Technical Field
[0001] The present invention generally relates to a method for producing a composite plated
product. More specifically, the invention relates to a method for producing a composite
plated product wherein a coating of a composite material containing carbon particles
in a silver layer is formed on a substrate and which is used as a material of contact
and terminal parts such as switches and connectors.
Background Art
[0002] Conventionally, as materials of contact and terminal parts such as switches and connectors,
there are used silver-plated products wherein a conductive material such as copper
or a copper alloy is plated with silver in order to prevent oxidation of the conductive
material due to heat in sliding processes.
[0003] However, there is a problem in that silver coatings are easily stripped by sliding
since they are soft and easily wear and since they generally have a high coefficient
of friction. In order to solve this problem, there is proposed a method for improving
the wear resistance of a conductive material by electroplating the conductive material
with a composite material wherein graphite particles are dispersed in a silver matrix
(see, e.g., Japanese Patent Laid-Open No.
9-7445). There is also proposed a method for producing a silver coating, which contains
graphite particles, by means of a plating bath to which a wetting agent suitable for
the dispersion of graphite particles is added (see, e.g., Japanese Patent Unexamined
Publication No.
5-505853 (National Publication of Translated Version of
PCT/DE91/00241)). Moreover, there is proposed a method for coating carbon particles with a metal
oxide or the like by the sol-gel method to enhance the dispersibility of the carbon
particles in a composite plating bath of silver and the carbon particles to increase
the quantity of carbon particles in a composite coating (see, e.g., Japanese Patent
Laid-Open No.
3-253598).
[0004] However, composite plated products produced by the above-described conventional methods
have a relatively high coefficient of friction and a relatively low wear resistance,
so that there is a problem in that the composite plated products can not be used as
the materials of long-life contacts and terminals. Therefore, it is desired to provide
a composite plated product which has a larger content of carbon, a larger quantity
of carbon particles on the surface thereof, and a better wear resistance than those
of the composite plated products produced by the conventional methods.
[0005] For that reason, the inventors has proposed a method for producing a composite plated
product wherein a coating of a composite material containing carbon particles in a
silver layer is formed on a substrate, the composite plated product having a large
content of carbon and a large quantity of carbon particles on the surface thereof
and having a low coefficient of friction and an excellent wear resistance, by electroplating
a substrate in a silver plating solution to which carbon particles treated by an oxidation
treatment and a silver matrix orientation adjusting agent are added (see Japanese
Patent Application No.
2005-195678).
[0006] However, there is a problem in that the wear resistance of the composite plated product
is deteriorated if the current density in the plating process is increased in order
to improve the productivity of the composite plated product in the method proposed
in Japanese Patent Application No.
2005-195678.
Disclosure of the Invention
[0007] It is therefore an object of the present invention to eliminate the aforementioned
problems and to provide a method for producing a composite plated product wherein
a coating of a composite material containing carbon particles in a silver layer is
formed on a substrate by using a composite plating solution wherein carbon particles
treated by an oxidation treatment and a silver matrix orientation adjusting agent
are added to a silver plating solution, said method being capable of preventing the
wear resistance of the composite plated product from being deteriorated even if the
current density in a plating process is increased.
[0008] In order to accomplish the aforementioned obj ect, the inventors have diligently
studied and found that it is possible to prevent the wear resistance of a composite
plated product from being deteriorated even if the current density in a plating process
is increased, if the molar ratio of silver to free cyanogen in a composite plating
solution is adjusted in a method for producing a composite plated product wherein
a coating of a composite material containing carbon particles in a silver layer is
formed on a substrate by using a composite plating solution wherein carbon particles
treated by an oxidation treatment and a silver matrix orientation adjusting agent
are added to a silver plating solution. Thus, the inventors have made the present
invention.
[0009] A method for producing a composite plated product according to the present invention,
comprises the steps of: preparing carbon particles and a silver matrix orientation
adjusting agent which is an agent for adjusting the orientation of a silver matrix;
treating the carbon particles by an oxidation treatment; adding the treated carbon
particles and the silver matrix orientation adjusting agent to a silver plating solution
to form a composite plating solution which contains the treated carbon particles and
the silver matrix orientation adjusting agent; and electroplating a substrate in the
composite plating solution to form a coating of a composite material, which contains
the treated carbon particles in a silver layer, on the substrate, wherein the molar
ratio of silver to free cyanogen in the composite plating solution is adjusted so
as not to be less than 0.7, preferably so as to be in the range of from 0.7 to 1.3.
In this method for producing a composite plated product, the silver matrix orientation
adjusting agent preferably contains selenium ions, and is more preferably potassium
selenocyanate. In addition, the concentration of the silver matrix orientation adjusting
agent in the composite plating solution is preferably adjusted so as to be in the
range of from 5 mg/l to 20 mg/l. Moreover, the coating is preferably formed by electroplating
the substrate at a current density of 1 to 3 A/dm
2.
[0010] A composite plating solution according to the present invention comprises: a silver
plating solution for plating a substrate with silver; carbon particles treated by
an oxidation treatment to be added to the silver plating solution; and a silver matrix
orientation adjusting agent added to the silver plating solution, wherein the molar
ratio of silver to free cyanogen in the composite plating solution is not less than
0.7.
[0011] According to the present invention, it is possible to prevent the wear resistance
of a composite plated product from being deteriorated even if the current density
in a plating process is increased, in a method for producing a composite plated product
wherein a coating of a composite material containing carbon particles in a silver
layer is formed on a substrate by using a composite plating solution wherein carbon
particles treated by an oxidation treatment and a silver matrix orientation adjusting
agent are added to a silver plating solution. Therefore, it is possible to improve
the productivity of the composite plated product. In addition, the composite plated
product can be used as a material capable of sufficiently increasing the life of terminals
such as switches and connectors.
Brief Description of the Drawings
[0012]
FIG. 1 is a schematic diagram for explaining an electric contact using a composite
plated product according to the present invention.
Best Mode for Carrying Out the Invention
[0013] In a preferred embodiment of a method for producing a composite plated product according
to the present invention, the molar ratio of silver to free cyanogen (the molar ratio
of silver/free cyanogen) in a composite plating solution, wherein carbon particles
treated by an oxidation treatment and a silver matrix orientation adjusting agent
are added to a silver plating solution, is adjusted to be 0.7 or more, preferably
in the range of from 0.7 to 1.3, and the amount of the silver matrix orientation adjusting
agent in the composite plating solution is preferably adjusted to be in the range
of from 5 mg/l to 20 mg/l. This composite plating solution is used for electroplating
a substrate, so that a coating of a composite material containing carbon particles
in a silver layer is formed on the substrate.
[0014] In the preferred embodiment of a method for producing a composite plated product
according to the present invention, lipophilic organic substances absorbed onto the
surface of carbon particles are removed by the oxidation treatment before the carbon
particles are added to a silver plating solution. Such lipophilic organic substances
include aliphatic hydrocarbons, such as alkanes and alkenes, and aromatic hydrocarbons,
such as alkylbenzene.
[0015] As the oxidation treatment for carbon particles, a wet oxidation treatment, or a
dry oxidation treatment using oxygen gas or the like may be used. In view of mass
production, a wet oxidation treatment is preferably used. If a wet oxidation treatment
is used, it is possible to uniformly treat carbon particles having a large surface
area.
[0016] As the wet oxidation treatment, there may be used a method for suspending carbon
particles in an aqueous solution containing a conductive salt to put therein platinum
electrodes or the like as a cathode and anode to carry out electrolysis, or a method
for suspending carbon particles in water to add an optimum quantity of oxidizing agent
thereto. In view of productivity, the latter is preferably used, and the quantity
of carbon particles added to water is preferably in the range of from 1 % to 20 %
by weight. The oxidizing agent may be nitric acid, hydrogen peroxide, potassium permanganate,
potassium persulfate, sodium perchlorate or the like. It is considered that the lipophilic
organic substances adhering to carbon particles are oxidized by the added oxidizing
agent so as to be soluble in water to be suitably removed from the surface of the
carbon particles. If the carbon particles treated by the wet oxidation treatment are
filtered and washed, it is possible to further enhance the function of removing the
lipophilic organic substances from the surface of the carbon particles.
[0017] The lipophilic organic substances, such as aliphatic and aromatic hydrocarbons, can
be thus removed from the surface of the carbon particles by the above-described oxidation
treatment. According to analysis based on gases heated at 300 °C, gases generated
by heating carbon particles to 300 °C after the oxidation treatment hardly contain
lipophilic aliphatic hydrocarbons such as alkanes and alkens, and lipophilic aromatic
hydrocarbons such as alkylbenzenes. Even if the carbon particles after the oxidation
treatment slightly contain aliphatic and aromatic hydrocarbons, the carbon particles
can be dispersed in a silver plating solution. However, the carbon particles do not
preferably contain hydrocarbons having a molecular weight of 160 or more, and the
intensity (the intensity in purge and gas chromatography and mass spectroscopy) of
gases generated at 300 °C from hydrocarbons having a molecular weight of less than
160 in the carbon particles is preferably 5,000,000 or less. It is considered that,
if the carbon particles contain hydrocarbons having a large molecular weight, the
surface of each of the carbon particles is coated with strong lipophilic hydrocarbons,
and the carbon particles are coagulated in the silver plating solution which is an
aqueous solution, so that the carbon particles do not form a coating of a composite
material.
[0018] When carbon particles, from which aliphatic and aromatic hydrocarbons are removed
by the above-described oxidation treatment, are suspended in the silver plating solution
to carry out electroplating, a cyanide containing silver plating solution is preferably
used as the silver plating solution. In the conventional methods, it is required to
add a surface active agent to a silver plating solution if it is a cyanide containing
silver plating solution. However, in the preferred embodiment of a method for producing
a composite plated product according to the present invention, it is not required
to add any surface active agents to the silver plating solution, since it is possible
to obtain a composite plating solution wherein carbon particles are uniformly dispersed
in the silver plating solution even if no surface active agent is added thereto. Furthermore,
the concentration of carbon particles in the composite plating solution is preferably
in the range of from 40 g/l to 200 g/l. If it is less than 40 g/l, the content of
carbon particles in the composite coating is considerably decreased, and if it exceeds
200 g/l, the viscosity of the composite plating solution is increased, so that it
is difficult to agitate the composite plating solution.
[0019] If a cyanide containing silver plating solution is used, it is possible to obtain
a composite coating which has a large content of carbon and a large quantity of carbon
particles on the surface thereof. It is considered that the reason why the content
of carbon in the coating is increased is that carbon particles are easily incorporated
into a silver matrix since the silver plating solution does not contain any surface
active agents to prevent the surface active agents from being absorbed onto the growth
surface of a silver plating crystal when the crystal grows. It is also considered
that the reason why the quantity of carbon particles on the surface of the coating
is increased is that it is difficult for the carbon particles to be removed from the
surface of the coating (similar to the cleaning function of detergent) during washing
after plating, since the silver plating solution does not contain any surface active
agents.
[0020] If carbon particles treated by the oxidation treatment are thus added to a silver
plating solution, it is possible to sufficiently disperse the carbon particles in
the silver plating solution without using any additives such as dispersing agents
and without coating the surface of the carbon particles. In addition, if such a silver
plating solution is used for carrying out electroplating, it is possible to produce
a composite plated product wherein a coating of a composite material containing the
carbon particles in a silver layer is formed on a substrate, the composite plated
product having a large content of carbon and a large quantity of carbon particles
on the surface thereof and having an excellent wear resistance.
[0021] In the preferred embodiment of a method for producing a composite plated product
according to the present invention, the cyanide containing silver plating solution
preferably contains potassium silver cyanide (K[Ag(CN)
2]) and potassium cyanide (KCN). The concentration (X) of potassium silver cyanide
in the cyanide containing silver plating solution is preferably in the range of from
about 250 g/l to about 300 g/l, and the concentration (Y) of potassium cyanide in
the cyanide containing silver plating solution is in the range of from about 80 g/l
to about 120 g/l. The molecular weight of potassium silver cyanide is 199, and the
molecular weight of potassium cyanide is 65.1. Therefore, the molar ratio (Z) of silver
to free cyanogen (the molar ratio of silver/free cyanogen) is preferably in the range
of from 0.7 to 1.3 ad derived from the expression Z = (X/199)/(Y/65.1). If this ratio
is less than 0.7, the orientation plane of the silver matrix is (111) plane to deteriorate
the wear resistance of the composite plated product when the current density in the
plating process is increased. On the other hand, if the molar ratio exceeds 1.3, it
is difficult to dissolve potassium silver cyanide serving as the source of silver.
[0022] In the preferred embodiment of a method for producing a composite plated product
according to the present invention, there is used a composite plating solution wherein
a silver matrix orientation adjusting agent for adjusting the orientation of a silver
matrix is added to a silver plating solution in addition to the carbon particles treated
by the oxidation treatment. The silver matrix orientation adjusting agent preferably
contains selenium (Se) ions, and is more preferably potassium selenocyanate (KSeCN).
The concentration of the silver matrix orientation adjusting agent in the composite
plating solution is preferably in the range of from 5 mg/l to 20 mg/l. If such a silver
matrix orientation adjusting agent is added to the silver plating solution, the orientation
of the silver matrix is considerably changed in accordance with the concentration
of selenium ions. That is, the orientation plane of the silver matrix is (111) plane
in conventional composite plated products coated with a composite material of silver
and graphite particles. However, if the silver matrix orientation adjusting agent
is added to the silver plating solution, the orientation plane of the silver matrix
is changed to be (220) plane. It is considered that the coating is formed of fine
crystal grains, so that the characteristics of the coating are greatly changed by
the direction of growth of crystal grains. It is also considered that, if the crystal
orientation of carbon particles in the composite material and the orientation of crystal
grains in the silver matrix are optimum, the silver matrix is easily deformed by friction
and sliding, and the coefficient of friction is greatly decreased in cooperation with
the lubricity of carbon particles, so that the wear resistance of the composite plated
product is improved.
[0023] It is considered that the composite coating of silver and carbon particles, wherein
the orientation plane of a silver matrix is (220) plane, is formed by adding selenium
ions to the composite plating solution containing carbon particles dispersed therein
without adding any surface active agents. That is, in conventional composite coatings
which contain graphite particles in the silver layer, a surface active agent is added
to a silver plating solution in order to sufficiently disperse carbon particles therein.
However, it is considered that the surface active agent is also absorbed onto the
composite coating to have an influence on the direction of growth of the silver matrix,
so that it is difficult to obtain a composite coating wherein the orientation plane
of a silver matrix is (220) plane.
[0024] By thus forming a composite coating wherein the orientation plane of the silver matrix
is (220) plane, the composite coating can have a lower coefficient of friction. That
is, if a silver plating solution containing a surface active agent is used as conventional
methods, it is not possible to obtain a composite coating wherein the orientation
plane of a silver matrix is (220) plane. Therefore, the coefficient of friction of
any one of the composite coating products produced by conventional methods is higher
than that of a composite coating product produced by the preferred embodiment of a
method for producing a composite plated product according to the present invention,
and the wear resistance thereof is lower than that of a composite coating product
produced by the preferred embodiment of a method for producing a composite plated
product according to the present invention.
[0025] By the above-described preferred embodiment of a method for producing a composite
plated product according the present invention, it is possible to produce a composite
plated product wherein a coating of a composite material containing 1.7 to 2.5 % by
weight of carbon particles in a silver layer is formed on a substrate, the quantity
of the carbon particles on the surface thereof (the rate of carbon particles coating
the substrate) being 25 % by area or more, and the orientation plane of a silver matrix
being (220) plane. Furthermore, the wear resistance of the composite plated product
is improved as the content of carbon in the composite coating is increased. In a composite
plated product produced by the above-described preferred embodiment of a method for
producing a composite plated product according to the present invention, the content
of carbon in the coating can be 1.7 to 2.5 % by weight, and the quantity of carbon
particles on the surface of the coating can be 25 % by area or more, although the
quantity of carbon particles on the surface of the coating is about 5 % by area in
conventional composite plated products of silver and graphite. Therefore, it is possible
to obtain a composite plated product having an excellent wear resistance. In addition,
since the orientation plane of the silver matrix is (220) plane, it is possible to
obtain a composite plated product having a coefficient of friction, which is greatly
decreased in cooperation with the lubricity of carbon particles, and having an excellent
wear resistance.
[0026] The thickness of the composite plated product is preferably in the range of from
2 µm to 10 µm. If the thickness of the composite plated product is less than 2 µm,
the wear resistance thereof is insufficient, and if it exceeds 10 µm, the production
efficiency thereof is bad.
[0027] In an electric contact comprising a stationary contact 10 and a movable contact 12
which is slidable on the stationary contact 10 in directions shown by arrow A in FIG.
1, if at least one of the stationary contact 10 and the movable contact 12 is formed
of a composite plated product according to the present invention, the electric contact
can have an excellent wear resistance. In this case, only a part of one of the stationary
contact 10 and the movable contact 12 contacting the other contact may be formed of
a composite plate product according to the present invention.
[0028] Examples of a method for producing a composite plated product according to the present
invention will be described below in detail.
Examples 1 and 2
[0029] First, 6 % by weight of scale-shaped graphite particles (Carbon SN-5 produced by
SEC Corporation) having a mean particle diameter of 5 µm were prepared as carbon particles
to be added to 3 liters of pure water. The mixed solution thus obtained was heated
to 50 °C while being stirred. Then, 1.2 liters of a solution containing 0.1 mol/l
of potassium persulfate was prepared as an oxidizing agent to be gradually dropped
to the mixed solution, and then, stirred for two hours to carry out an oxidation treatment.
Thereafter, filtration was carried out by means of a filter paper, and washing was
carried out.
[0030] With respect to carbon particles before and after the oxidation treatment, gases
generated at 300 °C were analyzed by means of a purge and gas chromatography and mass
spectrometer (Japan Analysis Industry JHS-100) (GCMAS QP-5050A produced by Shimadzu
Corp.). As a result, it was found that lipophilic aliphatic hydrocarbons, such as
nonane, decane and 3-methyl-2-hepten, and lipophilic aromatic hydrocarbons, such as
xylene, were removed from the carbon particles by the above-described oxidation treatment.
[0031] Then, 80 g/l of carbon particles treated by the above-described oxidation treatment
were added to a cyanide containing silver plating solution comprising 280 g/l of potassium
silver cyanide and 90 g/l of potassium cyanide, the molar ratio of silver/free cyanogen
in the cyanide containing silver plating solution being 1.01. After the carbon particles
were thus dispersed and suspended therein, 12 mg/l of potassium selenocyanate serving
as a silver matrix orientation adjusting agent was added thereto to prepare a composite
plating solution of silver and carbon particles. This composite plating solution was
used for electroplating a copper plate serving as a raw material having a thickness
of 0.3 mm at a temperature of 25 °C and at a current density of 1 A/dm
2 (Example 1) and 3 A/dm
2 (Example 2), respectively, to produce a composite plated product wherein a composite
coating of silver and carbon particles having a thickness of 5 µm was formed on the
copper plate. Furthermore, in order to improve the adhesion of the coating, silver
strike plating was carried out as underlayer plating at a temperature of 25 °C and
at a current density of 3 A/dm
2 in a silver strike plating bath containing 3 g/l of potassium silver cyanide and
100 g/l of potassium cyanide.
[0032] Samples were cut out of the composite plated product (containing the raw material)
to be prepared for analyses of Ag and C, respectively. The content by weight (X wt%)
of Ag in the sample was obtained by the plasma spectroscopic analysis by means of
an ICP device (IRIS/AR produced by Jarrell Ash Corporation), and the content by weight
(Y wt%) of C in the sample was obtained by the infrared analysis by means of a carbon/sulfur
microanalyzer (EMIA-U510 produced by HORIBA, Ltd.). Then, the content by weight of
C in the coating was calculated as Y/(X+Y). As a result, the content by weight of
C in the coating was 2.1 % and 2.5 % by weight in Examples 1 and 2, respectively.
[0033] The surface of a test piece cut out of each of the composite plated products was
observed, and the quantity (% by area) of carbon particles on the surface of the coating
of the test piece was calculated as follows. First, an image of the surface of the
test piece was taken as a super depth image at an objective lens power of 100 by means
of a super depth shape microscope (VK-8500 produced by KEYENCE CORPORATION). Then,
an image analyzing application (SCION IMAGE produced by SCION CORPORATION) was used
on a personal computer for incorporating the image as a monochrome to indicate the
contrast of the image as binary digits, so that the portions of silver were separated
from the portions of carbon particles. Then, the quantity of carbon particles on the
surface of the coating was calculated as a ratio Y/X of the number (Y) of pixels of
the portions of carbon particles to the number (X) of pixels of the whole image. As
a result, the quantity of carbon particles on the surface of the coating was 32 %
to 34 % by area in Examples 1 and 2, respectively.
[0034] Then, the orientation of the silver matrix of a test piece cut out of each of the
composite plated products was evaluated. In the evaluation of the orientation of the
silver matrix, an X-ray diffractometer (XRD) (RAF-rB produced by RIGAKU Corporation)
wasusedformeasuringX-ray diffraction peaks, and the plane orientation of the strongest
peak of the silver matrix was evaluated as the orientation of crystal of the coating.
Furthermore, Cu-Kα was used as a vessel for measuring the X-ray diffraction peaks
at 50 kV and 100 mA. In addition, a scintillation counter, a wide angle goniometer,
and a curved crystal monochromator were used. The scanning range 2 θ / θ was in the
range of from 10° to 90° , and the step width was 0.05° . The scanning mode was FT,
and the sampling time was 1.00 second. As a result, the orientation plane of the silver
matrix was (220) plane in Examples 1 and 2.
[0035] One of two test pieces cut out of each of the composite plated products thus obtained
was intended (R=3mm) to be used as an indenter, and the other test piece was used
as an evaluating sample, so that the wear resistance of each of the composite plated
products was evaluated by confirming the wearing state of each of the composite plated
products by continuing the reciprocating sliding movement (sliding distance: 10 mm,
sliding speed: 2.5 Hz) of the indenter while pushing the indenter against the evaluating
sample at a constant load (0.5 N) until the raw material was exposed. As a result,
in Examples 1 and 2, the raw material was not exposed after the reciprocating sliding
movement was repeated 500,000 times or more.
Examples 3 and 4
[0036] Composite plated products were produced by the same method as that in Examples 1
and 2, respectively, except that the amount of potassium selenocyanate added as a
silver matrix orientation adjusting agent was 16 mg/l. With respect to the composite
plated products thus obtained, the content of carbon particles in the coating, and
the quantity (% by area) of carbon particles on the surface of the coating were calculated
by the same methods as those in Examples 1 and 2, and the orientation of the silver
matrix and the wear resistance thereof were evaluated by the same methods as those
in Examples 1 and 2. As a result, in Examples 3 and 4, the content of carbon particles
was 1.6 % and 2.4 % by weight, respectively, and the quantity of carbon particles
on the surface was 33 % and 35 % by area, respectively. In addition, the orientationplane
of the silvermatrixwas (220) plane. Moreover, the substrate was not exposed after
the reciprocating sliding movement was repeated over 500,000 times.
Examples 5 and 6
[0037] Composite plated products were produced by the same method as that in Examples 1
and 2, respectively, except that there was used a cyanide containing silver plating
solution comprising 240 g/l of potassium silver cyanide and 90 g/l of potassium cyanide,
the molar ratio of silver/free cyanogen in the cyanide containing silver plating solution
being 0.87, and that the amount of potassium selenocyanate added as a silver matrix
orientation adjusting agent was 8 mg/l. With respect to the composite plated products
thus obtained, the content of carbon particles in the coating, and the quantity (%
by area) of carbon particles on the surface of the coating were calculated by the
same methods as those in Examples 1 and 2, and the orientation of the silver matrix
and the wear resistance thereof were evaluated by the same methods as those in Examples
1 and 2. As a result, in Examples 5 and 6, the content of carbon particles was 2.0
% and 1.8 % by weight, respectively, and the quantity of carbon particles on the surface
was 32 % and 31 % by area, respectively. In addition, the orientation plane of the
silver matrix was (220) plane. Moreover, the substrate was not exposed after the reciprocating
sliding movement was repeated over 500,000 times.
Examples 7 and 8
[0038] Composite plated products were produced by the same method as that in Examples 1
and 2, respectively, except that there was used a cyanide containing silver plating
solution comprising 240 g/l of potassium silver cyanide and 90 g/l of potassium cyanide,
the molar ratio of silver/free cyanogen in the cyanide containing silver plating solution
being 0.87. With respect to the composite plated products thus obtained, the content
of carbon particles in the coating, and the quantity (% by area) of carbon particles
on the surface of the coating were calculated by the same methods as those in Examples
1 and 2, and the orientation of the silver matrix and the wear resistance thereof
were evaluated by the same methods as those in Examples 1 and 2. As a result, in Examples
7 and 8, the content of carbon particles was 1.9 % and 2.3 % by weight, respectively,
and the quantity of carbon particles on the surface was 31 % and 33 % by area, respectively.
In addition, the orientation plane of the silver matrix was (220) plane. Moreover,
the substrate was not exposed after the reciprocating sliding movement was repeated
over 500,000 times.
Comparative Examples 1 and 2
[0039] Composite plated products were produced by the same method as that in Examples 1
and 2, respectively, except that there was used a cyanide containing silver plating
solution comprising 100 g/l of potassium silver cyanide and 120 g/l of potassium cyanide,
the molar ratio of silver/free cyanogen in the cyanide containing silver plating solution
being 0.27, and that the amount of potassium selenocyanate added as a silver matrix
orientation adjusting agent was 4 mg/l. With respect to the composite plated products
thus obtained, the content of carbon particles in the coating, and the quantity (%
by area) of carbon particles on the surface of the coating were calculated by the
same methods as those in Examples 1 and 2, and the orientation of the silver matrix
and the wear resistance thereof were evaluated by the same methods as those in Examples
1 and 2. As a result, in Comparative Examples 1 and 2, the content of carbon particles
was 2.2 % and 1.7 % by weight, respectively, and the quantity of carbon particles
on the surface was 34 % and 22 % by area, respectively. In addition, the orientation
plane of the silver matrix was (220) plane in Comparative Example 1 wherein electroplating
was carried out at a current density of 1 A/dm
2, whereas the orientation plane of the silver matrix was (111) plane in Comparative
Example 2 wherein electroplating was carried out at a current density of 3 A/dm
2. Moreover, the substrate was not exposed after the reciprocating sliding movement
was repeated over 500,000 times in Comparative Example 1 wherein electroplating was
carried out at a current density of 1 A/dm
2, whereas the substrate was exposed after the reciprocating sliding movement was repeated
about 480,000 times in Comparative Example 2 wherein electroplating was carried out
at a current density of 3 A/dm
2.
Comparative Examples 3 and 4
[0040] Composite plated products were produced by the same method as that in Comparative
Examples 1 and 2, respectively, except that the amount of potassium selenocyanate
added as a silver matrix orientation adjusting agent was 8 mg/l. With respect to the
composite plated products thus obtained, the content of carbon particles in the coating,
and the quantity (% by area) of carbon particles on the surface of the coating were
calculated by the same methods as those in Examples 1 and 2, and the orientation of
the silver matrix and the wear resistance thereof were evaluated by the same methods
as those in Examples 1 and 2. As a result, in Comparative Examples 3 and 4, the content
of carbon particles was 2.0 % and 1.5 % by weight, respectively, and the quantity
of carbon particles on the surface was 27 % and 21 % by area, respectively. In addition,
the orientation plane of the silver matrix was (220) plane in Comparative Example
3 wherein electroplating was carried out at a current density of 1 A/dm
2, whereas the orientation plane of the silver matrixwas (200) plane in Comparative
Example 4 wherein electroplating was carried out at a current density of 3 A/dm
2. Moreover, the substrate was not exposed after the reciprocating sliding movement
was repeated over 500,000 times in Comparative Example 3 wherein electroplating was
carried out at a current density of 1 A/dm
2, whereas the substrate was exposed after the reciprocating sliding movement was repeated
about 420,000 times in Comparative Example 4 wherein electroplating was carried out
at a current density of 3 A/dm
2.
Comparative Examples 5 and 6
[0041] Composite plated products were produced by the same method as that in Examples 1
and 2, respectively, except that there was used a cyanide containing silver plating
solution comprising 185 g/l of potassium silver cyanide and 90 g/l of potassium cyanide,
the molar ratio of silver/free cyanogen in the cyanide containing silver plating solution
being 0.67, and that the amount of potassium selenocyanate added as a silver matrix
orientation adjusting agent was 4 mg/l. With respect to the composite plated products
thus obtained, the content of carbon particles in the coating, and the quantity (%
by area) of carbon particles on the surface of the coating were calculated by the
same methods as those in Examples 1 and 2, and the orientation of the silver matrix
and the wear resistance thereof were evaluated by the same methods as those in Examples
1 and 2. As a result, in Comparative Examples 5 and 6, the content of carbon particles
was 1.8 % and 1.7 % by weight, respectively, and the quantity of carbon particles
on the surface was 33 % and 28 % by area, respectively. In addition, the orientation
plane of the silver matrix was (220) plane in Comparative Example 5 wherein electroplating
was carried out at a current density of 1 A/dm
2, whereas the orientation plane of the silver matrix was (200) plane in Comparative
Example 6 wherein electroplating was carried out at a current density of 3 A/dm
2. Moreover, the substrate was exposed after the reciprocating sliding movement was
repeated about 480,000 times in Comparative Example 5 wherein electroplating was carried
out at a current density of 1 A/dm
2, and the substrate was exposed after the reciprocating sliding movement was repeated
about 310,000 times in Comparative Example 6 wherein electroplating was carried out
at a current density of 3 A/dm
2.
Comparative Examples 7 and 8
[0042] Composite plated products were produced by the same method as that in Comparative
Examples 5 and 6, respectively, except that the amount of potassium selenocyanate
added as a silver matrix orientation adjusting agent was 12 mg/l. With respect to
the composite plated products thus obtained, the content of carbon particles in the
coating, and the quantity (% by area) of carbon particles on the surface of the coating
were calculated by the same methods as those in Examples 1 and 2, and the orientation
of the silver matrix and the wear resistance thereof were evaluated by the same methods
as those in Examples 1 and 2. As a result, in Comparative Examples 7 and 8, the content
of carbon particles was 1.8 % and 1.6 % by weight, respectively, and the quantity
of carbon particles on the surface was 31 % and 21 % by area, respectively. In addition,
the orientation plane of the silver matrix was (220) plane in Comparative Example
7 wherein electroplating was carried out at a current density of 1 A/dm
2, whereas the orientation plane of the silver matrix was (111) plane in Comparative
Example 8 wherein electroplating was carried out at a current density of 3 A/dm
2. Moreover, the substrate was not exposed after the reciprocating sliding movement
was repeated over 500,000 times in Comparative Example 7 wherein electroplating was
carried out at a current density of 1 A/dm
2, whereas the substrate was exposed after the reciprocating sliding movement was repeated
about 370,000 times in Comparative Example 8 wherein electroplating was carried out
at a current density of 3 A/dm
2.
Comparative Examples 9 and 10
[0043] Composite plated products were produced by the same method as that in Examples 1
and 2, respectively, except that the amount of potassium selenocyanate added as a
silver matrix orientation adjusting agent was 4 mg/l. With respect to the composite
plated products thus obtained, the content of carbon particles in the coating, and
the quantity (% by area) of carbon particles on the surface of the coating were calculated
by the same methods as those in Examples 1 and 2, and the orientation of the silver
matrix and the wear resistance thereof were evaluated by the same methods as those
in Examples 1 and 2. As a result, in Comparative Examples 9 and 10, the content of
carbon particles was 1.9 % and 1.7 % by weight, respectively, and the quantity of
carbon particles on the surface was 31 % and 27 % by area, respectively. In addition,
the orientation plane of the silver matrix was (220) plane in Comparative Example
9 wherein electroplating was carried out at a current density of 1 A/dm
2, whereas the orientation plane of the silver matrix was (111) plane in Comparative
Example 10 wherein electroplating was carried out at a current density of 3 A/dm
2. Moreover, the substrate was not exposed after the reciprocating sliding movement
was repeated over 500,000 times in Comparative Example 9 wherein electroplating was
carried out at a current density of 1 A/dm
2, whereas the substrate was exposed after the reciprocating sliding movement was repeated
about 370,000 times in Comparative Example 10 wherein electroplating was carried out
at a current density of 3 A/dm
2.
[0044] The results in Examples 1 through 8 and Comparative Examples 1 through 10 are shown
in Tables 1 and 2.
Table 1
|
[Ag(CN)2] (g/L) |
KCN g/L) |
Ag/CN |
KSeCN (mg/L) |
Current Density (A/dm2) |
Ex.1 |
280 |
90 |
1.01 |
12 |
1 |
Ex.2 |
280 |
90 |
1.01 |
12 |
3 |
Ex.3 |
280 |
90 |
1.01 |
16 |
1 |
Ex.4 |
280 |
90 |
1.01 |
16 |
3 |
Ex.5 |
240 |
90 |
0.87 |
8 |
1 |
Ex.6 |
240 |
90 |
0.87 |
8 |
3 |
Ex.7 |
240 |
90 |
0.87 |
12 |
1 |
Ex.8 |
240 |
90 |
0.87 |
12 |
3 |
comp.1 |
100 |
120 |
0.27 |
4 |
1 |
comp.2 |
100 |
120 |
0.27 |
4 |
3 |
comp.3 |
100 |
120 |
0.27 |
8 |
1 |
comp.4 |
100 |
120 |
0.27 |
8 |
3 |
comp.5 |
185 |
90 |
0.67 |
4 |
1 |
comp.6 |
185 |
90 |
0.67 |
4 |
3 |
comp.7 |
185 |
90 |
0.67 |
12 |
1 |
comp.8 |
185 |
90 |
0.67 |
12 |
3 |
comp.9 |
280 |
90 |
1.01 |
4 |
1 |
comp.10 |
280 |
90 |
1.01 |
4 |
3 |
Table 2
|
Content of C (% by Weight) |
Quantity of Carbon Particles on Surface (% by area) |
Crystal Orientation |
Wear Resistance |
Ex.1 |
2.1 |
32 |
220 |
over 500,000 |
Ex.2 |
2.5 |
34 |
220 |
over 500,000 |
Ex.3 |
1.6 |
33 |
220 |
over 500,000 |
Ex.4 |
2.4 |
35 |
220 |
over 500,000 |
Ex.5 |
2.0 |
32 |
220 |
over 500,000 |
Ex.6 |
1.8 |
31 |
220 |
over 500,000 |
Ex.7 |
1.9 |
31 |
220 |
over 500,000 |
Ex.8 |
2.3 |
33 |
220 |
over 500,000 |
comp.1 |
2.2 |
34 |
220 |
over 500,000 |
comp.2 |
1.7 |
22 |
111 |
about 480,000 |
comp.3 |
2.0 |
27 |
220 |
over 500,000 |
comp.4 |
1.5 |
21 |
200 |
about 420,000 |
comp.5 |
1.8 |
33 |
220 |
about 480,000 |
comp.6 |
1.7 |
28 |
200 |
about 310,000 |
comp.7 |
1.8 |
31 |
220 |
over 500,000 |
comp.8 |
1.6 |
21 |
111 |
about 370,000 |
comp.9 |
1.9 |
31 |
220 |
over 500,000 |
comp.10 |
1.7 |
27 |
111 |
about 370,000 |