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 PDFInfo
- 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
- Authority
- EP
- European Patent Office
- Prior art keywords
- cavity
- winding
- blank
- metal
- annular
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 238000000034 method Methods 0.000 title claims description 11
- 238000004519 manufacturing process Methods 0.000 title claims description 8
- 230000002787 reinforcement Effects 0.000 title claims description 6
- 229910052751 metal Inorganic materials 0.000 claims description 42
- 239000002184 metal Substances 0.000 claims description 42
- 238000004804 winding Methods 0.000 claims description 38
- 238000007906 compression Methods 0.000 claims description 10
- 239000000919 ceramic Substances 0.000 claims description 9
- 230000006835 compression Effects 0.000 claims description 8
- 230000003014 reinforcing effect Effects 0.000 claims description 8
- 239000002131 composite material Substances 0.000 claims description 6
- 238000003754 machining Methods 0.000 claims description 5
- 239000011888 foil Substances 0.000 claims description 3
- 230000007423 decrease Effects 0.000 claims description 2
- 239000000835 fiber Substances 0.000 description 6
- 238000001513 hot isostatic pressing Methods 0.000 description 6
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 5
- 230000004323 axial length Effects 0.000 description 5
- 239000010936 titanium Substances 0.000 description 5
- 229910052719 titanium Inorganic materials 0.000 description 5
- 230000003247 decreasing effect Effects 0.000 description 3
- 239000011159 matrix material Substances 0.000 description 3
- 238000003466 welding Methods 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- 238000005304 joining Methods 0.000 description 2
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 2
- 229910010271 silicon carbide Inorganic materials 0.000 description 2
- 241000135309 Processus Species 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000000295 complement effect Effects 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 238000000151 deposition Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 238000007598 dipping method Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000011065 in-situ storage Methods 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 230000007935 neutral effect Effects 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 238000010008 shearing Methods 0.000 description 1
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C14/00—Alloys based on titanium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C47/00—Making alloys containing metallic or non-metallic fibres or filaments
- C22C47/02—Pretreatment of the fibres or filaments
- C22C47/04—Pretreatment of the fibres or filaments by coating, e.g. with a protective or activated covering
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C47/00—Making alloys containing metallic or non-metallic fibres or filaments
- C22C47/02—Pretreatment of the fibres or filaments
- C22C47/06—Pretreatment of the fibres or filaments by forming the fibres or filaments into a preformed structure, e.g. using a temporary binder to form a mat-like element
- C22C47/062—Pretreatment of the fibres or filaments by forming the fibres or filaments into a preformed structure, e.g. using a temporary binder to form a mat-like element from wires or filaments only
- C22C47/064—Winding wires
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/4932—Turbomachine making
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/49336—Blade making
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/49336—Blade making
- Y10T29/49337—Composite blade
-
- 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
- Y10T29/49481—Wheel making
- Y10T29/4949—Material winding, e.g., reel, spool
-
- 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
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.
Landscapes
- 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
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
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.
- 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 et4 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 lafigure 3A ; et - la
figure 7 représente la pièce ainsi obtenue.
- the
Figures 1, 2, 3A and4 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 thefigure 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
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
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 (
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
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
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
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
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
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
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
L'opération suivante,
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
On procède ensuite à l'opération de compression isostatique à chaud proprement dite, consistant, par exemple, à placer l'ébauche, modifiée comme représente
Le résultat est représenté
On procède ensuite à une succession d'usinages (
Claims (6)
- 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.
- 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.
- 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.
- 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.
- 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.
- 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.
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 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2443265A1 EP2443265A1 (en) | 2012-04-25 |
EP2443265B1 true EP2443265B1 (en) | 2013-04-17 |
Family
ID=41647242
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP10738003.2A Active EP2443265B1 (en) | 2009-06-16 | 2010-06-14 | Process for the manufacture of a metallic workpiece incorporating an annular fibrous reinforcement |
Country Status (9)
Country | Link |
---|---|
US (1) | US8869397B2 (en) |
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) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2950078B1 (en) * | 2009-09-11 | 2012-10-05 | Messier Dowty Sa | METAL PIECE PROVIDED WITH FIBROUS REINFORCEMENTS WITH BITEAUTEE END. |
Family Cites Families (12)
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 |
-
2009
- 2009-06-16 FR FR0954029A patent/FR2946550A1/en not_active Withdrawn
-
2010
- 2010-06-14 US US13/378,815 patent/US8869397B2/en active Active
- 2010-06-14 EP EP10738003.2A patent/EP2443265B1/en active Active
- 2010-06-14 BR BRPI1015560A patent/BRPI1015560A2/en not_active IP Right Cessation
- 2010-06-14 JP JP2012515544A patent/JP2012530190A/en active Pending
- 2010-06-14 WO PCT/FR2010/051179 patent/WO2010146293A1/en active Application Filing
- 2010-06-14 CA CA2764774A patent/CA2764774C/en active Active
- 2010-06-14 CN CN201080027205.9A patent/CN102459681B/en active Active
- 2010-06-14 RU RU2012101466/02A patent/RU2012101466A/en not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
US8869397B2 (en) | 2014-10-28 |
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 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP2245204B1 (en) | Method for making parts with an insert made of a metal-matrix composite material | |
EP1726679B1 (en) | Method and device for producing a ceramic-fiber-reinforced metal strip and metal strip produced thereby | |
EP2245205B1 (en) | Process for manufacturing a metal part reinforced with ceramic fibres | |
CA2548607A1 (en) | Manufacturing process for a part with an insert made of a composite material with a metal matrix and ceramic fibres | |
EP1864027B1 (en) | Hollow structural rod and production method thereof | |
EP1726678A1 (en) | Process for fabricating a tubular body with a metal matrix composite insert | |
EP2307587B1 (en) | Method for producing a metallic part reinforced by ceramic fibres | |
FR2607071A1 (en) | PROCESS FOR FORMING ARTICLES REINFORCED BY FILAMENTS AND ARTICLES THUS FORMED | |
EP2680991B1 (en) | Method for manufacturing an integral rotationally symmetrical metal part including a reinforcement consisting of ceramic fibers | |
FR2713663A1 (en) | Fabrication of axisymmetrical composite components | |
EP1798429A1 (en) | Composite material tube rod and manufacturing method of such rod | |
EP2245206B1 (en) | Process for manufacturing a metal part reinforced with ceramic fibres | |
FR2970266A1 (en) | METHOD FOR MANUFACTURING A MONOBLOC ANNULAR METAL PIECE WITH A REINFORCING INSERT IN COMPOSITE MATERIAL, AND PART OBTAINED | |
EP2443265B1 (en) | Process for the manufacture of a metallic workpiece incorporating an annular fibrous reinforcement | |
EP2310547B1 (en) | Method for producing a metallic part comprising inner reinforcements consisting of ceramic fibres | |
EP2513350B1 (en) | Method for manufacturing a straight insert made of metal matrix composite material | |
WO2012114053A2 (en) | Method for manufacturing a metal part | |
EP2686123B1 (en) | Process for manufacturing a one-piece axisymmetric metallic part from composite fibrous structures | |
EP2552629B1 (en) | Method of manufacturing an elongate insert made of a metal matrix composite | |
FR2606320A1 (en) | PROCESS FOR FORMING FILAMENT REINFORCED METAL PRODUCTS |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
17P | Request for examination filed |
Effective date: 20111228 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO SE SI SK SM TR |
|
DAX | Request for extension of the european patent (deleted) | ||
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R079 Ref document number: 602010006427 Country of ref document: DE Free format text: PREVIOUS MAIN CLASS: C22C0047060000 Ipc: C22C0014000000 |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
RIC1 | Information provided on ipc code assigned before grant |
Ipc: C22C 47/04 20060101ALI20121005BHEP Ipc: C22C 14/00 20060101AFI20121005BHEP |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO SE SI SK SM TR |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D Free format text: NOT ENGLISH |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D Free format text: LANGUAGE OF EP DOCUMENT: FRENCH |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: REF Ref document number: 607366 Country of ref document: AT Kind code of ref document: T Effective date: 20130515 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 602010006427 Country of ref document: DE Effective date: 20130613 |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: MK05 Ref document number: 607366 Country of ref document: AT Kind code of ref document: T Effective date: 20130417 |
|
REG | Reference to a national code |
Ref country code: LT Ref legal event code: MG4D |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: VDEP Effective date: 20130417 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: PT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20130819 Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20130817 Ref country code: NO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20130717 Ref country code: SE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20130417 Ref country code: AT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20130417 Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20130718 Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20130417 Ref country code: ES Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20130728 Ref country code: SI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20130417 Ref country code: LT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20130417 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: PL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20130417 Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20130717 Ref country code: HR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20130417 Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20130417 Ref country code: LV Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20130417 |
|
BERE | Be: lapsed |
Owner name: MESSIER-BUGATTI-DOWTY Effective date: 20130630 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20130417 Ref country code: CZ Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20130417 Ref country code: EE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20130417 Ref country code: MC Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20130417 Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20130417 |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: RO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20130417 Ref country code: NL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20130417 Ref country code: IT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20130417 |
|
26N | No opposition filed |
Effective date: 20140120 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: MM4A |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20130630 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20130614 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 602010006427 Country of ref document: DE Effective date: 20140120 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20130417 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20140630 Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20140630 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SM Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20130417 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: TR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20130417 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: HU Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO Effective date: 20100614 Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20130614 Ref country code: MK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20130417 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 7 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 8 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: CD Owner name: MESSIER-BUGATTI-DOWTY, FR Effective date: 20170518 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 9 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20130417 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20240521 Year of fee payment: 15 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20240521 Year of fee payment: 15 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20240522 Year of fee payment: 15 |