EP2154583B1 - Hairspring for sprung balance - Google Patents

Hairspring for sprung balance Download PDF

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Publication number
EP2154583B1
EP2154583B1 EP09405126.5A EP09405126A EP2154583B1 EP 2154583 B1 EP2154583 B1 EP 2154583B1 EP 09405126 A EP09405126 A EP 09405126A EP 2154583 B1 EP2154583 B1 EP 2154583B1
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Prior art keywords
hairspring
blades
balance
plan
variable
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German (de)
French (fr)
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EP2154583A1 (en
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Jérôme Daout
Richard Bossart
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Rolex SA
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Rolex SA
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Priority to EP12180170.8A priority patent/EP2523053B1/en
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    • GPHYSICS
    • G04HOROLOGY
    • G04BMECHANICALLY-DRIVEN CLOCKS OR WATCHES; MECHANICAL PARTS OF CLOCKS OR WATCHES IN GENERAL; TIME PIECES USING THE POSITION OF THE SUN, MOON OR STARS
    • G04B17/00Mechanisms for stabilising frequency
    • G04B17/04Oscillators acting by spring tension
    • G04B17/06Oscillators with hairsprings, e.g. balance
    • G04B17/066Manufacture of the spiral spring
    • GPHYSICS
    • G04HOROLOGY
    • G04BMECHANICALLY-DRIVEN CLOCKS OR WATCHES; MECHANICAL PARTS OF CLOCKS OR WATCHES IN GENERAL; TIME PIECES USING THE POSITION OF THE SUN, MOON OR STARS
    • G04B17/00Mechanisms for stabilising frequency
    • G04B17/20Compensation of mechanisms for stabilising frequency

Definitions

  • the present invention relates to a hairspring for a sprung balance resonator comprising n blades, n ⁇ 2 (1a, 1b, 1c), integral at least by their respective homologous ends and wound in spirals with an angular offset capable of neutralizing the forces lateral generated when the homologous ends of said blades located at a first end of the hairspring are angularly displaced with respect to the homologous ends of said blades located at the second end of the hairspring.
  • a hairspring of the aforementioned type has already been described in EP 2,063,325 , published after the priority date of the present invention.
  • the aim of the present invention is to benefit from the advantages of this solution by overcoming, at least in part, the aforementioned drawbacks.
  • the subject of this invention is a hairspring for a sprung balance resonator according to claim 1.
  • FIG. 1 The first embodiment of the hairspring which is the subject of the invention is illustrated by figure 1 .
  • This flat hairspring comprises two blades 1a, 1b wound in the same direction, but with an offset of 2 ⁇ / 2, ie 180 °.
  • the respective internal ends of these blades 1a, 1b are integral with a ferrule 2 and their external ends are integral with a fixing ring 3. These external ends are also angularly offset by 180 °.
  • the fixing ring 3 of the outer ends of the blades 1a, 1b of the hairspring has an opening 3a to allow its attachment to the balance bridge. This fixing ring 3 therefore replaces the traditional eyebolt.
  • the two blades 1a, 1b of the hairspring must not touch each other during their contraction and expansion. This risk increases with the amplitude. This risk can therefore be reduced by limiting the amplitude.
  • the diameter of the balance spring can also be increased.
  • the height of the blade of the hairspring could also be varied.
  • thermo-compensation of the balance-spring is obtained by the formation, on the surface of the blades of the balance-spring, of a layer of amorphous silicon oxide, whose thermal coefficient of Young's modulus is of the opposite sign to that of monocrystalline silicon, as described in EP 1 422 436 .
  • This layer of amorphous silicon oxide allows compensation of the thermal coefficient of the Young's modulus whatever the crystallographic orientation of Si, (100), (111) or (110).
  • the number of blades forming the hairspring is not limited to two.
  • various other solutions such as that illustrated by figure 5 which is a variant of that of the figure 1 , but which comprises three blades 1a, 1b and 1c attached on the one hand to the ferrule 2 and on the other hand to the fixing ring 3.
  • the internal and external ends of these blades are angularly offset, with respect to each other. others, at an angle 2 ⁇ / 3.
  • This angular offset will advantageously be 2 ⁇ / n, n corresponding to the number of blades.
  • the blades forming the hairspring are attached to each other by their two respective ends.
  • the embodiment illustrated by figure 6 represents a hairspring with two blades 1a, 1b attached by their only internal ends to the ferrule 2. Their external ends are free, which allows to exert, on the two plates, a pre-tension in one direction or the other, in order to adjust the isochronism in particular.
  • a hairspring comprising four blades, two blades 1a, 1b arranged between the ferrule 2 and an intermediate ring 4 to which their outer ends are fixed and two blades 1c, 1d arranged between the intermediate ring and the fixing ring 3.
  • the intermediate ring 4 As light as possible, its structure can be hollowed out to reduce its mass as much as possible.
  • the inner blades 1a, 1b and the outer blades 1c, 1d can all be wound in the same direction as illustrated by figure 7 , or the internal blades 1a, 1b can be wound in the opposite direction of the external blades 1c, 1d, as illustrated by figure 8 .
  • thermo-compensation of the hairspring is then obtained by the formation of a layer of amorphous silicon oxide on the surface of the blades of the hairspring, by heat treatment for example.
  • Other suitable materials, adapted to the manufacturing methods allowing the production of a hairspring in a plane are likely to be used.
  • UV-lithographic processes such as UV-LIGA (Lithographie, Galvanmaschine und Abformung) could also make it possible to produce the type of hairspring which is the subject of the present invention in a metal alloy.
  • the two blades 1a, 1b are produced on an SOI (Silicon-On-Insulator, figures 10a, 10b ), which consists of a stack of layers of Si-SiO 2 -Si.
  • SOI Silicon-On-Insulator, figures 10a, 10b
  • a blade 1a is etched from the outer face of one of the layers of Si and the other blade 1b is etched from the outer face of the second layer of Si.
  • the inner ends of the two blades are made integral by the intermediate layer 8 of SiO 2 .
  • the advantage of this embodiment is to reduce the diameter of the hairspring, because the distance between two neighboring turns is increased. This advantage is even more pronounced if we extend the hairspring vertically as in the figure 10 .
  • the figure 11 illustrates another variant of figures 10a , 10b , in which the internal ends of the blades 1a, 1b are integral with the same ferrule, while their external ends are integral with the intermediate layer 5 of SiO 2 .

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Springs (AREA)
  • Micromachines (AREA)

Description

La présente invention se rapporte à un spiral pour résonateur balancier-spiral comportant n lames, n≥ 2 (1a, 1b, 1c), solidaires au moins par une leurs extrémités homologues respectives et enroulées en spirales avec un décalage angulaire apte à neutraliser les forces latérales engendrées lorsque les extrémités homologues desdites lames situées à une première extrémité du spiral sont déplacées angulairement par rapport aux extrémités homologues desdites lames situées à la seconde extrémité du spiral.The present invention relates to a hairspring for a sprung balance resonator comprising n blades, n ≥ 2 (1a, 1b, 1c), integral at least by their respective homologous ends and wound in spirals with an angular offset capable of neutralizing the forces lateral generated when the homologous ends of said blades located at a first end of the hairspring are angularly displaced with respect to the homologous ends of said blades located at the second end of the hairspring.

Un spiral du type susmentionné a déjà été décrit dans le EP 2 063 325 , publié après la date de priorité de la présente invention.A hairspring of the aforementioned type has already been described in EP 2,063,325 , published after the priority date of the present invention.

On sait que le centre de gravité d'un spiral plat se déplace pendant le mouvement oscillant du balancier. Ceci est dû au fait que l'une des extrémités du spiral est fixe, tandis que l'autre se déplace en restant toujours à la même distance de l'axe de balancier. Ce déplacement du centre de gravité à une influence sur l'isochronisme, du fait qu'il engendre des forces latérales sur les pivots de l'axe de balancier.We know that the center of gravity of a flat hairspring moves during the oscillating movement of the balance. This is due to the fact that one end of the hairspring is fixed, while the other moves while always remaining at the same distance from the balance axis. This displacement of the center of gravity has an influence on isochronism, because it generates lateral forces on the pivots of the balance axis.

Abraham-Louis Breguet eu l'idée de munir le spiral plat d'une ou deux courbes terminales permettant de remédier à ce défaut. Cette courbe a été ensuite théorisée par Ed. Phillips.Abraham-Louis Breguet had the idea of fitting the flat hairspring with one or two end curves to remedy this defect. This curve was then theorized by Ed. Phillips.

Avant la solution imaginée par Breguet et Phillips, T. Mudge avait proposé d'utiliser deux spiraux solidaires d'un même balancier et décalés de 180°. Les spiraux travaillant en synchronisme, mais en opposition de phase, les variations de leurs centres de gravité respectifs se compensent, mais leur décalage axial crée cependant un léger couple dans un plan contenant l'axe de balancier. Cette solution a été reprise dans des réalisations récentes.Before the solution devised by Breguet and Phillips, T. Mudge had proposed using two springs attached to the same balance and offset by 180 °. The hairsprings working in synchronism, but in phase opposition, the variations of their respective centers of gravity compensate each other, but their axial offset nevertheless creates a slight torque in a plane containing the balance axis. This solution has been taken up in recent achievements.

Le problème de cette solution réside dans le fait qu'il faut deux spiraux superposés, augmentant la hauteur, deux pitons et deux porte-pitons décalés de 180° autour de l'axe de balancier, deux raquettes et que chaque spiral doit être réglé en parfait synchronisme avec l'autre, conduisant à une solution extrêmement complexe et difficile à mettre au point. En plus, elle double le nombre de pièces.The problem with this solution lies in the fact that you need two superimposed hairsprings, increasing the height, two eyebolts and two eyebolts offset by 180 ° around the balance axis, two rackets and that each hairspring must be adjusted in perfect synchronism with the other, leading to an extremely complex and difficult solution to develop. In addition, it doubles the number of pieces.

Cette solution a été reprise dans plusieurs publications, notamment dans le US 3'553'956, dans le FR 2'447'571, ainsi que dans le CN 1'677'283.This solution has been used in several publications, in particular in US 3'553'956, in FR 2'447'571, as well as in CN 1'677'283.

Le but de la présente invention est de bénéficier des avantages de cette solution en remédiant, au moins en partie, aux inconvénients sus-mentionnés.The aim of the present invention is to benefit from the advantages of this solution by overcoming, at least in part, the aforementioned drawbacks.

A cet effet, cette invention a pour objet un spiral pour résonateur balancier-spiral selon la revendication 1.To this end, the subject of this invention is a hairspring for a sprung balance resonator according to claim 1.

Les dessins annexés illustrent, schématiquement et à titre d'exemple, plusieurs formes d'exécution du spiral objet de la présente invention.

  • La figure 1 est une vue en plan d'une première forme d'exécution;
  • la figure 2 est une vue en plan d'une forme d'exécution ne relevant pas de l'invention;
  • la figure 3 est un diagramme de variation du pas du spiral en fonction des tours depuis le centre vers l'extérieur pour la forme d'exécution de la figure 2;
  • la figure 4 est un diagramme de variation de l'épaisseur le long de la lame en fonction des tours depuis le centre vers l'extérieur pour la forme d'exécution de la figure 2;
  • la figure 5 est une vue en plan d'une deuxième forme d'exécution;
  • la figure 6 est une vue en plan d'une troisième forme d'exécution;
  • la figure 7 est une vue en plan d'une quatrième forme d'exécution;
  • la figure 8 est une vue en plan d'une cinquième forme d'exécution;
  • la figure 9 est une vue en élévation d'une forme d'exécution ne relevant pas de l'invention;
  • les figures 10a, 10b sont des vues en élévation de deux variantes d'une forme d'exécution ne relevant pas de l'invention;
  • la figure 11 est une vue en élévation d'une forme d'exécution ne relevant pas de l'invention.
The accompanying drawings illustrate, schematically and by way of example, several embodiments of the hairspring which is the subject of the present invention.
  • The figure 1 is a plan view of a first embodiment;
  • the figure 2 is a plan view of an embodiment not falling within the scope of the invention;
  • the figure 3 is a diagram of the variation of the pitch of the hairspring as a function of the turns from the center to the outside for the embodiment of the figure 2 ;
  • the figure 4 is a diagram of the variation of the thickness along the blade as a function of the turns from the center to the outside for the embodiment of the figure 2 ;
  • the figure 5 is a plan view of a second embodiment;
  • the figure 6 is a plan view of a third embodiment;
  • the figure 7 is a plan view of a fourth embodiment;
  • the figure 8 is a plan view of a fifth embodiment;
  • the figure 9 is an elevational view of an embodiment not falling within the scope of the invention;
  • the figures 10a , 10b are views in elevation of two variants of an embodiment not coming under the invention;
  • the figure 11 is an elevational view of an embodiment not falling within the scope of the invention.

La première forme d'exécution du spiral objet de l'invention est illustrée par la figure 1. Ce spiral plan comporte deux lames 1a, 1b enroulées dans le même sens, mais avec un décalage de 2π /2 soit 180°. Les extrémités internes respectives de ces lames 1a, 1b sont solidaires d'une virole 2 et leurs extrémités externes sont solidaires d'un anneau de fixation 3. Ces extrémités externes sont aussi décalées angulairement de 180°. L'anneau de fixation 3 des extrémités externes des lames 1a, 1b du spiral comporte une ouverture 3a pour permettre sa fixation au pont de balancier. Cet anneau de fixation 3 remplace donc le piton traditionnel.The first embodiment of the hairspring which is the subject of the invention is illustrated by figure 1 . This flat hairspring comprises two blades 1a, 1b wound in the same direction, but with an offset of 2π / 2, ie 180 °. The respective internal ends of these blades 1a, 1b are integral with a ferrule 2 and their external ends are integral with a fixing ring 3. These external ends are also angularly offset by 180 °. The fixing ring 3 of the outer ends of the blades 1a, 1b of the hairspring has an opening 3a to allow its attachment to the balance bridge. This fixing ring 3 therefore replaces the traditional eyebolt.

Les deux lames 1a, 1b du spiral ne doivent pas se toucher pendant leur contraction et leur expansion. Ce risque augmente avec l'amplitude. On peut donc réduire ce risque en limitant l'amplitude. Avantageusement cependant, on peut aussi augmenter le diamètre du spiral.The two blades 1a, 1b of the hairspring must not touch each other during their contraction and expansion. This risk increases with the amplitude. This risk can therefore be reduced by limiting the amplitude. Advantageously, however, the diameter of the balance spring can also be increased.

Une autre solution encore est celle qui consiste à faire varier le pas des spires et l'épaisseur des lames. C'est ce que montre la forme d'exécution de la figure 2, ainsi que les diagrammes des figures 3 et 4 qui illustrent respectivement la variation du pas des spires en micromètres et de l'épaisseur des lames en micromètres en fonction du nombre de tours des spires Nt des lames 1a, 1b enroulées de la figure 2, en partant du centre vers l'extérieur du spiral, pour éviter que les spires des lames 1a, 1b ne se touchent lors de l'alternance d'expansion et de contraction du spiral. La figure 3 permet de tracer l'une des deux lames 1a, 1b par la formule r(θ)=p(θ)*(θ/(2π))+r0, où r représente la distance de l'axe à la fibre neutre de la lame, r(θ=0)=r0=600 micromètres dans le cas des figures 2 à 4, et θ=Nt*2π.Yet another solution is that which consists in varying the pitch of the turns and the thickness of the blades. This is shown by the embodiment of the figure 2 , as well as the diagrams of figures 3 and 4 which respectively illustrate the variation of the pitch of the turns in micrometers and of the thickness of the blades in micrometers as a function of the number of turns of the turns Nt of the blades 1a, 1b wound on the figure 2 , starting from the center towards the outside of the hairspring, to prevent the turns of the blades 1a, 1b from touching each other during the alternation of expansion and contraction of the hairspring. The figure 3 allows you to plot one of the two blades 1a, 1b by the formula r (θ) = p (θ) * (θ / (2π)) + r0, where r represents the distance from the axis to the neutral fiber of the blade, r (θ = 0) = r0 = 600 micrometers in the case of figures 2 to 4 , and θ = Nt * 2π.

En variante on pourrait aussi faire varier la hauteur de la lame du spiral.As a variant, the height of the blade of the hairspring could also be varied.

Dans le cas de spiraux en silicium mono-cristallin, matériau susceptible d'être utilisé pour la réalisation du spiral objet de l'invention, la thermo-compensation du spiral est obtenue par la formation, à la surface des lames du spiral, d'une couche d'oxyde de silicium amorphe, dont le coefficient thermique du module d'Young est de signe opposé à celui du silicium mono-cristallin, comme décrit dans le EP 1 422 436 . Cette couche d'oxyde de silicium amorphe permet une compensation du coefficient thermique du module d'Young quelle que soit l'orientation cristallographique du Si, (100), (111) ou (110).In the case of balance-springs made of mono-crystalline silicon, a material capable of being used for making the balance-spring which is the subject of the invention, the thermo-compensation of the balance-spring is obtained by the formation, on the surface of the blades of the balance-spring, of a layer of amorphous silicon oxide, whose thermal coefficient of Young's modulus is of the opposite sign to that of monocrystalline silicon, as described in EP 1 422 436 . This layer of amorphous silicon oxide allows compensation of the thermal coefficient of the Young's modulus whatever the crystallographic orientation of Si, (100), (111) or (110).

Le nombre de lames formant le spiral n'est pas limité à deux. On peut imaginer en variante diverses autres solutions, telle que celle illustrée par la figure 5 qui est une variante de celle de la figure 1, mais qui comporte trois lames 1a, 1b et 1c rattachées d'une part à la virole 2 et d'autre part à l'anneau de fixation 3. Les extrémités internes et externes de ces lames sont décalées angulairement, les unes par rapport aux autres, d'un angle 2π /3. Ce décalage angulaire sera avantageusement de 2π/n, n correspondant au nombre de lames.The number of blades forming the hairspring is not limited to two. One can imagine as a variant various other solutions, such as that illustrated by figure 5 which is a variant of that of the figure 1 , but which comprises three blades 1a, 1b and 1c attached on the one hand to the ferrule 2 and on the other hand to the fixing ring 3. The internal and external ends of these blades are angularly offset, with respect to each other. others, at an angle 2π / 3. This angular offset will advantageously be 2π / n, n corresponding to the number of blades.

Des simulations effectuées sur la base des spiraux des figures 1 et 2 ont montré qu'il devrait être possible d'améliorer de façon très sensible l'isochronisme d'un résonateur balancier-spiral équipé d'un spiral objet de la présente invention.Simulations carried out on the basis of the balance springs figures 1 and 2 have shown that it should be possible to very significantly improve the isochronism of a sprung balance resonator equipped with a spring which is the subject of the present invention.

Dans les formes d'exécutions décrites jusqu'ici, les lames formant le spiral sont rattachées les unes aux autres par leurs deux extrémités respectives. La forme d'exécution illustrée par la figure 6 représente un spiral à deux lames 1a, 1b rattachées par leurs seules extrémités internes à la virole 2. Leurs extrémités externes sont libres, ce qui permet d'exercer, sur les deux lames, une pré-tension dans un sens ou dans l'autre, afin d'ajuster l'isochronisme notamment .In the embodiments described so far, the blades forming the hairspring are attached to each other by their two respective ends. The embodiment illustrated by figure 6 represents a hairspring with two blades 1a, 1b attached by their only internal ends to the ferrule 2. Their external ends are free, which allows to exert, on the two plates, a pre-tension in one direction or the other, in order to adjust the isochronism in particular.

D'autres variantes utilisant le même concept, à savoir un spiral à plusieurs lames coplanaires décalées angulairement et rattachées par au moins une de leurs extrémités homologues respectives sont envisageables.Other variants using the same concept, namely a hairspring with several coplanar blades angularly offset and attached by at least one of their respective homologous ends are possible.

C'est ainsi que l'on peut avoir un spiral comportant quatre lames, deux lames 1a, 1b disposées entre la virole 2 et un anneau intermédiaire 4 auquel leurs extrémités externes sont fixées et deux lames 1c, 1d disposées entre l'anneau intermédiaire et l'anneau de fixation 3. Pour rendre l'anneau intermédiaire 4 le plus léger possible, sa structure peut être évidée pour en réduire le plus possible sa masse.Thus it is possible to have a hairspring comprising four blades, two blades 1a, 1b arranged between the ferrule 2 and an intermediate ring 4 to which their outer ends are fixed and two blades 1c, 1d arranged between the intermediate ring and the fixing ring 3. To make the intermediate ring 4 as light as possible, its structure can be hollowed out to reduce its mass as much as possible.

Les lames internes 1a, 1b et les lames externes 1c, 1d peuvent être toutes enroulées dans le même sens comme illustré par la figure 7, ou les lames internes 1a, 1b peuvent être enroulées en sens contraire des lames externes 1c, 1d, comme illustré par la figure 8.The inner blades 1a, 1b and the outer blades 1c, 1d can all be wound in the same direction as illustrated by figure 7 , or the internal blades 1a, 1b can be wound in the opposite direction of the external blades 1c, 1d, as illustrated by figure 8 .

Il est évident que d'innombrables autres combinaisons peuvent être envisagées.It is obvious that countless other combinations can be considered.

Il est aussi évident que la conception nouvelle du spiral objet de l'invention ne se prête pas à la fabrication selon les procédés traditionnels des spiraux de type Nivarox/Parachrom.It is also obvious that the new design of the balance spring which is the subject of the invention does not lend itself to the manufacture according to the traditional methods of the Nivarox / Parachrom type balance springs.

Dans le cas présent, un procédé tout à fait adapté à la fabrication du spiral objet de l'invention est notamment celui décrit dans le EP 1 422 436 déjà mentionné, qui consiste à découper le spiral, par exemple par gravure plasma, dans une plaquette {001} de silicium monocristallin. La thermo-compensation du spiral est alors obtenue par la formation d'une couche d'oxyde de silicium amorphe à la surface des lames du spiral, par un traitement thermique par exemple.In the present case, a method entirely suitable for the manufacture of the hairspring which is the subject of the invention is in particular that described in EP 1 422 436 already mentioned, which consists in cutting the hairspring, for example by plasma etching, in a {001} monocrystalline silicon wafer. The thermo-compensation of the hairspring is then obtained by the formation of a layer of amorphous silicon oxide on the surface of the blades of the hairspring, by heat treatment for example.

On pourrait aussi utiliser un monocristal de quartz usiné de la même manière ou par usinage chimique. D'autres matériaux appropriés, adaptés aux modes de fabrication permettant la réalisation d'un spiral dans un plan sont susceptibles d'être utilisés.One could also use a quartz single crystal machined in the same way or by chemical machining. Other suitable materials, adapted to the manufacturing methods allowing the production of a hairspring in a plane are likely to be used.

L'utilisation de procédés photo-lithographiques tel que le UV-LIGA (Lithographie, Galvanisierung und Abformung) pourrait aussi permettre de réaliser le type de spiral objet de la présente invention en alliage métallique.The use of photo-lithographic processes such as UV-LIGA (Lithographie, Galvanisierung und Abformung) could also make it possible to produce the type of hairspring which is the subject of the present invention in a metal alloy.

Le procédé de fabrication ne fait pas partie de la présente invention. Les exemples de procédés, non limitatifs, énumérés ci-dessus à titre d'exemple, sont seulement destinés à montrer que les moyens techniques pour réaliser le nouveau type de spiral objet de l'invention existent déjà et que l'homme de l'art possède un éventail de possibilités pour réaliser ce spiral.The manufacturing process does not form part of the present invention. The examples of non-limiting methods, listed above by way of example, are only intended to show that the technical means for producing the new type of hairspring which is the subject of the invention already exist and that those skilled in the art has a range of possibilities for making this hairspring.

Lorsque l'on parle de spiral plat, il s'agit du spiral tel qu'il est obtenu. Cependant rien n'empêche, notamment dans la forme d'exécution de la figure 9, de situer les points d'encastrement 5 et 6 des extrémités externes des lames 1a, 1b hors du plan du spiral. C'est ainsi que l'on peut situer ces deux points d'encastrement respectivement de part et d'autre du plan du spiral, en sorte que les deux lames 1a, 1b formeront deux cônes symétriques de part et d'autre du plan du spiral. Cette solution présente l'avantage d'empêcher que les spires des deux lames ne se touchent. Cette solution permet de réaliser des spiraux de petit diamètre avec un grand nombre de tours. Elle constitue donc un autre moyen pour éviter le contact entre les lames du spiral lors de l'alternance d'expansions et de contractions.When we speak of a flat hairspring, it is the hairspring as it is obtained. However, nothing prevents, especially in the embodiment of the figure 9 , to locate the mounting points 5 and 6 of the outer ends of the blades 1a, 1b out of the plane of the hairspring. This is how we can locate these two fixing points respectively on either side of the plane of the hairspring, so that the two blades 1a, 1b will form two symmetrical cones on either side of the plane of the hairspring. spiral. This solution has the advantage of preventing the turns of the two blades from touching each other. This solution makes it possible to produce spirals of small diameter with a large number of turns. It therefore constitutes another means of avoiding contact between the blades of the hairspring during the alternation of expansions and contractions.

Selon une autre variante de l'invention les deux lames 1a, 1b sont réalisées sur un wafer SOI (Silicon-On-Insulator, figures 10a, 10b), qui consiste en un empilement de couches de Si-SiO2-Si. Une lame la est gravée depuis la face externe d'une des couches de Si et l'autre lame 1b est gravée depuis la face externe de la deuxième couche de Si. Dans ce cas, les extrémités internes des deux lames sont rendues solidaires par la couche intermédiaire 8 de SiO2. L'avantage de cette forme d'exécution est de réduire le diamètre du spiral, car on augmente la distance entre deux spires voisines. Cet avantage est encore plus prononcé si on étend le spiral verticalement comme à la figure 10.According to another variant of the invention, the two blades 1a, 1b are produced on an SOI (Silicon-On-Insulator, figures 10a, 10b ), which consists of a stack of layers of Si-SiO 2 -Si. A blade 1a is etched from the outer face of one of the layers of Si and the other blade 1b is etched from the outer face of the second layer of Si. In this case, the inner ends of the two blades are made integral by the intermediate layer 8 of SiO 2 . The advantage of this embodiment is to reduce the diameter of the hairspring, because the distance between two neighboring turns is increased. This advantage is even more pronounced if we extend the hairspring vertically as in the figure 10 .

La figure 11 illustre une autre variante des figures 10a, 10b, dans laquelle les extrémités internes des lames la, 1b sont solidaires d'une même virole, alors que leurs extrémités externes sont solidaires de la couche intermédiaire 5 de SiO2.The figure 11 illustrates another variant of figures 10a , 10b , in which the internal ends of the blades 1a, 1b are integral with the same ferrule, while their external ends are integral with the intermediate layer 5 of SiO 2 .

Claims (8)

  1. A hairspring for a balance wheel/hairspring resonator, which hairspring comprises n blades, where n ≥ 2, fastened via at least one of their respective homologous ends and wound in spirals with an angular offset capable of neutralizing the lateral forces likely to be exerted on its central arbor when one of the ends of each blade is moved angularly about said central arbor relative to its other end, the hairspring comprising a collet (2), the blades being coplanar and the intern ends being fastened to the collet.
  2. The hairspring as claimed in the preceding claim, wherein the blades are fastened to each other via their two respective ends.
  3. The hairspring as claimed in one of the preceding claims, wherein the pitch of the blades is variable.
  4. The hairspring as claimed in one of the preceding claims, wherein the thickness of the blades is variable.
  5. The hairspring as claimed in one of the preceding claims, wherein the height of the blades is variable.
  6. The hairspring as claimed in one of the preceding claims, which is formed from single-crystal silicon.
  7. The hairspring as claimed in claim 6, wherein the single-crystal silicon is covered with a layer of amorphous silicon oxide.
  8. The hairspring as claimed in one of claims 1 to 4, which is formed from quartz.
EP09405126.5A 2008-07-29 2009-07-24 Hairspring for sprung balance Active EP2154583B1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
EP09405126.5A EP2154583B1 (en) 2008-07-29 2009-07-24 Hairspring for sprung balance
EP12180170.8A EP2523053B1 (en) 2008-07-29 2009-07-24 Hairspring for sprung balance

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP08405188.7A EP2151722B8 (en) 2008-07-29 2008-07-29 Hairspring for balance-spring resonator
EP09405126.5A EP2154583B1 (en) 2008-07-29 2009-07-24 Hairspring for sprung balance

Related Child Applications (2)

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EP12180170.8A Division EP2523053B1 (en) 2008-07-29 2009-07-24 Hairspring for sprung balance
EP12180170.8A Division-Into EP2523053B1 (en) 2008-07-29 2009-07-24 Hairspring for sprung balance

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EP2154583A1 EP2154583A1 (en) 2010-02-17
EP2154583B1 true EP2154583B1 (en) 2020-08-05

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EP09405126.5A Active EP2154583B1 (en) 2008-07-29 2009-07-24 Hairspring for sprung balance
EP12180170.8A Active EP2523053B1 (en) 2008-07-29 2009-07-24 Hairspring for sprung balance

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US (2) US8002460B2 (en)
EP (3) EP2151722B8 (en)
JP (2) JP5474432B2 (en)
CN (2) CN101639661B (en)
CH (1) CH699178B1 (en)

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Also Published As

Publication number Publication date
CH699178B1 (en) 2014-05-15
JP2014089214A (en) 2014-05-15
JP2010032522A (en) 2010-02-12
EP2151722A1 (en) 2010-02-10
CH699178A2 (en) 2010-01-29
US8002460B2 (en) 2011-08-23
US8393783B2 (en) 2013-03-12
EP2523053A1 (en) 2012-11-14
JP5474432B2 (en) 2014-04-16
CN101639661A (en) 2010-02-03
US20100027382A1 (en) 2010-02-04
EP2523053B1 (en) 2021-12-22
JP5657152B2 (en) 2015-01-21
CN102520605A (en) 2012-06-27
EP2151722B1 (en) 2018-09-12
US20110249537A1 (en) 2011-10-13
EP2151722B8 (en) 2021-03-31
CN102520605B (en) 2014-02-26
EP2154583A1 (en) 2010-02-17
CN101639661B (en) 2012-07-04

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