EP2881804B1 - Hairspring-stud assembly for timepiece - Google Patents

Hairspring-stud assembly for timepiece Download PDF

Info

Publication number
EP2881804B1
EP2881804B1 EP14194961.0A EP14194961A EP2881804B1 EP 2881804 B1 EP2881804 B1 EP 2881804B1 EP 14194961 A EP14194961 A EP 14194961A EP 2881804 B1 EP2881804 B1 EP 2881804B1
Authority
EP
European Patent Office
Prior art keywords
thickness
balance spring
stud
component
gap
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
EP14194961.0A
Other languages
German (de)
French (fr)
Other versions
EP2881804A3 (en
EP2881804A2 (en
Inventor
Gaëtan Villard
Lucien Germond
Polychronis Nakis Karapatis
Stéphane Beugin
Sylvain Maréchal
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.)
Montres Breguet SA
Original Assignee
Montres Breguet 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
Priority claimed from EP13196153.4A external-priority patent/EP2881803B1/en
Application filed by Montres Breguet SA filed Critical Montres Breguet SA
Priority to EP14194961.0A priority Critical patent/EP2881804B1/en
Publication of EP2881804A2 publication Critical patent/EP2881804A2/en
Publication of EP2881804A3 publication Critical patent/EP2881804A3/en
Priority to US14/873,533 priority patent/US9367038B1/en
Priority to JP2015216431A priority patent/JP6018686B2/en
Priority to CN201510829127.9A priority patent/CN105629698B/en
Application granted granted Critical
Publication of EP2881804B1 publication Critical patent/EP2881804B1/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
    • G04B17/32Component parts or constructional details, e.g. collet, stud, virole or piton
    • G04B17/325Component parts or constructional details, e.g. collet, stud, virole or piton for fastening the hairspring in a fixed position, e.g. using a block
    • 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
    • G04B13/00Gearwork
    • G04B13/02Wheels; Pinions; Spindles; Pivots
    • 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
    • G04B15/00Escapements
    • G04B15/06Free escapements
    • 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
    • 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
    • G04B19/00Indicating the time by visual means
    • G04B19/04Hands; Discs with a single mark or the like
    • G04B19/044Mounting and setting of the hands on the axle
    • 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
    • G04B18/02Regulator or adjustment devices; Indexing devices, e.g. raquettes
    • G04B18/026Locking the hair spring in the indexing device, e.g. goupille of the raquette
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49579Watch or clock making
    • Y10T29/49581Watch or clock making having arbor, pinion, or balance

Description

Domaine de l'inventionField of the invention

L'invention concerne un ensemble comportant un spiral lequel comporte deux surfaces latérales opposées distantes d'une épaisseur de référence, et un piton comportant un logement dimensionné pour la réception dudit spiral, ledit piton comportant, autour dudit logement, au moins un composant monolithique en alliage à mémoire de forme comportant au moins deux pattes définissant ensemble un entrefer et chacune agencée pour prendre appui sur une desdites surfaces latérales opposées dudit spiral, et où à l'état libre, la largeur minimale dudit entrefer est supérieure à la valeur maximale de ladite épaisseur de référence quand ledit composant est dans une position ouverte correspondant à une structure martensitique, et où la largeur maximale dudit entrefer est inférieure à la valeur minimale de ladite épaisseur de référence quand ledit composant est dans une position fermée correspondant à une structure austénitique.The invention relates to an assembly comprising a spiral which comprises two opposite lateral surfaces distant from a reference thickness, and a stud having a housing dimensioned for receiving said spiral, said stud having, around said housing, at least one monolithic component in shape memory alloy having at least two tabs together defining an air gap and each arranged to bear on one of said opposite side surfaces of said hairspring, and wherein in the free state, the minimum width of said air gap is greater than the maximum value of said reference thickness when said component is in an open position corresponding to a martensite structure, and wherein the maximum width of said gap is less than the minimum value of said reference thickness when said component is in a closed position corresponding to an austenitic structure.

L'invention concerne encore un mouvement d'horlogerie comportant au moins un tel ensemble.The invention also relates to a watch movement comprising at least one such set.

L'invention concerne encore une pièce d'horlogerie comportant au moins un tel mouvement ou/et au moins un tel ensemble.The invention also relates to a timepiece comprising at least one such movement and / or at least one such set.

L'invention concerne encore un procédé de fixation d'un spiral à un piton.The invention further relates to a method of attaching a hairspring to a peg.

L'invention concerne le domaine des mécanismes oscillateurs mécaniques d'horlogerie, comportant un ressort-spiral.The invention relates to the field of mechanical clockwork oscillator mechanisms, comprising a spiral spring.

Arrière-plan de l'inventionBackground of the invention

Les mécanismes oscillateurs mécaniques d'horlogerie, comportant un ressort-spiral, comportent en général un piton pour la fixation de l'extrémité externe du ressort-spiral.Mechanical clockwork oscillator mechanisms, comprising a spiral spring, generally comprise a pin for fixing the outer end of the spiral spring.

La fixation du spiral au piton se fait en général par collage, ce qui n'est pas parfaitement reproductible, et peut entraîner une pollution du mouvement d'horlogerie.The attachment of the hairspring to the pin is usually done by gluing, which is not perfectly reproducible, and can lead to pollution of the watch movement.

Le document CH317531 A au nom de EBAUCHES BETTLACH SA décrit un piton à fente, dans une matière déformable plastiquement de façon à solidariser à demeure le piton et le spiral.The document CH317531 A in the name of EBAUCHES BETTLACH SA describes a slotted stud, in a plastically deformable material so as to permanently secure the stud and the spiral.

Le document EP1580625A1 au nom de ASULAB SA décrit la fixation d'une levée dans un logement d'une ancre, la portion comportant ce logement est dans un alliage à mémoire de forme apte à subir une transformation réversible entre une phase austénitique et une phase martensitique.The document EP1580625A1 in the name of ASULAB SA describes the fixing of a lift in a housing of an anchor, the portion comprising this housing is in a shape memory alloy capable of undergoing a reversible transformation between an austenitic phase and a martensitic phase.

Résumé de l'inventionSummary of the invention

L'invention se propose de fournir une alternative au collage du spiral dans le piton, et de le remplacer par une fixation reproductible du spiral, moins dépendante de l'opérateur effectuant l'assemblage.The invention proposes to provide an alternative to the gluing of the hairspring in the eye, and to replace it with a reproducible fixation of the hairspring, less dependent on the operator performing the assembly.

A cet effet, l'invention concerne un ensemble comportant un spiral lequel comporte deux surfaces latérales opposées distantes d'une épaisseur de référence, et tel piton dimensionné pour recevoir ledit spiral, selon la revendication 1.To this end, the invention relates to an assembly comprising a hairspring which comprises two opposite side surfaces remote from a reference thickness, and such piton sized to receive said hairspring according to claim 1.

L'invention concerne encore un mouvement d'horlogerie comportant au moins un tel ensemble.The invention also relates to a watch movement comprising at least one such set.

L'invention concerne encore une pièce d'horlogerie comportant au moins un tel mouvement ou/et au moins un tel ensemble.The invention also relates to a timepiece comprising at least one such movement and / or at least one such set.

L'invention concerne encore un procédé de fixation d'un spiral à un piton, selon la revendication 10.The invention further relates to a method of fixing a hairspring to a peg, according to claim 10.

L'invention concerne encore un autre procédé de fixation d'un spiral à un piton, selon la revendication 11.The invention also relates to another method of fixing a hairspring to a peg, according to claim 11.

Description sommaire des dessinsBrief description of the drawings

D'autres caractéristiques et avantages de l'invention apparaîtront à la lecture de la description détaillée qui va suivre, en référence aux dessins annexés, où :

  • la figure 1 représente, de façon schématisée et selon une coupe transversale du spiral, un spiral présenté dans un logement que comporte un piton à géométrie variable selon l'invention, lequel piton est dans une position ouverte ;
  • la figure 2 représente, de façon similaire à la figure 1, le même ensemble constitué du piton et du spiral, dans une position fermée du piton où le spiral est pincé entre deux pattes du piton ;
  • la figure 3 représente, de façon similaire à la figure 2, un tel ensemble oû le spiral est en position de butée sur une face d'appui du piton, et dans une position fermée du piton où le spiral est pincé entre deux pattes du piton ;
  • la figure 4 représente, de façon schématisée et en perspective, à l'état libre, un piton selon l'invention, en position fermée, et comportant deux pattes avec un profil de forme ;
  • la figure 5 représente, de façon schématisée et en vue de dessous, le piton de la figure 4 coopérant en position fermée de pincement d'un spiral lequel comporte une succession de zones de moindre et de plus forte épaisseur ;
  • la figure 6 représente, sous forme d'un schéma-blocs, une montre comportant un mouvement comportant un ensemble lui-même formé d'un spiral et d'un piton selon l'invention.
Other features and advantages of the invention will appear on reading the detailed description which follows, with reference to the appended drawings, in which:
  • the figure 1 represents, schematically and in a cross sectional view of the hairspring, a hairspring presented in a housing that comprises a peg with variable geometry according to the invention, which bolt is in an open position;
  • the figure 2 represents, similarly to the figure 1 , the same set consisting of the stud and the spiral, in a closed position of the peak where the spiral is pinched between two legs of the piton;
  • the figure 3 represents, similarly to the figure 2 such a set where the hairspring is in abutment position on a bearing face of the pin, and in a closed position of the pin where the hairspring is pinched between two legs of the pin;
  • the figure 4 represents, schematically and in perspective, in the free state, a pin according to the invention, in the closed position, and having two tabs with a shape profile;
  • the figure 5 represents, schematically and in a view from below, the peak of the figure 4 cooperating in the closed pinch position of a spiral which comprises a succession of areas of smaller and thicker;
  • the figure 6 represents, in the form of a block diagram, a watch comprising a movement comprising a set itself formed of a spiral and a stud according to the invention.

Description détaillée des modes de réalisation préférésDetailed Description of the Preferred Embodiments

Les mécanismes oscillateurs mécaniques d'horlogerie, comportant un ressort-spiral dont l'extrémité externe est fixé à un piton, lui-même fixé à une platine, un pont, un coq ou similaire.Mechanical clock oscillator mechanisms, comprising a spiral spring whose outer end is fixed to a pin, itself attached to a plate, a bridge, a cock or the like.

L'invention se propose d'assurer une fixation reproductible du spiral, moins dépendante de l'opérateur effectuant l'assemblage, et de préférence réalisable avec des moyens de production automatisés tel qu'un robot d'assemblage ou similaire, effectuant la préhension et le positionnement relatif des composants entre eux, auxquels composant ce robot est susceptible d'appliquer sélectivement une chauffe ou un refroidissement de façon localisée et quasiment instantanée.The invention proposes to provide a reproducible fixation of the hairspring, less dependent on the operator performing the assembly, and preferably achievable with automated production means such as a robot assembly or the like, performing the gripping and the relative positioning of the components between them, to which this robot component is capable of selectively applying heating or cooling in a localized and almost instantaneous manner.

L'invention concerne ainsi un piton 1 d'horlogerie comportant un logement pour la réception d'un spiral 3, ce spiral 3 comportant classiquement deux surfaces latérales opposées 31, 32, distantes d'une épaisseur de référence ER.The invention thus relates to a clock 1 having a housing for receiving a hairspring 3, this hairspring 3 conventionally comprising two opposite lateral surfaces 31, 32, distant from a reference thickness ER.

Selon l'invention, ce piton 1 comporte, autour du logement , au moins un composant 8 monolithique en alliage à mémoire de forme.According to the invention, this stud 1 comprises, around the housing, at least one monolithic component 8 of shape memory alloy.

L'alliage à mémoire de forme peut être choisi parmi différentes familles de matériaux, notamment et non limitativement des alliages à mémoire de forme activés thermiquement, des alliages à mémoire de forme activés magnétiquement, ou encore des polymères à mémoire de forme.The shape memory alloy may be chosen from different families of materials, in particular and without limitation heat-activated shape memory alloys, magnetically activated shape memory alloys, or shape memory polymers.

L'invention est décrite ici dans un exemple particulier, non limitatif, avec un alliage à mémoire de forme activé thermiquement.The invention is described herein in a particular nonlimiting example with a thermally activated shape memory alloy.

On distingue généralement, pour de tels alliages à mémoire de forme, un état dit martensitique et un état dit austénitique, qui correspondent à des structurations différentes du matériau, et à des répartitions spatiales des atomes différentes dans l'espace.For such shape memory alloys, a so-called martensitic state and a so-called austenitic state, which correspond to different structuring of the material, and to spatial distributions of the different atoms in space, are generally distinguished.

Ce composant 8 comporte au moins deux pattes 11, 12, qui définissent ensemble un entrefer E et chacune agencée pour prendre appui sur une des surfaces latérales opposées 31, 32, d'un tel spiral 3.This component 8 comprises at least two lugs 11, 12, which together define an air gap E and each arranged to bear on one of the opposite lateral surfaces 31, 32, of such a hairspring 3.

A l'état libre, la largeur minimale de cet entrefer E est supérieure à la valeur maximale de l'épaisseur de référence ER quand le composant 8 est dans une position ouverte correspondant à une structure martensitique, et la largeur maximale de l'entrefer E est inférieure à la valeur minimale de l'épaisseur de référence ER quand le composant 8 est dans une position fermée correspondant à une structure austénitique.In the free state, the minimum width of this gap E is greater than the maximum value of the reference thickness ER when the component 8 is in an open position corresponding to a martensitic structure, and the maximum width of the gap E is less than the minimum value of the reference thickness ER when the component 8 is in a closed position corresponding to an austenitic structure.

Les figures 1 et 2 illustrent ces deux positions ouverte et fermée du composant 8 autour du spiral 3. Les pattes 11 et 12 pincent le spiral 3, de préférence avec un appui sur toute la hauteur des surfaces latérales 31 et 32 du spiral, et sur toute l'épaisseur L du piton 1.The Figures 1 and 2 illustrate these two open and closed positions of the component 8 around the hairspring 3. The lugs 11 and 12 pinch the hairspring 3, preferably with a bearing on the entire height of the lateral surfaces 31 and 32 of the hairspring, and over the entire thickness L piton 1.

Dans une exécution particulière, tel que visible sur la figure 3, le logement du piton 1 comporte une surface d'appui de butée axiale 9 agencée pour recevoir en appui un chant 33 d'un spiral 3.In a particular embodiment, as visible on the figure 3 , the piton housing 1 comprises an axial abutment support surface 9 arranged to receive a support 33 of a hairspring 3.

Dans une exécution particulière, tel que visible sur les figures 1 à 4, le piton 1 est monolithique avec le composant 8.In a particular embodiment, as visible on the Figures 1 to 4 , piton 1 is monolithic with component 8.

Dans une exécution particulière du piton 1, l'alliage à mémoire de forme est choisi de façon à ce que le piton 1 supporte, sans modification notable de son serrage, une température de service minimale TSMIN de -20°C.In a particular embodiment of the piton 1, the shape memory alloy is chosen so that the piton 1 supports, without significant modification of its clamping, a minimum service temperature TSMIN of -20 ° C.

Dans une autre exécution particulière du piton 1, l'alliage à mémoire de forme est choisi de façon à ce que le piton 1 supporte, sans modification notable de son serrage, une température de service maximale TSMAX de +70°C.In another particular embodiment of the piton 1, the shape memory alloy is chosen so that the piton 1 supports, without significant modification of its clamping, a maximum operating temperature TSMAX of + 70 ° C.

L'invention concerne encore un ensemble 10 comportant un tel spiral 3 lequel comporte deux surfaces latérales opposées 31, 32, distantes d'une épaisseur de référence ER, et un tel piton 1 dimensionné pour recevoir ce spiral 3. Dans une exécution particulière, tel que visible sur la figure 5, le spiral 3 comporte localement au moins une zone de moindre épaisseur 30 dont l'épaisseur minimale est l'épaisseur de référence ER, pour laquelle est conçu le piton 1, et qui est encadrée par des zones de forte épaisseur 35 dont l'épaisseur minimale est supérieure à l'épaisseur de référence ER.The invention also relates to an assembly 10 comprising such a hairspring 3 which comprises two opposite lateral surfaces 31, 32, remote by a reference thickness ER, and such a pin 1 sized to receive this hairspring 3. In a particular embodiment, such that visible on the figure 5 , the spiral 3 locally comprises at least one zone of lesser thickness, the minimum thickness of which is the reference thickness ER, for which the piton 1 is designed, and which is framed by areas of great thickness 35 whose minimum thickness is greater than the reference thickness ER.

Plus particulièrement, le spiral 3 comporte une alternance de telles zones de moindre épaisseur 30 et de telles zones de forte épaisseur 35, pour l'ajustement de la longueur active du spiral 3 par la coopération discrète du piton 1 avec l'une de ces zones de moindre épaisseur 30. Le spiral 3 peut, encore, être gradué au niveau de ces différentes positions d'ajustement en longueur active.More particularly, the spiral 3 comprises an alternation of such areas of lesser thickness and such thick zones 35, for the adjustment of the active length of the spiral 3 by the discrete cooperation of the stud 1 with one of these zones. The hairspring 3 can, again, be graduated at these different positions of adjustment in active length.

Dans une exécution particulière, chaque zone de moindre épaisseur 30 à une longueur sensiblement égale, légèrement supérieure, à l'épaisseur des pattes 11, 12, du piton 1.In a particular embodiment, each zone of lesser thickness 30 has a length substantially equal to, slightly greater than, the thickness of the lugs 11, 12, of the peak 1.

Dans une exécution particulière, illustrée par les figures 4 et 5, ces zones de moindre épaisseur 30 ont toutes le même profil, et en ce que les pattes 11, 12, du piton 1 ont chacune un profil complémentaire du profil du spiral 3 qui leur fait face dans chaque zone de moindre épaisseur 30.In a particular execution, illustrated by the Figures 4 and 5 these zones of lesser thickness 30 all have the same profile, and in that the lugs 11, 12, of the piton 1 each have a complementary profile of the spiral profile 3 which faces them in each zone of lesser thickness 30.

L'invention concerne encore un mouvement d'horlogerie 100 comportant au moins un tel piton 1, ou/et un tel ensemble 10.The invention also relates to a watch movement 100 comprising at least one such stud 1, or / and such an assembly 10.

L'invention concerne encore une pièce d'horlogerie 1000 comportant au moins un tel mouvement 100, ou/et au moins un tel piton 1, ou/et un tel ensemble 10.The invention also relates to a timepiece 1000 comprising at least one such movement 100, or / and at least one such pin 1, and / or such a set 10.

Le procédé d'assemblage comporte des phases successives :

  • une première phase de déformation initiale du composant 8 en alliage à mémoire de forme dans un état martensitique et à une température inférieure à une première température de début de transformation As, caractéristique du début de la transformation de la structure martensitique en structure austénitique lors d'un chauffage ;
  • suivie d'une deuxième phase de mise en coopération du composant 8 avec le spiral 3, toujours dans cet état martensitique et à une température inférieure à la première température de transformation As ;
  • une troisième phase, dans laquelle le serrage du composant 8 sur le spiral 3 est réalisé par le chauffage à une température supérieure à une deuxième température de fin de transformation Af, qui est caractéristique de la fin de la transformation de la structure martensitique en structure austénitique lors d'un chauffage, et qui est donc supérieure à la première température de transformation As. L'assemblage conserve ensuite sa force de serrage tant qu'il ne repasse pas en-dessous d'une troisième température de transformation Ms, qui est caractéristique du début de la transformation de la structure austénitique en structure martensitique lors d'un refroidissement (la fin de cette transformation correspondant à une quatrième température de transformation Mf). L'emploi d'un matériau à large hystérèse (différence entre Ms et As) permet par exemple un montage à une température de l'ordre de l'ambiante (voisine de 20°C), un chauffage limité et le serrage conserve ensuite ses propriétés sur une large plage d'utilisation.
The assembly process comprises successive phases:
  • a first phase of initial deformation of the shape memory alloy component 8 in a martensitic state and at a temperature below a first transformation start temperature As, characteristic of the beginning of the transformation of the martensitic structure into austenitic structure when a heater ;
  • followed by a second phase of cooperation of the component 8 with the spring 3, still in this martensitic state and at a temperature below the first transformation temperature As;
  • a third phase, in which the tightening of the component 8 on the spiral 3 is achieved by heating to a temperature higher than a second end-of-transformation temperature Af, which is characteristic of the end of the transformation of the martensitic structure into austenitic structure during heating, and which is therefore greater than the first transformation temperature As. The assembly then retains its clamping force as long as it does not pass again below a third transformation temperature Ms, which is characteristic of the beginning of the transformation of the austenitic structure into a martensitic structure during cooling (the end of this transformation corresponding to a fourth transformation temperature Mf). The use of a material with a large hysteresis (difference between Ms and As) makes it possible, for example, to mount at a temperature of the order of the ambient (close to 20 ° C.), a limited heating and the clamping then retains its properties over a wide range of use.

L'objectif est de ne pas descendre en-dessous de la température de transformation Ms lors du service, de façon à éviter de modifier le serrage par une éventuelle transformation de phase, même partielle (c'est-à-dire sans forcément atteindre la quatrième température de transformation Mf à laquelle la transformation de structure austénitique en structure martensitique est complètement réalisée).The objective is not to go below the transformation temperature Ms during the service, so as to avoid modifying the clamping by a possible phase transformation, even partial (that is to say without necessarily reaching the fourth transformation temperature Mf at which the transformation of austenitic structure into a martensitic structure is completely realized).

Dans un mode de réalisation, l'alliage à mémoire de forme constituant le composant 8 est choisi de façon à autoriser une température de service minimale TSMIN de -20°C.In one embodiment, the shape memory alloy constituting component 8 is selected to allow a minimum operating temperature TSMIN of -20 ° C.

Dans un deuxième mode de réalisation, l'alliage à mémoire de forme constituant le composant 8 est choisi de façon à autoriser une température de service maximale TSMAX de +70°C.In a second embodiment, the shape memory alloy constituting the component 8 is chosen so as to allow a maximum operating temperature TSMAX of + 70 ° C.

Les températures de transformation et de fixation doivent être assez basses pour empêcher le desserrage du spiral si la montre dans lequel il est incorporé reste au froid.The processing and fixing temperatures must be low enough to prevent loosening of the hairspring if the watch in which it is incorporated remains cold.

Dans une autre réalisation particulière on réalise le composant dans un des alliages titane nickel de type « Nitinol », selon une première forme à température inférieure à -40°C, et selon une deuxième forme à température ambiante comprise entre -20°C et +70°C, cette deuxième forme permettant d'assurer le serrage requis pour une friction correcte et contrôlée du spiral. Des outillages médicaux, et notamment d'orthodontie, permettent d'effectuer un refroidissement très rapide vers -50°C ou -60°C, voire à des températures encore inférieures, pour amener le composant dans la première forme qui permet son enfilage sur le corps de piton. Il suffit de ramener l'ensemble à la température de la salle de montage, classiquement voisine de +20°C, pour assurer le serrage du composant dans sa deuxième forme, et effectuer immédiatement l'essai de mesure de couple de friction permettant de valider le composant pour son utilisation directe dans un mouvement.In another particular embodiment, the component is produced in one of the "Nitinol" nickel titanium alloys, in a first form at a temperature below -40 ° C., and in a second form at an ambient temperature of between -20 ° C. and + 70 ° C, this second form to ensure the clamping required for a correct and controlled friction of the spiral. Medical tools, and in particular orthodontics, allow very rapid cooling to -50 ° C or -60 ° C, or even lower temperatures, to bring the component in the first form that allows its threading on the piton body. It is sufficient to reduce the assembly to the temperature of the assembly room, conventionally close to + 20 ° C, to ensure the tightening of the component in its second form, and immediately perform the torque measurement test. friction to validate the component for its direct use in a movement.

L'invention concerne encore un procédé d'assemblage facilement automatisable avec un robot manipulateur comportant des moyens de chauffe ou un refroidissement de façon localisée et quasiment instantanée, par lequel on effectue différentes étapes successives.The invention also relates to an assembly method that can be easily automated with a manipulator robot comprising heating means or cooling in a localized and almost instantaneous manner, by which different successive steps are carried out.

Selon l'invention, ce procédé de fixation d'un spiral 3 à un piton 1. comporte les étapes successives suivantes :

  • on réalise, pour la réception d'un spiral 3 d'épaisseur de référence ER, un tel piton 1 comportant, autour d'un logement prévu pour la réception de ce spiral 3, au moins un composant 8 monolithique en alliage à mémoire de forme comportant au moins deux pattes 11, 12, définissant ensemble un entrefer E où, à l'état libre du piton 1, la largeur minimale de l'entrefer E est supérieure à la valeur maximale de l'épaisseur de référence ER quand le composant 8 est dans une position ouverte dans une structure martensitique, et la largeur maximale de l'entrefer E est inférieure à la valeur minimale de l'épaisseur de référence ER quand le composant 8 est dans une position fermée dans une structure austénitique ;
  • on effectue une première phase de déformation d'ouverture du composant 8 dans un état martensitique et à une température inférieure à une première température de début de transformation As, caractéristique du début de la transformation de la structure martensitique en structure austénitique lors d'un chauffage ;
  • on introduit un spiral 3 dans le logement , dans une position déterminée ou jusqu'à l'atteinte d'une position de butée ;
  • on effectue une deuxième phase de déformation de fermeture du composant 8, dans laquelle on réalise le serrage des pattes 11, 12, sur le spiral 3 par le chauffage du composant 8 à une température supérieure à une deuxième température de fin de transformation Af.
According to the invention, this method of fixing a hairspring 3 to a pin 1. comprises the following successive steps:
  • for the reception of a hairspring 3 of reference thickness ER, there is provided such a peg 1 comprising, around a housing provided for receiving this hairspring 3, at least one monolithic component 8 made of a shape memory alloy. having at least two tabs 11, 12, together defining an air gap E where, in the free state of the piton 1, the minimum width of the gap E is greater than the maximum value of the reference thickness ER when the component 8 is in an open position in a martensitic structure, and the maximum width of the gap E is less than the minimum value of the reference thickness ER when the component 8 is in a closed position in an austenitic structure;
  • a first phase of opening deformation of the component 8 is carried out in a martensitic state and at a temperature below a first start transformation temperature As, characteristic of the beginning of the transformation of the martensitic structure into austenitic structure during heating ;
  • a hairspring 3 is introduced into the housing in a determined position or until a stop position is reached;
  • a second phase of closure deformation of the component 8, in which the tabs 11, 12 are tightened on the spring 3 by heating the component 8 to a temperature higher than a second end of transformation temperature Af.

Dans une variante de ce procédé de fixation d'un spiral 3 à un piton 1, le procédé comporte les étapes successives suivantes :

  • on réalise, pour la réception d'un spiral 3 d'épaisseur de référence ER, un tel piton 1 comportant, autour d'un logement prévu pour la réception du spiral 3, au moins un composant 8 monolithique en alliage à mémoire de forme comportant au moins deux pattes 11, 12, définissant ensemble un entrefer E où, à l'état libre du piton 1, la largeur minimale de l'entrefer E est supérieure à la valeur maximale de l'épaisseur de référence ER quand le composant 8 est dans une position ouverte dans une structure martensitique, et en ce que la largeur maximale de l'entrefer E est inférieure à la valeur minimale de l'épaisseur de référence ER quand le composant 8 est dans une position fermée dans une structure austénitique à une température de service ;
  • on effectue une première phase de déformation d'ouverture du composant 8 dans une structure martensitique ;
  • on insère le spiral 3 dans le logement, et on les positionne l'un par rapport à l'autre en position adéquate ;
  • on les maintient l'un et l'autre en position jusqu'au retour à la température ambiante.
In a variant of this method of fixing a hairspring 3 to a pin 1, the method comprises the following successive steps:
  • for the reception of a hairspring 3 of reference thickness ER, there is provided such a peak 1 comprising, around a housing provided for receiving the hairspring 3, at least one monolithic component 8 made of a shape memory alloy comprising at least two tabs 11, 12, together defining an air gap E where, in the free state of the peak 1, the minimum width of the gap E is greater than the maximum value of the reference thickness ER when the component 8 is in an open position in a martensitic structure, and in that the maximum width of the gap E is less than the minimum value of the reference thickness ER when the component 8 is in a closed position in an austenitic structure at a temperature on duty ;
  • a first phase of opening deformation of the component 8 is carried out in a martensitic structure;
  • the hairspring 3 is inserted into the housing and positioned relative to each other in an adequate position;
  • they are held in position until the return to room temperature.

Dans une variante, on effectue une première phase de déformation d'ouverture du composant 8 dans une structure martensitique, puis on effectue un refroidissement ou une chauffe du composant 8 en alliage à mémoire de forme, puis on insère le spiral 3 dans le logement, et on les positionne l'un par rapport à l'autre en position adéquate. On comprend qu'il ne faut pas refroidir plus, ni réchauffer davantage, avant d'avoir inséré le spiral.In a variant, a first phase of opening deformation of the component 8 is carried out in a martensitic structure, then cooling or heating of the shape memory alloy component 8 is carried out, then the spiral 3 is inserted into the housing, and positioned relative to each other in an adequate position. We understand that we must not cool more, nor warm more, before inserting the hairspring.

Les températures Ms et Mf doivent être assez basses pour ne pas permettre au spiral de se desserrer si la montre reste au froid. Idéalement As et Af se situent autour de 20°C à 30 °C mais peuvent aussi prendre des valeurs différentes.The temperatures M s and M f must be low enough not to allow the hairspring to loosen if the watch remains cold. Ideally A s and A f are around 20 ° C to 30 ° C but can also take different values.

L'homme du métier saura extrapoler l'invention pour d'autres configurations, notamment une application réverse de l'invention.Those skilled in the art will be able to extrapolate the invention for other configurations, in particular a reverse application of the invention.

Le piton dans son état de stockage, avant montage du spiral, peut, ou bien être à branches parallèles auquel cas une opération d'écartement est réalisée juste avant le montage, ou bien être à branches divergentes, auquel cas on ne fait qu'y présenter le spiral en position. Dans l'un ou l'autre cas, l'écartement doit être le fruit d'une déformation préalable, afin que la mémoire de forme permette de retrouver l'état pré-déformation.The piton in its storage state, before mounting the hairspring, may or may be parallel branches in which case a spacer operation is performed just before mounting, or be divergent branches, in which case it is only y present the hairspring in position. In either case, the spacing must be the result of prior deformation, so that the shape memory allows to find the pre-deformation state.

Les termes techniques contenus dans la description ci-dessus (austénite, martensite, As, Af, Ms, Mf) sont pertinents principalement pour les alliages à mémoire de forme activés thermiquement. Ces concepts s'appliquent néanmoins également aux alliages à mémoire de forme activés magnétiquement ainsi qu'aux polymères à mémoire de forme.The technical terms contained in the above description (austenite, martensite, A s , A f , M s , M f ) are relevant primarily for thermally activated shape memory alloys. These concepts nevertheless apply magnetically activated shape memory alloys as well as shape memory polymers.

Dans le cas des alliages à mémoire de forme activés magnétiquement, les notions de températures de transition doivent être remplacées par des notions de seuils de champs magnétiques. Cette solution est avantageuse, dans le cas où le positionnement est fait sous champ magnétique, pour éliminer toute possibilité de desserrage à basse température.In the case of magnetically activated shape memory alloys, the notions of transition temperatures must be replaced by notions of magnetic field thresholds. This solution is advantageous, in the case where the positioning is done under a magnetic field, to eliminate any possibility of loosening at low temperature.

Dans le cas des polymères à mémoire de forme, qui sont souvent des copolymères blocs, les phases dites « austénitiques » et « martensitiques » n'existent pas en tant que telles, et la transition se fait au niveau moléculaire à une température de transition. Cette température peut correspondre à la température de transition vitreuse d'un des blocs ou à sa température de fusion.In the case of shape memory polymers, which are often block copolymers, the so-called "austenitic" and "martensitic" phases do not exist as such, and the transition occurs at the molecular level at a transition temperature. This temperature may correspond to the glass transition temperature of one of the blocks or to its melting temperature.

De façon non limitative, des matériaux à mémoire de forme utilisables pour la mise en oeuvre de l'invention sont :

  • ou bien des alliages à mémoire de forme activés thermiquement :
    • Ag-Cd
    • Au-Cd
    • Co-Ni-Al
    • Co-Ni-Ga
    • Cu-Al-Ni
    • Cu-Al-Be
    • Cu-Zn-Al
    • Cu-Zn-Si
    • Cu-Zn-Sn
    • Cu-Zn
    • Cu-Sn
    • In-Ti
    • Mn-Cu
    • Nb-Ru
    • Ta-Ru
    • Ni-Al
    • Ni-Ti
    • Ni-Ti-Fe
    • Ni-Ti-Cu
    • Ni-Ti-Nb
    • Ni-Ti-Pd
    • Ni-Ti-Hf
    • Fe-Pt
    • Fe-Mn-Si
    • Fe-Pd
    • Fe-Ni-Co-Ti
    • Ti-Pd
    • Ti-Pt
    • Ti-Au
  • ou bien des alliages à mémoire de forme activés magnétiquement :
    • Ni-Mn-Ga
    • Fe-Ni-Ga
    • Co-Ni-Ga
    • Fe-Pd
    • Fe-Pt
  • ou bien des polymères et copolymères à mémoire de forme :
    • PET-PEO
    • Polynorbornene
    • PE-Nylon
    • PE-PVA
    • PS-Poly(1,4-Butadiène)
    • Polyuréthanes.
Without limitation, shape memory materials that can be used for the implementation of the invention are:
  • or thermally activated shape memory alloys:
    • Ag-Cd
    • In-Cd
    • Co-Ni-Al
    • Co-Ni-Ga
    • Cu-Al-Ni
    • Cu-Al-Be
    • Cu-Zn-Al
    • Cu-Zn-Si
    • Cu-Zn-Sn
    • Cu-Zn
    • Cu-Sn
    • In-Ti
    • Mn-Cu
    • Nb-Ru
    • Ta-Ru
    • Ni-Al
    • Ni-Ti
    • Ni-Ti-Fe
    • Ni-Ti-Cu
    • Ni-Ti-Nb
    • Ni-Ti-Pd
    • Ni-Ti-Hf
    • Fe-Pt
    • Fe-Mn-Si
    • Fe-Pd
    • Fe-Ni-Co-Ti
    • Ti-Pd
    • Ti-Pt
    • Ti-Au
  • or else magnetically activated shape memory alloys:
    • Ni-Mn-Ga
    • Fe-Ni-Ga
    • Co-Ni-Ga
    • Fe-Pd
    • Fe-Pt
  • or polymers and copolymers with shape memory:
    • PET-PEO
    • polynorbornene
    • PE-nylon
    • PE-PVA
    • PS-Poly (1,4-butadiene)
    • Polyurethanes.

Bien sûr, ces matériaux à mémoire de forme utilisables pour la mise en oeuvre de l'invention peuvent, encore, être des alliages à mémoire de forme activés thermiquement ou/et activés magnétiquement.Of course, these shape memory materials that can be used for the implementation of the invention may, again, be heat-activated shape memory alloys and / or magnetically activated.

Grâce à l'invention, la force de serrage du piton sur le spiral est contrôlée précisément, dans un assemblage parfaitement reproductible.Thanks to the invention, the clamping force of the stud on the spiral is precisely controlled in a perfectly reproducible assembly.

Claims (11)

  1. Assembly (10) including a balance spring (3) which comprises two opposite lateral surfaces (31, 32) separated by a reference thickness (ER), and a balance spring stud (1) including a housing dimensioned to receive said balance spring (3) with two opposite lateral surfaces (31, 32) separated by a reference thickness (ER), said stud (1) including, around said housing, at least one one-piece component (8) made of a shape memory alloy and including at least two lugs (11, 12) defining together an air gap (E) and each arranged to rest on one of said opposite lateral surfaces (31, 32) of said balance spring (3), and wherein, in the free state, the minimum width of said air-gap (E) is greater than the maximum value of said reference thickness (ER) when said component (8) is in an open position corresponding to a martensitic structure, and wherein the maximum width of said air-gap (E) is less than the minimum value of said reference thickness (ER) when said component (8) is in a closed position corresponding to an austenitic structure, characterized in that said balance spring (3) locally includes at least one area of lesser thickness (30) whose minimum thickness is said reference thickness (ER) for which said stud (1) is devised, and which is surrounded by areas of large thickness (35) whose minimum thickness is greater than said reference thickness (ER).
  2. Assembly (10) according to claim 1, characterized in that said housing of said balance spring stud (1) includes an axial abutment surface (9) arranged to receive in abutment an edge (33) of a said balance spring (3).
  3. Assembly (10) according to claim 1 or 2, characterized in that said stud (1) is made in one piece with said component (8).
  4. Assembly (10) according to any of claims 1 to 3, characterized in that said balance spring (3) includes an alternation of said areas of lesser thickness (30) and areas of large thickness (35), for adjustment of the active length of said balance spring (3) through the discrete cooperation of said stud (1) with one of said areas of lesser thickness (30).
  5. Assembly (10) according to any of claims 1 to 4, characterized in that each said area of lesser thickness (30) has a length substantially equal to the thickness (L) of said lugs (11, 12) of said stud (1).
  6. Assembly (10) according to any of claims 1 to 5, characterized in that said areas of lesser thickness (30) all have the same profile, and in that said lugs (11, 12) of said stud (1) each have a complementary profile to the profile of said balance spring (3) which faces said lugs in each said area of lesser thickness (30).
  7. Timepiece movement (100) including at least one assembly (10) according to any of claims 1 to 6.
  8. Timepiece (200) including at least one movement (100) according to claim 7 or and an assembly (10) according to any of claims 1 to 6.
  9. Method for attaching a balance spring (3) to a balance spring stud (1) characterized in that the method includes the following steps:
    - a said balance spring stud (1) is produced for receiving a balance spring (3) of reference thickness (ER), said stud including, around a housing provided for receiving said balance spring (3), at least one one-piece component (8) made of a shape memory alloy and including at least two lugs (11, 12), defining together an air-gap (E) wherein, in the free state of said stud (1), the minimum width of said air-gap (E) is greater than the maximum value of said reference thickness (ER) when said component (8) is in an open position in a martensitic structure, and in that the maximum width of said air-gap (E) is less than the minimum value of said reference thickness (ER) when said component (8) is in a closed position in an austenitic structure;
    - said balance spring (3) is produced, locally including at least one area of lesser thickness (30) whose minimum thickness is said reference thickness (ER), for which said stud (1) is devised, and which is surrounded by areas of large thickness (35) whose minimum thickness is greater than said reference thickness (ER),
    - there is effected a first phase of deformation to open said component (8) in a martensitic state and at a lower temperature than a first transformation start temperature (As), characteristic of the start of transformation of the martensitic structure into an austenitic structure on heating;
    - - a balance spring (3) is inserted into said housing in a determined position or until a stop position is reached;
    - - there is effected a second phase of deformation to close said component (8), in which said lugs (11, 12) are clamped onto said balance spring (3) by heating said component (8) to a higher temperature than a second temperature (Af) at which the transformation from the martensitic structure to the austenitic structure ends.
  10. Method for attaching a balance spring (3) to a balance spring stud (1) characterized in that the method includes the following steps:
    - a said balance spring stud (1) is produced for receiving a balance spring (3) of reference thickness (ER), said stud including, around a housing provided for receiving said balance spring (3), at least one one-piece component (8) made of a shape memory alloy, whose temperature at which the transformation from the martensitic structure to the austenitic structure ends is lower than the ambient temperature, and including at least two lugs (11, 12), defining together an air-gap (E) wherein, in the free state of said stud (1), the minimum width of said air-gap (E) is greater than the maximum value of said reference thickness (ER) when said component (8) is in an open position in a martensitic structure, and in that the maximum width of said air-gap (E) is less than the minimum value of said reference thickness (ER) when said component (8) is in a closed position in an austenitic structure at an operating temperature;
    - said balance spring (3) is produced, locally including at least one area of lesser thickness (30) whose minimum thickness is said reference thickness (ER), for which said stud (1) is devised, and which is surrounded by areas of large thickness (35) whose minimum thickness is greater than said reference thickness (ER);
    - there is effected a first phase of deformation to open said component (8) in a martensitic structure;
    - said balance spring (3) is inserted in said housing , and the spring and housing are properly positioned with respect to each other;
    - they are maintained in position until the ambient temperature is reached again.
  11. Method according to claim 10, characterized in that the method includes the following series of steps:
    - a said balance spring stud (1) is produced for receiving a balance spring (3) of reference thickness (ER), said stud including, around a housing provided for receiving said balance spring (3), at least one one-piece component (8) made of a shape memory alloy and including at least two lugs (11, 12), defining together an air-gap (E) wherein, in the free state of said stud (1), the minimum width of said air-gap (E) is greater than the maximum value of said reference thickness (ER) when said component (8) is in an open position in a martensitic structure, and in that the maximum width of said air-gap (E) is less than the minimum value of said reference thickness (ER) when said component (8) is in a closed position in an austenitic structure at an operating temperature;
    - there is effected a first phase of deformation to open said component (8) in a martensitic structure;
    - cooling or heating is performed on said shape memory alloy component (8);
    - said balance spring (3) is inserted in said housing , and the spring and housing are properly positioned with respect to each other;
    - they are maintained in position until the ambient temperature is reached again.
EP14194961.0A 2013-12-09 2014-11-26 Hairspring-stud assembly for timepiece Active EP2881804B1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
EP14194961.0A EP2881804B1 (en) 2013-12-09 2014-11-26 Hairspring-stud assembly for timepiece
US14/873,533 US9367038B1 (en) 2013-12-09 2015-10-02 Balance spring stud for a timepiece
JP2015216431A JP6018686B2 (en) 2014-11-26 2015-11-04 Balance spring stud for timer
CN201510829127.9A CN105629698B (en) 2014-11-26 2015-11-25 Hairspring stud for clock and watch

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP13196153.4A EP2881803B1 (en) 2013-12-09 2013-12-09 Timepiece cannon-pinion
EP14194961.0A EP2881804B1 (en) 2013-12-09 2014-11-26 Hairspring-stud assembly for timepiece

Publications (3)

Publication Number Publication Date
EP2881804A2 EP2881804A2 (en) 2015-06-10
EP2881804A3 EP2881804A3 (en) 2015-08-26
EP2881804B1 true EP2881804B1 (en) 2017-08-02

Family

ID=56046786

Family Applications (1)

Application Number Title Priority Date Filing Date
EP14194961.0A Active EP2881804B1 (en) 2013-12-09 2014-11-26 Hairspring-stud assembly for timepiece

Country Status (4)

Country Link
US (1) US9367038B1 (en)
EP (1) EP2881804B1 (en)
JP (1) JP6018686B2 (en)
CN (1) CN105629698B (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10338259B2 (en) 2015-12-14 2019-07-02 Covidien Lp Surgical adapter assemblies and wireless detection of surgical loading units
EP3211486B1 (en) * 2016-02-25 2018-09-26 ETA SA Manufacture Horlogère Suisse Method for attaching a hairspring for mechanical clock movement
EP3252542B1 (en) * 2016-06-01 2022-05-18 Rolex Sa Part for fastening a timepiece hairspring
EP3252541A1 (en) * 2016-06-01 2017-12-06 Rolex Sa Part for fastening a timepiece hairspring
EP3617811A1 (en) * 2018-09-03 2020-03-04 Rolex Sa Method for producing friction by indenting
EP4202569A1 (en) 2021-12-21 2023-06-28 Montres Breguet S.A. Watch case with rotating bezel

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH317531A (en) * 1954-04-21 1956-11-30 Ebauches Bettlach Sa Piton
CH395869A (en) * 1963-07-05 1966-01-14 Fontainemelon Horlogerie Device for fixing the outer end of a watch balance spring
US5617377A (en) * 1995-12-13 1997-04-01 Perret, Jr.; Gerard A. Watchband connector pin utilizing shape memory material
EP1199615A4 (en) * 1999-07-29 2004-11-10 Seiko Instr Inc Mechanical timepiece with stud adjustment mechanism
EP1302821A3 (en) * 2001-10-10 2010-05-05 Franck Muller-Watchland SA Balance-spring for time measuring apparatus
EP1515200A1 (en) * 2003-09-10 2005-03-16 Patek Philippe S.A. Hairspring for timepiece
EP1580625A1 (en) 2004-03-23 2005-09-28 Asulab S.A. Device and method for fixing a pallet on an escapement anchor in a watch movement
JP2006214822A (en) * 2005-02-02 2006-08-17 Seiko Instruments Inc Mechanical timepiece including regulatable hairspring
WO2008029158A2 (en) * 2006-09-08 2008-03-13 Gideon Levingston Thermally compensating balance wheel
CH699882A2 (en) * 2008-11-06 2010-05-14 Montres Breguet Sa Elevated curve hairspring e.g. breguet hairspring, for use in timepiece, has lifting device arranged between external layer of spring and terminal curve so as to increase concentric development of hairspring
EP2804055B1 (en) * 2013-05-16 2016-03-09 Blancpain SA. Assembly consisting of a stud and a stud support

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Also Published As

Publication number Publication date
CN105629698B (en) 2018-04-03
US20160147196A1 (en) 2016-05-26
US9367038B1 (en) 2016-06-14
CN105629698A (en) 2016-06-01
JP6018686B2 (en) 2016-11-02
EP2881804A3 (en) 2015-08-26
JP2016099345A (en) 2016-05-30
EP2881804A2 (en) 2015-06-10

Similar Documents

Publication Publication Date Title
EP2881804B1 (en) Hairspring-stud assembly for timepiece
EP2881803B1 (en) Timepiece cannon-pinion
EP1730604B1 (en) Device and method for fixing a pallet on an escapement anchor in a watch movement
EP1991916A1 (en) Micromechanical piece with form opening for assembly on a spindle
EP2423764B1 (en) Device for measuring the torque of a hairspring
EP2860592A1 (en) Assembly system using a planar resilient locking member
EP2930572A2 (en) Clock set using an amorphous metal alloy
FR2956340A1 (en) METHOD AND DEVICE FOR DISASSEMBLING A CLOSELY ADJUSTED RING IN A BOREHOLE
CH708945A2 (en) Piton watch.
EP2860591A1 (en) Assembly system using a conical resilient locking member
EP3267265A2 (en) Method for producing a clockwork assembly and clockwork assembly thus obtained
WO2014173611A1 (en) Device and method for fixing a movement in a case
EP3430480B1 (en) Method for assembling a device comprising at least two parts
EP3032353B1 (en) Detachable stud support
CH708965A2 (en) Floor clock and indenting process.
CH707186A2 (en) Bimetallic element of dressing for a timepiece and its manufacturing process.
EP2798414B1 (en) Spring for clock movement
CH716957A2 (en) Guidance device for clock display.
CH719289A2 (en) Watch box with rotating bezel.
EP3839656B1 (en) Horological balance
EP4202569A1 (en) Watch case with rotating bezel
CH712218A2 (en) A method of assembling a device comprising at least two parts.
CH716553A1 (en) Friction spring and watch mechanism limiting the torque transmitted between two rotating parts.
CH710491A2 (en) Holding assembly or support of a timepiece balance spring.
CH706756A2 (en) Anchor for escapement for timepiece, has fastening device including elastic structure resting against pallet when pallet is received in housing such that pallet is adjusted and maintained in predetermined position in housing

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20141126

AK Designated contracting states

Kind code of ref document: A2

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

AX Request for extension of the european patent

Extension state: BA ME

REG Reference to a national code

Ref country code: DE

Ref legal event code: R079

Ref document number: 602014012469

Country of ref document: DE

Free format text: PREVIOUS MAIN CLASS: G04B0013020000

Ipc: G04B0018060000

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

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

AX Request for extension of the european patent

Extension state: BA ME

RIC1 Information provided on ipc code assigned before grant

Ipc: G04B 18/06 20060101AFI20150717BHEP

R17P Request for examination filed (corrected)

Effective date: 20160226

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

INTG Intention to grant announced

Effective date: 20170426

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

Ref country code: CH

Ref legal event code: NV

Representative=s name: ICB INGENIEURS CONSEILS EN BREVETS SA, CH

Ref country code: AT

Ref legal event code: REF

Ref document number: 915127

Country of ref document: AT

Kind code of ref document: T

Effective date: 20170815

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: 602014012469

Country of ref document: DE

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 4

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20170802

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 915127

Country of ref document: AT

Kind code of ref document: T

Effective date: 20170802

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

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: 20170802

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: 20170802

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: 20170802

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: 20170802

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: 20171102

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: 20170802

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: 20170802

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

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: 20170802

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: 20171202

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: 20171103

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: 20170802

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: 20171102

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: 20170802

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: 20170802

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

Ref country code: RO

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

Effective date: 20170802

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: 20170802

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: 20170802

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602014012469

Country of ref document: DE

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

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: 20170802

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: 20170802

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: 20170802

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: 20170802

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

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

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

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

Ref country code: MC

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

Effective date: 20170802

26N No opposition filed

Effective date: 20180503

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: 20171126

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: 20170802

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20171130

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

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

Ref country code: MT

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

Effective date: 20170802

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 5

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: 20171126

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: 20171130

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

Ref country code: HU

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

Effective date: 20141126

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: 20170802

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

Ref country code: MK

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

Effective date: 20170802

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

Ref country code: TR

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

Effective date: 20170802

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

Ref country code: PT

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

Effective date: 20170802

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: 20170802

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

Effective date: 20230611

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

Ref country code: GB

Payment date: 20231019

Year of fee payment: 10

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

Ref country code: FR

Payment date: 20231019

Year of fee payment: 10

Ref country code: DE

Payment date: 20231019

Year of fee payment: 10

Ref country code: CH

Payment date: 20231202

Year of fee payment: 10