US3657784A - Cladding of metals - Google Patents
Cladding of metals Download PDFInfo
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- US3657784A US3657784A US16943A US3657784DA US3657784A US 3657784 A US3657784 A US 3657784A US 16943 A US16943 A US 16943A US 3657784D A US3657784D A US 3657784DA US 3657784 A US3657784 A US 3657784A
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- United States
- Prior art keywords
- core
- alloy
- getter
- sheath
- article according
- Prior art date
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- Expired - Lifetime
Links
- 229910052751 metal Inorganic materials 0.000 title claims abstract description 40
- 239000002184 metal Substances 0.000 title claims abstract description 40
- 150000002739 metals Chemical class 0.000 title claims description 13
- 238000005253 cladding Methods 0.000 title description 21
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical group [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 claims abstract description 84
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 30
- 239000000956 alloy Substances 0.000 claims abstract description 30
- 239000003870 refractory metal Substances 0.000 claims abstract description 6
- 239000011162 core material Substances 0.000 claims description 73
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 33
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims description 29
- 230000004888 barrier function Effects 0.000 claims description 27
- 239000000463 material Substances 0.000 claims description 27
- CPLXHLVBOLITMK-UHFFFAOYSA-N Magnesium oxide Chemical compound [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 claims description 26
- 229910052750 molybdenum Inorganic materials 0.000 claims description 26
- 239000011733 molybdenum Substances 0.000 claims description 26
- 229910052726 zirconium Inorganic materials 0.000 claims description 21
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical group O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 claims description 16
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 15
- 239000001301 oxygen Substances 0.000 claims description 15
- 229910052760 oxygen Inorganic materials 0.000 claims description 15
- 239000011248 coating agent Substances 0.000 claims description 14
- 238000000576 coating method Methods 0.000 claims description 14
- 239000000395 magnesium oxide Substances 0.000 claims description 13
- 229910052758 niobium Inorganic materials 0.000 claims description 12
- 239000010955 niobium Substances 0.000 claims description 12
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims description 12
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 claims description 11
- 229910000599 Cr alloy Inorganic materials 0.000 claims description 9
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 9
- 239000000788 chromium alloy Substances 0.000 claims description 9
- 229910052715 tantalum Inorganic materials 0.000 claims description 9
- 229910052719 titanium Inorganic materials 0.000 claims description 9
- 239000010936 titanium Substances 0.000 claims description 9
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 claims description 9
- 229910001260 Pt alloy Inorganic materials 0.000 claims description 7
- 150000001875 compounds Chemical class 0.000 claims description 7
- 238000002844 melting Methods 0.000 claims description 7
- 230000008018 melting Effects 0.000 claims description 7
- -1 platinum group metals Chemical class 0.000 claims description 7
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 6
- 229910052721 tungsten Inorganic materials 0.000 claims description 6
- 239000010937 tungsten Substances 0.000 claims description 6
- 229910001182 Mo alloy Inorganic materials 0.000 claims description 5
- 229910052735 hafnium Inorganic materials 0.000 claims description 5
- VBJZVLUMGGDVMO-UHFFFAOYSA-N hafnium atom Chemical compound [Hf] VBJZVLUMGGDVMO-UHFFFAOYSA-N 0.000 claims description 5
- QSHDDOUJBYECFT-UHFFFAOYSA-N mercury Chemical compound [Hg] QSHDDOUJBYECFT-UHFFFAOYSA-N 0.000 claims description 5
- 229910052753 mercury Inorganic materials 0.000 claims description 5
- 229910052720 vanadium Inorganic materials 0.000 claims description 5
- GPPXJZIENCGNKB-UHFFFAOYSA-N vanadium Chemical compound [V]#[V] GPPXJZIENCGNKB-UHFFFAOYSA-N 0.000 claims description 5
- 150000001247 metal acetylides Chemical class 0.000 claims description 4
- 150000004767 nitrides Chemical class 0.000 claims description 4
- 150000003568 thioethers Chemical class 0.000 claims description 4
- 229910001362 Ta alloys Inorganic materials 0.000 claims description 3
- YCWDQIXAYITGJX-UHFFFAOYSA-N [Cr].[Ta].[Nb] Chemical compound [Cr].[Ta].[Nb] YCWDQIXAYITGJX-UHFFFAOYSA-N 0.000 claims description 3
- QVZNQFNKKMMPFH-UHFFFAOYSA-N chromium niobium Chemical compound [Cr].[Nb] QVZNQFNKKMMPFH-UHFFFAOYSA-N 0.000 claims description 3
- HBCZDZWFGVSUDJ-UHFFFAOYSA-N chromium tantalum Chemical compound [Cr].[Ta] HBCZDZWFGVSUDJ-UHFFFAOYSA-N 0.000 claims description 3
- 238000000354 decomposition reaction Methods 0.000 claims description 3
- RHDUVDHGVHBHCL-UHFFFAOYSA-N niobium tantalum Chemical compound [Nb].[Ta] RHDUVDHGVHBHCL-UHFFFAOYSA-N 0.000 claims description 3
- 229910021332 silicide Inorganic materials 0.000 claims description 3
- 239000000377 silicon dioxide Substances 0.000 claims description 3
- 229910001080 W alloy Inorganic materials 0.000 claims description 2
- 229910001092 metal group alloy Inorganic materials 0.000 claims description 2
- 229910000753 refractory alloy Inorganic materials 0.000 claims description 2
- 239000011521 glass Substances 0.000 abstract description 4
- 238000009987 spinning Methods 0.000 abstract description 2
- 229910052697 platinum Inorganic materials 0.000 description 29
- 239000006060 molten glass Substances 0.000 description 8
- 239000010948 rhodium Substances 0.000 description 6
- MHOVAHRLVXNVSD-UHFFFAOYSA-N rhodium atom Chemical compound [Rh] MHOVAHRLVXNVSD-UHFFFAOYSA-N 0.000 description 6
- KDLHZDBZIXYQEI-UHFFFAOYSA-N Palladium Chemical compound [Pd] KDLHZDBZIXYQEI-UHFFFAOYSA-N 0.000 description 4
- 229910052741 iridium Inorganic materials 0.000 description 4
- GKOZUEZYRPOHIO-UHFFFAOYSA-N iridium atom Chemical compound [Ir] GKOZUEZYRPOHIO-UHFFFAOYSA-N 0.000 description 4
- 229910052703 rhodium Inorganic materials 0.000 description 4
- 229910000629 Rh alloy Inorganic materials 0.000 description 3
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 3
- 230000009471 action Effects 0.000 description 2
- 239000002131 composite material Substances 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 230000003647 oxidation Effects 0.000 description 2
- 238000007254 oxidation reaction Methods 0.000 description 2
- RVTZCBVAJQQJTK-UHFFFAOYSA-N oxygen(2-);zirconium(4+) Chemical compound [O-2].[O-2].[Zr+4] RVTZCBVAJQQJTK-UHFFFAOYSA-N 0.000 description 2
- 229910052763 palladium Inorganic materials 0.000 description 2
- 229910052761 rare earth metal Inorganic materials 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- 229910001928 zirconium oxide Inorganic materials 0.000 description 2
- 229910052582 BN Inorganic materials 0.000 description 1
- PZNSFCLAULLKQX-UHFFFAOYSA-N Boron nitride Chemical compound N#B PZNSFCLAULLKQX-UHFFFAOYSA-N 0.000 description 1
- 229910052581 Si3N4 Inorganic materials 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000005012 migration Effects 0.000 description 1
- 238000013508 migration Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 229910000476 molybdenum oxide Inorganic materials 0.000 description 1
- 229910000484 niobium oxide Inorganic materials 0.000 description 1
- URLJKFSTXLNXLG-UHFFFAOYSA-N niobium(5+);oxygen(2-) Chemical compound [O-2].[O-2].[O-2].[O-2].[O-2].[Nb+5].[Nb+5] URLJKFSTXLNXLG-UHFFFAOYSA-N 0.000 description 1
- PQQKPALAQIIWST-UHFFFAOYSA-N oxomolybdenum Chemical class [Mo]=O PQQKPALAQIIWST-UHFFFAOYSA-N 0.000 description 1
- HWLDNSXPUQTBOD-UHFFFAOYSA-N platinum-iridium alloy Chemical compound [Ir].[Pt] HWLDNSXPUQTBOD-UHFFFAOYSA-N 0.000 description 1
- 230000000135 prohibitive effect Effects 0.000 description 1
- 150000002910 rare earth metals Chemical class 0.000 description 1
- 239000011819 refractory material Substances 0.000 description 1
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 description 1
- ZCUFMDLYAMJYST-UHFFFAOYSA-N thorium dioxide Chemical compound O=[Th]=O ZCUFMDLYAMJYST-UHFFFAOYSA-N 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
- ZVWKZXLXHLZXLS-UHFFFAOYSA-N zirconium nitride Chemical compound [Zr]#N ZVWKZXLXHLZXLS-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03B—MANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
- C03B5/00—Melting in furnaces; Furnaces so far as specially adapted for glass manufacture
- C03B5/16—Special features of the melting process; Auxiliary means specially adapted for glass-melting furnaces
- C03B5/167—Means for preventing damage to equipment, e.g. by molten glass, hot gases, batches
- C03B5/1672—Use of materials therefor
- C03B5/1675—Platinum group metals
-
- 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
- B23K20/00—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
- B23K20/22—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating taking account of the properties of the materials to be welded
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03B—MANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
- C03B5/00—Melting in furnaces; Furnaces so far as specially adapted for glass manufacture
- C03B5/16—Special features of the melting process; Auxiliary means specially adapted for glass-melting furnaces
- C03B5/167—Means for preventing damage to equipment, e.g. by molten glass, hot gases, batches
- C03B5/1672—Use of materials therefor
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12535—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12535—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
- Y10T428/12576—Boride, carbide or nitride component
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12535—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
- Y10T428/12583—Component contains compound of adjacent metal
- Y10T428/1259—Oxide
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12535—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
- Y10T428/12611—Oxide-containing component
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12535—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
- Y10T428/12611—Oxide-containing component
- Y10T428/12618—Plural oxides
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12806—Refractory [Group IVB, VB, or VIB] metal-base component
- Y10T428/12812—Diverse refractory group metal-base components: alternative to or next to each other
Definitions
- ABSTRACT Primary Examiner-L. Dewayne Rutledge Assistant Examiner-E. L. Weise Attorney-Hofgren, Wegner, Allen, Stellman & McCord [57] ABSTRACT
- This invention relates to articles for use at high operating temperatures (1,100-1,500 C.) and comprising a core made from a refractory metal or alloy and clad with a sheath of a platinum group metal or alloy based on at least one platinum group metal.
- Such articles in the form of stirrers, crucibles, spinning dies and the like have particular application in the glass industry.
- This invention relates to the cladding of refractory metals with platinum group metals or alloys based on at least one metal of the platinum group. Such alloys will be referred to herein as platinum base alloys.
- the invention is particularly but not exclusively applicable to the cladding with the aforesaid metals or alloys of articles which are used in the glass industry, such as, s'tirrers, crucibles, spinning dies, tube fabricating dies and the like.
- platinum group metals we have found platinum, rhodium, palladium and iridium particularly suitable cladding metals. 0f the alloys consisting predominantly of one or more platinum group metals, satisfactory results have been obtained from the following cladding alloys; rhodium/iridium; platinum/iridium; palladium/iridium, and platinum/rhodium/iridium.
- Such articles are required, in use, to withstand the action of molten glass at temperatures at least as high as 1,100" C. and sometimes as high as 1,500 C. Further, they are generally required not to introduce measurable quantities of impurities into molten glass with which they come into contact.
- a stirrer is typically in the form of an inverted T in which the vertical shaft is about 6 feet long and 1% inch diameter and the horizontal shaft is 4 feet long and 1% inch diameter.
- the platinum or rhodium/platinum sheath is usually applied by fitting suitably shaped pieces of platinum of platinum/rhodium alloy sheet round the article to be clad and then welding these pieces together so as to form a closely fitting cladding or covering for the core.
- the cladding is generally provided with one or more small exhaust tubes which communicate with the interfacial space between the cladding and the core but is otherwise gas-tight.
- the final stage in the cladding of the core involves a reduction in the pressure of the fluid (e.g. gas, vapor) in the interfacial space via the exhaust tube(s) down to a low value following which the tube(s) are pinch sealed.
- the pressure in the interfacial space is reduced in this way so as to minimize the oxidation of the molybdenum core in service and to improve the fit of the cladding.
- the value to which the pressure of the fluid in the interfacial space is reduced will depend inter alia on the geometry of the core and may be within the range of a few microns to 2 mm. of H,.
- Molydenum articles clad in this way were, however, found to be prone to early failure in service.
- the failure takes the form of a fracture or split in the cladding which permits molten glass'to reach the underlying molybdenum core.
- Attempts were, therefore, madeat least to reduce this effect by interposing a barrier layer of some refractory material such 'as alumina between the core and the cladding so as to prevent direct contact therebetween.
- the molybdenum is transferred to the platinum cladding in the vapour phase as one or more oxides of molybdenum. It is believed that the trioxide is predominant.
- the molybdenum oxides formed by the interaction of the core material and any residual oxygen in the interfacial space are tained at the lower operating temperatures in the region of volatilized and, when they contact the inner surface of the platinum cladding, they are reduced to the metal, which then alloys with the platinum.
- the oxygen liberated in this way is then available to oxidize more of the molybdenum core so that the action is continuous and we have found that the inner regions of the cladding begin to breakdown, thus leading to ultimate failure.
- the operating life of a core clad with platinum or with a platinum base alloy can be greatly improved if the core is made from a metal selected from the group consisting of niobium, tantalum, niobium-tantalum alloys, niobium-chromium alloys, tantalum-chromium alloys and niobium-tantalum-chromium alloys.
- the oxides of niobium and tantalum are much less volatile than the oxides of molybdenum at the operating temperatures of l,l00 1,400" C. or l,500 C.
- the platinum (or platinum base alloy) cladding is affected by cores of these metals much less, and, consequently, the operating life of the article is considerably increased.
- titanium, zirconium and vanadium do not form volatile oxides but their melting points are too low to allow of their effective use. They are weak mechanically at the average operating temperatures of 1,350 1,400 C. and moreover they have the undesirable tendency to alloy with the platinum or platinum based sheath to form diffused alloy layers, intermediate phases, and in some instances, phases with melting points lower than the temperature at which the component is intended to operate.
- an arrangement using a molybdenum core has a shorter operating life than is desirable, and attempts to prolong the operating life by reducing the pressure in the interfacial spaces between the core and the sheath have not up to the present time met with success.
- Suitable getter materials are metals such as zirconium, tantalum, niobium, titanium, vanadium or hafnium. These metals may also be applied in smaller quantities as dilute alloys of molybdenum or platinum.
- the invention also includes the use of a barrier layer between the core and getter layers and the outer sheath of the article.
- the barrier layer may comprise:
- refractory oxides i.e. oxides which are themselves refractory; not necessarily the oxides of refractory metals;
- refractory nitrides for example boron nitride and silicon nitride
- the above items (a) (e) include the compounds of the rare earth metals.
- an article intended to be used at high operating temperature, above l,000 C. comprises:
- a core comprising a refractory metal selected from the group consisting of molybdenum, tungsten and an alloy based on at least one of said metals;
- a barrier layer applied to the getter comprising a refractory compound selected from the group consisting of refractory carbides, silicides, borides, sulphides, nitrides and oxides, whereby volatilization of the oxides of said core material is prevented from forming with an outer sheath an alloy of lower melting point than that of the sheath, and
- an outer sheath enclosing the core, "getter” and barrier layers and comprising a material selected from the group consisting of the platinum group metals and an alloy based on at least one platinum group metal.
- the pressure in the interfacial space between core and sheath is within the range of a few microns to 2 mm. of mercury.
- the low oxygen pressure required to ensure the continued operation of the molybdenum cored component may be easily obtained by the use of a getter as detailed above.
- the use of these getters produce such a low partial pressure of oxygen that the more usual refractory oxides, such as alumina, zirconia and thoria, for example, tend to decompose.
- the metal so released tends to alloy with the platinum of the sheath and this again produces early failure of the component.
- a barrier layer to which this does not apply is composed of magnesia.
- a preferred embodiment of the invention is the use of magnesia as the barrier layer.
- a molybdenum or tungsten core may be flame-sprayed with zirconium metal.
- zirconium metal This results in a coating comprising a mixture of zirconium metal, zirconium oxide and zirconium nitride.
- zirconia is then flame-sprayed onto the previously flame-sprayed layer of zirconium.
- the quantity of zirconium first sprayed is chosen so that the amount of zirconium available is only slightly greater than that required to take-up the oxygen present in the interfacial space.
- the zirconium oxide is porous to allow a rapid movement of gas.
- zirconium or other getter may be incorporated within the molybdenum or tungsten core so as to form an alloy of for example 0.5 1 .0 wt. percent zirconium/molybdenum.
- a composite core comprising a central core of molybdenum having a first layer of titanium, zirconium or vanadium as getter and finally an outer barrier layer formed from a rare earth compound oxide with refractory properties, particularly magnesia, may be used.
- the getter may be plasmaor flame-sprayed in a layer uniformly over the molybdenum or tungsten surface of the core.
- the core e.g. 700 1,200 C.
- it may be concentrated at a point in a fairly cool area of the core (e.g. 700 1,200 C.) so that it can absorb oxygen very effectively without coming into direct contact with barrier layer materials at high temperature because such contact would lead to decomposition.
- the getter may be concentrated around the upper part of the stem, above the surface of the molten glass.
- tlameor plasma-sprayed magnesia When tlameor plasma-sprayed magnesia is used as the barrier layer it may be applied in combination with a small quantity of silica to assist adhesion to the core.
- An article intended to be used at high operating temperatures above l,000 C. comprising a molybdenum core, a zirconium metal coating on said core as a getter for oxygen, a barrier layer of the group consisting essentially of zirconia and magnesia on said zirconium metal getter, and a sheath enclosing the so coated core and consisting essentially of a material selected from the group consisting of a platinum group metal and an alloy having at least one platinum group metal.
- An article intended to be used at high operating temperatures above l,000.C. comprising a core of a metal selected from the group consisting of niobium, tantalum, niobium-tantalum alloy, niobium-chromium alloy, tantalum-chromium alloy and niobium-tantalum-chromium alloy, a getter for oxygen on the core consisting essentially of a refractory coating, a sheath of a material selected from the group consisting of a platinum group metal and an alloy having at least one platinum group metal, and a barrier layer interposed between said core and said sheath comprising a refractory compound compatible with said core and said sheath at the operating temperature, whereby volatilization of oxides of said core material is reduced and said core material is prevented from forming with said sheath an alloy having a melting point below said operating temperature.
- a metal selected from the group consisting of niobium, tantalum, niobium-tantalum alloy,
- An article according to claim 4 further having an interfacial space between the core and the sheath wherein the said space has a partial pressure of not more than 2 mm. of mercury.
- An article intended to be used at high operating temperatures above l,000 C. comprising: (a) a core consisting essentially of a refractory metal selected from the group consisting of molybdenum, tungsten and a refractory alloy based on at least one of said metals; (b) a getter for oxygen on the core consisting essentially of a refractory coating; (c) a barrier layer on the getter consisting essentially of a refractory compound selected from the group consisting of refractory carbides, silicides, borides, sulphides, nitrides and oxides, and (d) an outer sheath enclosing the core, getter and barrier layers and consisting essentially of a material selected from the group consisting of the platinum group metals and a platinum group metal alloy, volatilization of the oxides of said core material thereby being prevented from forming with said outer sheath an alloy of lower melting point than that of the sheath.
- An article according to claim 6 having an interfacial space between the core and the sheath wherein the said space has a partial pressure of not more than 2 mm. of mercury.
- getter is a material selected from the group consisting of zirconium, tantalum, niobium, titanium, vanadium and hafnium.
- core material is molybdenum alloyed with minor quantities of at least one of the materials of the group consisting of titanium and zirconium.
- barrier layer of magnesia includes a minor amount of silica.
- An article intended to be used at high operating temperatures above 1,000 C. having a core of the class consisting of molybdenum, tungsten, an alloy of molybdenum, and an alloy of tungsten, and a flame-sprayed coating on said core of zirconium, a further flame-sprayed coating thereon selected from the group consisting of zirconia and magnesia, and a sheath enclosing said coated core and comprising a material selected from the group consisting of a platinum group metal and an alloy of at least one platinum group metal.
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Abstract
Description
Claims (16)
- 2. An article according to claim 1 wherein said core comprises an alloy of said molybdenum with 0.5 - 1.0 wt. percent of zirconium.
- 3. An article according to claim 1 wherein the barrier layer comprises magnesia.
- 4. An article intended to be used at high operating temperatures above 1,000* C. comprising a core of a metal selected from the group consisting of niobium, tantalum, niobium-tantalum alloy, niobium-chromium alloy, tantalum-chromium alloy and niobium-tantalum-chromium alloy, a getter for oxygen on the core consisting essentially of a refractory coating, a sheath of a material selected from the groUp consisting of a platinum group metal and an alloy having at least one platinum group metal, and a barrier layer interposed between said core and said sheath comprising a refractory compound compatible with said core and said sheath at the operating temperature, whereby volatilization of oxides of said core material is reduced and said core material is prevented from forming with said sheath an alloy having a melting point below said operating temperature.
- 5. An article according to claim 4 further having an interfacial space between the core and the sheath wherein the said space has a partial pressure of not more than 2 mm. of mercury.
- 6. An article intended to be used at high operating temperatures above 1,000* C. comprising: (a) a core consisting essentially of a refractory metal selected from the group consisting of molybdenum, tungsten and a refractory alloy based on at least one of said metals; (b) a getter for oxygen on the core consisting essentially of a refractory coating; (c) a barrier layer on the getter consisting essentially of a refractory compound selected from the group consisting of refractory carbides, silicides, borides, sulphides, nitrides and oxides, and (d) an outer sheath enclosing the core, getter and barrier layers and consisting essentially of a material selected from the group consisting of the platinum group metals and a platinum group metal alloy, volatilization of the oxides of said core material thereby being prevented from forming with said outer sheath an alloy of lower melting point than that of the sheath.
- 7. An article according to claim 6 having an interfacial space between the core and the sheath wherein the said space has a partial pressure of not more than 2 mm. of mercury.
- 8. An article according to claim 7 wherein the getter is a material selected from the group consisting of zirconium, tantalum, niobium, titanium, vanadium and hafnium.
- 9. An article according to claim 8 wherein the getter material is present in relatively small quantities as dilute alloys of molybdenum or platinum.
- 10. An article according to claim 6 wherein the getter is in the form of a plasma or flame sprayed coating.
- 11. An article according to claim 6 wherein the getter is concentrated in an area which, in use, is not subject to temperatures greater than 1,200* C. so that the getter absorbs oxygen without contact with the barrier layer, thereby avoiding decomposition of the sheath material.
- 12. An article according to claim 6 wherein the core material is molybdenum alloyed with minor quantities of at least one of the materials of the group consisting of titanium and zirconium.
- 13. An article according to claim 6 wherein the core material is alloyed with at least one of the metals selected from the group consisting of titanium, zirconium, niobium, tantalum and hafnium.
- 14. An article according to claim 6 wherein the getter material comprises zirconium metal and the barrier layer is zirconia.
- 15. An article according to claim 6 wherein the getter material is zirconium and the barrier layer is magnesia.
- 16. An article according to claim 15 wherein the barrier layer of magnesia includes a minor amount of silica.
- 17. An article intended to be used at high operating temperatures above 1,000* C. having a core of the class consisting of molybdenum, tungsten, an alloy of molybdenum, and an alloy of tungsten, and a flame-sprayed coating on said core of zirconium, a further flame-sprayed coating thereon selected from the group consisting of zirconia and magnesia, and a sheath enclosing said coated core and comprising a material selected from the group consisting of a platinum group metal and an alloy of at least one platinum group metal.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US1694370A | 1970-03-05 | 1970-03-05 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3657784A true US3657784A (en) | 1972-04-25 |
Family
ID=21779852
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US16943A Expired - Lifetime US3657784A (en) | 1970-03-05 | 1970-03-05 | Cladding of metals |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3657784A (en) |
Cited By (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4036601A (en) * | 1974-03-26 | 1977-07-19 | Gesellschaft Fur Kernforschung M.B.H. | Corrosion-resistant turbine blades and method for producing them |
| FR2492806A1 (en) * | 1980-10-27 | 1982-04-30 | Owens Corning Fiberglass Corp | LAMINATES FOR COMING IN CONTACT WITH MOLTEN GLASS, METHOD FOR THE PREPARATION THEREOF AND USE THEREOF IN APPARATUS FOR PRODUCING GLASS FIBERS |
| US4342577A (en) * | 1980-10-27 | 1982-08-03 | Owens-Corning Fiberglas Corporation | Method and apparatus for forming glass fibers |
| US4343636A (en) * | 1981-04-20 | 1982-08-10 | Owens-Corning Fiberglas Corporation | Method and apparatus for forming glass fibers |
| US4348216A (en) * | 1980-10-27 | 1982-09-07 | Owens-Corning Fiberglas Corporation | Method and apparatus for forming glass fibers |
| US4402719A (en) * | 1980-10-27 | 1983-09-06 | Owens-Corning Fiberglas Corporation | Method and apparatus for forming glass fibers |
| US4402718A (en) * | 1980-10-27 | 1983-09-06 | Owens-Corning Fiberglas Corporation | Method and apparatus for forming glass fibers |
| US4404009A (en) * | 1982-12-22 | 1983-09-13 | Owens-Corning Fiberglas Corporation | Method and apparatus for forming glass fibers |
| US4427428A (en) | 1980-10-27 | 1984-01-24 | Owens-Corning Fiberglas Corporation | Feeder for forming glass fibers and method for making feeder |
| US4430105A (en) | 1980-10-27 | 1984-02-07 | Owens-Corning Fiberglas Corporation | Method and apparatus for forming glass fibers |
| US4447248A (en) * | 1982-07-15 | 1984-05-08 | Owens-Corning Fiberglas Corporation | Method of making and using glass fiber forming feeders |
| US4502936A (en) * | 1980-11-26 | 1985-03-05 | Imi Kynoch Limited | Electrode and electrolytic cell |
| US4532184A (en) * | 1983-11-23 | 1985-07-30 | Owens-Corning Fiberglas Corporation | Precious metal vaporization reduction |
| US4668262A (en) * | 1985-12-30 | 1987-05-26 | Owens-Corning Fiberglas Corporation | Protective coating for refractory metal substrates |
| US4685948A (en) * | 1985-02-08 | 1987-08-11 | Matsushita Electric Industrial Co., Ltd. | Mold for press-molding glass optical elements and a molding method using the same |
| US4889776A (en) * | 1987-08-17 | 1989-12-26 | Barson Corporation | Refractory metal composite coated article |
| US4942732A (en) * | 1987-08-17 | 1990-07-24 | Barson Corporation | Refractory metal composite coated article |
| US5432008A (en) * | 1988-12-05 | 1995-07-11 | Adiabatics, Inc. | Composition and methods for densifying refractory oxide coatings |
| EP0471505B1 (en) * | 1990-08-11 | 1996-10-02 | Johnson Matthey Public Limited Company | Coated article, its use and method of making the same |
| US6383050B1 (en) * | 1999-01-13 | 2002-05-07 | Canon Kabushiki Kaisha | Process for forming non-evaporative getter and method of producing image forming apparatus |
| US20050148255A1 (en) * | 2002-01-15 | 2005-07-07 | Doyle Mark L. | Platinum metal based article for high temperature applications |
| US20080151687A1 (en) * | 2006-12-21 | 2008-06-26 | Lee Martin Adelsberg | Method for minimizing erosion of refractory metal vessels in a glass making system |
| US20120125050A1 (en) * | 2010-09-30 | 2012-05-24 | Avanstrate Inc. | Method for manufacturing glass plate |
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| US2497090A (en) * | 1947-12-13 | 1950-02-14 | Eitel Mccullough Inc | Electrode and method of making the same |
| US2536673A (en) * | 1948-02-25 | 1951-01-02 | Rca Corp | Zirconium coating for electron discharge devices |
| US2681876A (en) * | 1949-01-24 | 1954-06-22 | Int Standard Electric Corp | Refractory coated article |
| US2947114A (en) * | 1957-05-09 | 1960-08-02 | Engelhard Ind Inc | Composite material |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| US2497090A (en) * | 1947-12-13 | 1950-02-14 | Eitel Mccullough Inc | Electrode and method of making the same |
| US2536673A (en) * | 1948-02-25 | 1951-01-02 | Rca Corp | Zirconium coating for electron discharge devices |
| US2681876A (en) * | 1949-01-24 | 1954-06-22 | Int Standard Electric Corp | Refractory coated article |
| US2947114A (en) * | 1957-05-09 | 1960-08-02 | Engelhard Ind Inc | Composite material |
Cited By (27)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4036601A (en) * | 1974-03-26 | 1977-07-19 | Gesellschaft Fur Kernforschung M.B.H. | Corrosion-resistant turbine blades and method for producing them |
| US4427428A (en) | 1980-10-27 | 1984-01-24 | Owens-Corning Fiberglas Corporation | Feeder for forming glass fibers and method for making feeder |
| FR2492806A1 (en) * | 1980-10-27 | 1982-04-30 | Owens Corning Fiberglass Corp | LAMINATES FOR COMING IN CONTACT WITH MOLTEN GLASS, METHOD FOR THE PREPARATION THEREOF AND USE THEREOF IN APPARATUS FOR PRODUCING GLASS FIBERS |
| WO1982001510A1 (en) * | 1980-10-27 | 1982-05-13 | Owens Corning Fiberglass Corp | Articles for contacting molten glass |
| US4342577A (en) * | 1980-10-27 | 1982-08-03 | Owens-Corning Fiberglas Corporation | Method and apparatus for forming glass fibers |
| US4348216A (en) * | 1980-10-27 | 1982-09-07 | Owens-Corning Fiberglas Corporation | Method and apparatus for forming glass fibers |
| US4402719A (en) * | 1980-10-27 | 1983-09-06 | Owens-Corning Fiberglas Corporation | Method and apparatus for forming glass fibers |
| US4402718A (en) * | 1980-10-27 | 1983-09-06 | Owens-Corning Fiberglas Corporation | Method and apparatus for forming glass fibers |
| US4430105A (en) | 1980-10-27 | 1984-02-07 | Owens-Corning Fiberglas Corporation | Method and apparatus for forming glass fibers |
| US4502936A (en) * | 1980-11-26 | 1985-03-05 | Imi Kynoch Limited | Electrode and electrolytic cell |
| US4343636A (en) * | 1981-04-20 | 1982-08-10 | Owens-Corning Fiberglas Corporation | Method and apparatus for forming glass fibers |
| US4447248A (en) * | 1982-07-15 | 1984-05-08 | Owens-Corning Fiberglas Corporation | Method of making and using glass fiber forming feeders |
| US4404009A (en) * | 1982-12-22 | 1983-09-13 | Owens-Corning Fiberglas Corporation | Method and apparatus for forming glass fibers |
| US4532184A (en) * | 1983-11-23 | 1985-07-30 | Owens-Corning Fiberglas Corporation | Precious metal vaporization reduction |
| US4685948A (en) * | 1985-02-08 | 1987-08-11 | Matsushita Electric Industrial Co., Ltd. | Mold for press-molding glass optical elements and a molding method using the same |
| US4668262A (en) * | 1985-12-30 | 1987-05-26 | Owens-Corning Fiberglas Corporation | Protective coating for refractory metal substrates |
| US4889776A (en) * | 1987-08-17 | 1989-12-26 | Barson Corporation | Refractory metal composite coated article |
| US4942732A (en) * | 1987-08-17 | 1990-07-24 | Barson Corporation | Refractory metal composite coated article |
| US5432008A (en) * | 1988-12-05 | 1995-07-11 | Adiabatics, Inc. | Composition and methods for densifying refractory oxide coatings |
| EP0471505B1 (en) * | 1990-08-11 | 1996-10-02 | Johnson Matthey Public Limited Company | Coated article, its use and method of making the same |
| US6383050B1 (en) * | 1999-01-13 | 2002-05-07 | Canon Kabushiki Kaisha | Process for forming non-evaporative getter and method of producing image forming apparatus |
| US20050148255A1 (en) * | 2002-01-15 | 2005-07-07 | Doyle Mark L. | Platinum metal based article for high temperature applications |
| US20080151687A1 (en) * | 2006-12-21 | 2008-06-26 | Lee Martin Adelsberg | Method for minimizing erosion of refractory metal vessels in a glass making system |
| WO2008088432A1 (en) * | 2006-12-21 | 2008-07-24 | Corning Incorporated | Method for minimizing erosion of refractory metal vessels in a glass making system |
| US8256951B2 (en) | 2006-12-21 | 2012-09-04 | Corning Incorporated | Stirrers for minimizing erosion of refractory metal vessels in a glass making system |
| US8485717B2 (en) | 2006-12-21 | 2013-07-16 | Corning Incorporated | Stirrers for minimizing erosion of refractory metal vessels in a glass making system |
| US20120125050A1 (en) * | 2010-09-30 | 2012-05-24 | Avanstrate Inc. | Method for manufacturing glass plate |
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