Metal sheet for separators of polymer electrolyte fuel cells, and metal sheet for manufacturing the same

10516174 ยท 2019-12-24

Assignee

Inventors

Cpc classification

International classification

Abstract

A metal sheet for separators of polymer electrolyte fuel cells comprises: a substrate made of metal; and a surface-coating layer with which a surface of the substrate is coated, with a strike layer in between, wherein a coating ratio of the strike layer on the substrate is 2% to 70%, the strike layer is distributed in a form of islands, and a maximum diameter of the islands of the strike layer as coating portions is 1.00 m or less and is not greater than a thickness of the surface-coating layer.

Claims

1. A metal sheet for separators of polymer electrolyte fuel cells, comprising: a substrate made of metal; and a surface-coating layer with which a surface of the substrate is coated, with a strike layer in between, wherein a coating ratio of the strike layer on the substrate is 2% to 70%, the strike layer is distributed in a form of islands, a maximum diameter of the islands of the strike layer as coating portions is 1.00 m or less and is not greater than a thickness of the surface-coating layer, the surface-coating layer is formed on a surface of the strike layer, and is made of a metal layer of Au, a metal oxide layer, a metal nitride layer, a metal carbide layer, a carbon material layer, a conductive polymer layer, an organic resin layer containing a conductive substance, or a mixed layer thereof, and the strike layer contains at least one element selected from the group consisting of Ni, Cu, and Ag.

2. The metal sheet for separators of polymer electrolyte fuel cells according to claim 1, wherein the strike layer is made of an alloy layer of Ni and P, and has a P content in a range of 5 mass % to 22 mass %.

3. The metal sheet for separators of polymer electrolyte fuel cells according to claim 1, wherein the strike layer is a Ni layer, a Cu layer, or a Ag layer.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) In the accompanying drawings:

(2) FIG. 1 is a schematic diagram illustrating the basic structure of a fuel cell.

DETAILED DESCRIPTION

(3) Detailed description is given below.

(4) (1) Metal Sheet Used as Substrate

(5) A metal sheet used as a substrate in the disclosure is not limited, but a stainless steel sheet (ferritic stainless steel sheet, austenitic stainless steel sheet, dual-phase stainless steel sheet), a titanium sheet, a titanium alloy sheet, and the like having excellent corrosion resistance are particularly advantageous.

(6) For example, as the stainless steel sheet, SUS447J1 (Cr: 30 mass %, Mo: 2 mass %), SUS445J1 (Cr: 22 mass %, Mo: 1 mass %), SUS443J1 (Cr: 21 mass %), SUS439 (Cr: 18 mass %), SUS316L (Cr: 18 mass %, Ni: 12 mass %, Mo: 2 mass %), or the like is suitable. SUS447J1 containing about 30 mass % Cr has high corrosion resistance, and so is particularly advantageous as the substrate for separators of polymer electrolyte fuel cells used in an environment where high corrosion resistance is required. As the titanium sheet, JIS 1 type or the like is suitable. As the titanium alloy sheet, JIS 61 type or the like is suitable.

(7) In view of the installation space or weight when stacking fuel cells, the sheet thickness of the metal sheet for separators is preferably in the range of 0.03 mm to 0.30 mm. If the sheet thickness of the metal sheet for separators is less than 0.03 mm, the production efficiency of the metal sheet decreases. If the sheet thickness of the metal sheet for separators is more than 0.30 mm, the installation space or weight when stacking fuel cells increases. The sheet thickness of the metal sheet for separators is more preferably 0.03 mm or more and 0.10 mm or less.

(8) (2) Surface-Coating Layer

(9) A surface-coating layer with which the surface of the substrate is coated is not limited, but a material excellent in corrosion resistance and conductivity in the use environment (pH: 3 (sulfuric acid environment), use temperature: 80 C.) of separators of polymer electrolyte fuel cells is preferably used. For example, a metal layer, an alloy layer, a metal oxide layer, a metal carbide layer, a metal nitride layer, a carbon material layer, a conductive polymer layer, an organic resin layer containing a conductive substance, or a mixed layer thereof is suitable.

(10) Examples of the metal layer include metal layers of Au, Ag, Cu, Pt, Pd, W, Sn, Ti, Al, Zr, Nb, Ta, Ru, Ir, and Ni. A metal layer of Au or Pt is particularly suitable.

(11) Examples of the alloy layer include Sn alloy layers of NiSn (Ni.sub.3Sn.sub.2, Ni.sub.3Sn.sub.4), CuSn (Cu.sub.3Sn, Cu.sub.6Sn.sub.5), FeSn (FeSn, FeSn.sub.2), SnAg, and SnCo, and alloy layers of NiW, NiCr, and TiTa. An alloy layer of NiSn or FeSn is particularly suitable.

(12) Examples of the metal oxide layer include metal oxide layers of SnO.sub.2, ZrO.sub.2, TiO.sub.2, WO.sub.3, SiO.sub.2, Al.sub.2O.sub.3, Nb.sub.2O.sub.5, IrO.sub.2, RuO.sub.2, PdO.sub.2, Ta.sub.2O.sub.5, Mo.sub.2O.sub.5, and Cr.sub.2O.sub.3. A metal oxide layer of TiO.sub.2 or SnO.sub.2 is particularly suitable.

(13) Examples of the metal nitride layer and the metal carbide layer include metal nitride layers and metal carbide layers of TiN, CrN, TiCN, TiAlN, AlCrN, TiC, WC, SiC, B.sub.4C, molybdenum nitride, CrC, TaC, and ZrN. A metal nitride layer of TiN is particularly suitable.

(14) Examples of the carbon material layer include carbon material layers of graphite, diamond, amorphous carbon, diamond-like carbon, carbon black, fullerene, and carbon nanotube. A carbon material layer of graphite or diamond-like carbon is particularly suitable.

(15) Examples of the conductive polymer layer include conductive polymer layers of polyaniline and polypyrrole.

(16) The organic resin layer containing a conductive substance contains at least one conductive substance selected from a metal, an alloy, a metal oxide, a metal nitride, a metal carbide, a carbon material, and a conductive polymer included in the aforementioned metal layer, alloy layer, metal oxide layer, metal nitride layer, metal carbide layer, carbon material layer, and conductive polymer layer, and contains at least one organic resin selected from epoxy resin, phenol resin, polyamide-imide resin, polyester resin, polyphenylene sulfide resin, polyamide resin, urethane resin, acrylic resin, polyethylene resin, polypropylene resin, carbodiimide resin, phenol epoxy resin, and the like. As the organic resin layer containing a conductive substance, for example, graphite-dispersed phenol resin or carbon black-dispersed epoxy resin is suitable.

(17) As the conductive substance, a metal and a carbon material (in particular, graphite, carbon black) are suitable. The content of the conductive substance is not limited, as long as predetermined conductivity is obtained in separators of polymer electrolyte fuel cells.

(18) Examples of the mixed layer include a mixed layer of a TiN-dispersed NiSn alloy.

(19) For the formation of the surface-coating layer on the surface of the metal substrate, a method such as plating, physical vapor deposition (PVD), chemical vapor deposition (CVD), electrodeposition, thermal spraying, surface melting treatment, or coating may be used depending on the type of the surface-coating layer to be formed.

(20) For example, in the case of providing the surface-coating layer that is the metal layer or the alloy layer, plating is suitable. In this case, by a conventionally known plating method the substrate is immersed in a plating bath adjusted to a predetermined composition and subjected to electroplating, electroless plating, or hot dip coating. The thickness of such a surface-coating layer is preferably 0.1 m or more and 5.0 m or less. If the thickness of the surface-coating layer is less than 0.1 m, coating defects increase and the corrosion resistance tends to degrade. If the thickness of the surface-coating layer is more than 5.0 m, the coating cost increases and manufacturability decreases. The thickness of the surface-coating layer is more preferably 0.5 m or more. The thickness of the surface-coating layer is more preferably 3.0 m or less.

(21) In the case of providing the metal oxide layer, the metal nitride layer, the metal carbide layer, or the carbon material layer, physical vapor deposition (PVD) or chemical vapor deposition (CVD) is suitable. The thickness of such a surface-coating layer is preferably in the range of 0.05 m to 1.0 m, for the same reason as above.

(22) In the case of providing the conductive polymer layer, electropolymerization is suitable. The thickness of such a surface-coating layer is preferably in the range of 0.1 m to 5.0 m, for the same reason as above.

(23) In the case of providing the organic resin layer containing a conductive substance, coating (a method of applying a predetermined coating solution and then firing) is suitable. The thickness of such a surface-coating layer is preferably in the range of 1.0 m to 50.0 m, for the same reason as above. The thickness of the surface-coating layer is more preferably 1.0 m or more. The thickness of the surface-coating layer is more preferably 10.0 m or less.

(24) (Strike Layer)

(25) Forming a strike layer between the metal substrate and the surface-coating layer improves the adhesion between the surface-coating layer and the substrate. The reason why forming the strike layer between the metal substrate and the surface-coating layer improves the adhesion between the surface-coating layer and the substrate is considered as follows.

(26) In the case where there is no strike layer, an inactive passive film or the like tends to be formed on the surface of the metal substrate, making it difficult to achieve high adhesion. In the case where the strike layer is provided, on the other hand, the formation of the passive film or the like is suppressed and the surface of the metal substrate is kept from becoming inactive, as a result of which the adhesion between the substrate and the surface-coating layer is improved.

(27) Moreover, a strike layer whose surface is uneven is more advantageous because the adhesion is further improved by the anchor effect.

(28) The disclosed metal sheet for separators of polymer electrolyte fuel cells thus has excellent adhesion between the substrate and the surface-coating layer, and therefore is advantageous in the process of forming the separator into a desired shape or the process of assembling the fuel cell where high adhesion is required, or when the fuel cell vibrates violently during use.

(29) It is very important to limit the coating ratio of the strike layer on the substrate and the coating form of the strike layer as follows: the coating ratio of the strike layer on the substrate: 2% to 70%.

(30) By limiting the coating ratio of the strike layer on the substrate to this range, the corrosion resistance in the separator use environment can be maintained even in the case where the surface-coating layer is made thinner. The reason for this is considered as follows.

(31) Typically, when the thickness of the surface-coating layer is reduced, in-layer defects from the surface-coating layer to the substrate increase. Through these defects, the strike layer between the metal substrate and the surface-coating layer is widely corroded continuously in the surface direction, causing the surface-coating layer above the strike layer to exfoliate from the metal substrate. When the surface-coating layer exfoliates, the substrate is exposed to the separator use environment, and as a result the corrosion resistance decreases.

(32) Limiting the coating ratio of the strike layer on the substrate to the aforementioned range, however, allows the strike layer to be formed discontinuously on the surface of the substrate. In other words, a discontinuous portion such as a non-coating area of the strike layer appears in part of the surface of the substrate. This discontinuous portion of the strike layer acts as an area that inhibits the propagation of the corrosion. Hence, the continuous corrosion of the strike layer is suppressed even in the case where the surface-coating layer is made thinner. The degradation of the corrosion resistance can be prevented in this way.

(33) If the coating ratio of the strike layer on the substrate is less than 2%, the adhesion between the metal substrate and the surface-coating layer decreases. If the coating ratio of the strike layer on the substrate is more than 70%, the corrosion resistance cannot be maintained in the case where the thickness of the surface-coating layer is reduced. Accordingly, the coating ratio of the strike layer on the substrate is limited to the range of 2% to 70%. The coating ratio of the strike layer on the substrate is preferably 5% or more. The coating ratio of the strike layer on the substrate is preferably 60% or less. The coating ratio of the strike layer on the substrate is more preferably 10% or more. The coating ratio of the strike layer on the substrate is more preferably 50% or less. The coating ratio of the strike layer on the substrate is further preferably 15% or more. The coating ratio of the strike layer on the substrate is further preferably 40% or less. the strike layer being distributed in the form of islands and the maximum diameter of the island-like coating portions of the strike layer being 1.00 m or less and being not greater than the thickness of the surface-coating layer.

(34) The strike layer needs to have a coating form in which the strike layer is distributed in the form of islands on the surface of the substrate and the maximum diameter of the island-like coating portions of the strike layer is 1.00 m or less.

(35) By limiting the coating form of the strike in this way, discontinuous portions such as non-coating areas of the strike layer are formed throughout the surface of the substrate. This suppresses the continuous corrosion of the strike layer more effectively, and prevents the degradation of the corrosion resistance more effectively. This also makes the whole interface between the metal substrate and the surface-coating layer rough, and so enhances the adhesion property by the anchor effect. Here, if the maximum diameter of the island-like coating portions is greater than the thickness of the surface-coating layer, the discontinuity of the strike layer with respect to the thickness of the surface-coating layer decreases relatively, and the corrosion resistance cannot be maintained. The maximum diameter of the island-like coating portions therefore needs to be not greater than the thickness of the surface-coating layer. The thickness of the surface-coating layer mentioned here is the average thickness of the surface-coating layer.

(36) Thus, the coating form of the strike layer is limited so that the strike layer is distributed in the form of islands on the surface of the substrate and the maximum diameter of the island-like coating portions of the strike layer is 1.00 m or less and is not greater than the thickness of the surface-coating layer.

(37) The maximum diameter of the island-like coating portions of the strike layer is preferably limited to 0.50 m or less and not greater than the thickness of the surface-coating layer. The maximum diameter of the island-like coating portions of the strike layer is more preferably limited to 0.10 m or less and not greater than the thickness of the surface-coating layer.

(38) The specific shape of each island-like coating portion is not limited, and may be any of circular, elliptic, polygonal, ameboid (a shape extending in a plurality of irregular directions), etc. The diameter of each island-like coating portion is defined as the diameter of the smallest circle that touches two or more points on the perimeter of the island-like coating portion and completely encloses the island-like coating portion.

(39) The strike layer is preferably a metal layer of Ni, Cu, Ag, Au, or the like or an alloy layer containing at least one selected from these elements. A Ni strike or a NiP strike made of an alloy layer of Ni and P is more preferable in terms of material cost.

(40) In the case of a NiP strike, it is further preferable to limit the P content in the NiP strike layer to the range of 5 mass % to 22 mass %.

(41) P content in NiP strike layer: 5 mass % to 22 mass %

(42) By limiting the P content in the NiP strike layer to this range, excellent corrosion resistance can be maintained more stably even in the event of long exposure to high potential in the separator environment. The reason for this is considered as follows.

(43) By limiting the P content in the NiP strike layer to the range of 5 mass % to 22 mass %, a more stable NiP compound in the separator use environment is formed, with it being possible to suppress the corrosion of the strike layer effectively for a longer time.

(44) If the P content in the NiP strike layer is less than 5 mass %, the improvement effect is insufficient. If the P content in the NiP strike layer is more than 22 mass %, the composition of the NiP strike tends to be not uniform. Such a range is also not preferable in terms of maintaining excellent corrosion resistance in the event of long exposure to high potential in the separator environment. Therefore, the P content in the NiP strike layer is preferably limited to the range of 5 mass % to 22 mass %. The P content in the NiP strike layer is more preferably 7 mass % or more. The P content in the NiP strike layer is more preferably 20 mass % or less. The P content in the NiP strike layer is further preferably 10 mass % or more. The P content in the NiP strike layer is further preferably 18 mass % or less.

(45) The method of forming the strike layer may be a conventionally known plating method whereby electroplating or electroless plating is performed in a plating bath adjusted to an appropriate composition. For example in the case of electroplating, to limit the coating form of the strike layer as mentioned above, the time of retention in the plating bath, i.e. the electroplating time, and the current density during electroplating need to be controlled appropriately.

(46) The electroplating time and the current density during electroplating influence the coating ratio of the strike layer on the substrate, and the current density during electroplating also influences the maximum diameter of the island-like coating portions. When the electroplating time is longer and the current density is higher, the coating ratio of the strike layer on the substrate is higher. Moreover, a higher current density typically facilitates nucleation, which contributes to a smaller maximum diameter of the island-like coating portions.

(47) For example, in the case of forming a Ni strike, a NiP strike, or a Cu strike, a current density of 6 A/dm.sup.2 or more and an electroplating time of 1 second or more are preferable in terms of achieving the desired coating form, although fine adjustment is needed for differences depending on the structure of the electroplating apparatus such as the distance between electrodes and the size of the plating tank. A current density of 7 A/dm.sup.2 or more and an electroplating time of 1 second or more are more preferable. If the current density is excessively high, the adhesion decreases. The upper limit of the current density is therefore preferably about 10 A/dm.sup.2. The electroplating time is preferably 180 seconds or less. The electroplating time is more preferably 60 seconds or less.

(48) In the case of forming an Ag strike or an Au strike, on the other hand, a current density of 4 A/dm.sup.2 or more and an electroplating time of 1 second or more are preferable. A current density of 5 A/dm.sup.2 or more and an electroplating time of 1 second or more are more preferable. If the current density is excessively high, the adhesion decreases. The upper limit of the current density is therefore preferably about 10 A/dm.sup.2. The electroplating time is preferably 180 seconds or less. The electroplating time is more preferably 60 seconds or less.

(49) The P content in the NiP strike layer is adjustable by the P concentration in the plating bath or the current density in plating.

(50) (4) Sn-Containing Oxide Layer

(51) In the disclosed metal sheet for separators, in the case where the surface-coating layer is a layer (Sn alloy layer) made of a Sn alloy layer, the surface of the Sn alloy layer is preferably coated with a Sn-containing oxide layer. This further improves the corrosion resistance for long time use in the separator use environment.

(52) The Sn-containing oxide layer with which the surface of the Sn alloy layer is coated is not a natural oxide layer created in the atmospheric environment but an oxide layer deliberately formed by a process such as immersion in an acid solution. The thickness of the natural oxide layer is typically about 2 nm to 3 nm.

(53) The main component of the Sn-containing oxide layer is preferably SnO.sub.2. The thickness of the Sn-containing oxide layer is preferably 5 nm or more. The thickness of the Sn-containing oxide layer is preferably 100 nm or less. The thickness of the Sn-containing oxide layer is more preferably 10 nm or more. The thickness of the Sn-containing oxide layer is more preferably 30 nm or less. If the Sn-containing oxide layer is excessively thick, the conductivity decreases. If the Sn-containing oxide layer is excessively thin, the corrosion resistance improvement effect in the separator use environment cannot be achieved.

(54) The reason why coating the surface of the Sn alloy layer with the Sn-containing oxide layer improves the corrosion resistance for long time use in the separator use environment is considered as follows. Since the Sn-containing oxide layer is very stable in the separator use environment, coating the surface of the surface-coating layer with the Sn-containing oxide layer suppresses the corrosion of the surface-coating layer effectively.

(55) Here, the oxide layer is deliberately formed by a process such as immersion in an acid solution instead of using a natural oxide layer, for the following reason. Through such a process, the oxide layer can be uniformly and accurately formed on the surface of the surface-coating layer, with it being possible to suppress the corrosion of the surface-coating layer very effectively.

(56) The Sn-containing oxide layer may be formed by a method of immersion in an acid aqueous solution having oxidizability such as hydrogen peroxide or nitric acid, or a method of anodic electrolysis.

(57) For example, the Sn-containing oxide layer can be formed by applying anodic electrolysis, in a sulfuric acid aqueous solution of a temperature of 60 C. and a pH of 1, to the metal sheet for separators having the surface-coating layer for 5 minutes with a current density of +1 mA/cm.sup.2.

(58) The method of forming the Sn-containing oxide layer is not limited to the above. Other examples include physical vapor deposition (PVD), chemical vapor deposition (CVD), and coating.

(59) (5) Other Features

(60) After forming the surface-coating layer on the surface of the metal substrate with the strike layer in between or after forming the Sn alloy layer on the surface of the metal substrate with the strike layer in between and then forming the Sn-containing oxide layer, a conductive layer with lower electric resistance may be further formed on the surface-coating layer or the Sn-containing oxide layer, to improve the conductivity which is one of the required properties of separators. For example, the surface-coating layer or the Sn-containing oxide layer may be coated with a metal layer, a conductive polymer layer, an alloy layer including conductive particles, or a polymer layer including conductive particles, in order to reduce the contact resistance.

EXAMPLES

(61) Separators of polymer electrolyte fuel cells are used in a severe corrosion environment of about 80 C. in temperature and 3 in pH, and therefore excellent corrosion resistance is required. Moreover, high adhesion between the metal substrate and the surface-coating layer is required so that the surface-coating layer does not peel off the metal substrate in the fuel cell manufacturing process such as the process of forming the separator into a desired shape or the process of assembling the fuel cell. In view of these required properties, the following two types of evaluation were conducted on the below-mentioned samples.

(62) (1) Evaluation of Corrosion Resistance (Stability in Separator Use Environment)

(63) Each sample was immersed in a sulfuric acid aqueous solution of a temperature of 80 C. and a pH of 3 and subjected to the application of a constant potential of 0.9 V (vs. SHE) for 100 hours using Ag/AgCl (saturated KCl aqueous solution) as a reference electrode, and the total electric charge conducted for 100 hours was measured. Based on the total electric charge conducted for 100 hours, the corrosion resistance after 100 hours in the separator use environment was evaluated by the following criteria. Excellent: the total electric charge conducted for 100 hours was less than 15 mC/cm.sup.2. Good: the total electric charge conducted for 100 hours was 15 mC/cm.sup.2 or more and less than 100 mC/cm.sup.2. Poor: the total electric charge conducted for 100 hours was 100 mC/cm.sup.2 or more.

(64) (2) Evaluation of Adhesion Property

(65) The adhesive face of Scotch tape was adhered to the surface of each sample obtained by forming a surface-coating layer on the surface of a metal substrate, in an area of 20 mm20 mm. The Scotch tape was then removed, and the adhesion property was evaluated by the following criteria. Good: the surface-coating layer did not peel after the removal of the Scotch tape. Poor: the surface-coating layer peeled after the removal of the Scotch tape.

Example 1

(66) Each of SUS447J1 (Cr: 30 mass %) of 0.05 mm in sheet thickness and titanium JIS 1 type of 0.05 mm in sheet thickness as a substrate was subjected to appropriate pretreatment such as degreasing, and then a strike layer with the coating form listed in Table 1 was formed on the substrate using the plating bath composition and plating condition listed in Table 1 and mentioned below. Next, a surface-coating layer with the average thickness listed in Table 1 was formed on the substrate having the strike layer, to obtain a metal sheet for separators.

(67) For the metal layer and alloy layer of Au and Ni.sub.3Sn.sub.2 and TiN-dispersed Ni.sub.3Sn.sub.2, the surface-coating layer was formed using the below-mentioned plating bath composition and plating condition. For the metal oxide layers of TiO.sub.2 and SnO.sub.2, the surface-coating layer was formed by physical vapor deposition (PVD). For the metal nitride layer (TiN), the surface-coating layer was formed by physical vapor deposition (PVD). For the carbon material layer (diamond-like carbon), the surface-coating layer was formed by chemical vapor deposition (CVD). For the conductive polymer layer (polyaniline), the surface-coating layer was formed by electropolymerization. For the organic resin layer containing a conductive substance (carbon black-dispersed epoxy resin and graphite-dispersed phenol resin), the surface-coating layer was formed by applying a predetermined coating solution and then firing.

(68) The carbon black-dispersed epoxy resin was obtained by dispersing carbon black particles with an average particle size of 50 nm in epoxy resin in a proportion of 20 mass %. The graphite-dispersed phenol resin was obtained by dispersing graphite particles with an average particle size of 3 m in phenol resin in a proportion of 20 mass %.

(69) In samples Nos. 45 and 47 to 50, the obtained metal sheet for separators was subjected to anodic electrolysis in a sulfuric acid aqueous solution of a temperature of 60 C. and a pH of 1 for 5 minutes with a current density of +1 mA/cm.sup.2, to form a Sn-containing oxide layer on the surface of the surface-coating layer.

(70) Each property was evaluated in the aforementioned manner using the obtained metal sheet for separators.

(71) The coating form of the strike layer was regulated by determining the relationship with the electroplating time and the current density beforehand. The average thickness of the surface-coating layer and the average thickness of the Sn-containing oxide layer were each regulated by determining the relationship with the plating time, the anodic electrolysis time, the layer formation time in physical vapor deposition (PVD) or chemical vapor deposition (CVD), and the amount of the coating solution applied in the coating beforehand. For comparison, a metal sheet for separators having no strike layer was also prepared, and each property was evaluated in the aforementioned manner.

(72) The coating ratio of the strike layer on the substrate and the maximum diameter of the island-like coating portions were measured by the following method.

(73) First, each sample obtained by forming the strike layer on the surface of the substrate (0.05 mm in thickness) was cut to about 10 mm W10 mm L. The coating form of the strike layer was observed using a scanning electron microscope (SEM), and the diameter of each island-like coating portion was measured and the maximum value of the diameters was determined.

(74) Next, the coating portion and non-coating portion of the strike layer were binarized using image analysis software, to calculate the coating ratio of the strike layer on the substrate. Although the magnification in the SEM observation may be freely changed according to the maximum diameter of the coating portions, the magnification is preferably about 10000 to 100000.

(75) The measurement of each of the coating ratio of the strike layer on the substrate and the diameter of each island-like coating portion was performed on 10 samples obtained by cutting the same sample having the strike layer to the aforementioned shape. The coating ratio of the strike layer on the substrate is the average coating ratio of the strike layer on the substrate of the 10 samples, and the maximum diameter of the island-like coating portions is the maximum value of the diameters of the island-like coating portions observed in the 10 samples.

(76) Here, the composition of the strike made of an alloy layer of Ni and P was measured by an energy-dispersive X-ray spectrometer (EDX) used in the SEM observation.

(77) Regarding the samples having no strike, - is shown in the fields of the coating ratio of the strike layer on the substrate and the maximum diameter of the island-like coating portion of the strike layer in Table 1.

(78) The average thickness of the surface-coating layer was measured by the following method. The measurement method in the case where the average thickness is 1.0 m or more is described first. Each sample obtained by forming the strike layer and the surface-coating layer on the surface of the substrate (0.05 mm in thickness) was cut to about 10 mm W15 mm L. The sample was then embedded in resin, polished in the cross section, and then observed using a scanning electron microscope (SEM) to measure the thickness of the surface-coating layer. The measurement of the thickness of the surface-coating layer was performed on 10 samples obtained by cutting the same sample having the surface-coating layer to the aforementioned shape, and the average thickness of these samples was set as the average thickness of the surface-coating layer.

(79) The measurement method in the case where the average thickness of the surface-coating layer is less than 1.0 m and the method of measuring the average thickness of the Sn-containing oxide layer are described next. Each sample obtained by forming the strike layer and the surface-coating layer and, for Nos. 45 and 47 to 50, further the Sn-containing oxide layer on the surface of the substrate (0.05 mm in thickness) was processed by a focused ion beam to prepare a thin film for cross-section observation. The produced thin film for cross-section observation was then observed using a transmission electron microscope (TEM), to measure the average thickness of each of the surface-coating layer and the Sn-containing oxide layer. In the measurement of the average thickness of each of the surface-coating layer and the Sn-containing oxide layer, the thickness of each of the surface-coating layer and the Sn-containing oxide layer in the prepared thin film for cross-section observation was measured at three locations, and the average value of the three locations was set as the average thickness of the corresponding one of the surface-coating layer and the Sn-containing oxide layer.

(80) Here, the composition of each of the surface-coating layer and the Sn-containing oxide layer was identified by an energy-dispersive X-ray spectrometer (EDX), X-ray diffractometer (XRD), laser Raman spectrometer, and/or Fourier transform infrared spectroscopic analyzer used in the SEM observation or TEM observation.

(81) (Plating Bath Composition and Plating Condition of Strike Layer)

(82) <Ni strike>

(83) Nickel chloride: 240 g/L

(84) Hydrochloric acid: 125 ml/L

(85) Temperature: 50 C.

(86) <Ni-P strike>

(87) Nickel sulfate: 1 mol/L

(88) Nickel chloride: 0.1 mol/L

(89) Boric acid: 0.5 mol/L

(90) Sodium phosphite: 0.05 mol/L to 5 mol/L

(91) Temperature: 60 C.

(92) <Cu strike>

(93) Copper cyanide: 30 g/L

(94) Sodium cyanide: 40 g/L

(95) Potassium hydroxide: 4 g/L

(96) Temperature: 40 C.

(97) <Ag strike>

(98) Silver potassium cyanide: 2 g/L

(99) Sodium cyanide: 120 g/L

(100) Temperature: 30 C.

(101) <Au strike>

(102) Gold potassium cyanide: 8 g/L

(103) Sodium citrate: 80 g/L

(104) Nickel sulfamate: 3 g/L

(105) Zinc acetate: 0.3 g/L

(106) Temperature: 30 C.

(107) (Plating Bath Composition and Plating Condition of Surface-Coating Layer)

(108) <Au>

(109) Gold potassium cyanide: 8 g/L

(110) Sodium citrate: 80 g/L

(111) Nickel sulfamate: 3 g/L

(112) Zinc acetate: 0.3 g/L

(113) Temperature: 30 C.

(114) Current density: 1 A/dm.sup.2

(115) <Ni.sub.3Sn.sub.2>

(116) Nickel chloride: 0.15 mol/L

(117) Tin chloride: 0.15 mol/L

(118) Potassium pyrophosphate: 0.45 mol/L

(119) Glycine: 0.15 mol/L

(120) Temperature: 60 C.

(121) Current density: 1 A/dm.sup.2

(122) <TiN-dispersed Ni.sub.3Sn.sub.2>

(123) Nickel chloride: 0.15 mol/L

(124) Tin chloride: 0.15 mol/L

(125) Potassium pyrophosphate: 0.45 mol/L

(126) Glycine: 0.15 mol/L

(127) Temperature: 60 C.

(128) Current density: 1 A/dm.sup.2

(129) Average particle size of dispersed TiN: 1.5 m

(130) In the disclosure, as long as a desired plating can be formed, a plating bath composition other than the above may be used according to a known plating method.

(131) Table 1 summarizes the results of evaluating the corrosion resistance (stability in the separator use environment) and the adhesion property for each sample obtained as described above.

(132) TABLE-US-00001 TABLE 1 Sample preparation condition Strike layer Current Electroplating Coating ratio of Maximum diameter of Sample density time strike layer island-like coating portion P content No. Substrate Type (A/dm.sup.2) (sec) (%) (m) (mass %) 1 Stainless steel N/A 2 SUS447J1 Ni 6 1 2 0.01 3 5 3 31 0.04 4 3 20 62 0.08 5 2 35 70 0.22 6 3 50 100 Connected and unmeasurable 7 NiP 7 1 5 0.02 13 8 6 1.5 11 0.03 14 9 6 2.5 27 0.04 15 10 3 5 27 0.11 15 11 2.5 6 27 0.21 15 12 2 7.5 27 0.54 15 13 1.5 10 27 0.93 15 14 1 15 27 1.60 15 15 6 6 42 0.02 15 16 5 10 50 0.07 15 17 1 80 67 1.00 16 18 2 50 75 0.80 16 19 1 130 86 1.60 16 20 3 60 100 Connected and unmeasurable 17 21 Cu 4 2 25 0.04 22 4 4 38 0.08 23 Ag 4 3 30 0.06 24 4 7 48 0.10 25 Au 4 1.5 16 0.04 26 4 3 33 0.06 27 Ni 5 2.5 25 0.04 28 Ag 5 1.5 18 0.03 29 1 80 84 0.80 30 N/A 31 NiP 6 2 20 0.03 15 32 1 130 86 1.60 16 33 Ni 6 1 2 0.01 34 6 1 2 0.01 35 2 40 74 0.30 36 NiP 6 2 20 0.04 15 37 1 130 86 1.60 16 38 NiP 6 2 20 0.04 15 39 2.5 25 55 0.20 16 40 Au 4 1.5 16 0.04 41 Ni 5 2.5 25 0.04 42 2 40 74 0.30 43 Ni 5 2.5 25 0.04 44 1.5 60 80 0.50 45 Titanium N/A 46 JIS 1 type Ni 5 2.5 28 0.04 47 NiP 6 2 24 0.03 15 48 Cu 4 2 25 0.05 49 Ag 4 3 30 0.06 50 Au 4 1.5 20 0.04 Sample preparation condition Surface-coating layer Sn-containing oxide layer Average Average Sample thickness Main thickness No. Type (m) Formation method component (nm) 1 Au 3.0 Plating 2 1.0 3 1.0 4 1.0 5 1.0 6 1.0 7 1.0 8 1.0 9 1.0 10 0.5 11 1.0 12 3.0 13 1.0 14 1.0 15 1.0 16 1.0 17 1.0 18 1.0 19 5.0 20 1.0 21 1.0 22 1.0 23 1.0 24 1.0 25 1.0 26 1.0 27 Carbon black- 10.0 Firing after application 28 dispersed epoxy resin 5.0 29 5.0 30 Graphite-dispersed 3.0 Firing after application 31 phenol resin 5.0 32 5.0 33 Diamond-like carbon 0.3 CVD 34 1.0 35 0.1 36 TiN-dispersed 2.0 Plating 37 Ni.sub.3Sn.sub.2 5.0 38 SnO.sub.2 0.1 PVD 39 0.1 40 TiO.sub.2 0.1 PVD 41 TiN 0.1 PVD 42 0.1 43 Polyaniline 1.0 Electropolymerization 44 1.0 45 Ni.sub.3Sn.sub.2 3.0 Plating SnO.sub.2 15 46 1.0 47 1.0 SnO.sub.2 15 48 1.0 SnO.sub.2 15 49 1.0 SnO.sub.2 15 50 1.0 SnO.sub.2 15 Total electric Evaluation result charge for 100 Peeling of surface- Corrosion Sample hours coating layer in tape resistance after 100 No. (mC/cm.sup.2) removal test hours Adhesion Remarks 1 12.3 Peeled Excellent Poor Comparative Example 2 14.0 Not peeled Excellent Good Example 3 16.1 Not peeled Good Good Example 4 17.4 Not peeled Good Good Example 5 18.8 Not peeled Good Good Example 6 398 Not peeled Poor Good Comparative Example 7 12.6 Not peeled Excellent Good Example 8 12.8 Not peeled Excellent Good Example 9 13.5 Not peeled Excellent Good Example 10 15.6 Not peeled Good Good Example 11 15.8 Not peeled Good Good Example 12 18.0 Not peeled Good Good Example 13 19.5 Not peeled Good Good Example 14 334 Not peeled Poor Good Comparative Example 15 15.1 Not peeled Good Good Example 16 16.3 Not peeled Good Good Example 17 20.5 Not peeled Good Good Example 18 165 Not peeled Poor Good Comparative Example 19 211 Not peeled Poor Good Comparative Example 20 384 Not peeled Poor Good Comparative Example 21 12.3 Not peeled Excellent Good Example 22 13.2 Not peeled Excellent Good Example 23 12.5 Not peeled Excellent Good Example 24 13.1 Not peeled Excellent Good Example 25 12.0 Not peeled Excellent Good Example 26 12.4 Not peeled Excellent Good Example 27 65.5 Not peeled Good Good Example 28 72.8 Not peeled Good Good Example 29 119 Not peeled Poor Good Comparative Example 30 56.7 Peeled Good Poor Comparative Example 31 67.7 Not peeled Good Good Example 32 216 Not peeled Poor Good Comparative Example 33 69.9 Not peeled Good Good Example 34 34.9 Not peeled Good Good Example 35 219 Not peeled Poor Good Comparative Example 36 64.1 Not peeled Good Good Example 37 211 Not peeled Poor Good Comparative Example 38 1.1 Not peeled Excellent Good Example 39 113 Not peeled Poor Good Comparative Example 40 1.5 Not peeled Excellent Good Example 41 32.5 Not peeled Good Good Example 42 174 Not peeled Poor Good Comparative Example 43 54.5 Not peeled Good Good Example 44 194 Not peeled Poor Good Comparative Example 45 9.9 Peeled Excellent Poor Comparative Example 46 38.5 Not peeled Good Good Example 47 11.4 Not peeled Excellent Good Example 48 10.9 Not peeled Excellent Good Example 49 10.7 Not peeled Excellent Good Example 50 10.1 Not peeled Excellent Good Example

(133) The table reveals the following points.

(134) (a) The samples of Examples all had low current density after 100 hours in the corrosion resistance evaluation, and had favorable corrosion resistance even in the event of long exposure to high potential as in the separator use environment. In particular, Nos. 2, 7 to 9, 21 to 26, 38, 40, and 47 to 50 had excellent corrosion resistance. Moreover, the samples of Examples all had excellent adhesion property.

(135) (b) The samples of Comparative Examples Nos. 1, 30, and 45 with no strike layer did not have desired adhesion property.

(136) (c) The samples of Comparative Examples Nos. 6, 14, 18 to 20, 29, 32, 35, 37, 39, 42, and 44 with the coating ratio of the strike layer on the substrate and/or the maximum diameter of the island-like coating portion being outside the appropriate range had high current density after 100 hours in the corrosion resistance evaluation, and did not have desired corrosion resistance.

REFERENCE SIGNS LIST

(137) 1 membrane-electrode joined body 2, 3 gas diffusion layer 4, 5 separator 6 air passage 7 hydrogen passage