US20060045791A1 - Low melting temperature silver braze alloy - Google Patents
Low melting temperature silver braze alloy Download PDFInfo
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- US20060045791A1 US20060045791A1 US10/929,819 US92981904A US2006045791A1 US 20060045791 A1 US20060045791 A1 US 20060045791A1 US 92981904 A US92981904 A US 92981904A US 2006045791 A1 US2006045791 A1 US 2006045791A1
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- Prior art keywords
- silver
- fuel cell
- alloy
- silicon
- accordance
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- 239000004332 silver Substances 0.000 title claims abstract description 48
- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 47
- 239000000956 alloy Substances 0.000 title claims abstract description 47
- 229910052709 silver Inorganic materials 0.000 title claims abstract description 43
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 title abstract description 43
- 230000008018 melting Effects 0.000 title description 7
- 238000002844 melting Methods 0.000 title description 7
- 239000000446 fuel Substances 0.000 claims abstract description 34
- 238000005219 brazing Methods 0.000 claims abstract description 26
- 239000010703 silicon Substances 0.000 claims abstract description 24
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 23
- 239000000919 ceramic Substances 0.000 claims abstract description 14
- 229910052751 metal Inorganic materials 0.000 claims abstract description 14
- 239000002184 metal Substances 0.000 claims abstract description 14
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims abstract description 7
- KJTLSVCANCCWHF-UHFFFAOYSA-N Ruthenium Chemical compound [Ru] KJTLSVCANCCWHF-UHFFFAOYSA-N 0.000 claims abstract description 7
- 229910052802 copper Inorganic materials 0.000 claims abstract description 7
- 239000010949 copper Substances 0.000 claims abstract description 7
- 229910052707 ruthenium Inorganic materials 0.000 claims abstract description 7
- 239000007787 solid Substances 0.000 claims abstract description 6
- 229910052720 vanadium Inorganic materials 0.000 claims abstract description 5
- 150000001875 compounds Chemical class 0.000 claims 2
- GPPXJZIENCGNKB-UHFFFAOYSA-N vanadium Chemical compound [V]#[V] GPPXJZIENCGNKB-UHFFFAOYSA-N 0.000 claims 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 abstract description 21
- 150000002739 metals Chemical class 0.000 abstract description 8
- 229910001316 Ag alloy Inorganic materials 0.000 abstract description 6
- 229910000676 Si alloy Inorganic materials 0.000 abstract description 5
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 abstract description 4
- 239000006023 eutectic alloy Substances 0.000 abstract description 2
- 210000004027 cell Anatomy 0.000 description 16
- 238000010587 phase diagram Methods 0.000 description 4
- QPLDLSVMHZLSFG-UHFFFAOYSA-N Copper oxide Chemical compound [Cu]=O QPLDLSVMHZLSFG-UHFFFAOYSA-N 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- 239000005751 Copper oxide Substances 0.000 description 2
- 229910000431 copper oxide Inorganic materials 0.000 description 2
- 230000005496 eutectics Effects 0.000 description 2
- 230000001590 oxidative effect Effects 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 229910000929 Ru alloy Inorganic materials 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 239000003792 electrolyte Substances 0.000 description 1
- 230000004927 fusion Effects 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 238000005304 joining Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
- B23K35/24—Selection of soldering or welding materials proper
- B23K35/30—Selection of soldering or welding materials proper with the principal constituent melting at less than 1550 degrees C
- B23K35/3006—Ag as the principal constituent
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/02—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape
- B23K35/0222—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape for use in soldering, brazing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/02—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape
- B23K35/0222—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape for use in soldering, brazing
- B23K35/0244—Powders, particles or spheres; Preforms made therefrom
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
- B23K35/24—Selection of soldering or welding materials proper
- B23K35/30—Selection of soldering or welding materials proper with the principal constituent melting at less than 1550 degrees C
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
- B23K35/24—Selection of soldering or welding materials proper
- B23K35/32—Selection of soldering or welding materials proper with the principal constituent melting at more than 1550 degrees C
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
- B23K35/24—Selection of soldering or welding materials proper
- B23K35/32—Selection of soldering or welding materials proper with the principal constituent melting at more than 1550 degrees C
- B23K35/322—Selection of soldering or welding materials proper with the principal constituent melting at more than 1550 degrees C a Pt-group metal as principal constituent
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B37/00—Joining burned ceramic articles with other burned ceramic articles or other articles by heating
- C04B37/003—Joining burned ceramic articles with other burned ceramic articles or other articles by heating by means of an interlayer consisting of a combination of materials selected from glass, or ceramic material with metals, metal oxides or metal salts
- C04B37/006—Joining burned ceramic articles with other burned ceramic articles or other articles by heating by means of an interlayer consisting of a combination of materials selected from glass, or ceramic material with metals, metal oxides or metal salts consisting of metals or metal salts
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B37/00—Joining burned ceramic articles with other burned ceramic articles or other articles by heating
- C04B37/02—Joining burned ceramic articles with other burned ceramic articles or other articles by heating with metallic articles
- C04B37/023—Joining burned ceramic articles with other burned ceramic articles or other articles by heating with metallic articles characterised by the interlayer used
- C04B37/026—Joining burned ceramic articles with other burned ceramic articles or other articles by heating with metallic articles characterised by the interlayer used consisting of metals or metal salts
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M8/00—Fuel cells; Manufacture thereof
- H01M8/02—Details
- H01M8/0271—Sealing or supporting means around electrodes, matrices or membranes
- H01M8/028—Sealing means characterised by their material
- H01M8/0282—Inorganic material
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/02—Aspects relating to interlayers, e.g. used to join ceramic articles with other articles by heating
- C04B2237/12—Metallic interlayers
- C04B2237/125—Metallic interlayers based on noble metals, e.g. silver
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M8/00—Fuel cells; Manufacture thereof
- H01M8/10—Fuel cells with solid electrolytes
- H01M8/12—Fuel cells with solid electrolytes operating at high temperature, e.g. with stabilised ZrO2 electrolyte
- H01M2008/1293—Fuel cells with solid oxide electrolytes
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/30—Hydrogen technology
- Y02E60/50—Fuel cells
Definitions
- the present invention relates to alloys for joining materials by brazing; more particularly, to silver-containing braze alloys for joining ceramics to metals; and most particularly, to silver braze alloys containing silicon to lower the liquidus temperature.
- Fuel cells which generate electric current by controllably combining elemental hydrogen and oxygen are well known.
- an anodic layer and a cathodic layer are separated by a permeable electrolyte formed of a ceramic solid oxide, such as yttrium-stabilized zirconium (YSZ).
- YSZ yttrium-stabilized zirconium
- SOFC solid oxide fuel cell
- a single cell is capable of generating a relatively small voltage and wattage, typically between about 0.5 volt and about 1.0 volt, depending upon load, and less than about 2 watts per cm 2 of cell surface. Therefore, in practice it is known to stack together, in electrical series, a plurality of cells.
- each ceramic-based fuel cell is bonded to a surrounding metal “cassette” frame to form a fuel cell sub-assembly, using a silver/copper-based braze.
- the copper is rapidly oxidized to form copper oxide which separates from the alloy, leaving essentially pure silver as the brazing material.
- the copper oxide migrates to the boundaries of the liquid and adheres to the ceramic and the metal, providing an attachment layer for the silver.
- Exemplary silver/copper and silver/vanadium braze alloys are disclosed in International Publication No. WO 03/059843, published 24 Jul. 2003, which is incorporated herein by reference.
- the liquidus temperature is substantially the melting point of pure silver, 962° C. This temperature is high enough to preclude use of some fuel cell materials which can be damaged by such high temperatures.
- a higher temperature braze could be used for the first seal, and a lower temperature braze for the second seal.
- a brazing alloy in accordance with the invention comprises elemental silver alloyed with another element that serves to reduce the liquidus temperature of the alloy to a temperature below the melting point of silver.
- a brazing alloy comprises elemental silver alloyed with elemental silicon in a silver/silicon ratio between about 95/5 and 99/1, preferably about 97/3.
- Brazing alloys in accordance with the invention are useful in bonding ceramics to ceramics, ceramics to metals, and metals to metals. Such metals are preferably alumina-forming. Copper, vanadium, or other oxygen-reactive surface bonding elements may also be included, and use of such brazing alloys is preferably carried out in an oxidizing atmosphere.
- FIG. 1 is a silver/silicon phase diagram
- FIG. 2 is a cross-sectional view of a portion of a fuel cell, showing bonding of a ceramic component to a metal component by a braze alloy in accordance with the invention
- FIG. 3 is a cross-sectional view of a portion of a fuel cell, similar to that shown in FIG. 2 , but showing a second braze alloy having a different liquidus temperature;
- FIG. 4 is a silver/ruthenium phase diagram.
- a phase diagram 10 for silver and silicon alloy mixtures is conventionally displayed, having temperature on the vertical axis as a function of weight percent silicon on the horizontal axis.
- the solidus/liquidus curve 12 for alloys of silver and silicon extends from pure silver (MP of about 962° C.) to pure silicon (MP 1414° C.). Addition of relatively small amounts of silicon to pure silver serves to depress the alloy liquidus temperature significantly; a eutectic point 14 of about 835° C. exists at a silver/silicon ratio of about 97/3. Useful liquidus temperature depressions below the 962° C. melting temperature of silver exist up to about 5% silicon.
- phase diagram 10 ′ for silver and ruthenium alloy mixtures of a second embodiment including solidus/liquidus curve 12 ′ and eutectic point 14 ′, is shown.
- a silver/ruthenium ratio between about 96/4 and 99/1, preferably about 97/3, a liquidus temperature of about 920° C. is achieved.
- the addition of relatively small amounts of ruthenium to pure silver similarly serves to depress the alloy liquidus temperature below the melting point of pure silver.
- a ceramic-based fuel cell element 18 is bonded to a metal cassette 20 by a braze seal formed of a silver/silicon braze alloy 22 in accordance with the invention.
- the braze alloy includes either copper or vanadium which is readily oxidized to form CuO or V 2 O 5 during fusion of the alloy in an oxidizing atmosphere.
- the oxides separate from the alloy in known fashion and provide an adhesion layer 24 on element 18 and cassette 20 for attachment of the remaining silver/silicon alloy 26 .
- FIG. 3 it can be seen how the use of two or more different silver/silicon braze alloys can be used so that a additional brazed seals can be formed without re-liquefying the already formed brazed seals.
- fuel cell element 18 is bonded to a second element, such as cassette 20 , by a braze seal formed of a silver/silicon braze alloy 22 having a liquidus temperature of less than 962° C., as described above.
- Third element 18 ′ can then be bonded to element 20 (or any other element in the fuel cell assembly) using a silver/silicon braze alloy 22 ′ having a different weight percentage concentration of silicon and having a liquidus temperature lower than the melting temperature of alloy 22 .
- braze alloy can be made from a mix of the elemental powders which would then be allowed to alloy during the brazing process.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Ceramic Engineering (AREA)
- Organic Chemistry (AREA)
- Structural Engineering (AREA)
- Materials Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Electrochemistry (AREA)
- General Chemical & Material Sciences (AREA)
- Sustainable Energy (AREA)
- Sustainable Development (AREA)
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- Inorganic Chemistry (AREA)
- Fuel Cell (AREA)
Abstract
A brazing alloy comprising elemental silver alloyed with elemental silicon in a silver/silicon ratio between about 95/5 and 99/1, preferably about 97/3. Small amounts of silicon alloyed with silver depress the alloy liquidus curve significantly, the liquidus temperature of a silver and silicon eutectic alloy being about 837° C. Brazing alloys in accordance with the invention are useful in bonding ceramics to ceramics, ceramics to metals, and metals to metals. Copper, vanadium, or other oxygen-reactive surface bonding elements may also be included. Silver/silicon alloys are useful in applications such as assembly of components of solid oxide fuel cells. A variety of silver/silicon alloy brazes can be used within the same fuel cell so that subsequent brazing can be performed without reliquifying a previous braze. A brazing alloy comprising elemental silver and ruthenium in a silver/ruthenium ratio between 97/3 and 99/1 is also included.
Description
- This invention was made with United States Government support under Government Contract/Purchase Order No. DE-FC26-02NT41246. The Government has certain rights in this invention
- The present invention relates to alloys for joining materials by brazing; more particularly, to silver-containing braze alloys for joining ceramics to metals; and most particularly, to silver braze alloys containing silicon to lower the liquidus temperature.
- Fuel cells which generate electric current by controllably combining elemental hydrogen and oxygen are well known. In one form of such a fuel cell, an anodic layer and a cathodic layer are separated by a permeable electrolyte formed of a ceramic solid oxide, such as yttrium-stabilized zirconium (YSZ). Such a fuel cell is known in the art as a “solid oxide fuel cell” (SOFC). A single cell is capable of generating a relatively small voltage and wattage, typically between about 0.5 volt and about 1.0 volt, depending upon load, and less than about 2 watts per cm2 of cell surface. Therefore, in practice it is known to stack together, in electrical series, a plurality of cells.
- In a currently-preferred arrangement, each ceramic-based fuel cell is bonded to a surrounding metal “cassette” frame to form a fuel cell sub-assembly, using a silver/copper-based braze. As the solid braze alloy is liquefied, the copper is rapidly oxidized to form copper oxide which separates from the alloy, leaving essentially pure silver as the brazing material. The copper oxide migrates to the boundaries of the liquid and adheres to the ceramic and the metal, providing an attachment layer for the silver. Exemplary silver/copper and silver/vanadium braze alloys are disclosed in International Publication No. WO 03/059843, published 24 Jul. 2003, which is incorporated herein by reference.
- A problem in the use of such alloys is that the liquidus temperature is substantially the melting point of pure silver, 962° C. This temperature is high enough to preclude use of some fuel cell materials which can be damaged by such high temperatures. In addition, in some manufacturing schemes it is desirable to perform two separate brazing steps, and it is further desirable that the first brazed seal not be reliquefied when performing the second seal. Thus, a higher temperature braze could be used for the first seal, and a lower temperature braze for the second seal.
- What is needed in the art is a means for lowering the liquidus temperature of a silver brazing alloy.
- It is a principal object of the present invention to provide an improved silver brazing alloy having a liquidus temperature significantly lower than the melting temperature of silver.
- Briefly described, a brazing alloy in accordance with the invention comprises elemental silver alloyed with another element that serves to reduce the liquidus temperature of the alloy to a temperature below the melting point of silver. In a preferred embodiment, a brazing alloy comprises elemental silver alloyed with elemental silicon in a silver/silicon ratio between about 95/5 and 99/1, preferably about 97/3. Silver melts at 962° C., but small amounts of silicon alloyed with silver depress the alloy liquidus point significantly, the liquidus temperature of a silver and silicon eutectic alloy being about 837° C. Brazing alloys in accordance with the invention are useful in bonding ceramics to ceramics, ceramics to metals, and metals to metals. Such metals are preferably alumina-forming. Copper, vanadium, or other oxygen-reactive surface bonding elements may also be included, and use of such brazing alloys is preferably carried out in an oxidizing atmosphere.
- The present invention will now be described, by way of example, with reference to the accompanying drawings, in which:
-
FIG. 1 is a silver/silicon phase diagram; and -
FIG. 2 is a cross-sectional view of a portion of a fuel cell, showing bonding of a ceramic component to a metal component by a braze alloy in accordance with the invention; -
FIG. 3 is a cross-sectional view of a portion of a fuel cell, similar to that shown inFIG. 2 , but showing a second braze alloy having a different liquidus temperature; and -
FIG. 4 is a silver/ruthenium phase diagram. - Referring to
FIG. 1 , a phase diagram 10 for silver and silicon alloy mixtures is conventionally displayed, having temperature on the vertical axis as a function of weight percent silicon on the horizontal axis. The solidus/liquidus curve 12 for alloys of silver and silicon extends from pure silver (MP of about 962° C.) to pure silicon (MP 1414° C.). Addition of relatively small amounts of silicon to pure silver serves to depress the alloy liquidus temperature significantly; aeutectic point 14 of about 835° C. exists at a silver/silicon ratio of about 97/3. Useful liquidus temperature depressions below the 962° C. melting temperature of silver exist up to about 5% silicon. - Referring to
FIG. 4 , a phase diagram 10′ for silver and ruthenium alloy mixtures of a second embodiment, including solidus/liquidus curve 12′ andeutectic point 14′, is shown. In a silver/ruthenium ratio between about 96/4 and 99/1, preferably about 97/3, a liquidus temperature of about 920° C. is achieved. Thus, the addition of relatively small amounts of ruthenium to pure silver similarly serves to depress the alloy liquidus temperature below the melting point of pure silver. - Referring to
FIG. 2 , in a solid-oxidefuel cell assembly 16, a ceramic-basedfuel cell element 18 is bonded to ametal cassette 20 by a braze seal formed of a silver/silicon braze alloy 22 in accordance with the invention. Preferably, the braze alloy includes either copper or vanadium which is readily oxidized to form CuO or V2O5 during fusion of the alloy in an oxidizing atmosphere. The oxides separate from the alloy in known fashion and provide anadhesion layer 24 onelement 18 andcassette 20 for attachment of the remaining silver/silicon alloy 26. - Referring to
FIG. 3 , it can be seen how the use of two or more different silver/silicon braze alloys can be used so that a additional brazed seals can be formed without re-liquefying the already formed brazed seals. As shown,fuel cell element 18 is bonded to a second element, such ascassette 20, by a braze seal formed of a silver/silicon braze alloy 22 having a liquidus temperature of less than 962° C., as described above.Third element 18′ can then be bonded to element 20 (or any other element in the fuel cell assembly) using a silver/silicon braze alloy 22′ having a different weight percentage concentration of silicon and having a liquidus temperature lower than the melting temperature ofalloy 22. - While the invention as described above concerns a reactive air brazing alloy, it is understood that he braze alloy can be made from a mix of the elemental powders which would then be allowed to alloy during the brazing process.
- While the invention has been described by reference to various specific embodiments, it should be understood that numerous changes may be made within the spirit and scope of the inventive concepts described. Accordingly, it is intended that the invention not be limited to the described embodiments, but will have full scope defined by the language of the following claims.
Claims (18)
1-8. (canceled)
9. A fuel cell assembly comprising a first component and a second component wherein said first and second components are bonded by a brazing alloy consisting essentially of silver and silicon, wherein said alloy has a liquidus temperature of less than 962° C.
10. A fuel cell assembly in accordance with claim 9 wherein the weight percent ratio of said silver to said silicon is between about 99/1 and about 95/5.
11. A fuel cell assembly in accordance with claim 23 wherein the weight percent ratio of said silver to said ruthenium is between about 99/1 and about 97/3.
12. A fuel cell assembly in accordance with claim 9 wherein at least one of said first and second components is a ceramic component.
13. A fuel cell assembly in accordance with claim 9 wherein at least one of said first and second components is a metal component.
14. A fuel cell assembly in accordance with claim 9 wherein said brazing alloy is a first brazing alloy, said fuel assembly further comprising an additional element wherein said additional element is bonded to one of said first element, second element and another element by a second brazing alloy having a liquidus temperature less than said liquidus temperature of said first brazing compound.
15. A fuel cell assembly in accordance with claim 9 wherein said assembly comprises a solid oxide fuel cell.
16-18. (canceled)
19-21. (not entered)
22. A fuel cell assembly in accordance with claim 10 wherein said liquidus temperature is about 835° C.
23. A fuel cell assembly comprising a first component and a second component wherein said first and second components are bonded by a brazing alloy consisting essentially of silver and ruthenium, wherein said alloy has a liquidus temperature of less than 962° C.
24. A fuel cell assembly in accordance with claim 23 wherein at least one of said first and second components is a ceramic component.
25. A fuel cell assembly in accordance with claim 23 wherein at least one of said first and second components is a metal component.
26. A fuel cell assembly in accordance with claim 23 wherein said brazing alloy is a first brazing alloy, said fuel assembly further comprising an additional element wherein said additional element is bonded to one of said first element, second element and another element by a second brazing alloy having a liquidus temperature less than said liquidus temperature of said first brazing compound.
27. A fuel cell assembly in accordance with claim 23 wherein said assembly comprises a solid oxide fuel cell.
28. A fuel cell assembly in accordance with claim 11 wherein said liquidus temperature is about 920° C.
29. A fuel cell assembly comprising a first component and a second component wherein said first and second components are bonded by a brazing alloy consisting essentially of silver, silicon, and a third elemental component selected from the group consisting of copper and vanadium, and wherein said alloy has a liquidus temperature of less than 962° C.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
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US10/929,819 US20060045791A1 (en) | 2004-08-30 | 2004-08-30 | Low melting temperature silver braze alloy |
EP05076961A EP1629936A1 (en) | 2004-08-30 | 2005-08-25 | Low melting temperature silver braze alloy |
Applications Claiming Priority (1)
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US10/929,819 US20060045791A1 (en) | 2004-08-30 | 2004-08-30 | Low melting temperature silver braze alloy |
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US20060045791A1 true US20060045791A1 (en) | 2006-03-02 |
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US10/929,819 Abandoned US20060045791A1 (en) | 2004-08-30 | 2004-08-30 | Low melting temperature silver braze alloy |
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US (1) | US20060045791A1 (en) |
EP (1) | EP1629936A1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20100218875A1 (en) * | 2007-06-11 | 2010-09-02 | Battelle Memorial Institute | Diffusion barriers in modified air brazes |
JP2015052139A (en) * | 2013-09-06 | 2015-03-19 | 日本特殊陶業株式会社 | Alloys and brazing materials |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102004047539A1 (en) | 2004-09-30 | 2006-04-06 | Elringklinger Ag | A fuel cell stack seal assembly and method of making a fuel cell stack |
US20080217382A1 (en) * | 2007-03-07 | 2008-09-11 | Battelle Memorial Institute | Metal-ceramic composite air braze with ceramic particulate |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4053728A (en) * | 1975-10-24 | 1977-10-11 | General Electric Company | Brazed joint between a beryllium-base part and a part primarily of a metal that is retractable with beryllium to form a brittle intermetallic compound |
US5330098A (en) * | 1988-11-07 | 1994-07-19 | The Morgan Crucible Co., Plc | Silver-copper-aluminum-titanium brazing alloy |
US5340658A (en) * | 1991-08-21 | 1994-08-23 | Ishihara Chemical Co., Ltd. | Composites made of carbon-based and metallic materials |
US6413649B2 (en) * | 1998-03-06 | 2002-07-02 | The Morgan Crucible Company Plc | Silver-copper-nickel infiltration brazing filler metal and composites made therefrom |
US20040155096A1 (en) * | 2003-02-07 | 2004-08-12 | General Electric Company | Diamond tool inserts pre-fixed with braze alloys and methods to manufacture thereof |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5865597A (en) * | 1981-10-15 | 1983-04-19 | Mitsubishi Metal Corp | Ag alloy brazing material with excellent surface quality for the brazed part |
US7055733B2 (en) * | 2002-01-11 | 2006-06-06 | Battelle Memorial Institute | Oxidation ceramic to metal braze seals for applications in high temperature electrochemical devices and method of making |
-
2004
- 2004-08-30 US US10/929,819 patent/US20060045791A1/en not_active Abandoned
-
2005
- 2005-08-25 EP EP05076961A patent/EP1629936A1/en not_active Withdrawn
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4053728A (en) * | 1975-10-24 | 1977-10-11 | General Electric Company | Brazed joint between a beryllium-base part and a part primarily of a metal that is retractable with beryllium to form a brittle intermetallic compound |
US5330098A (en) * | 1988-11-07 | 1994-07-19 | The Morgan Crucible Co., Plc | Silver-copper-aluminum-titanium brazing alloy |
US5340658A (en) * | 1991-08-21 | 1994-08-23 | Ishihara Chemical Co., Ltd. | Composites made of carbon-based and metallic materials |
US6413649B2 (en) * | 1998-03-06 | 2002-07-02 | The Morgan Crucible Company Plc | Silver-copper-nickel infiltration brazing filler metal and composites made therefrom |
US20040155096A1 (en) * | 2003-02-07 | 2004-08-12 | General Electric Company | Diamond tool inserts pre-fixed with braze alloys and methods to manufacture thereof |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20100218875A1 (en) * | 2007-06-11 | 2010-09-02 | Battelle Memorial Institute | Diffusion barriers in modified air brazes |
US8424747B2 (en) * | 2007-06-11 | 2013-04-23 | Battelle Memorial Institute | Diffusion barriers in modified air brazes |
KR101466417B1 (en) * | 2007-06-11 | 2014-11-28 | 바텔리 메모리얼 인스티튜트 | Diffusion barriers in modified air brazes |
JP2015052139A (en) * | 2013-09-06 | 2015-03-19 | 日本特殊陶業株式会社 | Alloys and brazing materials |
Also Published As
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