CA3058358C - Carbon material for catalyst carrier of polymer electrolyte fuel cell, and method of producing the same - Google Patents
Carbon material for catalyst carrier of polymer electrolyte fuel cell, and method of producing the same Download PDFInfo
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Abstract
Description
CARBON MATERIAL FOR CATALYST CARRIER OF POLYMER ELECTROLYTE
FUEL CELL, AND METHOD OF PRODUCING THE SAME
Technical Field [0001] The present invention relates to a carbon material for a catalyst carrier of a polymer electrolyte fuel cell and a method of producing the same.
Background Art
Meanwhile, as a catalyst metal, Pt or a Pt alloy, which can be used in a strongly acidic environment, and which exhibits high reactivity with respect to both the oxidation reaction and the reduction reaction, is mainly used. Further, with respect to the catalyst metal, since the oxidation reaction and the reduction reaction generally occur on the catalyst metal, in order to increase the utilization rate of the catalyst metal, it is necessary to increase the specific surface area with respect to mass. For this reason, particles having a size of about several nanometers are usually used as the catalyst metal.
Further, the porous carbon material is required to have a large mesopore volume (volume of mesopores with a pore diameter of from 2 to 50 nm), in order to support the catalyst metal in a state that is dispersed to the greatest extent possible. At the same time, when the catalyst layer to serve as the anode or the cathode is formed, it is necessary to diffuse the reactive gas supplied into the catalyst layer without resistance, and to discharge the water generated in the catalyst layer (produced water) without delay. For this purpose, it is necessary to form micropores in the catalyst layer that are suitable for diffusion of a reactive gas and discharge of produced water.
600 JD produced by Lion Corporation, and EC 300 produced by Lion Corporation have been used, for example. In addition, development of a porous carbon material having a more suitable specific surface area and mesopore volume, and also having a more suitable dendritic structure as a carbon material for a catalyst carrier has been attempted. As a porous carbon material that has been attracting particular attention in recent years, there is a dendritic carbon nanostructure that is produced from a metal acetylide, such as silver acetylide, having a three-dimensionally branched three-dimensional dendritic structure as an intermediate, and that maintains the three-dimensional dendritic structure. For a dendritic carbon nanostructure maintaining the three-dimensional dendritic structure, several proposals have been made so far.
Specifically, a porous carbon material prepared by a production method including the following steps has been proposed.
The method includes:
a step of preparing a solution containing a metal or a metal salt;
a step of blowing an acetylene gas into the solution to form a dendritic carbon nanostructure including a metal acetylide;
a step of heating the carbon nanostructure at from 60 to 80 C to form a metal-encapsulated dendritic carbon nanostructure in which a metal is encapsulated in the dendritic carbon nanostructure;
a step of heating the metal-encapsulated dendritic carbon nanostructure to from 160 to 200 C to eject the metal such that a dendritic mesoporous carbon structure is farmed; and a step of heating the mesoporous carbon structure to from 1600 to 2200 C in a reduced pressure atmosphere or in an inert gas atmosphere. The porous carbon material has a pore diameter of from 1 to 20 nm, and a cumulative pore volume of from 0.2 to 1.5 cc/g, which are obtained from a nitrogen adsorption isotherm analyzed by the Dollimore-Heal method, as well as a BET specific surface area of from 200 to 1300 m2/g.
The method includes:
an acetylide production step of forming a metal acetylide by blowing an acetylene gas into an aqueous ammonia solution containing a metal or a metal salt;
a first heat treatment step of heating the metal acetylide at from 60 to 80 C
to form a metal particle-encapsulated intermediate;
a second heat treatment step of heating the metal particle-encapsulated intermediate at from 120 to 200 C to make the metal particle-encapsulated intermediate eject the metal particles, thereby yielding a carbon material intermediate;
a washing treatment step of cleaning the carbon material intermediate by bringing the carbon material intermediate into contact with hot concentrated sulfuric acid;
and a third heat treatment step of heat-treating the cleaned carbon material intermediate at from 1000 to 2100 C to yield a carrier carbon material. The porous carbon material has a predetermined hydrogen content, a BET specific surface area of from 600 to 1500 m2/g, and a relative intensity ratio ID/JO, of the peak intensity ID of a D-band in a range of from 1200 to 1400 cm-1 to the peak intensity IG of a G¨band in a range of from 1500 to 1700 cm-1, obtained in a Raman spectrum, of from 1.0 to 2Ø
The method includes:
an acetylide production step of forming a metal acetylide by blowing an acetylene gas into an aqueous ammonia solution containing a metal or a metal salt;
a first heat treatment step of heating the metal acetylide at from 40 to 80 C
to form a metal particle-encapsulated intermediate;
a second heat treatment step of heating a compact formed by compressing the metal particle-encapsulated intermediate at a rate of temperature increase of 100 C
per minute or higher to 400 C or higher to make the metal particle-encapsulated intermediate eject the metal particles, thereby yielding a carbon material intermediate;
a washing treatment step of cleaning the carbon material intermediate by bringing the carbon material intermediate into contact with hot concentrated nitric acid, or hot concentrated sulfuric acid; and a third heat treatment step of heat-treating the cleaned carbon material intermediate at from 1400 to 2100 C in a vacuum or in an inert gas atmosphere to yield a carrier carbon material. The porous carbon material has the following characteristics.
The specific surface area SA of mesopores having a pore diameter of from 2 to 50 nm, which is obtained by analyzing a nitrogen adsorption isotherm of the adsorption process according to the Dollimore-Heal method, is from 600 and 1600 m2/g;
the relative intensity ratio IG./IG of the peak intensity IG of a G'-band in a range of from 2650 to 2700 cm-1 to the peak intensity IG of a G¨band in a range of from 1550 to 1650 cm-1, in a Raman spectrum, is from 0.8 to 2.2;
the specific pore surface area S2-io of a portion of mesopores having a pore diameter of from 2 nm to less than 10 nm is from 400 to 1100 m2/g, and the specific pore volume V2-10 is from 0.4 to 1.6 cc/g;
the specific pore surface area S10-50 of such a portion of mesopores having a pore diameter of from 10 nm to 50 nm is from 20 to 150 m2/g, and the specific pore volume V2-10 is from 0.4 to 1.6 cc/g; and the specific pore surface area S2 of pores having a pore diameter lower than 2 nm, which is deteimined by analyzing the nitrogen adsorption isotherm of the adsorption process by the Horvath-Kawazoe method, is from 250 to 550 m2/g.
The oxygen content OICP is from 0.1 to 3.0% by mass, the residual oxygen content 01200 C remaining after a heat treatment at 1200 C
in an inert gas atmosphere (or in a vacuum) is from 0.1 to 1.5% by mass, the BET specific surface area is from 300 to 1500 m2/g, the half-value width AG of the G band detected in a range of from 1550 to 1650 cnil of a Raman spectrum is from 30 to 70 cm-1, and the residual hydrogen content H1200 C remaining after a heat treatment at 1200 C in an inert gas atmosphere (or in a vacuum) is from 0.005 to 0.080% by mass.
Citation List Patent Document
Patent Document 1: WO 2014/129597 Al Patent Document 2: WO 2015/088025 Al Patent Document 3: WO 2015/141810 Al Patent Document 4: WO 2016/133132 Al SUMMARY OF INVENTION
Technical Problem
In a porous carbon material including such a dendritic carbon nanostructure having a three-dimensional dendritic structure, aggregation hardly occurs during a heat treatment at the time of preparation of a porous carbon material due to a large-sized dendritic structure.
Therefore, in general, it has been believed that a porous carbon material including dendritic carbon nanostructures having a three-dimensional dendritic structure is a porous carbon material whose power generation characteristics are ordinarily less susceptible to a negative influence of aggregation in forming a catalyst layer compared to porous carbon materials such as Ketjen black or acetylene black structured to have a high surface area.
Therefore, it was unexpected that some aggregation occurred in preparing a porous carbon material including dendritic carbon nanostructures having a three-dimensional dendritic structure.
As a result, regarding the quantitative examination of a graphitized material present in a porous carbon material, the following was found. Raman spectroscopic analysis was carried out using a laser Raman spectrophotometer combined with a microscope (microscopic laser Raman spectrophotometer). According to this Raman spectroscopic analysis, it became clear that "dispersion of Raman measurement values" appears in the relative intensity ratio ID/1G (R value) of the intensity of D-band (a peak appearing in the vicinity of 1360 cm-1, which is defined herein as a peak appearing in the range of from 1310 to 1410 cm-1; in the present disclosure, the description "intensity of D-band (near 1360 cm-1)" has the meaning corresponding to the above definition), measured under predetermined conditions, to the intensity of G-band (a peak appearing in the vicinity of 1580 cm-', which is defined herein as a peak appearing in the range of from 1530 to 1630 cm-1; in the present disclosure, the description "intensity of G-band (near 1580 cm')" has the meaning corresponding to the above definition), measured under predetermined conditions. As a result of an investigation focusing on the dispersion of Raman measurement values, it was found surprisingly that the standard deviation 8(R) of the R values had a close correlation with the presence of a graphitized material. From the above it has been known that a graphitized material present in a porous carbon material may be quantitatively rated using the standard deviation 8(R) of the R values.
values. By this means, micropores in the catalyst layer constituting the diffusion rate-determining step for oxygen and water vapor, may be optimized so as to improve the diffusion of oxygen and water vapor in the catalyst layer without sacrificing the power generation characteristics other than the high current characteristics and the durability required for a catalyst layer. By doing so, the output voltage at high current may be enhanced. The above has been found.
Another object of the present disclosure is to provide a method of producing a carbon material for a catalyst carrier, which is useful for producing a catalyst of this kind of polymer electrolyte fuel cell.
Solution to Problem
[1] A carbon material for a catalyst carrier of a polymer electrolyte fuel cell, which is a porous carbon material with a three-dimensionally branched three-dimensional dendritic structure, and satisfies the following (A), (B), and (C) at the same time:
(A) By a Raman spectroscopic analysis in which a laser beam with a wavelength of 532 nm is used as excitation light, the circular beam diameter for irradiating a sample is 1 gm, and optional 50 measurement points are measured with respect to the same sample, the obtained standard deviation 6(R) of an relative intensity ratio ID/IG (R value) of the intensity of D-band (near 1360 cm-1) to the intensity of G-band (near 1580 cm-1) is from 0.01 to 0.07, (B) a BET specific surface area SBET obtained by a BET analysis of a nitrogen gas adsorption isotherm is from 400 to 1520 m2/g, and (C) the nitrogen gas adsorption amount VNØ4-0 8 adsorbed during the relative pressure (p/po) from 0.4 to 0.8 in the nitrogen gas adsorption isotherm is from 100 to 300 cc(STP)/g.
[2] The carbon material for a catalyst carrier of a polymer electrolyte fuel cell according to [1] above, wherein the standard deviation 6(AG) of the full width at half maximum AG of a G-band (near 1580 cm-1) in the Raman spectroscopic analysis of (A) above is from 0.10 to 1.30.
[3] The carbon material for a catalyst carrier of a polymer electrolyte fuel cell according to [1] or [2] above, wherein the average value Rave of the measured R values in the Raman spectroscopic analysis of (A) above is from 1.3 to 1.85.
[4] The carbon material for a catalyst carrier of a polymer electrolyte fuel cell according to [2] above, wherein the average value AGave of the measured AG values in the Raman spectroscopic analysis of (A) above is from 45 to 75 cm-1.
[5] A method of producing a carbon material for a catalyst carrier of a polymer electrolyte fuel cell, the method including:
producing an acetylide by blowing an acetylene gas into a reaction solution including an aqueous ammonia solution of silver nitrate, to synthesize silver acetylide, a first heat treatment of heat-treating the silver acetylide at a temperature of from 40 to 80 C to prepare a silver particle-encapsulated intermediate;
a second heat treatment of causing a self-decomposing and explosive reaction of the silver particle-encapsulated intermediate at a temperature of from 120 to 200 C to yield a decomposition product, an oxidation treatment of heat-treating the decomposition product in an oxygen-containing atmosphere with an oxygen content of from 1 to 25% % by volume at from 80 to 150 C for from 10 min to 100 min to obtain the decomposition product which has been subjected to an oxidation treatment and freed from nonaromatic carbon by combustion of an oxygen-containing gas, a washing to removing silver from the decomposition product after the oxidation treatment to yield a carbon material intermediate, and a third heat treatment of heat-treating the carbon material intermediate in a vacuum, or an inert gas atmosphere at a temperature of from 1600 to 2300 C to yield a carbon material for a catalyst carrier.
Advantageous Effects of Invention
Further, by a producing method of the present disclosure, a carbon material for a catalyst carrier suitable for producing a catalyst of a polymer electrolyte fuel cell having improved high current (heavy-load) characteristics to exhibit a high output voltage at a high current, while maintaining the durability, may be produced.
BRIEF DESCRIPTION OF DRAWINGS
[Figure 1] Figure 1 is a graph chart having plotted the R values and AG values measured at 50 measurement points for the carbon material for a catalyst carrier of Experimental Example 5 on an R value vs. AG value graph.
[Figure 2] Figure 2 is a graph chart having plotted the R values and AG values measured at 50 measurement points for the carbon material for a catalyst carrier of Experimental Example 19 on an R value vs. AG value graph.
[Figure 3] Figure 3 is a graph chart having plotted the R values and AG values measured at 50 measurement points for the carbon material for a catalyst carrier of Experimental Example 22 on an R value vs. AG value graph.
[Figure 4] Figure 4 is a graph chart having plotted the R values and AG values measured at 50 measurement points for the carbon material for a catalyst carrier of Experimental Example 8 on an R value vs. AG value graph.
[Figure 5] Figure 5 is a graph chart having plotted the R values and AG values measured at 50 measurement points for the carbon material for a catalyst carrier of Experimental Example 13 on an R value vs. AG value graph.
[Figure 6] Figure 6 is a graph chart showing the Raman spectrum obtained by a Raman spectroscopic analysis on the porous carbon material of Experimental Example 5.
[Figure 7] Figure 7 is a graph chart showing the Raman spectrum obtained by a Raman spectroscopic analysis on the porous carbon material of Experimental Example 29.
[Figure 8] Figure 8 is a graph chart showing the Raman spectrum obtained by a Raman spectroscopic analysis on the porous carbon material of Experimental Example 33.
[Figure 9] Figure 9 is a photograph showing the measurement method of measuring a branch diameter, when a carbon material for a catalyst carrier of the present disclosure was observed with SEM.
[Figure 10] Figure 10 is an explanatory diagram showing the method of measuring a branch diameter of a carbon material for a catalyst carrier of the present disclosure.
DESCRIPTION OF EMBODIMENTS
A carbon material for a catalyst carrier of a polymer electrolyte fuel cell of the present disclosure is a porous carbon material which has a three-dimensionally branched three-dimensional dendritic structure, and satisfies the following (A), (B), and (C) at the same time:
(A) By a Raman spectroscopic analysis in which a laser beam with a wavelength of 532 nm is used as excitation light, the circular beam diameter for irradiating a sample is 1 ttm, and optional 50 measurement points are measured with respect to the same sample, the obtained standard deviation 8(R) of an intensity ratio 'DUG (R value) of the intensity of D-band (near 1360 cm) to the intensity of G-band (near 1580 cm1) is from 0.01 to 0.07, (B) a BET specific surface area SBET obtained by a BET analysis of a nitrogen gas adsorption isotherm is from 400 to 1520 m2/g, and (C) the nitrogen gas adsorption amount VN 0 4-0 8 adsorbed during the relative pressure (p/po) from 0.4 to 0.8 in the nitrogen gas adsorption isotherm is from 100 to 300 cc(STP)/g.
In this regard, the unit of a nitrogen gas adsorption amount is cc(STP)/g, the unit of a BET specific surface area SBET is m2/g, and the unit of the average value AGave of AG values is cm-1.
The porous carbon material with a three-dimensionally branched three-dimensional dendritic structure is preferably including dendritic carbon nanostructures.
Specifically, the dendritic carbon nanostructure is yielded from a silver acetylide having a three-dimensional dendritic structure as an intermediate. With respect to the carbon material for a catalyst carrier, the BET specific surface area SBET is from 400 m2/g to 1,520 m2/g, preferably from 400 m2/g to 1,500 m2/g, and more preferably from 500 m2/g to 1,400 m2/g. When the BET
specific surface area SBET is less than 400 m2/g, there is a risk that it becomes difficult to support catalyst metal fine particles at a high density in the pores. Meanwhile, when it is allowed to exceed 1,520 m2/g, the durability tends to be lowered as the crystallinity decreases substantially.
Conversely, when the standard deviation 6(R) of the R values exceeds 0.07, the content of a graphitized product increases. In addition, the particle size of the graphitized product also becomes relatively large. As a result, in a catalyst layer using such a carbon material as the catalyst carrier, a large number of aggregates appear in the layer, and therefore the high current characteristics may deteriorate. The reason why 50 measurement points was selected as the number of measurement points in a Raman spectroscopic analysis was because the number of measurement points was judged as an adequate number for detecting a graphitized material based on the result of the statistical processing of the "dispersion of Raman measurement values" in a Raman spectroscopic analysis.
values is preferably from 1.3 to 1.85. It is more preferably from 1.3 to 1.8.
Further, from the viewpoints of improvement of the crystallinity and improvement of the durability, the average value AGave of the measured AG values is preferably from 45 cm' to 75 cm-1, more preferably from 55 cm-I to 65 cm'.
For the standard deviation S(AG), the substantial minimum value is 0.10, but in the present disclosure, there is no particular restriction on the lower limit of the standard deviation 6(AG). On the contrary, when the standard deviation 6(AG) of the full width at half maximum AG exceeds 1.30, the pores in the catalyst layer collapse for the above-mentioned reason, so that the high current characteristics may be deteriorated.
When the average value Rave is less than 1.3, the crystallinity becomes too high and the ruggedness of the pore walls decreases, and the adsorbability of the catalyst metal fine particles to the pore walls may decrease. On the contrary, when it exceeds 1.85, the crystallinity is too low, and the durability may decrease. Meanwhile, the AG
value is also an index representing crystallinity similarly to the R value. Therefore, when the average value AGave is less than 45 cm-1, the crystallinity becomes too high and the ruggedness of the pore walls decreases, and the adsorbability of the catalyst metal fine particles to the pore walls may decrease. On the contrary, when AGave exceeds 75 cm-I, the crystallinity is too low and the durability may decrease.
When the nitrogen gas adsorption amount VN:0.4-0.8 is less than 100 cc(STP)/g, the pore volume of meso-size pores supporting catalyst metal fine particles becomes small, and there arises a risk that the gas diffusibility in micropores to be formed in a catalyst layer also decreases to increase the reaction resistance. On the contrary, when it exceeds 300 cc(STP)/g, the carbon wall forming the pores becomes too thin, and the mechanical strength of the material may be impaired to cause material destruction at an electrode producing step.
For this purpose, in addition to the production method heretofore generally adopted, an oxidation treatment step is applied in which a decomposition product is heat-treated in an oxygen-containing atmosphere 80 C or more and 150 C or less (preferably 85 C
or more and 145C or less) before silver is removed from the decomposition product, so as to remove nonaromatic carbon from the decomposition product to the extent possible.
Further, from the viewpoint of removing as selectively as possible nonaromatic carbon which is easily combustible compared to aromatic carbon, the oxygen content in the oxygen-containing atmosphere is preferably from 1% by volume to 25% by volume (preferably from 2% by volume to 23% by volume). Further, the treatment time of the oxidation treatment is from min to 100 mm (preferably from 10 min to 90 min), When the treatment temperature during the oxidation treatment is lower than 80 C, oxidation of nonaromatic carbon may become incomplete and a graphitized product may be formed. On the contrary, when the temperature exceeds 150 C, there is a possibility that aromatic carbon which should remain is lost by combustion. Regarding the oxygen content in the oxygen-containing atmosphere, when it is less than 1% by volume, oxidation of nonaromatic carbon may become incomplete, and a graphitized product may be formed. On the contrary, when it exceeds 30%
by volume, aromatic carbon which should remain may be lost by combustion. Furthermore, when it is attempted to shorten the treatment time below 10 min, exposure to a stronger oxidizing condition becomes necessary, and not only nonaromatic carbon but also aromatic carbon may be oxidized and consumed. On the contrary, if it exceeds 100 mm, the productivity may decrease and the production cost may be increased.
That is, a carbon material for a catalyst carrier of the present disclosure may be obtained by a producing method having the following steps.
An (acetylide producing step) where an acetylene gas is blown into a reaction solution incliding an ammoniac aqueous solution of silver nitrate to synthesize silver acetylide;
a (first heat treatment step) where the obtained silver acetylide is heat-treated at a temperature of from 40 to 80 C to prepare a silver particle-encapsulated intermediate;
a (second heat treatment step) where the silver particle-encapsulated intermediate is made to undergo a self-decomposing and explosive reaction at a temperature of from 120 to 200 C, and the decomposition product is recovered;
an (oxidation treatment step) where the recovered decomposition product is heat-treated in an oxygen-containing atmosphere with an oxygen content of from 1 to 25% by volume at from 80 to 150 C for from 10 min to 100 mm to remove nonaromatic carbon by a heat treatment due to combustion of an oxygen-containing gas;
a (washing step) where the carbon material intermediate is recovered by removing silver from the decomposition product after the oxidation treatment;
and a (third heat treatment step) where the recovered carbon material Intermediate is heat-treated in a vacuum or an inert gas atmosphere at a temperature of from 1600 to 2300 C.
Further, it is not only equivalent or superior to the conventional porous carbon materials of this type in terms of the BET specific surface area, and the durability, but also it is freed from a highly crystalline graphitized material having a relatively large aggregated structure to the extent possible. Consequently, in a catalyst layer prepared using a porous carbon material of the present disclosure as the catalyst carrier, a reactive gas may be diffused without resistance.
Further, micropores suitable for discharging water generated in the catalyst layer (generated water) without delay are formed. As a result, the high current (heavy-load) characteristics of a polymer electrolyte fuel cell may be remarkably improved (in other words, the output voltage at the time of high current may be significantly increased).
Examples
The measurements of the BET specific surface area SBET, nitrogen gas adsorption amount VN:0.4-0.8, standard deviation 6(R) of the R values, average value Rave of the R values, standard deviation 6(AG) of AG values, and average value AGave of the AG
values of carbon materials for a catalyst carrier prepared in the following Experimental Examples were respectively conducted as follows.
Approximately 30 mg of the carbon material for a catalyst carrier produced or prepared in each of the Experimental Examples was weighed and dried in a vacuum at 120 C
for 2 hours. Thereafter, nitrogen gas adsorption isotherm was measured using an automatic specific surface area measuring device (BELSORP-MAX, manufactured by MicrotracBEL
Corp.) using a nitrogen gas as an adsorbate. The BET specific surface area was calculated by carrying out a BET analysis in the p/po range of from 0.05 to 0.15 of an adsorption isotherm.
Also, the difference between the adsorption amount cc(STP)/g when the p/po of the adsorption isotherm was 0.8, and the adsorption amount cc(STP)/g when the p/po was 0.4 was calculated, and used as the value of VN:0.4-0.8.
Values, and Standard Deviation 6(AG) and Average Value AGav, of AG Values in Raman Spectroscopic Analysis]
Approximately 3 mg of samples of the carbon material for a catalyst carrier produced or prepared in each of the Experimental Examples was weighed out. The sample was mounted on a laser Raman spectrophotometer (model NRS-3100 manufactured by Jasco Corporation), and a measurement was carried out under measurement conditions:
excitation laser: 532 nm, laser power: 10 mW (sample irradiation power: 1.1 mW), microscope arrangement: backscattering, slit: 100 gm x 100 gm, objective lens: 100x, spot diameter: 1 gm, exposure time: 30 sec, observation wavenumber: from 2000 to 300 cm-1, and cumulative number: 6. From each of the obtained 6 spectra, the intensity (peak height) and the full width at half maximum AG of the G-band (near 1580 cm-1) were determined.
Further, the intensity (peak height) of the D-band (near 1360 cm-I), and the R value (relative intensity ratio ID/IG) were determined. In this regard, with respect to the same set sample, optional 50 measurement points were measured changing laser irradiation positions. With respect to the data obtained from the 50 measurement points, the standard deviations were calculated to find the standard deviation 6(R) of R values, and the standard deviation 6(AG) of AG values, as well as the average value Rave of R values and the average value AGme of AG
values.
(1) Silver Acetylide Producing Step Ammonia was added to an aqueous solution of silver nitrate adjusted to a concentration of 5% by mass such that ammonia becomes 8 times as much as silver nitrate in terms of molar ratio to prepare an ammoniac aqueous solution of silver nitrate. Then, firstly a nitrogen gas was blown therein for 40 to 60 min. Thereby, the dissolved oxygen was replaced with the inert gas to eliminate the risk of explosive decomposition of the silver acetylide produced in the silver acetylide producing step.
Next, an acetylene gas was blown into the ammoniac aqueous solution of silver nitrate prepared in this way at room temperature for about 10 min. When the acetylene gas began to emit as bubbles from the reaction solution, the acetylene gas blow was discontinued.
When silver nitrate and acetylene in the reaction solution were allowed to react further, a white precipitate of silver acetylide was formed.
The formed precipitate of silver acetylide was recovered by filtration through a membrane filter. The recovered precipitate was redispersed in methanol and filtrated again, and the collected precipitate was transferred into a petri dish,
(2) First Heat Treatment Step Approximately 0.5 g of silver acetylide yielded in the above silver acetylide producing step of each Experimental Example in a state impregnated with methanol was placed as it was in a stainless steel cylindrical container with a diameter of 5 cm. This was then placed in a vacuum electric heating furnace and dried in a vacuum at 60 C
for about from 15 to 30 mm to prepare a silver particle-encapsulated intermediate derived from silver acetylide of each of Experimental Example.
(3) Second Heat Treatment Step Next, the 60 C silver particle-encapsulated intermediate obtained in the first heat treatment step immediately after the vacuum drying was directly, without taking out from the vacuum electric heating furnace, heated to a temperature of 200 C. In the course of the heating, a self-decomposing and explosive reaction of silver acetylide was induced to prepare a carbon material intermediate including a composite of silver and carbon.
In the course of this self-decomposing and explosive reaction, silver nano-sized particles (silver nanoparticles) are formed. At the same time, a carbon layer with a hexagonal layer plane is formed surrounding such a silver nanoparticle to form skeleton with a three-dimensional dendritic structure. Furthermore, the produced silver nanoparticles are made porous by explosion energy and erupted outward through pores in the carbon layer to form silver aggregates (silver particles).
(4) Oxidation Treatment Step The decomposition product composing of a composite of silver and carbon obtained in the second heat treatment step was placed in an oxidation treatment container. Then, an oxygen-mixed nitrogen gas obtained by adding an oxygen gas in a nitrogen gas to the oxygen content shown in Table 1 was circulated through the oxidation treatment container. While circulating the oxygen mixed nitrogen gas through the oxidation treatment container, the temperature was raised at an elevation rate of 10C/min up to the temperature shown in Table 1.
The system was held at the temperature shown in Table 1 for the treatment time shown in Table 1 for performing the oxidation treatment of the decomposition product.
(5) Washing Treatment Step For the decomposition product after the oxidation treatment composed of a composite of silver and carbon obtained in the oxidation treatment step, a dissolution treatment (washing treatment) on silver was carried out at 60 C with concentrated nitric acid having a concentration of 30% by mass. By this way, silver particles and other unstable carbon compounds present on the surface of the carbon material intermediate were removed to obtain a cleaned carbon material intermediate.
In Experimental Examples 21, 22, and 23, the washing time in the washing treatment step was set respectively at 3 hours, 5 hours, and 10 hours for the same material obtained in the oxidation treatment step, while the heat treatment temperature in the third heat treatment step was 2000 C.
(6) Third Heat Treatment Step The carbon material intermediate cleaned in the washing treatment step was heat-treated in an inert gas atmosphere at the heating temperature set forth in Table 1 for 2 hours to yield a carbon material for a catalyst carrier of each of Experimental Examples.
The heat treatment temperature in the third heat treatment step was a temperature heretofore generally adopted for the control of crystallinity. Further, it was examined what influence the heat treatment temperature during the third heat treatment would exert on the physical properties and the battery characteristics of a porous carbon material originated from the decomposition product after the oxidation treatment obtained in each Experimental Example.
The results are shown in Table 2.
Further, with respect to each of carbon materials for a catalyst carrier obtained in Experimental Examples 5, 19, and 22, as well as Experimental Examples 8 and 13, the R
values and the AG values measured at 50 measurement points were plotted on a graph of R
value vs. AG value with the X axis for R values and the Y axis for AG values to obtain a dispersed relationship between these values. The results are shown in Figures 1 to 5.
In addition, commercially available carbon materials were also examined in Experimental Examples 27 to 34.
As porous carbon materials, a porous carbon material A (KETJENBLACK EC300, produced by Lion Specialty Chemicals Co., Ltd.) (Experimental Example 27), and a porous carbon material B (KETJENBLACK EC600JD, produced by Lion Specialty Chemicals Co., Ltd.) (Experimental Examples 28 to 31), each having a dendritic structure with well-developed pores, and a large specific surface area; were used; as a typical porous carbon material not having a dendritic structure, a porous carbon material C (CNOVEL-MH, produced by Toyo Carbon Co., Ltd.) (Experimental Example 32) was used; and as carbon materials having a well-developed dendritic structure, but not having a porous structure, a carbon material D (acetylene black (AB), produced by Denka Co., Ltd.) (Experimental Example 33), and a carbon material E (conductive grade #4300, produced by Tokai Carbon Co., Ltd.) (Experimental Example 34), were used. With respect to the porous carbon material B, four types were prepared based on the temperature at the third heat treatment, namely the porous carbon material B-1 treated at 1400 C, the porous carbon material B-2 treated at 1700 C, the porous carbon material B-3 treated at 2000 C, and the porous carbon material B-4 treated at 2100 C.
values, standard deviation 8(AG) of AG values, and average value AGave of AG values were measured.
The results are shown in Table 2.
Further, an example of the Raman spectra obtained in Raman spectroscopic analysis with respect to a porous carbon material obtained in each of Experimental Example 5, Experimental Example 29, and Experimental Example 33 is shown in one of Figures 6 to 8.
In this regard, in Figure 6 the assignment of peaks of D-band and G-band is shown.
Next, using each of the thus produced or prepared carbon materials for a catalyst carrier, catalysts for a polymer electrolyte fuel cell, on which a catalyst metal was supported, were prepared as described below. Further, using an obtained catalyst, an ink solution for a catalyst layer was prepared. Next, using the ink solution for a catalyst layer, a catalyst layer was formed. Further, using the formed catalyst layer a membrane electrode assembly (MEA) was produced, and the produced MEA was fitted into a fuel cell, and a power generation test was performed using a fuel cell measuring device. Preparation of each component and cell evaluation by a power generation test will be described in detail below.
(1) Preparation of Catalyst for Polymer Electrolyte Fuel Cell (Carbon Material Supporting Platinum) Each of carbon materials for a catalyst carrier prepared as above, or commercially available carbon materials, was dispersed in distilled water. Formaldehyde was added to the dispersion, the dispersion was placed in a water bath set at 40 C, and when the temperature of the dispersion reached the water bath temperature of 40 C, an aqueous nitric acid solution of a dinitrodiamine Pt complex was slowly poured into the dispersion with stirring.
Then, stirring was continued for about 2 hours, the dispersion was filtrated, and the obtained solid was washed. The solid obtained in this way was dried in a vacuum at 90 C, then pulverized in a mortar. Next, the solid was heat-treated at 200 C in an argon atmosphere containing 5%
by volume of hydrogen for 1 hour to yield a carbon material supporting platinum catalyst particles.
The supported platinum amount of the carbon material supporting platinum was regulated to 40% by mass with respect to the total mass of the carbon material for a catalyst carrier and the platinum particles, which was confirmed by a measurement based on inductively coupled plasma-atomic emission spectrometry (ICP-AES).
(2) Preparation of Catalyst Layer The carbon material supporting platinum (Pt catalyst) prepared as above was used.
Further, Nation (registered tradename) (produced by DuPont Co., Ltd., persulfonic acid-based ion exchange resin) was used as an electrolyte resin. The Pt catalyst and the Nation were mixed in an Ar atmosphere, such that the mass of the Nafion solid component is 1.0 times as much as the mass of the carbon material supporting platinum catalyst particles, and 0.5 times as much as non-porous carbon. After stirring gently, the Pt catalyst was crushed by ultrasonic waves. The total solid concentration of the Pt catalyst and the electrolyte resin was adjusted to 1.0% by mass of by adding ethanol, thereby completing a catalyst layer ink solution in which the Pt catalyst and the electrolyte resin were mixed.
Then, a drying treatment was carried out in argon at 120 C for 60 min to complete a catalyst layer.
(3) Preparation of MEA
An MEA (membrane electrode assembly) was produced by the following method using the catalyst layer prepared as above.
A square electrolyte membrane of 6 cm on a side was cut out from a Nation membrane (NR 211 produced by DuPont Co., Ltd.). Each of the anode or cathode catalyst layer coated on a Teflon (registered tradename) sheet was cut out with a cutter knife into a square of 2.5 cm on a side.
Between the anode catalyst layer and the cathode catalyst layer cut out as above, the electrolyte membrane was inserted such that the two catalyst layers sandwich the central part of the electrolyte membrane. Then, the electrolyte membrane was inserted tightly in contact with the catalyst layers without misalignment between the electrolyte membrane and the catalyst layers, and the laminate was pressed at 120 C under a pressure of 100 kg/cm2 for 10 mm. After cooling down to room temperature, only the Teflon (registered tradename) sheets were peeled off carefully from the respective catalyst layers of the anode and the cathode to compete an assembly of the catalyst layers and the electrolyte membrane, in which the respective catalyst layers of the anode and the cathode are fixed to the electrolyte membrane.
The basis weights of the catalyst metal component, the carbon material, and the electrolyte material in each of the produced MEA were calculated based on the mass of a catalyst layer fixed to the Nafion membrane (electrolyte membrane) found from the difference between the mass of the Teflon (registered tradename) sheet with the catalyst layer before pressing and the mass of the peeled Teflon (registered tradename) sheet after pressing, and the mass ratio of the components in the catalyst layer.
(4) Evaluation of Performance of Fuel Cell [Evaluation of High Current Characteristics]
An MEA produced using the carbon material for a catalyst carrier produced or prepared in each Experimental Example was fitted into a cell, which was then set on a fuel cell measuring apparatus, and the performance of the fuel cell was evaluated by the following procedure.
With respect to the reactive gases, on the cathode side air was supplied, and on the anode side pure hydrogen was supplied at a back pressure of 0.04 MPa by regulating the pressure with a back pressure regulating valve placed downstream of the cell so that the respective utilization rates became 40% and 70%. Meanwhile, the cell temperature was set at 80 C, and the supplied reactive gases on both the cathode and anode sides were bubbled through distilled water kept at 60 C in a humidifier, and the power generation in a low humidification state was evaluated.
The results are shown in Table 1.
(Acceptable Ranks) A: The output voltage at 1000 mA/cm2 is not less than 0.65 V.
B: The output voltage at 1000 mA/cm2 is not less than 0.60 V and less than 0.65 V.
(Rejected Rank) C: The output voltage is inferior to B.
[Evaluation of Durability]
In the cell, the anode was kept as it was (pure hydrogen with a gas utilization rate of 40% was supplied after bubbling humidification through distilled water kept at 60 C in a humidifier). On the other hand, an argon gas under the same humidification condition as above (bubbling through distilled water kept at 60 C in a humidifier) was fed to the cathode.
While maintaining these conditions, a cycle in which an operation of holding the cell voltage at 1.0 V for 4 sec, and then an operation of holding the cell voltage at 1.3 V
for 4 sec were performed in series (repetitive operation of rectangular pulse-like voltage profile), was repeated 400 times as a repetitive operation of the rectangular pulse-like voltage variation.
Thereafter the durability test was performed by examining the battery performance in the same manner as the evaluation of the high current characteristics described above. The durability was rated according to following criteria by which A and B were acceptable ranks, and C was a rejected rank. The results are shown in Table 1.
(Acceptable Ranks) A: The decay rate of the output voltage at 1000 mA/cm2 is not more than 10%.
B: The decay rate of the output voltage at 1000 mA/cm2 is more than 10% and less than 15%.
(Rejected Rank) C: Inferior to the acceptable rank B. Namely, the decay rate of the output voltage is not less than 15%.
[Table 1]
Oxidation treatment step Temperature Ex Oxygen Treatment of 3rd heat periment Temperature treatment Remarks symbol content time (% by ( C) (min) ( C) volume) Experimental Example I Ml - - 2000 , N
Experimental Example 2 M2 60 20 30 2000 N
Experimental Example 3 M3 70 20 30 2000 N
Experimental Example 4 M4 80 20 30 2000 G
Experimental Example 5 M5 100 20 30 2000 G
Experimental Example 6 M6 120 20 30 2000 G
Experimental Example 7 M7 140 20 30 2000 G
Experimental Example 8 M8 160 20 30 2000 N
Experimental Example 9 M9 100 20 5 2000 N
Experimental Example 10 M10 100 20 10 2000 G
Experimental Example 11 M11 100 20 60 2000 G
Experimental Example 12 M12 100 20 100 2000 G
Experimental Example 13 M13 100 20 120 2000 N
Experimental Example 14 M14 140 2 80 2000 G
Experimental Example 15 MI5 140 2 100 2000 G
Experimental Example 16 M16 140 2 120 2000 N
Experimental Example 17 M17 70 30 5 2000 N
Experimental Example 18 MI8 80 30 5 2000 N
Experimental Example 19 M19 110 5 80 2000 G
Experimental Example 20 M20 110 5 100 2000 G
Experimental Example 21 M21 100 15 25 2000 G
Experimental Example 22 M22 100 15 25 2000 G
Experimental Example 23 M23 100 15 25 2000 G
Experimental Example 24 M24 100 15 25 1600 G
Experimental Example 25 M25 100 15 25 1800 G
Experimental Example 26 M26 100 15 25 2200 G
Experimental Example 27 Porous carbon material A 1800 N
Experimental Example 28 Porous carbon material B-1 1400 N
Experimental Example 29 Porous carbon material B-2 1700 N
Experimental Example 30 Porous carbon material B-3 2000 N
Experimental Example 31 Porous carbon material B-4 2100 N
Experimental Example 32 Porous carbon material C 1800 N
Experimental Example 33 Carbon material D - N
Experimental Example 34 Carbon material E - N
[Table 2]
Carbon material for a catalyst carrier Power generation performance Experiment Remarks SBET AVN o 4-o s 43(R) 8(AG) R.,,, AG.,,, Power generation symbol Durability characteristics at (m2/g) cc(STP)/g ' (cm-1) (cm-1) (cm-1) (cm') 1000 mA/cm2 Experimental Example 1 M1 1090 105 0.14 1.82 1.6 57 C B N
Experimental Example 2 M2 - 1130 110 0.14 1.61 1.65 58 C B N
Experimental Example 3 M3 1140 115 0.14 1.63 1.7 60 C B N
Experimental Example 4 M4 1150 145 0.07 1.28 1.75 61 A B G
P
Experimental Example 5 M5 1160 135 0.06 0.97 1.69 60 A B G .
Experimental Example 6 M6 1010 130 0.04 0.93 1.6 57 A B G ' L, t\.) cs Experimental Example 7 M7 970 125 0.04 0.91 1.55 55 A B G N, H
tt, , Experimental Example 8 M8 890 90 0.09 1.89 1.66 56 C B N .
N, , Experimental Example 9 M9 1080 105 0.11 2.02 1.61 57 C B N
Experimental Example 10 M 10 1100 125 0.07 1.08 1.6 60 B B G
Experimental Example 11 MI1 1150 135 0.06 1.11 1.65 61 A B G
Experimental Example 12 M12 1160 125 0.06 1.37 1.65 60 B B G
Experimental Example 13 M13 1170 90 0.09 2.4 1.5 57 C B N
, Experimental Example 14 M14 1120 150 0.05 1.12 1.65 61 A B G
Experimental Example 15 M15 1020 155 0.06 1.14 1.85 67 A B G
Experimental Example 16 M16 940 95 0.17 1.37 1.85 72 C B N
_, Carbon material for a catalyst carrier Power generation performance Experiment Remarks SBET AVN 04-08 i5(R) i5(AG) Rave AGave Power generation symbol characteristics at Durability (m2/g) cc(STP)/g (cm') (cm-1) (cm-1) (c111-1) 1000 inA/cm2 Experimental Example 17 M17 980 95 0.17 1.48 1.45 64 C B N
Experimental Example 18 M18 960 95 0.16 1.47 1.5 62 C B N
Experimental Example 19 M19 1120 130 0.05 1 1.66 59 A B G
Experimental Example 20 M20 1170 135 0.05 0.79 1.65 58 A B G
Experimental Example 21 M21 1180 185 0.04 0.8 1.65 62 A A G
Experimental Example 22 M22 1190 195 0.04 0.64 1.7 61 A A G
Experimental Example 23 M23 1210 205 0.02 0.62 1.45 62 A A G P
L, Experimental Example 24 M24 1520 295 0.02 0.21 1.35 74 A B G
L, t_) Experimental Example 25 M25 1320 245 0.03 0.42 1.7 66 A B G
--.1 .
H
tt, Experimental Example 26 M26 910 145 0.05 0.79 1.6 53 A A G ,..
Experimental Example 27 Porous carbon material A
525 105 0.12 1.42 0.95 39 C B N ..., Experimental Example 28 Porous carbon material B-1 1200 382 0.11 1.43 1.62 66 B C N
Experimental Example 29 Porous carbon material B-2 580 215 0.11 1.43 0.78 40 B C N
Experimental Example 30 Porous carbon material B-3 360 126 0.11 1.42 0.75 39 C C N
Experimental Example 31 Porous carbon material B-4 290 107 0.11 1.43 0.72 38 C C N
Experimental Example 32 Porous carbon material C
1280 280 0.16 1.54 1.06 56 C C N
Experimental Example 33 Carbon material D 68 310 0.13 0.39 1.04 68 C A N
Experimental Example 34 Carbon material E 35 12 0.12 0.62 0.97 125 C A N
,
Claims (5)
(A) by a Raman spectroscopic analysis in which a laser beam with a wavelength of 532 nm is used as excitation light, a circular beam diameter for irradiating a sample is 1 pm, and 50 arbitrary measurement points are measured with respect to the same sample, an obtained standard deviation 6(R) of a relative intensity ratio ID/IG or R
value of an intensity of a D-band near 1360 cni1 to an intensity of a G-band near 1580 cm-1, is from 0.01 to 0.07, (B) a BET specific surface area SBET obtained by a BET analysis of a nitrogen gas adsorption isotherm, is from 400 to 1520 m2/g, and (C) a nitrogen gas adsorption amount VN:0.4-0.8 adsorbed during a relative pressure p/po from 0.4 to 0.8 in the nitrogen gas adsorption isotherm, is from 100 to cc(STP)/g.
producing an acetylide by blowing an acetylene gas into a reaction solution comprising an aqueous ammonia solution of silver nitrate to synthesize silver acetylide, a first heat treatment of heat-treating the silver acetylide at a temperature of from 40 to 80 C to prepare a silver particle-encapsulated intermediate, a second heat treatment of causing a self-decomposing and explosive reaction of the silver particle-encapsulated intermediate at a temperature of from 120 to 200 C to yield a decomposition product, an oxidation treatment of heat-treating the decomposition product in an oxygen-containing atmosphere with an oxygen content of from 1 to 25% by volume at from 80 to 150 C for from 10 min to 100 min to obtain the decomposition product which has been subjected to the oxidation treatment and freed from nonaromatic carbon by combustion of an oxygen-containing gas, washing to remove silver from the decomposition product after the oxidation treatment to yield a carbon material intermediate, and a third heat treatment of heat-treating the carbon material intermediate in a vacuum or an inert gas atmosphere at a temperature of from 1600 to 2300 C to yield the carbon material for the catalyst carrier.
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