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EP2735919B1 - Watch movement comprising a fusee - Google Patents

Watch movement comprising a fusee Download PDF

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Publication number
EP2735919B1
EP2735919B1 EP12194477.1A EP12194477A EP2735919B1 EP 2735919 B1 EP2735919 B1 EP 2735919B1 EP 12194477 A EP12194477 A EP 12194477A EP 2735919 B1 EP2735919 B1 EP 2735919B1
Authority
EP
European Patent Office
Prior art keywords
fusee
barrel
rocket
wire
guide
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
EP12194477.1A
Other languages
German (de)
French (fr)
Other versions
EP2735919A1 (en
Inventor
Eric Goeller
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
Application filed by Montres Breguet SA filed Critical Montres Breguet SA
Priority to EP12194477.1A priority Critical patent/EP2735919B1/en
Priority to US14/088,564 priority patent/US8858068B2/en
Priority to CN201310604254.XA priority patent/CN103838126B/en
Priority to RU2013152461/28A priority patent/RU2013152461A/en
Priority to JP2013244736A priority patent/JP5632948B2/en
Publication of EP2735919A1 publication Critical patent/EP2735919A1/en
Priority to HK14112068A priority patent/HK1198593A1/en
Application granted granted Critical
Publication of EP2735919B1 publication Critical patent/EP2735919B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • G04B1/00Driving mechanisms
    • G04B1/10Driving mechanisms with mainspring
    • G04B1/16Barrels; Arbors; Barrel axles
    • 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
    • G04B1/00Driving mechanisms
    • G04B1/10Driving mechanisms with mainspring
    • G04B1/22Compensation of changes in the motive power of the mainspring

Definitions

  • the present invention relates to a watch movement comprising a motor barrel, a rocket, movement winding means arranged to drive the rocket, a finishing gear train arranged to be driven by the rocket, and a chain, a rope or a wire of transmission stretched between the rocket and the barrel and arranged to unwind from the rocket and to wind on the barrel so that the barrel drives the finishing gear when the rocket rotates in a first direction, and arranged to unwind the barrel and to wind on the rocket so that the winding means arms the barrel when the rocket rotates in a second direction.
  • FIG. 1 is a schematic sectional view of the entire wheel of a timepiece comprising a rocket.
  • the reference 2 generally indicates the barrel
  • 4 indicates the rocket
  • 6 is the chain stretched between the barrel and the rocket
  • 8 is the ferris wheel that a ratchet system (not shown) rotates in solidarity with the barrel.
  • rocket in one direction 10 is the axis of the rocket
  • 12 is a square formed on the axis of the rocket to allow reassembly.
  • a rocket consists essentially of a conical shaped pulley whose throat winds in a spiral and which is connected to the engine cylinder by a chain.
  • the chain is wound from the barrel on the rocket so that the smallest radius receives the greatest force.
  • the chain winds progressively on the barrel by pulling on the rocket with a continuously increasing lever arm so as to compensate for the reduction of the spring force.
  • the large wheel 8 is arranged to drive the center pinion 14 and then, in a conventional manner, the center wheel 16 meshes with the average pinion 18, that the average wheel 20 meshes with the second pinion 22, and finally, that the second wheel 24 meshes with the exhaust pinion 26.
  • the axis of the center wheel carries the roadway 28 and the gun of the hours 30.
  • the roadway and the gun of the hours are connected to each other by the timer 32.
  • the illustrated cylinder has no teeth. It will be understood that, the barrel being devoid of toothing, reassembly must be performed via the rocket.
  • the known timepieces with rocket are usually equipped with a winding ratchet (not shown) which is integral with the axis of the rocket 4 via
  • the pumping means are arranged to drive the rocket in rotation in the direction opposite to the direction of travel.
  • a ratchet system ensures disengagement of the large wheel 8 when the rocket rotates in the opposite direction of the direction of travel.
  • the gear train is not driven in reverse during reassembly.
  • the chain communicates the rotation of the rocket drum barrel, which has the effect of arming the spring.
  • the use of a rocket is a very effective solution to compensate for the variation of the spring force.
  • the document CH 10599 describes a watch movement in which a rocket is provided between said movement and the barrel to compensate for the variation of the spring force.
  • the gear ratio of the finishing gear is selected to maintain the operation of the movement by winding the spring only once a year.
  • This mechanism representing a certain size, is used in floor clocks or wall clocks.
  • the rocket because of its conical shape, the rocket has a large footprint in the sense of height. It is therefore difficult to reconcile the use of a rocket with the requirements related to the design of a flat caliber. Efforts have been made to remedy this problem by producing lower rockets with a more compact shape.
  • An object of the present invention is therefore to overcome the disadvantages of the prior art which have just been described, and in particular to overcome the constraint of a minimum threshold for the slope of the cone of the rocket.
  • the present invention achieves this goal by providing a watch movement comprising a motor barrel and a rocket and according to the appended claim 1.
  • a roller is slidably mounted on a fixed guide oriented in the direction of the axis of the rocket parallel to the main surface thereof. Due to the presence of the roller, the wire changes direction when approaching the rocket. So, instead of Wrap and unroll perpendicular to the axis of rotation of the rocket, the wire wraps and unrolls the rocket perpendicular to the orientation of the fixed guide.
  • the rocket does not have the shape of a cone, but that of a plate, the main surface of the rocket being flat.
  • An advantage of this variant is to limit the height of the rocket as much as possible.
  • the roller comprises a pulley whose rim has a groove arranged to receive the wire, while the two side edges of the rim are arranged to roll on the bottom of the groove by enclosing the groove. thread.
  • FIGS. 3 , 4 and 5 are three views, respectively in perspective and in plan from above and from the side, of a first embodiment of the invention. It is recognized in the figures a barrel 102, which is housed a barrel spring (not shown), and a rocket 104 which is connected to the barrel by a wire 106.
  • the barrel is formed of a barrel drum 142 which serves as a housing for the spring, a barrel cover 144 which closes the box formed by the drum, and a barrel shaft (not shown ) which passes through the barrel and which is fixed at its ends to the plate and a bridge.
  • the barrel shaft acts as a pivot for the barrel.
  • the spring is hooked by one end to the shaft, and the other to the drum. When armed, the spring is wound against the circumference of the shaft. By seeking to return to its original form, the spring is unwound by rotating the barrel.
  • the cylinder 102 is kinematically connected to the rest of the movement by the wire 106. It therefore does not need toothing. This is called a smooth cylinder.
  • the wire 106 is stretched between the barrel 102 and the rocket 104 so as to transmit the rotational movement of the barrel to the rocket and vice versa.
  • the rocket 104 is generally in the form of a plate with a planar upper surface in which is formed a spiral groove 148 concentric with the axis of the rocket. At the periphery of the rocket, the groove opens on a notch 150 inside which is formed a through hole (not shown). One end of the wire 106 is inserted and fixed in the through hole. The wire is wound in the groove from the notch 150 so that the distance between the wire and the axis of the rocket 104 decreases as one moves away from the end of the wire. When the spring relaxes by rotating the barrel 102, the wire wraps around the barrel by driving the rocket.
  • a large wheel 180 whose teeth meshes with the center pinion of the watch (referenced 200) is arranged coaxially with the rocket 104.
  • the big wheel and the rocket are mounted idle on both ends of the same referenced shaft 182.
  • a planetary gear is interposed between the ferris wheel and the rocket.
  • the planet gear comprises a pinion 184 integral with the shaft 182, a ring gear 186 which is driven concentrically on the base of the rocket, and a satellite wheel consisting of a wheel 188 and a pinion 190 pivoted in an eccentric position on the board of the ferris wheel 180.
  • a winding ratchet 192 is also driven on the lower end of the shaft 182.
  • a pawl (not shown) is still provided to prevent the ratchet to turn in a first direction of rotation.
  • the operation of the planet gear is as follows. During disarming, the spring relaxes and rotates the barrel 102. The wire 106 is progressively transferred from the rocket to the barrel by driving the rocket 104 in the first direction of rotation.
  • the sawtooth profile of the winding ratchet has the effect of retaining the shaft 182 which can not rotate with the rocket.
  • the rocket drives the pinion 190 of the mobile satellite via the ring 186.
  • the wheel 188 of the satellite mobile meshes with the pinion 184 in solidarity with the shaft 182. Under these conditions, when the rocket rotates in the first direction, the satellite mobile is driven by the ring 186.
  • the pinion 184 is prevented from rotating by the ratchet, the satellite revolves around the shaft 182 in the opposite direction of the rocket, and drives the big wheel 180 with him.
  • the big wheel drives in turn the center pinion and through it all the finishing gear.
  • the watch movement which is the subject of the present description usually comprises means for winding the movement (not shown). These winding means are arranged to drive the winding ratchet 192 in the second direction of rotation. When the winding ratchet is actuated, it rotates the pinion 184 which it is secured. The pinion 184 engages with the wheel 188 of the satellite mobile and drives the latter in the first direction of rotation. The pinion 190 of the mobile satellite meshes with the ring gear 186 of the rocket. Note that the large wheel 180 can rotate in the second direction of rotation only. Indeed, in known manner, the finishing gear is associated with a second ratchet mechanism (not shown) which prevents any rotation of the train in the opposite direction to the direction of movement.
  • this blocking of the large wheel 180 prevents the satellite mobile from rotating around the shaft 182 in the first direction of rotation. It is therefore the rocket that is driven in the second direction of rotation by the satellite mobile via the ring 186. It will be understood that, when the rocket thus rotates in the second direction of rotation, the wire 106 is progressively transferred from the barrel 102 to the rocket 104 by driving the barrel in the direction of rotation corresponding to the winding of the spring.
  • a general characteristic of rockets is that the wire is wound on a surface of revolution that is not parallel to the axis of rotation of the rocket. This is why a spiral groove is almost always needed to guide the wire.
  • the surface on which the wire is wound is even perpendicular to the axis of rotation of the rocket. Under these conditions, even the presence of a groove is not sufficient to guide the wire so that it winds regularly on the rocket.
  • the watch movement comprises, in addition to the rocket, a fixed guide (referenced 155) and a roller (referenced 157) provided for guided the wire 106 and which is mounted sliding on the fixed guide.
  • the guide for the roller retractor is oriented parallel to the main surface of the rocket and in the direction of the axis of the rocket.
  • the guide according to the invention is oriented to allow the roller roller to slide parallel to a generator of the cone.
  • the guide 155 is oriented horizontally, parallel to a radius of the disk.
  • the pulley is rotatably mounted on the shaft 157 and, as already mentioned, it is also arranged to slide transversely along the shaft.
  • the diameter of the pulley is such that its rim penetrates into the spiral groove 148.
  • the wire 106 When the wire 106 is wound on the barrel 102, it is released from the rocket 104. Conversely, when the wire is unwound from the barrel, it winds in the spiral groove 148.
  • the introduction of the wire into the groove, as its extraction from it, is provided by the pulley 157.
  • the pulley has a groove around its periphery. This throat is arranged to receive and guide the thread.
  • the peripheral portion of the pulley is shaped to penetrate the spiral groove, so that through the pulley, the wire is passed under it, so as to be sandwiched between the bottom of the groove and the throat of the pulley.
  • one of the aims of the present invention is to reduce the size associated with a rocket. It will therefore be understood that it is advantageous to use a wire whose thickness is as small as possible. Indeed, if the wire is thinner, the spiral groove can also be narrower. At present, there is on the market a choice of extremely fine son. The diameter of these new generation wires is between a few tens and a few hundred microns. Even finer threads, made for example with nanotubes already exist in the laboratory. According to the embodiment of the invention which is the subject of this example, the wire wound on the barrel and the rocket to be a wire of a thickness of about 100 microns marketed by Berkley® under the name Nanofil®.
  • roller 157 very small roller.
  • This roller can be made for example in sapphire in the manner of a stone with hole.
  • the roller may take the form of a thin disk with a groove around its periphery and a hole arranged in its center for the guide 155.
  • FIGS. 6 and 7 illustrate an engine cylinder and a rocket implemented in a second embodiment of the invention.
  • the reel roller also fulfills the function of power reserve indicator. Notwithstanding this difference, the second embodiment is very similar to the previous one. This is the reason why the elements of the figures which are identical in the two embodiments are designated by the same reference numerals in the figures.
  • the axis 102 of the rocket is pivoted in bearing 265 carried by a bridge 263.
  • This bridge also carries the guide for the roller roller.
  • This guide is constituted by a shaft 255 suspended by its two ends at the bridge 263.
  • the bridge 263 still has a rectangular opening through which it is possible to see the guide 255 and the roller roller 257.
  • the roller retractor is associated with a jumper 259 provided with an index 261.
  • the jumper 259 which is integral in translation of the retractor roller, is visible through the rectangular opening in the bridge.
  • the index 261 always indicates the position of the roller, and the bridge 263 still carries a graduated scale arranged opposite the rectangular opening. The end of the index is arranged to cooperate with the scale to indicate the power reserve.
  • roller pulley is not necessarily constituted by a pulley rotatably mounted on an axis.
  • the wire could very well be arranged to slide in the throat of the roller without the latter is to turn on itself.

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Transmission Devices (AREA)
  • Electromechanical Clocks (AREA)

Description

DOMAINE DE L'INVENTIONFIELD OF THE INVENTION

La présente invention concerne un mouvement de montre comprenant un barillet moteur, une fusée, des moyens de remontage du mouvement agencés pour entraîner la fusée, un rouage de finissage agencé pour être entraîné par la fusée, et une chaîne, une corde ou un fil de transmission tendu entre la fusée et le barillet et agencé pour se dérouler de la fusée et pour s'enrouler sur le barillet de sorte que le barillet entraîne le rouage de finissage lorsque la fusée tourne dans un premier sens, et agencé pour se dérouler du barillet et pour s'enrouler sur la fusée de sorte que les moyens de remontage arme le barillet lorsque la fusée tourne dans un second sens.The present invention relates to a watch movement comprising a motor barrel, a rocket, movement winding means arranged to drive the rocket, a finishing gear train arranged to be driven by the rocket, and a chain, a rope or a wire of transmission stretched between the rocket and the barrel and arranged to unwind from the rocket and to wind on the barrel so that the barrel drives the finishing gear when the rocket rotates in a first direction, and arranged to unwind the barrel and to wind on the rocket so that the winding means arms the barrel when the rocket rotates in a second direction.

ART ANTERIEURPRIOR ART

Au XVe siècle sont apparues des horloges de relativement petites dimensions qui étaient actionnées par un ressort au lieu du poids habituel. Ces premières horloges à ressort étaient nettement moins précises que les horloges entraînées par un poids suspendu à un fil. En effet, comme on le sait bien, la force exercée par un ressort n'est pas constante mais diminue à mesure que le ressort se détend. Or, les échappements à verge et foliot utilisés à l'époque étaient extrêmement sensibles aux variations du couple moteur. Les horloges à ressort avaient donc tendance à ralentir progressivement à mesure que la réserve de marche s'épuisait.In the 15th century appeared clocks of relatively small dimensions that were actuated by a spring instead of the usual weight. These first spring clocks were significantly less accurate than the clocks driven by a weight suspended on a wire. Indeed, as is well known, the force exerted by a spring is not constant but decreases as the spring relaxes. However, the yard and foliage exhausts used at the time were extremely sensitive to variations in engine torque. The spring clocks therefore tended to slow down gradually as the power reserve ran out.

Une solution très ancienne pour égaliser la force fournie par un ressort de barillet au rouage de finissage est d'utiliser une fusée. Les figures 1 et 2 annexées illustrent deux modes de réalisation traditionnels d'un barillet couplé à une fusée. La figure 1 est une vue schématique en coupe de l'ensemble du rouage d'une pièce d'horlogerie comportant une fusée. Dans cette figure, la référence 2 indique généralement le barillet, 4 indique la fusée, 6 est la chaîne tendue entre le barillet et la fusée, 8 est la grande roue qu'un système à cliquet (non représenté) rend solidaire en rotation de la fusée dans un seul sens, 10 est l'axe de la fusée, et enfin, 12 est un carré formé sur l'axe de la fusée pour permettre le remontage. En se référant maintenant à la vue plus détaillée de la figure 2, on peut voir qu'une fusée consiste essentiellement en une poulie de forme conique dont la gorge s'enroule en spirale et qui est reliée au barillet moteur par une chaîne. La chaîne est enroulée depuis le barillet sur la fusée de sorte que le plus petit rayon reçoit la plus grande force. Lors du désarmage du ressort moteur, la chaîne s'enroule progressivement sur le barillet en tirant sur la fusée avec un bras de levier continuellement croissant de manière à compenser la réduction de la force du ressort.A very old solution to equalize the force provided by a barrel spring to the gear train is to use a rocket. The figures 1 and 2 annexed illustrate two traditional embodiments of a barrel coupled to a rocket. The figure 1 is a schematic sectional view of the entire wheel of a timepiece comprising a rocket. In this figure, the reference 2 generally indicates the barrel, 4 indicates the rocket, 6 is the chain stretched between the barrel and the rocket, 8 is the ferris wheel that a ratchet system (not shown) rotates in solidarity with the barrel. rocket in one direction, 10 is the axis of the rocket, and finally, 12 is a square formed on the axis of the rocket to allow reassembly. Referring now to the more detailed view of the figure 2 it can be seen that a rocket consists essentially of a conical shaped pulley whose throat winds in a spiral and which is connected to the engine cylinder by a chain. The chain is wound from the barrel on the rocket so that the smallest radius receives the greatest force. During the disarming of the mainspring, the chain winds progressively on the barrel by pulling on the rocket with a continuously increasing lever arm so as to compensate for the reduction of the spring force.

En se référant à nouveau à la figure 1, on peut voir que la grande roue 8 est agencée pour entraîner le pignon de centre 14 et qu'ensuite, de manière classique, la roue de centre 16 engrène avec le pignon moyenne 18, que la roue moyenne 20 engrène avec le pignon de seconde 22, et enfin, que la roue de seconde 24 engrène avec le pignon d'échappement 26. On peut voir encore que l'axe de la roue de centre porte la chaussée 28 et le canon des heures 30. La chaussée et le canon des heures sont reliés l'un à l'autre par la minuterie 32. On peut encore remarquer, aussi bien sur la figure 1 que la figure 2, que le barillet illustré ne présente pas de denture. On comprendra que, le barillet étant dépourvu de denture, le remontage doit s'effectuer par l'intermédiaire de la fusée. A cet effet, les pièces d'horlogerie à fusée connues sont habituellement équipées d'un rochet de remontage (non représenté) qui est solidaire de l'axe de la fusée 4 par l'intermédiaire du carré 12. Les moyens de remontages sont agencés pour entraîner la fusée en rotation dans le sens contraire du sens de marche. Comme on l'a déjà dit, un système à cliquet assure le débrayage de la grande roue 8 lorsque la fusée tourne dans le sens contraire du sens de marche. Ainsi, le rouage de finissage n'est pas entraîné en marche arrière lors du remontage. En revanche, la chaîne communique la rotation de la fusée au tambour du barillet, ce qui a pour effet d'armer le ressort.Referring again to the figure 1 it can be seen that the large wheel 8 is arranged to drive the center pinion 14 and then, in a conventional manner, the center wheel 16 meshes with the average pinion 18, that the average wheel 20 meshes with the second pinion 22, and finally, that the second wheel 24 meshes with the exhaust pinion 26. It can still be seen that the axis of the center wheel carries the roadway 28 and the gun of the hours 30. The roadway and the gun of the hours are connected to each other by the timer 32. We can also notice, as well on the figure 1 that the figure 2 , that the illustrated cylinder has no teeth. It will be understood that, the barrel being devoid of toothing, reassembly must be performed via the rocket. For this purpose, the known timepieces with rocket are usually equipped with a winding ratchet (not shown) which is integral with the axis of the rocket 4 via The pumping means are arranged to drive the rocket in rotation in the direction opposite to the direction of travel. As already mentioned, a ratchet system ensures disengagement of the large wheel 8 when the rocket rotates in the opposite direction of the direction of travel. Thus, the gear train is not driven in reverse during reassembly. On the other hand, the chain communicates the rotation of the rocket drum barrel, which has the effect of arming the spring.

Le recours à une fusée est une solution très efficace pour compenser la variation de la force de ressort. Notamment, le document CH 10599 décrit un mouvement horloger dans lequel une fusée est prévue entre ledit mouvement et le barillet afin de compenser la variation de la force du ressort. Le rapport d'engrenage du rouage de finissage est choisi de manière à maintenir le fonctionnement du mouvement au moyen du remontage du ressort une seule fois par an. Ce mécanisme, représentant un certain encombrement, est utilisé dans des horloges de parquet ou des horloges murales. Toutefois, en raison de sa forme conique, la fusée présente un encombrement important dans le sens de la hauteur. Il est donc difficile de concilier l'utilisation d'une fusée avec les impératifs liés à la conception d'un calibre plat. Des efforts ont été entrepris pour remédier à ce problème en réalisant des fusées moins hautes avec une forme plus ramassée. Toutefois, comme le montre notamment la figure 2, la direction à partir de laquelle la chaîne s'enroule sur la fusée doit être perpendiculaire à l'axe de rotation de la fusée. Dans ces conditions, on comprendra que la pente du cône de la fusée ne peut pas être réduite au-dessous d'un certain seuil.The use of a rocket is a very effective solution to compensate for the variation of the spring force. In particular, the document CH 10599 describes a watch movement in which a rocket is provided between said movement and the barrel to compensate for the variation of the spring force. The gear ratio of the finishing gear is selected to maintain the operation of the movement by winding the spring only once a year. This mechanism, representing a certain size, is used in floor clocks or wall clocks. However, because of its conical shape, the rocket has a large footprint in the sense of height. It is therefore difficult to reconcile the use of a rocket with the requirements related to the design of a flat caliber. Efforts have been made to remedy this problem by producing lower rockets with a more compact shape. However, as shown in particular figure 2 , the direction from which the chain winds on the rocket must be perpendicular to the axis of rotation of the rocket. Under these conditions, it will be understood that the slope of the cone of the rocket can not be reduced below a certain threshold.

BREF EXPOSE DE L'INVENTIONBRIEF SUMMARY OF THE INVENTION

Un but de la présente invention est donc de remédier aux inconvénients de l'art antérieur qui viennent d'être décrits, et notamment de s'affranchir de la contrainte d'un seuil minimal pour la pente du cône de la fusée. La présente invention atteint ce but en fournissant un mouvement de montre comprenant un barillet moteur et une fusée et conforme à la revendication 1 annexée.An object of the present invention is therefore to overcome the disadvantages of the prior art which have just been described, and in particular to overcome the constraint of a minimum threshold for the slope of the cone of the rocket. The present invention achieves this goal by providing a watch movement comprising a motor barrel and a rocket and according to the appended claim 1.

Conformément à l'invention, un galet enrouleur est monté coulissant sur un guide fixe orienté en direction de l'axe la fusée parallèlement à la surface principale de celle-ci. En raison de la présence du galet enrouleur, le fil change de direction en approchant de la fusée. Ainsi, au lieu de s'enrouler et de se dérouler perpendiculairement à l'axe de rotation de la fusée, le fil s'enroule et se déroule de la fusée perpendiculairement à l'orientation du guide fixe.According to the invention, a roller is slidably mounted on a fixed guide oriented in the direction of the axis of the rocket parallel to the main surface thereof. Due to the presence of the roller, the wire changes direction when approaching the rocket. So, instead of Wrap and unroll perpendicular to the axis of rotation of the rocket, the wire wraps and unrolls the rocket perpendicular to the orientation of the fixed guide.

Selon une variante avantageuse de l'invention, la fusée n'a pas la forme d'un cône, mais celle d'un plateau, la surface principale de la fusée étant donc plate. Un avantage de cette variante est de limiter au maximum la hauteur de la fusée.According to an advantageous variant of the invention, the rocket does not have the shape of a cone, but that of a plate, the main surface of the rocket being flat. An advantage of this variant is to limit the height of the rocket as much as possible.

Selon une autre variante avantageuse de l'invention, le galet enrouleur comprend une poulie dont la jante présente une gorge agencée pour recevoir le fil, alors que les deux bords latéraux de la jante sont agencés pour rouler sur le fond de la rainure en enserrant le fil.According to another advantageous variant of the invention, the roller comprises a pulley whose rim has a groove arranged to receive the wire, while the two side edges of the rim are arranged to roll on the bottom of the groove by enclosing the groove. thread.

BREVE DESCRIPTION DES FIGURESBRIEF DESCRIPTION OF THE FIGURES

D'autres caractéristiques et avantages de la présente invention apparaîtront à la lecture de la description qui va suivre, donnée uniquement à titre d'exemple non limitatif, et faite en référence aux dessins annexés dans lesquels :

  • la figure 1 est une vue schématique en coupe du rouage d'une pièce d'horlogerie de l'art antérieur comportant une fusée ;
  • la figure 2 est une vue en perspective montrant la chaîne tendue entre le barillet lisse et la fusée d'une pièce d'horlogerie de l'art antérieur ;
  • la figure 3 est une vue partielle en perspective montrant le barillet moteur et la fusée d'un mouvement de montre conforme à un premier mode de réalisation de l'invention;
  • la figure 4 est une vue en plan de dessus montrant le barillet moteur et la fusée de la figure 3 ;
  • la figure 5 est une vue en élévation du barillet moteur et de la fusée des figures 3 et 4 ;
  • la figure 6 est une vue partielle en plan de dessus montrant le barillet moteur et la fusée d'un mouvement de montre conforme à un deuxième mode de réalisation de l'invention ;
  • la figure 7 est une vue en coupe selon A-A de la figure 6.
Other features and advantages of the present invention will appear on reading the following description, given solely by way of non-limiting example, and with reference to the appended drawings in which:
  • the figure 1 is a schematic sectional view of the wheel of a timepiece of the prior art comprising a rocket;
  • the figure 2 is a perspective view showing the chain stretched between the smooth cylinder and the rocket of a timepiece of the prior art;
  • the figure 3 is a partial perspective view showing the engine cylinder and the rocket of a watch movement according to a first embodiment of the invention;
  • the figure 4 is a top plan view showing the engine cylinder and the rocket of the figure 3 ;
  • the figure 5 is an elevational view of the engine cylinder and rocket figures 3 and 4 ;
  • the figure 6 is a partial plan view showing the engine cylinder and the rocket of a watch movement according to a second embodiment of the invention;
  • the figure 7 is a sectional view according to AA of the figure 6 .

DESCRIPTION DETAILLEE DE MODES DE REALISATIONDETAILED DESCRIPTION OF EMBODIMENTS

Les figures 3, 4 et 5 sont trois vues, respectivement en perspective et en plan de dessus et de côté, d'un premier mode de réalisation de l'invention. On reconnait sur les figures un barillet 102, dans lequel est logé un ressort de barillet (non représenté), et une fusée 104 qui est reliée au barillet par un fil 106.The figures 3 , 4 and 5 are three views, respectively in perspective and in plan from above and from the side, of a first embodiment of the invention. It is recognized in the figures a barrel 102, which is housed a barrel spring (not shown), and a rocket 104 which is connected to the barrel by a wire 106.

De manière connue en soi, le barillet est formé d'un tambour de barillet 142 qui sert de logement au ressort, d'un couvercle de barillet 144 qui ferme la boîte formée par le tambour, et d'un arbre de barillet (non représenté) qui traverse le barillet et qui est fixé par ses extrémités à la platine et à un pont. L'arbre de barillet joue le rôle de pivot pour le barillet. Le ressort est accroché par une de ses extrémités à l'arbre, et par l'autre, au tambour. Lorsqu'il est armé, le ressort est enroulé contre la circonférence de l'arbre. En cherchant à reprendre sa forme initiale, le ressort se déroule en faisant tourner le barillet. Le barillet 102 est relié cinématiquement au reste du mouvement par le fil 106. Il n'a donc pas besoin de denture. Il s'agit de ce qu'on appelle un barillet lisse.In a manner known per se, the barrel is formed of a barrel drum 142 which serves as a housing for the spring, a barrel cover 144 which closes the box formed by the drum, and a barrel shaft (not shown ) which passes through the barrel and which is fixed at its ends to the plate and a bridge. The barrel shaft acts as a pivot for the barrel. The spring is hooked by one end to the shaft, and the other to the drum. When armed, the spring is wound against the circumference of the shaft. By seeking to return to its original form, the spring is unwound by rotating the barrel. The cylinder 102 is kinematically connected to the rest of the movement by the wire 106. It therefore does not need toothing. This is called a smooth cylinder.

Le fil 106 est tendu entre le barillet 102 et la fusée 104 de manière à transmettre le mouvement de rotation du barillet à la fusée et vice versa. La fusée 104 présente généralement la forme d'un plateau avec une surface principale supérieure plane dans laquelle est formée une rainure en spirale 148 concentrique à l'axe de la fusée. A la périphérie de la fusée, la rainure débouche sur une encoche 150 à l'intérieur de laquelle est formé un trou traversant (non représenté). Une extrémité du fil 106 est insérée et fixée dans le trou traversant. Le fil est enroulé dans la rainure à partir de l'encoche 150 de sorte que la distance entre le fil et l'axe de la fusée 104 diminue à mesure qu'on s'éloigne de l'extrémité du fil. Lorsque le ressort se détend en faisant tourner le barillet 102, le fil s'enroule autour du barillet en entraînant la fusée. Comme le fil est enroulé en spirale sur la fusée, on comprendra que le barillet tire la fusée avec un bras de levier qui augmente à mesure que le fil se dévide. Ainsi, lorsque la force du ressort est la plus petite, la distance séparant l'axe de la fusée et le point d'application de la force est la plus grande. La réduction de la force du ressort peut donc être compensée.The wire 106 is stretched between the barrel 102 and the rocket 104 so as to transmit the rotational movement of the barrel to the rocket and vice versa. The rocket 104 is generally in the form of a plate with a planar upper surface in which is formed a spiral groove 148 concentric with the axis of the rocket. At the periphery of the rocket, the groove opens on a notch 150 inside which is formed a through hole (not shown). One end of the wire 106 is inserted and fixed in the through hole. The wire is wound in the groove from the notch 150 so that the distance between the wire and the axis of the rocket 104 decreases as one moves away from the end of the wire. When the spring relaxes by rotating the barrel 102, the wire wraps around the barrel by driving the rocket. As the wire is spirally wound on the rocket, it will be understood that the barrel pulls the rocket with a lever arm that increases as the wire unwinds. Thus, when the spring force is the smallest, the distance between the axis of the rocket and the point of application of the force is the largest. The reduction of the spring force can therefore be compensated.

Comme on peut le voir sur la figure 5 et plus en détail sur la coupe de la figure 7, une grande roue 180, dont la denture engrène avec le pignon de centre de la montre (référencé 200), est arrangée coaxialement avec la fusée 104. La grande roue et la fusée sont montées folles sur les deux extrémités d'un même arbre référencé 182. On peut voir également qu'un engrenage planétaire est intercalé entre la grande roue et la fusée. L'engrenage planétaire comporte un pignon 184 solidaire de l'arbre 182, une couronne à denture extérieure 186, qui est chassée concentriquement sur la base de la fusée, et un mobile satellite constitué d'une roue 188 et d'un pignon 190 pivotés en position excentrée sur la planche de la grande roue 180. Un rochet de remontoir 192 est également chassé sur l'extrémité inférieure de l'arbre 182. De façon connue en soi, un cliquet (non représenté) est encore prévu pour empêcher le rochet de tourner dans un premier sens de rotation.As can be seen on the figure 5 and more in detail about the cut of the figure 7 a large wheel 180 whose teeth meshes with the center pinion of the watch (referenced 200) is arranged coaxially with the rocket 104. The big wheel and the rocket are mounted idle on both ends of the same referenced shaft 182. It can also be seen that a planetary gear is interposed between the ferris wheel and the rocket. The planet gear comprises a pinion 184 integral with the shaft 182, a ring gear 186 which is driven concentrically on the base of the rocket, and a satellite wheel consisting of a wheel 188 and a pinion 190 pivoted in an eccentric position on the board of the ferris wheel 180. A winding ratchet 192 is also driven on the lower end of the shaft 182. In a manner known per se, a pawl (not shown) is still provided to prevent the ratchet to turn in a first direction of rotation.

Le fonctionnement de l'engrenage planétaire est le suivant. Durant le désarmage, le ressort se détend et fait tourner le barillet 102. Le fil 106 est progressivement transféré de la fusée au barillet en entraînant la fusée 104 dans le premier sens de rotation. Le profil en dent de scie du rochet de remontage a pour effet de retenir l'arbre 182 qui ne peut pas tourner avec la fusée. La fusée entraîne le pignon 190 du mobile satellite par l'intermédiaire de la couronne 186. La roue 188 du mobile satellite engrène avec le pignon 184 solidaire de l'arbre 182. Dans ces conditions, lorsque la fusée tourne dans le premier sens, le mobile satellite est entraîné par la couronne 186. Comme le pignon 184 est empêché de tourner par le rochet, le satellite tourne autour de l'arbre 182 dans le sens contraire de la fusée, et entraîne la grande roue 180 avec lui. La grande roue entraîne à son tour le pignon de centre et par son intermédiaire tout le rouage de finissage.The operation of the planet gear is as follows. During disarming, the spring relaxes and rotates the barrel 102. The wire 106 is progressively transferred from the rocket to the barrel by driving the rocket 104 in the first direction of rotation. The sawtooth profile of the winding ratchet has the effect of retaining the shaft 182 which can not rotate with the rocket. The rocket drives the pinion 190 of the mobile satellite via the ring 186. The wheel 188 of the satellite mobile meshes with the pinion 184 in solidarity with the shaft 182. Under these conditions, when the rocket rotates in the first direction, the satellite mobile is driven by the ring 186. As the pinion 184 is prevented from rotating by the ratchet, the satellite revolves around the shaft 182 in the opposite direction of the rocket, and drives the big wheel 180 with him. The big wheel drives in turn the center pinion and through it all the finishing gear.

Le mouvement de montre qui fait l'objet de la présente description comporte de façon habituelle des moyens de remontage du mouvement (non représentés). Ces moyens de remontage sont agencés pour entraîner le rochet de remontage 192 dans le second sens de rotation. Lorsque le rochet de remontage est actionné, il fait tourner le pignon 184 duquel il est solidaire. Le pignon 184 engraine avec la roue 188 du mobile satellite et entraîne ce dernier dans le premier sens de rotation. Le pignon 190 du mobile satellite engrène lui-même avec la couronne dentée 186 de la fusée. A noter que la grande roue 180 peut tourner dans le second sens de rotation uniquement. En effet, de façon connue, le rouage de finissage est associé à un second mécanisme à cliquet (non représenté) qui empêche toute rotation du rouage dans le sens contraire au sens de la marche du mouvement. Dans ces conditions, on comprendra que ce blocage de la grande roue 180 empêche le mobile satellite de tourner autour de l'arbre 182 dans le premier sens de rotation. C'est donc la fusée qui est entraînée dans le deuxième sens de rotation par le mobile satellite via la couronne 186. On comprendra que, lorsque la fusée tourne ainsi dans le second sens de rotation, le fil 106 est progressivement transféré du barillet 102 à la fusée 104 en entraînant le barillet dans le sens de rotation correspondant à l'armage du ressort.The watch movement which is the subject of the present description usually comprises means for winding the movement (not shown). These winding means are arranged to drive the winding ratchet 192 in the second direction of rotation. When the winding ratchet is actuated, it rotates the pinion 184 which it is secured. The pinion 184 engages with the wheel 188 of the satellite mobile and drives the latter in the first direction of rotation. The pinion 190 of the mobile satellite meshes with the ring gear 186 of the rocket. Note that the large wheel 180 can rotate in the second direction of rotation only. Indeed, in known manner, the finishing gear is associated with a second ratchet mechanism (not shown) which prevents any rotation of the train in the opposite direction to the direction of movement. Under these conditions, it will be understood that this blocking of the large wheel 180 prevents the satellite mobile from rotating around the shaft 182 in the first direction of rotation. It is therefore the rocket that is driven in the second direction of rotation by the satellite mobile via the ring 186. It will be understood that, when the rocket thus rotates in the second direction of rotation, the wire 106 is progressively transferred from the barrel 102 to the rocket 104 by driving the barrel in the direction of rotation corresponding to the winding of the spring.

Une caractéristique générale des fusées est que le fil est enroulé sur une surface de révolution qui n'est pas parallèle à l'axe de rotation de la fusée. C'est la raison pour laquelle une rainure en spirale est presque toujours nécessaire pour guider le fil. Dans le cas d'une fusée plate comme décrite dans le présent exemple, la surface sur laquelle le fil s'enroule est même perpendiculaire à l'axe de rotation de la fusée. Dans ces conditions, même la présence d'une rainure ne suffit pas pour guider le fil de manière à ce qu'il s'enroule régulièrement sur la fusée. C'est la raison pour laquelle, selon l'invention, le mouvement de montre comprend, en plus de la fusée, un guide fixe (référencé 155) et un galet enrouleur (référencé 157) prévu pour guidé le fil 106 et qui est monté coulissant sur le guide fixe.A general characteristic of rockets is that the wire is wound on a surface of revolution that is not parallel to the axis of rotation of the rocket. This is why a spiral groove is almost always needed to guide the wire. In the case of a flat rocket like described in this example, the surface on which the wire is wound is even perpendicular to the axis of rotation of the rocket. Under these conditions, even the presence of a groove is not sufficient to guide the wire so that it winds regularly on the rocket. This is the reason why, according to the invention, the watch movement comprises, in addition to the rocket, a fixed guide (referenced 155) and a roller (referenced 157) provided for guided the wire 106 and which is mounted sliding on the fixed guide.

Conformément à l'invention, le guide pour le galet enrouleur est orienté parallèlement à la surface principale de la fusée et en direction de l'axe la fusée. En d'autres termes, dans le cas où la forme de la fusée est sensiblement celle d'un cône de révolution comme dans l'art antérieur, le guide selon l'invention est orienté de façon à permettre au galet enrouleur de coulisser parallèlement à une génératrice du cône. En revanche, si comme dans l'exemple illustré, la forme de la fusée 104 et sensiblement celle d'un disque, alors le guide 155 est orienté horizontalement, parallèlement à un rayon du disque. En se référant plus particulièrement à la figure 4, on peut voir que, dans le mode de réalisation illustré, le galet enrouleur 157 présente la forme d'une poulie de faible épaisseur, et que le guide 155 est constitué par un arbre cylindrique. La poulie est montée rotative sur l'arbre 157 et, comme on l'a déjà dit, elle est également agencée pour coulisser transversalement le long de l'arbre. Le diamètre de la poulie est tel que sa jante pénètre dans la rainure en spirale 148. Lorsque la fusée 104 tourne, la poulie 157 est guidée par les bords de la rainure, de sorte qu'elle parcourt la rainure en se décalant latéralement le long de l'arbre 155.According to the invention, the guide for the roller retractor is oriented parallel to the main surface of the rocket and in the direction of the axis of the rocket. In other words, in the case where the shape of the rocket is substantially that of a cone of revolution as in the prior art, the guide according to the invention is oriented to allow the roller roller to slide parallel to a generator of the cone. On the other hand, if, as in the illustrated example, the shape of the rocket 104 and substantially that of a disk, then the guide 155 is oriented horizontally, parallel to a radius of the disk. With particular reference to the figure 4 it can be seen that, in the illustrated embodiment, the roller 157 has the shape of a thin pulley, and the guide 155 is constituted by a cylindrical shaft. The pulley is rotatably mounted on the shaft 157 and, as already mentioned, it is also arranged to slide transversely along the shaft. The diameter of the pulley is such that its rim penetrates into the spiral groove 148. When the rocket 104 rotates, the pulley 157 is guided by the edges of the groove, so that it traverses the groove by shifting laterally along the groove. of the tree 155.

Lorsque le fil 106 s'enroule sur le barillet 102, il se dévide de la fusée 104. Inversement, lorsque le fil se déroule du barillet, il s'enroule dans la gorge en spirale 148. L'introduction du fil dans la rainure, comme son extraction à partir de celle-ci, est assurée par la poulie 157. A cet effet, la poulie présente un gorge autour de sa périphérie. Cette gorge est agencée pour recevoir et guider le fil. La partie périphérique de la poulie est conformée pour pénétrer dans la rainure en spirale, de sorte qu'en passant par la poulie, le fil soit amené à passer sous celle-ci, de manière à être pris en sandwich entre le fond de la rainure et le la gorge de la poulie.When the wire 106 is wound on the barrel 102, it is released from the rocket 104. Conversely, when the wire is unwound from the barrel, it winds in the spiral groove 148. The introduction of the wire into the groove, as its extraction from it, is provided by the pulley 157. For this purpose, the pulley has a groove around its periphery. This throat is arranged to receive and guide the thread. The peripheral portion of the pulley is shaped to penetrate the spiral groove, so that through the pulley, the wire is passed under it, so as to be sandwiched between the bottom of the groove and the throat of the pulley.

Comme on l'a dit plus haut, un des but de la présente invention est de réduire l'encombrement associé à une fusée. On comprendra donc qu'il est avantageux d'utiliser un fil dont l'épaisseur est la plus faible possible. En effet, si le fil est plus fin, la rainure en spirale peut également être plus étroite. A l'heure actuelle, on trouve sur le marché un choix de fils extrêmement fins. Le diamètre de ces fils de nouvelle génération se situe entre quelques dizaines et quelques centaines de microns. Des fils encore plus fin, réalisés par exemple avec des nanotubes existent déjà en laboratoire. Conformément au mode de réalisation de l'invention qui fait l'objet du présent exemple, le fil enroulé sur le barillet et la fusée pour être un fil d'une épaisseur d'environ 100 microns commercialisé par la société Berkley® sous l'appellation NanoFil®. On comprendra qu'avec un fil aussi fin, il est possible notamment d'utiliser un galet enrouleur 157 très petit. Ce galet peut être réalisé par exemple en saphir à la manière d'une pierre à trou. Dans ce cas, le galet pourra prendre la forme d'un disque mince avec une gorge autour de sa périphérie et un trou aménagé en son centre pour le guide 155.As mentioned above, one of the aims of the present invention is to reduce the size associated with a rocket. It will therefore be understood that it is advantageous to use a wire whose thickness is as small as possible. Indeed, if the wire is thinner, the spiral groove can also be narrower. At present, there is on the market a choice of extremely fine son. The diameter of these new generation wires is between a few tens and a few hundred microns. Even finer threads, made for example with nanotubes already exist in the laboratory. According to the embodiment of the invention which is the subject of this example, the wire wound on the barrel and the rocket to be a wire of a thickness of about 100 microns marketed by Berkley® under the name Nanofil®. It will be understood that with such a fine wire, it is possible in particular to use a roller 157 very small roller. This roller can be made for example in sapphire in the manner of a stone with hole. In this case, the roller may take the form of a thin disk with a groove around its periphery and a hole arranged in its center for the guide 155.

Les figures 6 et 7 illustrent un barillet moteur et une fusée mis en oeuvre dans un deuxième mode de réalisation de l'invention. Comme on le verra plus en détail ci-après, dans ce deuxième mode de réalisation, le galet enrouleur remplit également la fonction d'indicateur de réserve de marche. Nonobstant cette différence, le deuxième mode de réalisation est très semblable au précédent. C'est la raison pour laquelle les éléments des figures qui se retrouve à l'identique dans les deux modes de réalisations sont désignés par les mêmes numéros de référence sur les figures.The Figures 6 and 7 illustrate an engine cylinder and a rocket implemented in a second embodiment of the invention. As will be seen in more detail below, in this second embodiment, the reel roller also fulfills the function of power reserve indicator. Notwithstanding this difference, the second embodiment is very similar to the previous one. This is the reason why the elements of the figures which are identical in the two embodiments are designated by the same reference numerals in the figures.

En se référant plus particulièrement à la figure 6, on peut voir que l'axe 102 de la fusée est pivotée dans palier 265 porté par un pont 263. Ce pont porte également le guide pour le galet enrouleur. Ce guide est constitué par un arbre 255 suspendu par ses deux extrémités au pont 263. Le pont 263 présente encore une ouverture rectangulaire à travers laquelle il est possible de voir le guide 255 et le galet enrouleur 257. Dans l'exemple illustré, le galet enrouleur est associé à un cavalier 259 muni d'un index 261. Le cavalier 259, qui est solidaire en translation du galet enrouleur, est visible à travers l'ouverture rectangulaire aménagée dans le pont. L'index 261 indique toujours la position du galet, et le pont 263 porte encore une échelle graduée disposée en regard de l'ouverture rectangulaire. L'extrémité de l'index est agencée pour coopérer avec l'échelle graduée pour indiquer la réserve de marche.With particular reference to the figure 6 it can be seen that the axis 102 of the rocket is pivoted in bearing 265 carried by a bridge 263. This bridge also carries the guide for the roller roller. This guide is constituted by a shaft 255 suspended by its two ends at the bridge 263. The bridge 263 still has a rectangular opening through which it is possible to see the guide 255 and the roller roller 257. In the example shown, the roller retractor is associated with a jumper 259 provided with an index 261. The jumper 259, which is integral in translation of the retractor roller, is visible through the rectangular opening in the bridge. The index 261 always indicates the position of the roller, and the bridge 263 still carries a graduated scale arranged opposite the rectangular opening. The end of the index is arranged to cooperate with the scale to indicate the power reserve.

On comprendra en outre que diverses modifications et/ou améliorations évidentes pour un homme du métier peuvent être apportées aux modes de réalisation qui font l'objet de la présente description sans sortir du cadre de la présente invention définie par les revendications annexées. En particulier, le galet enrouleur n'est pas nécessairement constitué par une poulie montée rotative sur un axe. En effet, le fil pourrait très bien être agencé pour glisser dans la gorge du galet sans que ce dernier n'est à tourner sur lui-même.It will be further understood that various modifications and / or improvements obvious to those skilled in the art can be made to the embodiments which are the subject of the present description without departing from the scope of the present invention defined by the appended claims. In particular, the roller pulley is not necessarily constituted by a pulley rotatably mounted on an axis. Indeed, the wire could very well be arranged to slide in the throat of the roller without the latter is to turn on itself.

Claims (4)

  1. Watch movement comprising a barrel (102) having a barrel drum (142), a barrel arbor and a spring accommodated in the barrel drum, said spring being held between said arbor and said drum, wherein the movement additionally comprises a fusee (104) arranged to rotate in a first direction and in a second direction and having a main surface, which has a spiral groove (148) concentric to the axis of the fusee, a winding mechanism (192) arranged to rotate the fusee, a going train (200) arranged to be driven by the fusee and a transmission wire (106) extended between the fusee and the barrel, one of the ends of the wire being wound into the spiral groove, and the wire being arranged to unwind from the spiral groove of the fusee and to wind up onto the barrel so that the barrel drives the going train when the fusee rotates in the first direction and being arranged to unwind from the barrel and to wind onto the fusee guided by the spiral groove so that the winding mechanism winds the spring when the fusee rotates in the second direction, characterized in that the watch movement comprises a fixed guide (155; 255) and a winding roller (157; 257) mounted to slide on the fixed guide and arranged to guide the wire (106) between the barrel and the fusee, wherein the fixed guide is oriented in the direction of the axis of the fusee parallel to the main surface of the fusee, and the winding roller is arranged to slide on the guide transversely to the wire while being engaged in the spiral groove in order to pass through the groove, extracting the wire therefrom when the fusee rotates in the first direction and inserting the wire therein when the fusee rotates in the second direction.
  2. Watch movement according to claim 1, characterized in that the winding roller (157; 257) comprises a pulley having an edge arranged to penetrate into the spiral groove (147) and having a peripheral groove arranged to guide the wire (106).
  3. Watch movement according to claim 1 or 2, characterized in that the main surface of the fusee (104) is plane.
  4. Watch movement according to one of claims 1, 2 or 3, characterized in that the winding roller (257) is fixed against translation movement to an index (261) arranged to cooperate with a fixed scale oriented parallel to the fixed guide (255) in order to indicate the power reserve.
EP12194477.1A 2012-11-27 2012-11-27 Watch movement comprising a fusee Active EP2735919B1 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
EP12194477.1A EP2735919B1 (en) 2012-11-27 2012-11-27 Watch movement comprising a fusee
US14/088,564 US8858068B2 (en) 2012-11-27 2013-11-25 Watch movement comprising a fusee
CN201310604254.XA CN103838126B (en) 2012-11-27 2013-11-26 Table movement including stackfreed
RU2013152461/28A RU2013152461A (en) 2012-11-27 2013-11-26 FUZE WATCHING HOURS
JP2013244736A JP5632948B2 (en) 2012-11-27 2013-11-27 Wristwatch movement with fusies
HK14112068A HK1198593A1 (en) 2012-11-27 2014-12-01 Watch movement comprising a fusee

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP12194477.1A EP2735919B1 (en) 2012-11-27 2012-11-27 Watch movement comprising a fusee

Publications (2)

Publication Number Publication Date
EP2735919A1 EP2735919A1 (en) 2014-05-28
EP2735919B1 true EP2735919B1 (en) 2015-07-22

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EP12194477.1A Active EP2735919B1 (en) 2012-11-27 2012-11-27 Watch movement comprising a fusee

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US (1) US8858068B2 (en)
EP (1) EP2735919B1 (en)
JP (1) JP5632948B2 (en)
CN (1) CN103838126B (en)
HK (1) HK1198593A1 (en)
RU (1) RU2013152461A (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3217227B1 (en) * 2016-03-11 2019-02-27 The Swatch Group Research and Development Ltd. Timepiece regulator mechanism with optimised magnetic escapement
EP3312681B1 (en) * 2016-10-19 2020-01-29 Montres Breguet S.A. Clock movement comprising a device for equalising an engine torque
EP3502794B1 (en) * 2017-12-22 2020-10-21 Montres Breguet S.A. Repetition with chain wound onto a cam
EP3722888B1 (en) 2019-04-09 2023-05-17 Ecole Polytechnique Fédérale de Lausanne (EPFL) Mechanical oscillator with tunable isochronism defect
CN113053653A (en) * 2021-02-06 2021-06-29 杭州正昇安全科技有限公司 Magnetic ring inductance common mode winding machine

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20888A (en) * 1858-07-13 Escapement op watches
CH10599A (en) * 1895-06-06 1896-01-15 Carl Becker Clock with annual movement
US1468267A (en) * 1921-07-02 1923-09-18 Johnston Cyril Frederick Striking and chiming clock
US2496690A (en) * 1945-11-09 1950-02-07 Hamilton Watch Co Seconds setting mechanism
JPS63309778A (en) * 1987-06-11 1988-12-16 Kazuo Adachi Constant torque device for spiral spring
US7677540B1 (en) * 2003-04-04 2010-03-16 Duval Eugene F Dual pulley constant force mechanism
EP1970778B1 (en) * 2007-03-13 2009-09-16 Montres Breguet S.A. Timepiece comprising a device indicating the power reserve

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JP2014106235A (en) 2014-06-09
RU2013152461A (en) 2015-06-10
HK1198593A1 (en) 2015-04-30
US20140146646A1 (en) 2014-05-29
US8858068B2 (en) 2014-10-14
CN103838126B (en) 2016-09-21
EP2735919A1 (en) 2014-05-28
JP5632948B2 (en) 2014-11-26
CN103838126A (en) 2014-06-04

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