EP0030055A1 - Method for producing an improved layer, particular for a drill bit - Google Patents
Method for producing an improved layer, particular for a drill bit Download PDFInfo
- Publication number
- EP0030055A1 EP0030055A1 EP19800201107 EP80201107A EP0030055A1 EP 0030055 A1 EP0030055 A1 EP 0030055A1 EP 19800201107 EP19800201107 EP 19800201107 EP 80201107 A EP80201107 A EP 80201107A EP 0030055 A1 EP0030055 A1 EP 0030055A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- layer
- drill bit
- core member
- nickel
- wear
- 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
- 238000004519 manufacturing process Methods 0.000 title claims description 4
- 239000000843 powder Substances 0.000 claims abstract description 18
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims abstract description 16
- 238000000034 method Methods 0.000 claims abstract description 15
- 239000000463 material Substances 0.000 claims abstract description 13
- 229910052759 nickel Inorganic materials 0.000 claims abstract description 8
- 238000005245 sintering Methods 0.000 claims abstract description 7
- 238000007751 thermal spraying Methods 0.000 claims abstract description 6
- 229910000851 Alloy steel Inorganic materials 0.000 claims abstract description 5
- 239000011435 rock Substances 0.000 claims description 6
- 230000036346 tooth eruption Effects 0.000 claims description 6
- 238000010438 heat treatment Methods 0.000 claims description 4
- 239000007787 solid Substances 0.000 claims description 4
- 229910000831 Steel Inorganic materials 0.000 claims description 2
- 238000005553 drilling Methods 0.000 claims description 2
- 239000010959 steel Substances 0.000 claims description 2
- 239000000919 ceramic Substances 0.000 description 2
- 238000007750 plasma spraying Methods 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 229910001209 Low-carbon steel Inorganic materials 0.000 description 1
- 230000001427 coherent effect Effects 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 238000005488 sandblasting Methods 0.000 description 1
- 238000004904 shortening Methods 0.000 description 1
Images
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
- C23C4/18—After-treatment
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
- B22F7/06—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
-
- E—FIXED CONSTRUCTIONS
- E21—EARTH OR ROCK DRILLING; MINING
- E21B—EARTH OR ROCK DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
- E21B10/00—Drill bits
- E21B10/46—Drill bits characterised by wear resisting parts, e.g. diamond inserts
- E21B10/50—Drill bits characterised by wear resisting parts, e.g. diamond inserts the bit being of roller type
- E21B10/52—Drill bits characterised by wear resisting parts, e.g. diamond inserts the bit being of roller type with chisel- or button-type inserts
Definitions
- the invention relates to a method for producing an object on which an exterior layer is applied by thermal spraying, followed by a heat treatment, and to an object, in particular a drill bit, obtained pursuant to this method.
- the invention accordingly procures a method of the type mentioned at the beginning, characterized in that on a core member is applied, by cold isostatic compacting, a layer of a suitable powder material, followed by sintering, after which the exterior layer, which is a wear-resistant layer, is applied and then the structure thus obtained is isostatically compacted hot.
- a suitable powder material for this purpose is a nickel-containing alloy steel powder with preferably 3.5% nickel therein.
- the invention in addition procures a drill bit with cutting teeth provided with a wear-resistant layer, for drilling in rock.
- a supply of powder material is introduced into a rubber mold and distributed, after which the core member, which is usually a type of steel suitable for a bearing, is placed in the powder, following which the powder is pressed on.
- the core member may alternatively be placed in the mold first, after which the powder material is introduced and pressed on.
- the mold is closed and is then isostatically compacted cold until a coherent member having a density of approximately 90% is obtained.
- the compact removed from the mold is then sintered in a furnace. After cooling the sintered object is coated with a wear-resistant layer by thermal spraying, for example plasma spraying, after which the structure thus obtained is isostatically compacted hot.
- This hot isostatic compacting may be done by inserting the entire object in a thin- walled deep-drawn vessel or container of low-carbon steel having a wall thickness of approximately 0.5 mm, filled with a ceramic powder. This vessel is then heated and placed under pressure on all sides. After hot isostatic compacting the object may be readily separated from the surrounding ceramic mass and cleaned by sand blasting. This method proves to procure components with accurately shaped dimensions comparable to those of a forged product.
- the drill bit 1 shown in Fig. 1 is composed of a core member 3 , made of a bearing material, in which are applied the races 2 for the folling elements(not shown).
- a core member 3 made of a bearing material, in which are applied the races 2 for the folling elements(not shown).
- the preformed drill bit, isostatically compacted cold is removed from the mold and sintered in a sintering furnace at a temperature of approx. 1200°C at 1 atmosphere under reduction by hydrogen for approx. I hour, which operations lead to a density of approx. 90% of the compacted material.
- the wear-resistant layer 5 is applied on the layer 4 and the object obtained is then inserted into a vessel or container and isostatically compacted hot under a pressure of for example approx. 1600 atmospheres and at a temperature of approx. 1100°C for at least 2 ! hours.
- This operation results in a density of the layers 4 and 5 of 99% and a very solid bond between the layers.
- the original solid core member 3 after mechanical operations and heat treatment, acquires the shape, as represented in Fig. 1, in which the races 2 of the rolling elements are supplied.
- a device such as a drill bit, which in principle consists of three parts, namely, a significantly improved cutting part 5, a supporting part 4 and a core or bearing part 3, which parts are combined in an economically and technically advantageous manner such that the said drill bit satisfies the requirements set.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Mining & Mineral Resources (AREA)
- Life Sciences & Earth Sciences (AREA)
- Geology (AREA)
- Physics & Mathematics (AREA)
- Materials Engineering (AREA)
- Environmental & Geological Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Plasma & Fusion (AREA)
- Fluid Mechanics (AREA)
- Manufacturing & Machinery (AREA)
- Composite Materials (AREA)
- General Life Sciences & Earth Sciences (AREA)
- Geochemistry & Mineralogy (AREA)
- Earth Drilling (AREA)
- Powder Metallurgy (AREA)
- Coating By Spraying Or Casting (AREA)
Abstract
Description
- Method for producing an object on which an exterior layer is applied by thermal spraying and object, in particular a drill bit, obtained pursuant to this method. f
- The invention relates to a method for producing an object on which an exterior layer is applied by thermal spraying, followed by a heat treatment, and to an object, in particular a drill bit, obtained pursuant to this method.
- Such a method is disclosed in British Patent 1,367,762. In application of the method described above to objects wherein it is required that the exterior layer applied be capable, in operation, of withstanding great variable forces, for example, that it must be resistant to wear, however, it happens that this layer sometimes chips off, thus shortening the life of the object obtained.
- The invention accordingly procures a method of the type mentioned at the beginning, characterized in that on a core member is applied, by cold isostatic compacting, a layer of a suitable powder material, followed by sintering, after which the exterior layer, which is a wear-resistant layer, is applied and then the structure thus obtained is isostatically compacted hot.
- It has been found that a suitable powder material for this purpose is a nickel-containing alloy steel powder with preferably 3.5% nickel therein.
- The invention in addition procures a drill bit with cutting teeth provided with a wear-resistant layer, for drilling in rock.
- For the performance of a method pursuant to the invention a supply of powder material is introduced into a rubber mold and distributed, after which the core member, which is usually a type of steel suitable for a bearing, is placed in the powder, following which the powder is pressed on. The core member may alternatively be placed in the mold first, after which the powder material is introduced and pressed on. The mold is closed and is then isostatically compacted cold until a coherent member having a density of approximately 90% is obtained. The compact removed from the mold is then sintered in a furnace. After cooling the sintered object is coated with a wear-resistant layer by thermal spraying, for example plasma spraying, after which the structure thus obtained is isostatically compacted hot. This hot isostatic compacting may be done by inserting the entire object in a thin- walled deep-drawn vessel or container of low-carbon steel having a wall thickness of approximately 0.5 mm, filled with a ceramic powder. This vessel is then heated and placed under pressure on all sides. After hot isostatic compacting the object may be readily separated from the surrounding ceramic mass and cleaned by sand blasting. This method proves to procure components with accurately shaped dimensions comparable to those of a forged product.
- When a drill bit for rock is produced in this fashion, after sintering not the entire surface of the cutting teeth but only the parts thereof which come directly into contact with the rock are coated with the wear-resistant layer by thermal spraying. Following the selective application of the wear-resistant layer the preformed drill bit is subjected in its entirety to hot isostatic compacting, as described above.
- The invention is now explained in greater detail by means of the accompanying drawing, which represents a preferred embodiment of the invention.
- Fig. 1 is a cross section of a drill bit produced according to the invention.
- Fig. 2 is a perspective view of a portion of this drill bit.
- The drill bit 1 shown in Fig. 1 is composed of a core member 3 , made of a bearing material, in which are applied the races 2 for the folling elements(not shown). On this core member 3, solid at the beginning, is applied, in a rubber mold, a
layer 4 of powder, which combination is isostatically compacted cold. This operation takes place preferably under a pressure of approximately 6000 atmospheres at room temperature. Then the preformed drill bit, isostatically compacted cold, is removed from the mold and sintered in a sintering furnace at a temperature of approx. 1200°C at 1 atmosphere under reduction by hydrogen for approx. I hour, which operations lead to a density of approx. 90% of the compacted material. Then, by means of plasma spraying technique, the wear-resistant layer 5 is applied on thelayer 4 and the object obtained is then inserted into a vessel or container and isostatically compacted hot under a pressure of for example approx. 1600 atmospheres and at a temperature of approx. 1100°C for at least 2 ! hours. This operation results in a density of the 4 and 5 of 99% and a very solid bond between the layers.layers - It will be found by the method pursuant to the invention that the mechanical properties of the drill bit thus formed are greatly improved, like the bond between the
4 and 5, on the one hand, and thelayers layer 4 and the core member 3, on the other. By this means the desired effect of very high resistance to wear and resistance to chipping of the cutting teeth is obtained, combined with a core member which functionally has other possible applications, such as, for example, the function of a bearing. - It is noted that the original solid core member 3, after mechanical operations and heat treatment, acquires the shape, as represented in Fig. 1, in which the races 2 of the rolling elements are supplied.
- It may be seen further from Fig. 2 that not the entire surface of the cutting teeth of the drill bit is provided with the wear-
resistant layer 5, but that the wear-resistant layer is applied only on the places where the tooth comes directly into contact with rock during operation. - Thus there is procured by the invention a device, such as a drill bit, which in principle consists of three parts, namely, a significantly improved
cutting part 5, a supportingpart 4 and a core or bearing part 3, which parts are combined in an economically and technically advantageous manner such that the said drill bit satisfies the requirements set.
Claims (10)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| NL7908745 | 1979-12-04 | ||
| NL7908745A NL7908745A (en) | 1979-12-04 | 1979-12-04 | METHOD FOR MANUFACTURING AN ARTICLE APPLIED BY THERMAL SPRAYING AND OBJECT, IN PARTICULAR A DRILLING CHISEL, OBTAINED BY THIS METHOD |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP0030055A1 true EP0030055A1 (en) | 1981-06-10 |
| EP0030055B1 EP0030055B1 (en) | 1985-09-18 |
Family
ID=19834277
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP19800201107 Expired EP0030055B1 (en) | 1979-12-04 | 1980-11-24 | Method for producing an improved layer, particular for a drill bit |
Country Status (6)
| Country | Link |
|---|---|
| EP (1) | EP0030055B1 (en) |
| JP (1) | JPS5697093A (en) |
| AU (1) | AU539718B2 (en) |
| CA (1) | CA1162182A (en) |
| DE (1) | DE3071100D1 (en) |
| NL (1) | NL7908745A (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0089155A3 (en) * | 1982-03-05 | 1983-12-07 | Rolls-Royce Plc | Composite articles and a method for their manufacture |
| FR2546448A1 (en) * | 1983-05-25 | 1984-11-30 | Maschf Augsburg Nuernberg Ag | COATED METALLIC OBJECT AND METHOD FOR MANUFACTURING THE SAME |
| EP0169717A3 (en) * | 1984-07-23 | 1986-12-30 | Cdp, Ltd. | Rolling cutters for drill bits, and processes to produce same |
| EP0322224A3 (en) * | 1987-12-23 | 1990-03-07 | Precision Castparts Corp. | Method of forming a metal article from powdered metal |
| WO1999023272A1 (en) * | 1997-11-03 | 1999-05-14 | Siemens Aktiengesellschaft | Method for producing a protective coating on a base body intended to be impinged upon by a hot gas and corresponding product |
| GB2376242A (en) * | 2001-05-01 | 2002-12-11 | Smith International | Roller cone bits with wear and fracture resistant coatings |
| WO2002077314A3 (en) * | 2001-03-26 | 2004-03-11 | Bodycote Imt Inc | Corrosion resistant component and method for fabricating same |
| RU2238346C1 (en) * | 2003-01-20 | 2004-10-20 | Гончаров Виталий Степанович | Gaseous thermal spraying method |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4597456A (en) * | 1984-07-23 | 1986-07-01 | Cdp, Ltd. | Conical cutters for drill bits, and processes to produce same |
| DE19747385A1 (en) * | 1997-10-27 | 1999-04-29 | Linde Ag | Manufacture of molded parts |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| NL54863C (en) * | 1900-01-01 | |||
| FR1434158A (en) * | 1964-11-25 | 1966-04-08 | Sfec | Improvements to refractory protective coatings, and method of manufacturing these elements |
| GB1367762A (en) * | 1971-09-17 | 1974-09-25 | Ass Eng Ltd | cermet materials |
| US3882581A (en) * | 1974-03-13 | 1975-05-13 | Minnesota Mining & Mfg | Coated, partially laminated carbide cutting tool insert |
| NL7703234A (en) * | 1977-03-25 | 1978-09-27 | Skf Ind Trading & Dev | METHOD FOR MANUFACTURING A DRILL CHUCK INCLUDING HARD WEAR-RESISTANT ELEMENTS, AND DRILL CHAPTER MADE ACCORDING TO THE METHOD |
| NL7804454A (en) * | 1978-04-26 | 1979-10-30 | Skf Ind Trading & Dev | METHOD OF APPLYING A DENSE LAYER OF CERAMIC METAL OR CERMETS ON A METAL ARTICLE |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5347307A (en) * | 1976-10-13 | 1978-04-27 | Tone Boring Co | Tricone bit cone and process for production thereof |
-
1979
- 1979-12-04 NL NL7908745A patent/NL7908745A/en not_active Application Discontinuation
-
1980
- 1980-11-14 AU AU64386/80A patent/AU539718B2/en not_active Ceased
- 1980-11-24 EP EP19800201107 patent/EP0030055B1/en not_active Expired
- 1980-11-24 DE DE8080201107T patent/DE3071100D1/en not_active Expired
- 1980-12-03 JP JP16970880A patent/JPS5697093A/en active Granted
- 1980-12-03 CA CA000366074A patent/CA1162182A/en not_active Expired
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| NL54863C (en) * | 1900-01-01 | |||
| FR1434158A (en) * | 1964-11-25 | 1966-04-08 | Sfec | Improvements to refractory protective coatings, and method of manufacturing these elements |
| GB1367762A (en) * | 1971-09-17 | 1974-09-25 | Ass Eng Ltd | cermet materials |
| US3882581A (en) * | 1974-03-13 | 1975-05-13 | Minnesota Mining & Mfg | Coated, partially laminated carbide cutting tool insert |
| FR2263991A1 (en) * | 1974-03-13 | 1975-10-10 | Minnesota Mining & Mfg | |
| NL7703234A (en) * | 1977-03-25 | 1978-09-27 | Skf Ind Trading & Dev | METHOD FOR MANUFACTURING A DRILL CHUCK INCLUDING HARD WEAR-RESISTANT ELEMENTS, AND DRILL CHAPTER MADE ACCORDING TO THE METHOD |
| NL7804454A (en) * | 1978-04-26 | 1979-10-30 | Skf Ind Trading & Dev | METHOD OF APPLYING A DENSE LAYER OF CERAMIC METAL OR CERMETS ON A METAL ARTICLE |
| EP0005285A1 (en) * | 1978-04-26 | 1979-11-14 | SKF Industrial Trading & Development Co, B.V. | Process for applying a dense layer of cermets or cemented carbides to a metal object |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0089155A3 (en) * | 1982-03-05 | 1983-12-07 | Rolls-Royce Plc | Composite articles and a method for their manufacture |
| FR2546448A1 (en) * | 1983-05-25 | 1984-11-30 | Maschf Augsburg Nuernberg Ag | COATED METALLIC OBJECT AND METHOD FOR MANUFACTURING THE SAME |
| EP0169717A3 (en) * | 1984-07-23 | 1986-12-30 | Cdp, Ltd. | Rolling cutters for drill bits, and processes to produce same |
| EP0322224A3 (en) * | 1987-12-23 | 1990-03-07 | Precision Castparts Corp. | Method of forming a metal article from powdered metal |
| WO1999023272A1 (en) * | 1997-11-03 | 1999-05-14 | Siemens Aktiengesellschaft | Method for producing a protective coating on a base body intended to be impinged upon by a hot gas and corresponding product |
| WO2002077314A3 (en) * | 2001-03-26 | 2004-03-11 | Bodycote Imt Inc | Corrosion resistant component and method for fabricating same |
| US6878412B2 (en) | 2001-03-26 | 2005-04-12 | Bodycote Imt, Inc. | Corrosion resistant component and method for fabricating same |
| GB2376242A (en) * | 2001-05-01 | 2002-12-11 | Smith International | Roller cone bits with wear and fracture resistant coatings |
| US6615935B2 (en) | 2001-05-01 | 2003-09-09 | Smith International, Inc. | Roller cone bits with wear and fracture resistant surface |
| GB2376242B (en) * | 2001-05-01 | 2005-11-23 | Smith International | Roller cone bits with wear and fracture resistant surface |
| RU2238346C1 (en) * | 2003-01-20 | 2004-10-20 | Гончаров Виталий Степанович | Gaseous thermal spraying method |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS6343550B2 (en) | 1988-08-31 |
| CA1162182A (en) | 1984-02-14 |
| DE3071100D1 (en) | 1985-10-24 |
| AU539718B2 (en) | 1984-10-11 |
| JPS5697093A (en) | 1981-08-05 |
| AU6438680A (en) | 1981-06-11 |
| NL7908745A (en) | 1981-07-01 |
| EP0030055B1 (en) | 1985-09-18 |
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