A method of making abrasive bodies
13 claims: 13 independent, 0 dependent
- 1A method of making an abrasive body comprising an abrasive compact, a backing of cemented carbide bonded to the abrasive compact, and a metal-containing substrate bonded to the backing through a bonding layer comprising nickel, copper, cobalt, iron or an alloy containing one or more of these metals, including the steps of:(a) providing a composite abrasive compact comprising an abrasive compact bonded to a cemented carbide backing;(b) depositing a layer of nickel, copper, cobalt, iron or an alloy containing one or more of these metals on a surface of a metal-containing substrate, applying a transverse pressure to the layer, raising the temperature of the layer to a temperature below its melting point and maintaining the pressure and temperature for a period sufficient to enable the layer to bond to the substrate;(c) polishing the exposed surface of the metal layer;(d) bringing the backing and substrate together so that the metal layer contacts a surface of the backing;(e) urging the backing and substrate together by applying a tranverse pressure thereto;(f) raising the temperature of the metal layer to a suitable temperature below its melting point;and(g) maintaining the pressure and temperature for a time sufficient to cause diffusion bonding between the backing and the substrate steps (f) and (g) being carried out in an inert atmosphere. 1. Procédé de fabrication d'un corps abrasif comportant un aggloméré abrasif, un support de carbure cémenté lié à l'agglomeré abrasif, et un substrat contenant un métal et lié au support par l'intermédiaire d'une couche de liaison comprenant du nickel, du cuivre, du cobalt, du fer ou un alliage de l'un ou plusieures des ces métaux, incluant les étapes suivantes: (a) fourniture d'un aggloméré abrasif composite comportant un aggloméré abrasif lié à un support de carbure cémenté;(b) dépôt d'une couche de nickel, cuivre, cobalt, fer ou d'un alliage contenant un ou plusieurs de ces métaux sur une surface du substrat contenant un métal, application d'une pression transversale à cette couche, élévation de la température de la couche à un niveau situé en dessous de son point de fusion et maintien de cette température et de cette pression pendant un laps de temps suffisant pour assurer la liaison de la couche au substrat;(c) polissage de la surface exposée de la couche métallique;(d) mise en contact du support et du substrat de manière que la couche métallique soit en contact avec une surface du support;(e) pressage conjoint du support et du substrat en leur appliquant une pression transversale;(f) élévation de la température de la couche métallique à un niveau convenable situé en dessous de son point de fusion;et(g) maintien de la pression et de la température pendant un temps suffisant pour provoquer la liaison par diffusion du support et du substrat, les étapes (f) et (g) étant effectuées en atmosphère inerte. 1. Verfahren zur Herstellung von Schleifkörpern mit einem Schleif-Compact, einer mit dem Schleif-Compact verbundenen Rückschicht aus Sintercarbid und einem metallhaltigen, mit der Rückschicht durch eine bindende Schicht, die Nickel, Kupfer, Cobalt, Eisen oder eine eines oder mehrere dieser Metalle enthaltende Legierung enthält, verbundenen Substrat, wobei das Verfahren die folgenden Schritte umfaßt: (a) Bereitstellen eines Verbund - Schleif - Compacts aus einem Schleif-Compact, der mit einer Rückschicht aus Sintercarbid verbunden ist;(b) Abscheiden einer Schicht aus Nickel, Kupfer, Cobalt, Eisen oder einer eines oder mehrere dieser Metalle enthaltenden Legierung auf einer Oberfläche des metallhaltigen Substrats, Einwirkenlassen eines transversalen Drucks auf die Schicht, Erhöhen der Temperatur der Schicht auf eine Temperatur unterhalb ihres Schmelzpunktes und Aufrechterhalten des Druckes und der Temperatur während einer ausreichenden Zeitspanne, um die Bindung der Schicht an das Substrat zu ermöglichen;(c) Polieren der freiliegenden Oberfläche der Metall-Schicht;(d) Zusammenbringen der Rückschicht und des Substrats, so daß die Metall-Schicht mit der Oberfläche der Rückschicht in Berührung gelangt;(e) zwangsweises Zusammendrücken von Rückschicht und Substrat durch Einwirkenlassen eines transversalen Drucks darauf;(f) Erhöhen der Temperatur der Metall-Schicht auf eine geeignete Temperatur unterhalb ihres Schmelzpunktes;und(g) Aufrechterhalten des Druckes und der Temperatur während einer ausreichenden Zeitspanne, um eine Diffusionsverbindung zwischen der Rückschicht und dem Substrat zu bewirken, wobei die Schritte (f) und (g) in einer inerten Atmosphäre durchgeführt werden.
- 2A method of claim 1 wherein in step (g) the transverse pressure applied to the backing and substrate is in the range 40 to 300 N/mm2. 2. Procédé selon la revendication 1, caractérisé en ce que dans l'étape (g) la pression transversale appliquée au support et au substrat se situe dans la gamme de 40 à 300 N/mm2. 2. Verfahren nach Anspruch 1, dadurch gekennzeichnet, daß in Schritt (g) der auf die Rückschicht und das Substrat zur Einwirkung gebrachte transversale Druck im Bereich von 40 bis 300 N/mm2 liegt.
- 3A method of claim 1 or claim 2 wherein in the step (g) the temperature to which the metal layer is raised is in the range 650 to 750°C. 3. Procédé selon la revendication 1 ou la revendication 2, caractérisé en ce que dans l'étape (g) la température à laquelle est élevée la couche métallique se situe dans la gamme de 650°C à 750°C. 3. Verfahren nach Anspruch 1 oder Anspruch 2, dadurch gekennzeichnet, daß in Schritt (g) die erhöhte Temperatur, auf die die Metallschicht gebracht wird, im Bereich von 650°C bis 750°C liegt.
- 4A method of any one of the claims 1 to 3 wherein in step (g) the pressure and temperature are maintained for a period of 5 to 300 minutes. 4. Procédé selon l'une quelconque des revendications 1 à 3, caractérisé en ce que dans l'étape (g) la pression et la température sont maintenues pendant une période de 5 à 300 minutes. 4. Verfahren nach irgendeinem der Ansprüche 1 bis 3, dadurch gekennzeichnet, daß in Schritt (g) der Druck und die Temperatur eine Zeitspanne von 5 bis 300 min aufrechterhalten werden.
- 5A method of claim 4 wherein the pressure and temperature are maintained for a period of 5 to 35 minutes. 5. Procédé selon la revendication 4 caractérisé en ce que la pression et la température sont maintenues pendant une période de 5 à 35 minutes. 5. Verfahren nach Anspruch 4, dadurch gekennzeichnet, daß der Druck und die Temperatur eine Zeitspanne von 5 bis 35 min aufrechterhalten werden.
- 6A method according to any one of claims 1 to 5 wherein the substrate and backing after having been brought together in step (d) are placed in the cavity of an assembly comprising a surround body having a cavity formed therein and an expansion body located in the cavity and having a coefficient of thermal expansion greater than that of the surround body, and the temperature of the assembly raised to the desired temperature of step (f) thereby causing the expansion body to expand and apply the desired transverse pressure of step (e) to the backing and substrate. 6. Procédé selon l'une quelconque des revendications 1 à 5, caractérisé en ce que le substrat et le support après avoir été mis ensemble dans l'étape (d) sont placés dans la cavité d'un montage comportant un corps d'entourage muni lui même d'une cavité intérieure et un corps de dilatation logé dans celle ci et possédant un coefficient de dilatation thermique plus grand que celui du corps d'entourage, et en ce que la température de montage est élevée au niveau souhaité de l'étape (f) dans le but de provoquer la dilatation du corps de dilatation et permettre l'application dans l'étape (e) de la pression transversale souhaitée au support et au substrat. 6. Verfahren nach irgendeinem der Ansprüche 1 bis 5, dadurch gekennzeichnet, daß das Substrat und die Rückschicht, nachdem sie in Schritt (d) zusammengebracht wurden, in den Hohlraum einer Vorrichtung gebracht werden, die einen Hüllkörper mit einem darin ausgebildeten Hohlraum und einen in dem Hohlraum befindlichen Expansionskörper umfaßt, der einen größeren thermischen Ausdehnungskoeffizienten als der Hüllkörper gewünschte Temperatur des Schrittes (f) erhöht wird, wodurch bewirkt wird, daß der Expansionskörper sich ausdehnt und den gewünschten transversalen Druck des Schrittes (e) auf die Rückschicht und das Substrat zur Einwirkung bringt.
- 7A method according to claim 6 wherein the temperature of the assembly is raised by placing it in a furnace. 7. Procédé selon la revendication 6, caractérisé en ce que la température du montage est élevée en le plaçant dans un four. 7. Verfahren nach Anspruch 6, dadurch gekennzeichnet, daß die Temperatur der Vorrichtung dadurch erhöht wird, daß sie in einen Ofen gestellt wird.
- 8A method according to claim 6 or claim 7 wherein the surround body is made of cemented carbide or a ceramic based on silicon nitride or zirconia. 8. Procédé selon la revendications 6 ou la revendication 7, caractérisé en ce que le corps d'entourage est fait en carbure cémenté ou en céramique à base de nitrure de silicium ou de zircone. 8. Verfahren nach Anspruch 6 oder Anspruch 7, dadurch gekennzeichnet, daß der Hüllkörper aus Sintercarbid oder einer Keramik auf der Basis von Siliciumnitrid oder Zirconiumdioxid besteht.
- 9A method according to any one of claims 6 to 8 wherein the expansion body is made of Nimonic (RTM). 9. Procédé selon l'une quelconque des revendications 6 à 8, caractérisé en ce que le corps de dilatation est fait en Nimonic (M.D.). 9. Verfahren nach irgendeinem der Ansprüche 6 bis 8, dadurch gekennzeichnet, daß der Expansionskörper aus Nimonic (eingetr. Warenzeichen) besteht.
- 10A method of any one of the preceding claims wherein in step (b) the pressure applied to the metal layer is in the range 1 to 200 N/mm. 10. Procédé selon l'une quelconque des revendications précédentes, caractérisé en ce que dans l'étape (b) la pression appliquée à la couche métallique se situe dans la gamme de 1 à 200 M/mm2. 10. Verfahren nach irgendeinem der vorhergehenden Ansprüche, dadurch gekennzeichnet, daß in Schritt (b) der auf die Metall-Schicht zur Einwirkung gebrachte transversale Druck im Bereich von 1 bis 200 N/mm2 liegt.
- 11A method of any one of the preceding claims wherein in step (b) the temperature to which the metal layer is raised is in the range 700°C to 1100°C. 11. Procédé selon l'une quelconque des revendications precédentes, caractérisé en ce que dans l'étape (b) la température à laquelle la couche métallique est élevée se situe dans la gamme allant de 700°C à 1100°C. 11. Verfahren nach irgendeinem der vorhergehenden Ansprüche, dadurch gekennzeichnet, daß in Schritt (b) die erhöhte Temperatur, auf die die Metallschicht gebracht wird, im Bereich von 700°C bis 1100°C liegt.
- 12A method of any one of the preceding claims wherein in step (b) the pressure and temperature applied to the metal layer are maintained for a period of 5 to 300 minutes. 12. Procédé selon l'une quelconque des revendications précédentes, caractérisé en ce que dans l'étape (b) la pression et la temperature appliquées à la couche métallique sont maintenues pendant une période de 5 à 300 minutes. 12. Verfahren nach irgendeinem der vorhergehenden Ansprüche, dadurch gekennzeichnet, daß in Schritt (b) der Druck und die Temperatur, die auf die Metallschicht zur Einwirkung gebracht werden, eine Zeitspanne von 5 bis 300 min aufrechterhalten werden.
- 13A method of any one of the preceding claims wherein in step (b) the pressure and temperature applied to the metal layer are maintained for a period of 5 to 30 minutes. 13. Procédé selon l'une quelconque des revendications précédentes, caractérisé en ce que dans l'étape (b) la pression et la température appliquées à la couche métallique sont maintenues pendant une période de 5 à 30 minutes. 13. Verfahren nach irgendeinem der vorhergehenden Ansprüche, dadurch gekennzeichnet, daß in Schritt (b) der Druck und did Temperatur, die auf die Metallschicht zur Einwirkung gebracht werden, eine Zeitspanne von 5 bis 35 min aufrechterhalten werden.
Independent claims13
44 paragraphs, as filed
Background of the invention
This invention relates to a method of making an abrasive body.
One type of insert or cutting element for drill crowns currently available on the market consists of a diamond compact bonded to a support backing of metal bonded (cemented) carbide which in turn is bonded to a larger substrate of metal bonded carbide by means of a brazing filler metal. The brazing filler metal has a melting point above 700°C to ensure that a good bond is achieved and maintained between the substrate and backing during the severe conditions which will prevail during use of the drill crown. Care must be exercised during the manufacture of the inserts to ensure that degradation of the diamond compact layer does not occur during brazing of the backing to the substrate. This may be achieved by placing the diamond compact in contact with a heat sink during the brazing.
Description of the drawings
<ul id="ul0001" list-style="none"><li>Figure 1 illustrates a side view of an embodiment of an abrasive body of the invention;</li><li>Figure 2 illustrates a sectional side view of an assembly for use in the method of the invention; and</li><li>Figure 3 illustrates a partially sectioned perspective view of the assembly of Figure 2.</li></ul>
World Oil, Vol. 190 Pages 63 to 70 (1980) describes the bonding of a composite diamond compact to a cemented carbide post. The composite diamond compact consists of a diamond compact bonded to a cemented carbide support. It is the cemented carbide support which is bonded to the post and this bonding is achieved using known diffusion bonding techniques.
Oil and Gas Journal, Vol. 77, Pages 111 to 114 (1979) also describes the bonding of a composite diamond compact to a cemented carbide support using known diffusion bonding techniques.
Welding Journal, Vol. 54, Pages 799 to 804 (1975) discusses diffusion bonding which is a process whereby a joint is effected by heating two clean smooth surfaces while they are pressed into close contact to effect a bond between the two surfaces.
Summary of the invention
According to the present invention, there is provided a method of making an abrasive body comprising an abrasive compact, a backing of cemented carbide bonded to the abrasive compact, and a metal-containing substrate bonded to the backing through a bonding layer comprising nickel, copper, cobalt, iron or an alloy containing one or more of these metals, including the steps of: <ul id="ul0002" list-style="none"><li>(a) providing a composite abrasive compact comprising an abrasive compact bonded to a cemented carbide backing;</li><li>(b) depositing a layer of nickel, copper, cobalt, iron or an alloy containing one or more of these metals on a surface of a metal-containing substrate, applying a transverse pressure to the layer, raising the temperature of the layer to a temperature below its melting point and maintaining the pressure and temperature for a period sufficient to enable the layer to bond to the substrate;</li><li>(c) polishing the exposed surface of the metal layer;</li><li>(d) bringing the backing and substrate together so that the metal layer contacts a surface of the backing;</li><li>(e) urging the backing and substrate together by applying a transverse pressure thereto;</li><li>(f) raising the temperature of the metal layer to a suitable temperature below its melting point; and</li><li>(g) maintaining the pressure and temperature for a time sufficient to cause diffusion bonding between the backing and the substrate, steps (f) and (g) being carried out in an inert atmosphere.</li></ul>
Detailed description of the invention
Abrasive compacts are well known in the art and consist of a polycrystalline mass of superhard abrasive particles bonded into a hard conglomerate. Such compacts will generally have a second or bonding phase which invariably contains a catalyst or solvent for the particular superhard abrasive particle of the compact. The superhard abrasives currently known and used in compacts are diamond and cubic boron nitride.
The cemented carbide backing may be any known in the art such as cemented titanium carbide, cemented tantalum carbide, cemented tungsten carbide or mixtures thereof. The metal phase for such cemented carbides is generally nickel, cobalt or iron which is present in an amount of 3 to 35 percent by weight.
The abrasive compact may be bonded directly to the carbide backing or it may be bonded to the carbide backing through a bonding layer.
Abrasive compacts which are bonded to a cemented carbide backing are also known as "composite abrasive compacts". Examples of abrasive compacts and composite abrasive compacts can be found in British Patent Specification No. 1,489,130, and United States Patent Specifications Nos. 3,745,623 and 3,743,489.
The substrate will generally be larger in mass and volume than the combined mass and volume of the abrasive compact and carbide backing. The substrate will generally be a cemented carbide, but it can also be a steel such as a hardened steel.
The bonding layer between the backing and the substrate will generally have a thickness of up to 220 µm (microns). It has been found that the shear strength of the bond between the backing and the substrate can be high, i.e. 140 N/mm<sup>2</sup> or higher.
The abrasive body of the invention has application as a component for an abrasive tool. In particular, the abrasive body has application as an insert, i.e. cutting element, for a drill bit or crown. An example of such a cutting element is illustrated by Figure 1 of the accompanying drawings. Referring to this Figure, there is shown a cutting element comprising a disc-shaped abrasive compact 10 bonded to a cemented carbide backing 12. The carbide backing 12 is located in a recess 14 in an elongate substrate 16. Bonding of the carbide backing 12 to the substrate 16 is achieved through a bonding layer 18 of the type described above.
The abrasive bodies of the invention will generally be made by first manufacturing a composite abrasive compact consisting of the abrasive compact bonded to the cemented carbide backing by methods known in the art such as those described in British Patent No. 1,489,130. and United States Patents No. 3,745,623 and 3,743,489. Thereafter, the composite abrasive compact will be bonded to the substrate through a bonding layer as defined above using diffusion bonding techniques. Diffusion bonding is known in the art and is a process which produces a metal-to-metal bond in which atoms of the metal migrate across the joint interface and form continuous grain. The process is a solid state process with the metal not reaching its melting point. Diffusion bonding has been found to produce bonds of excellent strength between the backing and substrate under conditions where damage to the abrasive particle of the abrasive compact is substantially avoided. In other words, the compact is substantially free of graphite in the case of diamond compacts and substantially free of hexagonal boron nitride in the case of cubic boron nitride compacts.
During diffusion bonding of the backing to the substrate the pressure applied will generally be 40 to 300 N/mm<sup>2</sup> and the temperature applied will be typically of the order of 650 to 750°C. The diffusion bonding will take place in a vacuum 1,33xlO-<sup>2</sup>Pa (10-<sup>4</sup> Torr) or better or other inert atmosphere such as an inert gas to minimise damage to the abrasive particles of the abrasive compact taking place. The pressure and temperature may be maintained for a period of 5 to 300, typically 5 to 35, minutes to ensure that a good bond is achieved.
The transverse pressure may be applied in the method of the invention by methods known in the art, for example, using a hydraulic cylinder press.
One particular method of applying the desired transverse pressure to the backing and substrate utilises the difference in coefficient of thermal expansion between an outer surround body and an inner expansion body. The method involves placing the substrate and backing, after they have been brought together in step (c), in the cavity of an assembly comprising a surround body having a cavity formed therein and an expansion body located in the cavity and having a coefficient of thermal expansion greater than the surround body, and raising the temperature of the assembly to the desired temperature of step (e) thereby causing the expansion body to expand and apply the desired transverse pressure of step (d) to the backing and the substrate.
Typically the temperature of the assembly is raised by placing it in a furnace.
The surround body may be made of cemented carbide or a ceramic based on silicon nitride or zirconia.
The expansion body is typically made of a metal or alloy which has a high coefficient of thermal expansion. An example of a suitable alloy is the nickel-based alloy Nimonic (Registered Trade Mark).
The surface of the cavity in contact with the expansion body may be sloping and match a sloping surface of the body. Alternatively, the expansion body may be in two contacting parts, the contacting surfaces being sloping and matching.
If the expansion body reacts detrimentally with the components being bonded under the applied temperature conditions, a suitable inert filler material may be provided between the expansion body and the components being bonded.
This method of applying pressure has particular application to the bonding of composite abrasive compacts to tool shanks, i.e. the tool shank is the substrate.
The attached Figures 2 and 3 illustrate an embodiment of this aspect of the invention.
Referring to these Figures, there is shown an assembly 20 comprising a surround body 22 made of cemented carbide and having a slot or cavity 24 formed therein. The surround body 22 is mounted in recess 26 in a steel supporting base 28.
Located in the cavity 24 are opposing wedges 30, 32 which have contacting sloping surfaces along line 34. These wedges are made of the alloy Nimonic (Registered Trade Mark).
Also located in the cavity is a packing element 36 in contact with the surface 38 of wedge 32. Located between the packing element 36 and the surface 40 of the surround body is a tool shank 42 in bonding relationship with a composite abrasive compact 44 comprising an abrasive compact 46 bonded to a cemented carbide backing 48. Located between the tool shank 42 and the backing 48 is a thin metal layer 50 suitable for creating a diffusion bond between the tool shank and the backing.
In order to achieve effective diffusion bonding between the tool shank and the backing the entire assembly is placed in a furnace at a suitable temperature. The temperature must be such as to allow diffusion bonding to take place. At this temperature the Nimonic (RTM) wedges 30, 32 expand at a faster rate than the surround body 22. This has the effect of exerting a bonding pressure on the tool shank 42 and backing 48.
Polishing of the exposed surface of the metal layer is important and preferred to ensure that the surface is as flat as possible. Polishing may be achieved by use of a diamond polishing tool. The surface of the backing to which the substrate is bonded should also be as flat as possible.
The metal layer bonded to the surface of the substrate does tend to buckle and distort, particularly during polishing. To minimise this, it has been found necessary to deposit the layer on the surface, apply a transverse pressure to the layer, raise the temperature of the layer to a temperature below the melting point and maintain the pressure and temperature for a period sufficientto enable the layer to bond to the substrate. Typically, the pressure applied to the layer is in the range 1 to 200 N/mm<sup>2</sup> and the temperature to which the metal layer is raised is 700°C to 1100°C. These conditions of temperature and pressure may be maintained for a period of 5 to 300 minutes, typically 5 to 30 minutes. The metal may be deposited on the surface of the substrate by methods known in the art such as electroplating, electroless plating, vapour deposition or sputtering or placing a foil of the metal in contact with the substrate or placing the foil in contact with a metal coated surface of the substrate. The transverse pressure may be applied to the layer by methods known in the art.
Prior to contacting the carbide backing with the metal coated surface of the substrate, the surface of the backing to be bonded may be provided with a thin metal coat of the same or similar metal to that which is used for coating a surface of the substrate. Such layer may be deposited on the surface of the backing by methods known in the art such as electroplating, electroless plating, vacuum deposition and sputtering.
The invention is further illustrated by the following examples.
Example 1
A stub of cobalt-bonded tungsten carbide had a disc of annealed nickel deposited on a surface thereof. A pressure of 100 N/mm<sup>2</sup> was applied to the nickel coated surface and the temperature raised to 830°C. These conditions were maintained for a period of 20 minutes. Thereafter, the exposed surface of the nickel layer was polished with a diamond polishing tool. The thickness of the nickel coat was 120 pm (microns).
A disc-shaped composite abrasive compact consisting of a diamond compact bonded to a cobalt-bonded tungsten carbide backing was manufactured by the method described in British Patent No. 1,489,130. This composite abrasive compact was then bonded to the stub by first contacting the rear surface of the backing with the nickel layer on the stub. A transverse pressure of 290 N/mm<sup>2</sup> was applied to the composite abrasive compact and the stub to urge the two together and the temperature of the interface, i.e. nickel layer, raised to 725°C. This treatment was carried out in a vacuum of 1,33x10-<sup>2</sup>Pa (10-<sup>4</sup> Torr). These conditions were maintained for a period of 30 minutes.
An excellent bond was achieved between the carbide backing and the carbide stub by this diffusion bonding technique. The shear strength of the bond was measured and it was found to be of the order of 390 N/mm<sup>2</sup>. The thickness of the bonding layer between the backing and the stub was of the order of 120 <sub>Jl</sub>m (microns).
Example 2
The procedure set out in Example 1 was followed save that in bonding the nickel coated stub to the composite abrasive compact the following conditions were used: <tables id="tabl0001" num="0001"><img file="EP0090657B1_D0001.tif" /></tables>
The shear strength of the bond between the carbide backing and the stub was found to be greater than 400 N/mm<sup>2</sup>.
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17 members in 6 offices
Priority claims10
| Document | Office | Kind | Date |
|---|---|---|---|
| 8209409 | United Kingdom | A | |
| 8209409 | United Kingdom | A | |
| 8209409 | United Kingdom | – | |
| 8302620 | United Kingdom | A | |
| 8302620 | United Kingdom | A | |
| 8302620 | United Kingdom | – | |
| 8209409 | – | – | – |
| 8302620 | – | – | – |
| GB19820009409 | – | – | – |
| GB19830002620 | – | – | – |
Members17
| Document | Office | Kind | |
|---|---|---|---|
| GB8302620D0 | United Kingdom | D0 | |
| EP0090657A2 | European Patent Office (EPO) | A2 | |
| EP0090658A2 | European Patent Office (EPO) | A2 | |
| ZA831948B | South Africa | B | |
| ZA831949B | South Africa | B | |
| JPS58211861A | Japan | A | |
| JPS58217270A | Japan | A | |
| EP0090657A3 | European Patent Office (EPO) | A3 | |
| EP0090658A3 | European Patent Office (EPO) | A3 | |
| US4496372A | United States of America | A | |
| US4505721A | United States of America | A | |
| EP0090657B1This record | European Patent Office (EPO) | B1 | |
| DE3368886D1 | Germany | D1 | |
| EP0090658B1 | European Patent Office (EPO) | B1 | |
| DE3372267D1 | Germany | D1 | |
| JPH034336B2 | Japan | B2 | |
| JPH0356868B2 | Japan | B2 |
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| Designated contracting statesAK | AK | EP | |
| (expected) grantORIGINAL CODE: 0009210GRAA | GRAA | EP | |
| Request for examination filed17P | 17P | EP | |
| Designated contracting statesAK | AK | EP | |
| Designated contracting statesAK | AK | EP | |
| Search report despatchedORIGINAL CODE: 0009013PUAL | PUAL | EP | |
| Designated contracting statesAK | AK | EP | |
| Designated contracting statesAK | AK | EP | |
| Public reference made under article 153(3) epc to a published international application that has entered the european phaseORIGINAL CODE: 0009012PUAI | PUAI | EP |
Numbers
- Publication
- 0090657
- Publication, DOCDB
- 0090657
- Publication, EPODOC
- EP0090657
- Application
- 83301794
- Application, DOCDB
- 83301794
- Application, EPODOC
- EP19830301794
Titles3
- German
- Verfahren zur Herstellung von Schleifkörpern
- English
- A method of making abrasive bodies
- French
- Procédé pour la fabrication de corps abrasifs
Classification
- CPC, 26
- B23K20/16
- B22F3/14
- B22F7/06
- B23K20/22
- B23P15/30
- B24D3/007
- B24D3/06
- B24D18/00
- C04B35/645
- C04B37/025
- C04B37/026
- C04B2237/08
- C04B2237/123
- C04B2237/124
- C04B2237/348
- C04B2237/361
- C04B2237/363
- C04B2237/368
- C04B2237/401
- C04B2237/405
- C04B2237/52
- C04B2237/64
- C04B2237/708
- C04B2237/72
- C04B2237/76
- C04B2237/78
- IPC, 12
- B22F3 14
- B22F7 06
- B23K20 16
- B23K20 22
- B23P15 30
- B24D3 00
- B24D3 06
- B24D18 00
- C04B37 02
- C08J5 14
- E21B10 56
- E21B10 567
Designated states9
- Contracting states, 9
- Belgium
- Switzerland
- Germany
- France
- United Kingdom
- Italy
- Liechtenstein
- Netherlands (Kingdom of the)
- Sweden
