GB2320034A - Coating of continuous casting machine grid plates - Google Patents
Coating of continuous casting machine grid plates Download PDFInfo
- Publication number
- GB2320034A GB2320034A GB9714452A GB9714452A GB2320034A GB 2320034 A GB2320034 A GB 2320034A GB 9714452 A GB9714452 A GB 9714452A GB 9714452 A GB9714452 A GB 9714452A GB 2320034 A GB2320034 A GB 2320034A
- Authority
- GB
- United Kingdom
- Prior art keywords
- coating
- islands
- grid plate
- ceramo
- ceramic
- 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.)
- Granted
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
- C23C4/06—Metallic material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/04—Continuous casting of metals, i.e. casting in indefinite lengths into open-ended moulds
- B22D11/059—Mould materials or platings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/12—Accessories for subsequent treating or working cast stock in situ
- B22D11/124—Accessories for subsequent treating or working cast stock in situ for cooling
- B22D11/1243—Accessories for subsequent treating or working cast stock in situ for cooling by using cooling grids or cooling plates
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/12—Accessories for subsequent treating or working cast stock in situ
- B22D11/128—Accessories for subsequent treating or working cast stock in situ for removing
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/18—After-treatment
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Organic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
- Plasma & Fusion (AREA)
- Metallurgy (AREA)
- Physics & Mathematics (AREA)
- Coating By Spraying Or Casting (AREA)
- Application Of Or Painting With Fluid Materials (AREA)
- Coating With Molten Metal (AREA)
- Continuous Casting (AREA)
- Moulds For Moulding Plastics Or The Like (AREA)
- Mold Materials And Core Materials (AREA)
- Ceramic Products (AREA)
Abstract
A coating consisting of ceramo-metallic material, e.g. WC-Co, is applied to an internal surface of a grid plate by flame spraying. A ceramic slurry is applied and fired to produce a ceramic coating which is partially removed to produce a composite ceramo-metallic and ceramic surface which is then bonded and densified. The coating is in the form of an array of islands. A ceramic slurry may then be applied and fixed to produce a ceramic coating which is partially removed to produce a composite ceramic-metallic and ceramic surface which is then bonded and densified. The ceramic slurry may contain a chromium compound capable of being converted into chromium oxide at temperatures of at least 300{C. The composite surface may then be impregnated with a solution of at least one soluble compound capable of being converted on heating, into an insoluble substance which bonds the coatings. The soluble compound may be selected from chromia and phosphate forming compounds.
Description
1 2320034 COATING OF CON7LNUOUS CASTING MACHENE GRED PLATES Document.;:
163729 This invention relates to the coating of components used in the continuous casting of ferrous and non-ferrous materials.
The topmost stage of a continuous casting machine is composed of a hollow box made up of side plates and end plates (and sometimes a central divider), usually of copper, which are water cooled. At the initial stage of casting a plug or dummy bar is positioned at the bottom of the mould and molten metal is poured into the mould from a ladle via a tundish. The water-cooled copper walls of the mould and the cold surface of the plug create a thin solidified skin which contains the molten material. As the molten metal continuous to solidify, the plug is slowly withdrawn downwards from the mould zone whilst the level of molten material at the top of the mould is maintained by continuously adding further molten material. A mould powder may be added simultaneously, to form a layer on the surface of the molten metal.
As the plug or dummy bar and the solidifying slab or strand to which it is now attached leaves the mould zone, it then enters a grid plate zone. The grid plates are usually made of cast iron or steel. Each grid plate comprises several raised "fmgers" with surfaces which are in contact with the chilled skin of the slab and which continue to constrain the solidifying slab to the requisite cross-sectional shape whilst cooling water is continuously sprayed onto the surface of the slab in between the fingers. During the time of this transfer of the slab from the mould and through the grid plate zone, the thickness of the chilled skin is increasing.
The slab then passes further on down through the machine through a series of guides and rolls, which continue to constrain the slab to the designed shape. Whilst passing down the casting machine the plane of the slab is gradually changed from avertical 2 direction to a horizontal direction until the fully solidified but still hot slab emerges on a conveyor table at the bottom of the machine, where it is cut to the requisite length.
The surfaces of the grid plates are subject to severe wear due to the abrasive, adhesive, and erosive wear mechanisms induced by the high ferrostatic pressures, the high temperatures, and the formation of oxide skins and exacerbated by the entrainment of extraneous third body particles. In a relatively short time, these components become so worn that they are unable to constrain the slab to the correct size and shape. The casting campaign then has to be terminated whilst new or refurbished parts are fitted. Thus the severe wear of these critical components limits the casting time and therefore the efficiency of the continuous casting process. There is, therefore, a need for a coating that is capable of withstanding the aggressive high temperature wear environment thus extending the length of the normal continuous casting campaign.
The present invention provides a method of protecting a grid plate for a continuous casting machine against wear, the method comprising applying to a strand-confining surface of the grid plate, by flame spraying, a coating consisting of ceramo-metallic material, the coating being in the form of an array of mutually isolated islands of the ceramo-metallic material.
In particular the invention provides a method of protecting a grid plate for a continuous casting machine against wear, comprising: (a) applying to a strand-confining surface of the grid plate, by flame spraying, a rough first coating consisting of ceramo-metallic material, the first coating being in the form of an array of mutually isolated islands of the ceraino-metallic material. (b) applying a ceramic slurry to the islands of ceramometallic material,- (c) heating the ceramic slurry to form a second coating consisting of ceramic material; (d) removing excess ceramic material from the second coating to produce a composite ceramo- metallic and ceramic surface; (e) impregnating the composite surface with a solution of at least one soluble compound capable of being converted, on heating, into an insoluble substance which bonds the coatings; and 3 (f) heating the coatings to cause bonding and densification of the coatings by the said substance; whereby a composite coating is produced which is in the form of an array of mutually isolated islands.
Step (e) preferably comprises impregnating the composite surface with a solution of at least one chromia or phosphate forming compound.
The final ceramic coating is preferably a so-called Monitox coating, which is achieved by applying to a substrate a slurry containing a chromium compound capable of being converted into a chromium oxide and/or a chromium phosphate at temperatures of at least 250T, heating the slurry to produce a porous ceramic coating, and then densifying and bonding the coating by one or more process cycles comprising impregnating the porous coating with at least one chromia or phosphate forming solution, removing excess impregnant, and heating. Such a technique is described in GB-A-1 466 074, for example.
The first coating may be any cermet (ceramo-metallic) coating but is preferably a tungsten carbide cobalt coating and is preferably applied in several successive layers. The flame spraying process is preferably a high velocity oxygen - liquid fuel process which is often referred to as an HVOF process. This process is a commercially available flame spraying process in which fuel and oxygen are combusted in a specially designed chamber which is connected to a water-cooled tube or nozzle at the combustion chamber exit. The combustion products are accelerated down the nozzle, constituting a gun or torch. Powdered materials of closely controlled sizes are metered into the gun and are thus accelerated and heated as they pass along the hot high-velocity gas stream. Upon impacting with the substrate at a specific distance from the gun the particles splat and build up upon each other and the substrate to form a highly bonded and dense coating. Various coatings can be produced in this manner but a tungsten carbide 17% cobalt coating is the preferred coating.
4 All flame sprayed coatings to a greater or lesser degree contain microcracks or fissures which are the result of the quench stresses generated as the hot high velocity particles impact upon the substrate. Sometimes these micro-cracks can be extremely small, to such an extent that they are very difficult to discern using normal metallographic techniques. However, these very small cracks can propagate under the superimposed thermally and mechanically generated stresses and unless they can be effectively 'locked' or 'keyed' the coating will eventually fail by progressive spallation. The Monitox coating process induces the growth of oxides within these very small fissures and thus creates a resistance to crack propagation, The Monitox coating is applied in an aqueous slurry form containing various oxides and chemicals, This layer is then dried and heated (up to 500OC) and at this stage is 'soft' in that it is a collection of hard particles which are not very well bonded to each other or to the substrate. Thus, at this stage, excess coating can easily be removed by scraping or sanding operations so as to reveal the peaks of the underlying tungsten carbide coating which, in the 'as sprayed' condition, exhibits a coarse surface somewhat like a coarse sandpaper. Thus, a relatively smooth composite surface can be produced which comprises areas of ceramic and carbide material. This composite surface is then further densified and hardened by a cyclic process of impregnation and further heat treatment; for example from 3 to 10 cycles of impregnation and heat treatment can be required.
When coating the grid plates, it has been found to be surprisingly beneficial to form a pattern of separate islands. It appears that any particular thickness may be applied, but a thickness of approx. 0.38 mm (0.015 inch) is presently preferred. It has been found to be particularly beneficial to deposit the coating in an island pattern in which each island is approx. 5 mm, square or 5 min in diameter and each island is defined at its perimeter by an uncoated band approx. 2 mm wide. The inventor believes that the island pattern allows the coating to accommodate the high thermal stresses which are imposed on the grid plates during service, thus preventing premature coating failure by spallation. A suitable thickness range may be from 0.3 to 0.5 mm. The transverse dimensions of the islands may conveniently be in the range from 4 to 8 mm, the islands being spaced apart by 1 to 3 mm, for example.
The invention will be described further, by way of example with reference to the accompanying drawing, whose sole Figure schematically shows the internal surface of a grid plate.
Example: Process for coating grid plates (1) Degrease the grid plates.
(2) Mask where required.
(3) Grit-blast. (4) Apply WC - 17% Co coating to the fingers of the grid plates by HVOF using masking devices to ensure the requisite 'island pattern'. (5) Re-mask. (6) Apply Monitox slurry.
(7) Fire at approx. 450 to 500'C.
(8) Cool.
(9) Remove excess ceramic.
(10) Impregnate the coatings with oxide or phosphate forming compounds.
(11) Fire at approx. 450 to 5000C. (12)Repeat operations (10) and (11) for 3 to 10 cycles.
The drawing shows a cast iron grid plate 1 with gaps 2, through which cooling water is sprayed, and raised fingers 3 provided with the composite coating 4 made up of a pattern of rectangular islands 5 (approx. 5 mm square, separated by at least 1 mm).
6
Claims (15)
1. A method of protecting a grid plate for a continuous casting machine against wear, the method comprising applying to a strand-confining surface of the grid plate, by flame spraying, a coating consisting of ceramo-metallic material, the coating being in the form of an array of mutually isolated islands of the cerarno-metallic material.
2. A method of protecting a grid plate for a continuous casting machine against wear, the method comprising: a) applying to a strand-confining surface of the grid plate, by flame spraying, a rough first coating consisting of ceraino-metallic material, the first coating being in the form of an array of mutually isolated islands of the ceramo-metallic material, b) applying a ceramic slurry to the islands of ceramo-metallic material; c) heating the ceramic slurry to form a second coating consisting of ceramic material; d) removing excess ceramic material from the second coating to produce a composite ceramo-metallic and ceramic surface; e) impregnating the composite surface with a solution of at least one soluble compound capable of being converted, on heating, into an insoluble substance which bonds the coatings; and f) heating the coatings to cause bonding and densification of the coatings by the said substance; whereby a composite coating is produced which is in the form of an array of mutually isolated islands.
3. A method as claimed in claim 1 or 2, wherein the islands have a thickness of 0.3 - 0.5 mm.
7 4, A method as claimed in any preceding claim, wherein the islands have transverse dimensions in the range
4 - 8 mm.
5. A method as claimed in any preceding claim, wherein the islands are spaced apart by 1 - 3 min.
6. A method as claimed in any preceding claim, wherein the islands are substantially square.
7. A method as claimed in claim 2, wherein the ceramic slurry contains a chromium compound capable of being converted into chromium oxide at temperatures of at least 3000C.
8. A method as claimed in claim 2, wherein the soluble compound is selected from chromia and phosphate forming compounds capable of being converted into oxides and phosphates on heating.
9. A method as claimed in claim 2, wherein the impregnation/heat treatment cycle of steps (e) and (f) is repeated.
10. A method as claimed in any preceding claim, wherein the cerarnometallic material is applied by a high-velocity oxygen - liquid fuel process.
11. A method as claimed in any preceding claim, wherein the ceramometailic material contains a carbide, preferably tungsten carbide.
12. A method as claimed in claim 11, wherein the said material contains cobalt.
8
13. A method of protecting a grid plate for a continuous casting machine, substantially as described herein.
14. A grid plate produced by a method as claimed in any preceding claim.
1C7 Amendments to the claims have been fNed as follows 1. A method of protecting a grid plate for a continuous casting machine against wear, the method comprising applying to a strand-confining surface of the grid plate, by flame spraying, a coating consisting of ceramo-metallic material, the coating being in the form of an array of mutually isolated islands of the ceramo-metallic material.
2. A method of protecting a grid plate for a continuous casting machine against wear, the method comprising: a) applying to a strand-confining surface of the grid plate, by flame spraying, a rough first coating consisting of ceramo-metallic material, the first coating being in the form of an array of mutually isolated islands of the ceramo-metallic material; b) applying a ceramic slurry to the islands of ceramo-metaflic material; c) heating the ceramic slurry to form a second coating consisting of ceramic material; d) removing excess ceramic material from the second coating to produce a composite ceramo-metallic and ceramic surface; e) impregnating the composite surface with a solution of at least one soluble compound capable of being converted, on heating, into an insoluble substance which bonds the coatings; and f) heating the coatings to cause bonding and densification of the coatings by the said substance; whereby a composite coating is produced which is in the form of an array of mutually isolated islands.
3. A method as claimed in claim 1 or 2, wherein the islands have a thickness of 0.3 - 0.5 mm.
/0 4. A method as claimed in any preceding claim, wherein the islands have transverse dimensions in the range 4 - 8 mm.
5. A method as claimed in any preceding claim, wherein the islands are spaced apart by 1 - 3 mTn.
6. A method as claimed in any preceding claim, wherein the islands are substantially square.
7. A method as claimed in claim 2, wherein the ceramic slurry contains ' a chromium compound capable of being converted into chromium oxide at temperatures of at least 2STC.
8. A method as claimed in claim 2, wherein the soluble compound is selected from chromia and phosphate forming compounds capable of being converted into oxides and phosphates on heating Cr 9. A method as claimed M" claim 2, wherein the impregnation/heat treatment cycle of steps (e) and (f) is repeated.
10. A method as claimed in any preceding claim, wherein the ceramometallic material is applied by a high-velocity oxygen - liquid fuel process.
I- 11. A method as claimed in any preceding claim, wherein the ceramometallic material contains a carbide.
12. A method as claimed in claim 11, wherein the said carbide is rmgsten carbide.
13. A method as claimed in claim 11 or 12, wherein the said mateTial contains cobalt.
11 14. A method of protecting a grid plate for a continuous casting machine, substantially as described herein.
15. A grid plate produced by a method as claimed in any preceding claim.
0
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9714452A GB2320034B (en) | 1996-11-08 | 1996-11-08 | Coating of continuous casting machine grid plates |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9714452A GB2320034B (en) | 1996-11-08 | 1996-11-08 | Coating of continuous casting machine grid plates |
GB9623344A GB2319042B (en) | 1996-11-08 | 1996-11-08 | Coating of continuous casting machine components |
Publications (4)
Publication Number | Publication Date |
---|---|
GB9714452D0 GB9714452D0 (en) | 1997-09-10 |
GB2320034A true GB2320034A (en) | 1998-06-10 |
GB2320034A8 GB2320034A8 (en) | 1998-07-13 |
GB2320034B GB2320034B (en) | 1998-11-11 |
Family
ID=10802694
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9714452A Expired - Lifetime GB2320034B (en) | 1996-11-08 | 1996-11-08 | Coating of continuous casting machine grid plates |
GB9623344A Expired - Lifetime GB2319042B (en) | 1996-11-08 | 1996-11-08 | Coating of continuous casting machine components |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9623344A Expired - Lifetime GB2319042B (en) | 1996-11-08 | 1996-11-08 | Coating of continuous casting machine components |
Country Status (10)
Country | Link |
---|---|
EP (1) | EP0946778B1 (en) |
JP (1) | JP2001504162A (en) |
AT (1) | ATE204615T1 (en) |
AU (1) | AU4877597A (en) |
DE (1) | DE69706317T2 (en) |
DK (1) | DK0946778T3 (en) |
ES (1) | ES2163139T3 (en) |
GB (2) | GB2320034B (en) |
PT (1) | PT946778E (en) |
WO (1) | WO1998021379A1 (en) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6284682B1 (en) * | 1999-08-26 | 2001-09-04 | The University Of British Columbia | Process for making chemically bonded sol-gel ceramics |
CH694010A5 (en) * | 1999-09-03 | 2004-06-15 | Concast Standard Ag | Continuous casting with wear. |
FR2807071B1 (en) | 2000-03-28 | 2002-11-15 | Dja Dodane Jean Et Associes | CERAMO-METALLIC ANTI-ADHESIVE COATING FOR CULINARY UTENSILS |
DE10345865A1 (en) * | 2003-10-01 | 2005-04-21 | Km Europa Metal Ag | Process for coating a mold body used in a continuous casting plant and mold body of a continuous casting plant |
CN101530904B (en) * | 2009-04-03 | 2010-11-10 | 西安交通大学 | Composite material hammerhead of crusher and negative pressure casting method thereof |
CN113186479B (en) * | 2021-04-13 | 2022-02-01 | 杭州九阳小家电有限公司 | Pot and manufacturing method thereof |
CN114381682A (en) * | 2022-01-17 | 2022-04-22 | 马鞍山钢铁股份有限公司 | Method for improving wear resistance of Y-shaped crystallizer copper plate |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4446199A (en) * | 1982-07-30 | 1984-05-01 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Overlay metallic-cermet alloy coating systems |
JPS60118362A (en) * | 1983-11-30 | 1985-06-25 | Nippon Steel Corp | Billet supporting device for continuous casting |
JPH0275447A (en) * | 1988-09-09 | 1990-03-15 | Nomura Techno Res Kk | Mold for continuous casting |
GB2269392A (en) * | 1992-08-06 | 1994-02-09 | Monitor Coatings & Eng | Coating of components with final impregnation with chromia or phosphate forming compound |
WO1994007611A1 (en) * | 1992-10-01 | 1994-04-14 | Motorola, Inc. | Method for forming circuitry by a spraying process with stencil |
US5499672A (en) * | 1994-06-01 | 1996-03-19 | Chuetsu Metal Works Co., Ltd. | Mold for continuous casting which comprises a flame sprayed coating layer of a tungsten carbide-based wear-resistant material |
Family Cites Families (12)
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US2689803A (en) * | 1951-11-03 | 1954-09-21 | Pittsburgh Plate Glass Co | Method of producing a film of uniform electroconductivity on refractory bases |
NL6616433A (en) * | 1965-11-29 | 1967-05-30 | ||
GB1570348A (en) * | 1977-04-28 | 1980-07-02 | British Steel Corp | Coated graphite dies |
US4410564A (en) * | 1981-10-19 | 1983-10-18 | Raivi S.A. | Manufacturing process for heat emitting plates |
GB8400661D0 (en) * | 1984-01-11 | 1984-02-15 | Singer A R E | Spray deposition of metal |
GB2154614B (en) * | 1984-02-22 | 1987-11-18 | H I P | Densified coatings by application of direct fluid pressure |
JPS60221151A (en) * | 1984-04-18 | 1985-11-05 | Kawasaki Steel Corp | Continuous casting mold and formation of thermally sprayed film on inside surface of mold |
US4577431A (en) * | 1984-05-02 | 1986-03-25 | General Electric Company | Wear resistant gun barrel and method of forming |
JPS60240993A (en) * | 1984-05-14 | 1985-11-29 | Kobe Steel Ltd | Outside tube evaporating type heat transfer tube and manufacturing thereof |
WO1990000945A1 (en) * | 1988-07-22 | 1990-02-08 | Satosen Co., Ltd. | Mold for continuously casting steel |
SU1738869A1 (en) * | 1989-12-28 | 1992-06-07 | Центральный институт повышения квалификации кадров авиационной промышленности | Method for formation of coatings |
JP3080651B2 (en) * | 1991-11-29 | 2000-08-28 | 日鉄ハード株式会社 | Method for producing immersion member for molten metal bath |
-
1996
- 1996-11-08 GB GB9714452A patent/GB2320034B/en not_active Expired - Lifetime
- 1996-11-08 GB GB9623344A patent/GB2319042B/en not_active Expired - Lifetime
-
1997
- 1997-11-07 WO PCT/GB1997/003073 patent/WO1998021379A1/en active IP Right Grant
- 1997-11-07 AT AT97911364T patent/ATE204615T1/en active
- 1997-11-07 PT PT97911364T patent/PT946778E/en unknown
- 1997-11-07 JP JP52229398A patent/JP2001504162A/en not_active Ceased
- 1997-11-07 DE DE69706317T patent/DE69706317T2/en not_active Expired - Lifetime
- 1997-11-07 EP EP97911364A patent/EP0946778B1/en not_active Expired - Lifetime
- 1997-11-07 ES ES97911364T patent/ES2163139T3/en not_active Expired - Lifetime
- 1997-11-07 AU AU48775/97A patent/AU4877597A/en not_active Abandoned
- 1997-11-07 DK DK97911364T patent/DK0946778T3/en active
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4446199A (en) * | 1982-07-30 | 1984-05-01 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Overlay metallic-cermet alloy coating systems |
JPS60118362A (en) * | 1983-11-30 | 1985-06-25 | Nippon Steel Corp | Billet supporting device for continuous casting |
JPH0275447A (en) * | 1988-09-09 | 1990-03-15 | Nomura Techno Res Kk | Mold for continuous casting |
GB2269392A (en) * | 1992-08-06 | 1994-02-09 | Monitor Coatings & Eng | Coating of components with final impregnation with chromia or phosphate forming compound |
WO1994007611A1 (en) * | 1992-10-01 | 1994-04-14 | Motorola, Inc. | Method for forming circuitry by a spraying process with stencil |
US5499672A (en) * | 1994-06-01 | 1996-03-19 | Chuetsu Metal Works Co., Ltd. | Mold for continuous casting which comprises a flame sprayed coating layer of a tungsten carbide-based wear-resistant material |
Non-Patent Citations (2)
Title |
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Japio Abstract of JP 02 075447 A * |
Japio Abstract of JP 60 118362 A * |
Also Published As
Publication number | Publication date |
---|---|
GB2320034B (en) | 1998-11-11 |
GB2319042B (en) | 1998-11-11 |
ATE204615T1 (en) | 2001-09-15 |
PT946778E (en) | 2002-02-28 |
GB9623344D0 (en) | 1997-01-08 |
EP0946778A1 (en) | 1999-10-06 |
WO1998021379A1 (en) | 1998-05-22 |
ES2163139T3 (en) | 2002-01-16 |
DK0946778T3 (en) | 2001-12-17 |
JP2001504162A (en) | 2001-03-27 |
EP0946778B1 (en) | 2001-08-22 |
GB2320034A8 (en) | 1998-07-13 |
DE69706317T2 (en) | 2002-05-16 |
AU4877597A (en) | 1998-06-03 |
GB9714452D0 (en) | 1997-09-10 |
GB2319042A (en) | 1998-05-13 |
DE69706317D1 (en) | 2001-09-27 |
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