EP3796102A1 - Method for manufacturing a balance for a timepiece - Google Patents

Method for manufacturing a balance for a timepiece Download PDF

Info

Publication number
EP3796102A1
EP3796102A1 EP20201790.1A EP20201790A EP3796102A1 EP 3796102 A1 EP3796102 A1 EP 3796102A1 EP 20201790 A EP20201790 A EP 20201790A EP 3796102 A1 EP3796102 A1 EP 3796102A1
Authority
EP
European Patent Office
Prior art keywords
metal alloy
balance
ppm
hub
mold
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.)
Granted
Application number
EP20201790.1A
Other languages
German (de)
French (fr)
Other versions
EP3796102B1 (en
Inventor
Alexandre Haemmerli
Jean-Claude Martin
Lionel Paratte
Yves Winkler
Gianni Di Domenico
Pascal Winkler
Jean-Luc Helfer
Lionel TOMBEZ
Baptiste Hinaux
Donald Corson
Michel Willemin
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Swatch Group Research and Development SA
Original Assignee
Swatch Group Research and Development SA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Swatch Group Research and Development SA filed Critical Swatch Group Research and Development SA
Priority to EP20201790.1A priority Critical patent/EP3796102B1/en
Publication of EP3796102A1 publication Critical patent/EP3796102A1/en
Application granted granted Critical
Publication of EP3796102B1 publication Critical patent/EP3796102B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • GPHYSICS
    • G04HOROLOGY
    • G04BMECHANICALLY-DRIVEN CLOCKS OR WATCHES; MECHANICAL PARTS OF CLOCKS OR WATCHES IN GENERAL; TIME PIECES USING THE POSITION OF THE SUN, MOON OR STARS
    • G04B17/00Mechanisms for stabilising frequency
    • G04B17/04Oscillators acting by spring tension
    • G04B17/06Oscillators with hairsprings, e.g. balance
    • G04B17/066Manufacture of the spiral spring
    • GPHYSICS
    • G04HOROLOGY
    • G04BMECHANICALLY-DRIVEN CLOCKS OR WATCHES; MECHANICAL PARTS OF CLOCKS OR WATCHES IN GENERAL; TIME PIECES USING THE POSITION OF THE SUN, MOON OR STARS
    • G04B17/00Mechanisms for stabilising frequency
    • G04B17/04Oscillators acting by spring tension
    • G04B17/06Oscillators with hairsprings, e.g. balance
    • G04B17/063Balance construction
    • GPHYSICS
    • G04HOROLOGY
    • G04BMECHANICALLY-DRIVEN CLOCKS OR WATCHES; MECHANICAL PARTS OF CLOCKS OR WATCHES IN GENERAL; TIME PIECES USING THE POSITION OF THE SUN, MOON OR STARS
    • G04B17/00Mechanisms for stabilising frequency
    • G04B17/20Compensation of mechanisms for stabilising frequency
    • G04B17/22Compensation of mechanisms for stabilising frequency for the effect of variations of temperature
    • G04B17/222Compensation of mechanisms for stabilising frequency for the effect of variations of temperature with balances
    • GPHYSICS
    • G04HOROLOGY
    • G04BMECHANICALLY-DRIVEN CLOCKS OR WATCHES; MECHANICAL PARTS OF CLOCKS OR WATCHES IN GENERAL; TIME PIECES USING THE POSITION OF THE SUN, MOON OR STARS
    • G04B17/00Mechanisms for stabilising frequency
    • G04B17/20Compensation of mechanisms for stabilising frequency
    • G04B17/22Compensation of mechanisms for stabilising frequency for the effect of variations of temperature
    • G04B17/227Compensation of mechanisms for stabilising frequency for the effect of variations of temperature composition and manufacture of the material used
    • GPHYSICS
    • G04HOROLOGY
    • G04BMECHANICALLY-DRIVEN CLOCKS OR WATCHES; MECHANICAL PARTS OF CLOCKS OR WATCHES IN GENERAL; TIME PIECES USING THE POSITION OF THE SUN, MOON OR STARS
    • G04B18/00Mechanisms for setting frequency
    • G04B18/006Mechanisms for setting frequency by adjusting the devices fixed on the balance
    • GPHYSICS
    • G04HOROLOGY
    • G04DAPPARATUS OR TOOLS SPECIALLY DESIGNED FOR MAKING OR MAINTAINING CLOCKS OR WATCHES
    • G04D3/00Watchmakers' or watch-repairers' machines or tools for working materials
    • G04D3/0002Watchmakers' or watch-repairers' machines or tools for working materials for mechanical working other than with a lathe
    • G04D3/0035Watchmakers' or watch-repairers' machines or tools for working materials for mechanical working other than with a lathe for components of the regulating mechanism
    • G04D3/0038Watchmakers' or watch-repairers' machines or tools for working materials for mechanical working other than with a lathe for components of the regulating mechanism for balances
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C9/00Moulds or cores; Moulding processes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D15/00Casting using a mould or core of which a part significant to the process is of high thermal conductivity, e.g. chill casting; Moulds or accessories specially adapted therefor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D25/00Special casting characterised by the nature of the product
    • B22D25/02Special casting characterised by the nature of the product by its peculiarity of shape; of works of art
    • B22D25/026Casting jewelry articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D27/00Treating the metal in the mould while it is molten or ductile ; Pressure or vacuum casting
    • B22D27/04Influencing the temperature of the metal, e.g. by heating or cooling the mould
    • 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
    • C22C16/00Alloys based on zirconium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/08Ferrous alloys, e.g. steel alloys containing nickel
    • GPHYSICS
    • G04HOROLOGY
    • G04CELECTROMECHANICAL CLOCKS OR WATCHES
    • G04C3/00Electromechanical clocks or watches independent of other time-pieces and in which the movement is maintained by electric means
    • G04C3/04Electromechanical clocks or watches independent of other time-pieces and in which the movement is maintained by electric means wherein movement is regulated by a balance

Definitions

  • the invention relates to a method of manufacturing a balance for a timepiece comprising a rim, a hub and at least one arm connecting the hub to said rim.
  • the oscillator or resonator of a mechanical watch consists of a spiral spring and a flywheel called a balance.
  • Thermal variations cause the stiffness of the hairspring to vary, as well as the geometries of the hairspring and balance, which modifies the spring constant and inertia, and therefore the frequency of oscillation.
  • Watchmakers have worked hard to have temperature-stable oscillators and several avenues have been explored / exploited, one of which won a Nobel Prize to Charles-Edouardclair for the development of the Elinvar alloy, the modulus of elasticity of which increases with increasing temperature. temperature and compensates for the increase in inertia of the balance.
  • the monocrystalline quartz hairspring enables thermal compensation for the change in inertia of the balance.
  • quartz is limited to materials having a thermal expansion coefficient of the order of 10 ppm / ° C, which corresponds for example titanium and platinum.
  • the main problem with these materials is the machinability and control of a fine structure and / or a perfect finish (mirror polish for example).
  • titanium its relatively low density limits its use for large balance wheels and in the case of platinum, its high price limits its use to prestige and luxury products.
  • the object of the present invention is to remedy these drawbacks by proposing a method of manufacturing a balance made of new materials allowing simpler and more precise manufacture, so as to reduce, for example, the dispersion of inertia and / or of unbalance within the same production batch.
  • a metal alloy balance wheel can be made using a simplified manufacturing process such as a casting process or a hot forming process.
  • the metal alloy in its at least partially amorphous form has the property of having a much larger elastic range than its crystalline equivalent, thanks to the absence of dislocation. This property makes it possible to overmold or integrate into the balance elements making it possible to improve the centering as well as to adjust the inertia and / or the unbalance.
  • a balance 1 for a timepiece conventionally comprises a rim 2, continuous or not, defining the outside diameter of the balance 1, a hub 4, forming its central part and provided with a hole 6 intended to receive a shaft (not shown) defining the pivot axis of the balance 1.
  • the hub 4 is integrally connected to the rim 2 by arms 8.
  • the arms 8 are here four in number and are arranged at 90 °. We also usually find balances with two or three arms, arranged respectively at 180 ° or 120 °.
  • the rim 2, the hub 4 and the arms 8 are made from the same metal alloy.
  • the balance 1 is in one piece, that is to say made in one piece.
  • the balance 1 can for example be made entirely from an alloy based on platinum or palladium which will be described in detail below. Since platinum in particular has a high density (21,000 kg / m 3 ), the platinum alloy used in the invention also has a high density (15.5 g / cm 3 ), so that the addition of elements in dense material to increase the inertia of the balance will not necessarily be necessary.
  • the cooling step d) can be carried out at a cooling rate chosen to obtain a crystalline, partially amorphous or completely amorphous alloy.
  • the balance 1 can also be produced entirely, for example, from an alloy based on titanium or on zirconium which will be described in detail below.
  • Zirconium for example having a lower density
  • the zirconium alloy used in the invention also has a lower density (6.5 g / cm 3 ), so that the addition of elements of more dense material for increasing the inertia of the balance is recommended, especially if you want to make a small balance for small movements. These elements make it possible to increase the inertia of the balance while keeping an aesthetic serge geometry and with good aerodynamic properties.
  • the rim 2 can comprise first elements for adjusting the inertia 10 overmolded, said first elements for adjusting the inertia 10 being made of a material having a density greater than the density of the metal alloy.
  • These first elements of the inertia 10 can for example be made of tungsten or tungsten carbide, and are obtained by overmolding.
  • the method according to the invention comprises a step of overmolding said first inertia adjustment elements 10 in the rim 2, by means of inserts placed in the mold before the introduction of the metal alloy, and overmolded, said first inertia adjusting elements 10 being made of a first material having a density greater than the density of said metal alloy.
  • the arms and the hub of the balance are made of a metal alloy, the rim being made of a material having a density greater than the density of said metal alloy used for the arms and the hub.
  • This material can itself be the metal alloy based on platinum or palladium as defined below or another material.
  • the arms and the hub of the balance wheel are made in the amorphous metal alloy based on zirconium as defined below to allow the balance to be paired with a hairspring, preferably in monocrystalline quartz, and the rim is made in another material having a density greater than the density of the metal alloy based on zirconium used for the arms and the hub in order to improve the inertia of the balance.
  • the cooling step d) can be carried out at a cooling rate chosen to obtain a crystalline, partially amorphous or completely amorphous alloy.
  • the methods of the invention according to the first or second embodiments advantageously use the properties of a metal alloy capable of being in at least partially amorphous form when heated to easily shape it in order to achieve a metal alloy balance.
  • a metal alloy capable of being in an at least partially amorphous form when heated allows great ease in shaping allowing the manufacture of parts with complicated shapes with greater precision.
  • One process advantageously used is the hot forming of an amorphous preform.
  • This preform is obtained by melting in a furnace the metallic elements intended to constitute the metallic alloy. This melting is carried out under a controlled atmosphere with the aim of obtaining as low a contamination of the oxygen alloy as possible. Once these elements are melted, they are cast in the form of a semi-finished product, then cooled rapidly in order to maintain the partially or completely amorphous state.
  • the hot forming is carried out in order to obtain a final part. This hot forming is carried out by pressing in a temperature range between the glass transition temperature Tg and the crystallization temperature Tx of the metal alloy for a determined time to maintain an at least partially amorphous structure. This is done in order to maintain the elastic properties characteristic of amorphous metals.
  • the balance can also be produced by casting or by injection.
  • This process consists in casting or injecting the metal alloy heated to a temperature between its glass transition temperature and its crystallization temperature so as to be at least partially amorphous in a mold having the shape of the final part.
  • the mold can be reused or dissolved to release the parts.
  • the molding process has the advantage of perfectly replicating the geometry of the balance, including any decorations or surface structuring. This results in less dispersion of inertia and better centering on a production batch of balances.
  • the molding process makes it possible to obtain a balance with an aesthetic geometry, with sharp interior angles, a serge profile and / or domed arm, and a perfect finish. It is also possible to provide a non-continuous serge.
  • the mold will be made in silicon by a DRIE process. It is obvious that the mold can also be produced by machining by milling, laser, electroerosion or any other type of machining.
  • the elastic properties characteristic of amorphous metals are used to overmold or integrate functional and / or decorative elements in the rim and / or at the level of the arms and / or at the level of the hub, for example by means of corresponding inserts placed in the front mold. the introduction of the metal alloy heated between its glass transition temperature and its crystallization temperature to be at least partially amorphous.
  • the rim 2 can comprise housings 12 intended to receive second elements for adjusting the inertia and / or unbalance 14, as shown in FIG. figure 3 .
  • These housings 12 can advantageously be provided during the manufacture of the balance 1 by molding, in accordance with the methods of the invention.
  • the second inertia and / or unbalance adjustment elements 14, 15 can be, for example, weights, slotted weights, pins 14, split pins, or pins with unbalance 15, which act as weights. These elements are driven out or clipped into the corresponding housings 12.
  • the figure 4 shows a sectional view along line AA of the figure 3 showing the pin with unbalance 15 inserted in the housing 12 provided in the rim 2.
  • these elements for increasing the inertia of the balance are preferably used with a rim made of a low density material, such as titanium or zirconium, but can also be used with a rim made of another material.
  • the 12 units shown on the figure 3 can also constitute housings intended to receive aesthetic and / or luminescent elements, such as tritium tubes (not shown), or capsules of phosphorescent materials (of the Superluminova type, for example) or fluorescent.
  • aesthetic and / or luminescent elements such as tritium tubes (not shown), or capsules of phosphorescent materials (of the Superluminova type, for example) or fluorescent.
  • one or the other of the methods comprises a step of overmolding flexible centering elements 16, 17 on the hub 4, on its inner periphery or on its surface.
  • the hub 4 can include integrated flexible centering elements, which allow self-centering of the balance when it is mounted on an axis by virtue of the elastic deformation of said flexible centering elements.
  • said integrated flexible centering elements 16 are elastic blades provided on the inner periphery of the hub 4 so as to be positioned in the hole 6.
  • said integrated flexible centering elements 17 are provided on the surface of the hub 4 and are distributed around the hole 6.
  • the flexible centering elements 16 and 17 can advantageously be put in place during the manufacture of the balance 1 by molding, in accordance with methods of the invention.
  • one or the other of the methods comprises a step of overmolding third flexible inertia adjustment elements 19, 20, 22a, 22b in the arm 8.
  • at least l one of the arms 8 carries integrated flexible third inertia adjustment elements.
  • the end of the arm 8 on the side of the rim 2 ends in two branches 8a, 8b forming between them a housing 18 in which is integrated a third element for adjusting the inertia 19 flexible bistable "V" for the adjustment frequency.
  • the third inertia adjustment element 20 is made of a material having expansion properties different from the metal alloy of the balance of the invention, such as silicon or silicon oxide.
  • the end of the arm 8 on the side of the rim 2 ends in three branches 8a, 8b, 8c forming between them two housings 18a, 18b in which are integrated third elements for adjusting the inertia 22a, 22b flexible multi- stable ratchet for frequency adjustment.
  • These third flexible inertia adjustment elements 19, 20, 22a, 22b for adjusting the frequency can advantageously be put in place during the manufacture of the balance 1 by molding, in accordance with the methods of the invention.
  • These third flexible inertia adjustment elements 19, 20, 22a, 22b for frequency adjustment can be used as well when the entire balance wheel is in the same metal alloy as when the arms are in metal alloy, the rest of the balance, and in particular the serge, being in another material.
  • one or the other of the methods of the invention is used a mold having microstructures forming a decoration or a photonic network.
  • one of the arm 8, of the rim 2 and of the hub 4 has a structured surface condition. Only one of the elements can have a structured surface condition or all the elements of the balance can have a structured surface condition, this structured surface condition may be the same or different.
  • the figure 10 shows a balance of the invention for which the serge 2 has a structured surface condition different from the structured surface condition presented by the arm 8.
  • This structured surface condition can be a polished, satin, sandblasted, pearl, sunny condition. , etc.
  • microstructures forming a photonic network in order to replicate these microstructures on the surface of the balance.
  • These microstructures can make it possible to create a photonic crystal giving the part a certain color, a hologram, or a diffraction grating which can constitute an anti-counterfeiting element.
  • the structures are introduced directly into the mold, and are replicated during the manufacture of the balances by hot forming, which no longer requires termination operations. It is also possible to add a logo to the mold.
  • the metal alloy used in the processes of the invention exhibits a coefficient of thermal expansion typically less than 25 ppm / ° C and greater than 7 ppm / ° C, and is capable of being in at least partially amorphous form when it is heated to a temperature between its glass transition temperature and its crystallization temperature.
  • the metal alloy used in the methods of the invention is based on an element chosen from the group consisting of platinum, zirconium, titanium, palladium, nickel, aluminum and iron.
  • the expression “based on an element” means that said metal alloy contains at least 50% by weight of said element.
  • Said metal alloy used in the present invention may be based on platinum and has a coefficient of thermal expansion of less than 12 ppm / ° C, preferably between 8 ppm / ° C and 12 ppm / ° C.
  • the metal alloy used in the present invention can also be based on zirconium and has a coefficient of thermal expansion of less than 12 ppm / ° C, preferably between 8 ppm / ° C and 11 ppm / ° C.
  • the metal alloy used in the present invention can also be based on palladium and has a coefficient of thermal expansion of less than 20 ppm / ° C, preferably between 13 ppm / ° C and 18 ppm / ° C.
  • the alloys used in the invention do not contain any impurities. However, they may include traces of impurities which can result, often inevitably, from the production of said alloys.
  • the alloys used in the present invention have a thermal expansion coefficient of less than 12 ppm / ° C and greater than 8 ppm / ° C, they can be used to make at least part of a balance which will be paired with a hairspring. preferably monocrystalline quartz.
  • the alloys used in the present invention having a thermal expansion coefficient of less than 20 ppm / ° C and greater than 13 ppm / ° C can be used to make at least part of a balance which will be paired with a metal hairspring or silicon.
  • said metal alloy used in the present invention based on platinum consists, in atomic% values, of: 57.5% Pt, 14.7% Cu, 5.3% Ni, 22.5% P.
  • Such an alloy has an expansion coefficient thermal between 11 and 12 ppm / ° C.
  • said metal alloy used in the present invention based on zirconium consists, in atomic% values, of: 58.5% Zr, 15.6% Cu, 12.8% Ni, 10.3% Al, 2.8% Nb.
  • Such an alloy has a thermal expansion coefficient of between 10.5 and 11 ppm / ° C.
  • said metal alloy used in the present invention based on palladium consists, in atomic% values, of: 43% Pd, 27% Cu, 10% Ni, 20% P.
  • Such an alloy has an expansion coefficient temperature between 15 and 16 ppm / ° C.
  • the balance according to the invention is made of a material making it possible to use a simple manufacturing process while having a thermal expansion coefficient allowing it to be paired with a monocrystalline quartz hairspring, and / or in metal or silicon. , preferably monocrystalline quartz.
  • the balance according to the invention also makes it possible to have at least arms having a coefficient of thermal expansion making it possible to pair it with a monocrystalline quartz hairspring, and / or in metal or in silicon, while having great inertia while keeping a compact and aesthetic serge geometry, of small volume, using an adequate serge, either comprising elements made of a material of greater density, or being itself made of a higher density material.

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Metallurgy (AREA)
  • Manufacturing & Machinery (AREA)
  • Adornments (AREA)
  • Forging (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)
  • Micromachines (AREA)

Abstract

L'invention concerne un procédé de fabrication d'un balancier en alliage métallique par moulage, ledit procédé comprenant les étapes suivantes : réaliser un moule ayant la forme négative du balancier (1) ; se munir d'un alliage métallique présentant un coefficient de dilatation thermique inférieur à 25 ppm/°C et capable d'être sous une forme au moins partiellement amorphe lorsqu'il est chauffé à une température comprise entre sa température de transition vitreuse et sa température de cristallisation ; introduire dans le moule l'alliage métallique, ledit alliage métallique étant chauffé à une température comprise entre sa température de transition vitreuse et sa température de cristallisation pour être formé à chaud et pour former un balancier ; refroidir ledit alliage métallique pour obtenir un balancier (1) dans ledit alliage métallique ; libérer le balancier (1) obtenu à l'étape d) de son moule, ledit procédé étant caractérisé en ce qu'il comprend une étape de surmoulage d'éléments de centrage flexibles (16, 17) sur le moyeu (4).

Figure imgaf001
The invention relates to a method of manufacturing a metal alloy balance by casting, said method comprising the following steps: producing a mold having the negative shape of the balance (1); be provided with a metal alloy having a coefficient of thermal expansion of less than 25 ppm / ° C and capable of being in an at least partially amorphous form when it is heated to a temperature between its glass transition temperature and its temperature crystallization; introducing the metal alloy into the mold, said metal alloy being heated to a temperature between its glass transition temperature and its crystallization temperature in order to be hot formed and to form a balance; cooling said metal alloy to obtain a balance (1) in said metal alloy; releasing the balance (1) obtained in step d) from its mold, said method being characterized in that it comprises a step of overmolding flexible centering elements (16, 17) on the hub (4).
Figure imgaf001

Description

Domaine de l'inventionField of the invention

L'invention concerne un procédé de fabrication d'un balancier pour pièce d'horlogerie comprenant une serge, un moyeu et au moins un bras reliant le moyeu à ladite serge.The invention relates to a method of manufacturing a balance for a timepiece comprising a rim, a hub and at least one arm connecting the hub to said rim.

Arrière-plan de l'inventionBackground of the invention

L'oscillateur ou résonateur d'une montre mécanique est constitué d'un ressort spiral et d'un volant d'inertie appelé balancier. Les variations thermiques font varier la rigidité du spiral, ainsi que les géométries du spiral et du balancier, ce qui modifie la constante de ressort et l'inertie, et donc la fréquence d'oscillation. Les horlogers ont beaucoup travaillé pour avoir des oscillateurs stables en température et plusieurs voies ont été explorées/exploitées dont une qui a valu un Prix Nobel à Charles-Edouard Guillaume pour le développement de l'alliage Elinvar dont le module d'élasticité augmente avec la température et compense l'augmentation d'inertie du balancier. Par la suite, le développement du silicium oxydé, donc compensé thermiquement, a surpassé les performances de l'Elinvar et a pour avantage d'être moins sensible aux champs magnétiques. De même le spiral en quartz monocristallin permet une compensation thermique du changement d'inertie du balancier. Mais contrairement au silicium oxydé dont l'épaisseur d'oxyde peut être variée suivant le matériau de balancier utilisé, le quartz est limité aux matériaux ayant un coefficient de dilatation thermique de l'ordre de 10 ppm/°C, ce qui correspond par exemple au titane et au platine. Le problème principal de ces matériaux est l'usinabilité et la maîtrise de structure fine et/ou d'une finition parfaite (poli miroir par exemple). Dans le cas du titane, sa relativement faible densité limite son utilisation pour des grands balanciers et dans le cas du platine son prix élevé limite son utilisation à des produits de prestige et de luxe.The oscillator or resonator of a mechanical watch consists of a spiral spring and a flywheel called a balance. Thermal variations cause the stiffness of the hairspring to vary, as well as the geometries of the hairspring and balance, which modifies the spring constant and inertia, and therefore the frequency of oscillation. Watchmakers have worked hard to have temperature-stable oscillators and several avenues have been explored / exploited, one of which won a Nobel Prize to Charles-Edouard Guillaume for the development of the Elinvar alloy, the modulus of elasticity of which increases with increasing temperature. temperature and compensates for the increase in inertia of the balance. Subsequently, the development of oxidized silicon, therefore thermally compensated, surpassed the performance of the Elinvar and has the advantage of being less sensitive to magnetic fields. Likewise, the monocrystalline quartz hairspring enables thermal compensation for the change in inertia of the balance. But unlike oxidized silicon, the oxide thickness of which can be varied depending on the balance material used, quartz is limited to materials having a thermal expansion coefficient of the order of 10 ppm / ° C, which corresponds for example titanium and platinum. The main problem with these materials is the machinability and control of a fine structure and / or a perfect finish (mirror polish for example). In the case of titanium, its relatively low density limits its use for large balance wheels and in the case of platinum, its high price limits its use to prestige and luxury products.

On connaît des procédés de fabrication de balancier par moulage d'un matériau partiellement amorphe, comme dans le document EP 3 170 579 A1 .There are known methods of manufacturing a balance by molding a partially amorphous material, as in the document EP 3 170 579 A1 .

Résumé de l'inventionSummary of the invention

La présente invention a pour but de remédier à ces inconvénients en proposant un procédé de fabrication d'un balancier réalisé dans de nouveaux matériaux permettant une fabrication plus simple et plus précise, de manière à réduire par exemple la dispersion d'inertie et/ou de balourd au sein d'un même lot de production.The object of the present invention is to remedy these drawbacks by proposing a method of manufacturing a balance made of new materials allowing simpler and more precise manufacture, so as to reduce, for example, the dispersion of inertia and / or of unbalance within the same production batch.

A cet effet, l'invention se rapporte tout d'abord à un procédé de fabrication d'un balancier pour pièce d'horlogerie comprenant une serge, un moyeu et au moins un bras reliant le moyeu à ladite serge, la serge, le moyeu et les bras étant réalisés dans un alliage métallique, ledit procédé comprenant les étapes suivantes:

  1. a) réaliser un moule ayant la forme négative du balancier
  2. b) se munir d'un alliage métallique présentant un coefficient de dilatation thermique inférieur à 25 ppm/°C et capable d'être sous une forme au moins partiellement amorphe lorsqu'il est chauffé à une température comprise entre sa température de transition vitreuse et sa température de cristallisation
  3. c) introduire dans le moule l'alliage métallique, ledit alliage métallique étant chauffé à une température comprise entre sa température de transition vitreuse et sa température de cristallisation pour être formé à chaud et former un balancier
  4. d) refroidir ledit alliage métallique pour obtenir un balancier dans ledit alliage métallique
  5. e) libérer le balancier obtenu à l'étape d) de son moule,
le procédé étant caractérisé en ce qu'il comprend une étape de surmoulage d'éléments de centrage flexibles sur le moyeu.To this end, the invention relates first of all to a method of manufacturing a balance for a timepiece comprising a rim, a hub and at least one arm connecting the hub to said rim, the rim, the hub. and the arms being made of a metal alloy, said method comprising the following steps:
  1. a) make a mold with the negative shape of the balance
  2. b) be provided with a metal alloy having a thermal expansion coefficient of less than 25 ppm / ° C and capable of being in an at least partially amorphous form when it is heated to a temperature between its glass transition temperature and its crystallization temperature
  3. c) introducing the metal alloy into the mold, said metal alloy being heated to a temperature between its glass transition temperature and its crystallization temperature in order to be hot formed and to form a pendulum
  4. d) cooling said metal alloy to obtain a balance in said metal alloy
  5. e) release the balance obtained in step d) from its mold,
the method being characterized in that it comprises a step of overmolding flexible centering elements on the hub.

La présente invention concerne également un procédé de fabrication d'un balancier pour pièce d'horlogerie comprenant une serge, un moyeu et au moins un bras reliant le moyeu à ladite serge, le moyeu et le bras étant réalisés dans un alliage métallique, et la serge étant réalisée dans un matériau présentant une masse volumique supérieure à la masse volumique dudit alliage métallique dans lequel le moyeu et le bras sont réalisés, ledit procédé comprenant les étapes suivantes :

  • a) réaliser un moule ayant la forme négative du balancier ;
  • a') insérer dans le moule une serge ou des éléments de serge réalisés dans un matériau présentant une masse volumique supérieure à la masse volumique dudit alliage métallique ;
  • b) se munir d'un alliage métallique présentant un coefficient de dilatation thermique inférieur à 25 ppm/°C et capable d'être sous une forme au moins partiellement amorphe lorsqu'il est chauffé à une température comprise entre sa température de transition vitreuse et sa température de cristallisation ;
  • c) introduire dans le moule l'alliage métallique, ledit alliage métallique étant chauffé à une température comprise entre sa température de transition vitreuse et sa température de cristallisation pour être formé à chaud et surmouler la serge ou les éléments de serge pour former un balancier avec inserts ;
  • d) refroidir ledit alliage métallique pour obtenir un balancier avec inserts ;
  • e) libérer le balancier obtenu à l'étape d) de son moule,
le procédé étant caractérisé en ce qu'il comprend une étape de surmoulage d'éléments de centrage flexibles sur le moyeu.The present invention also relates to a method of manufacturing a balance for a timepiece comprising a rim, a hub and at least one arm connecting the hub to said rim, the hub and the arm being made of a metal alloy, and the rim being made of a material having a density greater than the density of said metal alloy in which the hub and the arm are made, said method comprising the following steps:
  • a) making a mold having the negative shape of the balance;
  • a ') inserting into the mold a serge or serge elements made of a material having a density greater than the density of said metal alloy;
  • b) be provided with a metal alloy having a thermal expansion coefficient of less than 25 ppm / ° C and capable of being in an at least partially amorphous form when it is heated to a temperature between its glass transition temperature and its crystallization temperature;
  • c) introducing the metal alloy into the mold, said metal alloy being heated to a temperature between its glass transition temperature and its crystallization temperature in order to be hot-formed and overmold the serge or the serge elements to form a balance with inserts;
  • d) cooling said metal alloy to obtain a balance with inserts;
  • e) release the balance obtained in step d) from its mold,
the method being characterized in that it comprises a step of overmolding flexible centering elements on the hub.

Grâce aux propriétés des métaux amorphes, un balancier en alliage métallique peut être réalisé en utilisant un procédé de fabrication simplifié tel qu'un procédé de coulée ou un procédé de formage à chaud. En outre, l'alliage métallique sous sa forme au moins partiellement amorphe a pour propriété d'avoir une plage élastique bien plus grande que son équivalent cristallin, grâce à l'absence de dislocation. Cette propriété permet de surmouler ou d'intégrer au balancier des éléments permettant d'améliorer le centrage ainsi que de régler l'inertie et/ou le balourd.Due to the properties of amorphous metals, a metal alloy balance wheel can be made using a simplified manufacturing process such as a casting process or a hot forming process. In addition, the metal alloy in its at least partially amorphous form has the property of having a much larger elastic range than its crystalline equivalent, thanks to the absence of dislocation. This property makes it possible to overmold or integrate into the balance elements making it possible to improve the centering as well as to adjust the inertia and / or the unbalance.

Description sommaire des dessinsBrief description of the drawings

D'autres particularités et avantages ressortiront clairement de la description qui en est faite ci-après, à titre indicatif et nullement limitatif, en référence aux dessins annexés, dans lesquels :

  • la figure 1 est une vue en perspective d'un balancier fabriqué selon l'invention ;
  • la figure 2 est une vue de dessus partielle d'une variante de balancier réalisé selon l'invention ;
  • la figure 3 est une vue de dessus partielle d'une autre variante de balancier réalisé selon l'invention ;
  • la figure 4 est une vue en coupe selon l'axe A-A de la figure 3 ; et
  • les figures 5 à 10 sont des vues de dessus partielles d'autres variantes de balancier réalisé selon l'invention.
Other features and advantages will emerge clearly from the description which is given below, by way of indication and in no way limiting, with reference to the appended drawings, in which:
  • the figure 1 is a perspective view of a balance manufactured according to the invention;
  • the figure 2 is a partial top view of a variant of a balance made according to the invention;
  • the figure 3 is a partial top view of another variant of a balance made according to the invention;
  • the figure 4 is a sectional view along the AA axis of the figure 3 ; and
  • the figures 5 to 10 are partial top views of other variants of a balance made according to the invention.

Description détaillée des modes de réalisation préférésDetailed description of the preferred embodiments

En référence à la figure 1, il est représenté un balancier 1 pour pièce d'horlogerie. Un tel balancier 1 comprend d'une manière traditionnelle une serge 2, continue ou non, définissant le diamètre extérieur du balancier 1, un moyeu 4, formant sa partie centrale et muni d'un trou 6 destiné à recevoir un arbre (non représenté) définissant l'axe de pivotement du balancier 1. Le moyeu 4 est relié solidairement à la serge 2 par des bras 8. Les bras 8 sont ici au nombre de quatre et sont disposés à 90°. On trouve aussi usuellement des balanciers avec deux ou trois bras, disposés respectivement à 180° ou 120°.With reference to the figure 1 , there is shown a balance 1 for a timepiece. Such a balance 1 conventionally comprises a rim 2, continuous or not, defining the outside diameter of the balance 1, a hub 4, forming its central part and provided with a hole 6 intended to receive a shaft (not shown) defining the pivot axis of the balance 1. The hub 4 is integrally connected to the rim 2 by arms 8. The arms 8 are here four in number and are arranged at 90 °. We also usually find balances with two or three arms, arranged respectively at 180 ° or 120 °.

Selon un premier mode de réalisation, la serge 2, le moyeu 4 et les bras 8 sont réalisés dans un même alliage métallique. D'une manière avantageuse, le balancier 1 est monobloc, c'est-à-dire réalisé d'une seule pièce.According to a first embodiment, the rim 2, the hub 4 and the arms 8 are made from the same metal alloy. Advantageously, the balance 1 is in one piece, that is to say made in one piece.

Le balancier 1 peut par exemple être réalisé entièrement dans un alliage à base de platine ou de palladium qui sera décrit en détail ci-après. Le platine notamment présentant une grande masse volumique (21000 kg/m3), l'alliage en platine utilisé dans l'invention présente également une masse volumique élevée (15.5 g/cm3), de sorte que l'ajout d'éléments en matériau dense pour augmenter l'inertie du balancier ne sera pas forcément nécessaire.The balance 1 can for example be made entirely from an alloy based on platinum or palladium which will be described in detail below. Since platinum in particular has a high density (21,000 kg / m 3 ), the platinum alloy used in the invention also has a high density (15.5 g / cm 3 ), so that the addition of elements in dense material to increase the inertia of the balance will not necessarily be necessary.

A cet effet, conformément à un premier mode de réalisation de l'invention, le procédé de fabrication d'un balancier 1, dans lequel la serge 2, le moyeu 4 et le bras 8 sont réalisés dans un même alliage métallique, comprend les étapes suivantes:

  1. a) réaliser un moule ayant la forme négative du balancier 1, y compris d'éventuelles structures décoratives de surface ;
  2. b) se munir d'un alliage métallique présentant un coefficient de dilatation thermique typiquement inférieur à 25 ppm/°C et capable d'être sous une forme au moins partiellement amorphe lorsqu'il est chauffé à une température comprise entre sa température de transition vitreuse et sa température de cristallisation ;
  3. c) introduire dans le moule l'alliage métallique, ledit alliage métallique étant chauffé à une température comprise entre sa température de transition vitreuse et sa température de cristallisation pour être formé à chaud et former un balancier ;
  4. d) refroidir ledit alliage métallique pour obtenir un balancier 1 dans ledit alliage métallique ;
  5. e) libérer le balancier 1 obtenu à l'étape d) de son moule.
To this end, in accordance with a first embodiment of the invention, the method of manufacturing a balance 1, in which the rim 2, the hub 4 and the arm 8 are made of the same metal alloy, comprises the steps following:
  1. a) making a mold having the negative shape of the balance 1, including any decorative surface structures;
  2. b) use a metal alloy having a thermal expansion coefficient typically less than 25 ppm / ° C and capable of being in at least partially amorphous form when heated to a temperature between its glass transition temperature and its crystallization temperature;
  3. c) introducing the metal alloy into the mold, said metal alloy being heated to a temperature between its glass transition temperature and its crystallization temperature in order to be hot formed and to form a balance;
  4. d) cooling said metal alloy to obtain a balance 1 in said metal alloy;
  5. e) releasing the balance 1 obtained in step d) from its mold.

L'étape d) de refroidissement peut se faire à une vitesse de refroidissement choisie pour obtenir un alliage cristallin, partiellement amorphe ou totalement amorphe.The cooling step d) can be carried out at a cooling rate chosen to obtain a crystalline, partially amorphous or completely amorphous alloy.

Le balancier 1 peut également être réalisé entièrement par exemple dans un alliage à base de titane ou de zirconium qui sera décrit en détails ci-après. Le zirconium par exemple présentant une masse volumique plus faible, l'alliage en zirconium utilisé dans l'invention présente également une masse volumique plus faible (6.5 g/cm3), de sorte que l'ajout d'éléments en matériau plus dense pour augmenter l'inertie du balancier est recommandé, notamment si l'on souhaite réaliser un balancier de petite taille pour de petits mouvements. Ces éléments permettent d'augmenter l'inertie du balancier tout en gardant une géométrie de serge esthétique et avec de bonnes propriétés aérodynamiques.The balance 1 can also be produced entirely, for example, from an alloy based on titanium or on zirconium which will be described in detail below. Zirconium, for example having a lower density, the zirconium alloy used in the invention also has a lower density (6.5 g / cm 3 ), so that the addition of elements of more dense material for increasing the inertia of the balance is recommended, especially if you want to make a small balance for small movements. These elements make it possible to increase the inertia of the balance while keeping an aesthetic serge geometry and with good aerodynamic properties.

Ainsi, selon une première variante représentée sur la figure 2, la serge 2 peut comprendre des premiers éléments de réglage de l'inertie 10 surmoulés, lesdits premiers éléments de réglage de l'inertie 10 étant réalisés dans un matériau présentant une masse volumique supérieure à la masse volumique de l'alliage métallique. Ces premiers éléments de réglage de l'inertie 10 peuvent par exemple être en tungstène ou carbure de tungstène, et sont obtenus par surmoulage.Thus, according to a first variant shown in figure 2 , the rim 2 can comprise first elements for adjusting the inertia 10 overmolded, said first elements for adjusting the inertia 10 being made of a material having a density greater than the density of the metal alloy. These first elements of the inertia 10 can for example be made of tungsten or tungsten carbide, and are obtained by overmolding.

A cet effet, le procédé selon l'invention comprend une étape de surmoulage desdits premiers éléments de réglage de l'inertie 10 dans la serge 2, au moyen d'inserts placés dans le moule avant l'introduction de l'alliage métallique, et surmoulés, lesdits premiers éléments de réglage de l'inertie 10 étant réalisés dans un premier matériau présentant une masse volumique supérieure à la masse volumique dudit alliage métallique.To this end, the method according to the invention comprises a step of overmolding said first inertia adjustment elements 10 in the rim 2, by means of inserts placed in the mold before the introduction of the metal alloy, and overmolded, said first inertia adjusting elements 10 being made of a first material having a density greater than the density of said metal alloy.

Selon un second mode de réalisation, les bras et le moyeu du balancier sont réalisés dans un alliage métallique, la serge étant réalisée dans un matériau présentant une masse volumique supérieure à la masse volumique dudit alliage métallique utilisé pour les bras et le moyeu. Ce matériau peut être lui-même l'alliage métallique à base de platine ou de palladium tel que défini ci-dessous ou un autre matériau.According to a second embodiment, the arms and the hub of the balance are made of a metal alloy, the rim being made of a material having a density greater than the density of said metal alloy used for the arms and the hub. This material can itself be the metal alloy based on platinum or palladium as defined below or another material.

Par exemple, les bras et le moyeu du balancier sont réalisés dans l'alliage métallique amorphe à base de zirconium tel que défini ci-dessous pour permettre d'appairer le balancier avec un spiral de préférence en quartz monocristallin, et la serge est réalisée dans un autre matériau présentant une masse volumique supérieure à la masse volumique de l'alliage métallique à base de zirconium utilisé pour les bras et le moyeu afin d'améliorer l'inertie du balancier.For example, the arms and the hub of the balance wheel are made in the amorphous metal alloy based on zirconium as defined below to allow the balance to be paired with a hairspring, preferably in monocrystalline quartz, and the rim is made in another material having a density greater than the density of the metal alloy based on zirconium used for the arms and the hub in order to improve the inertia of the balance.

A cet effet, conformément à un second mode de réalisation de l'invention, le procédé de fabrication d'un balancier pour pièce d'horlogerie dans lequel le moyeu 4 et les bras 8 sont réalisés dans un alliage métallique, et la serge 2 est réalisée dans un second matériau présentant une masse volumique supérieure à la masse volumique dudit alliage métallique dans lequel le moyeu 4 et les bras 8 sont réalisés, comprend les étapes suivantes:

  • a) réaliser un moule ayant la forme négative du balancier, y compris d'éventuelles structures décoratives de surface ;
  • a') insérer dans le moule une serge ou des éléments de serge réalisés dans un matériau présentant une masse volumique supérieure à la masse volumique dudit alliage métallique;
  • b) se munir d'un alliage métallique présentant un coefficient de dilatation thermique typiquement inférieur à 25 ppm/°C et capable d'être sous une forme au moins partiellement amorphe lorsqu'il est chauffé à une température comprise entre sa température de transition vitreuse et sa température de cristallisation ;
  • c) introduire dans le moule l'alliage métallique, ledit alliage métallique étant chauffé à une température comprise entre sa température de transition vitreuse et sa température de cristallisation pour être formé à chaud et surmouler la serge ou les éléments de serge pour former un balancier avec inserts ;
  • d) refroidir ledit alliage métallique pour obtenir un balancier avec ses inserts ;
  • e) libérer le balancier obtenu à l'étape d) de son moule.
To this end, in accordance with a second embodiment of the invention, the method of manufacturing a balance for a timepiece in which the hub 4 and the arms 8 are made of a metal alloy, and the rim 2 is produced in a second material having a density greater than the density of said metal alloy in which the hub 4 and the arms 8 are made, comprises the following steps:
  • a) making a mold having the negative shape of the balance, including any decorative surface structures;
  • a ') inserting into the mold a serge or serge elements made of a material having a density greater than the density of said metal alloy;
  • b) be provided with a metal alloy having a thermal expansion coefficient typically less than 25 ppm / ° C and capable of being in an at least partially amorphous form when it is heated to a temperature between its glass transition temperature and its crystallization temperature;
  • c) introducing the metal alloy into the mold, said metal alloy being heated to a temperature between its glass transition temperature and its crystallization temperature in order to be hot-formed and overmold the serge or the serge elements to form a balance with inserts;
  • d) cooling said metal alloy to obtain a balance with its inserts;
  • e) releasing the balance obtained in step d) from its mold.

L'étape d) de refroidissement peut se faire à une vitesse de refroidissement choisie pour obtenir un alliage cristallin, partiellement amorphe ou totalement amorphe.The cooling step d) can be carried out at a cooling rate chosen to obtain a crystalline, partially amorphous or completely amorphous alloy.

Les procédés de l'invention selon le premier ou deuxième modes de réalisation utilisent de manière avantageuse les propriétés d'un alliage métallique capable d'être sous une forme au moins partiellement amorphe lorsqu'il est chauffé pour le mettre facilement en forme afin de réaliser un balancier en alliage métallique.The methods of the invention according to the first or second embodiments advantageously use the properties of a metal alloy capable of being in at least partially amorphous form when heated to easily shape it in order to achieve a metal alloy balance.

En effet, un alliage métallique capable d'être sous une forme au moins partiellement amorphe lorsqu'il est chauffé permet une grande facilité dans la mise en forme permettant la fabrication de pièces aux formes compliquées avec une plus grande précision. Cela est dû aux caractéristiques particulières des « métaux amorphes » qui peuvent se ramollir tout en restant amorphes durant un certain temps dans un intervalle de température [Tg - Tx] donné propre à chaque alliage (par exemple pour l'alliage à base de Zr : Tg=440°C et Tx=520°C). Il est ainsi possible de les mettre en forme sous une contrainte relativement faible et à une température peu élevée permettant alors l'utilisation d'un procédé simplifié tel que le formage à chaud. L'utilisation d'un tel matériau permet en outre de reproduire très précisément des géométries fines car la viscosité de l'alliage diminue fortement en fonction de la température dans l'intervalle de température [Tg - Tx] et l'alliage épouse ainsi tous les détails du négatif. Par exemple, pour un matériau à base de platine tel que défini ci-dessous, la mise en forme se fait aux alentours de 300°C pour une viscosité atteignant 103 Pa.s pour une contrainte de 1MPa, au lieu d'une viscosité de 1012 Pa.s à la température Tg. L'utilisation de matrices a pour avantage la création de pièces en trois dimensions de grande précision, ce que le découpage ou l'étampage ne permettent pas d'obtenir.Indeed, a metal alloy capable of being in an at least partially amorphous form when heated allows great ease in shaping allowing the manufacture of parts with complicated shapes with greater precision. This is due to particular characteristics of "amorphous metals" which can soften while remaining amorphous for a certain time in a given temperature interval [Tg - Tx] specific to each alloy (for example for the alloy based on Zr: Tg = 440 ° C and Tx = 520 ° C). It is thus possible to shape them under a relatively low stress and at a low temperature, then allowing the use of a simplified process such as hot forming. The use of such a material also makes it possible to reproduce very precisely fine geometries because the viscosity of the alloy decreases sharply as a function of the temperature in the temperature interval [Tg - Tx] and the alloy thus follows all the details of the negative. For example, for a platinum-based material as defined below, the shaping takes place around 300 ° C for a viscosity reaching 10 3 Pa.s for a stress of 1 MPa, instead of a viscosity of 10 12 Pa.s at temperature Tg. The advantage of using dies is the creation of three-dimensional parts with great precision, which cutting or stamping cannot achieve.

Un procédé utilisé avantageusement est le formage à chaud d'une préforme amorphe. Cette préforme est obtenue par fusion dans un four des éléments métalliques destinés à constituer l'alliage métallique. Cette fusion est faite sous atmosphère contrôlée avec pour but d'obtenir une contamination de l'alliage en oxygène aussi faible que possible. Une fois ces éléments fondus, ils sont coulés sous forme de produit semi-fini, puis refroidis rapidement afin de conserver l'état partiellement ou totalement amorphe. Une fois la préforme réalisée, le formage à chaud est effectué dans le but d'obtenir une pièce définitive. Ce formage à chaud est réalisé par pressage dans une gamme de température comprise entre la température de transition vitreuse Tg et la température de cristallisation Tx de l'alliage métallique durant un temps déterminé pour conserver une structure au moins partiellement amorphe. Ceci est fait dans le but de conserver les propriétés élastiques caractéristiques des métaux amorphes.One process advantageously used is the hot forming of an amorphous preform. This preform is obtained by melting in a furnace the metallic elements intended to constitute the metallic alloy. This melting is carried out under a controlled atmosphere with the aim of obtaining as low a contamination of the oxygen alloy as possible. Once these elements are melted, they are cast in the form of a semi-finished product, then cooled rapidly in order to maintain the partially or completely amorphous state. Once the preform has been produced, the hot forming is carried out in order to obtain a final part. This hot forming is carried out by pressing in a temperature range between the glass transition temperature Tg and the crystallization temperature Tx of the metal alloy for a determined time to maintain an at least partially amorphous structure. This is done in order to maintain the elastic properties characteristic of amorphous metals.

Typiquement pour l'alliage à base de Zr et pour une température de 440°C, le temps de pressage ne devra pas dépasser 120 secondes environ. Ainsi, le formage à chaud permet de conserver l'état amorphe initial de la préforme. Les différentes étapes de mise en forme définitive du balancier monobloc selon l'invention sont alors :

  1. 1) chauffage des matrices ayant la forme négative du balancier jusqu'à une température choisie
  2. 2) introduction de la préforme en métal amorphe entre les matrices chaudes,
  3. 3) application d'une force de fermeture sur les matrices afin de répliquer la géométrie de ces dernières sur la préforme en métal amorphe,
  4. 4) attente durant un temps maximal choisi,
  5. 5) ouverture des matrices,
  6. 6) refroidissement du balancier, et
  7. 7) sortie du balancier des matrices.
Typically for the Zr-based alloy and for a temperature of 440 ° C, the pressing time should not exceed approximately 120 seconds. Thus, hot forming makes it possible to retain the initial amorphous state of the preform. The various stages of final shaping of the monobloc balance according to the invention are then:
  1. 1) heating of the dies having the negative shape of the balance to a selected temperature
  2. 2) introduction of the amorphous metal preform between the hot dies,
  3. 3) application of a closing force on the dies in order to replicate the geometry of the latter on the amorphous metal preform,
  4. 4) waiting for a selected maximum time,
  5. 5) opening of the dies,
  6. 6) cooling of the balance, and
  7. 7) exit of the die balance.

Bien entendu, le balancier peut être aussi réalisé par coulée ou par injection. Ce procédé consiste à couler ou injecter l'alliage métallique chauffé à une température comprise entre sa température de transition vitreuse et sa température de cristallisation pour être au moins partiellement amorphe dans un moule possédant la forme de la pièce définitive.Of course, the balance can also be produced by casting or by injection. This process consists in casting or injecting the metal alloy heated to a temperature between its glass transition temperature and its crystallization temperature so as to be at least partially amorphous in a mold having the shape of the final part.

Le moule peut être réutilisé ou dissout pour libérer les pièces. Le procédé par moulage présente l'avantage de répliquer parfaitement la géométrie du balancier, y compris d'éventuels décors ou structuration de surface. On obtient une moins grande dispersion d'inertie et un meilleur centrage sur un lot de production de balanciers. Le procédé par moulage permet d'obtenir un balancier à la géométrie esthétique, avec des angles intérieurs vifs, un profil de serge et/ou de bras bombé, et une finition parfaite. Il est également possible de prévoir une serge non continue. Pour une qualité maximale, le moule sera réalisé dans du silicium par un procédé DRIE. Il est bien évident que le moule peut également être réalisé par usinage par fraisage, laser, électroérosion ou tout autre type d'usinage.The mold can be reused or dissolved to release the parts. The molding process has the advantage of perfectly replicating the geometry of the balance, including any decorations or surface structuring. This results in less dispersion of inertia and better centering on a production batch of balances. The molding process makes it possible to obtain a balance with an aesthetic geometry, with sharp interior angles, a serge profile and / or domed arm, and a perfect finish. It is also possible to provide a non-continuous serge. For maximum quality, the mold will be made in silicon by a DRIE process. It is obvious that the mold can also be produced by machining by milling, laser, electroerosion or any other type of machining.

Les propriétés élastiques caractéristiques des métaux amorphes sont utilisées pour surmouler ou intégrer des éléments fonctionnels et/ou décoratifs dans la serge et/ou au niveau des bras et/ou au niveau du moyeu par exemple au moyen d'inserts correspondants placés dans le moule avant l'introduction de l'alliage métallique chauffé entre sa température de transition vitreuse et sa température de cristallisation pour être au moins partiellement amorphe.The elastic properties characteristic of amorphous metals are used to overmold or integrate functional and / or decorative elements in the rim and / or at the level of the arms and / or at the level of the hub, for example by means of corresponding inserts placed in the front mold. the introduction of the metal alloy heated between its glass transition temperature and its crystallization temperature to be at least partially amorphous.

Indépendamment du premier ou second modes de réalisation des procédés de l'invention, la serge 2 peut comprendre des logements 12 destinés à recevoir des deuxièmes éléments de réglage de l'inertie et/ou de balourd 14, 15 comme représenté sur la figure 3. Ces logements 12 peuvent avantageusement être prévus lors de la fabrication du balancier 1 par moulage, conformément aux procédés de l'invention. Les deuxièmes éléments de réglage de l'inertie et/ou de balourd 14, 15 peuvent être par exemple des masselottes, des masselottes fendues, des goupilles 14, des goupilles fendues, ou des goupilles avec balourd 15, qui font office de masselottes. Ces éléments sont chassés ou clippés dans les logements correspondants 12. Sur la figure 3 sont représentées une goupille 14 insérée dans son logement 12, ainsi qu'une goupille avec balourd 15 insérée dans son logement 12. La figure 4 montre une vue en coupe selon la ligne A-A de la figure 3 représentant la goupille avec balourd 15 insérée dans le logement 12 prévu dans la serge 2.Independently of the first or second embodiments of the methods of the invention, the rim 2 can comprise housings 12 intended to receive second elements for adjusting the inertia and / or unbalance 14, as shown in FIG. figure 3 . These housings 12 can advantageously be provided during the manufacture of the balance 1 by molding, in accordance with the methods of the invention. The second inertia and / or unbalance adjustment elements 14, 15 can be, for example, weights, slotted weights, pins 14, split pins, or pins with unbalance 15, which act as weights. These elements are driven out or clipped into the corresponding housings 12. On the figure 3 are shown a pin 14 inserted in its housing 12, as well as a pin with unbalance 15 inserted in its housing 12. The figure 4 shows a sectional view along line AA of the figure 3 showing the pin with unbalance 15 inserted in the housing 12 provided in the rim 2.

Il est bien évident que ces éléments pour augmenter l'inertie du balancier sont utilisés préférentiellement avec une serge réalisée dans un matériau de faible densité, tel que le titane ou le zirconium mais peuvent être aussi utilisés avec une serge dans un autre matériau.It is obvious that these elements for increasing the inertia of the balance are preferably used with a rim made of a low density material, such as titanium or zirconium, but can also be used with a rim made of another material.

Pour augmenter l'inertie du balancier, il est également possible de prévoir une serge plus épaisse ou plus large, notamment dans le cas de balanciers plus grands.To increase the inertia of the balance, it is also possible to provide a thicker or wider rim, in particular in the case of larger balance wheels.

Les logements 12 représentés sur la figure 3 peuvent également constituer des logements destinés à recevoir des éléments esthétiques et/ ou luminescents, tels que des tubes de tritium (non représentés), ou des capsules de matériaux phosphorescents (du type Superluminova, par exemple) ou fluorescents.The 12 units shown on the figure 3 can also constitute housings intended to receive aesthetic and / or luminescent elements, such as tritium tubes (not shown), or capsules of phosphorescent materials (of the Superluminova type, for example) or fluorescent.

Selon une autre variante de l'invention, l'un ou l'autre des procédés comprend une étape de surmoulage d'éléments de centrage flexibles 16, 17 sur le moyeu 4, sur son pourtour intérieur ou à sa surface. Ainsi, le moyeu 4 peut comprendre des éléments de centrage flexibles intégrés, qui permettent un auto-centrage du balancier lors de son montage sur un axe grâce à la déformation élastique desdits éléments de centrage flexibles.According to another variant of the invention, one or the other of the methods comprises a step of overmolding flexible centering elements 16, 17 on the hub 4, on its inner periphery or on its surface. Thus, the hub 4 can include integrated flexible centering elements, which allow self-centering of the balance when it is mounted on an axis by virtue of the elastic deformation of said flexible centering elements.

Selon la figure 5, lesdits éléments de centrage flexibles intégrés 16 sont des lames élastiques prévues sur le pourtour intérieur du moyeu 4 de manière à être positionnées dans le trou 6.According to figure 5 , said integrated flexible centering elements 16 are elastic blades provided on the inner periphery of the hub 4 so as to be positioned in the hole 6.

Selon la figure 6, lesdits éléments de centrage flexibles intégrés 17 sont prévus sur la surface du moyeu 4 et sont répartis autour du trou 6. Les éléments de centrage flexibles 16 et 17 peuvent avantageusement être mis en place lors de la fabrication du balancier 1 par moulage, conformément aux procédés de l'invention.According to figure 6 , said integrated flexible centering elements 17 are provided on the surface of the hub 4 and are distributed around the hole 6. The flexible centering elements 16 and 17 can advantageously be put in place during the manufacture of the balance 1 by molding, in accordance with methods of the invention.

Selon une autre variante de l'invention, l'un ou l'autre des procédés comprend une étape de surmoulage de troisièmes éléments de réglage de l'inertie 19, 20, 22a, 22b flexibles dans le bras 8. Ainsi, au moins l'un des bras 8 porte des troisièmes éléments de réglage de l'inertie flexibles intégrés.According to another variant of the invention, one or the other of the methods comprises a step of overmolding third flexible inertia adjustment elements 19, 20, 22a, 22b in the arm 8. Thus, at least l one of the arms 8 carries integrated flexible third inertia adjustment elements.

Selon la figure 7, l'extrémité du bras 8 du côté de la serge 2 se termine en deux branches 8a, 8b formant entre elles un logement 18 dans lequel est intégré un troisième élément de réglage de l'inertie 19 flexible bistable en « V » pour le réglage de la fréquence.According to figure 7 , the end of the arm 8 on the side of the rim 2 ends in two branches 8a, 8b forming between them a housing 18 in which is integrated a third element for adjusting the inertia 19 flexible bistable "V" for the adjustment frequency.

Selon la figure 8, il est prévu dans le logement 18 un troisième élément de réglage de l'inertie 20 flexible en flambage pour le réglage de la fréquence. A cet effet, le troisième élément de réglage de l'inertie 20 est réalisé dans un matériau présentant des propriétés de dilatation différentes de l'alliage métallique du balancier de l'invention, tel que le silicium ou l'oxyde de silicium.According to figure 8 , there is provided in the housing 18 a third element 20 for adjusting the inertia 20 flexible in buckling for adjusting the frequency. For this purpose, the third inertia adjustment element 20 is made of a material having expansion properties different from the metal alloy of the balance of the invention, such as silicon or silicon oxide.

Selon la figure 9, l'extrémité du bras 8 du côté de la serge 2 se termine en trois branches 8a, 8b, 8c formant entre elles deux logements 18a, 18b dans lesquels sont intégrés des troisièmes éléments de réglage de l'inertie 22a, 22b flexibles multi-stables à cliquet pour le réglage de la fréquence.According to figure 9 , the end of the arm 8 on the side of the rim 2 ends in three branches 8a, 8b, 8c forming between them two housings 18a, 18b in which are integrated third elements for adjusting the inertia 22a, 22b flexible multi- stable ratchet for frequency adjustment.

Ces troisièmes éléments de réglage de l'inertie flexibles 19, 20, 22a, 22b pour le réglage de la fréquence peuvent avantageusement être mis en place lors de la fabrication du balancier 1 par moulage, conformément aux procédés de l'invention.These third flexible inertia adjustment elements 19, 20, 22a, 22b for adjusting the frequency can advantageously be put in place during the manufacture of the balance 1 by molding, in accordance with the methods of the invention.

Ces troisièmes éléments de réglage de l'inertie flexibles 19, 20, 22a, 22b pour le réglage de la fréquence peuvent être aussi bien utilisés lorsque l'ensemble du balancier est dans un même alliage métallique que lorsque les bras sont en alliage métallique, le reste du balancier, et notamment la serge, étant dans un autre matériau.These third flexible inertia adjustment elements 19, 20, 22a, 22b for frequency adjustment can be used as well when the entire balance wheel is in the same metal alloy as when the arms are in metal alloy, the rest of the balance, and in particular the serge, being in another material.

Selon une autre variante de l'invention, on utilise dans l'un ou l'autre des procédés de l'invention un moule présentant des microstructures formant un décor ou un réseau photonique. Ainsi, l'un du bras 8, de la serge 2 et du moyeu 4 présente un état de surface structuré. Seul l'un des éléments peut présenter un état de surface structuré ou tous les éléments du balancier peuvent présenter un état de surface structuré, cet état de surface structuré pouvant être identique ou différent. La figure 10 représente un balancier de l'invention pour lequel la serge 2 présente un état de surface structuré différent de l'état de surface structuré présenté par le bras 8. Cet état de surface structuré peut être un état poli, satiné, sablé, perlé, ensoleillé, etc. Il est possible de prévoir également dans le moule pour la fabrication du balancier des microstructures formant un réseau photonique afin de répliquer ces microstructures à la surface du balancier. Ces microstructures peuvent permettre de créer un cristal photonique donnant à la pièce une certaine couleur, un hologramme, ou un réseau de diffraction pouvant constituer un élément anti-contrefaçon. Les structures sont directement introduites dans le moule, et sont répliquées lors de la fabrication des balanciers par formage à chaud, ce qui ne nécessite plus d'opérations de terminaison. Il est également possible d'ajouter un logo au moule.According to another variant of the invention, one or the other of the methods of the invention is used a mold having microstructures forming a decoration or a photonic network. Thus, one of the arm 8, of the rim 2 and of the hub 4 has a structured surface condition. Only one of the elements can have a structured surface condition or all the elements of the balance can have a structured surface condition, this structured surface condition may be the same or different. The figure 10 shows a balance of the invention for which the serge 2 has a structured surface condition different from the structured surface condition presented by the arm 8. This structured surface condition can be a polished, satin, sandblasted, pearl, sunny condition. , etc. It is also possible to provide in the mold for the manufacture of the balance, microstructures forming a photonic network in order to replicate these microstructures on the surface of the balance. These microstructures can make it possible to create a photonic crystal giving the part a certain color, a hologram, or a diffraction grating which can constitute an anti-counterfeiting element. The structures are introduced directly into the mold, and are replicated during the manufacture of the balances by hot forming, which no longer requires termination operations. It is also possible to add a logo to the mold.

L'alliage métallique utilisé dans les procédés de l'invention présente un coefficient de dilatation thermique typiquement inférieur à 25 ppm/°C et supérieur à 7 ppm/°C, et est capable d'être sous une forme au moins partiellement amorphe lorsqu'il est chauffé à une température comprise entre sa température de transition vitreuse et sa température de cristallisation.The metal alloy used in the processes of the invention exhibits a coefficient of thermal expansion typically less than 25 ppm / ° C and greater than 7 ppm / ° C, and is capable of being in at least partially amorphous form when it is heated to a temperature between its glass transition temperature and its crystallization temperature.

De préférence, l'alliage métallique utilisé dans les procédés de l'invention est à base d'un élément choisi parmi le groupe constitué du platine, du zirconium, du titane, du palladium, du nickel, de l'aluminium et du fer.Preferably, the metal alloy used in the methods of the invention is based on an element chosen from the group consisting of platinum, zirconium, titanium, palladium, nickel, aluminum and iron.

Dans la présente description, l'expression « à base d'un élément » signifie que ledit alliage métallique contient au moins 50% en poids dudit élément.In the present description, the expression “based on an element” means that said metal alloy contains at least 50% by weight of said element.

Ledit alliage métallique utilisé dans la présente invention peut être à base de platine et présente un coefficient de dilatation thermique inférieur 12 ppm/°C, de préférence compris entre 8 ppm/°C et 12 ppm/°C.Said metal alloy used in the present invention may be based on platinum and has a coefficient of thermal expansion of less than 12 ppm / ° C, preferably between 8 ppm / ° C and 12 ppm / ° C.

Un tel alliage métallique à base de platine peut être constitué, en valeurs en % atomique, de :

  • une base de platine dont la teneur constitue la balance,
  • 13 à 17% de cuivre,
  • 3 à 7% de nickel,
  • 20 à 25% de phosphore.
Such a platinum-based metal alloy can consist, in atomic% values, of:
  • a platinum base whose content constitutes the balance,
  • 13 to 17% copper,
  • 3 to 7% nickel,
  • 20 to 25% phosphorus.

L'alliage métallique utilisé dans la présente invention peut aussi être à base de zirconium et présente un coefficient de dilatation thermique inférieur 12 ppm/°C, de préférence compris entre 8 ppm/°C et 11 ppm/°C.The metal alloy used in the present invention can also be based on zirconium and has a coefficient of thermal expansion of less than 12 ppm / ° C, preferably between 8 ppm / ° C and 11 ppm / ° C.

Un tel alliage métallique à base de zirconium peut être constitué, en valeurs en % atomique, de :

  • une base de zirconium dont la teneur constitue la balance,
  • 14 à 20% de cuivre,
  • 12 à 13% de nickel,
  • 9 à 11% d'aluminium,
  • 2 à 4 % de niobium.
Such a metal alloy based on zirconium can consist, in atomic% values, of:
  • a zirconium base, the content of which constitutes the balance,
  • 14 to 20% copper,
  • 12 to 13% nickel,
  • 9 to 11% aluminum,
  • 2-4% niobium.

L'alliage métallique utilisé dans la présente invention peut aussi être à base de palladium et présente un coefficient de dilatation thermique inférieur à 20 ppm/°C, de préférence compris entre 13 ppm/°C et 18 ppm/°C.The metal alloy used in the present invention can also be based on palladium and has a coefficient of thermal expansion of less than 20 ppm / ° C, preferably between 13 ppm / ° C and 18 ppm / ° C.

Un tel alliage métallique à base de palladium peut être constitué, en valeurs en % atomique, de :

  • une base de palladium, dont la teneur constitue la balance,
  • 25 à 30% de cuivre,
  • 8 à 12% de nickel,
  • 18 à 22% de phosphore.
Such a palladium-based metal alloy can consist, in atomic% values, of:
  • a palladium base, the content of which constitutes the balance,
  • 25 to 30% copper,
  • 8 to 12% nickel,
  • 18 to 22% phosphorus.

Idéalement, les alliages utilisés dans l'invention ne contiennent aucune impureté. Toutefois, ils peuvent comprendre des traces d'impuretés qui peuvent résulter, de manière souvent inévitable, de l'élaboration desdits alliages.Ideally, the alloys used in the invention do not contain any impurities. However, they may include traces of impurities which can result, often inevitably, from the production of said alloys.

Lorsque les alliages utilisés dans la présente invention présentent un coefficient de dilatation thermique inférieur à 12 ppm/°C et supérieur à 8 ppm/°C, ils peuvent être utilisés pour réaliser au moins une partie d'un balancier qui sera appairé à un spiral de préférence en quartz monocristallin. Les alliages utilisés dans la présente invention présentant un coefficient de dilatation thermique inférieur à 20 ppm/°C et supérieur à 13 ppm/°C peuvent être utilisés pour réaliser au moins une partie d'un balancier qui sera appairé à un spiral en métal ou en silicium.When the alloys used in the present invention have a thermal expansion coefficient of less than 12 ppm / ° C and greater than 8 ppm / ° C, they can be used to make at least part of a balance which will be paired with a hairspring. preferably monocrystalline quartz. The alloys used in the present invention having a thermal expansion coefficient of less than 20 ppm / ° C and greater than 13 ppm / ° C can be used to make at least part of a balance which will be paired with a metal hairspring or silicon.

Plus préférentiellement, ledit alliage métallique utilisé dans la présente invention à base de platine est constitué, en valeurs en % atomique, de : 57.5% Pt, 14.7% Cu, 5.3% Ni, 22.5% P. Un tel alliage présente un coefficient de dilatation thermique compris entre 11 et 12 ppm/°C.More preferably, said metal alloy used in the present invention based on platinum consists, in atomic% values, of: 57.5% Pt, 14.7% Cu, 5.3% Ni, 22.5% P. Such an alloy has an expansion coefficient thermal between 11 and 12 ppm / ° C.

Plus préférentiellement, ledit alliage métallique utilisé dans la présente invention à base de zirconium est constitué, en valeurs en % atomique, de : 58.5% Zr, 15.6% Cu, 12.8% Ni, 10.3% Al, 2.8% Nb. Un tel alliage présente un coefficient de dilatation thermique compris entre 10.5 et 11 ppm/°C.More preferably, said metal alloy used in the present invention based on zirconium consists, in atomic% values, of: 58.5% Zr, 15.6% Cu, 12.8% Ni, 10.3% Al, 2.8% Nb. Such an alloy has a thermal expansion coefficient of between 10.5 and 11 ppm / ° C.

Plus préférentiellement, ledit alliage métallique utilisé dans la présente invention à base de palladium est constitué, en valeurs en % atomique, de : 43% Pd, 27% Cu, 10% Ni, 20% P. Un tel alliage présente un coefficient de dilatation thermique compris entre 15 et 16 ppm/°C.More preferably, said metal alloy used in the present invention based on palladium consists, in atomic% values, of: 43% Pd, 27% Cu, 10% Ni, 20% P. Such an alloy has an expansion coefficient temperature between 15 and 16 ppm / ° C.

Ainsi, le balancier selon l'invention est réalisé dans un matériau permettant d'utiliser un procédé de fabrication simple tout en présentant un coefficient de dilatation thermique permettant de l'appairer à un spiral en quartz monocristallin, et/ou en métal ou en silicium, de préférence en quartz monocristallin. Le balancier selon l'invention permet également d'avoir au moins des bras présentant un coefficient de dilatation thermique permettant de l'appairer à un spiral en quartz monocristallin, et/ou en métal ou en silicium, tout en ayant une grande inertie en gardant une géométrie de serge compacte et esthétique, de petit volume, à l'aide d'une serge adéquate, soit comprenant des éléments réalisés dans un matériau de plus grande densité, soit étant elle-même réalisée dans un matériau de plus grande densité.Thus, the balance according to the invention is made of a material making it possible to use a simple manufacturing process while having a thermal expansion coefficient allowing it to be paired with a monocrystalline quartz hairspring, and / or in metal or silicon. , preferably monocrystalline quartz. The balance according to the invention also makes it possible to have at least arms having a coefficient of thermal expansion making it possible to pair it with a monocrystalline quartz hairspring, and / or in metal or in silicon, while having great inertia while keeping a compact and aesthetic serge geometry, of small volume, using an adequate serge, either comprising elements made of a material of greater density, or being itself made of a higher density material.

Claims (15)

Procédé de fabrication d'un balancier (1) pour pièce d'horlogerie comprenant une serge (2), un moyeu (4) et au moins un bras (8) reliant le moyeu (4) à ladite serge (2), la serge (2), le moyeu (4) et le bras (8) étant réalisés dans un alliage métallique, ledit procédé comprenant les étapes suivantes: a) réaliser un moule ayant la forme négative du balancier (1) ; b) se munir d'un alliage métallique présentant un coefficient de dilatation thermique inférieur à 25 ppm/°C et capable d'être sous une forme au moins partiellement amorphe lorsqu'il est chauffé à une température comprise entre sa température de transition vitreuse et sa température de cristallisation ; c) introduire dans le moule l'alliage métallique, ledit alliage métallique étant chauffé à une température comprise entre sa température de transition vitreuse et sa température de cristallisation pour être formé à chaud et former un balancier ; d) refroidir ledit alliage métallique pour obtenir un balancier (1) dans ledit alliage métallique ; e) libérer le balancier (1) obtenu à l'étape d) de son moule ; le procédé étant caractérisé en ce qu'il comprend une étape de surmoulage d'éléments de centrage flexibles (16, 17) sur le moyeu (4).Method of manufacturing a balance (1) for a timepiece comprising a rim (2), a hub (4) and at least one arm (8) connecting the hub (4) to said rim (2), the rim (2), the hub (4) and the arm (8) being made of a metal alloy, said method comprising the following steps: a) making a mold having the negative shape of the balance (1); b) be provided with a metal alloy having a thermal expansion coefficient of less than 25 ppm / ° C and capable of being in an at least partially amorphous form when it is heated to a temperature between its glass transition temperature and its crystallization temperature; c) introducing the metal alloy into the mold, said metal alloy being heated to a temperature between its glass transition temperature and its crystallization temperature in order to be hot formed and to form a balance; d) cooling said metal alloy to obtain a balance (1) in said metal alloy; e) releasing the balance (1) obtained in step d) from its mold; the method being characterized in that it comprises a step of overmolding flexible centering elements (16, 17) on the hub (4). Procédé selon la revendication précédente, caractérisé en ce qu'il comprend une étape de surmoulage de premiers éléments de réglage de l'inertie (10) dans la serge (2), lesdits premiers éléments de réglage de l'inertie (10) étant réalisés dans un premier matériau présentant une masse volumique supérieure à la masse volumique dudit alliage métallique.Method according to the preceding claim, characterized in that it comprises a step of overmolding first inertia adjusting elements (10) in the rim (2), said first inertia adjusting elements (10) being produced in a first material having a density greater than the density of said metal alloy. Procédé de fabrication d'un balancier pour pièce d'horlogerie comprenant une serge (2), un moyeu (4) et au moins un bras (8) reliant le moyeu (4) à ladite serge (2), le moyeu (4) et le bras (8) étant réalisés dans un alliage métallique, et la serge (2) étant réalisée dans un second matériau présentant une masse volumique supérieure à la masse volumique dudit alliage métallique dans lequel le moyeu (4) et le bras (8) sont réalisés, ledit procédé comprenant les étapes suivantes : a) réaliser un moule ayant la forme négative du balancier ; a') insérer dans le moule une serge ou des éléments de serge réalisés dans un matériau présentant une masse volumique supérieure à la masse volumique dudit alliage métallique b) se munir d'un alliage métallique présentant un coefficient de dilatation thermique inférieur à 25 ppm/°C et capable d'être sous une forme au moins partiellement amorphe lorsqu'il est chauffé à une température comprise entre sa température de transition vitreuse et sa température de cristallisation c) introduire dans le moule l'alliage métallique, ledit alliage métallique étant chauffé à une température comprise entre sa température de transition vitreuse et sa température de cristallisation pour être formé à chaud et surmouler la serge ou les éléments de serge pour former un balancier avec inserts d) refroidir ledit alliage métallique pour obtenir un balancier avec inserts e) libérer le balancier obtenu à l'étape d) de son moule ; le procédé étant caractérisé en ce qu'il comprend une étape de surmoulage d'éléments de centrage flexibles (16, 17) sur le moyeu (4).Method of manufacturing a balance for a timepiece comprising a rim (2), a hub (4) and at least one arm (8) connecting the hub (4) to said rim (2), the hub (4) and the arm (8) being made of a metal alloy, and the rim (2) being made of a second material having a density greater than the density of said metal alloy in which the hub (4) and the arm (8) are made, said method comprising the following steps: a) making a mold having the negative shape of the balance; a ') inserting into the mold a serge or serge elements made of a material having a density greater than the density of said metal alloy b) be provided with a metal alloy having a thermal expansion coefficient of less than 25 ppm / ° C and capable of being in an at least partially amorphous form when it is heated to a temperature between its glass transition temperature and its crystallization temperature c) introducing the metal alloy into the mold, said metal alloy being heated to a temperature between its glass transition temperature and its crystallization temperature in order to be hot-formed and overmold the serge or the serge elements to form a balance with inserts d) cooling said metal alloy to obtain a balance with inserts e) releasing the balance obtained in step d) from its mold; the method being characterized in that it comprises a step of overmolding flexible centering elements (16, 17) on the hub (4). Procédé selon l'une des revendications précédentes, caractérisé en ce que la serge (2) comprend des logements (12) destinés à recevoir des deuxièmes éléments de réglage de l'inertie et/ou de balourd (14, 15).Method according to one of the preceding claims, characterized in that the rim (2) comprises housings (12) intended to receive second elements for adjusting the inertia and / or unbalance (14, 15). Procédé selon l'une des revendications précédentes, caractérisé en ce que la serge (2) comprend des logements (12) destinés à recevoir des éléments décoratifs et/ou luminescents.Method according to one of the preceding claims, characterized in that the serge (2) comprises housings (12) intended to receive decorative and / or luminescent elements. Procédé selon l'une des revendication précédentes, caractérisé en ce que lesdits éléments de centrage flexibles (16) intégrés sont prévus sur le pourtour intérieur du moyeu (4).Method according to one of the preceding claims, characterized in that said integrated flexible centering elements (16) are provided on the inner periphery of the hub (4). Procédé selon l'une des revendications précédentes, caractérisé en ce qu'il comprend une étape de surmoulage de troisièmes éléments de réglage de l'inertie (19, 20, 22a, 22b) flexibles dans le bras (8).Method according to one of the preceding claims, characterized in that it comprises a step of overmolding third flexible inertia adjustment elements (19, 20, 22a, 22b) in the arm (8). Procédé selon l'une des revendications précédentes, caractérisé en ce que le moule présente des microstructures formant un décor ou un réseau photonique.Method according to one of the preceding claims, characterized in that the mold has microstructures forming a decoration or a photonic network. Procédé selon l'une des revendications précédentes, caractérisé en ce que ledit alliage métallique est à base d'un élément choisi parmi le groupe constitué du platine, du zirconium, du titane, du palladium, du nickel, de l'aluminium et du fer.Process according to one of the preceding claims, characterized in that the said metal alloy is based on an element chosen from the group consisting of platinum, zirconium, titanium, palladium, nickel, aluminum and iron . Procédé selon l'une des revendications précédentes, caractérisé en ce que ledit alliage métallique est à base de platine et présente un coefficient de dilatation thermique inférieur 12 ppm/°C, de préférence compris entre 8 ppm/°C et 12 ppm/°C.Process according to one of the preceding claims, characterized in that the said metal alloy is based on platinum and has a thermal expansion coefficient of less than 12 ppm / ° C, preferably between 8 ppm / ° C and 12 ppm / ° C . Procédé selon la revendication 10, caractérisé en ce que l'alliage métallique à base de platine est constitué, en valeurs en % atomique, de : - une base de platine dont la teneur constitue la balance, - 13 à 17% de cuivre, - 3 à 7% de nickel, - 20 à 25% de phosphore. Process according to Claim 10, characterized in that the platinum-based metal alloy consists, in atomic% values, of: - a platinum base whose content constitutes the balance, - 13 to 17% copper, - 3 to 7% nickel, - 20 to 25% phosphorus. Procédé selon l'une des revendications 1 à 9, caractérisé en ce que ledit alliage métallique est à base de zirconium et présente un coefficient de dilatation thermique inférieur 12 ppm/°C, de préférence compris entre 8 ppm/°C et 11 ppm/°C.Process according to one of Claims 1 to 9, characterized in that the said metal alloy is based on zirconium and has a coefficient thermal expansion less than 12 ppm / ° C, preferably between 8 ppm / ° C and 11 ppm / ° C. Procédé selon la revendication 12, caractérisé en ce que l'alliage métallique à base de zirconium est constitué, en valeurs en % atomique, de : - une base de zirconium dont la teneur constitue la balance, - 14 à 20% de cuivre, - 12 à 13% de nickel, - 9 à 11% d'aluminium, - 2 à 4 % de niobium. Process according to Claim 12, characterized in that the metal alloy based on zirconium consists, in atomic% values, of: - a zirconium base, the content of which constitutes the balance, - 14 to 20% copper, - 12 to 13% nickel, - 9 to 11% aluminum, - 2 to 4% niobium. Procédé selon l'une des revendications 1 à 9, caractérisé en ce que ledit alliage métallique est à base de palladium et présente un coefficient de dilatation thermique inférieur à 20 ppm/°C, de préférence compris entre 13 ppm/°C et 18 ppm/°C.Process according to one of Claims 1 to 9, characterized in that the said metal alloy is based on palladium and has a thermal expansion coefficient of less than 20 ppm / ° C, preferably between 13 ppm / ° C and 18 ppm / ° C. Procédé selon la revendication 14, caractérisé en ce que l'alliage métallique à base de palladium est constitué, en valeurs en % atomique, de - une base de palladium, dont la teneur constitue la balance, - 25 à 30% de cuivre, - 8 à 12% de nickel, - 18 à 22% de phosphore. Process according to Claim 14, characterized in that the metal alloy based on palladium consists, in atomic% values, of - a palladium base, the content of which constitutes the balance, - 25 to 30% copper, - 8 to 12% nickel, - 18 to 22% phosphorus.
EP20201790.1A 2017-12-22 2017-12-22 Method for manufacturing a balance for a timepiece Active EP3796102B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP20201790.1A EP3796102B1 (en) 2017-12-22 2017-12-22 Method for manufacturing a balance for a timepiece

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP20201790.1A EP3796102B1 (en) 2017-12-22 2017-12-22 Method for manufacturing a balance for a timepiece
EP17210299.8A EP3502787B1 (en) 2017-12-22 2017-12-22 Method for manufacturing a balance for a timepiece

Related Parent Applications (2)

Application Number Title Priority Date Filing Date
EP17210299.8A Division EP3502787B1 (en) 2017-12-22 2017-12-22 Method for manufacturing a balance for a timepiece
EP17210299.8A Division-Into EP3502787B1 (en) 2017-12-22 2017-12-22 Method for manufacturing a balance for a timepiece

Publications (2)

Publication Number Publication Date
EP3796102A1 true EP3796102A1 (en) 2021-03-24
EP3796102B1 EP3796102B1 (en) 2022-04-20

Family

ID=60811893

Family Applications (2)

Application Number Title Priority Date Filing Date
EP17210299.8A Active EP3502787B1 (en) 2017-12-22 2017-12-22 Method for manufacturing a balance for a timepiece
EP20201790.1A Active EP3796102B1 (en) 2017-12-22 2017-12-22 Method for manufacturing a balance for a timepiece

Family Applications Before (1)

Application Number Title Priority Date Filing Date
EP17210299.8A Active EP3502787B1 (en) 2017-12-22 2017-12-22 Method for manufacturing a balance for a timepiece

Country Status (4)

Country Link
US (2) US11307535B2 (en)
EP (2) EP3502787B1 (en)
JP (1) JP6770049B2 (en)
CN (2) CN109960137B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3796101A1 (en) * 2019-09-20 2021-03-24 Nivarox-FAR S.A. Hairspring for clock movement
CH716669B1 (en) * 2019-10-03 2023-02-15 Richemont Int Sa Method of manufacturing a balance pivot shaft.
CN115537598B (en) * 2022-10-10 2023-06-20 东莞理工学院 Wide-temperature-range adjustable linear low-thermal-expansion titanium-niobium alloy and preparation method thereof
CN115537599B (en) * 2022-10-13 2023-06-06 东莞理工学院 Titanium-niobium alloy with high elastic modulus and near-zero linear expansion coefficient and preparation method thereof

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2395402A1 (en) * 2010-06-11 2011-12-14 Montres Breguet SA High frequency balance wheel for timepiece
EP2703909A1 (en) * 2012-09-04 2014-03-05 The Swatch Group Research and Development Ltd. Paired balance wheel - hairspring resonator
EP3170579A1 (en) 2015-11-18 2017-05-24 The Swatch Group Research and Development Ltd. Method for manufacturing a part from amorphous metal

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US387973A (en) * 1887-12-02 1888-08-14 Watch-balance
CH621669GA3 (en) * 1977-12-23 1981-02-27 Method of manufacturing a pivoted clockwork balance and clockwork balance obtained according to this method
EP1258786B1 (en) * 2001-05-18 2008-02-20 Rolex Sa Self-compensating spring for a mechanical oscillator of balance-spring type
WO2004030848A1 (en) * 2002-09-30 2004-04-15 Liquidmetal Technologies Investment casting of bulk-solidifying amorphous alloys
CN101589347A (en) 2006-12-21 2009-11-25 康普利计时股份有限公司 Mechanical oscillator for timepiece
EP2104008A1 (en) * 2008-03-20 2009-09-23 Nivarox-FAR S.A. Single-body regulating organ and method for manufacturing same
EP2104005A1 (en) 2008-03-20 2009-09-23 Nivarox-FAR S.A. Composite balance and method of manufacturing thereof
CH707106B1 (en) 2012-12-21 2014-04-30 Montres Tudor SA adjusting screw and watch balance wheel comprising such a screw for adjusting the inertia.
CN206178347U (en) 2015-11-13 2017-05-17 尼瓦洛克斯-法尔股份有限公司 Balance, clock cassette mechanism and clock and watch spare with inertia is adjusted
EP3182211A1 (en) 2015-12-17 2017-06-21 Nivarox-FAR S.A. Composite part with resilient means under stress
EP3217229B1 (en) 2016-03-07 2020-01-01 Montres Breguet S.A. Adjustable auxiliary thermal compensation system
EP3217228B1 (en) 2016-03-07 2019-08-28 Montres Breguet S.A. Bimetal device sensitive to temperature changes
EP3252545B1 (en) 2016-06-03 2019-10-16 The Swatch Group Research and Development Ltd. Timepiece mechanism with balance wheel inertia adjustment

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2395402A1 (en) * 2010-06-11 2011-12-14 Montres Breguet SA High frequency balance wheel for timepiece
EP2703909A1 (en) * 2012-09-04 2014-03-05 The Swatch Group Research and Development Ltd. Paired balance wheel - hairspring resonator
EP3170579A1 (en) 2015-11-18 2017-05-24 The Swatch Group Research and Development Ltd. Method for manufacturing a part from amorphous metal

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
AGILENT: "Material Expansion Coefficients", LASER AND OPTICS USER'S MANUAL, 31 December 2002 (2002-12-31), USA, XP055485562, Retrieved from the Internet <URL:https://psec.uchicago.edu/thermal_coefficients/cte_metals_05517-90143.pdf> [retrieved on 20180619] *

Also Published As

Publication number Publication date
CN109960137A (en) 2019-07-02
EP3502787A1 (en) 2019-06-26
US11640140B2 (en) 2023-05-02
US20220163923A1 (en) 2022-05-26
CN109960137B (en) 2021-04-09
US20190196408A1 (en) 2019-06-27
JP6770049B2 (en) 2020-10-14
CN112965355A (en) 2021-06-15
EP3502787B1 (en) 2020-11-18
EP3796102B1 (en) 2022-04-20
US11307535B2 (en) 2022-04-19
JP2019113533A (en) 2019-07-11

Similar Documents

Publication Publication Date Title
EP3502787B1 (en) Method for manufacturing a balance for a timepiece
EP2585876B1 (en) Escapement system for a timepiece
EP2585882B1 (en) Timepiece anti-shock system
US9329572B2 (en) Timepiece hand
EP2350746B1 (en) Method of making a bottom plate for a watch
EP2104005A1 (en) Composite balance and method of manufacturing thereof
EP2585880A1 (en) Timepiece dial feet
EP3377247B1 (en) Method for manufacturing a part from amorphous metal
WO2017016950A1 (en) Assembly of parts made of fragile material
CH714514A2 (en) Method of manufacturing a pendulum for a timepiece
WO2019120959A1 (en) Balance for timepiece and method for manufacturing such a balance
CH714512A2 (en) Pendulum for a timepiece and method of manufacturing such a pendulum.
WO2011161079A1 (en) Shock-absorbing system for a timepiece
WO2011161181A1 (en) Assembly of parts made of fragile material
EP2708372A1 (en) Writing instrument
CH703343B1 (en) Needle of timepiece.
CH719106A1 (en) Multi-metallic monolithic watchmaker or jeweler component made by sintering.
WO2023078693A1 (en) Contrasting watch component made by multi-metal printing
CH703344A2 (en) Shock absorbing bearing for balance staff of mobile of mechanical watch, has spring that is arranged to exert axial force on pivot system and is made of partially or totally amorphous material with metal element
EP4307053A1 (en) Method for manufacturing a clock component
CH711923B1 (en) Process for manufacturing a composite part with elastic means under stress, composite part and watch assortment.
CH711381A2 (en) A part comprising an amorphous metal alloy foam part and a manufacturing method.

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

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

Free format text: STATUS: THE APPLICATION HAS BEEN PUBLISHED

AC Divisional application: reference to earlier application

Ref document number: 3502787

Country of ref document: EP

Kind code of ref document: P

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 RS SE SI SK SM TR

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

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20210924

RBV Designated contracting states (corrected)

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 RS SE SI SK SM TR

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

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

Free format text: STATUS: GRANT OF PATENT IS INTENDED

RIC1 Information provided on ipc code assigned before grant

Ipc: C22C 16/00 20060101ALN20220124BHEP

Ipc: B22D 27/04 20060101ALN20220124BHEP

Ipc: B22D 25/02 20060101ALN20220124BHEP

Ipc: B22D 15/00 20060101ALN20220124BHEP

Ipc: C22C 14/00 20060101ALN20220124BHEP

Ipc: C22C 38/08 20060101ALN20220124BHEP

Ipc: C22C 21/00 20060101ALN20220124BHEP

Ipc: B22C 9/00 20060101ALN20220124BHEP

Ipc: G04B 18/00 20060101ALI20220124BHEP

Ipc: G04B 17/22 20060101AFI20220124BHEP

INTG Intention to grant announced

Effective date: 20220208

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

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

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AC Divisional application: reference to earlier application

Ref document number: 3502787

Country of ref document: EP

Kind code of ref document: P

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 RS 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: DE

Ref legal event code: R096

Ref document number: 602017056434

Country of ref document: DE

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 1485639

Country of ref document: AT

Kind code of ref document: T

Effective date: 20220515

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG9D

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20220420

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 1485639

Country of ref document: AT

Kind code of ref document: T

Effective date: 20220420

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

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: 20220420

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

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: 20220420

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: 20220822

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: 20220720

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: 20220420

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: 20220420

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: 20220721

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: 20220420

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: 20220420

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: 20220720

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: 20220420

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

Ref country code: RS

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: 20220420

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: 20220420

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: 20220420

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: 20220820

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602017056434

Country of ref document: DE

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: 20220420

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: 20220420

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: 20220420

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: 20220420

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: 20220420

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: 20220420

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

26N No opposition filed

Effective date: 20230123

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: 20220420

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

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: 20220420

P01 Opt-out of the competence of the unified patent court (upc) registered

Effective date: 20230615

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

Effective date: 20221222

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20221231

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

Ref country code: LU

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

Effective date: 20221222

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: 20221222

Ref country code: GB

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

Effective date: 20221222

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: 20221231

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

Ref country code: IT

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

Effective date: 20220420

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

Ref country code: FR

Payment date: 20231122

Year of fee payment: 7

Ref country code: DE

Payment date: 20231121

Year of fee payment: 7

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

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: 20220420

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

Ref country code: CH

Payment date: 20240102

Year of fee payment: 7