EP2552629B1 - Method of manufacturing an elongate insert made of a metal matrix composite - Google Patents
Method of manufacturing an elongate insert made of a metal matrix composite Download PDFInfo
- Publication number
- EP2552629B1 EP2552629B1 EP11718434.1A EP11718434A EP2552629B1 EP 2552629 B1 EP2552629 B1 EP 2552629B1 EP 11718434 A EP11718434 A EP 11718434A EP 2552629 B1 EP2552629 B1 EP 2552629B1
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- EP
- European Patent Office
- Prior art keywords
- shaping element
- insert
- coated
- bundle
- metal
- 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
- C22C47/20—Making alloys containing metallic or non-metallic fibres or filaments by subjecting to pressure and heat an assembly comprising at least one metal layer or sheet and one layer of fibres or filaments
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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
- B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
- B22F2998/10—Processes characterised by the sequence of their steps
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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
- Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
- Y10T156/10—Methods of surface bonding and/or assembly therefor
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49801—Shaping fiber or fibered material
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49947—Assembling or joining by applying separate fastener
- Y10T29/49966—Assembling or joining by applying separate fastener with supplemental joining
- Y10T29/49968—Metal fusion joining
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/29—Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
- Y10T428/2913—Rod, strand, filament or fiber
- Y10T428/2929—Bicomponent, conjugate, composite or collateral fibers or filaments [i.e., coextruded sheath-core or side-by-side type]
- Y10T428/2931—Fibers or filaments nonconcentric [e.g., side-by-side or eccentric, etc.]
Definitions
- the present invention relates to the field of composite metal matrix materials and more particularly to a method of manufacturing an insert formed of ceramic fibers in a metal matrix to reinforce a metal part.
- CMM composite metal matrix insert
- 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 tensile strength much higher than that of titanium (typically 4000 MPa against 1000 MPa). It is therefore 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. other.
- the ceramic fibers are resistant to erosion, but must necessarily be reinforced with metal.
- These composite materials can be used in the manufacture of disks, shafts, cylinder bodies, housings, spacers, as reinforcements of monolithic parts such as blades, etc.
- a known reinforcement technique consists in inserting a circular winding of coated fibers into the part.
- a CMM insert manufacturing technique is based on the principle of coated wire winding described in the patent EP 1.726.677 deposited in the name of Snecma.
- the insert is obtained from a plurality of coated yarns each comprising a ceramic fiber coated with a metal sheath. This type of yarn is referred to as coated yarn thereafter.
- the manufacture comprises a step of winding a bundle or a sheet connected son son coated around a piece of revolution perpendicular to the axis of the piece.
- the insert is then subjected to a hot isostatic pressing step in a container.
- a container is a blank of a metal part in which a cavity for receiving the insert made of CMM material has been machined and which is then subjected to a hot isostatic compaction treatment. This treatment is designated CIC thereafter.
- the described parts thus obtained are of circular type and are particularly suitable, in addition to the compressor discs for producing circular parts such as shafts, cylinder bodies or housings.
- the method comprises producing an insert blank by winding a bundle or a bonded web of coated wires around an annular support, a portion of which comprises a rectilinear or substantially rectilinear portion, as described in FIG. document EP-1950003-A1 .
- the process described in the patent FR 2,919,284 to Snecma and Messier-Dowty develops this principle and then comprises inserting the above insert blank into a first metal container, hot isostatic compaction of the first container, followed by machining thereof to form an element. insert.
- the method of manufacturing a mechanical part comprises the following steps: insertion of the insert element into a second container, hot isostatic compaction of the second container and machining of the second container for form the desired mechanical part.
- the mechanical part thus obtained for example a connecting rod, advantageously makes it possible to transmit unidirectional tensile and / or compressive forces in the direction of the ceramic fibers that have been integrated therein.
- the winding in particular on oval shapes, induces stresses in the wound insert that may loosen resulting in deformation of the insert during cutting.
- a reinforcement whose number of fibers is lower along the edge of the integral piece of the fastener allows a better transition of efforts at the latter.
- the patent US3828417 discloses a method for forming a bundle of coated fibers.
- the objective of the present invention is the development of a technique for making inserts at reduced cost and easily industrializable.
- the invention also aims a manufacturing technique that allows the realization of so-called form inserts that is to say whose cross section may be different from the square or rectangular shape.
- This object is achieved by a method of manufacturing an elongated insert according to claim 1.
- the beam is formed from coated yarns which are unwound from yarn packages.
- the bundle of wires before it passes through the shaping element has interstitial spaces resulting from the circular section of the coated wires.
- the shaping element is dimensioned so as to reduce the expansion of the wires and the interstitial spaces while giving the beam the desired shape. This solves the problem of industrialization and formatting of the wire bundle.
- the passage section of the shaping element is chosen freely according to the shape, in the transverse plane, desired of the insert.
- the shaping element comprises at least two rotary rollers, the axes of the two rollers being oriented perpendicular to the direction of advancement of the coated son.
- the shaping element comprises in particular fixed lateral supports between the rollers.
- the shaping element may also comprise a plurality of rollers constituting the contour of the passage section. The function of the rollers is to reduce the friction on the bundle of coated threads accompanying its movement. Fixed elements are also suitable insofar as the friction of the fibers is reduced.
- a metal foil also referred to as a foil, is advantageously interposed between the coated strands of the bundle and at least a portion of the sides of the shaping element.
- the rings are formed for example of a metal sheet, forming a strap with which the beam is tightly wrapped and whose ends are welded after being folded over one another.
- the bundle of coated wires is then cut to the desired length corresponding to the length of the insert to be placed in the metal container.
- the son coated before their bundling are guided in their movement towards the shaping element so as to form subassemblies or elementary beams. It may be sheets that are superimposed on each other to form said beam.
- An elementary beam is formed by simultaneously unwinding the coated son of the subassembly from separate coils. For example one can thus form a stack of plies of rectilinear coated son obtained by flat juxtaposing a given number of coated son, until a number of layers determined. More particularly, a first ply is deposited on a bearing surface, in particular comprising a metal sheet, and the last sheet is covered through the shaping element.
- the elementary beams can have any shape of cross section.
- the son is coated in elementary bundles in a plurality of guides, chutes or tubes which are arranged to converge towards the passage section of the forming element.
- the method of the invention is a step of a method of manufacturing a metal part comprising the incorporation of the insert thus formed into a metal container and hot isostatic compaction of the assembly, as described by example in the patent application FR2933422 or the request FR2933423 in the name of Messier Dowty .
- the solution of the invention allows the incorporation of the insert in a container, immediately downstream of the shaping element.
- the container may comprise a longitudinal through housing in which it comes to slide the bundle of coated son.
- FIG. 1a extracted from the patent application FR 2,919,284 to Snecma and Messier-Dowty we see a container 1 with a main body 4 of elongate shape, intended to form a connecting rod of a landing gear for example. It has machined a groove 41 on each of the two faces of the body 4. This groove allows the housing of an insert 3 which comprises two straight portions parallel or not between them joined at the ends by a portion in an arc.
- 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 lid must be perfectly assembled to prevent the fibers, which have a very small diameter, of the order of 0.25 mm, can not escape during the 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 a suitable enclosure to undergo hot isostatic compaction treatment.
- This treatment is intended to make the container, its lid and the plies of coated son solidarity with each other and form a monolithic piece.
- 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 clearance with the portion of the cover 5 adjacent to the pin 51.
- the pressure is exerted in the direction perpendicular to the surface of the cover causing the collapse of the covers.
- the heat and the pressure, respectively of the order of 1000 ° C. and 1000 bars allow the metal of the matrix to fill the voids between the coated wires constituting the insert.
- the volume of the insert decreases by about 23%.
- the post is thus moved towards the bottom of the groove and the game on either side of the post is absorbed.
- the metal parts soldered by diffusion and the coated wire insert compacted; the part is thus reinforced by the coated threads imprisoned in the mass.
- the figure 1d represents the part blank obtained with two inserts visible in transparency. The blank is then machined to obtain the desired part. The ceramic fibers are thus incorporated in the areas of the part which ensure the transmission of the forces in traction and compression.
- inserts used according to the teaching of this patent FR 2 919 283 are ring-shaped but as described in the patent application FR 2 919 284 they can be formed of elongated elements in bars. In the latter case the inserts are incorporated, according to the technique described in this document, in the container after having been compacted beforehand.
- the realization of rectilinear inserts according to FR 2 919 284 comprises winding the coated wires around a ring-shaped winding device with rectilinear portions.
- the shape may be oblong, with rectilinear portions, or polygonal whose sides of the polygon constitute the rectilinear portions.
- the turns of the ring are immobilized together by means of welded metal straps.
- the assembly is incorporated in a container and undergoes hot isostatic compaction treatment according to the technique described above. From the semi-finished part, elongated compact inserts are manufactured which are individually incorporated into containers for the manufacture of parts with ceramic fiber reinforcements.
- the embodiment of the inserts is simplified by forming inserts of elongate shape made directly of coated wires 13 assembled in the manner of bundles or bundles.
- an example of an installation for carrying out the method of the invention comprises a reel 10 supporting a plurality of rows of reels 12 on which the coated wires 13 are wound. Coated wires are driven from their respective coils in a system slides chute 14 to which they converge. The system gathers the coated wires into a bundle. At this stage the beam is relatively abundant.
- the coated yarns are advantageously arranged in a plurality of subassemblies or layers of coated yarns 13 juxtaposed, parallel to each other.
- a foil or foil 16, thin, is disposed on the bottom of the gutter-shaped tool 14.
- the metal foil is preferably the same as that of the metal part to which the insert is intended. This is for example a titanium alloy.
- Coated son rest on the lower foil 16. They are stacked on each other for example in layers.
- the width of the plies, the number of coated threads which constitute the plies, may vary from the base to the upper ply.
- the beam may have a trapezoidal shape in section.
- a foil 15 is placed on the top of the stack of plies son coated.
- the number of threads in the plies is not limiting, it depends on the part to be manufactured, the representation of the figures is merely indicative, the diameter of the threads is not at the same scale as that of the gutter.
- the coated yarns are juxtaposed in the webs without fluttering or with a minimum of floating between the yarns. At this stage the coated wires have not undergone any transverse stress.
- the wires can be arranged in sub-assemblies formed of elementary beams that are united in a single beam, 13f.
- the beam 13f coated son is thus guided through the shaping element 17 where it undergoes a transverse compression.
- the shaping element here comprises two rollers 17g with horizontal axes. As we see on the figure 3 , the rollers are rotatably mounted in a frame 17b. The spacing between the two rollers can be adjusted by vertical displacement of their support. Appropriate motors possibly, not shown, drive them in rotation.
- the contour of the passage section of the shaping element is completed by two fixed supports, forming slides 17l, arranged laterally on either side of the beam.
- the supports 17l are integral with the frame 17b. According to this example, they are inclined relative to the vertical.
- the contour of the passage section of the shaping element is thus trapezoidal.
- the bundle of coated wires takes the form of the shaping element, here trapezoidal. At the output of the shaping element, it is therefore necessary to maintain the beam in the given form.
- Small foils 18 forming straps are then put in place to hold the assembly, by going around the bundle of coated wires.
- the beam is thus pulled through the shaping element by means of a traction tool by means of clamps for example.
- the insert 13i is shown finished at figure 4 .
- a plurality of rollers or rollers may be arranged in the shaping element around the beam to give it a polygonal shape.
- the sides of the polygon can be straight but they can also be curved. Just choose a suitable profile.
- the shape and the transverse dimensions of the shaping element can be defined by the geometry and the dimensions of the insert that one wishes to use. In this case, the number of coated wires required to form the insert is determined. Conversely, an insert with a determined number of coated wires may be needed. In this case, the passage section of the shaping element is adjusted so that it can contain as output the desired number of coated wires.
- the figure 5 shows another non-limiting example of embodiment of the shaping element. It is formed of two rollers 17'g of horizontal axes and curved profile cooperating with two rollers 17'l of vertical axes and straight profile.
- the present method also allows the realization of a plurality of inserts simultaneously, cutting the inserts in the length of the beam thus obtained.
- the insert once finished; as represented in figure 4 is incorporated in a metal container according to the known method and described above to form a metal part.
- a metal container according to the known method and described above to form a metal part.
- grooves are made rectilinear in which there are two rectilinear inserts per side of the container. For the rest the process is the same.
- one of the foils is used both as a support and as a lid of the metal container in which the insert is disposed.
- the lid is welded to the container while realizing the vacuum in the room before the hot isostatic compaction treatment.
Description
La présente invention concerne le domaine des matériaux composites à matrice métallique et vise plus particulièrement un procédé de fabrication d'un insert formé de fibres céramiques dans une matrice métallique pour renforcer une pièce métallique.The present invention relates to the field of composite metal matrix materials and more particularly to a method of manufacturing an insert formed of ceramic fibers in a metal matrix to reinforce a metal part.
Dans le domaine de l'aéronautique, notamment, un objectif constant est l'optimisation de la résistance des pièces pour une masse et un encombrement minimaux. Certaines pièces peuvent désormais comporter un insert en matériau composite à matrice métallique, désigné par la suite CMM, la pièce pouvant être par ailleurs monolithique. 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 bien supérieure à celle du titane (typiquement, 4000 MPa contre 1000 MPa). Ce sont donc 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 field of aeronautics, in particular, a constant objective is the optimization of the resistance of the parts for a minimum mass and a bulk. Some parts may now include a composite metal matrix insert, hereafter referred to as CMM, the part possibly being monolithic. 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 tensile strength much higher than that of titanium (typically 4000 MPa against 1000 MPa). It is therefore 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. other. In addition, the ceramic fibers are resistant to erosion, but must necessarily be reinforced with metal.
Ces matériaux composites peuvent être utilisés dans la fabrication de disques, d'arbres, de corps de vérins, de carters, d'entretoises, comme renforts de pièces monolithiques telles des aubes, etc.These composite materials can be used in the manufacture of disks, shafts, cylinder bodies, housings, spacers, as reinforcements of monolithic parts such as blades, etc.
Pour des disques de compresseur dans un turboréacteur par exemple une technique connue de renforcement consiste à insérer dans la pièce un bobinage circulaire de fibres enduites. Une technique de fabrication d'insert CMM repose sur le principe de bobinage de fils enduits décrit dans le brevet
Les pièces décrites ainsi obtenues sont de type circulaire et conviennent particulièrement, outre les disques de compresseur pour la réalisation de pièces circulaires telles que des arbres, des corps de vérins ou des carters.The described parts thus obtained are of circular type and are particularly suitable, in addition to the compressor discs for producing circular parts such as shafts, cylinder bodies or housings.
D'autres pièces mécaniques requièrent des propriétés différentes de celles présentées par les pièces circulaires. C'est le cas notamment des bielles utilisées par exemple dans les systèmes d'atterrissage ou des pièces de structure telles que des suspensions de moteurs, de forme essentiellement oblongue. La fonction de ces pièces est de transmettre un effort de traction et/ou de compression unidirectionnel. Le renforcement de ces pièces nécessite alors des inserts en CMM de forme rectiligne ou sensiblement rectiligne, au moins en partie. En effet les fibres doivent être orientées suivant la direction des efforts.Other mechanical parts require properties different from those presented by the circular parts. This is particularly the case of rods used for example in landing systems or structural parts such as engine suspensions, substantially oblong shape. The function of these parts is to transmit a tensile force and / or unidirectional compression. The reinforcement of these parts then requires CMM inserts of rectilinear or substantially rectilinear shape, at least in part. Indeed, the fibers must be oriented in the direction of the efforts.
La fabrication de ces inserts de manière industrielle et au moindre coût est délicate.The manufacture of these inserts industrially and at the least cost is delicate.
On connaît un procédé de fabrication d'une pièce mécanique comportant au moins un insert en matériau CMM. Le procédé comprend la fabrication d'une ébauche d'insert par bobinage d'un faisceau ou d'une nappe liée de fils enduits autour d'un support annulaire dont une partie comprend une portion rectiligne ou sensiblement rectiligne, comme cela est décrit dans le document
Le procédé décrit dans le brevet
Au lieu de passer par l'étape intermédiaire de compaction de l'ébauche d'insert suivie de sa découpe en éléments d'insert rectilignes, on pourrait envisager de découper la bobine annulaire formant l'ébauche en assurant le maintien des fils enduits en faisceau. La demande de brevet
Cette solution présente plusieurs inconvénients qui impactent l'industrialisation de ces opérations :
On perd les fils enduits au niveau des parties non droites. Cette perte n'est pas négligeable car le demi-produit fil enduit représente un coût important dans le coût total de la pièce.This solution has several drawbacks that impact the industrialization of these operations:
The coated wires are lost at the non-straight parts. This loss is not negligible because the semi-finished wire product represents a significant cost in the total cost of the part.
Le bobinage, notamment sur des formes ovales, induit des contraintes dans l'insert bobiné qui risquent de se relâcher se traduisant par une déformation de l'insert lors de la découpe.The winding, in particular on oval shapes, induces stresses in the wound insert that may loosen resulting in deformation of the insert during cutting.
Ces techniques nécessitent de multiplier les systèmes de maintien des fils enduits au droit des zones de découpe.
Par ailleurs, une technique fondée sur l'enroulement par bobinage d'une nappe de fils enduits préalablement assemblés vise essentiellement la réalisation d'inserts de section transversale, perpendiculaire aux fibres, carrée ou rectangulaire.
Pour certaines applications, il serait souhaitable d'avoir un insert de section différente du carré ou du rectangle afin d'améliorer la reprise d'efforts entre l'insert composite et le reste de la structure de la pièce. En effet, des renforts de section par exemple trapézoïdale ou elliptique permettraient d'éviter ou au moins de limiter les sauts de raideur et ainsi d'améliorer la tenue mécanique des zones de transition.
Par exemple, pour des pièces allongées telles que des pièces de train d'atterrissage ou des bielles de suspension de moteur comportant des attaches latérales entre leurs extrémités, un renfort dont le nombre de fibres est plus faible le long du bord de la pièce solidaire de l'attache permet une meilleure transition des efforts au niveau de cette dernière.
Le brevet
L'objectif de la présente invention est la mise au point d'une technique de réalisation d'inserts à coût réduit et facilement industrialisable.
L'invention a également pour objectif une technique de fabrication qui permet la réalisation d'inserts dits de forme c'est-à-dire dont la section transversale peut être différente de la forme carrée ou rectangulaire.
On parvient à cet objectif avec un procédé de fabrication d'un insert de forme allongée selon la revendication 1. De préférence, on forme le faisceau à partir de fils enduits que l'on déroule depuis des bobines de fils.These techniques require the multiplication of the maintenance systems of the coated wires to the right of the cutting zones.
Moreover, a technique based on the winding by winding of a ply of pre-assembled coated yarns is essentially aimed at producing inserts of cross section, perpendicular to the fibers, square or rectangular.
For some applications, it would be desirable to have an insert of different section square or rectangle to improve the recovery of forces between the composite insert and the rest of the structure of the room. Indeed, sectional reinforcements, for example trapezoidal or elliptical, would avoid or at least limit stiffness jumps and thus improve the mechanical strength of the transition zones.
For example, for elongated parts such as landing gear pieces or engine suspension connecting rods having lateral fasteners between their ends, a reinforcement whose number of fibers is lower along the edge of the integral piece of the fastener allows a better transition of efforts at the latter.
The patent
The objective of the present invention is the development of a technique for making inserts at reduced cost and easily industrializable.
The invention also aims a manufacturing technique that allows the realization of so-called form inserts that is to say whose cross section may be different from the square or rectangular shape.
This object is achieved by a method of manufacturing an elongated insert according to claim 1. Preferably, the beam is formed from coated yarns which are unwound from yarn packages.
Le faisceau de fils avant son passage au travers de l'élément conformateur présente des espaces interstitiels résultant de la section circulaire des fils enduits. L'élément conformateur est dimensionné de manière à réduire le foisonnement des fils et les espaces interstitiels tout en donnant au faisceau la forme souhaitée. On résout ainsi simplement le problème d'industrialisation et mise en forme du faisceau de fils. La section de passage de l'élément conformateur est choisie librement en fonction de la forme, dans le plan transversal, souhaitée de l'insert.The bundle of wires before it passes through the shaping element has interstitial spaces resulting from the circular section of the coated wires. The shaping element is dimensioned so as to reduce the expansion of the wires and the interstitial spaces while giving the beam the desired shape. This solves the problem of industrialization and formatting of the wire bundle. The passage section of the shaping element is chosen freely according to the shape, in the transverse plane, desired of the insert.
Selon un mode de réalisation, l'élément conformateur comprend au moins deux galets rotatifs, les axes des deux galets étant orientés perpendiculairement à la direction d'avancement des fils enduits. Pour compléter le contour, l'élément conformateur comprend notamment des supports latéraux fixes entre les galets. L'élément conformateur peut aussi comprendre une pluralité de galets constituant le contour de la section de passage. La fonction des galets est de réduire les frottements sur le faisceau de fils enduits en accompagnant son déplacement. Des éléments fixes conviennent aussi dans la mesure où le frottement des fibres est réduit.According to one embodiment, the shaping element comprises at least two rotary rollers, the axes of the two rollers being oriented perpendicular to the direction of advancement of the coated son. To complete the contour, the shaping element comprises in particular fixed lateral supports between the rollers. The shaping element may also comprise a plurality of rollers constituting the contour of the passage section. The function of the rollers is to reduce the friction on the bundle of coated threads accompanying its movement. Fixed elements are also suitable insofar as the friction of the fibers is reduced.
On peut ainsi former un élément conformateur dont la section de passage est polygonale avec des côtés rectilignes ou courbes ou encore de section ovale ou circulaire.It is thus possible to form a shaping element whose passage section is polygonal with rectilinear or curved sides or of oval or circular section.
Afin de faciliter le guidage des fibres à l'élément conformateur et ultérieurement leur maintien ensemble dans le faisceau, une feuille métallique, désignée clinquant aussi, est avantageusement interposée entre les fils enduits du faisceau et au moins une partie des côtés de l'élément conformateur.In order to facilitate the guiding of the fibers to the shaping element and subsequently to hold them together in the bundle, a metal foil, also referred to as a foil, is advantageously interposed between the coated strands of the bundle and at least a portion of the sides of the shaping element. .
On assure le maintien de l'assemblage des fils enduits par des anneaux ou bagues placés le long de l'insert en aval de son passage à travers de l'élément conformateur. Les bagues sont formées par exemple d'une feuille métallique, formant une sangle avec laquelle on entoure le faisceau de manière serrée et dont on soude les extrémités après les avoir repliées l'une sur l'autre.Maintaining the assembly of coated son by rings or rings placed along the insert downstream of its passage through the shaping element. The rings are formed for example of a metal sheet, forming a strap with which the beam is tightly wrapped and whose ends are welded after being folded over one another.
On tronçonne ensuite le faisceau de fils enduits à la longueur souhaitée correspondant à la longueur de l'insert à placer dans le conteneur métallique. Pour éviter le foisonnement des fils enduits en extrémités de l'insert, rendant difficile la manipulation de celui-ci et sa mise en place dans le conteneur, il est judicieux de scier le faisceau à travers une bague de serrage car les portions de bague obtenues sont placées en extrémité et assurent le serrage du faisceau.The bundle of coated wires is then cut to the desired length corresponding to the length of the insert to be placed in the metal container. To avoid the proliferation of son coated end of the insert, making it difficult to handle it and its introduction in the container, it is advisable to saw the beam through a clamping ring because the ring portions obtained are placed at the end and ensure the tightening of the beam.
Selon une mise en oeuvre du procédé, les fils enduits avant leur regroupement en faisceau sont guidées dans leur déplacement vers l'élément conformateur de manière à former des sous ensembles ou faisceaux élémentaires. Il peut s'agir de nappes que l'on superpose les unes sur les autres pour former ledit faisceau. On forme un faisceau élémentaire en déroulant simultanément les fils enduits du sous ensemble depuis des bobines séparées. Par exemple on peut former ainsi un empilement de nappes de fils enduits rectilignes obtenues en juxtaposant à plat un nombre déterminé de fils enduits, jusqu'à obtenir un nombre de nappes déterminé. Plus particulièrement, on dépose une première nappe sur une surface d'appui, notamment comprenant une feuille métallique, et on recouvre la dernière nappe à travers de l'élément conformateur. Au lieu de nappes, les faisceaux élémentaires peuvent avoir toute forme de section transversale.According to one implementation of the method, the son coated before their bundling are guided in their movement towards the shaping element so as to form subassemblies or elementary beams. It may be sheets that are superimposed on each other to form said beam. An elementary beam is formed by simultaneously unwinding the coated son of the subassembly from separate coils. For example one can thus form a stack of plies of rectilinear coated son obtained by flat juxtaposing a given number of coated son, until a number of layers determined. More particularly, a first ply is deposited on a bearing surface, in particular comprising a metal sheet, and the last sheet is covered through the shaping element. Instead of plies, the elementary beams can have any shape of cross section.
Selon une autre mise en oeuvre, on regroupe les fils enduits en faisceaux élémentaires dans une pluralité de guides, goulottes ou tubes qui sont disposés de manière à converger vers la section de passage de l'élément conformateur.According to another embodiment, the son is coated in elementary bundles in a plurality of guides, chutes or tubes which are arranged to converge towards the passage section of the forming element.
Le procédé de l'invention est une étape d'un procédé de fabrication d'une pièce métallique comprenant l'incorporation de l'insert ainsi réalisé dans un conteneur métallique et la compaction isostatique à chaud de l'ensemble, comme cela est décrit par exemple dans la demande de brevet
Selon ce type de procédé,
- au moins un logement pour un insert est usiné dans un corps métallique formant le conteneur,
- ledit insert est disposé dans le logement,
- un couvercle métallique est placé sur le corps de façon à recouvrir l'insert,
- le couvercle est soudé sur le corps métallique,
- l'ensemble du corps métallique avec couvercle est soudé par compression isostatique à chaud et
- on usine ledit ensemble traité pour obtenir ladite pièce.
- at least one housing for an insert is machined in a metal body forming the container,
- said insert is disposed in the housing,
- a metal cover is placed on the body so as to cover the insert,
- the lid is welded to the metal body,
- the entire metal body with cover is welded by hot isostatic compression and
- said treated assembly is machined to obtain said workpiece.
La solution de l'invention permet l'incorporation de l'insert dans un conteneur, immédiatement en aval de l'élément conformateur. Par exemple, le conteneur peut comprendre un logement longitudinal traversant dans lequel on vient glisser le faisceau de fils enduits.The solution of the invention allows the incorporation of the insert in a container, immediately downstream of the shaping element. For example, the container may comprise a longitudinal through housing in which it comes to slide the bundle of coated son.
L'invention sera mieux comprise et d'autres buts détails caractéristiques et avantages de celles-ci apparaîtront plus clairement au cours de la description explicative détaillée qui suit, de modes de réalisation de l'invention donnés à titre d'exemple purement illustratif et non limitatif en référence aux dessins schématiques annexés.The invention will be better understood and other features and advantages thereof will become more clearly apparent in the following detailed explanatory description of embodiments of the invention given by way of purely illustrative and non-illustrative example. limiting with reference to the attached schematic drawings.
Sur ces dessins
- La
figure 1 montre les différentes étapes 1a, à 1d de fabrication d'une pièce de forme allongée selon l'art antérieur ; - La
figure 2 représente une vue de côté d'une installation de fabrication d'un insert rectiligne conforme à l'invention ; - La
figure 3 montre l'installation de lafigure 2 , vue de face ; - La
figure 4 montre un insert fabriqué conformément à l'invention ; - La
figure 5 montre une variante de filière de forme.
- The
figure 1 shows thedifferent steps 1a to 1d of manufacturing an elongate piece according to the prior art; - The
figure 2 represents a side view of an installation for manufacturing a rectilinear insert according to the invention; - The
figure 3 shows the installation of thefigure 2 , front view ; - The
figure 4 shows an insert manufactured according to the invention; - The
figure 5 shows a variant of shape die.
Sur la
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, de l'ordre de 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.The grooves and the inserts are complementary shapes so that the insert is fit without play in the groove. Note that the groove in the container and the pin on the lid must be perfectly assembled to prevent the fibers, which have a very small diameter, of the order of 0.25 mm, can not escape during the hot isostatic compaction. Two
Le conteneur est visible sur la
La chaleur et la pression, respectivement de l'ordre de 1000°C et 1000 bars permettent au métal de la matrice de combler les vides entre les fils enduits constituant l'insert. Le volume de l'insert diminue d'environ 23%. Le tenon est ainsi déplacé en direction du fond de la rainure et le jeu de part et d'autre du tenon est absorbé. À la fin du processus, les parties métalliques se sont soudées par diffusion et l'insert de fils enduits s'est compacté; la pièce est ainsi renforcée par les fils enduits emprisonnés dans la masse.The heat and the pressure, respectively of the order of 1000 ° C. and 1000 bars allow the metal of the matrix to fill the voids between the coated wires constituting the insert. The volume of the insert decreases by about 23%. The post is thus moved towards the bottom of the groove and the game on either side of the post is absorbed. At the end of the process, the metal parts soldered by diffusion and the coated wire insert compacted; the part is thus reinforced by the coated threads imprisoned in the mass.
La
Les inserts utilisés selon l'enseignement de ce brevet
La réalisation des inserts rectilignes selon
Après formation de l'enroulement du ou des fils enduits en un anneau, les spires de l'anneau sont immobilisées entre elles au moyen de sangles métalliques soudées. L'ensemble est incorporé dans un conteneur et subit un traitement de compaction isostatique à chaud selon la technique décrite ci-dessus. A partir de la pièce semi finie on usine des inserts compacts de forme allongée que l'on incorpore individuellement dans des conteneurs pour la fabrication de pièces avec des renforts en fibres céramiques.After forming the winding of the son or son coated in a ring, the turns of the ring are immobilized together by means of welded metal straps. The assembly is incorporated in a container and undergoes hot isostatic compaction treatment according to the technique described above. From the semi-finished part, elongated compact inserts are manufactured which are individually incorporated into containers for the manufacture of parts with ceramic fiber reinforcements.
Conformément à l'invention, on simplifie la réalisation des inserts en formant des inserts de forme allongée constitués directement de fils enduits 13 assemblés à la manière de fagots ou de faisceaux.According to the invention, the embodiment of the inserts is simplified by forming inserts of elongate shape made directly of
En se reportant à la
Un clinquant ou feuille métallique 16, mince, est disposé sur le fond de l'outillage en forme de gouttière 14. Le métal du clinquant est de préférence le même que celui de la pièce métallique à laquelle l'insert est destiné. Il s'agit par exemple d'un alliage de titane.A foil or foil 16, thin, is disposed on the bottom of the gutter-shaped
Les fils enduits reposent sur le clinquant inférieur 16. Ils sont empilés les uns sur les autres par exemple en nappes. La largeur des nappes, le nombre de fils enduits qui constituent les nappes, peut varier depuis la base jusqu'à la nappe supérieure. Par exemple, le faisceau peut avoir une forme trapézoïdale en section. Un clinquant 15 est placé sur le sommet de l'empilement des nappes de fils enduits.Coated son rest on the
Le nombre de fils dans les nappes n'est pas limitatif, il dépend de la pièce à fabriquer, la représentation des figures est simplement indicative, le diamètre des fils n'est pas à la même échelle que celle de la gouttière. Les fils enduits sont juxtaposés dans les nappes sans flottement ou avec un minimum de flottement entre les fils. A ce stade les fils enduits n'ont subi aucune contrainte transversale.The number of threads in the plies is not limiting, it depends on the part to be manufactured, the representation of the figures is merely indicative, the diameter of the threads is not at the same scale as that of the gutter. The coated yarns are juxtaposed in the webs without fluttering or with a minimum of floating between the yarns. At this stage the coated wires have not undergone any transverse stress.
Au lieu de nappes on peut disposer les fils en sous ensembles formés de faisceaux élémentaires que l'on réunit en un faisceau unique, 13f.Instead of layers, the wires can be arranged in sub-assemblies formed of elementary beams that are united in a single beam, 13f.
Le faisceau 13f de fils enduits est ainsi guidé à travers l'élément conformateur 17 où il subit une compression transversale. L'élément conformateur comprend ici deux galets 17g à axes horizontaux. Comme on le voit sur la
En passant au travers de l'élément conformateur, le faisceau de fils enduits prend la forme de l'élément conformateur, ici trapézoïdal. En sortie de l'élément conformateur, il est donc nécessaire d'assurer le maintien du faisceau dans la forme donnée.Passing through the shaping element, the bundle of coated wires takes the form of the shaping element, here trapezoidal. At the output of the shaping element, it is therefore necessary to maintain the beam in the given form.
Des petits clinquants 18 formant des sangles sont ensuite mis en place pour maintenir l'ensemble, en faisant le tour du faisceau de fils enduits.Small foils 18 forming straps are then put in place to hold the assembly, by going around the bundle of coated wires.
Le faisceau est ainsi tiré à travers l'élément conformateur au moyen d'un outil de traction par l'intermédiaire de pinces par exemple.The beam is thus pulled through the shaping element by means of a traction tool by means of clamps for example.
L'insert 13i est représenté fini à la
On comprend que le présent procédé n'est pas limité à la réalisation d'inserts de section carrée, rectangulaire ou trapézoïdale. De nombreuses formes sont à la portée de l'homme du métier. On peut disposer dans l'élément conformateur une pluralité de rouleaux ou galets autour du faisceau pour lui donner une forme polygonale. Les côtés du polygone peuvent être droits mais ils peuvent aussi être courbes. Il suffit de choisir un profil convenable.It is understood that the present method is not limited to the production of inserts of square, rectangular or trapezoidal section. Many forms are within the reach of the skilled person. A plurality of rollers or rollers may be arranged in the shaping element around the beam to give it a polygonal shape. The sides of the polygon can be straight but they can also be curved. Just choose a suitable profile.
La forme et les dimensions transversales de l'élément conformateur peuvent être définies par la géométrie et les dimensions de l'insert que l'on souhaite utiliser. Dans ce cas on détermine le nombre de fils enduits nécessaire pour former l'insert. Inversement on peut avoir besoin d'un insert avec un nombre déterminé de fils enduits. Dans ce cas, on ajuste la section de passage de l'élément conformateur de manière à ce qu'il puisse contenir en sortie le nombre souhaité de fils enduits.The shape and the transverse dimensions of the shaping element can be defined by the geometry and the dimensions of the insert that one wishes to use. In this case, the number of coated wires required to form the insert is determined. Conversely, an insert with a determined number of coated wires may be needed. In this case, the passage section of the shaping element is adjusted so that it can contain as output the desired number of coated wires.
Il est avantageux de disposer d'éléments de guidage réglables en position transversalement pour permettre en position rétractée la mise en place du faisceau de fils enduits avant qu'ils ne soient serrés sur le faisceau. Le réglage de l'écartement des galets et des supporte métalliques permet d'ajuster la section de passage et celle de sortie du faisceau de fils enduits.It is advantageous to have guide members adjustable in position transversely to allow in the retracted position the establishment of the bundle of coated son before they are tight on the beam. The adjustment of the spacing of the rollers and the metal supports makes it possible to adjust the passage section and the output section of the bundle of coated threads.
Il peut être également avantageux de disposer des éléments vibrants favorisant le tassement des fils enduits dans le faisceau.It may also be advantageous to have vibrating elements promoting the compression of the coated wires in the bundle.
La
Le présent procédé permet également la réalisation d'une pluralité d'inserts simultanément, on découpe les inserts dans la longueur du faisceau ainsi obtenu.The present method also allows the realization of a plurality of inserts simultaneously, cutting the inserts in the length of the beam thus obtained.
L'insert une fois terminé ; tel que celui représenté à la
Conformément à un mode de réalisation particulier de la pièce métallique, l'un des clinquants est utilisé à la fois comme support et comme couvercle du conteneur métallique dans lequel l'insert est disposé. Le couvercle est soudé sur le conteneur tout en réalisant le vide dans la pièce avant le traitement de compaction isostatique à chaud.According to a particular embodiment of the metal part, one of the foils is used both as a support and as a lid of the metal container in which the insert is disposed. The lid is welded to the container while realizing the vacuum in the room before the hot isostatic compaction treatment.
Claims (12)
- Method for manufacturing an insert of elongate shape designed to be incorporated by CIC into a metal container, comprising coated yarns bound together, the said coated yarns being formed of metal-coated ceramic fibres, characterized in that it comprises a step consisting in placing the coated yarns (13) side by side in a bundle (13f) consisting of a plurality of layers of coated yarns, in pulling the bundle of coated yarns through a shaping element (17) so as to compact it transversely while forming it with a determined cross section by the shaping element, and in placing straps (18) transversely clamping the bundle, downstream of the shaping element.
- Method according to the preceding claim, the shaping element (17) comprising at least two rotary rollers (17g) between which the bundle is guided.
- Method according to the preceding claim, the two rollers having parallel axes.
- Method according to the preceding claim, the shaping element comprising two lateral supports (171) between the rollers (17g).
- Method according to one of the preceding claims, the passageway cross section of the shaping element (17) being polygonal with rectilinear or curved sides.
- Method according to one of Claims 1 to 4, the passageway cross section of the shaping element being oval or circular.
- Method according to one of Claims 1 to 4, the passageway cross section of the shaping element being rectangular or square.
- Method according to one of Claims 1 to 4, the passageway cross section of the shaping element being trapezoidal.
- Method according to one of the preceding claims, a metal sheet (15, 16) being interposed between the coated yarns of the bundle and at least one portion of the sides of the shaping element.
- Method according to one of the preceding claims, wherein, before they are grouped into the bundle, the coated yarns are placed in elementary bundles that are assembled together to form the said bundle.
- Method according to one of the preceding claims, the straps (18) being placed along the insert downstream of the shaping element.
- Method for manufacturing a metal part comprising the following steps :- manufacturing an insert according to one of the preceding claims,- incorporation of said insert in a metal container, and- the hot isostatic compaction of the assembly.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
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FR1052494A FR2958299B1 (en) | 2010-04-01 | 2010-04-01 | METHOD FOR MANUFACTURING AN EXTENDED FORM INSERT IN METALLIC MATRIX COMPOSITE MATERIAL |
PCT/FR2011/050697 WO2011121232A2 (en) | 2010-04-01 | 2011-03-30 | Method of manufacturing an elongate insert made of a metal matrix composite |
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EP2552629B1 true EP2552629B1 (en) | 2018-09-05 |
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EP (1) | EP2552629B1 (en) |
JP (1) | JP6125421B2 (en) |
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CN114524220B (en) * | 2022-02-22 | 2024-01-09 | 合肥陶陶新材料科技有限公司 | Material guiding equipment for ceramic part production |
Citations (1)
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EP1950003A1 (en) * | 2007-01-23 | 2008-07-30 | Snecma | Tubular part including an insert made of a metal matrix composite material |
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2010
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2011
- 2011-03-30 CA CA2793987A patent/CA2793987C/en active Active
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- 2011-03-30 CN CN201180016581.2A patent/CN103167919B/en active Active
- 2011-03-30 WO PCT/FR2011/050697 patent/WO2011121232A2/en active Application Filing
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EP1950003A1 (en) * | 2007-01-23 | 2008-07-30 | Snecma | Tubular part including an insert made of a metal matrix composite material |
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BR112012024513A2 (en) | 2017-07-18 |
WO2011121232A2 (en) | 2011-10-06 |
JP2013527313A (en) | 2013-06-27 |
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CN103167919B (en) | 2016-06-15 |
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EP2552629A2 (en) | 2013-02-06 |
FR2958299A1 (en) | 2011-10-07 |
CA2793987C (en) | 2017-10-31 |
CN103167919A (en) | 2013-06-19 |
RU2566238C2 (en) | 2015-10-20 |
US8684255B2 (en) | 2014-04-01 |
JP6125421B2 (en) | 2017-05-10 |
CA2793987A1 (en) | 2011-10-06 |
WO2011121232A3 (en) | 2013-03-07 |
RU2012144324A (en) | 2014-05-10 |
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