EP3825782B1 - Reinforced timepiece component - Google Patents

Reinforced timepiece component Download PDF

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Publication number
EP3825782B1
EP3825782B1 EP19211198.7A EP19211198A EP3825782B1 EP 3825782 B1 EP3825782 B1 EP 3825782B1 EP 19211198 A EP19211198 A EP 19211198A EP 3825782 B1 EP3825782 B1 EP 3825782B1
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EP
European Patent Office
Prior art keywords
edge
timepiece
component
piece
timepiece component
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EP19211198.7A
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German (de)
French (fr)
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EP3825782A1 (en
Inventor
James Hide
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Patek Philippe SA Geneve
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Patek Philippe SA Geneve
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Priority to EP19211198.7A priority Critical patent/EP3825782B1/en
Publication of EP3825782A1 publication Critical patent/EP3825782A1/en
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    • 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
    • G04B18/00Mechanisms for setting frequency
    • G04B18/006Mechanisms for setting frequency by adjusting the devices fixed on the balance

Definitions

  • the present invention relates to a watch component comprising a composite part comprising an upper face, a lower face and an edge, made of a first material and coated with a second material to increase its mechanical resistance, a part of its edge being devoid of this coating.
  • the present invention also relates to a method of manufacturing such a component.
  • Silicon is a material of choice for the production of watch components due to its low density, its elasticity, its non-magnetism and its ability to be machined using engraving techniques.
  • its mechanical strength, in particular its impact resistance is relatively low because, on the one hand, silicon does not deform plastically and, on the other hand, the beginnings of rupture propagate very easily along its crystalline planes.
  • the patent application WO 2007/000271 proposes for this to produce a coating in a thick amorphous material, such as silicon oxide, nitride or carbide, titanium nitride or carbide, silicon oxide being the preferred material and its thickness being, in in this case, at least five times greater than the thickness of the silicon oxide formed naturally on the surface of the silicon in contact with the ambient air.
  • Watch components comprising a silicon structure covered with a reinforcing layer of silicon oxide are also described in the patent application WO 2008/135817 of the present plaintiff.
  • micro-etching techniques used for the manufacture of silicon parts allow the simultaneous production of a batch of parts from the same silicon wafer.
  • silicon parts are left to constitute attachments or bridges holding each of the parts attached to the rest of the plate. These fasteners will later be broken to release the parts from the plate.
  • the fasteners may only be broken at the end of the manufacturing process, which implies that the reinforcement layer is formed, after etching, on the entire silicon wafer, including the parts and fasteners.
  • the parts In practice, after releasing the parts from the plate, if there are any attachment parts remaining on the parts, they are often removed by machining or abrasion, for aesthetic reasons.
  • the areas of the surface of the final parts where the fasteners were located are made of silicon, that is to say they are not covered by the reinforcing layer (for example in silicon oxide) since this layer was formed before the breakage of the attachments.
  • These zones therefore constitute areas of fragility which will allow possible ruptures resulting from shocks to propagate inside the part and cause it to rupture.
  • the fragility of these areas is aggravated by the fact that their surface condition is generally less good than that of the rest of the part and that they can present micro-cracks as soon as they form.
  • the patent application EP 2 503 404 describes a manufacturing process making it possible to limit the impact of such fragile zones on the solidity of the component.
  • it is proposed, contrary to the practice which consists of eliminating by machining or abrasion the possible remainder of the attachment parts on the parts once separated from the plate, to detach the part from the plate so as to that at least part of at least one fastener is left on the final component ready to be mounted in the mechanism.
  • the clip is typically laser cut so that its length is at least equal to its width and/or its thickness. Leaving at least part of at least one fastener on the final component makes it possible to significantly increase the mechanical strength of the component.
  • the fasteners or fastening parts left distance the uncoated surfaces created by the detachment of the structure from the rest of the exterior surface of the component, which limits the propagation of the beginnings of rupture.
  • This solution is however not entirely satisfactory insofar as, even if the fasteners or parts of fasteners limit the propagation of the beginnings of rupture in the event of an indirect impact, a direct impact on the weakened zone can lead to an impact on the residue. attachment.
  • the invention relates to a watch component comprising a composite part comprising an upper face, a lower face and an edge, made of a first material and coated with a second material to increase its mechanical resistance, at least part of its edge being devoid of of this coating, typically following the breakage of one or more fasteners resulting from its manufacturing process.
  • the part or parts of the edge of the part devoid of this coating constitute areas of fragility of the component.
  • An aim of the present invention is to provide such a component whose risk of rupture or damage in the event of impact, typically direct, on the or one of said fragile zones is reduced.
  • the invention proposes a watch component comprising a composite part comprising an upper face, a lower face and a edge, made of a first material and coated with a second material to increase its mechanical resistance, at least part of its edge being devoid of this coating, typically following the breakage of one or more fasteners resulting from its manufacturing process, said watch component being characterized in that it comprises a protective member which, in top view or in bottom view , extends outside the edge of the part at said part devoid of coating, covering at least partially, and preferably completely, said part.
  • Said protective member makes it possible to limit the possibility of direct impacts on the part of the edge of the composite part devoid of coating with which it is associated and thus has, as its name indicates, a protective function.
  • said protective member has another function such as, for example, an adjustment function, a weighting function, or a tribological function, preferably, an adjustment function.
  • a protective member having an adjustment function we can for example cite a weight for adjusting the inertia of a balance wheel, an eccentric allowing, by being pivoted, to adjust a rest or function position of a component with which it cooperates or well to adjust the stroke of a component with which it cooperates.
  • the watch component is characterized in that said at least part of the edge of its composite part devoid of coating is located recessed in the component, typically in a notch in the edge of said composite part. This is thus doubly protected against direct impacts, by the protective member and by the rest of the edge of the composite part.
  • the composite part of the component according to the invention may comprise several parts of its edge devoid of coating. It then typically has at least as many protective organs as said parts so that each of said parts devoid of coating is associated with a distinct protective organ.
  • each of the protective members associated with a part of the edge of the composite part devoid of coating extends outside the edge of this part at the level of this part by covering this part at least partially.
  • a protective member When a protective member is an adjusting member, it extends outside the edge of the part at the level of the part devoid of coating with which it is associated, covering at least partially and preferably completely this part and this regardless of its adjustment position.
  • the invention also proposes a watch mechanism comprising a first watch component according to the invention and a second watch component intended to cooperate directly with said first watch component during operation of the mechanism, characterized in that the second watch component cannot reach the first watch component only on a part of the edge of its composite part carrying the coating or on a protective member and this regardless of the adjustment position of the adjustable protective member(s) if there are any.
  • the invention also relates to a timepiece such as a wristwatch, a pocket watch, a clock or a clock comprising such a watch mechanism.
  • Step a) of the manufacturing process according to the invention is typically carried out using the deep reactive ion etching technique DRIE (Deep Reactive Ion Etching).
  • DRIE Deep Reactive Ion Etching
  • Step c) of the manufacturing process according to the invention is preferably implemented by cutting the fasteners by machining means, for example by laser. It can also be implemented by making a break, for example by making two beginnings of breakage then applying a force on the fastener to break it.
  • the first material according to the invention is typically a “fragile” material, that is to say one which is not capable of plastic deformation (at room temperature, i.e. at 25°C).
  • This is typically silicon.
  • silicon can be monocrystalline, polycrystalline or amorphous, and have different crystalline orientations. It may also be doped or not.
  • the second material according to the invention is for example silicon oxide, carbide or nitride, titanium nitride or carbide or diamond, silicon oxide being preferred.
  • the protective member according to the invention is typically made from a metal base, for example a copper-beryllium or nickel phosphorus alloy, gold, platinum, steel or nickel. Alternatively, it could also be made of wood, ceramic, polymer or rigid foam.
  • the watch component according to the invention has reinforced mechanical resistance, in particular to direct shocks.
  • the arrangement of its protective member(s) makes it less likely to suffer damage or even break in the event of an impact, for example during storage, transport, assembly or assembly. use within a watch mechanism.
  • the component according to the invention also has the advantage of being able to be manufactured precisely and in batches, a large number of components being able to be produced simultaneously from the same plate.
  • a balance 1 for a regulating member of the sprung balance type of a mechanical watch movement comprises, according to a particular embodiment of the invention, a composite structure 2 of low density carrying at its periphery metal parts 3 having a high density and inertia adjustment weights 11.
  • the balance wheel 1 and its structure 2 typically extend in a plane.
  • Structure 2 has an upper face 2.1 and a lower face 2.2 delimiting its section 2.3.
  • slice we mean the slice defining the exterior contour of the structure 2 of balance 1. This therefore excludes the interior contours of the openings 2.4 which are optional.
  • Structure 2 comprises a board 4 of thickness e, typically constant.
  • the board 4 has an annular central part 5 through which the shaft on which the balance 1 is intended to be mounted can pass, a rim, for example comprising two parts 6a and 6b in the form of diametrically opposed arcs of a circle, arm 7 connecting the central part 5 to the two parts 6a, 6b of the serge and, in each of the parts 6a, 6b of the serge, cavities 8 in which the metal parts 3 are located.
  • the structure 2 comprises also edges 9 projecting from the upper surface of the board 4. These edges 9 extend in height the wall of the cavities 8, allowing the cavities 8 and therefore the metal parts 3 which fill them to have a greater height or thickness than the thickness e of the board 4.
  • Each of the cavities 8 and the metal parts 3 has an elongated and curved shape which follows the arcuate contour of the part 6a or 6b of the serge in which it is located.
  • the number and dimensions of the metal parts 3 may vary. Their function is to weigh down the serge in order to increase the moment of inertia to mass ratio of the balance 1.
  • the structure 2 comprises four pins 10 each carrying a weight 11, said weights 11 allowing the adjustment of the moment of inertia of the balance 1.
  • These weights 11 are typically held on the pins 10 by elastic tightening.
  • the elastic tightening is such that each of them is able to pivot around the pin which carries it for adjusting the inertia of the balance 1.
  • the balance 1 can be entirely monolithic.
  • Structure 2 is therefore typically monolithic. It is made of a base material 12, for example silicon, covered with a coating 13 intended to increase the mechanical resistance of the balance 1, in particular its resistance to shocks.
  • the coating 13 is, for example, a layer of silicon oxide.
  • the balance wheel 1 is manufactured using a process similar to that described in the patent application WO 2008/135817 of the present plaintiff.
  • a plate of the base material 12 is etched, preferably by DRIE deep reactive ion etching, to form a batch of parts each having the shape of the structure 2, each of these parts being attached to the rest of the plate by fasteners or bridges of material left during engraving.
  • the coating 13 is formed on all surfaces of the plate, including the surfaces of parts and fasteners.
  • the metal parts 3 are formed in cavities defined by the coated parts, namely the cavities 8, typically by electroforming (galvanic growth).
  • the parts are detached from the plate and the adjustment weights 11 are mounted on the balance 1.
  • the coating 13 can be formed by applying a heat treatment to the plate to oxidize its surfaces, as in the patent application WO 2008/135817 .
  • the coating 13 can be formed for example by chemical vapor deposition or physical vapor deposition.
  • the detachment of the parts from the plate creates fragile end surfaces 15, devoid of the coating 13.
  • the detachment is typically carried out in a manner which leaves attachment parts 14 on the parts in order to to limit the propagation of the beginnings of rupture which could occur on these “fragile” surfaces, as described in the request EP 2 503 404 .
  • said attachment parts 14 project onto edge 2.3 of each part.
  • Each of them is covered by the coating 13 except on the part of its edge 2.3 corresponding to its end surface 15 created by the detachment of the parts from the plate ( figure 4a ).
  • the length of the attachment parts 14 is typically greater than or equal to its width and/or its thickness measured at the level of the end surface 15, as described in the application EP 2 503 404 .
  • the position of the pins 10 and the dimensions of the weights 11 are such that, in top view, each of the weights 11 extends outside the section 2.3 of the structure 2 at the level of a part separate attachment 14 by at least partially covering the part 15 of the edge of this attachment 14 devoid of covering 13. The whole is arranged so that this is the case whatever the adjustment position of the weight 11 considered.
  • Each adjustment weight 11 thus plays a protective role by limiting the possibility of direct shocks on the “fragile” parts 15 of section 2.3 of the balance 1 which could occur during its storage, transport or assembly in a watch mechanism or after said assembly, during the normal operation of said watch mechanism.
  • FIG 2 illustrates part of a watch mechanism comprising, among other things, a plate 16 on which the balance 1 is mounted and a balance stop mechanism 20, also called “stop-second” or “stop-balance”.
  • the balance stop 20 comprises an elastic arm 21 actuable by the time setting rod (not shown) of the mechanism and whose end is intended to cooperate directly with the periphery of the balance 1 to stop its oscillation by friction, and this regardless of its position. It is possible that it hits it directly next to one of its attachments 14 presenting a fragile zone 15.
  • the arm 21 of the balance stop 20 generally has a thickness or height h corresponding to the sum of the thickness e of the board 4 and the thickness e' of its flyweight and is arranged so that if it hits the balance 1 at the level of a fragile part 15 of its edge 2.3, the impact is on the flyweight 11 and not on said fragile part 15. In other positions of the balance 1, the arm 21 would typically strike directly on a part of section 2.3 carrying the covering 13 or on another of the four weights 11.
  • the height h of the balance arm 21 could be different from the moment the protection function is ensured.
  • the arm 21 is arranged so that, once mounted in the watch mechanism, it is horizontally facing both at least part of the section 2.3 of the board 4 of the balance 1 and at least one part weights 11.
  • the weights 11 therefore have a dual role, they serve both as a protective member or mechanical “shield” of the balance 1 against shocks which may be unpredictable (transport, assembly, etc.) or predictable. (repeated impacts against a balance stop for example) and inertia adjustment member.
  • the weights 11 must have a high density to provide inertia to the balance 1 and preferably high mechanical resistance. If they are typically made of a copper - beryllium alloy, other materials traditionally used for the production of adjustment weights, such as gold, platinum, steel, nickel or a nickel-phosphorus alloy are quite suitable in the scope of the invention.
  • the adjustment weights 11 could be mounted on the pins 10 before the fasteners break.
  • the structure 2 comprises four fragile parts 15 and four pins 10 each carrying an adjustment weight 11, each of said weights 11 protecting one of said fragile parts 15. It is clear that the structure 2 could comprise a different number of fragile parts 15 and weights and that only certain fragile parts 15 could be protected by weights or that only certain weights 11 protect a fragile part 15.
  • the component according to the invention is a watchmaking hammer and its adjustment member is an eccentric allowing the adjustment of its rest position against a stop.
  • the component according to the invention is a balance wheel 100 comprising a composite structure 102, typically made of silicon covered with silicon oxide, comprising an upper face, a lower face and a edge.
  • a so-called fragile part 115 of this slice corresponding to the surface created by the breakage of a manufacturing fastener 114, is devoid of coating.
  • the structure 102 comprises pins 110 carrying inertia washers, one of which 111 is positioned so that, in top view, it extends outside the edge of the structure at the level of said fragile part 115 by completely covering said part.
  • This inertia washer has a dual role, both protective in that it limits the possibility of direct shocks on the fragile part 115 and both weighting to increase the inertia of the balance 100.
  • the part fragile 115 of the edge of the structure 102 is set back in this structure, in a notch in its edge, so as to further limit the possibility of direct impacts on the fragile part 115.
  • the manufacturing process according to the invention makes it possible to produce a large number of components simultaneously from the same wafer.
  • the watch component according to the invention has an aesthetic advantage in that it allows these attachment parts to be hidden. .

Description

La présente invention concerne un composant horloger comprenant une pièce composite comprenant une face supérieure, une face inférieure et une tranche, réalisée en un premier matériau et revêtue d'un deuxième matériau pour augmenter sa résistance mécanique, une partie de sa tranche étant dépourvue de ce revêtement. La présente invention concerne également un procédé de fabrication d'un tel composant.The present invention relates to a watch component comprising a composite part comprising an upper face, a lower face and an edge, made of a first material and coated with a second material to increase its mechanical resistance, a part of its edge being devoid of this coating. The present invention also relates to a method of manufacturing such a component.

ART ANTERIEURPRIOR ART

Le silicium est un matériau de choix pour la réalisation de composants horlogers en raison de sa faible densité, de son élasticité, de son amagnétisme et de son aptitude à être usiné par des techniques de gravure. Cependant, à l'état brut, sa résistance mécanique, en particulier sa résistance aux chocs, est relativement faible car, d'une part, le silicium ne se déforme pas plastiquement et, d'autre part, les amorces de rupture se propagent très facilement le long de ses plans cristallins.Silicon is a material of choice for the production of watch components due to its low density, its elasticity, its non-magnetism and its ability to be machined using engraving techniques. However, in the raw state, its mechanical strength, in particular its impact resistance, is relatively low because, on the one hand, silicon does not deform plastically and, on the other hand, the beginnings of rupture propagate very easily along its crystalline planes.

Il existe des solutions pour renforcer mécaniquement des pièces en silicium. Par exemple, la demande de brevet WO 2007/000271 propose pour cela de réaliser un revêtement en un matériau amorphe épais, tel que l'oxyde, le nitrure ou le carbure de silicium, le nitrure ou le carbure de titane, l'oxyde de silicium étant le matériau préféré et son épaisseur étant, dans ce cas, au moins cinq fois supérieure à l'épaisseur de l'oxyde de silicium formé naturellement à la surface du silicium au contact de l'air ambiant. Des composants horlogers comprenant une structure en silicium recouverte d'une couche de renfort en oxyde de silicium sont également décrits dans la demande de brevet WO 2008/135817 de la présente demanderesse.There are solutions for mechanically strengthening silicon parts. For example, the patent application WO 2007/000271 proposes for this to produce a coating in a thick amorphous material, such as silicon oxide, nitride or carbide, titanium nitride or carbide, silicon oxide being the preferred material and its thickness being, in in this case, at least five times greater than the thickness of the silicon oxide formed naturally on the surface of the silicon in contact with the ambient air. Watch components comprising a silicon structure covered with a reinforcing layer of silicon oxide are also described in the patent application WO 2008/135817 of the present plaintiff.

Les techniques de micro-gravure utilisées pour la fabrication de pièces en silicium permettent la réalisation simultanée d'un lot de pièces à partir d'une même plaque de silicium. Ainsi, lors de la gravure, des parties en silicium sont laissées pour constituer des attaches ou ponts maintenant chacune des pièces attachée au reste de la plaque. Ces attaches seront plus tard cassées pour libérer les pièces de la plaque.The micro-etching techniques used for the manufacture of silicon parts allow the simultaneous production of a batch of parts from the same silicon wafer. Thus, during engraving, silicon parts are left to constitute attachments or bridges holding each of the parts attached to the rest of the plate. These fasteners will later be broken to release the parts from the plate.

Comme l'indique la demande de brevet précitée WO 2008/135817 , les attaches peuvent n'être cassées qu'à la fin du procédé de fabrication, ce qui implique que la couche de renfort est formée, après la gravure, sur toute la plaque de silicium, y compris les pièces et les attaches. En pratique, après la libération des pièces de la plaque, s'il reste des parties d'attache sur les pièces, elles sont souvent éliminées par usinage ou abrasion, pour des raisons esthétiques. Les zones de la surface des pièces finales où se trouvaient les attaches sont en silicium c'est-à-dire qu'elles ne sont pas recouvertes par la couche de renfort (par exemple en oxyde de silicium) puisque cette couche a été formée avant la rupture des attaches. Ces zones constituent donc des zones de fragilité qui laisseront les éventuelles amorces de rupture consécutives à des chocs se propager à l'intérieur de la pièce et causer une rupture de celle-ci. De plus, la fragilité de ces zones est aggravée par le fait que leur état de surface est généralement moins bon que celui du reste de la pièce et qu'elles peuvent dès leur formation présenter des micro-fissures.As indicated in the aforementioned patent application WO 2008/135817 , the fasteners may only be broken at the end of the manufacturing process, which implies that the reinforcement layer is formed, after etching, on the entire silicon wafer, including the parts and fasteners. In practice, after releasing the parts from the plate, if there are any attachment parts remaining on the parts, they are often removed by machining or abrasion, for aesthetic reasons. The areas of the surface of the final parts where the fasteners were located are made of silicon, that is to say they are not covered by the reinforcing layer (for example in silicon oxide) since this layer was formed before the breakage of the attachments. These zones therefore constitute areas of fragility which will allow possible ruptures resulting from shocks to propagate inside the part and cause it to rupture. In addition, the fragility of these areas is aggravated by the fact that their surface condition is generally less good than that of the rest of the part and that they can present micro-cracks as soon as they form.

La demande de brevet EP 2 503 404 décrit un procédé de fabrication permettant de limiter l'impact de telles zones de fragilité sur la solidité du composant. Pour cela, il est proposé, contrairement à l'usage qui consiste à éliminer par usinage ou abrasion l'éventuel reste des parties d'attache sur les pièces une fois séparées de la plaque, de détacher la pièce de la plaque de sorte qu'au moins une partie d'au moins une attache soit laissée sur le composant final prêt à être monté dans le mécanisme. L'attache est typiquement découpée au laser de sorte que sa longueur est au moins égale à sa largeur et/ou à son épaisseur. Le fait de laisser au moins une partie d'au moins une attache sur le composant final permet d'augmenter significativement la résistance mécanique du composant. En effet, les attaches ou parties d'attache laissées éloignent du reste de la surface extérieure du composant les surfaces non revêtues créées par le détachement de la structure ce qui limite la propagation des amorces de rupture. Cette solution n'est cependant pas entièrement satisfaisante dans la mesure où, même si les attaches ou parties d'attaches limitent la propagation des amorces de rupture en cas de choc indirect, un choc direct sur la zone fragilisée peut entraîner un impact sur le résidu d'attache.The patent application EP 2 503 404 describes a manufacturing process making it possible to limit the impact of such fragile zones on the solidity of the component. For this, it is proposed, contrary to the practice which consists of eliminating by machining or abrasion the possible remainder of the attachment parts on the parts once separated from the plate, to detach the part from the plate so as to that at least part of at least one fastener is left on the final component ready to be mounted in the mechanism. The clip is typically laser cut so that its length is at least equal to its width and/or its thickness. Leaving at least part of at least one fastener on the final component makes it possible to significantly increase the mechanical strength of the component. In fact, the fasteners or fastening parts left distance the uncoated surfaces created by the detachment of the structure from the rest of the exterior surface of the component, which limits the propagation of the beginnings of rupture. This solution is however not entirely satisfactory insofar as, even if the fasteners or parts of fasteners limit the propagation of the beginnings of rupture in the event of an indirect impact, a direct impact on the weakened zone can lead to an impact on the residue. attachment.

L'invention concerne un composant horloger comprenant une pièce composite comprenant une face supérieure, une face inférieure et une tranche, réalisée en un premier matériau et revêtue d'un deuxième matériau pour augmenter sa résistance mécanique, au moins une partie de sa tranche étant dépourvue de ce revêtement, typiquement suite à la rupture d'une ou plusieurs attaches issues de son procédé de fabrication. La ou les parties de la tranche de la pièce dépourvues de ce revêtement constituent des zones de fragilité du composant.The invention relates to a watch component comprising a composite part comprising an upper face, a lower face and an edge, made of a first material and coated with a second material to increase its mechanical resistance, at least part of its edge being devoid of of this coating, typically following the breakage of one or more fasteners resulting from its manufacturing process. The part or parts of the edge of the part devoid of this coating constitute areas of fragility of the component.

Un but de la présente invention est de fournir un tel composant dont le risque de rupture ou d'endommagement en cas de choc, typiquement direct, sur la ou l'une desdites zones de fragilité est diminué.An aim of the present invention is to provide such a component whose risk of rupture or damage in the event of impact, typically direct, on the or one of said fragile zones is reduced.

BREF EXPOSE DE L'INVENTIONBRIEF STATEMENT OF THE INVENTION

L'invention propose à cette fin un composant horloger comprenant une pièce composite comprenant une face supérieure, une face inférieure et une tranche, réalisée en un premier matériau et revêtue d'un deuxième matériau pour augmenter sa résistance mécanique, au moins une partie de sa tranche étant dépourvue de ce revêtement, typiquement suite à la rupture d'une ou plusieurs attaches issues de son procédé de fabrication, ledit composant horloger étant caractérisé en ce qu'il comprend un organe protecteur qui, en vue de dessus ou en vue de dessous, s'étend à l'extérieur de la tranche de la pièce au niveau de ladite partie dépourvue de revêtement en couvrant au moins partiellement, et de préférence totalement, ladite partie.To this end, the invention proposes a watch component comprising a composite part comprising an upper face, a lower face and a edge, made of a first material and coated with a second material to increase its mechanical resistance, at least part of its edge being devoid of this coating, typically following the breakage of one or more fasteners resulting from its manufacturing process, said watch component being characterized in that it comprises a protective member which, in top view or in bottom view , extends outside the edge of the part at said part devoid of coating, covering at least partially, and preferably completely, said part.

Ledit organe protecteur permet de limiter la possibilité de chocs directs sur la partie de la tranche de la pièce composite dépourvue de revêtement à laquelle il est associé et possède ainsi, comme son nom l'indique, une fonction protectrice.Said protective member makes it possible to limit the possibility of direct impacts on the part of the edge of the composite part devoid of coating with which it is associated and thus has, as its name indicates, a protective function.

De préférence, en plus de sa fonction protectrice, ledit organe protecteur possède une autre fonction telle que, par exemple, une fonction de réglage, une fonction d'alourdissement, ou une fonction tribologique, de préférence, une fonction de réglage.Preferably, in addition to its protective function, said protective member has another function such as, for example, an adjustment function, a weighting function, or a tribological function, preferably, an adjustment function.

Comme organe protecteur ayant une fonction de réglage on peut par exemple citer une masselotte de réglage de l'inertie d'un balancier, un excentrique permettant en étant pivoté de régler une position de repos ou de fonction d'un composant avec lequel il coopère ou bien de régler la course d'un composant avec lequel il coopère.As a protective member having an adjustment function, we can for example cite a weight for adjusting the inertia of a balance wheel, an eccentric allowing, by being pivoted, to adjust a rest or function position of a component with which it cooperates or well to adjust the stroke of a component with which it cooperates.

Dans une forme de réalisation avantageuse de l'invention, le composant horloger est caractérisé en ce que ladite au moins une partie de la tranche de sa pièce composite dépourvue de revêtement se situe en retrait dans le composant, typiquement dans une échancrure de la tranche de ladite pièce composite. Celle-ci est ainsi doublement protégée contre des chocs directs, par l'organe protecteur et par le reste de la tranche de la pièce composite.In an advantageous embodiment of the invention, the watch component is characterized in that said at least part of the edge of its composite part devoid of coating is located recessed in the component, typically in a notch in the edge of said composite part. This is thus doubly protected against direct impacts, by the protective member and by the rest of the edge of the composite part.

La pièce composite du composant selon l'invention peut comprendre plusieurs parties de sa tranche dépourvues de revêtement. Il possède alors typiquement au moins autant d'organes protecteurs que desdites parties de sorte qu'à chacune desdites parties dépourvues de revêtement est associée un organe protecteur distinct. Dans ce cas, en vue de dessus ou en vue de dessous, chacun des organes protecteurs associé à une partie de la tranche de la pièce composite dépourvue de revêtement s'étend à l'extérieur de la tranche de cette pièce au niveau de cette partie en couvrant au moins partiellement cette partie.The composite part of the component according to the invention may comprise several parts of its edge devoid of coating. It then typically has at least as many protective organs as said parts so that each of said parts devoid of coating is associated with a distinct protective organ. In this case, in top view or bottom view, each of the protective members associated with a part of the edge of the composite part devoid of coating extends outside the edge of this part at the level of this part by covering this part at least partially.

Lorsqu'un organe protecteur est un organe de réglage, il s'étend à l'extérieur de la tranche de la pièce au niveau de la partie dépourvue de revêtement à laquelle il est associé en couvrant au moins partiellement et de préférence totalement cette partie et cela quelle que soit sa position de réglage.When a protective member is an adjusting member, it extends outside the edge of the part at the level of the part devoid of coating with which it is associated, covering at least partially and preferably completely this part and this regardless of its adjustment position.

L'invention propose également un mécanisme d'horlogerie comprenant un premier composant horloger selon l'invention et un second composant horloger destiné à venir coopérer directement avec ledit premier composant horloger lors du fonctionnement du mécanisme, caractérisé en ce que le second composant horloger ne puisse atteindre le premier composant horloger que sur une partie de la tranche de sa pièce composite portant le revêtement ou sur un organe protecteur et cela quelle que soit la position de réglage du ou des organes protecteur réglables s'il y en a.The invention also proposes a watch mechanism comprising a first watch component according to the invention and a second watch component intended to cooperate directly with said first watch component during operation of the mechanism, characterized in that the second watch component cannot reach the first watch component only on a part of the edge of its composite part carrying the coating or on a protective member and this regardless of the adjustment position of the adjustable protective member(s) if there are any.

L'invention concerne aussi une pièce d'horlogerie telle qu'une montre-bracelet, une montre de poche, une pendule ou une pendulette comportant un tel mécanisme horloger.The invention also relates to a timepiece such as a wristwatch, a pocket watch, a clock or a clock comprising such a watch mechanism.

Enfin, l'invention concerne un procédé de fabrication d'un composant horloger prêt à être monté dans un mécanisme horloger comprenant les étapes suivantes :

  1. a. graver une pièce ayant une forme souhaitée pour le composant dans une plaque d'un premier matériau en laissant au moins une attache entre la pièce et le reste de la plaque, ladite pièce comprenant une face supérieure, une face inférieure et une tranche,
  2. b. revêtir la plaque d'un deuxième matériau destiné à augmenter la résistance mécanique de la structure et couvrant ainsi la pièce et la ou les attache(s),
  3. c. détacher la pièce de la plaque en sectionnant la ou les attache(s), puis, optionnellement, éliminer les portions d'attache(s) restantes, une ou plusieurs partie(s) de la tranche de la pièce étant alors dépourvue(s) dudit revêtement, et
  4. d. fixer au moins un organe protecteur sur la pièce, de manière à ce que, en vue de dessus ou en vue de dessous, ledit organe protecteur s'étende à l'extérieur de sa tranche au niveau de la partie ou d'une des parties de sa tranche dépourvue(s) de revêtement en couvrant au moins partiellement ladite partie,
les étapes c) et d) pouvant être interverties.Finally, the invention relates to a method of manufacturing a watch component ready to be mounted in a watch mechanism comprising the following steps:
  1. has. engrave a part having a desired shape for the component in a plate of a first material leaving at least one attachment between the part and the rest of the plate, said part comprising an upper face, a lower face and a edge,
  2. b. coat the plate with a second material intended to increase the mechanical resistance of the structure and thus covering the part and the fastener(s),
  3. vs. detach the part from the plate by cutting the fastener(s), then, optionally, eliminate the remaining portions of fastener(s), one or more part(s) of the edge of the part then being devoid(s) of said covering, and
  4. d. fix at least one protective member on the part, so that, in view from above or in view from below, said protective member extends outside its edge at the level of the part or one of the parts of its edge devoid of coating by covering at least partially said part,
steps c) and d) can be interchanged.

L'étape a) du procédé de fabrication selon l'invention est typiquement réalisée à l'aide de la technique de gravure ionique réactive profonde DRIE (Deep Reactive Ion Etching).Step a) of the manufacturing process according to the invention is typically carried out using the deep reactive ion etching technique DRIE (Deep Reactive Ion Etching).

L'étape c) du procédé de fabrication selon l'invention est de préférence mise en oeuvre en coupant les attaches par des moyens d'usinage, par exemple au laser. Elle peut également être mise en oeuvre en réalisant une cassure, par exemple en réalisant deux amorces de rupture puis en appliquant une force sur l'attache pour la casser.Step c) of the manufacturing process according to the invention is preferably implemented by cutting the fasteners by machining means, for example by laser. It can also be implemented by making a break, for example by making two beginnings of breakage then applying a force on the fastener to break it.

De manière préférée, lors de l'étape c) au moins une partie d'au moins une attache est laissée sur le composant final prêt à être monté dans le mécanisme, ladite au moins une partie d'au moins une attache faisant saillie sur la tranche du composant final et présentant au moins l'une des caractéristiques suivantes :

  1. a. une longueur au moins égale à sa largeur,
  2. b. une longueur au moins égale à son épaisseur,
  3. c. une longueur au moins égale à la moitié de la longueur qu'avait l'attache avant l'étape de détachement
comme cela est décrit dans la demande EP 2 503 404 , de manière à diminuer d'avantage le risque de rupture ou d'endommagement du composant consécutivement à des chocs.Preferably, during step c) at least part of at least one fastener is left on the final component ready to be mounted in the mechanism, said at least part of at least one fastener projecting on the slice of the final component and having at least one of the following characteristics:
  1. has. a length at least equal to its width,
  2. b. a length at least equal to its thickness,
  3. vs. a length at least equal to half the length that the fastener had before the detachment step
as described in the application EP 2 503 404 , so as to further reduce the risk of breakage or damage to the component following shocks.

Le premier matériau selon l'invention est typiquement un matériau « fragile » c'est-à-dire qui n'est pas capable de se déformer plastiquement (à température ambiante, soit à 25°C). Il s'agit typiquement du silicium. Dans ce cas, le silicium peut être monocristallin, polycristallin ou amorphe, et avoir différentes orientations cristallines. Il peut en outre être dopé ou non.The first material according to the invention is typically a “fragile” material, that is to say one which is not capable of plastic deformation (at room temperature, i.e. at 25°C). This is typically silicon. In this case, silicon can be monocrystalline, polycrystalline or amorphous, and have different crystalline orientations. It may also be doped or not.

Le deuxième matériau selon l'invention est par exemple de l'oxyde, du carbure ou du nitrure de silicium, du nitrure ou du carbure de titane ou du diamant, l'oxyde de silicium étant préféré.The second material according to the invention is for example silicon oxide, carbide or nitride, titanium nitride or carbide or diamond, silicon oxide being preferred.

L'organe protecteur selon l'invention est typiquement réalisé à base de métal, par exemple en un alliage cuivre-béryllium ou nickel phosphore, en or, en platine, en acier ou en nickel. En variante, il pourrait également être réalisé en bois, céramique, polymère ou mousse rigide.The protective member according to the invention is typically made from a metal base, for example a copper-beryllium or nickel phosphorus alloy, gold, platinum, steel or nickel. Alternatively, it could also be made of wood, ceramic, polymer or rigid foam.

Le composant horloger selon l'invention présente une résistance mécanique renforcée, en particulier aux chocs directs. L'agencement de son ou de ses organe(s) protecteur(s) le rend moins susceptible de subir des détériorations voire de se rompre en cas de choc, par exemple lors de son stockage, de son transport, de son montage ou de son utilisation au sein d'un mécanisme horloger.The watch component according to the invention has reinforced mechanical resistance, in particular to direct shocks. The arrangement of its protective member(s) makes it less likely to suffer damage or even break in the event of an impact, for example during storage, transport, assembly or assembly. use within a watch mechanism.

Le composant selon l'invention présente également l'avantage de pouvoir être fabriqué de manière précise et par lots, un grand nombre de composants pouvant être réalisé simultanément à partir d'une même plaque.The component according to the invention also has the advantage of being able to be manufactured precisely and in batches, a large number of components being able to be produced simultaneously from the same plate.

BREVE DESCRIPTION DES FIGURESBRIEF DESCRIPTION OF THE FIGURES

D'autres caractéristiques et avantages de la présente invention apparaîtront à la lecture de la description détaillée suivante faite en référence aux dessins annexés dans lesquels :

  • la figure 1 est une vue en perspective de dessus d'un balancier selon un mode de réalisation particulier de l'invention ;
  • la figure 2 est une vue de dessus d'une partie d'un mécanisme horloger selon un mode de réalisation particulier de l'invention, ledit mécanisme comprenant le balancier illustré à la figure 1 et un stop-balancier ;
  • la figure 3 est vue de dessus en transparence illustrant une partie du balancier et du stop-balancier illustrés à la figure 2 ;
  • la figure 4a est une vue de profil coupée selon l'axe I-I du balancier et du stop-balancier illustrés à la figure 1 ; la figure 4b est une vue de profil coupée selon l'axe II-II, du balancier et du stop-balancier illustrés à la figure 2 ;
  • la figure 5 est une vue de dessus en transparence d'un balancier selon un autre mode de réalisation de l'invention.
Other characteristics and advantages of the present invention will appear on reading the following detailed description given with reference to the appended drawings in which:
  • there figure 1 is a top perspective view of a balance according to a particular embodiment of the invention;
  • there figure 2 is a top view of a part of a watch mechanism according to a particular embodiment of the invention, said mechanism comprising the balance wheel illustrated in figure 1 and a balance stop;
  • there Figure 3 is seen from above in transparency illustrating part of the balance and the stop-balance illustrated in the figure 2 ;
  • there figure 4a is a profile view cut along axis II of the balance wheel and the balance stop illustrated in figure 1 ; there figure 4b is a profile view cut along axis II-II, of the balance wheel and the balance stop illustrated in figure 2 ;
  • there Figure 5 is a transparent top view of a balance wheel according to another embodiment of the invention.

DESCRIPTION DETAILLEEDETAILED DESCRIPTION

En référence aux figures 1 à 4b, un balancier 1 pour un organe régulateur de type balancier-spiral d'un mouvement d'horlogerie mécanique comprend, selon un mode de réalisation particulier de l'invention, une structure composite 2 de faible masse volumique portant à sa périphérie des parties métalliques 3 ayant une masse volumique élevée et des masselottes de réglage de l'inertie 11.With reference to figures 1 to 4b , a balance 1 for a regulating member of the sprung balance type of a mechanical watch movement comprises, according to a particular embodiment of the invention, a composite structure 2 of low density carrying at its periphery metal parts 3 having a high density and inertia adjustment weights 11.

Le balancier 1 et sa structure 2 s'étendent typiquement dans un plan. La structure 2 présente une face supérieure 2.1 et une face inférieure 2.2 délimitant sa tranche 2.3. Par « tranche » on entend la tranche définissant le contour extérieur de la structure 2 de balancier 1. Cela exclut donc les contours intérieurs des ouvertures 2.4 qui sont optionnelles.The balance wheel 1 and its structure 2 typically extend in a plane. Structure 2 has an upper face 2.1 and a lower face 2.2 delimiting its section 2.3. By “slice” we mean the slice defining the exterior contour of the structure 2 of balance 1. This therefore excludes the interior contours of the openings 2.4 which are optional.

La structure 2 comprend une planche 4 d'épaisseur e, typiquement constante. La planche 4 présente une partie centrale annulaire 5 à travers laquelle peut passer l'arbre sur lequel est destiné à être monté le balancier 1, une serge, par exemple comprenant deux parties 6a et 6b en forme d'arcs de cercle diamétralement opposées, des bras 7 reliant la partie centrale 5 aux deux parties 6a, 6b de la serge et, dans chacune des parties 6a, 6b de la serge, des cavités 8 dans lesquelles sont situées les parties métalliques 3. La structure 2 comprend aussi des rebords 9 faisant saillie sur la surface supérieure de la planche 4. Ces rebords 9 prolongent en hauteur la paroi des cavités 8, permettant aux cavités 8 et donc aux parties métalliques 3 qui les remplissent d'avoir une plus grande hauteur ou épaisseur que l'épaisseur e de la planche 4. Chacune des cavités 8 et des parties métalliques 3 a une forme allongée et courbe qui suit le contour en arc de cercle de la partie 6a ou 6b de la serge dans laquelle elle se trouve. Le nombre et les dimensions des parties métalliques 3 peuvent varier. Leur fonction est d'alourdir la serge afin d'augmenter le rapport moment d'inertie sur masse du balancier 1.Structure 2 comprises a board 4 of thickness e, typically constant. The board 4 has an annular central part 5 through which the shaft on which the balance 1 is intended to be mounted can pass, a rim, for example comprising two parts 6a and 6b in the form of diametrically opposed arcs of a circle, arm 7 connecting the central part 5 to the two parts 6a, 6b of the serge and, in each of the parts 6a, 6b of the serge, cavities 8 in which the metal parts 3 are located. The structure 2 comprises also edges 9 projecting from the upper surface of the board 4. These edges 9 extend in height the wall of the cavities 8, allowing the cavities 8 and therefore the metal parts 3 which fill them to have a greater height or thickness than the thickness e of the board 4. Each of the cavities 8 and the metal parts 3 has an elongated and curved shape which follows the arcuate contour of the part 6a or 6b of the serge in which it is located. The number and dimensions of the metal parts 3 may vary. Their function is to weigh down the serge in order to increase the moment of inertia to mass ratio of the balance 1.

Enfin, la structure 2 comprend quatre tétons 10 portant chacun une masselotte 11, lesdites masselottes 11 permettant le réglage du moment d'inertie du balancier 1. Ces masselottes 11 sont typiquement maintenues sur les tétons 10 par serrage élastique. Le serrage élastique est tel que chacune d'elles est apte à pivoter autour du téton qui la porte pour le réglage de l'inertie du balancier 1.Finally, the structure 2 comprises four pins 10 each carrying a weight 11, said weights 11 allowing the adjustment of the moment of inertia of the balance 1. These weights 11 are typically held on the pins 10 by elastic tightening. The elastic tightening is such that each of them is able to pivot around the pin which carries it for adjusting the inertia of the balance 1.

A l'exception des parties métalliques 3 et des masselottes 11 qui sont rapportées, le balancier 1 peut être entièrement monolithique. La structure 2 est donc typiquement monolithique. Elle est réalisée en un matériau de base 12, par exemple du silicium, recouvert d'un revêtement 13 destiné à augmenter la résistance mécanique du balancier 1, notamment sa résistance aux chocs. Le revêtement 13 est, par exemple, une couche d'oxyde de silicium.With the exception of the metal parts 3 and the weights 11 which are attached, the balance 1 can be entirely monolithic. Structure 2 is therefore typically monolithic. It is made of a base material 12, for example silicon, covered with a coating 13 intended to increase the mechanical resistance of the balance 1, in particular its resistance to shocks. The coating 13 is, for example, a layer of silicon oxide.

Le balancier 1 est fabriqué selon un procédé similaire à celui décrit dans la demande de brevet WO 2008/135817 de la présente demanderesse. Ainsi, une plaque du matériau de base 12 est gravée, de préférence par gravure ionique réactive profonde DRIE, pour former un lot de pièces ayant chacune la forme de la structure 2, chacune de ces pièces étant attachée au reste de la plaque par des attaches ou ponts de matière laissés pendant la gravure. Ensuite, le revêtement 13 est formé sur toutes les surfaces de la plaque, y compris les surfaces des pièces et des attaches. Puis les parties métalliques 3 sont formées dans des cavités définies par les pièces revêtues, à savoir les cavités 8, typiquement par électro-formage (croissance galvanique). Enfin, les pièces sont détachées de la plaque et les masselottes de réglage 11 sont montées sur le balancier 1.The balance wheel 1 is manufactured using a process similar to that described in the patent application WO 2008/135817 of the present plaintiff. Thus, a plate of the base material 12 is etched, preferably by DRIE deep reactive ion etching, to form a batch of parts each having the shape of the structure 2, each of these parts being attached to the rest of the plate by fasteners or bridges of material left during engraving. Then the coating 13 is formed on all surfaces of the plate, including the surfaces of parts and fasteners. Then the metal parts 3 are formed in cavities defined by the coated parts, namely the cavities 8, typically by electroforming (galvanic growth). Finally, the parts are detached from the plate and the adjustment weights 11 are mounted on the balance 1.

Dans le cas d'un revêtement 13 d'oxyde de silicium sur un matériau de base 12 constitué de silicium, le revêtement 13 peut être formé en appliquant un traitement thermique à la plaque pour oxyder ses surfaces, comme dans la demande de brevet WO 2008/135817 . Dans les autres cas, le revêtement 13 peut être formé par exemple par un dépôt chimique en phase vapeur ou un dépôt physique en phase vapeur.In the case of a coating 13 of silicon oxide on a base material 12 consisting of silicon, the coating 13 can be formed by applying a heat treatment to the plate to oxidize its surfaces, as in the patent application WO 2008/135817 . In other cases, the coating 13 can be formed for example by chemical vapor deposition or physical vapor deposition.

Le détachement des pièces de la plaque créé des surfaces d'extrémité 15 fragiles, dépourvues du revêtement 13. Dans le cadre de l'invention, le détachement est typiquement effectué d'une manière qui laisse des parties d'attaches 14 sur les pièces afin de limiter la propagation d'amorces de rupture qui pourraient se produire sur ces surfaces « fragiles », comme décrit dans la demande EP 2 503 404 . Ainsi, comme montré aux figures 1 à 4a, lesdites parties d'attaches 14 font saillie sur la tranche 2.3 de chaque pièce. Chacune d'elles est couverte par le revêtement 13 sauf sur la partie de sa tranche 2.3 correspondant à sa surface d'extrémité 15 créée par le détachement des pièces de la plaque (figure 4a). La longueur des parties d'attache 14 est typiquement supérieure ou égale à sa largeur et/ou à son épaisseur mesurées au niveau de la surface d'extrémité 15, comme décrit dans la demande EP 2 503 404 .The detachment of the parts from the plate creates fragile end surfaces 15, devoid of the coating 13. In the context of the invention, the detachment is typically carried out in a manner which leaves attachment parts 14 on the parts in order to to limit the propagation of the beginnings of rupture which could occur on these “fragile” surfaces, as described in the request EP 2 503 404 . Thus, as shown in figures 1 to 4a , said attachment parts 14 project onto edge 2.3 of each part. Each of them is covered by the coating 13 except on the part of its edge 2.3 corresponding to its end surface 15 created by the detachment of the parts from the plate ( figure 4a ). The length of the attachment parts 14 is typically greater than or equal to its width and/or its thickness measured at the level of the end surface 15, as described in the application EP 2 503 404 .

Dans la présente invention, la position des tétons 10 et les dimensions des masselottes 11 sont telles que, en vue de dessus, chacune des masselottes 11 s'étend à l'extérieur de la tranche 2.3 de la structure 2 au niveau d'une partie d'attache 14 distincte en couvrant au moins partiellement la partie 15 de la tranche de cette attache 14 dépourvue de revêtement 13. Le tout est agencé de sorte que cela soit le cas quelle que soit la position de réglage de la masselotte 11 considérée.In the present invention, the position of the pins 10 and the dimensions of the weights 11 are such that, in top view, each of the weights 11 extends outside the section 2.3 of the structure 2 at the level of a part separate attachment 14 by at least partially covering the part 15 of the edge of this attachment 14 devoid of covering 13. The whole is arranged so that this is the case whatever the adjustment position of the weight 11 considered.

Chaque masselotte de réglage 11 joue ainsi un rôle protecteur en limitant la possibilité de chocs directs sur les parties «fragiles » 15 de la tranche 2.3 du balancier 1 qui pourraient survenir lors de son stockage, de son transport ou de son montage dans un mécanisme horloger ou encore après ledit montage, au cours du fonctionnement normal dudit mécanisme horloger.Each adjustment weight 11 thus plays a protective role by limiting the possibility of direct shocks on the “fragile” parts 15 of section 2.3 of the balance 1 which could occur during its storage, transport or assembly in a watch mechanism or after said assembly, during the normal operation of said watch mechanism.

La figure 2 illustre une partie d'un mécanisme horloger comprenant, entre autres, une platine 16 sur laquelle sont montés le balancier 1 et un mécanisme d'arrêt de balancier 20, également appelé « stop-seconde » ou « stop-balancier ». Le stop-balancier 20 comprend un bras élastique 21 actionnable par la tige de mise à l'heure (non illustrée) du mécanisme et dont l'extrémité est destinée à venir coopérer directement avec la périphérie du balancier 1 pour arrêter son oscillation par friction, et cela quel que soit sa position. Il est possible qu'il vienne le frapper directement en regard d'une de ses attaches 14 présentant une zone 15 fragile.There figure 2 illustrates part of a watch mechanism comprising, among other things, a plate 16 on which the balance 1 is mounted and a balance stop mechanism 20, also called “stop-second” or “stop-balance”. The balance stop 20 comprises an elastic arm 21 actuable by the time setting rod (not shown) of the mechanism and whose end is intended to cooperate directly with the periphery of the balance 1 to stop its oscillation by friction, and this regardless of its position. It is possible that it hits it directly next to one of its attachments 14 presenting a fragile zone 15.

Comme on peut le voir aux figures 4a et 4b, le bras 21 du stop-balancier 20 présente généralement une épaisseur ou hauteur h correspondant à la somme de l'épaisseur e de la planche 4 et de l'épaisseur e' de sa masselotte et est agencé de sorte que s'il frappe le balancier 1 au niveau d'une partie fragile 15 de sa tranche 2.3, le choc se fait sur la masselotte 11 et non sur ladite partie fragile 15. Dans d'autres positions du balancier 1, le bras 21 viendrait typiquement frapper directement sur une partie de la tranche 2.3 portant le revêtement 13 ou bien sur une autre des quatre masselottes 11.As we can see in figures 4a and 4b , the arm 21 of the balance stop 20 generally has a thickness or height h corresponding to the sum of the thickness e of the board 4 and the thickness e' of its flyweight and is arranged so that if it hits the balance 1 at the level of a fragile part 15 of its edge 2.3, the impact is on the flyweight 11 and not on said fragile part 15. In other positions of the balance 1, the arm 21 would typically strike directly on a part of section 2.3 carrying the covering 13 or on another of the four weights 11.

La hauteur h du bras 21 de balancier pourrait être différente à partir du moment où la fonction de protection est assurée. Typiquement, le bras 21 est agencé pour que, une fois monté dans le mécanisme horloger, il soit horizontalement en regard à la fois d'au moins une partie de la tranche 2.3 de la planche 4 du balancier 1 et d'au moins une partie des masselottes 11.The height h of the balance arm 21 could be different from the moment the protection function is ensured. Typically, the arm 21 is arranged so that, once mounted in the watch mechanism, it is horizontally facing both at least part of the section 2.3 of the board 4 of the balance 1 and at least one part weights 11.

En plus de son rôle protecteur limitant la possibilité de chocs directs sur les parties «fragiles » 15 de la tranche 2.3 du balancier 1 qui pourraient survenir depuis sa fabrication et jusqu'à son montage dans un mécanisme horloger, les masselottes 11 ont un rôle protecteur vis-à-vis des chocs contre le bras 21 du stop-balancier 20. De cette façon, le risque de rupture ou d'endommagement majeur du balancier 1 lors de l'actionnement du stop-balancier 20 est significativement réduit.In addition to its protective role limiting the possibility of direct impacts on the “fragile” parts 15 of section 2.3 of the balance 1 which could occur from its manufacture and until its assembly in a watch mechanism, the weights 11 have a protective role with respect to impacts against the arm 21 of the balance stop 20. In this way, the risk of breakage or major damage to the balance 1 during actuation of the balance stop 20 is significantly reduced.

Au vu de ce qui précède, les masselottes 11 ont donc un rôle double, elles servent à la fois d'organe protecteur ou « bouclier » mécanique du balancier 1 contre des chocs qui peuvent être imprévisibles (transport, montage ...) ou prévisibles (chocs répétés contre un stop-balancier par exemple) et d'organe de réglage de l'inertie.In view of the above, the weights 11 therefore have a dual role, they serve both as a protective member or mechanical “shield” of the balance 1 against shocks which may be unpredictable (transport, assembly, etc.) or predictable. (repeated impacts against a balance stop for example) and inertia adjustment member.

Pour satisfaire leur rôle double, les masselottes 11 doivent avoir une masse volumique élevée pour apporter de l'inertie au balancier 1 et de préférence une résistance mécanique élevée. Si elles sont typiquement réalisées en un alliage cuivre - béryllium, les autres matériaux traditionnellement utilisés pour la réalisation de masselottes de réglage, comme l'or, le platine, l'acier, le nickel ou un alliage nickel-phosphore conviennent tout à fait dans le cadre de l'invention.To satisfy their dual role, the weights 11 must have a high density to provide inertia to the balance 1 and preferably high mechanical resistance. If they are typically made of a copper - beryllium alloy, other materials traditionally used for the production of adjustment weights, such as gold, platinum, steel, nickel or a nickel-phosphorus alloy are quite suitable in the scope of the invention.

En variante, il est envisageable de réaliser un balancier 1 selon l'invention dont les parties d'attache 14 auraient été éliminées complètement, typiquement par abrasion, les parties fragiles 15 de la tranche 2.3 non recouvertes du revêtement 13 affleureraient alors le reste de la tranche 2.3. Dans ce cas, la position des tétons 10 et les dimensions des masselottes 11 seraient telles que, en vue de dessus, chacune des masselottes 11 s'étendrait à l'extérieur de la tranche 2.3 de la structure 2 au niveau d'une de ses parties 15 dépourvue de revêtement distincte, en couvrant au moins partiellement ladite partie 15, le tout étant agencé de sorte que cela soit le cas quelle que soit la position de réglage de la masselotte 11 considérée.As a variant, it is possible to produce a balance wheel 1 according to the invention whose attachment parts 14 would have been completely eliminated, typically by abrasion, the fragile parts 15 of section 2.3 not covered with coating 13 would then be flush with the rest of section 2.3. In this case, the position of the pins 10 and the dimensions of the weights 11 would be such that, in top view, each of the weights 11 would extend outside the section 2.3 of the structure 2 at the level of one of its parts 15 devoid of distinct coating, by at least partially covering said part 15, the whole being arranged so that this is the case whatever the adjustment position of the weight 11 considered.

Dans une variante du procédé de fabrication du balancier 1 selon l'invention, les masselottes de réglage 11 pourraient être montées sur les tétons 10 avant la rupture des attaches.In a variant of the method of manufacturing the balance 1 according to the invention, the adjustment weights 11 could be mounted on the pins 10 before the fasteners break.

Dans l'exemple illustré aux figures 1 à 4b, la structure 2 comprend quatre parties fragiles 15 et quatre tétons 10 portant chacun une masselotte de réglage 11, chacune desdites masselottes 11 protégeant une desdites parties fragiles 15. Il est clair que la structure 2 pourrait comprendre un nombre différent de parties fragiles 15 et de masselottes et que seulement certaines parties fragiles 15 pourraient être protégées par des masselottes ou bien que seulement certaines masselottes 11 protègent une partie fragile 15.In the example illustrated in figures 1 to 4b , the structure 2 comprises four fragile parts 15 and four pins 10 each carrying an adjustment weight 11, each of said weights 11 protecting one of said fragile parts 15. It is clear that the structure 2 could comprise a different number of fragile parts 15 and weights and that only certain fragile parts 15 could be protected by weights or that only certain weights 11 protect a fragile part 15.

Dans un autre mode de réalisation, le composant selon l'invention est un marteau d'horlogerie et son organe de réglage est un excentrique permettant le réglage de sa position de repos contre une butée.In another embodiment, the component according to the invention is a watchmaking hammer and its adjustment member is an eccentric allowing the adjustment of its rest position against a stop.

En référence à la figure 5, dans encore un autre mode de réalisation, le composant selon l'invention est balancier 100 comprenant une structure composite 102, typiquement en silicium recouvert d'oxyde de silicium, comprenant une face supérieure, une face inférieure et une tranche. Une partie dite fragile 115 de cette tranche, correspondant à la surface créée par la cassure d'une attache de fabrication 114, est dépourvue de revêtement. La structure 102 comprend des tétons 110 portant des rondelles d'inertie dont l'une d'elles 111 est positionnée de sorte que, en vue de dessus, elle s'étend à l'extérieur de la tranche de la structure au niveau de ladite partie fragile 115 en couvrant totalement ladite partie. Cette rondelle d'inertie a un rôle double, à la fois protecteur en ce qu'elle limite la possibilité de chocs directs sur la partie fragile 115 et à la fois d'alourdissement pour augmenter l'inertie du balancier 100. Avantageusement, la partie fragile 115 de la tranche de la structure 102 se situe en retrait dans cette structure, dans une échancrure de sa tranche, de manière à limiter davantage la possibilité de chocs directs sur la partie fragile 115.In reference to the Figure 5 , in yet another embodiment, the component according to the invention is a balance wheel 100 comprising a composite structure 102, typically made of silicon covered with silicon oxide, comprising an upper face, a lower face and a edge. A so-called fragile part 115 of this slice, corresponding to the surface created by the breakage of a manufacturing fastener 114, is devoid of coating. The structure 102 comprises pins 110 carrying inertia washers, one of which 111 is positioned so that, in top view, it extends outside the edge of the structure at the level of said fragile part 115 by completely covering said part. This inertia washer has a dual role, both protective in that it limits the possibility of direct shocks on the fragile part 115 and both weighting to increase the inertia of the balance 100. Advantageously, the part fragile 115 of the edge of the structure 102 is set back in this structure, in a notch in its edge, so as to further limit the possibility of direct impacts on the fragile part 115.

Outre sa grande précision, liée à la précision de son étape (a) de gravure, le procédé de fabrication selon l'invention permet de réaliser un grand nombre de composants simultanément à partir d'une même plaquette.In addition to its high precision, linked to the precision of its engraving step (a), the manufacturing process according to the invention makes it possible to produce a large number of components simultaneously from the same wafer.

Bien que l'invention ait été décrite ci-dessus pour des pièces en silicium recouvertes d'oxyde de silicium, elle pourrait être appliquée à d'autres matériaux composites tels que le verre trempé.Although the invention was described above for silicon parts coated with silicon oxide, it could be applied to other composite materials such as tempered glass.

Quel que soit le composant horloger réalisé, il est envisageable de graver la pièce de base de ce composant de sorte que la partie de la tranche de cette pièce dépourvue de revêtement à l'issue du procédé de fabrication se trouve en retrait dans le composant, typiquement dans une échancrure de ladite tranche, comme dans le cas du balancier 100 illustré à la figure 5. Ainsi, ladite partie dépourvue de revêtement se trouve doublement protégée, par l'organe de réglage et par le reste de la tranche de sa pièce de base.Whatever the watch component produced, it is possible to engrave the base part of this component so that the part of the edge of this part devoid of coating at the end of the manufacturing process is recessed in the component, typically in a notch of said slice, as in the case of the balance 100 illustrated in figure 5 . Thus, said part devoid of coating is doubly protected, by the adjustment member and by the rest of the edge of its base part.

En plus des nombreux avantages évoqués plus haut, dans le cas préféré où des parties d'attaches sont laissées sur le composant final, le composant horloger selon l'invention présente un avantage esthétique en ce qu'il permet de cacher ces parties d'attaches.In addition to the numerous advantages mentioned above, in the preferred case where attachment parts are left on the final component, the watch component according to the invention has an aesthetic advantage in that it allows these attachment parts to be hidden. .

Claims (15)

  1. Timepiece component (1; 100) comprising a composite piece (2; 102) comprising an upper face (2.1), a lower face (2.2) and an edge (2.3), and being made from a first material (12) and coated with a second material (13) to increase the mechanical strength thereof, at least one part (15; 115) of its edge (2.3) being free of this coating (13), said timepiece component (1; 100) being characterised in that it comprises a protective member (11; 111) which, as seen from above or from below, extends outside of the edge (2.3) of the piece at said part (15; 115), at least partially covering said part (15; 115).
  2. Timepiece component (1; 100) as claimed in claim 1, characterised in that, as seen from above or from below, said protective member (11; 111) extends outside of the edge (2.3) of the piece (2; 102) at said part (15, 115), completely covering said part (15; 115).
  3. Timepiece component (1; 100) as claimed in claim 1 or 2, characterised in that, in addition to limiting the possibility of direct impacts on said part (15; 115), said protective member (11; 111) has a function such as a weighing-down function, a setting function or a modifying function for the tribological properties of said composite piece.
  4. Timepiece component (1) as claimed in claim 3, characterised in that said protective member (11) is a setting member, and in that, as seen from above or from below, it extends outside of the edge (2.3) of the piece (2) at said part (15), at least partially covering said part (15), regardless of its setting position.
  5. Timepiece component (1; 100) as claimed in any one of the preceding claims, characterised in that said first material (12) is made of silicon.
  6. Timepiece component (1; 100) as claimed in any one of the preceding claims, characterised in that said second material (13) is selected from silicon dioxide, carbide or nitride, titanium nitride or carbide, or diamond, preferably silicon dioxide.
  7. Timepiece component (1; 100) as claimed in any one of the preceding claims, characterised in that said protective member (11; 111) is produced based on metal, preferably from a nickel-phosphorous or copper-beryllium alloy, from gold, from platinum, from steel or from nickel.
  8. Timepiece component (1) as claimed in any one of claims 1 to 7, characterised in that it is a balance, and in that said protective member (11) comprises an inertia-block for setting the inertia of the balance.
  9. Timepiece component (100) as claimed in any one of the preceding claims, characterised in that said part (115) of the edge free of coating is recessed in the component, typically in a notch in the edge of said composite piece (102).
  10. Timepiece component (1) as claimed in any one of the preceding claims, characterised in that said composite piece comprises several parts (15) of its edge (2.3) which are free of coating (13) and at least as many protective members (11) as said parts (15), the whole being arranged such that a separate protective member (11) is associated with each of said parts (15) free of coating.
  11. Timepiece mechanism comprising a first timepiece component (1) as claimed in any one of claims 1 to 10 and a second timepiece component (20) intended to cooperate directly with said first timepiece component (1) when said mechanism is operating, characterised in that the second timepiece component (20) can contact the first timepiece component (1) only via one part of its edge (2.3) bearing the coating (13) or via a protective member (11), regardless of the setting position of the settable protective member(s) (11) if present.
  12. Timepiece mechanism as claimed in claim 11, characterised in that the part of said second timepiece component (20) intended to cooperate directly with said first timepiece component (1) is horizontally facing both at least one part of the edge (2.3) of said first component (1) and at least one part of the or each protective member.
  13. Timepiece mechanism as claimed in claim 11 or 12 when dependent on claim 8, characterised in that said second timepiece component comprises a balance stopping mechanism (20).
  14. Timepiece such as a wristwatch, a pocket-watch, a clock or a miniature clock comprising a timepiece mechanism as claimed in any one of claims 11 to 13.
  15. Method for manufacturing a timepiece component (1) ready to be mounted in a timepiece mechanism, comprising the following steps:
    a. etching a piece having a desired shape for the component (1) in a plate of a first material (12), leaving at least one tie between the piece and the rest of the plate, said piece comprising an upper face (2.1), a lower face (2.2) and an edge (2.3),
    b. coating the plate with a second material (13) intended to increase the mechanical strength of the piece and thereby covering the part and the tie(s),
    c. detaching the piece from the plate by separating the tie(s), then optionally removing the remaining tie portion(s) (14), one or more parts (15) of the edge (2.3) of the piece thus being free of said coating (13),
    d. attaching at least one protective member (11) to the piece (2) such that, as seen from above or from below, said protective member (11) extends outside of the edge (2.3) of the piece (2) at the part (15) or one of the parts (15) of its edge (2.3) which is or are free of coating (13), at least partially covering said part (15),
    wherein steps c) and d) can be inverted.
EP19211198.7A 2019-11-25 2019-11-25 Reinforced timepiece component Active EP3825782B1 (en)

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EP19211198.7A EP3825782B1 (en) 2019-11-25 2019-11-25 Reinforced timepiece component

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Application Number Priority Date Filing Date Title
EP19211198.7A EP3825782B1 (en) 2019-11-25 2019-11-25 Reinforced timepiece component

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EP3825782A1 EP3825782A1 (en) 2021-05-26
EP3825782B1 true EP3825782B1 (en) 2023-11-15

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Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2506093B1 (en) * 2011-03-30 2014-04-09 Patek Philippe SA Genève Balance for clockwork
EP3182213B1 (en) * 2015-12-16 2018-09-12 Société anonyme de la Manufacture d'Horlogerie Audemars Piguet & Cie Mechanism for adjusting an average speed in a clock movement and clock movement
EP2503404B1 (en) * 2011-03-23 2019-05-01 Patek Philippe SA Genève Method for manufacturing a mechanical component, in particular an horological component

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8339904B2 (en) 2005-06-28 2012-12-25 Eta Sa Manufacture Horlogère Suisse Reinforced micro-mechanical part
CH714952B1 (en) 2007-05-08 2019-10-31 Patek Philippe Sa Geneve Watchmaking component, its method of manufacture and application of this method.
EP2337221A1 (en) * 2009-12-15 2011-06-22 The Swatch Group Research and Development Ltd. Resonator thermocompensated at least to the first and second orders
CH702799B1 (en) * 2010-03-04 2012-12-31 Montres Breguet Sa Timepiece including a high-frequency mechanical motion.

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2503404B1 (en) * 2011-03-23 2019-05-01 Patek Philippe SA Genève Method for manufacturing a mechanical component, in particular an horological component
EP2506093B1 (en) * 2011-03-30 2014-04-09 Patek Philippe SA Genève Balance for clockwork
EP3182213B1 (en) * 2015-12-16 2018-09-12 Société anonyme de la Manufacture d'Horlogerie Audemars Piguet & Cie Mechanism for adjusting an average speed in a clock movement and clock movement

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