EP1827670A1 - Keramik-metall- oder metalllegierungsverbindungsanordnung - Google Patents
Keramik-metall- oder metalllegierungsverbindungsanordnungInfo
- Publication number
- EP1827670A1 EP1827670A1 EP05825170A EP05825170A EP1827670A1 EP 1827670 A1 EP1827670 A1 EP 1827670A1 EP 05825170 A EP05825170 A EP 05825170A EP 05825170 A EP05825170 A EP 05825170A EP 1827670 A1 EP1827670 A1 EP 1827670A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- junction
- metal
- zone
- ceramic
- temperature
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
- 229910052751 metal Inorganic materials 0.000 title claims abstract description 61
- 239000002184 metal Substances 0.000 title claims abstract description 61
- 229910001092 metal group alloy Inorganic materials 0.000 title claims description 43
- 239000000919 ceramic Substances 0.000 claims abstract description 81
- 239000000463 material Substances 0.000 claims abstract description 40
- 238000004519 manufacturing process Methods 0.000 claims abstract description 18
- 238000000926 separation method Methods 0.000 claims abstract description 4
- 239000011521 glass Substances 0.000 claims description 49
- 239000012530 fluid Substances 0.000 claims description 19
- 239000007789 gas Substances 0.000 claims description 13
- 238000010438 heat treatment Methods 0.000 claims description 9
- 238000000034 method Methods 0.000 claims description 9
- 230000006641 stabilisation Effects 0.000 claims description 9
- 238000011105 stabilization Methods 0.000 claims description 9
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 8
- 239000000126 substance Substances 0.000 claims description 8
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 7
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 7
- 230000015572 biosynthetic process Effects 0.000 claims description 7
- 239000001301 oxygen Substances 0.000 claims description 7
- 229910052760 oxygen Inorganic materials 0.000 claims description 7
- 239000007787 solid Substances 0.000 claims description 7
- 230000003647 oxidation Effects 0.000 claims description 6
- 238000007254 oxidation reaction Methods 0.000 claims description 6
- 230000001590 oxidative effect Effects 0.000 claims description 6
- 239000002243 precursor Substances 0.000 claims description 6
- 239000013078 crystal Substances 0.000 claims description 5
- 238000002844 melting Methods 0.000 claims description 5
- 230000008018 melting Effects 0.000 claims description 5
- 239000010416 ion conductor Substances 0.000 claims description 4
- 230000009467 reduction Effects 0.000 claims description 4
- 229910052804 chromium Inorganic materials 0.000 claims description 3
- 239000011651 chromium Substances 0.000 claims description 3
- 238000000280 densification Methods 0.000 claims description 3
- 229910052759 nickel Inorganic materials 0.000 claims description 3
- 229910052757 nitrogen Inorganic materials 0.000 claims description 3
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 2
- 229910000420 cerium oxide Inorganic materials 0.000 claims description 2
- DRVWBEJJZZTIGJ-UHFFFAOYSA-N cerium(3+);oxygen(2-) Chemical class [O-2].[O-2].[O-2].[Ce+3].[Ce+3] DRVWBEJJZZTIGJ-UHFFFAOYSA-N 0.000 claims description 2
- 239000011532 electronic conductor Substances 0.000 claims description 2
- 239000011261 inert gas Substances 0.000 claims description 2
- 229910044991 metal oxide Inorganic materials 0.000 claims description 2
- 150000004706 metal oxides Chemical class 0.000 claims description 2
- 238000003825 pressing Methods 0.000 claims description 2
- 238000005245 sintering Methods 0.000 claims description 2
- 238000005266 casting Methods 0.000 claims 1
- 238000007789 sealing Methods 0.000 abstract description 3
- 238000005304 joining Methods 0.000 description 15
- 229910045601 alloy Inorganic materials 0.000 description 14
- 239000000956 alloy Substances 0.000 description 14
- 239000000203 mixture Substances 0.000 description 13
- 230000035882 stress Effects 0.000 description 7
- 239000000843 powder Substances 0.000 description 6
- 238000013459 approach Methods 0.000 description 5
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 5
- 239000012528 membrane Substances 0.000 description 4
- 230000008901 benefit Effects 0.000 description 3
- 238000006243 chemical reaction Methods 0.000 description 3
- 238000001816 cooling Methods 0.000 description 3
- 238000002425 crystallisation Methods 0.000 description 3
- 230000008025 crystallization Effects 0.000 description 3
- 238000013461 design Methods 0.000 description 3
- 238000009472 formulation Methods 0.000 description 3
- 230000006872 improvement Effects 0.000 description 3
- 238000002360 preparation method Methods 0.000 description 3
- 238000003786 synthesis reaction Methods 0.000 description 3
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 2
- 239000011324 bead Substances 0.000 description 2
- 229910002091 carbon monoxide Inorganic materials 0.000 description 2
- 238000005238 degreasing Methods 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 239000000835 fiber Substances 0.000 description 2
- 238000011049 filling Methods 0.000 description 2
- 230000009477 glass transition Effects 0.000 description 2
- 239000006060 molten glass Substances 0.000 description 2
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical compound [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 description 2
- 238000007711 solidification Methods 0.000 description 2
- 230000008023 solidification Effects 0.000 description 2
- 230000003746 surface roughness Effects 0.000 description 2
- 230000008646 thermal stress Effects 0.000 description 2
- 238000003826 uniaxial pressing Methods 0.000 description 2
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 description 1
- 206010021143 Hypoxia Diseases 0.000 description 1
- 229910000502 Li-aluminosilicate Inorganic materials 0.000 description 1
- 101100438470 Trichosurus vulpecula CSN2 gene Proteins 0.000 description 1
- FQNGWRSKYZLJDK-UHFFFAOYSA-N [Ca].[Ba] Chemical compound [Ca].[Ba] FQNGWRSKYZLJDK-UHFFFAOYSA-N 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 229910000323 aluminium silicate Inorganic materials 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 238000004873 anchoring Methods 0.000 description 1
- 238000000137 annealing Methods 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 229910052788 barium Inorganic materials 0.000 description 1
- DSAJWYNOEDNPEQ-UHFFFAOYSA-N barium atom Chemical compound [Ba] DSAJWYNOEDNPEQ-UHFFFAOYSA-N 0.000 description 1
- 235000012215 calcium aluminium silicate Nutrition 0.000 description 1
- 239000000404 calcium aluminium silicate Substances 0.000 description 1
- 229940078583 calcium aluminosilicate Drugs 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 230000003197 catalytic effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000003153 chemical reaction reagent Substances 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000010411 cooking Methods 0.000 description 1
- 229910052593 corundum Inorganic materials 0.000 description 1
- 239000010431 corundum Substances 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 229910001873 dinitrogen Inorganic materials 0.000 description 1
- HNPSIPDUKPIQMN-UHFFFAOYSA-N dioxosilane;oxo(oxoalumanyloxy)alumane Chemical compound O=[Si]=O.O=[Al]O[Al]=O HNPSIPDUKPIQMN-UHFFFAOYSA-N 0.000 description 1
- 229910001882 dioxygen Inorganic materials 0.000 description 1
- 238000004090 dissolution Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 229910001026 inconel Inorganic materials 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 150000002500 ions Chemical class 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 229910052746 lanthanum Inorganic materials 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 229910052697 platinum Inorganic materials 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 230000009257 reactivity Effects 0.000 description 1
- 239000011819 refractory material Substances 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 238000005488 sandblasting Methods 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 238000010583 slow cooling Methods 0.000 description 1
- 238000003892 spreading Methods 0.000 description 1
- 230000007480 spreading Effects 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 238000002411 thermogravimetry Methods 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 238000002604 ultrasonography Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Chemical compound O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
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- 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
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/01—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics
- C04B35/26—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on ferrites
- C04B35/2641—Compositions containing one or more ferrites of the group comprising rare earth metals and one or more ferrites of the group comprising alkali metals, alkaline earth metals or lead
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
- B01D53/00—Separation of gases or vapours; Recovering vapours of volatile solvents from gases; Chemical or biological purification of waste gases, e.g. engine exhaust gases, smoke, fumes, flue gases, aerosols
- B01D53/34—Chemical or biological purification of waste gases
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01J—CHEMICAL OR PHYSICAL PROCESSES, e.g. CATALYSIS OR COLLOID CHEMISTRY; THEIR RELEVANT APPARATUS
- B01J19/00—Chemical, physical or physico-chemical processes in general; Their relevant apparatus
- B01J19/24—Stationary reactors without moving elements inside
- B01J19/2475—Membrane reactors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01J—CHEMICAL OR PHYSICAL PROCESSES, e.g. CATALYSIS OR COLLOID CHEMISTRY; THEIR RELEVANT APPARATUS
- B01J4/00—Feed or outlet devices; Feed or outlet control devices
- B01J4/001—Feed or outlet devices as such, e.g. feeding tubes
-
- C—CHEMISTRY; METALLURGY
- C01—INORGANIC CHEMISTRY
- C01B—NON-METALLIC ELEMENTS; COMPOUNDS THEREOF; METALLOIDS OR COMPOUNDS THEREOF NOT COVERED BY SUBCLASS C01C
- C01B13/00—Oxygen; Ozone; Oxides or hydroxides in general
- C01B13/02—Preparation of oxygen
- C01B13/0229—Purification or separation processes
- C01B13/0248—Physical processing only
- C01B13/0251—Physical processing only by making use of membranes
- C01B13/0255—Physical processing only by making use of membranes characterised by the type of membrane
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- C—CHEMISTRY; METALLURGY
- C01—INORGANIC CHEMISTRY
- C01B—NON-METALLIC ELEMENTS; COMPOUNDS THEREOF; METALLOIDS OR COMPOUNDS THEREOF NOT COVERED BY SUBCLASS C01C
- C01B21/00—Nitrogen; Compounds thereof
- C01B21/04—Purification or separation of nitrogen
- C01B21/0405—Purification or separation processes
- C01B21/0433—Physical processing only
- C01B21/0438—Physical processing only by making use of membranes
- C01B21/0444—Physical processing only by making use of membranes characterised by the membrane
-
- C—CHEMISTRY; METALLURGY
- C01—INORGANIC CHEMISTRY
- C01B—NON-METALLIC ELEMENTS; COMPOUNDS THEREOF; METALLOIDS OR COMPOUNDS THEREOF NOT COVERED BY SUBCLASS C01C
- C01B3/00—Hydrogen; Gaseous mixtures containing hydrogen; Separation of hydrogen from mixtures containing it; Purification of hydrogen
- C01B3/02—Production of hydrogen or of gaseous mixtures containing a substantial proportion of hydrogen
- C01B3/32—Production of hydrogen or of gaseous mixtures containing a substantial proportion of hydrogen by reaction of gaseous or liquid organic compounds with gasifying agents, e.g. water, carbon dioxide, air
- C01B3/34—Production of hydrogen or of gaseous mixtures containing a substantial proportion of hydrogen by reaction of gaseous or liquid organic compounds with gasifying agents, e.g. water, carbon dioxide, air by reaction of hydrocarbons with gasifying agents
- C01B3/36—Production of hydrogen or of gaseous mixtures containing a substantial proportion of hydrogen by reaction of gaseous or liquid organic compounds with gasifying agents, e.g. water, carbon dioxide, air by reaction of hydrocarbons with gasifying agents using oxygen or mixtures containing oxygen as gasifying agents
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
- C03C8/00—Enamels; Glazes; Fusion seal compositions being frit compositions having non-frit additions
- C03C8/24—Fusion seal compositions being frit compositions having non-frit additions, i.e. for use as seals between dissimilar materials, e.g. glass and metal; Glass solders
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- 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
- C04B37/025—Joining burned ceramic articles with other burned ceramic articles or other articles by heating with metallic articles characterised by the interlayer used consisting of glass or ceramic material
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2311/00—Metals, their alloys or their compounds
- B32B2311/22—Nickel or cobalt
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- C—CHEMISTRY; METALLURGY
- C01—INORGANIC CHEMISTRY
- C01B—NON-METALLIC ELEMENTS; COMPOUNDS THEREOF; METALLOIDS OR COMPOUNDS THEREOF NOT COVERED BY SUBCLASS C01C
- C01B2203/00—Integrated processes for the production of hydrogen or synthesis gas
- C01B2203/02—Processes for making hydrogen or synthesis gas
- C01B2203/025—Processes for making hydrogen or synthesis gas containing a partial oxidation step
- C01B2203/0255—Processes for making hydrogen or synthesis gas containing a partial oxidation step containing a non-catalytic partial oxidation step
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- C—CHEMISTRY; METALLURGY
- C01—INORGANIC CHEMISTRY
- C01B—NON-METALLIC ELEMENTS; COMPOUNDS THEREOF; METALLOIDS OR COMPOUNDS THEREOF NOT COVERED BY SUBCLASS C01C
- C01B2203/00—Integrated processes for the production of hydrogen or synthesis gas
- C01B2203/12—Feeding the process for making hydrogen or synthesis gas
- C01B2203/1205—Composition of the feed
- C01B2203/1211—Organic compounds or organic mixtures used in the process for making hydrogen or synthesis gas
- C01B2203/1235—Hydrocarbons
- C01B2203/1241—Natural gas or methane
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- C—CHEMISTRY; METALLURGY
- C01—INORGANIC CHEMISTRY
- C01B—NON-METALLIC ELEMENTS; COMPOUNDS THEREOF; METALLOIDS OR COMPOUNDS THEREOF NOT COVERED BY SUBCLASS C01C
- C01B2210/00—Purification or separation of specific gases
- C01B2210/0043—Impurity removed
- C01B2210/0046—Nitrogen
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- 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
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/32—Metal oxides, mixed metal oxides, or oxide-forming salts thereof, e.g. carbonates, nitrates, (oxy)hydroxides, chlorides
- C04B2235/3205—Alkaline earth oxides or oxide forming salts thereof, e.g. beryllium oxide
- C04B2235/3213—Strontium oxides or oxide-forming salts thereof
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- 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
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/32—Metal oxides, mixed metal oxides, or oxide-forming salts thereof, e.g. carbonates, nitrates, (oxy)hydroxides, chlorides
- C04B2235/3224—Rare earth oxide or oxide forming salts thereof, e.g. scandium oxide
- C04B2235/3227—Lanthanum oxide or oxide-forming salts thereof
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- 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
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/32—Metal oxides, mixed metal oxides, or oxide-forming salts thereof, e.g. carbonates, nitrates, (oxy)hydroxides, chlorides
- C04B2235/3231—Refractory metal oxides, their mixed metal oxides, or oxide-forming salts thereof
- C04B2235/3232—Titanium oxides or titanates, e.g. rutile or anatase
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- 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
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/32—Metal oxides, mixed metal oxides, or oxide-forming salts thereof, e.g. carbonates, nitrates, (oxy)hydroxides, chlorides
- C04B2235/3286—Gallium oxides, gallates, indium oxides, indates, thallium oxides, thallates or oxide forming salts thereof, e.g. zinc gallate
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- 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
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/70—Aspects relating to sintered or melt-casted ceramic products
- C04B2235/74—Physical characteristics
- C04B2235/77—Density
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- 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
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/70—Aspects relating to sintered or melt-casted ceramic products
- C04B2235/96—Properties of ceramic products, e.g. mechanical properties such as strength, toughness, wear resistance
- C04B2235/9607—Thermal properties, e.g. thermal expansion coefficient
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- 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
- C04B2237/10—Glass interlayers, e.g. frit or flux
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- 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
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/34—Oxidic
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- 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
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/40—Metallic
- C04B2237/405—Iron metal group, e.g. Co or Ni
Definitions
- the invention relates to a ceramic-metal junction assembly comprising a ceramic part, a piece of metal or metal alloy and a ceramic - metal or metal alloy junction element which provides a junction between the two parts, as well as a reactor having such a junction assembly.
- ceramic membrane metal reactors such as a CMR (membrane catalytic reactor), for example for the production or separation of gases
- CMR membrane catalytic reactor
- Such reactors generally comprise within them a ceramic part or membrane, which is usually in the form of a substantially hollow tube closed at one of its ends and open at the other end, which partially envelops an inner zone.
- the two atmospheres are thus present in said reactor, do not communicate directly with each other and are separated by the ceramic part.
- At least one exchange which is often gaseous, selective, takes place between the two atmospheres via and through the ceramic part, and may give rise to at least one reaction on one side or the other of said ceramic piece.
- the tube is most often held in place in the reactor via a piece of metal or metal alloy, generally of the same metal or metal alloy as said wall of the reactor. said piece may belong to said wall or may simply be attached to said wall.
- the most critical parameters are the coefficient of thermal expansion (CET) and the chemical and physical stability of the material. Indeed, in a temperature range from room temperature to a high temperature, it is essential to take into account factors such as the possible evaporation of component (s) of said material, the evolution of the TEC and / or the eventual crystallization of component ( s) of said material. In this respect, partially or fully crystallized materials offer more extensive possibilities, especially in terms of the evolution of the thermal expansion coefficient as a function of the temperature, and of the high temperature stability time.
- a first approach consisted in crystallizing glass to better adapt its properties, which led to the development of specific glasses of the Lithium AluminoSilicate or LAS type (US4921738), Barium AluminoSilicate or BAS (US6430966) or Barium calcium AluminoSilicate or BCAS . These compositions have a good refractoriness and a CET greater than those of conventional uncrystallized compositions. Unfortunately, they have too much chemical reactivity with ceramics.
- a second approach has been to add a crystallized phase in a glass in order to increase the CET or to use a crystallizable glass, for example in the form of powder or preform (US5725218, US6402156).
- a crystallizable glass for example in the form of powder or preform (US5725218, US6402156).
- US5725218, US6402156 the multiplication of the interfaces created by the presence of several phases in the joining material increases the possibilities of leaks and therefore loss of sealing of the junction assembly.
- a first approach consisted in compressing a joining element consisting of a deformable junction material, said element being pressed against the metal or metal alloy part and on the ceramic piece.
- the junction material is generally a fluid phase such as for example glass. It then adapts to the shape of said parts. It can then undergo compression forces that allow it to ensure good contact with said parts at its interfaces with them.
- EP-A-1 067 320 discloses a junction element formed of at least one metal toroidal ring, said ring being able to deform. Such a joining element therefore makes it possible to maintain a pressure at the interfaces between the connecting element and the metal or alloy part. metal and the aforementioned ceramic part. Such a joining element makes it possible above all to limit the radial stresses which are exerted on the ceramic part during thermal cycles, since the ring is formed by a metal sheet whose thickness is much smaller than the width of the ring. .
- a fluid phase in particular glass
- This fluid phase poses a problem of stiffening the junction at temperatures where said phase is not fluid, in particular at temperatures ranging from room temperature (approximately 20 ° C.) to the softening temperature of said phase.
- the junction assembly according to the invention overcomes the problems described above, and to provide other advantages.
- One of the objects of the invention is to propose a junction assembly which makes it possible to limit the stresses exerted on the ceramic part, in particular during thermal cycles varying between the ambient temperature and a high temperature.
- the invention relates to a ceramic-metal junction assembly, said assembly comprising: 1) at least one ceramic piece in the form of a hollow tube and substantially cylindrical axis (X'X), closed to one of its ends and open at the other end, defining an inner zone called ceramic zone and an outer zone called metal zone, said ceramic and metallic zones not communicating with each other and being separated at least partially by the ceramic part, at least partially sheathed by
- junction zone substantially cylindrical and hollow axis (X'X) at least partially enveloping said tube, a substantially annular axis space ( X'X) being provided between said tube and said junction zone,
- the seal between said tube and said sleeve being provided by at least one ceramic-metal junction element which is in contact with the tube and with said junction zone of the socket, the junction element being at least partially present in said annular space occupying a subspace (4a) and preferably in the form of a substantially annular piece,
- said ceramic having a coefficient of thermal expansion (CET) greater than or equal to the coefficient of thermal expansion (TEC) of the metal or metal alloy, said metal alloy comprising at least 10% by weight of nickel and at least 15% by weight of chromium,
- Said connecting element comprising at least one joining material, preferably consisting of said joining material, ensuring gas tightness of 20-900 0 C, preferably being solid at a temperature of 650 to 900 0 C, and having a coefficient of thermal expansion (CET) of the ambient temperature at 900 ° C. greater than or equal to 9.times.10.sup.- 6 / ° C., preferably from 9 to 15.times.10.sup.- 6 / 0.degree. C., said joining assembly being such that said zone junction has a small dimension, along any axis (Y'Y) passing through said junction area and perpendicular to the axis (X'X).
- the dimension ratio along the axis (X'X) of the junction zone to the subspace is at least equal to 2/1, and is preferably in the range of 2/1 to 100/1.
- the ratio of dimensions along the axis (X'X) of the junction zone to the subspace is the ratio of the mean dimension along the axis (X'X) of the junction zone to the average dimension according to the axis (X'X) of the subspace.
- said dimension is the height of the ring.
- the combination of the properties of the joining material and the possibilities of deformation of the socket makes it possible to have a junction assembly which provides improvements over the junction assemblies of the prior art.
- improvements are mainly expressed in terms of the chemical and physical stability of the junction assembly, the limitation of the stresses exerted on the ceramic tube, the achievement of a gaseous seal from ambient temperature to high temperature, and improvement of the resistance of the junction assembly to thermal cycles ranging from ambient temperature to high temperature.
- the presence of a junction zone of small size of the sleeve advantageously provides according to the invention possibilities of deformation of said sleeve.
- Such deformations limit the stresses exerted on the ceramic tube, in particular in the temperature range from ambient temperature (about 20 ° C.) to high temperature.
- gas-tightness of 20 to 900 ° C.” is meant according to the invention that no leakage (s) of gas from 20 to 900 ° C. occurs.
- solid at a temperature of 600 to 900 ° C.” is meant according to the invention that the viscosity is greater than 12 mPa.s for a glass and that said temperature is below the melting temperature for a crystal.
- said joining material is solid at the temperature (s) of use of said assembly.
- the "coefficient of thermal expansion (CET)" is a standard data for the skilled person.
- small dimension is meant according to the invention that the dimension is small and is in a range of size that can be easily found by the skilled person, depending on the given parameters such as the CET of the material of junction, and the shape of the socket.
- the minimum dimension is given by the machinability of the metal or metal alloy.
- An example of a small dimension will be given below in the examples.
- said small dimension is about 20 to 500 ⁇ m, preferably about 50 to 400 ⁇ m, more preferably about 200 to 300 ⁇ m.
- the ceramic tube is generally a ceramic membrane present inside a reactor.
- the bushing is generally such that it can be mechanically and tightly bonded, typically by screwing, welding or any other method of tight assembly known to those skilled in the art, generally in a manner, fixed or removable, to a such reactor, preferably a wall of a reactor.
- the ceramic is generally an ionic conductor, preferably an ionic and electronic conductor, said ceramic more preferably comprising at least one crystalline lattice comprising at least one oxygen deficiency, said ceramic being, even more preferably chosen from ceramics of perovskite crystal structure and cerium oxides.
- the ceramic is composed of a porous layer (located on the ZM side) and a dense layer (located on the ZC side) of respective Lao compositions, 5 Sr 0 ⁇ Fe O , 9 Ti 0 , i ⁇ 3 - ⁇ . Lao ⁇ Sro, 4Feo, GGAO, i ⁇ 3- ⁇ .
- the coefficient of thermal expansion (TEC) of the ceramic generally depends on its formulation. In general, it is from 9 to 20.10 "6/0 C.
- said metal or metal alloy comprises on one part of, preferably on all, the surface of said junction zone, at least one layer of at least one oxide typically of thickness greater than or equal to approximately 1 ⁇ m and preferably thickness less than or equal to about 10 ⁇ m.
- at least one layer of at least one oxide typically of thickness greater than or equal to approximately 1 ⁇ m and preferably thickness less than or equal to about 10 ⁇ m.
- the presence of such an oxide layer makes it possible to protect the metal or metal alloy during the manufacture of the junction assembly and, above all, ensures an adhesion function between the joining material and the metal or metal alloy. If this layer is too thin (typically less than or equal to about 1 micron), the adhesion of the junction between the joining material and the metal or metal alloy is difficult to achieve.
- this layer is too thick (typically greater than or equal to about 10 microns), it may flake during said manufacture, and therefore not to ensure adhesion role.
- the skilled person is able to establish a range of thicknesses and / or an optimum thickness of the layer according to the data available.
- the metal may be, for example, nickel or platinum.
- the metal alloy generally has the following properties: resistance to oxidation under an oxidizing atmosphere up to 1200 ° C., resistance to reduction under a reducing atmosphere up to 1200 ° C., resistance to creep up to 1200 ° C., a melting point greater than or equal to 1200 ° C., and a thermal expansion coefficient (TEC) of 20 ° C. at 900 ° C. of 8 ° to
- the alloy is generally selected from stainless steels which are for example commercial alloys such as Haynes 230® alloy, the alloy 800HT ® and Inconel 686®.
- said joining material is glass, which has a coefficient of thermal expansion (TEC) greater than the coefficient of thermal expansion (TEC) of the metal or metal alloy and lower than the coefficient of thermal expansion (CET ) ceramic, resistance to a pressure difference between the ceramic zone and the metal zone of between 0 and 3 MPa, chemical stability with respect to the ceramic, chemical stability with respect to the metal or of the metal alloy, resistance to reduction under a reducing atmosphere up to 1200 ° C., resistance to oxidation under an oxidizing atmosphere up to 1200 ° C., adhesion to the metal or metal alloy and adhesion to the metal. ceramic.
- TEC coefficient of thermal expansion
- CET coefficient of thermal expansion
- the ceramic tube is generally closed at one end by any shape such as square or hemispherical or any intermediate shape.
- the open end of the ceramic tube may be of a shape facilitating anchoring on / in the socket.
- the invention also relates to a method of manufacturing an assembly as described above, said method comprising the following successive steps: 1. At least partial preoxidation of a surface of a junction zone of a metal sleeve or metal alloy or a precursor thereof, so as to form at least partially at least one layer of at least one metal oxide on said surface;
- heat treatment of the assembly of step 2 under an inert gas such as nitrogen, under partial pressure of oxygen of between 0 and 22%, and at a temperature of 650 to 1200 ° C. for a period of 5 minutes. mn to 10 hours, comprising a rise in temperature from room temperature to a treatment temperature, at least one temperature step at the treatment temperature, at least one temperature decrease to a stabilization temperature, at least a stabilization plateau at the stabilization temperature, and at least one final descent to a treatment end temperature which is most often ambient temperature, said heat treatment leading to the formation of the connecting element within the junction assembly.
- an inert gas such as nitrogen
- temperature plateau is meant according to the invention that said temperature is generally maintained for a period of a few minutes to a few hours depending on the materials used.
- the treatment temperature can be fixed or vary within the indicated range.
- Said method may further comprise an additional step, which is performed between the preceding steps 1 and 2 or preceding the preceding step 1, said additional step being the following step: Manufacturing a junction material preform, in the form of a substantially cylindrical and hollow tube open at at least one of its ends, said manufacture comprising at least one pressing and a densification, or at least one sintering, or at least one minus a melting and pouring in a mold, at a temperature of 600 to
- the invention relates to a reactor, said reactor comprising at least a majority of said junction assembly according to the invention or manufactured according to a process according to the invention, said reactor surrounding the ZM zone, the metal sleeve or metal alloy of the junction assembly being mechanically connected to said reactor, and the axis (X'X) being disposed substantially vertically, said reactor comprising at least one fluid inlet in the zone ZM and at least one fluid outlet of the zone ZM, said reactor further comprising at least one fluid inlet in the zone ZC and at least one fluid outlet of the zone ZC.
- the reactor generally must withstand a pressure of from 1 to 30 bars (0.1 to 3 M.Pa), and at a temperature from room temperature to at least 900 0 C or even to 1200 0 C. In addition, it must consist of at least one metal or metal alloy that is resistant to a generally reducing atmosphere.
- a selective passage of fluid within said reactor is possible between the zone ZC and the zone ZM through the ceramic tube, preferably from the zone ZC to the zone ZM.
- the junction assembly is linked mechanically to a wall of said reactor.
- said fluid is gaseous and comprises at least one gaseous component.
- Such a reactor is generally such that at least one of its walls is metallic, most often of the same metal or metal alloy as said sleeve, or of a metal or metal alloy that is chemically compatible with the metal or metal alloy. of the socket.
- the invention finally relates to a method of using said reactor for the production of gas and / or the separation of gas, at a use temperature of 400 ° C. to 900 ° C., said joining assembly being such that the junction is solid at the temperature to which it is subjected during said use.
- the use temperature is less than or equal to the softening temperature of the glass when the joining material is glass.
- said reactor can be used for the production of synthesis gas from methane and oxygen.
- the operating temperature may vary or be fixed in the range indicated above. Inside the reactor, the temperature can be distributed unevenly.
- FIG. 1 schematically represents a partial view of a reactor comprising, for the most part, within it a junction assembly according to the invention.
- FIG. 2 schematically represents a partial view of the junction assembly according to the invention of FIG. 1.
- FIG. 3 represents, in a particular example, the thermal cycle to which a junction assembly according to the invention is subjected during its manufacture.
- FIG. 1 schematically represents a partial view of a reactor 6 comprising, for the most part, a junction assembly 5 according to the invention.
- Said junction assembly 5 has been welded to the rim of an orifice 10 of a wall of said reactor 6.
- Said reactor 6 comprises a piece or socket made of metal or metal alloy 2, a ceramic part or tube 3, and a junction element 1 of substantially annular shape and installed in a substantially annular space 4 occupying a substantially annular subspace (4a) formed between the parts 2 and 3.
- Said junction assembly 5 and each of the parts 2, 3 and 1 which compose it are all substantially coaxial axis (X'X) substantially vertical.
- the inside of the reactor 6 is divided by the device into two zones ZM and ZC, which are physically separated mainly by the ceramic tube 3.
- the junction assembly delineates the zone ZC.
- the reactor 6 and the junction assembly delimit the zone ZM.
- the reactor 6 comprises a fluid inlet 7 in the zone ZM and a fluid outlet 8 of the zone ZM
- the reactor 6 also comprises a fluid inlet 9 in the zone ZC, which serves both at the inlet and at the fluid outlet 9 of the zone ZC.
- the arrows indicate the flow direction of the fluids, which are usually gases.
- synthesis gas mixture of hydrogen gas H 2 and carbon monoxide CO
- the air enters the zone ZC through the inlet 9, while methane gas supplies the zone ZM through the inlet 7.
- the zone ZM is under a pressure of 30 bar (3 MPa).
- O 2 oxygen passes through the junction assembly 5 through the wall of the ceramic tube 3.
- This passage is in the form of O 2 " ions, which pass through the ceramic by the O 2 vacancies present in its crystal lattice.
- the reaction CH4 + O 2 -> H 2 + CO can then take place, which leads to the production of a synthesis gas mixture which is discharged through the outlet 8.
- the hydrogen gas H 2 and carbon monoxide CO can be easily separated from each other by If necessary, the nitrogen gas N 2 remaining in zone ZC emerges via inlet 9.
- FIG. 2 schematically represents a partial view of the junction assembly according to the invention as represented in FIG. 1.
- the ceramic piece 3 is a cylindrical tube plugged at one end. It also delimits a ceramic zone ZC inside said tube 3 and an outer zone called metal zone ZM.
- the closed end 3b of the tube 3 has a hemispherical shape and is opposite the sleeve 2. This side is defined as the high side in the following description.
- the other end 3a of the tube 3 is open and is located inside the socket 2. This side is defined as the low side in the following description.
- the metal zone ZM and the ceramic zone ZC do not communicate directly with each other, but only through the wall of the ceramic tube 3.
- the sleeve 2 is substantially hollow.
- the outer diameter of the sleeve 2 is on this constant embodiment for the lower 2d and median 2f.
- junction zone 2b The thickness 1 of the junction zone 2b is the small dimension 1 according to the invention.
- the ceramic tube 3 is adjusted to the first recess and its lower portion 3a rests on the shoulder 2c.
- the wedging of the tube 3 on the sleeve 2 is performed through the shoulder 2a.
- junction zone 2b is of small dimension 1 along the axis (Y'Y).
- the joining element 1 is annular. On this realization, it occupies only a subspace 4a annular of the annular space 4.
- the height of the joining element 1 is less than the height L of the junction zone 2b.
- the insertion depth of the joining element 1 in the sleeve 2 is such that its upper part is substantially at the same level as the upper end of the sleeve 2.
- junction assembly 5 of the example is as shown in Figure 2.
- the dimensions of the different parts are as follows:
- Width 1 of the junction area 2b 0.25 mm
- the sleeve 2 thus defined is a part (or ring) made of an alloy which is Haynes 230®.
- Haynes 230® alloy is a good refractory material, which has been chosen for its refractoriness, resistance to high temperature oxidation and its TEC of 15.2.10 ⁇ 6 / ° C between room temperature and 800 0 C. Its composition is as follows (% by weight): Ni 57%, Cr 22%, Mo 2%, W 14%, Fe 3%, C 0.1%, Al 0.3%.
- the ceramic piece 3 is a ceramic tube 3 which is closed at one end 3b and which is composed on its entire wall with a porous layer (located on the
- the porous layer is thick
- the dimensions of the tube are:
- the joining material is glass and forms a joining element 1 in the form of a substantially annular piece or cord 1.
- This cord 1 is completely inserted in the space 4, occupying a subspace (4a) , the top of the cord (1) being located at the height of the junction zone 2b.
- Two different glasses were tested as a joining material.
- the dimensions of the joining element 1 are:
- the dimension ratio along the axis (X'X) of the junction zone 2b to the annular subspace 4a is equal to 5 / 2.5 or 2.
- the junction assembly 5 as defined above is produced according to the invention to ensure a gas-tight connection between the ceramic tube 3, and the sleeve 2 of metal or metal alloy, of cylindrical axis symmetry (X'X), and having a particular shape (a "design"), using a glass which is the joining material.
- a pressure differential between 0 and 30 bar is applied between the inside and the outside of the ceramic tube 3 and therefore between the two zones ZM and ZC on each side of the junction, the pressure being higher on the ZM side.
- the two atmospheres present respectively in the zones ZC and ZM thus separated are respectively one oxidizing and the other reducing.
- the maximum working temperature is here between 700 and 900 ° C., but the tightness must be ensured between the ambient temperature (approximately 20 ° C.) and the said maximum temperature of use.
- the first PVl tested glass is as described in US6430966; it crystallizes easily to form a phase of thermal expansion coefficient close to
- the second PV2 tested glass is a commercial glass
- Table 1 composition of PV1 and PV2 glasses (% by weight)
- the sleeve 2 Haynes 230® alloy is machined from a cylinder to obtain the sleeve 2 as shown in Figure 2 and as described above.
- This cylinder is characterized by a chamber constituting a junction zone (thickness), at and inside which is installed the glass bead 1 which is the connecting element 1.
- the deformation of the metal or of the metal alloy in this part advantageously makes it possible to limit the thermal stresses likely to be exerted on the ceramic, mainly because of the differences in coefficients of thermal expansion between the materials.
- the free space between the shoulder 2a and the glass bead 1 is preferably substantially completely filled with a filler material (not shown here) to hold the glass preform in position during the junction heat treatment.
- the machined bushing 2 first undergoes a cleaning and degreasing step to eliminate machining residues.
- the piece is immersed in a saponifying solution, the preparation protocol is as explained in Table 3, for 1 hour, with action of ultra sounds.
- the junction zone 2b of said sleeve 2 is sandblasted with corundum (Al2O 3 ) to develop the surface roughness promoting mechanical adhesion by penetration of the glass in the asperities.
- the measured roughness has an Ra of the order of 2.5 ⁇ m.
- Preoxidation The adhesion is further improved by the formation of an oxide layer on the surface of the alloy, in this case by exposure to air at 900 ° C. for 30 min. By partial dissolution of these oxides in the glass, a chemical continuity will be ensured at the glass / alloy interface.
- the thickness of the oxide layer must be large enough not to attack the socket 2 during the manufacturing process of the junction assembly, but not too important not to lead to its peeling.
- Thermogravimetric analysis made it possible to determine the optimal thermal cycle for the formation of such an oxide layer.
- the objective is to obtain a cord 1 of dense glass between the tube 3 and the sleeve 2.
- PVl glass PVl glass is in the form of crushed pieces which are pressed by uniaxial pressing and baking under air at 700 ° C. for 30 min and then densified in air at 0 ° C. for 15 minutes The compactness obtained is approximately 98% of the theoretical density.
- PV2 glass PV2 glass is in the form of powder
- Direct use in this form poses the following difficulties: volume decrease between packed powder and molten glass, fast flow of molten glass
- the shaping is carried out by uniaxial pressing of said powder and cooking in air at 700 0 C for 30 min.
- the preform corresponds to a section of inner diameter tube close to the outside diameter of the tube 3 and outside diameter close to the inside diameter of the sleeve 2.
- the compactness obtained after densification is about 98% of the theoretical density.
- the glass preform when present must particularly remain at the junction zone 2b of the sleeve 2.
- This filling makes it possible subsequently to maintain a glass preform in the junction zone 2b of the sleeve 2.
- a Nextel® type fiber (alumina) wrapped around the tube 3 to wedge it in the socket 2.
- the materials used for filling are typically MgO which is perfectly chemically inert and / or corundum and / or ceramic powder of the same ceramic as that constituting the tube 3, and / or Nextel® fiber.
- the objective of this heat treatment is to create the ceramic / glass and alloy / glass interfaces.
- This step must be carried out under an inert atmosphere such as a nitrogen (N 2 ) atmosphere, or under partial pressure of oxygen, in order not to modify the composition of the ceramic.
- N 2 nitrogen
- the temperature and the dwell time must be perfectly controlled to prevent collapse of the glass.
- the solidification of the glass can exert constraints. It is necessary to carry out a very slow descent, above the stabilization temperature (or temperature of tension). Below, the glass being solid and the constraints related to phase change and solidification being completely relaxed, the cooling rate can be faster.
- PVl glass PVl glass crystallizes easily in a CET structure close to 13.10 "6 / C
- the aim is to take advantage of its fluidity to set it up and create the interfaces, before crystallizing it to increase its CET (limitation of thermal stresses) and improve its stability at high temperature
- the study of the crystallization of PVl has shown that after 4 hours at 85O 0 C, the CET reaches a value of 12.8 ⁇ 10 -6 / ° C.
- An ATD analysis carried out under air and under N 2 shows the presence of two crystallization peaks, the first being at 875 ° C. and the second being at 1000 ° C.
- the heat treatment cycle therefore consists of a plateau at 115 ° C. for 15 minutes and then a plateau at 85O 0 C for 4 hours to crystallize the glass, followed by a descent to room temperature, at 2 ° C / min between 85O 0 C and 700 0 C, 1 ° C / min between 700 ° C and 45O 0 C then 20 ° C / min to 20 ° C. • PV2 glass
- the approach is slightly different from that of PVl glass.
- the goal is to get the glass spread to create the ceramic / glass and alloy / glass interfaces.
- the viscosity curve of PV2 glass is known. Its softening temperature is at 715 0 C and its stabilization temperature (or annealing) is at 53O 0 C.
- the thermal cycle is as shown in Figure 3 which is a curve giving the temperature T ( 0 C) as a function of time t (hours).
- This cycle is therefore composed of a rise in temperature at 2 ° / min, a spreading step of 10 min at 75 ° C., a rapid descent of approximately up to a stabilization temperature (53 ° C.), d a stabilizing bearing, and a slow cooling then a faster cooling to room temperature.
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Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
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FR0413533A FR2879594B1 (fr) | 2004-12-17 | 2004-12-17 | Ensemble de jonction ceramique-metal ou alliage metallique |
PCT/FR2005/051080 WO2006064160A1 (fr) | 2004-12-17 | 2005-12-13 | Ensemble de jonction céramique - métal ou alliage métallique |
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EP1827670A1 true EP1827670A1 (de) | 2007-09-05 |
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EP05825170A Withdrawn EP1827670A1 (de) | 2004-12-17 | 2005-12-13 | Keramik-metall- oder metalllegierungsverbindungsanordnung |
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EP (1) | EP1827670A1 (de) |
JP (1) | JP2008524099A (de) |
CN (1) | CN101080265A (de) |
FR (1) | FR2879594B1 (de) |
WO (1) | WO2006064160A1 (de) |
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FR2987878B1 (fr) * | 2012-03-12 | 2014-05-09 | Air Liquide | Nouveau joint ceramique/metal et son procede d'elaboration |
EP2935155B1 (de) | 2012-12-19 | 2019-02-13 | Praxair Technology Inc. | Verfahren zum abdichten einer sauerstofftransportmembrananordnung |
US9212113B2 (en) | 2013-04-26 | 2015-12-15 | Praxair Technology, Inc. | Method and system for producing a synthesis gas using an oxygen transport membrane based reforming system with secondary reforming and auxiliary heat source |
US9296671B2 (en) | 2013-04-26 | 2016-03-29 | Praxair Technology, Inc. | Method and system for producing methanol using an integrated oxygen transport membrane based reforming system |
US9938145B2 (en) | 2013-04-26 | 2018-04-10 | Praxair Technology, Inc. | Method and system for adjusting synthesis gas module in an oxygen transport membrane based reforming system |
US9452401B2 (en) | 2013-10-07 | 2016-09-27 | Praxair Technology, Inc. | Ceramic oxygen transport membrane array reactor and reforming method |
WO2015160609A1 (en) | 2014-04-16 | 2015-10-22 | Praxair Technology, Inc. | Method and system for oxygen transport membrane enhanced integrated gasifier combined cycle (igcc) |
US10441922B2 (en) | 2015-06-29 | 2019-10-15 | Praxair Technology, Inc. | Dual function composite oxygen transport membrane |
US10118823B2 (en) | 2015-12-15 | 2018-11-06 | Praxair Technology, Inc. | Method of thermally-stabilizing an oxygen transport membrane-based reforming system |
WO2017112677A1 (en) * | 2015-12-21 | 2017-06-29 | Praxair Technology, Inc. | Apparatus including a ceramic component, a metal component, and a glass sealing material and a process of forming the apparatus |
US9938146B2 (en) | 2015-12-28 | 2018-04-10 | Praxair Technology, Inc. | High aspect ratio catalytic reactor and catalyst inserts therefor |
JP2019513081A (ja) | 2016-04-01 | 2019-05-23 | プラクスエア・テクノロジー・インコーポレイテッド | 触媒含有酸素輸送膜 |
US10010876B2 (en) | 2016-11-23 | 2018-07-03 | Praxair Technology, Inc. | Catalyst for high temperature steam reforming |
WO2019226435A1 (en) | 2018-05-21 | 2019-11-28 | Praxair Technology, Inc. | Otm syngas panel with gas heated reformer |
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SE95361C1 (de) * | 1934-08-13 | 1939-04-05 | ||
GB527580A (en) * | 1938-04-27 | 1940-10-11 | Bosch Gmbh Robert | Improvements in and relating to gas-tight joints between metallic and ceramic insulating bodies |
FR2592320B1 (fr) * | 1985-12-30 | 1988-04-08 | Inst Francais Du Petrole | Nouveau procede d'oxydation d'une charge oxydable en phase gazeuse et reacteur pour la mise en oeuvre de ce procede. |
GB9412786D0 (en) * | 1994-06-24 | 1994-08-17 | Johnson Matthey Plc | Improved reformer |
US6402156B1 (en) * | 1999-04-16 | 2002-06-11 | Eltron Research, Inc. | Glass-ceramic seals for ceramic membrane chemical reactor application |
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- 2004-12-17 FR FR0413533A patent/FR2879594B1/fr not_active Expired - Fee Related
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- 2005-12-13 JP JP2007546141A patent/JP2008524099A/ja active Pending
- 2005-12-13 EP EP05825170A patent/EP1827670A1/de not_active Withdrawn
- 2005-12-13 WO PCT/FR2005/051080 patent/WO2006064160A1/fr active Application Filing
- 2005-12-13 CN CNA2005800433793A patent/CN101080265A/zh active Pending
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WO2006064160A1 (fr) | 2006-06-22 |
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