it is not easy to provide a thick plating having a uniform
thickness over the entire area. Also, such a thick plating layer tends to keep a web
form because it is difficult to roll. This solution is therefore not suitable for
continuous production. Thus, it is an ordinary practice to increase the conductivity
of the material by electroless plating and then provide an electroplating layer of
a predetermined thickness.
[0009] The unwoven fabric formed by this conventional method shows high mechanical strength
because plating is provided between fibers. But due to the properties of the plating
solution, variations in the distribution of fibers tend to widen. The unwoven fabric
thus formed is low in quality stability. If this unwoven fabric is used for batteries,
the content of metallic impurities which have been used as catalysts will exceed 100
ppm, so that the variations in the properties of electrodes will increase to such
a extent that such electrodes are practically useless. It is therefore desired to
provide a method for manufacturing a stable metallic unwoven fabric without reducing
the number of joint portions between metal fibers.
[0010] An object of the present invention is to provide a method of manufacturing an unwoven
metal fabric in which by making possible a direct, stable electroplating of unwoven
carbon fiber, the amount of impurities is reduced and the variation in quality is
minimized while keeping the mechanical strength and the porosity at high level.
[0011] Another object of the prevent invention is to provide an unwoven metal fabric which
is uniform in quality and low in the content of impurities, has high mechanical strength
and porosity and a large surface area of the metal portion, and is highly resistant
to thermal stress.
[0012] According to this invention, unwoven carbon fabric having carbon fibers bound together
by a resin is heated preferably at a temperature of 550-850°C in an inert atmosphere
using N₂ gas or Ar gas for one to two hours to impart conductivity to the binder resin
by carbonizing it. During this carbonizing process, the fiber surfaces and the resin
surface at its joint portion are finely roughened. A metal layer is formed on the
surface of the substrate of the unwoven carbon fabric thus heat-treated (i.e. on the
surfaces of the fibers and the resin) by electroplating. Then, the unwoven carbon
fabric is removed by roasting (baking for decarbonization), leaving an aggregate of
hollow metal fibers connected together and having their voids communicating with each
other. The aggregate of hollow metal fibers thus formed is heated in a reducing atmosphere
to densify them. The desired unwoven metal fiber, is thus obtained.
[0013] The unwoven carbon fiber, which is the substrate of the metal fabric according to
this invention, is prepared by forming a mixture of carbon fibers and a binder into
sheet form and drying the sheet thus formed so as to have a desired porosity. The
carbon fibers used may be mainly carbon fibers, graphite fibers or activated carbon
fibers.
[0014] The carbon fiber should be obtained by baking at preferably 750 - 900°C. If less
than 750°C, the resistivity of the carbon fibers will become too high (10⁴-10⁶Ω ·
cm), so that the resistivity of the sheet will be too high for the sheet to be electroplated.
If higher than 900°C, the fabric has to be heated in baking after electroplating to
more than 750°C to remove carbon fibers and binder. This lowers the strength of the
unwoven metal fabric.
[0015] The diameter of the fibers should be 7-20 µm. If less than 7 µm, the fabric formed
into sheet will be too limp and thus difficult to handle. If over 20 µm, the sheet
formed will be too stiff. The carbon packing density (how much fiber is filled per
unit volume) when the carbon fibers are formed into sheet form is determined by the
fiber length. The packing density in turn determines the structure of the unwoven
metal fabric finally obtained.
[0016] Namely, if the fabric formed is used as a filter, the carbon packing density factor
will influence its collecting capacity. If it is used as a battery electrode, the
carbon packing density will influence the contents of active materials. Also, it influences
the strength of the sheet. The fiber length should be determined so that the fiber
packing density will be 2-20%. If the fiber length is longer than 20 mm, the packing
density will be less than 2%. The sheet formed tends to be too low in strength. If
the fiber length is shorter than 3 mm, the fiber packing density will exceed 20%.
The fabric formed tends to be too low in porosity.
[0017] The amount of resin relative to the amount of carbon fibers should be within a predetermined
range. If lower than this range, it will be impossible to form the fibers into sheet
form. If higher than the range, the fabric will be clogged with the resin. The amount
of resin is adjustable by removing the volatile content by heating it. The structure
of the end product is influenced by the amount of resin.
[0018] To remove the volatile content of the resin, the fabric should be heated at a temperature
between 200°C and 350°C in the atmosphere. At a temperature less than 200 °C, the
volatile content would not volatilize sufficiently. The resin may foam when the fiber
sheet is later subjected to carbonizing later. If higher than 350°C, the resin would
decompose, weakening the structure of the fabric in sheet form. The heating conditions
should be controlled so that after this step, the resin content decreases to 5-15
wt%. If less than 5 wt%, it would be difficult for the fabric to retain its sheet
form. If more than 15 wt%, the fabric may be clogged with resin and also tend to be
stiff and difficult to bend. This step should be carried out for 10-90 minutes in
the atmosphere.
[0019] Then, the resin is carbonized in a non-oxidizing atmosphere. The non-oxidizing gas
used here may be H₂, low-molecular hydrocarbon, argon, N₂ gas. Argon or N₂ gas is
preferable. The heat treatment for carbonizing should be carried out once or more
than once at 500-850°C. From an economical viewpoint, the duration of this step should
be limited within 90 minutes. If the temperature is less than 500°C, the resin will
not carbonize sufficiently and thus the fabric will be low in conductivity for electroplating.
If higher than 850°C, the resin will carbonize excessively, so that the fabric sheet
will be low in flexibility. Under these conditions, the resin at the surface of carbon
fibers and at the joint portions between carbon fibers tend to agglomerate upon carbonizing,
so that the fabric thus treated will have a surface roughness of 0.5-1.5 µm. It is
preferable to treat the fabric for about one hour at 550-700°C.
[0020] The carbon unwoven fabric thus formed shows electrical conductivity even at the joint
portions. Its surface roughness is 0.5-1.5 µm. It is flexible enough to withstand
continuous plating. The surface roughness refers to irregularity in the direction
of thickness of carbon fiber.
[0021] Plating treatment is carried out using the unwoven carbon fiber as a cathode. The
metal to be plated may be of any kind provided it can be electroplated. Preferably,
a metal should be selected from Ni, Cu, Ag and Fe. As plating baths for Ni, Cu, Ag
and Fe, watts type, a copper sulfate solution, a silver cyanide solution, and a ferrous
sulfate solution are ordinarily used, respectively.
[0022] Plating conditions will be described in detail in the description of Examples. They
are determined so that the plating obtained has an average thickness of 3-10 µm. If
thinner than 3 µm, the fabric tends to be too low in strength and too flexible to
maintain its quality. If thicker than 10 µm, the entire unwoven fabric would become
so stiff that it is more likely to develop cracks when bent and also its porosity
would be low.
[0023] The porosity of the unwoven metal fabric should be controlled to 80 - 98% by adjusting
the packing density and the resin content of the unwoven carbon fabric and the thickness
of plating.
[0024] The metallic unwoven fabric after plating should be roasted in the atmosphere within
the temperature range of 600 - 900 C according to the kind of metal used to remove
the carbon fiber.
[0025] The unwoven fabric made up of metal fibers which has been surface-oxidized and hollowed
by roasting is reduced in a reducing atmosphere at a temperature of 600-1000 °C into
an end product.
[0026] In the aggregate of hollow metal fibers thus obtained, all the fiber are hollow and
each fiber has a roughness of 0.5-1.5 µm both on the inner and outer surfaces, with
the hollow fibers intersecting each other. The joint portions between them are wide
and joined together due to carbonization of the resin. Namely, the joint portions
have at least a width equal to or more than 50% of the diameter of the hollow portion
of each fiber (approximate to the original carbon fiber diameter). This prevent the
metal at the joint portions from being extremely thick. Such wide joint portions are
obtained by adjusting the resin content present in the unwoven carbon fabric to 5-15
wt% by heat treatment in the atmosphere.
[0027] According to the method of this invention, the resin binder forming the unwoven carbon
fabric is given conductivity by carbonizing it. Thus, it is possible to form a metal
layer directly on the surface of the resin, as well as on the carbon fibers, by electroplating.
Thus, there is no need to subject the fabric to electroless plating, which is not
favorable because it tends to widen quality variation of metal fabrics obtained and
also it causes the inclusion of impurities.
[0028] Further, by electroplating, the plating layer is deposited uniformly on the unwoven
carbon fabric, so that the wall thickness of the metal fibers will be very uniform.
Thus, the wall thickness of the hollow metal fibers can be made extremely thin, while
keeping a required mechanical strength of the fibers. This makes it possible to increase
the porosity of the entire fabric by reducing the wall thickness of the plated layer.
[0029] The unwoven metal fabric formed by the method according to this invention is made
up of metal fibers having their voids communicating with one another and having their
inner and outer surfaces roughened finely. Thus, its surface area is extremely large,
so that such metal fabric is especially suited for use as a catalyst or a catalyst
carrier. Also, because of its large surface area and high porosity, it shows excellent
collecting capacity when it is used as filter.
[0030] Moreover, because of its hollow structure and low metal-to-void ratio, the metal
fabric according to the present invention is extremely lightweight. Also, since metal
fibers are strongly bound together, the fabric as a whole has high mechanical strength.
Due to uniform wall thickness of the metal fibers, local stress concentration is less
liable to occur. This leads to prolonged life expectancy of the fabric.
[0031] Other features and objects of the present invention will become apparent from the
following description made with reference to the accompanying drawings, in which:
Figs. 1A to 1C are partially cutaway enlarged perspective views of the unwoven metal
fabric according to this invention, showing it after each of the manufacturing steps;
and
Figs. 2A to 2C are enlarged perspective views of joint portion of the unwoven metal
fabric, showing it after each of the manufacturing steps.
(Example 1)
[0032] An unwoven fabric 0.3 mm thick and 40 g/m² in weight per unit area was formed from
13 µm-diameter carbon fibers 1, using an epoxy resin as a binder. The content of resin
was 20 wt%. Fig. 1A shows an enlarged view of its part. Fig. 2A shows its joint portion.
[0033] This unwoven fabric was heated at 300°C in the atmosphere for one hour to remove
any low-temperature-volatile content in the binder. As a result, the content of binder
decreased to 10.1 wt% of the entire unwoven fabric. Then, the fabric was heated at
650°C for one hour in N₂ gas. Fig. 1B shows its portion. The surface is seen to have
irregularities 2. Fig. 2B shows its joint portion.
[0034] The fabric obtained was cut to a 200 mm x 400 mm sheet. The sheet was immersed in
a nickel plating bath shown in Fig. 1 and plated for 30 minutes while applying a current
at a rate of 9.42 A/dm² to form a plating layer 3. Fig. 1C shows a portion of the
fabric thus obtained.
[0035] Part of the fabric thus obtained was cut off and observed under an optical microscope
to measure the thickness of plating and the extent of surface irregularity was observed
under a scanning microscope. The results of measurements are shown at No. 1 in Table
1. The gap width at the joint in the table is the value
a in Fig. 2C and the gap diameter in the table is the value
b in Fig. 2C. This is the case for the other tables.
(Example 2)
[0036] Carbon fabrics were prepared in the same manner as in Example 1 with different contents
of epoxy resin as shown at Nos. 2-7 of Table 1. They were heated under the same conditions
as in Example 1, and then plated with nickel. Table 1 shows the results of observations
of these specimens. The specimens had different plating thicknesses from one another.
This was accomplished by changing the plating time.
(Example 3)
[0037] An unwoven fabric 0.42 mm thick and 30 g/m² in weight per unit area was formed from
carbon fibers 1 having a diameter of 7 µm, using an unsaturated polyester resin as
a binder. The content of resin was 20 wt% of the entire fabric.
[0038] This unwoven fabric was heated at 280°C in the atmosphere for 40 minutes to remove
any low-temperature-volatile content in the binder until the content of binder decreases
to 9.0 wt%. Then, the fabric was heated at 750°C for 40 minutes in N₂ gas.
[0039] The material thus obtained was wound on a 200-mm-diameter roll, and passed through
a plating bath for 25 minutes while applying a current at a rate of 11.3 A/dm² to
form a nickel plating layer 3 shown in Fig. 1C by continuous plating.
[0040] The fabric thus obtained was then roasted at 900°C for 10 minutes, and heated at
1000°C in H₂ gas to reduce its surface. An unwoven fabric made up of hollow metal
fibers 3 shown in Fig. 2C was obtained. As is apparent from this figure, the interior
of one metal fiber 3 communicates with that of another through an opening 5 at the
joint portion. The diameter
a of the opening 5 (gap width at joint) and the internal diameter
b of the metal fibers 3 (gap diameter) are determined to satisfy the relation a/b >
0.5.
[0041] Part of the metallic unwoven fabric thus obtained was cut off for observation under
an optical microscope and to measure its tensile strength. The results of observation
and measurement are shown at No. 8 in Table 2
(Example 4)
[0042] The same carbon fabrics as used in Example 3 were heated under different heating
conditions shown in Table 2 at Nos. 9-20. They were then plated with nickel in the
same manner as in Example 3. There were some specimens which could not be wound on
rolls. Such specimens were cut to 200 mm x 400 mm sheets and plated in batches. These
speciments were plated for 25 minutes while applying a current at a rate of 11.3 A/dm².
The results are shown at Nos. 9-20 in Table 2.
(Example 5)
[0043] The same unwoven carbon fabric as used in Example 1 was heated in the same manner
as in Example 1.
[0044] The unplated unwoven fabric thus obtained was cut to 200 mm x 400 mm sheets, and
the sheets were plated with nickel in the nickel bath shown in Table 1 under different
plating conditions.
[0045] After plating, the sheets were roasted and reduced under the conditions shown in
Table 3.
[0046] Part of each sheet was cut off for optical microscopic observation and to measure
its tensile strength. The results of observation and measurement are shown at Nos.
21-27 in Table 3.
(Example 6)
[0047] The same unwoven carbon fabric as used in Example 1 was heated in the same manner
as in Example 1.
[0048] The unplated unwoven fabric thus obtained was cut to a 200 mm x 400 mm sheet, and
the sheet was plated with Cu in a bath (containing 200 g/l of CuSO₄·5H₂O and 52 g/l
of H₂SO₄) kept at 30±2°C at a current of 2.0 A/dm² for 98 minutes.
[0049] After plating, it was roasted at 800°C for five minutes in the atmosphere, and then
reduced in an H₂ gas atmosphere at 950°C for 20 minutes. We observed the plating thus
formed. The results of observation are shown at No. 28 in Table 4.
(Example 7)
[0050] The same unwoven carbon fabric was plated with Ag under the same conditions as in
Example 6.
[0051] The Ag plating was formed in a bath containing 6 g/liter of AgCN and 110 g/liter
of KCN kept at 25 ± 2°C at a current of 5 A/dm² for 55 minutes.
[0052] After plating, it was roasted at 800°C for three minutes in the atmosphere, and then
reduced in an H₂ gas atmosphere at 850°C for 40 minutes. We observed the plating thus
formed. The results of observation are shown at No. 29 in Table 4.
(Example 8)
[0053] The same unwoven carbon fabric was plated with Fe under the same conditions as in
Example 7.
[0054] The Fe plating was formed in a bath containing 350 g/liter of FeSO4 (NH₄)₂SO₄·6H₂O
and 120 g/liter of (NH₄)₂SO₄ bath kept at 60°C±2°C at a current of 8 A/dm² for 35
minutes.
[0055] After plating, it was roasted at 800°C for three minutes in the atmosphere, and then
reduced in an H₂ gas atmosphere at 850°C for 40 minutes. We observed the plating thus
formed. The results of observation are shown at No. 30 in Table 4.
(Example 9)
[0056] An unwoven fabric 1.3 mm thick and 50 g/m² in weight per unit area was formed from
13-µm-diameter carbon fibers 1, using an epoxy resin as a binder. The content of resin
was 20 wt%.
[0057] This unwoven fabric was heated at 300°C in the atmosphere for one hour to remove
any low-temperature-volatile content in the binder. As a result, the content of binder
decreased to 10.1 wt% of the entire unwoven fabric.
[0058] Then, the fabric was heated at 650°C for one hour in N₂ gas. The fabric obtained
was cut to a 200 mm x 400 mm sheet. The sheet was immersed in a nickel plating bath
shown in Table 1 and plated for 38 minutes while applying a current at rate of 9.42
A/dm².
[0059] Part of the fabric thus obtained was cut off and observed under an optical microscope
to measure the thickness of plating and the extent of surface irregularity Its porosity
and tensile strength were also measured. The results of measurements are shown at
No. 31 in Table 4.
[0060] The hollow portions of the metal fibers communicate with each other through openings
formed at the joint portions of the fibers, so that the metal layer has a uniform
thickness. Such a metal layer shows increased strength and high resistance to thermal
stress.
[0061] According to the method of the present invention, electrical conductivity is given
to the joint portions of the carbon fibers by carbonizing the binder resin. When carbonizing,
the carbon fibers and the binder resin are roughened finely. A plating layer can be
formed directly on the unwoven carbon fabric thus formed by electroplating. Thus,
it is possible to form a sufficiently thin layer without the possibility of inclusion
of impurities and wide quality variation. The unwoven metal fabric made up of hollow
metal fibers according to the present invention excels conventional metal fabrics
of this type in its mechanical strength, porosity, surface area, distribution of fibers
and weight.
[Table 1]
| No |
Amount of binder after volatile removed (wt%) |
*1 Electroplating |
Gap width a / diameter b of hollow portions |
Roughness at surface (µm) |
| |
|
Average Thickness (µm) |
Gap width a at joint portions (µm) |
|
|
| 1 |
10.1 |
7 |
12.1 |
0.93 |
1.0 |
| 2 |
5.1 |
10 |
6.5 |
0.5 |
0.5 |
| 3 |
7.3 |
9 |
9.1 |
0.7 |
0.8 |
| 4 |
12.2 |
9 |
14.3 |
1.1 |
1.2 |
| 5 |
14.8 |
5 |
17.0 |
1.3 |
1.5 |
| 6 |
*2 15.5 |
7 |
17.9 |
1.4 |
1.8 |
| 7 |
9.0 |
3 |
13.0 |
1.0 |
0.5 |
| *1 For plating, watt bath (45 g/l of boric acid, 40 g/l of nickel chloride, 330 g/l
of nickel sulfide) was used, Ni plate as anode. Used at about 55°C while agitating.
Plating conditions; Current constant at 9.42 A/dm², plating thickness adjusted by
changing the plating time. |
| *2 This is a control example. |

[0062]
[Table 4]
| No |
Metal plated |
Plated State |
Gap width a / diameter b of hollow portions |
Porosity (%) |
Tensile Strength (kg/mm²) |
| |
|
Average Thickness (µm) |
Roughness at surface (µm) |
Gap width a at joint portions (µm) |
|
|
|
| 28 |
Cu |
7.0 |
1.1 |
9.1 |
0.70 |
88 |
1.7 |
| 29 |
Ag |
8.2 |
1.0 |
12.1 |
0.93 |
85 |
1.5 |
| 30 |
Fe |
8.2 |
1.0 |
12.1 |
0.93 |
85 |
1.2 |
| 31 |
Ni |
7.0 |
1.0 |
12.1 |
0.93 |
97.0 |
1.5 |
1. An unwoven metal fabric comprising an aggregate of hollow metal fibers, said metal
fibers being joined together, the hollow portions of said fibers communicating with
each other at joint portions between said metal fibers, said metal fibers having a
roughness of 0.5-1.5 µm on inner and outer surfaces thereof.
2. An unwoven metal fabric as claimed in claim 1 wherein the portion of the fabric except
said joint portions has an average metal thickness of 3-10 µm.
3. An unwoven metal fabric as claimed in claim 1 or 2 wherein it has a porosity of 80
to 98%.
4. An unwoven metal fabric as claimed in any of claims 1-3 wherein the minimum width
of the opening of said metal fibers at said joint portions is not less than 50% of
the diameter of the hollow portions of said metal fibers.
5. An unwoven metal fabric as claimed in any of claims 1-4 wherein said metal fibers
are formed from one selected from the group consisting of Ni, Cu, Ag and Fe.
6. A method of manufacturing an unwoven metal fabric comprising the steps of joining
a plurality of carbon fibers together by means of a resin to provide an unwoven fabric
material, heating said unwoven fabric material to carbonate said resin and impart
conductivity to said resin and roughen both the fiber surface and the resin surface,
forming a metal layer on the surface of said fabric and said resin by electroplating,
roasting the unwoven fabric material to remove the carbon fibers, and reducing said
unwoven fabric material in a reducing atmosphere to make dense the metallic structure.
7. A method of manufacturing an unwoven metal fabric as claimed in claim 6 wherein said
heating step comprises heating said unwoven fabric material at 200-350°C in the atmosphere
and then heating at 500-850°C in a non-oxidizing atmosphere, said heatings being carried
out at least once.
8. A method of manufacturing an unwoven metal fabric as claimed in claim 6 or 7 wherein
as the carbon fibers forming said unwoven carbon fabric is one obtained by heating
carbon fiber to 750-900°C.
9. A method of manufacturing an unwoven metal fabric as claimed in any of claims 6-8
wherein said carbon fibers forming said unwoven carbon fabric have a diameter of 7-20
µ m, a fiber length of 3-20 mm and a packing density of 2-20%.