EP2245205B1 - Process for manufacturing a metal part reinforced with ceramic fibres - Google Patents

Process for manufacturing a metal part reinforced with ceramic fibres Download PDF

Info

Publication number
EP2245205B1
EP2245205B1 EP08867577A EP08867577A EP2245205B1 EP 2245205 B1 EP2245205 B1 EP 2245205B1 EP 08867577 A EP08867577 A EP 08867577A EP 08867577 A EP08867577 A EP 08867577A EP 2245205 B1 EP2245205 B1 EP 2245205B1
Authority
EP
European Patent Office
Prior art keywords
insert
cover
metal
housing
machined
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.)
Active
Application number
EP08867577A
Other languages
German (de)
French (fr)
Other versions
EP2245205A1 (en
Inventor
Richard Masson
Dominique Ducos
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Landing Systems SAS
Original Assignee
Messier Dowty SA
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Messier Dowty SA filed Critical Messier Dowty SA
Publication of EP2245205A1 publication Critical patent/EP2245205A1/en
Application granted granted Critical
Publication of EP2245205B1 publication Critical patent/EP2245205B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C47/00Making alloys containing metallic or non-metallic fibres or filaments
    • C22C47/02Pretreatment of the fibres or filaments
    • C22C47/025Aligning or orienting the fibres
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C47/00Making alloys containing metallic or non-metallic fibres or filaments
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49002Electrical device making
    • Y10T29/49009Dynamoelectric machine
    • Y10T29/49012Rotor
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49316Impeller making
    • Y10T29/49336Blade making
    • Y10T29/49339Hollow blade
    • Y10T29/49341Hollow blade with cooling passage
    • Y10T29/49343Passage contains tubular insert
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49801Shaping fiber or fibered material
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • Y10T29/49947Assembling or joining by applying separate fastener
    • Y10T29/49966Assembling or joining by applying separate fastener with supplemental joining
    • Y10T29/49968Metal fusion joining
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/4998Combined manufacture including applying or shaping of fluent material
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49995Shaping one-piece blank by removing material

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 provides the elasticity and flexibility to handle them.
  • a known method of manufacturing such parts with reinforcement comprises producing a coil of wire coated around a mandrel.
  • the coil is then incorporated into a container or metal main body in which a groove forming the housing for the insert has been machined beforehand.
  • 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.
  • 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 in arranging 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 are welded together and with the walls of the groove, by diffusion, to form a dense set composed of a metal alloy in which the ceramic fibers extend annularly.
  • the resulting part is then machined to the desired shape.
  • the method allows the manufacture of axisymmetric aeronautical parts such as rotor discs or monobloc bladed disks as well as shafts, cylinder bodies, housings, etc.
  • the applicant has developed a method of manufacturing elongated parts incorporating an insert with straight portions contributing to the transmission of unidirectional tensile forces and / or compression. This process is described in the patent application FR07 / 05453 of July 26, 2007 .
  • the Applicant has also developed a method of manufacturing a rectilinear insert. It consists in producing a coil-shaped insert blank, compacting it in a container by hot isostatic pressing and then machining the rectilinear inserts in the compacted container. Such a process is described in the patent application FR 07/05454 of 26 July 2007 .
  • 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.
  • the groove is reconstituted 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.
  • metal parts comprising one or more metal matrix composite reinforcements from coiled fiber winding and a container - body and lid.
  • These structures are efficient but have a high manufacturing cost.
  • the machining of the main body of the container with its lid represents a significant fraction of the total cost of the parts.
  • the applicant has set itself the objective of improving the process for manufacturing elongated parts in the sense of simplifying the steps of the range and reducing costs.
  • the invention is based on the observation that the machining of a rectilinear groove passing through the entire body of the container is much easier to master than a non-through groove.
  • the solution of the invention is of particular interest with the introduction of two inserts, of elongate shape, arranged in two parallel rectilinear branches or not.
  • an annular insert with two rectilinear branches interconnected by two parts arcuate.
  • the housing is machined according to the precise shape of the insert. Adjusting the shape of the housing to that of the insert has proved to be a very delicate and expensive operation.
  • the machining and setting up more simple without sacrificing the strength of the piece in the end since the fibers work essentially in their longitudinal direction in the central section of the piece.
  • the lid comprises a plate and one or more tabs secured to the plate. More particularly, the plate and the tongue or tabs are obtained by machining the same thick plate. According to one variant, the tongue or tabs and the plate form separate pieces.
  • a chamfer is machined on the upper edge of the groove forming the housing of the insert. This chamfer allows the gradual settlement of the tongue on the insert and to obtain a gradual deformation, that is to say without discontinuity.
  • the invention is particularly advantageous when the insert is of polygonal cross section, in particular rectangular. It can be oval or circular.
  • the insert is either formed of bundled metal-coated fibers or formed of ceramic fibers in a single metal matrix.
  • FIG. 1 On the figure 1 , extracted from the patent application FR 07/05453 , we see a container 1 with a main body 4 of elongate shape, for forming a connecting rod of a landing gear for example.
  • a groove 41 has been machined on each of the two faces of the body 4. This groove makes it possible to hold an insert 3 which comprises two rectilinear portions parallel or not between them joined at the ends by a portion of an arc of a circle.
  • the inserts are of the ceramic fiber type coated with metal such as titanium.
  • the grooves and the inserts are complementary shapes so that the insert is fit without play in the groove.
  • the groove in the container and the pin on the cover must be perfectly assembled to prevent the fibers, which have a very small diameter, 0.25 mm can not escape during hot isostatic compaction.
  • Two covers 5 are provided with a projecting portion forming a pin 51 and cover the faces of the body 4. The ten bears on the insert housed in the groove and closes the latter.
  • the cover 5 is welded, for example by electron beam, to the body 4, providing a vacuum inside the container.
  • the container is visible on the figure 1b ; it is partly torn off to show the inserts.
  • the container is then placed in an enclosure to undergo hot isostatic compression treatment.
  • the cross-section of the container of the figure 1c shows that the edges 42 of the groove 41 are chamfered so as to provide a clearance with the part of the cover 5 adjacent to the pin 51.
  • the pressure is exerted in the direction perpendicular to the surface of the lid generating the collapse of the lids.
  • the pressure and the heat of the order of 1000 ° C. and 1000 bars, allow the metal of the matrix to occupy the voids between the coated wires constituting the insert.
  • the volume of the insert decreases by about 23%. The tenon is thus moved down and the game on both sides of the tenon is absorbed.
  • the figure 1d represents the part blank obtained with two inserts visible in transparency.
  • the blank is then machined so as to obtain the part 8 represented on the figure 2 .
  • This part 8 has recesses 81 between the branches 82.
  • the ceramic fibers are incorporated in the branches 82 which ensure the transmission of forces in traction and compression.
  • the inserts used are ring-shaped but as described in the patent application FR 07/05454 they can be formed of rectilinear elements in bars. In the latter case the rectilinear elements are incorporated in the container after being compacted before.
  • a metal body 10 of elongate shape with respect to the figure is shown an upper face 10A and a lower face 10B.
  • Two rectilinear grooves 10A1, 10A2 and 10B1, 10B2 were machined on each of the two faces.
  • the grooves pass through the body 10 in the direction of the length and open into the two end faces 10C and 10D.
  • the length of the grooves is equal to that L of the body 10. They serve as housing for rectilinear inserts 11, formed of bundles of coated ceramic fibers and of length 1 less than L.
  • the upper edge 10A1 ', 10A2', 10B1 'and 10B2 'of the groove portion forming the housing of the inserts is chamfered.
  • a tongue 14 covers each insert 11 disposed in its housing.
  • the tongue 14 of the same length L that the body 10 comprises a cutting height so as to form two end portions 14a and 14b and a central portion 14c of length 1.
  • the plate 12 covers the upper face 10A respectively lower 10B of the body 10.
  • the height of the tongue is equal to the depth of the groove which must be sufficient to contain the insert 11.
  • the method of the invention thus makes it possible to produce any elongate piece incorporating one or more rectilinear inserts.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)

Abstract

A process for manufacturing a metal part reinforced with ceramic fibers, in which: a housing for an insert is machined in a metal body having an upper face; an insert formed from a fiber bundle having a metal matrix is placed in the housing; a metal cover is placed on the metal body so as to cover the insert; the cover is welded onto the metal body; the assembly including the metal body with the cover undergoes a hot isostatic compression treatment; and the treated assembly is machined to obtain the part. The insert is a rectilinear insert and the housing forms a rectilinear groove that extends beyond the insert and is open at each end, the groove being filled by a tab when the cover is placed on the metal body.

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 plus grande résistance 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, particularly 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 procure 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 provides the elasticity and flexibility to handle them.

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 incorporé dans un conteneur ou corps principal métallique dans lequel on a usiné au préalable une rainure formant le logement pour l'insert. La profondeur de la rainure est supérieure à la hauteur du bobinage. Un couvercle est placé sur le conteneur et soudé à sa périphérie. 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 incorporated into a container or metal main body in which a groove forming the housing for the insert has been machined beforehand. 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. 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 in arranging 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.

Au cours de ce traitement 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'un alliage métallique au sein duquel s'étendent annulairement les fibres céramiques. La pièce obtenue est ensuite usinée à la forme souhaitée.During this treatment the metallic sheaths of the coated wires are welded together and with the walls of the groove, by diffusion, to form a dense set composed of a metal alloy in which the ceramic fibers extend annularly. 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 ou des disques aubagés monoblocs mais aussi des arbres, des corps de vérin, des carters, etc.The method allows the manufacture of axisymmetric aeronautical parts such as rotor discs or monobloc bladed disks as well as shafts, cylinder bodies, housings, etc.

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.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.

La demanderesse a développé un procédé de fabrication de pièces de forme allongée et incorporant un insert avec des parties rectilignes contribuant à la transmission des efforts de traction et/ou de compression unidirectionnels. Ce procédé est décrit dans la demande de brevet FR07/05453 du 26 juillet 2007 . La demanderesse a également développé un procédé de fabrication d'un insert rectiligne. Il consiste à réaliser une ébauche d'insert en forme de bobine, à compacter celle-ci dans un conteneur par compression isostatique à chaud puis à usiner les inserts rectilignes dans le conteneur compacté. Un tel procédé est décrit dans la demande de brevet FR 07/05454 du 26 juillet 2007 .The applicant has developed a method of manufacturing elongated parts incorporating an insert with straight portions contributing to the transmission of unidirectional tensile forces and / or compression. This process is described in the patent application FR07 / 05453 of July 26, 2007 . The Applicant has also developed a method of manufacturing a rectilinear insert. It consists in producing a coil-shaped insert blank, compacting it in a container by hot isostatic pressing and then machining the rectilinear inserts in the compacted container. Such a process is described in the patent application FR 07/05454 of 26 July 2007 .

Cependant lorsque 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 et ne doivent par permettre à une fibre de s'échapper.However, when the parts to be made are not axisymmetrical but are long, with an oval shape or with rectilinear portions, a 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 force the realization of housing in which they fit perfectly and should not allow a fiber to escape.

Au lieu de fabriquer l'insert séparément puis de le transférer dans la rainure du corps principal, le brevet FR 2886290 au nom de Snecma propose de réaliser, selon une variante, le bobinage directement sur le corps principal. Au lieu d'une rainure on ménage deux épaulements dans celui-ci. Le premier présente une surface d'appui pour le bobinage direct d'un fil enduit. Cette surface est parallèle à la direction de bobinage. Lorsque le bobinage est achevé, on reconstitue la rainure en plaçant une pièce sur le corps principal qui est de forme complémentaire à celle d'un second épaulement formant un gradin par rapport au premier épaulement. Puis on dispose le couvercle avec le tenon sur l'insert que l'on vient de bobiner et on procède au compactage de l'ensemble. Cette solution ne résout que partiellement le problème de fabrication car l'assemblage reste complexe.Instead of making the insert separately and then transferring it into the groove of the main body, 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 reconstituted 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.

Ainsi les techniques actuelles de fabrication permettent de créer des pièces métalliques comportant un ou plusieurs renforts en composites à matrice métallique à partir de bobinage de fibres enduites et d'un conteneur - corps et couvercle. Ces structures sont performantes mais ont un coût de fabrication élevé. En particulier l'usinage du corps principal du conteneur avec son couvercle représente une fraction importante du coût total des pièces.Thus, current manufacturing techniques make it possible to create metal parts comprising one or more metal matrix composite reinforcements from coiled fiber winding and a container - body and lid. These structures are efficient but have a high manufacturing cost. In particular the machining of the main body of the container with its lid represents a significant fraction of the total cost of the parts.

La demanderesse s'est fixé comme objectif d'améliorer le procédé de fabrication de pièces de forme allongée 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 process for manufacturing elongated parts in the sense of simplifying the steps of the range and reducing costs.

On parvient à cet objectif, conformément à l'invention, avec un procédé de fabrication d'une pièce métallique renforcée de fibres céramiques, selon lequel :

  • on usine, dans un corps métallique présentant une face supérieure, un logement pour un insert,
  • on dispose un insert formé d'un faisceau 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,
  • on traite l'ensemble du corps métallique avec couvercle par compression isostatique à chaud et
  • on usine ledit ensemble traité pour obtenir ladite pièce,
caractérisé par le fait que l'insert est rectiligne, le logement forme une rainure rectiligne ouverte à chaque extrémité, ladite rainure étant comblée par une languette au moment de la fenneture par le couvercle.This object is achieved according to the invention with a method of manufacturing a metal piece reinforced with ceramic fibers, according to which:
  • a housing for an insert is machined in a metal body having an upper face,
  • an insert formed of a metal matrix fiber bundle is provided in the housing,
  • a metal cover is placed on the body so as to cover the insert,
  • we weld the lid on the metal body,
  • the entire metal body with lid is treated by hot isostatic pressing and
  • said treated assembly is machined to obtain said part,
characterized in that the insert is rectilinear, the housing forms a rectilinear groove open at each end, said groove being filled by a tongue at the time of closure by the lid.

L'invention repose sur la constatation que l'usinage d'une rainure rectiligne traversant tout le corps du conteneur est beaucoup plus simple à maîtriser qu'une rainure non débouchante. La solution de l'invention présente un intérêt particulier avec la mise en place de deux inserts, de forme allongée, agencés selon deux branches rectilignes parallèles ou non. Selon la technique antérieure, pour obtenir deux renforts internes longitudinaux, on réalise au préalable un insert de forme annulaire avec deux branches rectilignes reliées entre elles par deux parties en arc de cercle. Ensuite on usine le logement en fonction de la forme précise de l'insert. Ajuster la forme du logement à celle de l'insert s'est révélé être une opération très délicate et onéreuse. Ainsi en supprimant l'arrondi on rend l'usinage et la mise en place plus simples sans sacrifier à la résistance de la pièce au final puisque les fibres travaillent essentiellement selon leur direction longitudinale dans la section centrale de la pièce.The invention is based on the observation that the machining of a rectilinear groove passing through the entire body of the container is much easier to master than a non-through groove. The solution of the invention is of particular interest with the introduction of two inserts, of elongate shape, arranged in two parallel rectilinear branches or not. According to Prior art, to obtain two longitudinal internal reinforcements, is first carried out an annular insert with two rectilinear branches interconnected by two parts arcuate. Then the housing is machined according to the precise shape of the insert. Adjusting the shape of the housing to that of the insert has proved to be a very delicate and expensive operation. Thus by eliminating the rounding makes the machining and setting up more simple without sacrificing the strength of the piece in the end since the fibers work essentially in their longitudinal direction in the central section of the piece.

Dans la pratique le couvercle comprend une plaque et une ou plusieurs languettes solidaires de la plaque. Plus particulièrement la plaque et la ou les languettes sont obtenues par usinage d'une même plaque épaisse. Selon une variante, la ou les languettes et la plaque forment des pièces séparées.In practice the lid comprises a plate and one or more tabs secured to the plate. More particularly, the plate and the tongue or tabs are obtained by machining the same thick plate. According to one variant, the tongue or tabs and the plate form separate pieces.

De préférence, on usine un chanfrein sur le bord supérieur de la rainure formant le logement de l'insert. Ce chanfrein permet le tassement progressif de la languette sur l'insert et d'obtenir une déformée progressive, c'est-à-dire sans discontinuité.Preferably, a chamfer is machined on the upper edge of the groove forming the housing of the insert. This chamfer allows the gradual settlement of the tongue on the insert and to obtain a gradual deformation, that is to say without discontinuity.

L'invention est particulièrement avantageuse quand l'insert est à section transversale polygonale, notamment rectangulaire. Elle peut être aussi ovale ou circulaire. L'insert est soit formé de fibres enduites de métal assemblées en faisceau soit formé de fibres céramiques dans une seule matrice métallique.The invention is particularly advantageous when the insert is of polygonal cross section, in particular rectangular. It can be oval or circular. The insert is either formed of bundled metal-coated fibers or formed of ceramic fibers in a single metal matrix.

On décrit maintenant l'invention plus en détail en référence aux dessins annexés sur lesquels

  • La figure 1 montre les différentes étapes 1a, 1b, 1c, 1d de fabrication d'une pièce de forme allongée selon l'art antérieur connu du présent déposant ;
  • La figure 2 montre un exemple de pièce obtenue après usinage d'un conteneur incorporant des inserts ;
  • La figure 3 montre en perspective un corps métallique usiné conformément à l'invention ;
  • La figure 4 montre en perspective des languettes associées à une plaque pour former le couvercle fermant le corps métallique de la figure 3 ;
  • La figure 5 montre en perspective éclatée les différents composants avant leur assemblage.
The invention will now be described in more detail with reference to the accompanying drawings in which
  • The figure 1 shows the different steps 1a, 1b, 1c, 1d of manufacturing an elongate piece according to the prior art known to the present applicant;
  • The figure 2 shows an example of a part obtained after machining a container incorporating inserts;
  • The figure 3 shows in perspective a metal body machined according to the invention;
  • The figure 4 perspective watch tabs associated with a plate to form the lid closing the metal body of the figure 3 ;
  • The figure 5 shows exploded perspective the different components before assembly.

Sur la figure 1, extraite de la demande de brevet FR 07/05453 , on voit un conteneur 1 avec un corps principal 4 de forme allongée, destiné à former une bielle d'une train d'atterrissage par exemple. On a usiné une rainure 41 sur chacune des deux faces du corps 4. Cette rainure permet le logement d'un insert 3 qui comprend deux portions rectilignes parallèles ou non entre elles réunies aux extrémités par une portions en arc de cercle. Les inserts sont du type à fibres céramiques enduites de métal tel que le titane. Les rainures et les inserts sont de formes complémentaires de manière à ce que l'insert soit ajusté sans jeu dans la rainure. On note que la rainure dans le conteneur et le tenon sur le couvercle doivent parfaitement s'assembler pour éviter que les fibres, qui ont un très faible diamètre, 0,25 mm ne puissent s'échapper lors de la compaction isostatique à chaud. Deux couvercles 5 sont pourvus d'une partie en saillie formant tenon 51 et viennent recouvrir les faces du corps 4. Le tenon vient en appui sur l'insert logé dans la rainure et colmate cette dernière. On soude, par exemple par faisceau d'électron, le couvercle 5 au corps 4 en assurant le vide à l'intérieur du conteneur. Le conteneur est visible sur la figure 1b; il est en partie arraché pour montrer les inserts. Le conteneur est ensuite disposé dans une enceinte pour subir un traitement de compression isostatique à chaud. La coupe transversale du conteneur de la figure 1c montre que les bords 42 de la rainure 41 sont chanfreinés de manière à ménager un jeu avec la partie du couvercle 5 adjacente au tenon 51. Lors de l'opération de compression isostatique à chaud, la pression est exercée selon la direction perpendiculaire à la surface du couvercle générant l'affaissement des couvercles. La pression et la chaleur, de l'ordre de 1000°C et 1000 bars permettent au métal de la matrice d'occuper les vides entre les fils enduits constituant l'insert. Le volume de l'insert diminue d'environ 23%. Le tenon est ainsi déplacé vers le bas et le jeu de part et d'autre du tenon est absorbé. À la fin du processus, le métal a fusionné et le conteneur s'est compacté; la pièce est ainsi renforcée par les fils emprisonnés dans la masse. La figure 1d représente l'ébauche de pièce obtenue avec deux inserts visibles en transparence. L'ébauche est ensuite usinée de manière à obtenir la pièce 8 représentée sur la figure 2. Cette pièce 8 présente des évidements 81 entre les branches 82. Les fibres céramiques sont incorporées dans les branches 82 qui assurent la transmission des efforts en traction et compression. Les inserts utilisés sont de forme annulaire mais comme cela l'a été décrit dans la demande de brevet FR 07/05454 ils peuvent être formés d'éléments rectilignes en barreaux. Dans ce dernier cas les éléments rectilignes sont incorporés dans le conteneur après avoir été auparavant compactés.On the figure 1 , extracted from the patent application FR 07/05453 , we see a container 1 with a main body 4 of elongate shape, for forming a connecting rod of a landing gear for example. A groove 41 has been machined on each of the two faces of the body 4. This groove makes it possible to hold an insert 3 which comprises two rectilinear portions parallel or not between them joined at the ends by a portion of an arc of a circle. The inserts are of the ceramic fiber type coated with metal such as titanium. The grooves and the inserts are complementary shapes so that the insert is fit without play in the groove. It is noted that the groove in the container and the pin on the cover must be perfectly assembled to prevent the fibers, which have a very small diameter, 0.25 mm can not escape during hot isostatic compaction. Two covers 5 are provided with a projecting portion forming a pin 51 and cover the faces of the body 4. The ten bears on the insert housed in the groove and closes the latter. The cover 5 is welded, for example by electron beam, to the body 4, providing a vacuum inside the container. The container is visible on the figure 1b ; it is partly torn off to show the inserts. The container is then placed in an enclosure to undergo hot isostatic compression treatment. The cross-section of the container of the figure 1c shows that the edges 42 of the groove 41 are chamfered so as to provide a clearance with the part of the cover 5 adjacent to the pin 51. During the hot isostatic pressing operation, the pressure is exerted in the direction perpendicular to the surface of the lid generating the collapse of the lids. The pressure and the heat, of the order of 1000 ° C. and 1000 bars, allow the metal of the matrix to occupy the voids between the coated wires constituting the insert. The volume of the insert decreases by about 23%. The tenon is thus moved down and the game on both sides of the tenon is absorbed. At the end of the process, the metal fused and the container compacted; the piece is thus reinforced by the wires imprisoned in the mass. The figure 1d represents the part blank obtained with two inserts visible in transparency. The blank is then machined so as to obtain the part 8 represented on the figure 2 . This part 8 has recesses 81 between the branches 82. The ceramic fibers are incorporated in the branches 82 which ensure the transmission of forces in traction and compression. The inserts used are ring-shaped but as described in the patent application FR 07/05454 they can be formed of rectilinear elements in bars. In the latter case the rectilinear elements are incorporated in the container after being compacted before.

La solution de l'invention permet d'obtenir de telles pièces de façon plus économique.The solution of the invention makes it possible to obtain such parts more economically.

En se reportant aux figures 3, 4 et 5, on voit un corps métallique 10 de forme allongée avec par rapport à la figure une face supérieure 10A et une face inférieure 10B. On a usiné sur chacune des deux faces deux rainures rectilignes 10A1, 10A2 et 10B1, 10B2. Les rainures traversent le corps 10 dans le sens de la longueur et débouchent dans les deux faces 10C et 10D d'extrémité. La longueur des rainures est égale à celle L du corps 10. Elles servent de logement à des inserts rectilignes 11, formés de faisceaux de fibres céramiques enduites et de longueur 1 inférieure à L. Le bord supérieur 10A1', 10A2', 10B1' et 10B2' de la partie de la rainure formant logement des inserts est chanfreiné. Une languette 14 recouvre chaque insert 11 disposé dans son logement. La languette 14 de même longueur L que le corps 10 comprend une découpe en hauteur de manière à former deux portions d'extrémité 14a et 14b ainsi qu'une portion centrale 14c de longueur 1. La plaque 12 vient recouvrir la face supérieure 10A respectivement inférieure 10B du corps 10. La hauteur de la languette est égale à la profondeur de la rainure qui doit être suffisante pour contenir l'insert 11.Referring to Figures 3, 4 and 5 a metal body 10 of elongate shape with respect to the figure is shown an upper face 10A and a lower face 10B. Two rectilinear grooves 10A1, 10A2 and 10B1, 10B2 were machined on each of the two faces. The grooves pass through the body 10 in the direction of the length and open into the two end faces 10C and 10D. The length of the grooves is equal to that L of the body 10. They serve as housing for rectilinear inserts 11, formed of bundles of coated ceramic fibers and of length 1 less than L. The upper edge 10A1 ', 10A2', 10B1 'and 10B2 'of the groove portion forming the housing of the inserts is chamfered. A tongue 14 covers each insert 11 disposed in its housing. The tongue 14 of the same length L that the body 10 comprises a cutting height so as to form two end portions 14a and 14b and a central portion 14c of length 1. The plate 12 covers the upper face 10A respectively lower 10B of the body 10. The height of the tongue is equal to the depth of the groove which must be sufficient to contain the insert 11.

La fabrication d'un exemple de pièce selon l'invention avec 4 inserts comprend ainsi les étapes suivantes :

  • On prépare un corps 10 métallique, en alliage de titane par exemple, avec une face plane supérieure et une face plane inférieure ;
  • On usine deux rainures rectilignes ouvertes 10A1, 10A2 respectivement 10B1 10B2 sur chacune des deux faces, supérieure et inférieure. Les rainures débouchent sur les faces d'extrémité du corps. Cette opération est relativement simple car on n' à considérer que la profondeur et la largeur de la rainure.
  • On usine deux zones centrales chanfreinées 10A1', 10A2' respectivement 10B1', 10B2' sur les faces libres des rainures, de longueur correspondant à celle des inserts.
  • On met en place les inserts 11 dans les rainures au niveau des zones chanfreinées. Conformément à une première réalisation les inserts sont formés d'un faisceau assemblé de fibres rectilignes enduites. Conformément à un deuxième mode de réalisation préféré les inserts sont préfabriqués selon la méthode décrite dans la demande de brevet FR 07/05454 . Les inserts dans ce cas forment des barreaux avec des fibres céramiques dans une matrice métallique. Ce sont des éléments rectilignes déjà compactés par compression isostatique à chaud.
  • On met en place les languettes 14 sur les inserts 11 avec la portion centrale 14c le long de l'insert et les portions d'extrémité 14a et 14b en bout de l'insert 11.
  • On place les plaques et on les soude sous vide sur les faces du corps 10.
  • On introduit les conteneurs ainsi préparés dans une enceinte à compression isostatique à chaud.
  • On chauffe et on met en compression pour une compaction du conteneur.
  • L'ébauche obtenue est prête pour être usinée.
  • On obtient par exemple la pièce de la figure 2.
The manufacture of an exemplary part according to the invention with 4 inserts thus comprises the following steps:
  • A metal body, of titanium alloy for example, is prepared with an upper planar face and a lower planar face;
  • Two straight rectilinear grooves 10A1, 10A2 and 10B1 10B2 are machined on each of the two upper and lower faces. The grooves open on the end faces of the body. This operation is relatively simple because one only has to consider the depth and the width of the groove.
  • Two chamfered central zones 10A1 ', 10A2' and 10B1 ', 10B2' are machined on the free faces of the grooves, of length corresponding to that of the inserts.
  • The inserts 11 are placed in the grooves at the chamfered areas. According to a first embodiment the inserts are formed of an assembled bundle of coated rectilinear fibers. According to a second preferred embodiment, the inserts are prefabricated according to the method described in the patent application. FR 07/05454 . The inserts in this case form bars with fibers ceramics in a metal matrix. They are rectilinear elements already compacted by hot isostatic compression.
  • The tabs 14 are placed on the inserts 11 with the central portion 14c along the insert and the end portions 14a and 14b at the end of the insert 11.
  • The plates are placed and vacuum-welded on the faces of the body 10.
  • The containers thus prepared are introduced into a hot isostatic compression chamber.
  • It is heated and put into compression for compaction of the container.
  • The blank obtained is ready to be machined.
  • For example, the piece of the figure 2 .

Au lieu de rapporter séparément les languettes 14 et la plaque 12, on peut réaliser ces deux parties en un seule pièce par usinage des languettes dans une plaque épaisse. Le résultat obtenu est le même a priori.Instead of separately reporting the tabs 14 and the plate 12, these two parts can be made in one piece by machining the tabs in a thick plate. The result obtained is the same a priori.

Le procédé de l'invention permet ainsi de réaliser toute pièce de forme allongée incorporant un ou plusieurs inserts rectilignes.The method of the invention thus makes it possible to produce any elongate piece incorporating one or more rectilinear inserts.

Claims (9)

  1. A process for manufacturing a metal part reinforced with ceramic fibers, in which:
    - at least one housing for an insert is machined in a metal body (10) having an upper face (10A, 10B);
    - at least one insert (11) formed from a bundle of fibers having a metal matrix is placed in the housing;
    - a metal cover (12) is positioned on the body so as to cover the insert (11);
    - the cover (12) is welded onto the metal body (10);
    - the assembly, namely the metal body with the cover, is treated by hot isostatic pressing; and
    - said treated assembly is machined in order to obtain said part,
    characterized in that the insert (11) is straight and the housing forms a straight slot (10A1, 10A2, 10B1, 10B2) which extends beyond the insert and is open at each end, said slot being filled by a tongue (14) at the moment of closure by the cover (12).
  2. The process as claimed in the preceding claim, in which the tongue (14) is integral with a plate (12) forming the cover.
  3. The process as claimed in the preceding claim, in which the tongue is integral with the plate and is obtained by machining a thick plate in order to form the cover.
  4. The process as claimed in claim 1, the tongue (14) of which is separate from the plate (12) of the cover.
  5. The process as claimed in one of the preceding claims, in which a bevel (10A1', 10A2', 10B1', 10B2') is machined on the upper edge of the slot (10A1, 10A2, 10B1, 10B2) forming the housing for the insert (11).
  6. The process as claimed in one of the preceding claims, in which the insert has a polygonal, especially rectangular, oval or circular, cross section.
  7. The process as claimed in one of the preceding claims, the insert of which is formed from metal-coated fibers assembled into a bundle.
  8. The process as claimed in one of claims 1 to 6, in which the insert is formed from ceramic fibers in a metal matrix.
  9. The process as claimed in one of the preceding claims, in which at least a second insert is placed in the metal body.
EP08867577A 2007-12-28 2008-12-24 Process for manufacturing a metal part reinforced with ceramic fibres Active EP2245205B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0709172A FR2925896B1 (en) 2007-12-28 2007-12-28 PROCESS FOR MANUFACTURING A CERAMIC FIBER REINFORCED METAL PIECE
PCT/EP2008/068294 WO2009083573A1 (en) 2007-12-28 2008-12-24 Process for manufacturing a metal part reinforced with ceramic fibres

Publications (2)

Publication Number Publication Date
EP2245205A1 EP2245205A1 (en) 2010-11-03
EP2245205B1 true EP2245205B1 (en) 2011-07-13

Family

ID=40110945

Family Applications (1)

Application Number Title Priority Date Filing Date
EP08867577A Active EP2245205B1 (en) 2007-12-28 2008-12-24 Process for manufacturing a metal part reinforced with ceramic fibres

Country Status (12)

Country Link
US (1) US8458886B2 (en)
EP (1) EP2245205B1 (en)
JP (1) JP5539222B2 (en)
CN (1) CN101952473B (en)
AT (1) ATE516381T1 (en)
BR (1) BRPI0821441A8 (en)
CA (1) CA2710547C (en)
ES (1) ES2373388T3 (en)
FR (1) FR2925896B1 (en)
IL (1) IL206628A0 (en)
RU (1) RU2477762C2 (en)
WO (1) WO2009083573A1 (en)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9596993B2 (en) 2007-07-12 2017-03-21 Volcano Corporation Automatic calibration systems and methods of use
WO2009009802A1 (en) 2007-07-12 2009-01-15 Volcano Corporation Oct-ivus catheter for concurrent luminal imaging
FR2933423B1 (en) * 2008-07-04 2010-09-17 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
FR2950078B1 (en) * 2009-09-11 2012-10-05 Messier Dowty Sa METAL PIECE PROVIDED WITH FIBROUS REINFORCEMENTS WITH BITEAUTEE END.
FR2950077B1 (en) * 2009-09-11 2014-07-18 Messier Dowty Sa METHOD FOR MANUFACTURING A FIBER-REINFORCED METAL ROD, AND ROD THUS OBTAINED
FR2952944B1 (en) * 2009-11-25 2014-05-02 Messier Dowty Sa PROCESS FOR MANUFACTURING A COMPOSITE METALLIC PART WITH INTERNAL FIBER REINFORCEMENTS, PREFORMING METHOD AND METAL PIECE OBTAINED
FR2953859B1 (en) * 2009-12-16 2013-12-20 Snecma METHOD FOR MANUFACTURING A RIGHT-SHAPED INSERT IN METALLIC MATRIX COMPOSITE MATERIAL
FR2958299B1 (en) 2010-04-01 2012-05-04 Snecma METHOD FOR MANUFACTURING AN EXTENDED FORM INSERT IN METALLIC MATRIX COMPOSITE MATERIAL
WO2013033592A1 (en) 2011-08-31 2013-03-07 Volcano Corporation Optical-electrical rotary joint and methods of use
US10070827B2 (en) 2012-10-05 2018-09-11 Volcano Corporation Automatic image playback
US9367965B2 (en) 2012-10-05 2016-06-14 Volcano Corporation Systems and methods for generating images of tissue
CN113705586A (en) 2013-03-07 2021-11-26 飞利浦影像引导治疗公司 Multi-modal segmentation in intravascular images
US9292145B2 (en) 2013-07-08 2016-03-22 Elo Touch Solutions, Inc. Multi-user multi-touch projected capacitance touch sensor
FR3039839B1 (en) * 2015-08-06 2019-12-20 Safran Aircraft Engines PROCESS FOR MANUFACTURING A PART OF COMPOSITE MATERIAL

Family Cites Families (52)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1359065A (en) * 1920-04-14 1920-11-16 Axel F Holmberg Metal reinforcement and support for concrete tanks
US3333334A (en) * 1963-10-23 1967-08-01 Rca Corp Method of making magnetic body with pattern of imbedded non-magnetic material
US3571901A (en) * 1969-06-13 1971-03-23 Union Carbide Corp Method of fabricating a carbon-fiber reinforced composite article
US3754839A (en) * 1972-05-01 1973-08-28 United Aircraft Corp Filament reinforced rotor assembly
US3765796A (en) * 1972-05-01 1973-10-16 United Aircraft Corp Filament reinforced rotor assembly
US3844019A (en) * 1972-06-07 1974-10-29 W Shwayder Saw and impact resistant security bar and method of making same
SU491440A1 (en) * 1973-08-13 1975-11-15 Предприятие П/Я Р-6209 A method of producing a fiber-reinforced composite material
US4587177A (en) * 1985-04-04 1986-05-06 Imperial Clevite Inc. Cast metal composite article
US4867644A (en) * 1987-05-15 1989-09-19 Allied-Signal Inc. Composite member, unitary rotor member including same, and method of making
US4919594A (en) * 1987-05-15 1990-04-24 Allied-Signal Inc. Composite member, unitary rotor member including same, and method of making
US4935055A (en) * 1988-01-07 1990-06-19 Lanxide Technology Company, Lp Method of making metal matrix composite with the use of a barrier
US5561173A (en) * 1990-06-19 1996-10-01 Carolyn M. Dry Self-repairing, reinforced matrix materials
GB2247492B (en) * 1990-09-01 1995-01-11 Rolls Royce Plc A method of making a fibre reinforced metal component
US5431984A (en) * 1990-12-11 1995-07-11 Avco Corporation Composite preforms with groves for fibers and groves for off-gassing
US5225015A (en) * 1991-04-15 1993-07-06 Corning Incorporated Method for making stiffened ceramic matrix composite panel
JP3871071B2 (en) * 1996-01-08 2007-01-24 石川島播磨重工業株式会社 Fabrication method of fiber reinforced metal products
GB9619890D0 (en) * 1996-09-24 1996-11-06 Rolls Royce Plc A method of making a fibre reinforced metal component
JPH10176231A (en) * 1996-12-16 1998-06-30 Ishikawajima Harima Heavy Ind Co Ltd Fiber reinforced metal product and its manufacture
JPH11103594A (en) * 1997-09-29 1999-04-13 Meidensha Corp Drive circuit of switched reluctance motor
AT408153B (en) * 1998-09-02 2001-09-25 Electrovac METAL MATRIX COMPOSITE (MMC) COMPONENT
DE59911362D1 (en) * 1998-10-31 2005-02-03 Deutsch Zentr Luft & Raumfahrt Method for producing a long-fiber-reinforced component
DE10005250B4 (en) * 1999-02-09 2004-10-28 Mtu Aero Engines Gmbh Process for the production of fiber-reinforced metallic components
US6630093B1 (en) * 1999-08-21 2003-10-07 Ronald D. Jones Method for making freeform-fabricated core composite articles
US6623678B2 (en) * 2001-01-31 2003-09-23 Karsten Manufacturing Corp. Method of making a prototype golf club grip
DE10112863C1 (en) * 2001-03-16 2002-11-28 Fraunhofer Ges Forschung Process for producing a hollow fiber or capillary membrane module
US6745819B2 (en) * 2001-05-17 2004-06-08 Tht Presses Inc. Vertical die casting press and method of producing die cast metal parts
ITTO20010621A1 (en) * 2001-06-27 2002-12-27 Campagnolo Srl CRANK FOR BICYCLE AND PROCEDURE FOR ITS MANUFACTURE.
JP2003029082A (en) * 2001-07-13 2003-01-29 Ntt Advanced Technology Corp Storing member for optical fiber coupler
US7794520B2 (en) * 2002-06-13 2010-09-14 Touchstone Research Laboratory, Ltd. Metal matrix composites with intermetallic reinforcements
CA2495373C (en) * 2002-08-15 2012-07-24 David Gerber Controlled artificial intervertebral disc implant
GB0324810D0 (en) * 2003-10-24 2003-11-26 Rolls Royce Plc A method of manufacturing a fibre reinforced metal matrix composite article
GB0327044D0 (en) * 2003-11-18 2004-04-07 Rolls Royce Plc A method of manufacturing a fibre reinforced metal matrix composite article and a cassette for use therein
GB0327002D0 (en) * 2003-11-20 2003-12-24 Rolls Royce Plc A method of manufacturing a fibre reinforced metal matrix composite article
US7220492B2 (en) * 2003-12-18 2007-05-22 3M Innovative Properties Company Metal matrix composite articles
US7584571B2 (en) * 2004-03-05 2009-09-08 Eric Thomas Ryan One piece polygonal carbon fiber rod with integral spine
US6986203B2 (en) * 2004-03-24 2006-01-17 Union Composites Co., Ltd. Manufacturing method for a composite coil spring
US20060024490A1 (en) * 2004-07-29 2006-02-02 3M Innovative Properties Company Metal matrix composites, and methods for making the same
US20060166027A1 (en) * 2005-01-26 2006-07-27 Dr. Boris Amusin Impact resistant composite metal structure
US20060244165A1 (en) * 2005-04-27 2006-11-02 Dai Huang Manufacturing carbon fiber reinforced ceramics as brake discs
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
FR2886181B1 (en) * 2005-05-27 2008-12-26 Snecma Moteurs Sa METHOD FOR MANUFACTURING A TUBULAR PIECE WITH AN INSERT IN METALLIC MATRIX COMPOSITE MATERIAL
US7361100B1 (en) * 2006-12-20 2008-04-22 Karsten Manufacturing Corporation Metal composite golf club head
FR2925897B1 (en) * 2007-12-28 2010-07-30 Messier Dowty Sa METHOD FOR MANUFACTURING PIECES WITH INSERT IN METALLIC MATRIX COMPOSITE MATERIAL
FR2925895B1 (en) * 2007-12-28 2010-02-05 Messier Dowty Sa PROCESS FOR MANUFACTURING A CERAMIC FIBER REINFORCED METAL PIECE
FR2933423B1 (en) * 2008-07-04 2010-09-17 Messier Dowty Sa PROCESS FOR MANUFACTURING A CERAMIC FIBER REINFORCED METAL PIECE
RU2011109216A (en) * 2008-08-13 2012-09-20 Ормко Корпорейшн (Us) AESTHETIC ORTHODONTIC BRACKET AND METHOD OF ITS MANUFACTURE
FR2950077B1 (en) * 2009-09-11 2014-07-18 Messier Dowty Sa METHOD FOR MANUFACTURING A FIBER-REINFORCED METAL ROD, AND ROD THUS OBTAINED
FR2952944B1 (en) * 2009-11-25 2014-05-02 Messier Dowty Sa PROCESS FOR MANUFACTURING A COMPOSITE METALLIC PART WITH INTERNAL FIBER REINFORCEMENTS, PREFORMING METHOD AND METAL PIECE OBTAINED
FR2953859B1 (en) * 2009-12-16 2013-12-20 Snecma METHOD FOR MANUFACTURING A RIGHT-SHAPED INSERT IN METALLIC MATRIX COMPOSITE MATERIAL
GB201013440D0 (en) * 2010-08-11 2010-09-22 Rolls Royce Plc A method of manufacturing a fibre reinforced metal matrix composite article
US8944789B2 (en) * 2010-12-10 2015-02-03 National Oilwell Varco, L.P. Enhanced elastomeric stator insert via reinforcing agent distribution and orientation

Also Published As

Publication number Publication date
US20110005061A1 (en) 2011-01-13
US8458886B2 (en) 2013-06-11
JP5539222B2 (en) 2014-07-02
IL206628A0 (en) 2010-12-30
WO2009083573A1 (en) 2009-07-09
RU2477762C2 (en) 2013-03-20
EP2245205A1 (en) 2010-11-03
ATE516381T1 (en) 2011-07-15
CA2710547C (en) 2016-11-08
RU2010131656A (en) 2012-02-10
JP2011508677A (en) 2011-03-17
BRPI0821441A8 (en) 2016-02-10
CN101952473B (en) 2012-07-18
FR2925896B1 (en) 2010-02-05
ES2373388T3 (en) 2012-02-03
CA2710547A1 (en) 2009-07-09
FR2925896A1 (en) 2009-07-03
BRPI0821441A2 (en) 2015-06-16
CN101952473A (en) 2011-01-19

Similar Documents

Publication Publication Date Title
EP2245205B1 (en) Process for manufacturing a metal part reinforced with ceramic fibres
EP2245204B1 (en) Method for making parts with an insert made of a metal-matrix composite material
EP2307587B1 (en) Method for producing a metallic part reinforced by ceramic fibres
EP2179069A2 (en) Mechanical part including an insert made of a composite material
FR2919283A1 (en) Manufacturing mechanical component, comprises fabricating an insert by winding beam or sheet linked with coated wire around a rotating component, and inserting insert in opposite sides of container undergoing hot isostatic compaction
CA2710451C (en) Process for manufacturing a metal part reinforced with ceramic fibres
EP2310547B1 (en) Method for producing a metallic part comprising inner reinforcements consisting of ceramic fibres
CA2783421C (en) Method for manufacturing a straight insert made of metal matrix composite material
EP2552629B1 (en) Method of manufacturing an elongate insert made of a metal matrix composite
CA2764774C (en) Method for making a metal part including a fibrous annular reinforcement
FR2972661A1 (en) PROCESS FOR MANUFACTURING A MONOBLOC REVOLUTION METAL PART FROM COMPOSITE FIBROUS STRUCTURES

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20100623

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MT NL NO PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA MK RS

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

DAX Request for extension of the european patent (deleted)
GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MT NL NO PL PT RO SE SI SK TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: FRENCH

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602008008299

Country of ref document: DE

Effective date: 20110908

REG Reference to a national code

Ref country code: NL

Ref legal event code: VDEP

Effective date: 20110713

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 516381

Country of ref document: AT

Kind code of ref document: T

Effective date: 20110713

RAP2 Party data changed (patent owner data changed or rights of a patent transferred)

Owner name: MESSIER-BUGATTI-DOWTY

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20111013

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20111114

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20111113

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110713

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110713

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110713

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110713

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110713

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2373388

Country of ref document: ES

Kind code of ref document: T3

Effective date: 20120203

REG Reference to a national code

Ref country code: IE

Ref legal event code: FD4D

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20111014

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110713

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110713

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110713

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110713

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110713

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110713

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110713

Ref country code: IE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110713

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110713

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110713

26N No opposition filed

Effective date: 20120416

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110713

BERE Be: lapsed

Owner name: MESSIER-DOWTY SA

Effective date: 20111231

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20111231

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602008008299

Country of ref document: DE

Effective date: 20120416

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20111231

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110713

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: ES

Payment date: 20121205

Year of fee payment: 5

Ref country code: IT

Payment date: 20121122

Year of fee payment: 5

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20111224

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20111013

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110713

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20121231

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20121231

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110713

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 20150708

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20131225

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20131231

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 8

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20131224

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 9

REG Reference to a national code

Ref country code: FR

Ref legal event code: CD

Owner name: MESSIER-BUGATTI-DOWTY, FR

Effective date: 20170518

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 10

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20211118

Year of fee payment: 14

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20220616

Year of fee payment: 15

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20221224

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20221224

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20231122

Year of fee payment: 16

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 602008008299

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20240702

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20240702