EP2191029B1 - Mechanical part including an insert made of a composite material - Google Patents
Mechanical part including an insert made of a composite material Download PDFInfo
- Publication number
- EP2191029B1 EP2191029B1 EP08830741A EP08830741A EP2191029B1 EP 2191029 B1 EP2191029 B1 EP 2191029B1 EP 08830741 A EP08830741 A EP 08830741A EP 08830741 A EP08830741 A EP 08830741A EP 2191029 B1 EP2191029 B1 EP 2191029B1
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- EP
- European Patent Office
- Prior art keywords
- insert
- mechanical part
- winding
- composite material
- mandrel
- 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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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
- 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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- 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
-
- 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
- C22C47/14—Making alloys containing metallic or non-metallic fibres or filaments by powder metallurgy, i.e. by processing mixtures of metal powder and 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
- C22C49/00—Alloys containing metallic or non-metallic fibres or filaments
- C22C49/02—Alloys containing metallic or non-metallic fibres or filaments characterised by the matrix material
- C22C49/04—Light metals
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2999/00—Aspects linked to processes or compositions used in powder metallurgy
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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
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12486—Laterally noncoextensive components [e.g., embedded, etc.]
Definitions
- the present invention relates to a mechanical part comprising an insert made of composite material of the type consisting of ceramic fibers in a metal matrix, as well as a method of manufacturing this mechanical part and a winding device designed for implementing the manufacturing method. .
- the invention applies to any type of mechanical part whose function is to transmit a traction force and / or compression mainly unidirectional.
- some mechanical parts may comprise an insert made of composite material with a metal matrix, such parts being able to be monobloc.
- a composite material comprises a matrix of metal alloy, for example titanium alloy Ti, within which fibers extend, for example ceramic fibers of SiC silicon carbide.
- Such fibers have a much higher tensile and compressive strength than titanium. It is therefore mainly the fibers that take up the efforts, the metal alloy matrix ensuring a binder function with the rest of the part, as well as protection and insulation of the fibers, which must not come into contact with each other. others.
- the ceramic fibers are resistant to erosion, but must necessarily be reinforced with metal.
- the composite materials as described above are known to be used, in the aeronautical field, for the manufacture of disks, shafts, bodies of jacks, housings, spacers or as reinforcements of single-piece parts such as blades.
- a technique for manufacturing these parts is described in the document FR 2886290 , representative of the technological background of the invention, in which one of the essential manufacturing steps consists in winding a bundle or a ply of coated wires around a piece of circular revolution perpendicular to the axis of rotation thereof.
- the described parts thus obtained are of circular type and are particularly suitable for producing circular parts such as shafts, cylinder bodies, housings or discs.
- the patent US3669364 describes the manufacture of a panel by winding wires coated around a mandrel and forming the workpiece after diffusion welding.
- DE10005250 describes the manufacture of a piece of complex shape by winding son coated around a mandrel followed by shaping the assembly before diffusion welding.
- connecting rods essentially oblong shape, whose function is to transmit a tensile force and / or unidirectional compression.
- a metal matrix rod reinforced with conferred ceramic fibers is described by US Patent 4671336 .
- the invention particularly relates to a method of manufacturing a mechanical part comprising at least one composite material insert of the type consisting of ceramic fibers in a metal matrix capable of transmitting tensile forces and / or unidirectional compression between its ends .
- the invention relates to a method for manufacturing a mechanical part according to the features of claim 1.
- the mechanical part thus obtained for example a connecting rod, advantageously makes it possible to transmit unidirectional traction and / or compression forces.
- the figure 1 represents an example of a mechanical part such as a rod 1 whose shape is generally oblong, that is to say of elongated shape. It has two ends 13 and 14.
- the function of a connecting rod 1 is to transmit a movement, and / or tensile forces T and / or compression C, between two parts articulated at its ends along parallel axes Z1 and Z2 .
- the rod 1 has at each of its ends 13 and 14 a cylindrical recess 11 or 12 whose axes correspond to the parallel axes Z1 and Z2.
- This type of rod 1 can be used, for example, in the design of the undercarriages or in that of turbomachines comprising rods for taking up thrust force.
- the figure 2 represents an example of winding device 20 according to the invention.
- the winding device 20 is particularly suitable for producing an insert for a mechanical part such as a connecting rod.
- This winding device 20 comprises a hollow mandrel piece 2 of oblong shape acting as mandrel and two flanges 21 and 22 oblong and substantially identical.
- the mandrel part 2 has a geometry of revolution, that is to say a geometry describing a closed structure usually curved.
- the dimensions of the flanges 21 and 22 are greater than the dimensions of the mandrel part 2 so that the periphery 27 of each flange 21 and 22 extends beyond the periphery of the mandrel part 2.
- the mandrel part 2 is sandwiched between the flanges 21 and 22.
- the threads 32 are wound on the mandrel piece 2 when the winding device 20 is rotated along the winding axis Z.
- the flanges 21 and 22 retain axially the son coatings 32 and guide them.
- the winding device 20 belongs to an assembly forming a winding system.
- the winding system further comprises means for rotating the winding device 20 and means for providing a bundle or a bonded sheet of coated threads 32.
- the chuck part 2 comprises two rectilinear winding portions 24. These straight winding portions 24 are oriented perpendicular to the winding axis Z. Thus, at least a part of the winding of the wires 32 around the mandrel part 2 is performs in a rectilinear direction.
- the winding of the coated wires 32 is carried out perpendicularly to the winding axis Z, in other words, the coated wires 32 are substantially oriented perpendicularly to the winding axis Z.
- these rectilinear winding portions 24 are parallel and interposed between two circular portions 25. It is possible to vary the dimensions of the mandrel part 2, in particular its thickness in the axial direction Z, the length of the rectilinear winding portions 24 and the radius of curvature of the circular pieces 25, depending on the dimensions of the desired insert 3.
- the circular pieces 25 may also have different radii. Thus, the portions of rectilinear windings 24 may not be parallel.
- the winding around the chuck part 2 having rectilinear winding portions 24 allows to generate in a short time an insert 3 having at least one rectilinear generator consisting of a large number of coiled son 32 parallel and unidirectional.
- the insert 3 once wound, can be removed from the winding device 20 by separating the flanges 21 and 22 from one another.
- the shape of the insert 3 thus formed must be fixed to prevent the son 32 lose their orientation. Several techniques can be implemented for this purpose.
- a first technique for maintaining the shape of the insert 3 consists in providing, at the beginning of winding, a step of winding a first metal foil for hooking up the inner part of the insert 3 and, at the end of winding, a step of winding a second metal foil 28 of attachment of the outer part of the insert 3.
- the first metal foil constitutes the mandrel piece 2.
- the coated son 32 are thus between the foils 2 and 28, as shown on the figure 3 .
- each flange 21 and 22 has notches 23 on its periphery 27.
- Each notch 23 of the flange 21 is disposed opposite a notch 23 of the flange 22, thus forming a pair of notches 23.
- the fixing metal straps 31 is facilitated by the dimensions of the notches 23 extending inwardly of the flanges 21 and 22 to a depth d.
- the depth d of the notches 23 must be such that it is possible to access the hollow interior 29 of the chuck part 2 which is arranged around a hub of the winding device 20, not visible on the figure 2 , comprising an alternation of notches and teeth, the notches of the hub being in phase with the notches 23 of the flanges 21 and 22.
- the depth d extends beyond the winding surface of the mandrel piece 2.
- Each pair of notches 23 is intended to allow the attachment of a metal strap 31.
- the metal straps 31 are made of a metallic material identical to that of the container 4, described in connection with the figure 4 and the chuck part 2.
- the metal straps 31 are fixed around the insert 3 by a contact welding process.
- the metal straps 31 are arranged at regular intervals on the wound insert 3.
- insert 3 coiled and the metal straps 31 put in place, it can be removed from the winding device 20 by separating the flanges 21 and 22 from one another.
- An example of insert 3 thus obtained is represented in figure 3 . It consists of an oblong-shaped mandrel piece comprising two rectilinear and parallel portions 34 interposed between two circular portions 35.
- a second technique for maintaining the shape of the insert 3, which does not require the use of straps 31, consists in providing a mandrel-forming piece 2 forming an oblong mandrel comprising at least one radial flange, for example of L-shaped cross-section or in U, on which the wires 32 are wound.
- a bonded sheet of coated son 32 it is possible to secure it to the mandrel piece 2 on which it is wound and to the sheet of the lower layer by means of a method by contact welding between two electrodes and passage of a medium frequency current.
- the wires 32 are thus welded as the winding progresses so that, when the insert 3 is extracted from the winding device 20, it forms a part integral with the mandrel part 2.
- the insert 3 is then inserted into a container 4, as shown in FIG. figure 4 .
- the container 4 comprises for this purpose a groove 41 of complementary shape to the insert 3 and in which is housed the insert 3.
- the container 4 is the preform of the metal alloy matrix, preferably titanium Ti.
- a lid 5 is attached to the container 4 by electron beam welding, evacuated, and then compacted by a hot isostatic compaction process.
- the assembly is then machined to obtain the final mechanical part 10: a rod 10, represented on the figure 5 .
- the rod 10, of identical shape to the rod 1 of the figure 1 further comprises an insert of composite material 3, with a geometry of revolution, whose son 32 are partly oriented in a rectilinear direction.
- This rectilinear direction is perpendicular to the axes Z1 and Z2.
- This link 10 advantageously allows to transmit the unidirectional traction and / or compression forces.
- the rectilinear portions 34 of the inserts 3 comprise son all oriented in the same rectilinear direction.
- the invention applies to any type of mechanical part whose function is to transmit a traction force and / or compression mainly unidirectional and is therefore not limited only to connecting rods that are only an example of application.
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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)
- Manufacturing Of Tubular Articles Or Embedded Moulded Articles (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Moulding By Coating Moulds (AREA)
Description
La présente invention concerne une pièce mécanique comportant un insert en matériau composite du type constitué de fibres céramiques dans une matrice métallique, ainsi qu'un procédé de fabrication de cette pièce mécanique et un dispositif de bobinage conçu pour la mise en oeuvre du procédé de fabrication. L'invention s'applique à tout type de pièce mécanique dont la fonction est de transmettre un effort de traction et/ou de compression principalement unidirectionnel.The present invention relates to a mechanical part comprising an insert made of composite material of the type consisting of ceramic fibers in a metal matrix, as well as a method of manufacturing this mechanical part and a winding device designed for implementing the manufacturing method. . The invention applies to any type of mechanical part whose function is to transmit a traction force and / or compression mainly unidirectional.
Dans le domaine aéronautique, notamment, un objectif constant est l'optimisation de la résistance des pièces mécaniques pour une masse et un encombrement minimaux. Ainsi, certaines pièces mécaniques peuvent comporter un insert en matériau composite à matrice métallique, de telles pièces pouvant être monoblocs. Un tel matériau composite comporte une matrice d'alliage métallique, par exemple d'alliage de titane Ti, au sein de laquelle s'étendent des fibres, par exemple des fibres céramiques de carbure de silicium SiC. De telles fibres présentent une résistance en traction et en compression bien supérieure à celle du titane. Ce sont donc principalement les fibres qui reprennent les efforts, la matrice d'alliage métallique assurant une fonction de liant avec le reste de la pièce, ainsi que de protection et d'isolation des fibres, qui ne doivent pas entrer en contact les unes avec les autres. En outre, les fibres céramiques sont résistantes à l'érosion, mais doivent nécessairement être renforcées par du métal.In the aeronautical field, in particular, a constant objective is the optimization of the resistance of mechanical parts for a minimum mass and size. Thus, some mechanical parts may comprise an insert made of composite material with a metal matrix, such parts being able to be monobloc. Such a composite material comprises a matrix of metal alloy, for example titanium alloy Ti, within which fibers extend, for example ceramic fibers of SiC silicon carbide. Such fibers have a much higher tensile and compressive strength than titanium. It is therefore mainly the fibers that take up the efforts, the metal alloy matrix ensuring a binder function with the rest of the part, as well as protection and insulation of the fibers, which must not come into contact with each other. others. In addition, the ceramic fibers are resistant to erosion, but must necessarily be reinforced with metal.
Les matériaux composites tels que décrits ci-dessus sont connus pour être utilisés, dans le domaine aéronautique, pour la fabrication de disques, d'arbres, de corps de vérins, de carters, d'entretoises ou comme renforts de pièces monoblocs telles que des aubes.The composite materials as described above are known to be used, in the aeronautical field, for the manufacture of disks, shafts, bodies of jacks, housings, spacers or as reinforcements of single-piece parts such as blades.
Une technique de fabrication de ces pièces est décrite dans le document
Toutefois, certaines pièces mécaniques requièrent des propriétés différentes de celles présentées par les pièces circulaires. C'est le cas notamment des bielles, de forme essentiellement oblongue, dont la fonction est de transmettre un effort de traction et/ou de compression unidirectionnel.However, some mechanical parts require properties different from those presented by the circular parts. This is the case in particular connecting rods, essentially oblong shape, whose function is to transmit a tensile force and / or unidirectional compression.
Une bielle en matrice métallique renforcée par des fibres ceramiques confirmes est décrite par
L'invention a notamment pour objet un procédé de fabrication d'une pièce mécanique comportant au moins un insert en matériau composite du type constitué de fibres céramiques dans une matrice métallique capable de transmettre des efforts de traction et/ou de compression unidirectionnels entre ses extrémités.The invention particularly relates to a method of manufacturing a mechanical part comprising at least one composite material insert of the type consisting of ceramic fibers in a metal matrix capable of transmitting tensile forces and / or unidirectional compression between its ends .
A cet effet, l'invention concerne un procédé de fabrication d'une pièce mécanique selon les caractéristiques de la revendication 1.For this purpose, the invention relates to a method for manufacturing a mechanical part according to the features of claim 1.
La pièce mécanique ainsi obtenue, par exemple une bielle, permet avantageusement de transmettre des efforts de traction et/ou de compression unidirectionnels.The mechanical part thus obtained, for example a connecting rod, advantageously makes it possible to transmit unidirectional traction and / or compression forces.
D'autres avantages et caractéristiques de l'invention ressortiront à la lecture de la description détaillée qui suit en référence aux figures annexées sur lesquelles :
- la
figure 1 représente une vue en perspective d'un exemple de pièce mécanique selon l'art antérieur ; - la
figure 2 représente une vue en perspective d'un exemple de dispositif de bobinage selon l'invention ; - la
figure 3 représente une vue en perspective d'un exemple d'insert obtenu selon le procédé de fabrication de l'invention ; - la
figure 4 représente un exemple d'insert, de conteneur destiné à accueillir l'insert et de couvercle métallique destiné à recouvrir de manière étanche le conteneur et l'insert ; - la
figure 5 représente une vue en perspective d'un exemple de pièce mécanique obtenue selon le procédé de fabrication de l'invention ; - la
figure 6 représente une variante du procédé de fabrication de l'invention ; - la
figure 7 représente une vue en coupe d'un autre exemple de pièce mécanique obtenue selon la variante du procédé de fabrication de l'invention ; et- la
figure 8 représente une vue en perspective de l'exemple de pièce mécanique obtenue selon la variante du procédé de fabrication de l'invention.
- la
- the
figure 1 is a perspective view of an example of a mechanical part according to the prior art; - the
figure 2 is a perspective view of an exemplary winding device according to the invention; - the
figure 3 represents a perspective view of an example of an insert obtained according to the manufacturing method of the invention; - the
figure 4 represents an example of an insert, a container for receiving the insert and a metal lid for sealingly covering the container and the insert; - the
figure 5 is a perspective view of an example of a mechanical part obtained according to the manufacturing method of the invention; - the
figure 6 represents a variant of the manufacturing method of the invention; - the
figure 7 is a sectional view of another example of a mechanical part obtained according to the variant of the manufacturing method of the invention; and- the
figure 8 represents a perspective view of the example of mechanical part obtained according to the variant of the manufacturing method of the invention.
- the
Les techniques de fabrication d'une pièce mécanique, comportant un insert en matériau composite, décrites dans le document
La
La
Le dispositif de bobinage 20 appartient à un ensemble formant un système de bobinage. Le système de bobinage comprend en outre des moyens pour mettre en rotation le dispositif de bobinage 20 et des moyens de fourniture d'un faisceau ou d'une nappe liée de fils enduits 32.The
La pièce formant mandrin 2 comporte deux portions de bobinage rectilignes 24. Ces portions de bobinage rectilignes 24 sont orientées perpendiculairement à l'axe de bobinage Z. Ainsi, au moins une partie du bobinage des fils 32 autour de la pièce formant mandrin 2 s'effectue selon une direction rectiligne. Le bobinage des fils enduits 32 s'effectue de manière perpendiculaire à l'axe de bobinage Z, autrement dit, les fils enduits 32 sont sensiblement orientés perpendiculairement à l'axe de bobinage Z.The
Dans l'exemple représenté sur la
Le bobinage autour de la pièce formant mandrin 2 comportant des portions de bobinage rectilignes 24 permet de générer en peu de temps un insert 3 comportant au moins une génératrice rectiligne constituée d'un grand nombre de fils enduits 32 parallèles et unidirectionnels.The winding around the
L'insert 3, une fois bobiné, peut être retiré du dispositif de bobinage 20 en désolidarisant les flasques 21 et 22 l'un de l'autre. La forme de l'insert 3 ainsi formé doit être figée pour éviter que les fils 32 perdent leur orientation. Plusieurs techniques peuvent être mises en oeuvre dans ce but.The
Une première technique de maintien en forme de l'insert 3 consiste à prévoir, en début de bobinage, une étape de bobinage d'un premier clinquant métallique d'accrochage de la partie interne de l'insert 3 et, en fin de bobinage, une étape de bobinage d'un second clinquant 28 métallique d'accrochage de la partie externe de l'insert 3. Dans cet exemple, le premier clinquant métallique constitue la pièce formant mandrin 2. Les fils enduits 32 se trouvent donc ainsi entre les clinquants 2 et 28, comme représenté sur la
Par ailleurs, comme illustré sur la
Chaque paire d'encoches 23 est destinée à permettre la fixation d'une sangle métallique 31. Les sangles métalliques 31 sont constituées d'un matériau métallique identique à celui du conteneur 4, décrit en liaison avec la
Une fois l'insert 3 bobiné et les sangles métalliques 31 mises en place, celui-ci peut être retiré du dispositif de bobinage 20 en désolidarisant les flasques 21 et 22 l'un de l'autre. Un exemple d'insert 3 ainsi obtenu est représenté en
Une deuxième technique de maintien en forme de l'insert 3, ne nécessitant pas l'utilisation de sangles 31, consiste à prévoir une pièce formant mandrin 2 formant un mandrin oblong comportant au moins un rebord radial, par exemple à section transversale en L ou en U, sur lequel s'enroulent les fils 32. Lorsqu'une nappe liée de fils enduits 32 est utilisée, il est possible de la solidariser à la pièce formant mandrin 2 sur laquelle elle est enroulée et à la nappe de la couche inférieure au moyen d'un procédé par soudage par contact entre deux électrodes et passage d'un courant moyenne fréquence. Les fils 32 sont ainsi soudés au fur et à mesure du bobinage de sorte que, lorsque l'insert 3 est extrait du dispositif de bobinage 20, il forme une pièce solidaire avec la pièce formant mandrin 2.A second technique for maintaining the shape of the
L'insert 3 est ensuite inséré dans un conteneur 4, comme représenté sur la
L'ensemble est ensuite usiné pour obtenir la pièce mécanique 10 finale : une bielle 10, représentée sur la
L'invention s'applique à tout type de pièce mécanique dont la fonction est de transmettre un effort de traction et/ou de compression principalement unidirectionnel et ne se limite donc pas uniquement aux bielles qui ne constituent qu'un exemple d'application.The invention applies to any type of mechanical part whose function is to transmit a traction force and / or compression mainly unidirectional and is therefore not limited only to connecting rods that are only an example of application.
Claims (7)
- Method for producing an elongated mechanical part (10, 110) having two ends and a cylindrical aperture (11, 12) at each end, the axes (Z1, Z2) of the apertures being mutually parallel, characterised in that an insert (3) made of composite material is produced by winding a plurality of coated wires (32), which form a bundle or a bonded mat and each comprise a ceramic fibre encased in a metal sheath, around a part (2) which forms a mandrel, at least a portion of the winding taking place in a rectilinear direction, the part (2) which forms a mandrel comprising two portions of rectilinear winding (24) interposed between two circular portions (25), and the insert being inserted, after formation, into a container (4) having a groove, the shape of which is complementary to that of the insert (3), and covered by a lid (5) in order to undergo hot isostatic compaction therein, the assembly then being machined in order to form said elongated mechanical part having two cylindrical apertures and ceramic fibres which are perpendicular to the axes of the apertures.
- Method for producing a mechanical part (10, 110) according to claim 1, wherein the two circular portions (25) have different radii.
- Method for producing a mechanical part (10, 110) according to either of the preceding claims, comprising the incorporation of two inserts (3) on each side of two opposite surfaces (42) of a container (4) in order to undergo hot isostatic compaction.
- Method for producing a mechanical part (110) according to the preceding claim, comprising the positioning of the inserts (3) in planes (P2,P2) which form a non-zero angle α.
- Elongated mechanical part (10, 110) having two ends and a cylindrical aperture at each end, comprising at least one insert (3) made of metal matrix composite material, within which ceramic fibres extend, the composite material insert (3) being obtained from a plurality of coated wires (32), which each comprise a ceramic fibre encased in a metal sheath, characterised in that the insert (3) has a geometry which describes a closed structure and the ceramic fibres of which are oriented, in part, in at least one rectilinear direction between the two cylindrical apertures (11, 12).
- Mechanical part (110) according to claim 5, comprising at least two inserts (3) which are positioned on each side of a central plane (P1) of the mechanical part (10).
- Mechanical part (110) according to claim 6, wherein the two inserts (3) are positioned in planes (P2, P3) which form an angle α between each other.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0705453A FR2919283B1 (en) | 2007-07-26 | 2007-07-26 | MECHANICAL PIECE COMPRISING AN INSERT IN COMPOSITE MATERIAL. |
| PCT/FR2008/001014 WO2009034263A2 (en) | 2007-07-26 | 2008-07-10 | Mechanical part including an insert made of a composite material |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP2191029A2 EP2191029A2 (en) | 2010-06-02 |
| EP2191029B1 true EP2191029B1 (en) | 2013-01-23 |
Family
ID=39537980
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP08830741A Active EP2191029B1 (en) | 2007-07-26 | 2008-07-10 | Mechanical part including an insert made of a composite material |
Country Status (10)
| Country | Link |
|---|---|
| US (1) | US8920935B2 (en) |
| EP (1) | EP2191029B1 (en) |
| JP (1) | JP2010534763A (en) |
| CN (1) | CN101999010B (en) |
| BR (1) | BRPI0814322A2 (en) |
| CA (1) | CA2694370C (en) |
| FR (1) | FR2919283B1 (en) |
| IL (1) | IL203453A (en) |
| RU (1) | RU2490355C2 (en) |
| WO (1) | WO2009034263A2 (en) |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2911524B1 (en) * | 2007-01-23 | 2009-08-21 | Snecma Sa | TUBULAR PIECE COMPRISING A METALLIC MATRIX COMPOSITE INSERT. |
| 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 |
| FR2946550A1 (en) * | 2009-06-16 | 2010-12-17 | Messier Dowty Sa | PROCESS FOR MANUFACTURING A METAL PIECE INCORPORATING A FIBROUS ANNULAR REINFORCEMENT. |
| BR112012001965B8 (en) | 2009-07-28 | 2021-08-03 | Snecma | beam for the suspension of a turbo engine on the structure of an aircraft, use of a beam, and aircraft |
| FR2950078B1 (en) * | 2009-09-11 | 2012-10-05 | Messier Dowty Sa | METAL PIECE PROVIDED WITH FIBROUS REINFORCEMENTS WITH BITEAUTEE END. |
| 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 |
| FR2975317B1 (en) * | 2011-05-18 | 2013-05-31 | Snecma | METHOD FOR MANUFACTURING BY DIFFUSION WELDING OF A MONOBLOC PIECE FOR A TURBOMACHINE |
| FR2978696B1 (en) * | 2011-08-01 | 2013-08-23 | Messier Bugatti Dowty | ROD IN COMPOSITE MATERIAL HAVING INCREASED MECHANICAL STRENGTH |
| CN106425022B (en) * | 2016-11-18 | 2019-01-18 | 南京理工大学 | A kind of method of CMT increasing material manufacturing composite element |
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| GB803270A (en) * | 1956-11-28 | 1958-10-22 | Richard Elliot Young | Improvements relating to filament wound hollow elements and methods for making the same |
| US3033487A (en) * | 1961-04-12 | 1962-05-08 | Uel T Walker | Fishhook and leader holder |
| US3668748A (en) * | 1969-09-12 | 1972-06-13 | American Standard Inc | Process for producing whisker-reinforced metal matrix composites by liquid-phase consolidation |
| US3669364A (en) * | 1970-02-09 | 1972-06-13 | North American Rockwell | Stress-oriented filament winding in composite panels |
| DE2137425A1 (en) * | 1970-07-30 | 1972-02-03 | Illinois Tool Works Ine , Chicago IU (VStA) | Shipping drum |
| JPS627825A (en) * | 1985-07-04 | 1987-01-14 | Toshiba Corp | Manufacture of preform of metal base composite material |
| JPH05508885A (en) * | 1990-06-29 | 1993-12-09 | フレックスリン サービシズ リミテッド | Method for manufacturing reinforced composite material and filament material for use in this method |
| JPH11147673A (en) * | 1997-11-17 | 1999-06-02 | Senshin Zairyo Riyo Gas Generator Kenkyusho:Kk | Preform manufacturing device for frm, and manufacture thereof |
| DE10005250B4 (en) * | 1999-02-09 | 2004-10-28 | Mtu Aero Engines Gmbh | Process for the production of fiber-reinforced metallic components |
| CN1860264A (en) * | 2003-08-04 | 2006-11-08 | 帝人纤维株式会社 | Method and device for producing ultra-short fibers |
| US20060225252A1 (en) * | 2003-08-04 | 2006-10-12 | Naohiko Shindo | Method and device for manufacturing extremely short fiber |
| FR2884564B1 (en) * | 2005-04-15 | 2011-01-14 | Snecma Moteurs | METHOD OF ASSEMBLING TWO PARTS OF WHICH AT LEAST ONE IS OF COMPOSITE MATERIAL, INSERT FOR THE REALIZATION OF THE ASSEMBLY |
| 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 |
| US8414724B2 (en) * | 2006-12-02 | 2013-04-09 | The Boeing Company | Composite tube having cobonded end fittings and method of making same |
| FR2911524B1 (en) * | 2007-01-23 | 2009-08-21 | Snecma Sa | TUBULAR PIECE COMPRISING A METALLIC MATRIX COMPOSITE INSERT. |
-
2007
- 2007-07-26 FR FR0705453A patent/FR2919283B1/en active Active
-
2008
- 2008-07-10 CA CA2694370A patent/CA2694370C/en active Active
- 2008-07-10 WO PCT/FR2008/001014 patent/WO2009034263A2/en not_active Ceased
- 2008-07-10 US US12/670,786 patent/US8920935B2/en active Active
- 2008-07-10 RU RU2010107049/02A patent/RU2490355C2/en active
- 2008-07-10 CN CN200880100598.4A patent/CN101999010B/en active Active
- 2008-07-10 JP JP2010517435A patent/JP2010534763A/en active Pending
- 2008-07-10 EP EP08830741A patent/EP2191029B1/en active Active
- 2008-07-10 BR BRPI0814322-6A2A patent/BRPI0814322A2/en not_active IP Right Cessation
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Also Published As
| Publication number | Publication date |
|---|---|
| CN101999010B (en) | 2014-07-30 |
| EP2191029A2 (en) | 2010-06-02 |
| US20100291339A1 (en) | 2010-11-18 |
| IL203453A (en) | 2014-08-31 |
| BRPI0814322A2 (en) | 2015-01-20 |
| CA2694370A1 (en) | 2009-03-19 |
| CN101999010A (en) | 2011-03-30 |
| FR2919283A1 (en) | 2009-01-30 |
| FR2919283B1 (en) | 2010-09-17 |
| US8920935B2 (en) | 2014-12-30 |
| RU2490355C2 (en) | 2013-08-20 |
| WO2009034263A3 (en) | 2009-10-22 |
| JP2010534763A (en) | 2010-11-11 |
| CA2694370C (en) | 2016-10-18 |
| WO2009034263A2 (en) | 2009-03-19 |
| RU2010107049A (en) | 2011-09-10 |
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