EP2245206B1 - Process for manufacturing a metal part reinforced with ceramic fibres - Google Patents
Process for manufacturing a metal part reinforced with ceramic fibres Download PDFInfo
- Publication number
- EP2245206B1 EP2245206B1 EP08869214A EP08869214A EP2245206B1 EP 2245206 B1 EP2245206 B1 EP 2245206B1 EP 08869214 A EP08869214 A EP 08869214A EP 08869214 A EP08869214 A EP 08869214A EP 2245206 B1 EP2245206 B1 EP 2245206B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- notch
- insert
- face
- cover
- metal body
- 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.)
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- 229910052751 metal Inorganic materials 0.000 title claims abstract description 40
- 239000002184 metal Substances 0.000 title claims abstract description 40
- 238000000034 method Methods 0.000 title claims abstract description 24
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 13
- 239000000919 ceramic Substances 0.000 title claims abstract description 11
- 239000000835 fiber Substances 0.000 claims abstract description 14
- 238000001513 hot isostatic pressing Methods 0.000 claims abstract description 6
- 239000011159 matrix material Substances 0.000 claims abstract description 6
- 230000000295 complement effect Effects 0.000 claims abstract description 5
- 238000004804 winding Methods 0.000 claims description 20
- 230000006835 compression Effects 0.000 description 10
- 238000007906 compression Methods 0.000 description 10
- 238000003754 machining Methods 0.000 description 5
- 238000004088 simulation Methods 0.000 description 3
- 229910001069 Ti alloy Inorganic materials 0.000 description 2
- 238000005056 compaction Methods 0.000 description 2
- 230000002787 reinforcement Effects 0.000 description 2
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 2
- 229910010271 silicon carbide Inorganic materials 0.000 description 2
- 208000031968 Cadaver Diseases 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 238000010348 incorporation Methods 0.000 description 1
- 238000005304 joining Methods 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Images
Classifications
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C47/00—Making alloys containing metallic or non-metallic fibres or filaments
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C47/00—Making alloys containing metallic or non-metallic fibres or filaments
- C22C47/02—Pretreatment of the fibres or filaments
- C22C47/04—Pretreatment of the fibres or filaments by coating, e.g. with a protective or activated covering
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C47/00—Making alloys containing metallic or non-metallic fibres or filaments
- C22C47/02—Pretreatment of the fibres or filaments
- C22C47/06—Pretreatment of the fibres or filaments by forming the fibres or filaments into a preformed structure, e.g. using a temporary binder to form a mat-like element
- C22C47/062—Pretreatment of the fibres or filaments by forming the fibres or filaments into a preformed structure, e.g. using a temporary binder to form a mat-like element from wires or filaments only
- C22C47/064—Winding wires
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- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
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- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/4932—Turbomachine making
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- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/49336—Blade making
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- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/49336—Blade making
- Y10T29/49337—Composite blade
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- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49801—Shaping fiber or fibered material
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- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49885—Assembling or joining with coating before or during assembling
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- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49947—Assembling or joining by applying separate fastener
- Y10T29/49966—Assembling or joining by applying separate fastener with supplemental joining
- Y10T29/49968—Metal fusion joining
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- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/4998—Combined manufacture including applying or shaping of fluent material
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- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/4998—Combined manufacture including applying or shaping of fluent material
- Y10T29/49982—Coating
- Y10T29/49984—Coating and casting
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- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/4998—Combined manufacture including applying or shaping of fluent material
- Y10T29/49982—Coating
- Y10T29/49986—Subsequent to metal working
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- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/4998—Combined manufacture including applying or shaping of fluent material
- Y10T29/49993—Filling of opening
Definitions
- the present invention relates to the manufacture of metal parts comprising internal reinforcements formed of ceramic fibers, and comprising the incorporation of a composite material insert of the type consisting of ceramic fibers in a metal matrix.
- Ceramic fibers are for example silicon carbide fibers, SiC, which have a tensile strength and compression much higher than that of a metal such as titanium.
- metal matrix ceramic son which comprise a ceramic fiber coated with metal. They are also called CMM fibers or coated wires.
- the metal gives the elasticity and the flexibility necessary for their handling.
- a known method of manufacturing such parts with reinforcement comprises producing a coil of wire coated around a mandrel.
- the coil is then introduced into a container or metal main body in which a groove forming a housing has been previously machined.
- the depth of the groove is greater than the height of the winding.
- a lid is placed on the container and welded to its periphery after evacuation.
- the cover has a post complementary shape to that of the groove, and its height is adapted to that of the coil placed in the groove so as to fill the groove.
- a hot isostatic pressing step is then carried out during which the lid is deformed and the winding is compressed by the tenon.
- the technique of hot isostatic compression consists of placing the part in an enclosure where it is subjected to a high pressure, of the order of 1000 bar and a temperature also high, of the order of 1000 ° C for a few hours.
- the metallic sheaths of the coated wires weld together and with the walls of the groove by diffusion to form a dense compound of metal alloy within which the ceramic fibers extend.
- the resulting part is then machined to the desired shape.
- the method allows the manufacture of axisymmetric aeronautical parts such as rotor disks, bladed disks, shafts, cylinder bodies, housings, etc. Oblong parts are also produced to form connecting rods for example.
- the machining of the groove in the main body is difficult to achieve especially because of the small rays in the bottom of the groove. This small radius is necessary to allow the housing of the insert which has a rectangular section. Machining the corresponding post in the cover is not easy either because of the non-emerging angles. When in particular the parts to be produced are not axisymmetric but are long, with an oval shape or with rectilinear portions, precise adjustment over long lengths is difficult to obtain. This is even more difficult for inserts formed of very rigid coated son because of the ceramic fibers that require the realization of housing in which they fit perfectly.
- the patent FR 2886290 In the name of Snecma proposes to realize, according to a variant, the winding directly on the main body. Instead of a groove there are two shoulders in it. The first has a bearing surface for the direct winding of a coated wire. This surface is parallel to the winding direction. When the winding is complete, the groove is reconstructed by placing a piece on the main body which is of complementary shape to that of a second shoulder forming a step relative to the first shoulder. Then we have the cover with the pin on the insert that has just wound and compacts the whole. This solution only partially solves the manufacturing problem because the assembly remains complex.
- the applicant has set itself the objective of improving the manufacturing process of such parts in the sense of simplifying the steps of the range and reducing costs.
- the method of manufacturing a metal piece reinforced with ceramic fibers according to which forming a housing for an insert in a metal body having an upper face, there is at least one insert formed from metal matrix fibers in the housing, a metal cover is placed on the body so as to cover the insert, the lid is welded to the metal body after it has been evacuated, the assembly is subjected to a hot isostatic pressing treatment and the treated unit is machined to the desired shape, is characterized in that the housing has the shape of an L-section notch with two faces perpendicular to each other, the lid having an internal section L-shaped section and complementary shape to that of the notch of the metal body with said insert, the cover being shaped externally so that the pressure forces are exerted perpendicularly to said faces of the notch.
- the notch of the metal body comprises a face perpendicular to said upper face and a face parallel to said upper face.
- the insert is first formed by winding a coated wire and is placed in place in the notch.
- the insert is formed by winding a wire coated directly in the notch, the latter forming a winding mandrel.
- the insert may have an annular shape. It can thus, depending on the geometry of the part to be reinforced, form an axisymmetric ring or even for pieces of elongated shape presenting at least one rectilinear portion.
- the insert can also for parts of elongate shape not be annular and be formed of one or more rectilinear elements.
- the cross section of the winding is rectangular, a first face of the winding bearing against one face of the notch and a second face of the winding bearing against the other face of the notch.
- the cover has a centering surface portion cooperating with a face of the notch, in particular the face of the notch of the main body perpendicular to the upper face thereof, for centering and guiding the deformation of the lid on the body. main.
- the scheme of the figure 1 illustrates a procedure of the prior art.
- the main body P metal, comprises a rectangular groove R.
- the insert I consisting of a bundle of coated son temporarily held and bonded to each other.
- a second cover member C is placed on the main body P; it has a post T of shape adapted to the groove R and which is based on the insert I.
- the edges of the groove R or the tenon T are chamfered so as to provide clearance with the part of the lid adjacent to the pin.
- the volume of the insert decreases by 23%.
- the tenon is thus moved down and the game on both sides of the tenon is absorbed.
- the metal has merged; the piece is thus reinforced by the wires imprisoned in the mass.
- a main body 139 of revolution about the axis 140 comprises a central inner portion relative to the height axis H 'equal to the height of the container. Its periphery 142 is chamfered to a first shoulder 143 of height h and width d. At the periphery of this shoulder is a second shoulder 144 whose radial dimension completes the width of the container. Its surface 145 extends at an altitude lower than that of the surface of the first annular shoulder. An annular insert 147 formed of a bundle of coated wires temporarily bonded together was placed.
- An outer ring 146 has been reported on the second shoulder height corresponding to that of the central portion of the main body.
- the outer ring 147 is welded to reconstruct a groove with the first shoulder.
- the cover 148 has an annular projection 149 and bears on the bundle of coated son. We find from this phase the previous method.
- the figure 3 shows, in cross section with perspective, a part of a workpiece incorporating an insert.
- the main body 2 of the metal part, of titanium alloy for example has an upper face 21 is a peripheral edge 22; a notch 23 with an L-shaped section is machined behind the edge 22.
- This notch has a face 23 P, perpendicular to the upper face 21, and a face 23S parallel to the latter.
- the height H of 23P and the width L of 23S are determined according to the dimensions of the insert to be placed.
- the main body 2 has an edge surface portion 24 at one end. lower altitude than the 23S surface; a shoulder 25 forms the transition between the two parts 23 and 22.
- An insert 3 formed from a bundle of coated son and rectangular cross section is housed in the notch. Its height Hi is slightly lower than that of the face 23P and its width Li is also lower than that of the face 23S.
- the insert may advantageously be produced, in a nonlimiting manner, according to one of the methods taught by the patent.
- FR 2,886,290 This includes the structure of the coated yarns, their manufacture, the manufacture of a bonded ply of coated yarns, the joining of this ply either to the metal support on which it is wound or to the lower ply, the welding of yarns by laser or by contact between two electrodes.
- a cover 4 shaped to fit the different parts of the main body with the insert. More specifically, it comprises a bottom wall 41 which bears on the upper face 21, an edge wall 44 which bears on the edge surface portion 24 and a side wall 42 perpendicular to the two walls 41 and 44.
- This side wall has an internal notch 43.
- the notch 43 has an L-shaped cross-section with a face 43P perpendicular to the bottom wall 41. This face extends on the side of the shoulder 25 that it overlaps.
- the notch has a face 43S parallel to the face 23S of the notch 23 of the main body 2 and bears against the upper face of the insert 3.
- the width of the face 43S is the same as that of the face 23S.
- the wall 42 is in contact with the latter by its surface portion 42P.
- the lid does not marry the main body 2 in three places.
- a chamfer is machined between the upper face 21 of the main body and the notch 23 forming a clearance with the bottom wall 41. This clearance can also be obtained by digging the bottom wall.
- a clearance is provided between the edge wall 44 and the edge surface 24.
- the width Li of the insert being slightly smaller than that of the face 23S of the notch 23, a space is created between the face 43P of the notch 43 of the lid and the insert.
- the assembly is subjected to a hot isostatic pressing treatment.
- the pressure is exerted on the assembly producing forces in two directions P1 and P2.
- the pressure force in the direction P1 is exerted on the outer face of the cover of the bottom wall 41 and the edge wall 44 which are parallel.
- the pressure is also exerted in the direction P2 perpendicular to P1 on the outer face of the side wall 42 which is perpendicular to the first two outer faces.
- the insert is of annular shape it does not undergo deformation in the plane perpendicular to the axis of the ring.
- the method of the invention has the advantage of being able to make the notch on the main body using a conventional milling tool. It is the same for the notch on the lid.
- the notch can be of revolution for the realization of an axisymmetrical part.
- the figure 6 perspective watch with part torn off the assembly of a main body 102 with a lid 104.
- the main body 102 has a notch of revolution 123 about the axis thereof, for the housing of an insert 103 which is shaped annular.
- the assembly is covered with a lid 104 with a notch 143.
- the insert is retained between the notch 123 of the body 102 and the notch 143 of the lid 104.
- the object of the isostatic compression is the compression of the insert 103 in the direction P1.
- the faces 142P and 143P of the notch 143 slide along the faces 123P and 125 of the body 102 by compressing the insert 103.
- the secondary compression is provided by the efforts in the direction P2 which deform the wall 142.
- the insert can be made by winding separately and then attached to the notch. However the shape allows a direct winding on the notch.
- the invention allows the realization of parts which are not axisymmetric as that represented on the figure 7 .
- the references point to the same parts as to the figure 3 and are increased by 200.
- the main body 202 has an elongated shape which is divided into two half-circle portions connected by two straight portions.
- the notch 223 is of elongate shape with two parts in a semi-circle and two straight parts. This notch receives an insert of corresponding shape.
- the part comprises two faces with two notches 223 which are covered by two lids. 204 which each comprise a notch 243.
- a notch which is not necessarily annular. It may be for example rectilinear portions. The machining of corresponding notches is also easy.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Crystallography & Structural Chemistry (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
Abstract
Description
La présente invention concerne la fabrication de pièces métalliques comportant des renforts internes formés de fibres céramiques, et comprenant l'incorporation d'un insert en matériau composite du type constitué de fibres céramiques dans une matrice métalliqueThe present invention relates to the manufacture of metal parts comprising internal reinforcements formed of ceramic fibers, and comprising the incorporation of a composite material insert of the type consisting of ceramic fibers in a metal matrix.
Dans le but de réduire la masse des pièces métalliques tout en leur assurant une résistance plus importante notamment en traction ou en compression, il est connu d'incorporer des fibres céramiques dans la masse. Il s'agit par exemple de fibres de carbure de silicium, SiC, qui présentent une résistance à la traction et la compression largement supérieure à celle d'un métal comme le titane.In order to reduce the mass of the metal parts while providing greater strength especially in tension or compression, it is known to incorporate ceramic fibers in the mass. These are for example silicon carbide fibers, SiC, which have a tensile strength and compression much higher than that of a metal such as titanium.
La fabrication de ces pièces passe par la formation préalable d'inserts à partir de fils céramiques à matrice métallique qui comprennent une fibre céramique enduite de métal. Ils sont désignés aussi fibres CMM ou fils enduits. Le métal donne l'élasticité et la souplesse nécessaires à leur manipulation.The manufacture of these parts requires the prior formation of inserts from metal matrix ceramic son which comprise a ceramic fiber coated with metal. They are also called CMM fibers or coated wires. The metal gives the elasticity and the flexibility necessary for their handling.
Un procédé connu de fabrication de telles pièces avec renfort comprend la réalisation d'un bobinage de fil enduit autour d'un mandrin. Le bobinage est ensuite introduit dans un conteneur ou corps principal métallique dans lequel on a usiné au préalable une rainure formant un logement. La profondeur de la rainure est supérieure à la hauteur du bobinage. Un couvercle est placé sur le conteneur et soudé à sa périphérie après mise sous vide. Le couvercle présente un tenon de forme complémentaire à celle de la rainure, et sa hauteur est adaptée à celle du bobinage placé dans la rainure de façon à venir combler la rainure. On procède ensuite à une étape de compression isostatique à chaud au cours de laquelle le couvercle est déformé et le bobinage est comprimé par le tenon.A known method of manufacturing such parts with reinforcement comprises producing a coil of wire coated around a mandrel. The coil is then introduced into a container or metal main body in which a groove forming a housing has been previously machined. The depth of the groove is greater than the height of the winding. A lid is placed on the container and welded to its periphery after evacuation. The cover has a post complementary shape to that of the groove, and its height is adapted to that of the coil placed in the groove so as to fill the groove. A hot isostatic pressing step is then carried out during which the lid is deformed and the winding is compressed by the tenon.
La technique de compression isostatique à chaud consiste à disposer la pièce dans une enceinte où elle est soumise à une pression élevée, de l'ordre de 1000 bars et une température également élevée, de l'ordre de 1000°C pendant quelques heures.The technique of hot isostatic compression consists of placing the part in an enclosure where it is subjected to a high pressure, of the order of 1000 bar and a temperature also high, of the order of 1000 ° C for a few hours.
Les gaines métalliques des fils enduits se soudent entre elles et avec les parois de la rainure par diffusion pour former un ensemble dense composé d'alliage métallique au sein duquel s'étendent les fibres céramiques. La pièce obtenue est ensuite usinée à la forme souhaitée.The metallic sheaths of the coated wires weld together and with the walls of the groove by diffusion to form a dense compound of metal alloy within which the ceramic fibers extend. The resulting part is then machined to the desired shape.
Le procédé permet la fabrication de pièces aéronautiques axisymétriques telles que des disques de rotor, des disques aubagés monoblocs, des arbres, des corps de vérin, des carters, etc. On réalise aussi des pièces oblongues pour constituer des bielles par exemple.The method allows the manufacture of axisymmetric aeronautical parts such as rotor disks, bladed disks, shafts, cylinder bodies, housings, etc. Oblong parts are also produced to form connecting rods for example.
L'usinage de la rainure dans le corps principal est difficile à réaliser notamment en raison des faibles rayons dans le fond de la rainure. Ce faible rayon est nécessaire pour permettre le logement de l'insert qui a une section rectangulaire. L'usinage du tenon correspondant dans le couvercle n'est pas aisé non plus a cause des angles non débouchants. Lorsqu'en particulier les pièces à réaliser ne sont pas axisymétriques mais sont longues, avec une forme ovale ou bien avec des portions rectilignes, un ajustement précis sur des longueurs importantes est difficile à obtenir. Cela est encore plus difficile pour des inserts formés de fils enduits très rigides en raison des fibres céramiques qui obligent la réalisation de logements dans lequel ils s'adaptent parfaitement.The machining of the groove in the main body is difficult to achieve especially because of the small rays in the bottom of the groove. This small radius is necessary to allow the housing of the insert which has a rectangular section. Machining the corresponding post in the cover is not easy either because of the non-emerging angles. When in particular the parts to be produced are not axisymmetric but are long, with an oval shape or with rectilinear portions, precise adjustment over long lengths is difficult to obtain. This is even more difficult for inserts formed of very rigid coated son because of the ceramic fibers that require the realization of housing in which they fit perfectly.
Au lieu de fabriquer l'insert séparément puis de le transférer dans la rainure du corps principal, le brevet
La demanderesse s'est fixé comme objectif d'améliorer le procédé de fabrication de telles pièces dans le sens d'une simplification des étapes de la gamme et d'une réduction des coûts.The applicant has set itself the objective of improving the manufacturing process of such parts in the sense of simplifying the steps of the range and reducing costs.
Conformément à l'invention le procédé de fabrication d'une pièce métallique renforcée de fibres céramiques, selon lequel
on forme, dans un corps métallique présentant une face supérieure, un logement pour un insert,
on dispose au moins un insert formé à partir de fibres à matrice métallique dans le logement,
on place un couvercle métallique sur le corps de façon à recouvrir l' insert,
on soude le couvercle sur le corps métallique après sa mise sous vide,
on soumet l'ensemble à un traitement de compression isostatique à chaud et
on usine l'ensemble traité à la forme souhaitée,
est caractérisé par le fait que le logement a la forme d'une encoche à section en L avec deux faces perpendiculaires entre elles, le couvercle présentant une encoche interne à section en L et de forme complémentaire à celle de l'encoche du corps métallique avec ledit insert, le couvercle étant conformé extérieurement de façon que les efforts de pression s'exercent perpendiculairement aux dites faces de l'encoche.According to the invention the method of manufacturing a metal piece reinforced with ceramic fibers, according to which
forming a housing for an insert in a metal body having an upper face,
there is at least one insert formed from metal matrix fibers in the housing,
a metal cover is placed on the body so as to cover the insert,
the lid is welded to the metal body after it has been evacuated,
the assembly is subjected to a hot isostatic pressing treatment and
the treated unit is machined to the desired shape,
is characterized in that the housing has the shape of an L-section notch with two faces perpendicular to each other, the lid having an internal section L-shaped section and complementary shape to that of the notch of the metal body with said insert, the cover being shaped externally so that the pressure forces are exerted perpendicularly to said faces of the notch.
De préférence, l'encoche du corps métallique comprend une face perpendiculaire à ladite face supérieure et une face parallèle à ladite face supérieure.Preferably, the notch of the metal body comprises a face perpendicular to said upper face and a face parallel to said upper face.
En modifiant ainsi par rapport à l'art antérieur la géométrie des pièces à assembler, on dispose d'un meilleur accès pour l'outil d'usinage du logement de l'insert aussi bien pour le corps principal que pour le couvercle, ce qui rend ces opérations moins délicates à réaliser et donc moins onéreuses. Le nombre de pièces est réduit à deux ce qui simplifie l'assemblage par rapport à la solution précédente. Par ailleurs cette géométrie permet une application des efforts de pression selon deux directions non parallèles contribuant à un compactage plus efficace. Il est à noter que dans le cas d'un insert annulaire, la déformation de l'insert est parallèle à son axe.By thus modifying the geometry of the parts to be assembled with respect to the prior art, better access is available for the machining tool of the housing of the insert both for the main body and for the lid, which makes these operations less difficult to perform and therefore less expensive. The number of parts is reduced to two which simplifies the assembly compared to the previous solution. Moreover this geometry allows an application of pressure forces in two non-parallel directions contributing to a more efficient compaction. It should be noted that in the case of an annular insert, the deformation of the insert is parallel to its axis.
Cette solution permet des mises en oeuvre différentes. Selon un premier mode de réalisation on forme au préalable l'insert par bobinage d'un fil enduit et on le met en place dans l'encoche. Selon un autre mode de réalisation on forme l'insert par bobinage d'un fil enduit directement dans l'encoche, cette dernière formant mandrin de bobinage.This solution allows different implementations. According to a first embodiment, the insert is first formed by winding a coated wire and is placed in place in the notch. According to another embodiment, the insert is formed by winding a wire coated directly in the notch, the latter forming a winding mandrel.
Cette solution permet aussi la réalisation de pièces différentes. L'insert peut avoir une forme annulaire. Il peut ainsi selon la géométrie de la pièce à renforcer former un anneau axisymétrique ou bien encore pour des pièces de forme allongée présenter au moins une portion rectiligne. L'insert peut encore pour des pièces de forme allongée ne pas être annulaire et être formé d'un ou de plusieurs éléments rectilignes.This solution also allows the realization of different parts. The insert may have an annular shape. It can thus, depending on the geometry of the part to be reinforced, form an axisymmetric ring or even for pieces of elongated shape presenting at least one rectilinear portion. The insert can also for parts of elongate shape not be annular and be formed of one or more rectilinear elements.
Plus précisément la section transversale du bobinage est rectangulaire, une première face du bobinage venant en appui contre une face de l'encoche et une deuxième face du bobinage venant en appui contre l'autre face de l'encoche.More precisely, the cross section of the winding is rectangular, a first face of the winding bearing against one face of the notch and a second face of the winding bearing against the other face of the notch.
Avantageusement le couvercle présente une portion de surface de centrage coopérant avec une face de l'encoche, notamment la face de l'encoche du corps principal perpendiculaire à la face supérieure de celui-ci, pour centrer et guider la déformation du couvercle sur le corps principal.Advantageously, the cover has a centering surface portion cooperating with a face of the notch, in particular the face of the notch of the main body perpendicular to the upper face thereof, for centering and guiding the deformation of the lid on the body. main.
On décrit maintenant l'invention plus en détail en référence aux dessins annexés sur lesquels
- La
figure 1 représente un schéma de réalisation d'une pièce avec insert selon l'art antérieur. - La
figure 2 montre la solution de l'art antérieur tel que présenté dans le brevetFR 2886290 - La
figure 3 montre la solution de l'invention avec une encoche à la fois sur le corps principal et sur le couvercle. - Les
figures 4 et 5 sont une simulation de la déformation du couvercle et de l'insert pendant l'opération de compression isostatique à chaud. - La
figure 6 montre l'application de l'invention à la réalisation d'une pièce axisymétrique. - La
figure 7 montre l'application de l'invention à la réalisation d'une pièce de forme allongée. - La
figure 8 montre un exemple de pièce finie réalisée conformément à l'invention, après usinage.
- The
figure 1 represents a diagram of embodiment of a piece with insert according to the prior art. - The
figure 2 shows the solution of the prior art as presented in the patentFR 2886290 - The
figure 3 shows the solution of the invention with a notch on both the main body and the lid. - The
Figures 4 and 5 are a simulation of the deformation of the lid and the insert during the hot isostatic pressing operation. - The
figure 6 shows the application of the invention to the realization of an axisymmetric part. - The
figure 7 shows the application of the invention to the production of an elongate piece. - The
figure 8 shows an example of finished part made according to the invention, after machining.
Le schéma de la
Comme on le voit sur la
On a représenté sur les figures suivantes un mode de réalisation non limitatif de la solution de l'invention.The following figures show a non-limiting embodiment of the solution of the invention.
La
Un insert 3 formé à partir d'un faisceau de fils enduits et de section transversale rectangulaire est logé dans l'encoche. Sa hauteur Hi est légèrement inférieure à celle de la face 23P et sa largeur Li est également inférieure à celle de la face 23S.An
L'insert peut être avantageusement réalisé, de façon non limitative, selon l'une des méthodes enseignées par le brevet
Lorsque l'insert est rectiligne, il est avantageusement déjà compacté et fabriqué selon la technique décrite dans la demande de brevet déposée par la demanderesse sous le numéro
On a placé sur le corps principal 2 un couvercle 4 conformé de façon à épouser les différentes parties du corps principal avec l'insert. Plus précisément, il comprend une paroi de fond 41 qui s'appuie sur la face supérieure 21, une paroi de bord 44 qui s'appuie sur la portion de surface de bord 24 et une paroi latérale 42 perpendiculaire entre les deux parois 41 et 44. Cette paroi latérale présente une encoche 43 interne. L'encoche 43 est à section transversale en L avec une face 43P perpendiculaire à la paroi de fond 41. Cette face se prolonge du côté de l'épaulement 25 qu'il chevauche. L'encoche présente une face 43S parallèle à la face 23S de l'encoche 23 du corps principal 2 et en appui contre la face supérieure de l'insert 3. La largeur de la face 43S est la même que celle de la face 23S. Comme la hauteur Hi de l'insert est légèrement inférieure à la hauteur H de la face 23P, la paroi 42 est en contact avec cette dernière par sa portion de surface 42P.There is placed on the main body 2 a cover 4 shaped to fit the different parts of the main body with the insert. More specifically, it comprises a
Le couvercle n'épouse pas le corps principal 2 en trois endroits. Un chanfrein est usiné entre la face supérieure 21 du corps principal et l'encoche 23 ménageant un jeu avec la paroi de fond 41. Ce jeu peut aussi être obtenu par creusement de la paroi de fond. De même un jeu est ménagé entre la paroi de bord 44 et la surface de bord 24. On note aussi que la largeur Li de l'insert étant légèrement inférieure à celle de la face 23S de l'encoche 23, un espace est créé entre la face 43P de l'encoche 43 du couvercle et l'insert.The lid does not marry the
Lorsque le couvercle et le corps principal sont disposés ainsi, soudés et sous vide, on soumet l'ensemble à un traitement de compression isostatique à chaud. La pression s'exerce sur l'ensemble produisant des efforts selon deux directions P1 et P2. L'effort de pression selon la direction P1 s'exerce sur la face extérieure du couvercle de la paroi de fond 41 et de la paroi de bord 44 qui sont parallèles. La pression s'exerce aussi selon la direction P2 perpendiculaire à P1 sur la face extérieure de la paroi latérale 42 qui est perpendiculaire aux deux premières faces extérieures.When the cover and the main body are thus arranged, welded and under vacuum, the assembly is subjected to a hot isostatic pressing treatment. The pressure is exerted on the assembly producing forces in two directions P1 and P2. The pressure force in the direction P1 is exerted on the outer face of the cover of the
Les efforts sur le couvercle selon la direction P1 conduisent à une déformation de celui-ci parallèlement aux faces 23P et 43P avec compactage de l'insert dans cette direction et absorption du jeu entre les parois de fond 41 et de bord 44 du couvercle 4 et les faces supérieure 21 et de bord 24 du corps principal 2.The forces on the cover in the direction P1 lead to a deformation thereof in parallel with the
Le jeu entre la face 43P de l'encoche du couvercle et l'insert est également absorbé par la déformation du couvercle résultant des efforts de pression selon la direction P2.The clearance between the
Dans la mesure où l'insert est de forme annulaire il ne subit pas de déformation dans le plan perpendiculaire à l'axe de l'anneau.Insofar as the insert is of annular shape it does not undergo deformation in the plane perpendicular to the axis of the ring.
On a représenté sur les
En raison des formes simples qu'il implique, le procédé de l'invention présente l'avantage de pouvoir réaliser l'encoche sur le corps principal à l'aide d'un outil de fraisage conventionnel. Il en est de même pour l'encoche sur le couvercle.Because of the simple shapes involved, the method of the invention has the advantage of being able to make the notch on the main body using a conventional milling tool. It is the same for the notch on the lid.
L'encoche peut être de révolution pour la réalisation d'une pièce axisymétrique. La
Le corps principal 102 présente une encoche de révolution 123 autour de l'axe de celui-ci, pour le logement d'un insert 103 qui est de forme annulaire. L'ensemble est recouvert d'un couvercle 104 avec une encoche 143. On retrouve les mêmes éléments que dans la
L'insert peut être réalisé par bobinage séparément puis rapporté sur l'encoche. Cependant la forme permet un bobinage direct sur l'encoche.The insert can be made by winding separately and then attached to the notch. However the shape allows a direct winding on the notch.
L'invention permet la réalisation de pièces qui ne sont pas axisymétriques comme celle représentée sur la
On a représenté en 210 la pièce assemblée prête pour le traitement de compression isostatique à chaud.There is shown in 210 the assembled part ready for hot isostatic compression treatment.
Sur la
De façon plus générale, on peut aisément ménager dans un corps principal une encoche qui n'est pas nécessairement annulaire. Il peut s'agir par exemple de portions rectilignes. L'usinage d'encoches correspondantes est également aisé.More generally, it is easy to arrange in a main body a notch which is not necessarily annular. It may be for example rectilinear portions. The machining of corresponding notches is also easy.
Claims (10)
- A process for manufacturing a metal part reinforced with ceramic fibers, in which: a housing for an insert is formed in a main metal body (2) having an upper face (21); an insert (3) formed from fibers with a metal matrix is positioned in the housing; a metal cover (4) is placed on the main body (2) so as to cover the insert (3); the cover is welded to the metal body under vacuum; the assembly is subjected to a hot isostatic pressing treatment; and the treated assembly is machined to the desired shape, said process being characterized in that the housing has the shape of a notch (23) of L-shaped cross section with two mutually perpendicular faces (23P and 23S), the cover (4) having an internal notch (43) of L-shaped cross section and of shape complementary to that of the notch (23) in the metal body with said insert (3), the cover (4) being shaped on the outside so that the compressive forces are exerted perpendicular to said faces (23P and 23S) of the notch (23).
- The process as claimed in claim 1, in which the notch (23) in the metal body comprises a face (23P) perpendicular to the upper face (21) of the main metal body (2) and a face (23S) parallel to the upper face (21) of said body (2).
- The process as claimed in claim 1 or 2, in which the insert (3) is formed beforehand by winding a coated filament and it is placed in the notch (23) of the main metal body (2).
- The process as claimed in claim 1 or 2, in which the insert is formed by winding a coated filament directly in the notch (23) of the main metal body, said notch forming a winding mandrel.
- The process as claimed in either of claims 3 and 4, in which the insert has an annular shape.
- The process as claimed in the preceding claim, in which the insert forms an axisymmetric ring.
- The process as claimed in claim 5, in which the ring formed by the insert has at least one straight portion.
- The process as claimed in one of claims 3 to 7, the cross section of the winding of which is rectangular, a first face of the winding bearing against one face of the notch (23) of the main metal body (2) and a second face of the winding bearing against the other face of the notch (23).
- The process as claimed in one of the preceding claims, the cover of which has a centering surface portion that cooperates with one face of the notch (23) of the main metal body in order to center and guide the deformation of the cover on the main body.
- The process as claimed in the preceding claim, the face (23P) being perpendicular to the upper face (21) of the main metal body, the centering surface portion of which cooperates with said face (23P) of the notch perpendicular to the upper face (21) of said notch.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0709171A FR2925895B1 (en) | 2007-12-28 | 2007-12-28 | PROCESS FOR MANUFACTURING A CERAMIC FIBER REINFORCED METAL PIECE |
PCT/EP2008/068293 WO2009083572A1 (en) | 2007-12-28 | 2008-12-24 | Process for manufacturing a metal part reinforced with ceramic fibres |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2245206A1 EP2245206A1 (en) | 2010-11-03 |
EP2245206B1 true EP2245206B1 (en) | 2011-08-17 |
Family
ID=40120291
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP08869214A Active EP2245206B1 (en) | 2007-12-28 | 2008-12-24 | Process for manufacturing a metal part reinforced with ceramic fibres |
Country Status (12)
Country | Link |
---|---|
US (1) | US8495810B2 (en) |
EP (1) | EP2245206B1 (en) |
JP (1) | JP5270693B2 (en) |
CN (1) | CN101918610B (en) |
AT (1) | ATE520797T1 (en) |
BR (1) | BRPI0821416A8 (en) |
CA (1) | CA2710451C (en) |
ES (1) | ES2374242T3 (en) |
FR (1) | FR2925895B1 (en) |
IL (1) | IL206627A0 (en) |
RU (1) | RU2477761C2 (en) |
WO (1) | WO2009083572A1 (en) |
Families Citing this family (6)
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FR2925896B1 (en) * | 2007-12-28 | 2010-02-05 | Messier Dowty Sa | PROCESS FOR MANUFACTURING A CERAMIC FIBER REINFORCED METAL PIECE |
FR2933422B1 (en) * | 2008-07-04 | 2011-05-13 | Messier Dowty Sa | METHOD FOR MANUFACTURING A METAL PIECE COMPRISING INTERNAL REINFORCEMENTS FORMED OF CERAMIC FIBERS |
CN102470928A (en) | 2009-07-28 | 2012-05-23 | 斯奈克玛 | Beam for suspending a turboshaft engine from an aircraft structure |
FR2970266B1 (en) * | 2011-01-10 | 2013-12-06 | Snecma | METHOD FOR MANUFACTURING A MONOBLOC ANNULAR METAL PIECE WITH A REINFORCING INSERT IN COMPOSITE MATERIAL, AND PART OBTAINED |
FR2972661B1 (en) * | 2011-03-15 | 2013-04-12 | Snecma | PROCESS FOR MANUFACTURING A MONOBLOC REVOLUTION METAL PART FROM COMPOSITE FIBROUS STRUCTURES |
FR2975317B1 (en) * | 2011-05-18 | 2013-05-31 | Snecma | METHOD FOR MANUFACTURING BY DIFFUSION WELDING OF A MONOBLOC PIECE FOR A TURBOMACHINE |
Family Cites Families (11)
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SU491440A1 (en) * | 1973-08-13 | 1975-11-15 | Предприятие П/Я Р-6209 | A method of producing a fiber-reinforced composite material |
US4935055A (en) * | 1988-01-07 | 1990-06-19 | Lanxide Technology Company, Lp | Method of making metal matrix composite with the use of a barrier |
FR2713662B1 (en) * | 1993-12-08 | 1996-01-12 | Snecma | Process for obtaining a circular metal part reinforced with fibers. |
EP0938592A2 (en) * | 1996-09-12 | 1999-09-01 | Minnesota Mining And Manufacturing Company | Metal matrix composite tape |
GB9619890D0 (en) * | 1996-09-24 | 1996-11-06 | Rolls Royce Plc | A method of making a fibre reinforced metal component |
EP1099774B1 (en) * | 1999-11-04 | 2006-04-05 | AVIO S.p.A. | Method of producing an element of composite material |
GB0327002D0 (en) * | 2003-11-20 | 2003-12-24 | Rolls Royce Plc | A method of manufacturing a fibre reinforced metal matrix composite article |
US20060254744A1 (en) * | 2005-01-31 | 2006-11-16 | Touchstone Research Laboratory, Ltd. | Selective reinforcement with metal matrix composites |
FR2886291B1 (en) * | 2005-05-27 | 2007-07-13 | Snecma Moteurs Sa | METHOD FOR MANUFACTURING A COIL INSERT COIL |
FR2886290B1 (en) * | 2005-05-27 | 2007-07-13 | Snecma Moteurs Sa | METHOD FOR MANUFACTURING A PIECE WITH AN INSERT IN METALLIC MATRIX COMPOSITE MATERIAL AND CERAMIC FIBERS |
EP2045896B1 (en) * | 2006-07-26 | 2019-09-04 | Mitsubishi Electric Corporation | Dynamo-electric machine |
-
2007
- 2007-12-28 FR FR0709171A patent/FR2925895B1/en not_active Expired - Fee Related
-
2008
- 2008-12-24 RU RU2010131654/02A patent/RU2477761C2/en not_active IP Right Cessation
- 2008-12-24 EP EP08869214A patent/EP2245206B1/en active Active
- 2008-12-24 WO PCT/EP2008/068293 patent/WO2009083572A1/en active Application Filing
- 2008-12-24 AT AT08869214T patent/ATE520797T1/en not_active IP Right Cessation
- 2008-12-24 CN CN2008801231218A patent/CN101918610B/en active Active
- 2008-12-24 ES ES08869214T patent/ES2374242T3/en active Active
- 2008-12-24 CA CA2710451A patent/CA2710451C/en not_active Expired - Fee Related
- 2008-12-24 US US12/810,751 patent/US8495810B2/en active Active
- 2008-12-24 BR BRPI0821416A patent/BRPI0821416A8/en not_active IP Right Cessation
- 2008-12-24 JP JP2010540142A patent/JP5270693B2/en not_active Expired - Fee Related
-
2010
- 2010-06-24 IL IL206627A patent/IL206627A0/en unknown
Also Published As
Publication number | Publication date |
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IL206627A0 (en) | 2010-12-30 |
EP2245206A1 (en) | 2010-11-03 |
JP5270693B2 (en) | 2013-08-21 |
ES2374242T3 (en) | 2012-02-15 |
RU2477761C2 (en) | 2013-03-20 |
FR2925895B1 (en) | 2010-02-05 |
CN101918610B (en) | 2012-04-25 |
ATE520797T1 (en) | 2011-09-15 |
FR2925895A1 (en) | 2009-07-03 |
BRPI0821416A8 (en) | 2016-02-10 |
BRPI0821416A2 (en) | 2015-06-16 |
CN101918610A (en) | 2010-12-15 |
RU2010131654A (en) | 2012-02-10 |
US8495810B2 (en) | 2013-07-30 |
WO2009083572A1 (en) | 2009-07-09 |
JP2011508676A (en) | 2011-03-17 |
CA2710451C (en) | 2016-12-20 |
US20110005060A1 (en) | 2011-01-13 |
CA2710451A1 (en) | 2009-07-09 |
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