EP2443265B1 - Process for the manufacture of a metallic workpiece incorporating an annular fibrous reinforcement - Google Patents

Process for the manufacture of a metallic workpiece incorporating an annular fibrous reinforcement Download PDF

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Publication number
EP2443265B1
EP2443265B1 EP10738003.2A EP10738003A EP2443265B1 EP 2443265 B1 EP2443265 B1 EP 2443265B1 EP 10738003 A EP10738003 A EP 10738003A EP 2443265 B1 EP2443265 B1 EP 2443265B1
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EP
European Patent Office
Prior art keywords
cavity
winding
blank
metal
annular
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EP10738003.2A
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German (de)
French (fr)
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EP2443265A1 (en
Inventor
Patrick Dunleavy
Jean-Michel Patrick Maurice Franchet
Gilles Charles Casimir Klein
Richard Masson
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Safran Landing Systems SAS
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Messier Bugatti Dowty SA
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C14/00Alloys based on titanium
    • 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
    • C22C47/04Pretreatment of the fibres or filaments by coating, e.g. with a protective or activated covering
    • 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
    • C22C47/06Pretreatment 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
    • C22C47/062Pretreatment 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
    • C22C47/064Winding wires
    • 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
    • Y10T29/4932Turbomachine making
    • 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
    • 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
    • Y10T29/49337Composite blade
    • 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
    • Y10T29/49481Wheel making
    • Y10T29/4949Material winding, e.g., reel, spool
    • 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

Definitions

  • the invention relates to a metal part having an annular portion including a coaxial annular fiber reinforcement, in the form of a coil of composite material enclosed in a metal matrix.
  • the invention relates more particularly to the manufacture of such a piece with improved strength. It also relates to a metal part enclosing such a coaxial annular reinforcement, see for example DE-A-10 2004 001 262 .
  • the ceramic is, for example, silicon carbide wire which has a tensile or compressive strength greater than that of a metal, such as titanium for example.
  • the document FR 2,886,290 proposes to carry out the winding directly on a part of the blank forming the winding mandrel. It is therefore an "external" winding of the most classic. More precisely, this part has two shoulders. The radially innermost shoulder forms a lateral bearing surface for the winding. The adjacent cylindrical portion forms the base surface on which the winding is made. It has a rectangular shape in right cross section. After winding, complete the blank by complementary metal parts, including an outer ring and a side cover having a pin coming into contact with the winding.
  • This assembly is then subjected to a hot isostatic pressing step during which the cover, in particular, is deformed so that the winding is compressed by the tenon.
  • the hot isostatic pressing operation is known per se; it consists in placing the aforementioned assembly in a box and subjecting this assembly, for several hours, to a high pressure of the order of 1000 bar and at a temperature of the order of 1000 ° C. After this operation, the piece, from a single block, is machined to the desired shape and dimensions. Generally, the different parts of the blank and the sheathing of the ceramic wire are of the same metal so that the finished part is provided with a wound composite insert, embedded in a homogeneous metal matrix.
  • the zone reinforced by the winding has a generally rectangular cross section. To lighten the part and increase the tensile strength / compression in the tangential direction, it is desirable that this reinforced area, surrounded by exclusively metal parts, occupies as large a volume as possible.
  • This rectangular cross-section insert arrangement may not be completely satisfactory in the direction of the forces applied to the workpiece. While the fiber strength is excellent tangential to both tensile and compressive, it is lower than that of pure metal when the forces are applied in a direction transverse to the fibers. As examples, this is particularly the case when the annular piece thus manufactured is a rotating part provided with blades, such as a turbine disk, in particular for an aircraft turbojet engine. Another piece subjected to transverse forces is the "rotating sleeve" connected to jacks in a landing gear mechanism.
  • the basic idea of the invention consists in establishing a "zone of progressivity" in pure metal in this outer radial region, laterally between the periphery and the zone where the turns are located. This leads, according to the invention, to conform the winding so that it has a right cross section of axial length decreasing radially outwardly at least in an outer radial zone of the axisymmetric part.
  • a coiled portion having a trapezoidal or triangle-shaped cross section at least in its radially outermost portion is capable of responding to the problem data.
  • a half-wave shape may also be considered provided that the proportion of pure metal increases radially outward of the room, all other things being equal.
  • the reinforcing wire is composed of a ceramic core, sheathed with metal.
  • the shape of the coil thus obtained that is to say, in fine, the shape of the zone provided with ceramic fibers makes it possible to reserve radially outwards of said zone and on either side thereof larger masses of pure metal (titanium for example) allowing a substantially radial force to transfer "progressively" in the fibers along directions turning it into effort more and more oriented tangentially.
  • the coil can be stabilized during its formation by welds joining certain turns together by their metal sheath.
  • the winding of the reinforcing wire is initiated by fixing an end thereof to the bottom of the cavity and the winding is continued by rotating the blank about its axis while feeding the wire at a controlled speed relative to the speed of rotation of the blank.
  • the feeding speed of the wire is such that it urges said blank in the direction of rotation thereof.
  • annular piece such as a rotor disc
  • metal blank 11 for example titanium
  • axisymmetric here cross section rectangular right
  • this section may have a different shape depending on the geometry of the final part that is desired.
  • the blank has a coaxial inner face 12, here cylindrical.
  • the next step is to practice, in the mass of the blank, for example by machining, a cavity 14 opening (opening) on said coaxial inner face 12. It is possible for example to rotate the blank about the axis X and introduce a cutting tool by the central portion, accessible, of said blank. Material is removed until an annular cavity opens on said coaxial inner face of the blank. Note it can be from an already hollow blank, the machining operation simply to complete the cavity to give it the desired shape and dimensions.
  • the cavity 14 has a right cross section of axial length decreasing radially outwardly over at least a portion of its height.
  • the cavity has (in a right cross-section and in a radial direction from the inside to the outside) a rectangular shape 15 extended by a trapezoidal shape 16.
  • This second part of the cavity could have a triangular shape or any other shape whose axial length (along the X axis) decreases from the inside to the outside.
  • the following operation is to wind in situ a reinforcing wire 21, here ceramic (silicon carbide) coated with metal.
  • the metal is here titanium, that is to say the same metal as that which constitutes the blank.
  • This operation illustrated in figure 3A , is carried out by introducing the wire through the opening of the cavity and depositing it from the cylindrical bottom 23 of the cavity by adjacent turns and then by successive layers of turns until the entire space of the cavity is completely filled, by a coil of contiguous turns 25.
  • the wire is fed via a rigid tubular guide 27 movable in a controlled manner parallel to the X axis (to form a layer) and radially recessed (to develop the following successive layers).
  • the guide 27 is oriented as shown on the Figures 3A and 3B that is, its end 27A is at a small angle to the circumferential winding direction of the turns.
  • the winding of the wire 21 is started by fixing (by welding) one end thereof to the cylindrical bottom wall 23 of the cavity, near one end thereof, and the blank 11 is rotated around its end.
  • X axis and feeding the wire at a controlled speed relative to the speed of rotation of the blank. For example, it is possible to continuously adjust the speed at which the wire 21 is brought so that this speed is always substantially equal to the winding speed. taking into account the speed of rotation of the blank and the diameter of the layer of turns during winding.
  • the feed speed of the wire is such that it solicits the roughing in the direction of rotation of the latter.
  • the wire 21 may be pushed inside the guide 27 by a drive rotary roller drive system (not shown) with possibility of longitudinal sliding so that said wire is in slight compression between its output of the guide 27 and the point where it takes its place in the winding.
  • the blank 11 is mounted in free rotation and that it is the stress exerted on the wire itself which drives it in rotation during the winding.
  • the turns are stabilized at given winding intervals, by welding points or lines joining the metal sheaths of certain turns.
  • the weld can be an electrical or induction weld, under vacuum or in a neutral atmosphere of argon.
  • a welding process as described in FR 2,886,290 can be implemented.
  • figure 4 consists, for example, in closing a cavity 14 filled with the coil 25.
  • a cylindrical metal annular wall 30, here made of titanium is placed in register with the opening of the cavity.
  • This wall here has the same length as the axial length of the opening so that during hot isostatic compression, it can deform radially outwardly penetrate the cavity, compacting the winding itself.
  • the cylindrical annular wall 30 can be dimensioned so that its diameter is slightly greater than that of the central opening of the blank but while carrying this annular wall at a low temperature (by dipping it in liquid nitrogen, for example ) before putting it in place.
  • the annular wall 30 engages the cavity by starting to compact the coil.
  • the closure of said cavity comprises its evacuation with hermetic closure by a welded metal sheet 32.
  • This metal sheet is welded on both sides of the opening of the cavity, before the hot isostatic pressing operation.
  • the hot isostatic pressing operation proper consisting of, for example, placing the blank, modified as shown, is then carried out. figure 4 , in a box for several hours, bringing the pressure to 1000 bar and the temperature to 1000 ° C, approximately.
  • FIG. 5 The result is represented figure 5 . It can be seen that the annular wall 30 is engaged in the cavity, driving the metal foil 32.
  • the assembly forms only a single block with a large part of the volume occupied by a coil of high-strength ceramic wire, embedded in a metal matrix resulting from the melting of the metal sheath of the wire used during winding.
  • the final piece 36 of the figure 7 comprises purely metallic external lateral zones (17a, 18a), making it possible to increase the transverse mechanical strength of the part and locally to limit the breaks of stiffness favoring breaks.
  • These so-called "progressivity" zones have the effect of bringing the efforts gradually, by shearing, into the fibrous reinforcement (the winding) in order to convert the tensile forces / circumferential compression for which the resistance of the wound zone is optimal.

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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)

Description

L'invention se rapporte à une pièce métallique présentant une partie annulaire englobant un renfort annulaire coaxial fibreux, sous forme d'une bobine en matériau composite englobée dans une matrice métallique. L'invention concerne plus particulièrement la fabrication d'une telle pièce bénéficiant d'une résistance améliorée. Elle concerne également une pièce métallique renfermant un tel renfort annulaire coaxial, voir par exemple DE-A-10 2004 001 262 .The invention relates to a metal part having an annular portion including a coaxial annular fiber reinforcement, in the form of a coil of composite material enclosed in a metal matrix. The invention relates more particularly to the manufacture of such a piece with improved strength. It also relates to a metal part enclosing such a coaxial annular reinforcement, see for example DE-A-10 2004 001 262 .

Il est connu de réduire la masse d'une pièce métallique annulaire tout en lui assurant une résistance très importante en traction ou compression tangentielle, en incorporant des fibres de matériau composite comme par exemple en céramique dans la masse métallique. La céramique est par exemple du carbure de silicium en fil qui présente une résistance à la traction ou à la compression supérieure à celle d'un métal, comme le titane par exemple.It is known to reduce the mass of an annular metal part while providing a very high resistance in tangential tension or compression, by incorporating fibers of composite material such as ceramic in the metal mass. The ceramic is, for example, silicon carbide wire which has a tensile or compressive strength greater than that of a metal, such as titanium for example.

Pour obtenir une telle pièce, on peut réaliser un bobinage de fil de céramique enduit de métal à l'intérieur d'une ébauche de la pièce. Par exemple, le document FR 2 886 290 propose de réaliser le bobinage directement sur une partie de l'ébauche formant mandrin de bobinage. Il s'agit donc d'un bobinage "externe" des plus classiques. Plus précisément, cette partie comporte deux épaulements. L'épaulement le plus interne radialement forme une surface d'appui latérale pour le bobinage. La partie cylindrique adjacente forme la surface de base sur laquelle on réalise le bobinage. Celui-ci a une forme rectangulaire en section transversale droite. Après bobinage, on complète l'ébauche par des parties métalliques complémentaires, notamment un anneau extérieur et un couvercle latéral présentant un tenon venant au contact du bobinage. Cet ensemble est ensuite soumis à une étape de compression isostatique à chaud au cours de laquelle le couvercle, notamment, est déformé en sorte que le bobinage soit comprimé par le tenon. L'opération de compression isostatique à chaud est connue en soi ; elle consiste à placer l'ensemble précité dans un caisson et à soumettre cet ensemble, pendant plusieurs heures, à une pression élevée de l'ordre de 1 000 bars et à une température de l'ordre de 1 000°C. Après cette opération, la pièce, d'un seul bloc, est usinée à la forme et aux dimensions souhaitées. Généralement, les différentes parties de l'ébauche et le gainage du fil de céramique sont du même métal en sorte que la pièce finie se trouve pourvue d'un insert composite bobiné, noyé dans une matrice métallique homogène.To obtain such a part, it is possible to produce a winding of metal-coated ceramic wire inside a blank of the part. For example, the document FR 2,886,290 proposes to carry out the winding directly on a part of the blank forming the winding mandrel. It is therefore an "external" winding of the most classic. More precisely, this part has two shoulders. The radially innermost shoulder forms a lateral bearing surface for the winding. The adjacent cylindrical portion forms the base surface on which the winding is made. It has a rectangular shape in right cross section. After winding, complete the blank by complementary metal parts, including an outer ring and a side cover having a pin coming into contact with the winding. This assembly is then subjected to a hot isostatic pressing step during which the cover, in particular, is deformed so that the winding is compressed by the tenon. The hot isostatic pressing operation is known per se; it consists in placing the aforementioned assembly in a box and subjecting this assembly, for several hours, to a high pressure of the order of 1000 bar and at a temperature of the order of 1000 ° C. After this operation, the piece, from a single block, is machined to the desired shape and dimensions. Generally, the different parts of the blank and the sheathing of the ceramic wire are of the same metal so that the finished part is provided with a wound composite insert, embedded in a homogeneous metal matrix.

La zone renforcée par le bobinage a une section transversale droite globalement rectangulaire. Pour alléger la pièce et augmenter la résistance à la traction/compression dans le sens tangentiel, il est souhaitable que cette zone renforcée, entourée de parties exclusivement métalliques, occupe un volume aussi important que possible.The zone reinforced by the winding has a generally rectangular cross section. To lighten the part and increase the tensile strength / compression in the tangential direction, it is desirable that this reinforced area, surrounded by exclusively metal parts, occupies as large a volume as possible.

Cet agencement à insert de section droite rectangulaire peut ne pas être complètement satisfaisant suivant la direction des efforts qui sont appliqués à la pièce. Alors que la résistance des fibres est excellente tangentiellement tant à la traction qu'à la compression, elle est inférieure à celle du métal pur lorsque les efforts sont appliqués dans un sens transverse aux fibres. A titre d'exemples, c'est particulièrement le cas lorsque la pièce annulaire ainsi fabriquée est une pièce tournante munie d'aubes, comme un disque de turbine, notamment pour un turboréacteur d'avion. Une autre pièce soumise à des efforts transversaux est le "manchon tournant" relié à des vérins dans un mécanisme d'atterrisseur.This rectangular cross-section insert arrangement may not be completely satisfactory in the direction of the forces applied to the workpiece. While the fiber strength is excellent tangential to both tensile and compressive, it is lower than that of pure metal when the forces are applied in a direction transverse to the fibers. As examples, this is particularly the case when the annular piece thus manufactured is a rotating part provided with blades, such as a turbine disk, in particular for an aircraft turbojet engine. Another piece subjected to transverse forces is the "rotating sleeve" connected to jacks in a landing gear mechanism.

Avec une pièce munie d'un bobinage à section transversale droite rectangulaire, des ruptures sont possibles dans la partie extérieure de la zone renforcée.With a part provided with a winding with rectangular straight cross-section, breaks are possible in the outside part of the reinforced zone.

L'idée de base de l'invention consiste à établir une "zone de progressivité" en métal pur dans cette région radiale externe, latéralement entre la périphérie et la zone où se trouvent les spires. Ceci conduit, selon l'invention, à conformer le bobinage de façon que celui-ci présente une section transversale droite de longueur axiale décroissant radialement vers l'extérieur au moins dans une zone radiale extérieure de la pièce axisymétrique.The basic idea of the invention consists in establishing a "zone of progressivity" in pure metal in this outer radial region, laterally between the periphery and the zone where the turns are located. This leads, according to the invention, to conform the winding so that it has a right cross section of axial length decreasing radially outwardly at least in an outer radial zone of the axisymmetric part.

Par exemple, une partie bobinée ayant une section transversale en forme de trapèze ou de triangle au moins dans sa partie radialement la plus extérieure est susceptible de répondre aux données du problème. Une forme en demi-onde peut aussi être envisagée pourvu que la proportion de métal pur augmente radialement vers l'extérieur de la pièce, toutes choses égales par ailleurs.For example, a coiled portion having a trapezoidal or triangle-shaped cross section at least in its radially outermost portion is capable of responding to the problem data. A half-wave shape may also be considered provided that the proportion of pure metal increases radially outward of the room, all other things being equal.

Une autre difficulté est alors de réaliser la pièce car le bobinage "externe" tel que décrit ci-dessus est difficile à envisager. L'invention propose aussi une nouvelle approche du bobinage, dit "bobinage interne".Another difficulty is then to make the part because the "external" winding as described above is difficult to envisage. The invention also proposes a new approach to winding, called "internal winding".

Plus précisément, l'invention concerne un procédé de fabrication d'une pièce métallique annulaire axisymétrique renforcée par inclusion dans celle-ci d'un renfort annulaire coaxial sous forme de bobine en matériau composite, caractérisé en ce qu'il comprend les étapes consistant à :

  • élaborer une ébauche métallique annulaire de ladite pièce,
  • pratiquer ou achever une cavité ouvrant sur une face intérieure coaxiale de ladite ébauche et présentant une section transversale droite de longueur axiale décroissant radialement vers l'extérieur sur au moins une partie de sa hauteur,
  • enrouler un fil de renfort dans ladite cavité de façon à remplir sensiblement tout l'espace de celle-ci par une bobine,
  • fermer ladite cavité enmettant en place un élément de paroi métallique en regard de l'ouverture de ladite cavité, puis,
  • soumettre l'ensemble à un processus de compression isostatique à chaud, et
  • usiner ladite ébauche pour obtenir la géométrie finale de ladite pièce.
More specifically, the invention relates to a method for manufacturing an annular axisymmetric metal piece reinforced by inclusion therein of a coaxial annular reinforcement in the form of a composite material coil, characterized in that it comprises the steps of :
  • developing an annular metal blank of said part,
  • practicing or completing a cavity opening on a coaxial inner face of said blank and having a right cross section of axial length decreasing radially outwardly over at least a portion of its height,
  • winding a reinforcing wire into said cavity so as to fill substantially all the space thereof with a coil,
  • closing said cavity by putting in place a metal wall element facing the opening of said cavity, then,
  • subject the assembly to a process of hot isostatic compression, and
  • machining said blank to obtain the final geometry of said part.

On entend par "section transversale droite", une section dans un plan contenant l'axe de la pièce axisymétrique considérée, plus précisément l'axe de l'ébauche dans la définition qui précède.The term "right cross section", a section in a plane containing the axis of the axisymmetrical part considered, more precisely the axis of the blank in the above definition.

Selon une caractéristique avantageuse, le fil de renfort est composé d'une âme en céramique, gainée de métal.According to an advantageous characteristic, the reinforcing wire is composed of a ceramic core, sheathed with metal.

La forme du bobinage ainsi obtenu, c'est-à-dire, in fine, la forme de la zone munie de fibres de céramique permet de réserver radialement vers l'extérieur de ladite zone et de part et d'autre de celle-ci des masses plus importantes de métal pur (titane par exemple) permettant à un effort essentiellement radial de se transférer "progressivement" dans les fibres suivant des directions le transformant en effort de plus en plus orienté tangentiellement.The shape of the coil thus obtained, that is to say, in fine, the shape of the zone provided with ceramic fibers makes it possible to reserve radially outwards of said zone and on either side thereof larger masses of pure metal (titanium for example) allowing a substantially radial force to transfer "progressively" in the fibers along directions turning it into effort more and more oriented tangentially.

On peut stabiliser la bobine au cours de sa formation par des soudures réunissant certaines spires entre elles par leur gaine de métal.The coil can be stabilized during its formation by welds joining certain turns together by their metal sheath.

Pour procéder au bobinage dit "interne" on amorce le bobinage du fil de renfort en fixant une extrémité de celui-ci au fond de la cavité et on poursuit le bobinage en faisant tourner l'ébauche autour de son axe tout en alimentant le fil à une vitesse contrôlée par rapport à la vitesse de rotation de l'ébauche.To proceed with the so-called "internal" winding, the winding of the reinforcing wire is initiated by fixing an end thereof to the bottom of the cavity and the winding is continued by rotating the blank about its axis while feeding the wire at a controlled speed relative to the speed of rotation of the blank.

Avantageusement, la vitesse d'alimentation du fil est telle qu'il sollicite ladite ébauche dans le sens de rotation de celle-ci.Advantageously, the feeding speed of the wire is such that it urges said blank in the direction of rotation thereof.

L'invention sera mieux comprise et d'autres avantages de celle-ci apparaîtront plus clairement à la lumière de la description qui va suivre illustrant un procédé de fabrication d'une pièce métallique annulaire axisymétrique renforcée par un bobinage coaxial, donnée uniquement à titre d'exemples et faite en référence aux dessins annexés, dans lesquels :

  • les figures 1, 2, 3A et 4 à 6 illustrent par des vues en coupe transversale droite les différentes étapes du procédé de fabrication d'une pièce métallique annulaire axisymétrique renforcée par bobinage d'un fil de renfort ;
  • la figure 3B est une vue partielle en perspective illustrant la phase de la figure 3A ; et
  • la figure 7 représente la pièce ainsi obtenue.
The invention will be better understood and other advantages thereof will appear more clearly in the light of the following description illustrating a method of manufacturing an axisymmetric annular metal part reinforced by a coaxial winding, given only as a examples and with reference to the accompanying drawings, in which:
  • the Figures 1, 2, 3A and 4 to 6 illustrate by cross-sectional views right the different steps of the method of manufacturing an axisymmetric annular metal part reinforced by winding a reinforcing wire;
  • the figure 3B is a partial perspective view illustrating the phase of the figure 3A ; and
  • the figure 7 represents the piece thus obtained.

En se reportant aux dessins, on va décrire un procédé permettant de réaliser une pièce annulaire telle qu'un disque de rotor, à partir d'une ébauche métallique 11, par exemple en titane, elle-même annulaire et axisymétrique, ici à section transversale droite rectangulaire, comme représenté sur la figure 1. L'axe de révolution de l'ébauche est référencé X.Referring to the drawings, there will be described a method for producing an annular piece such as a rotor disc, from a metal blank 11, for example titanium, itself annular and axisymmetric, here cross section rectangular right, as shown on the figure 1 . The axis of revolution of the blank is referenced X.

Bien entendu, cette section peut avoir une forme différente en fonction de la géométrie de la pièce finale que l'on désire obtenir.Of course, this section may have a different shape depending on the geometry of the final part that is desired.

L'ébauche comporte une face intérieure coaxiale 12, ici cylindrique.The blank has a coaxial inner face 12, here cylindrical.

Il s'agit à la fois d'alléger ladite pièce finale tout en lui conférant une résistance mécanique accrue.This is both to lighten said final piece while giving it increased mechanical strength.

Après l'élaboration d'une telle ébauche, l'étape suivante (figure 2) consiste à pratiquer, dans la masse de l'ébauche, par exemple par usinage, une cavité 14 ouvrant (débouchant) sur ladite face intérieure coaxiale 12. On peut par exemple faire tourner l'ébauche autour de l'axe X et introduire un outil de coupe par la partie centrale, accessible, de ladite ébauche. On enlève de la matière jusqu'à obtenir une cavité annulaire ouvrant sur ladite face intérieure coaxiale de l'ébauche. Il est à noter qu'on peut partir d'une ébauche déjà creuse, l'opération d'usinage consistant simplement à achever la cavité pour lui donner la forme et les dimensions voulues.After the development of such a draft, the next step ( figure 2 ) is to practice, in the mass of the blank, for example by machining, a cavity 14 opening (opening) on said coaxial inner face 12. It is possible for example to rotate the blank about the axis X and introduce a cutting tool by the central portion, accessible, of said blank. Material is removed until an annular cavity opens on said coaxial inner face of the blank. Note it can be from an already hollow blank, the machining operation simply to complete the cavity to give it the desired shape and dimensions.

Selon une caractéristique importante, la cavité 14 présente une section transversale droite de longueur axiale décroissant radialement vers l'extérieur sur au moins une partie de sa hauteur. Dans l'exemple, la cavité a (selon une section transversale droite et suivant une direction radiale de l'intérieur vers l'extérieur) une forme rectangulaire 15 prolongée par une forme trapézoïdale 16. Cette seconde partie de la cavité pourrait avoir une forme triangulaire ou toute autre forme dont la longueur axiale (selon l'axe X) décroît de l'intérieur vers l'extérieur.According to an important characteristic, the cavity 14 has a right cross section of axial length decreasing radially outwardly over at least a portion of its height. In the example, the cavity has (in a right cross-section and in a radial direction from the inside to the outside) a rectangular shape 15 extended by a trapezoidal shape 16. This second part of the cavity could have a triangular shape or any other shape whose axial length (along the X axis) decreases from the inside to the outside.

Il en résulte une réserve de métal pur dans les zones latérales 17, 18 indiquées en pointillé, par rapport à ce qui serait obtenu si la cavité avait une section transversale droite rectangulaire.This results in a reserve of pure metal in the lateral zones 17, 18 indicated in dotted lines, compared to what would be obtained if the cavity had a rectangular cross section.

L'opération suivante consiste à enrouler in situ un fil de renfort 21, ici en céramique (carbure de silicium) enrobé de métal. Le métal est ici du titane, c'est-à-dire le même métal que celui qui constitue l'ébauche. Cette opération, illustrée à la figure 3A, s'effectue en introduisant le fil par l'ouverture de la cavité et en le déposant à partir du fond cylindrique 23 de la cavité par spires adjacentes puis par couches successives de spires jusqu'à remplir entièrement tout l'espace de la cavité, par une bobine de spires jointives 25.The following operation is to wind in situ a reinforcing wire 21, here ceramic (silicon carbide) coated with metal. The metal is here titanium, that is to say the same metal as that which constitutes the blank. This operation, illustrated in figure 3A , is carried out by introducing the wire through the opening of the cavity and depositing it from the cylindrical bottom 23 of the cavity by adjacent turns and then by successive layers of turns until the entire space of the cavity is completely filled, by a coil of contiguous turns 25.

Pour le bobinage, on peut procéder ainsi. On alimente le fil via un guide tubulaire rigide 27 déplaçable de façon contrôlée parallèlement à l'axe X (pour former une couche) et radialement en retrait (pour élaborer les couches successives suivantes). Le guide 27 est orienté comme représenté sur les figures 3A et 3B, c'est-à-dire que son extrémité 27A fait un angle faible par rapport à la direction circonférentielle d'enroulement des spires.For winding, this can be done. The wire is fed via a rigid tubular guide 27 movable in a controlled manner parallel to the X axis (to form a layer) and radially recessed (to develop the following successive layers). The guide 27 is oriented as shown on the Figures 3A and 3B that is, its end 27A is at a small angle to the circumferential winding direction of the turns.

On amorce le bobinage du fil 21 en fixant (par soudure) une extrémité de celui-ci à la paroi de fond cylindrique 23 de la cavité, près d'une extrémité de celle-ci et on fait tourner l'ébauche 11 autour de son axe X, et en alimentant le fil à une vitesse contrôlée par rapport à la vitesse de rotation de l'ébauche. On peut par exemple ajuster en permanence la vitesse à laquelle le fil 21 est amené, pour que cette vitesse soit toujours sensiblement égale à la vitesse d'enroulement, compte tenu de la vitesse de rotation de l'ébauche et du diamètre de la couche de spires en cours de bobinage.The winding of the wire 21 is started by fixing (by welding) one end thereof to the cylindrical bottom wall 23 of the cavity, near one end thereof, and the blank 11 is rotated around its end. X axis, and feeding the wire at a controlled speed relative to the speed of rotation of the blank. For example, it is possible to continuously adjust the speed at which the wire 21 is brought so that this speed is always substantially equal to the winding speed. taking into account the speed of rotation of the blank and the diameter of the layer of turns during winding.

On pourra aussi faire en sorte que la vitesse d'alimentation du fil soit telle qu'il sollicite l'ébauche dans le sens de rotation de celle-ci. Par exemple, le fil 21 pourra être poussé à l'intérieur du guide 27 par un système d'entraînement à galets rotatifs moteurs (non représenté) avec possibilité de glissement longitudinal en sorte que ledit fil soit en légère compression entre sa sortie du guide 27 et le point où il prend sa place dans le bobinage. On peut même envisager que l'ébauche 11 soit montée en rotation libre et que ce soit la sollicitation exercée sur le fil lui-même qui l'entraîne en rotation pendant le bobinage.It will also be possible to ensure that the feed speed of the wire is such that it solicits the roughing in the direction of rotation of the latter. For example, the wire 21 may be pushed inside the guide 27 by a drive rotary roller drive system (not shown) with possibility of longitudinal sliding so that said wire is in slight compression between its output of the guide 27 and the point where it takes its place in the winding. It can even be envisaged that the blank 11 is mounted in free rotation and that it is the stress exerted on the wire itself which drives it in rotation during the winding.

Pour éviter le foisonnement, les spires sont stabilisées à intervalles de bobinage donnés, par des points ou lignes de soudure joignant les gaines métalliques de certaines spires.To avoid expansion, the turns are stabilized at given winding intervals, by welding points or lines joining the metal sheaths of certain turns.

De façon connue en soi, la soudure peut être une soudure électrique ou par induction, sous vide ou sous atmosphère neutre d'argon. Un processus de soudure tel que décrit dans FR 2 886 290 peut être mis en oeuvre.In a manner known per se, the weld can be an electrical or induction weld, under vacuum or in a neutral atmosphere of argon. A welding process as described in FR 2,886,290 can be implemented.

L'opération suivante, figure 4, consiste à refermer la cavité 14 remplie par la bobine 25. Par exemple, on met en place une paroi annulaire cylindrique métallique 30, ici en titane, en regard de l'ouverture de la cavité. Cette paroi a ici la même longueur que la longueur axiale de l'ouverture en sorte que pendant la compression isostatique à chaud, elle pourra en se déformant radialement vers l'extérieur pénétrer dans la cavité, en compactant le bobinage lui-même. On peut dimensionner la paroi annulaire cylindrique 30 en faisant en sorte que son diamètre soit légèrement supérieur à celui de l'ouverture centrale de l'ébauche mais en portant cette paroi annulaire à basse température (en la plongeant dans de l'azote liquide par exemple) avant de la mettre en place. Ainsi, même avant le début de l'opération de compression isostatique à chaud, la paroi annulaire 30 s'engage dans la cavité en commençant à compacter le bobinage.The following operation, figure 4 consists, for example, in closing a cavity 14 filled with the coil 25. For example, a cylindrical metal annular wall 30, here made of titanium, is placed in register with the opening of the cavity. This wall here has the same length as the axial length of the opening so that during hot isostatic compression, it can deform radially outwardly penetrate the cavity, compacting the winding itself. The cylindrical annular wall 30 can be dimensioned so that its diameter is slightly greater than that of the central opening of the blank but while carrying this annular wall at a low temperature (by dipping it in liquid nitrogen, for example ) before putting it in place. Thus, even before the start of the hot isostatic pressing operation, the annular wall 30 engages the cavity by starting to compact the coil.

Avantageusement, la fermeture de ladite cavité comprend sa mise sous vide avec fermeture hermétique par une feuille métallique 32 soudée. Cette feuille métallique est soudée de part et d'autre de l'ouverture de la cavité, avant l'opération de compression isostatique à chaud.Advantageously, the closure of said cavity comprises its evacuation with hermetic closure by a welded metal sheet 32. This metal sheet is welded on both sides of the opening of the cavity, before the hot isostatic pressing operation.

On procède ensuite à l'opération de compression isostatique à chaud proprement dite, consistant, par exemple, à placer l'ébauche, modifiée comme représente figure 4, dans un caisson pendant plusieurs heures en portant la pression à 1 000 bars et la température à 1 000°C, environ.The hot isostatic pressing operation proper, consisting of, for example, placing the blank, modified as shown, is then carried out. figure 4 , in a box for several hours, bringing the pressure to 1000 bar and the temperature to 1000 ° C, approximately.

Le résultat est représenté figure 5. On voit que la paroi annulaire 30 s'est engagée dans la cavité, entraînant la feuille métallique 32. L'ensemble ne forme plus qu'un seul bloc avec une grande partie du volume occupé par un bobinage de fil en céramique à haute résistance, noyé dans une matrice métallique résultant de la fusion de la gaine métallique du fil utilisé pendant le bobinage.The result is represented figure 5 . It can be seen that the annular wall 30 is engaged in the cavity, driving the metal foil 32. The assembly forms only a single block with a large part of the volume occupied by a coil of high-strength ceramic wire, embedded in a metal matrix resulting from the melting of the metal sheath of the wire used during winding.

On procède ensuite à une succession d'usinages (figure 6) ayant pour but, à partir de l'ébauche transformée par l'opération de compression isostatique à chaud de définir le contour 35 de la pièce voulue (représenté en pointillé sur la figure 6). La pièce finale 36 de la figure 7 comporte des zones latérales externes (17a, 18a) purement métalliques, permettant d'augmenter la résistance mécanique transversale de la pièce et de limiter localement les sauts de raideur favorisant les ruptures. Ces zones dites "de progressivité" ont pour effet de faire rentrer les efforts progressivement, par cisaillement, dans le renfort fibreux (le bobinage) afin de convertir les efforts en traction/ compression circonférentielle pour lesquels la résistance de la zone bobinée est optimale.We then proceed to a series of machining operations ( figure 6 ) intended, from the blank transformed by the hot isostatic pressing operation, to define the contour of the desired part (shown in dashed line on the figure 6 ). The final piece 36 of the figure 7 comprises purely metallic external lateral zones (17a, 18a), making it possible to increase the transverse mechanical strength of the part and locally to limit the breaks of stiffness favoring breaks. These so-called "progressivity" zones have the effect of bringing the efforts gradually, by shearing, into the fibrous reinforcement (the winding) in order to convert the tensile forces / circumferential compression for which the resistance of the wound zone is optimal.

Claims (6)

  1. A method of fabricating an axisymmetric annular metal part reinforced by including coaxial annular reinforcement therein in the form of a winding of composite material, the method comprising the steps consisting in:
    preparing an annular metal blank (11) for said part;
    making or finishing off a cavity (14) that opens out into a coaxial inside face of said blank and that possesses a right cross-section of axial extent that decreases going radially outwards over at least a portion of its height; and
    • winding a reinforcing yarn (21) in said cavity so as to fill substantially all of the space therein with a winding,
    the method being characterized in that it further comprises the steps consisting in:
    • closing said cavity by putting into place a metal cylindrical wall (30) in register with the opening of said cavity; then
    • subjecting the assembly to a hot isostatic compression process; and
    • machining said blank to obtain the final shape of said part.
  2. A method according to claim 1, characterized in that said reinforcing yarn (21) is made up of a core of composite material such as ceramic, sheathed in metal, and in that the winding that is being formed is stabilized by welds bonding together certain turns via their metal sheaths.
  3. A method according to claim 1 or 2, characterized in that the winding of the reinforcing yarn is started by fixing one end thereof to the bottom (23) of the cavity, and in that winding is continued by causing said blank to turn about its axis (X) while feeding the yarn at a speed that is controlled relative to the speed of rotation of the blank.
  4. A method according to claim 3, characterized in that the yarn (21) is fed at a speed that is such that it applies a force on said blank in its direction of rotation.
  5. A method according to any one of the preceding claims, characterized in that said open cavity is shaped in such a manner as to give it a cross-section that is triangular or trapezoidal (16) at least in part, at least in the radially outermost portion thereof.
  6. A method according to any one of the preceding claims, characterized in that closing said cavity includes evacuating it and hermetically closing it with a metal foil (32) that is welded on either side of the opening in said cavity, prior to performing the hot isostatic compression operation, said metal foil covering radially inwards said metal cylindrical wall (30) and being taken with it during the hot isostatic compression process.
EP10738003.2A 2009-06-16 2010-06-14 Process for the manufacture of a metallic workpiece incorporating an annular fibrous reinforcement Active EP2443265B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0954029A FR2946550A1 (en) 2009-06-16 2009-06-16 PROCESS FOR MANUFACTURING A METAL PIECE INCORPORATING A FIBROUS ANNULAR REINFORCEMENT.
PCT/FR2010/051179 WO2010146293A1 (en) 2009-06-16 2010-06-14 Method for making a metal part including a fibrous annular reinforcement

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EP2443265A1 EP2443265A1 (en) 2012-04-25
EP2443265B1 true EP2443265B1 (en) 2013-04-17

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EP (1) EP2443265B1 (en)
JP (1) JP2012530190A (en)
CN (1) CN102459681B (en)
BR (1) BRPI1015560A2 (en)
CA (1) CA2764774C (en)
FR (1) FR2946550A1 (en)
RU (1) RU2012101466A (en)
WO (1) WO2010146293A1 (en)

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FR2950078B1 (en) * 2009-09-11 2012-10-05 Messier Dowty Sa METAL PIECE PROVIDED WITH FIBROUS REINFORCEMENTS WITH BITEAUTEE END.

Family Cites Families (12)

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Publication number Priority date Publication date Assignee Title
US3828417A (en) * 1970-08-26 1974-08-13 Commw Scient Corp Method for fabricating composite material reinforced by uniformaly spaced filaments
US4867644A (en) * 1987-05-15 1989-09-19 Allied-Signal Inc. Composite member, unitary rotor member including same, and method of making
JP2003138352A (en) 2001-10-29 2003-05-14 Mitsubishi Heavy Ind Ltd Method for forming metal matrix composite
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
DE102004001262B4 (en) * 2004-01-08 2007-03-01 Mtu Aero Engines Gmbh Method and device for depositing fibers in recesses, in particular in the manufacture of MMC components
US7118063B2 (en) 2004-07-29 2006-10-10 Sequa Corporation Wire/fiber ring and method for manufacturing the same
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
FR2919283B1 (en) 2007-07-26 2010-09-17 Snecma MECHANICAL PIECE COMPRISING AN INSERT IN COMPOSITE MATERIAL.
FR2933422B1 (en) 2008-07-04 2011-05-13 Messier Dowty Sa METHOD FOR MANUFACTURING A METAL PIECE COMPRISING INTERNAL REINFORCEMENTS FORMED OF CERAMIC FIBERS
FR2933423B1 (en) 2008-07-04 2010-09-17 Messier Dowty Sa PROCESS FOR MANUFACTURING A CERAMIC FIBER REINFORCED METAL PIECE

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RU2012101466A (en) 2013-07-27
JP2012530190A (en) 2012-11-29
CA2764774A1 (en) 2010-12-23
BRPI1015560A2 (en) 2016-04-26
CN102459681A (en) 2012-05-16
CA2764774C (en) 2018-02-20
FR2946550A1 (en) 2010-12-17
WO2010146293A1 (en) 2010-12-23
US20120124838A1 (en) 2012-05-24
EP2443265A1 (en) 2012-04-25
CN102459681B (en) 2015-07-01

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