EP3767397B1 - Clock movement comprising a rotary element provided with a magnetic structure having a periodic configuration - Google Patents

Clock movement comprising a rotary element provided with a magnetic structure having a periodic configuration Download PDF

Info

Publication number
EP3767397B1
EP3767397B1 EP19187333.0A EP19187333A EP3767397B1 EP 3767397 B1 EP3767397 B1 EP 3767397B1 EP 19187333 A EP19187333 A EP 19187333A EP 3767397 B1 EP3767397 B1 EP 3767397B1
Authority
EP
European Patent Office
Prior art keywords
magnetic
elements
angular
torque
timepiece movement
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
EP19187333.0A
Other languages
German (de)
French (fr)
Other versions
EP3767397A1 (en
Inventor
Gianni Di Domenico
Marc Stranczl
Benoît LEGERET
René Piguet
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Swatch Group Research and Development SA
Original Assignee
Swatch Group Research and Development SA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Swatch Group Research and Development SA filed Critical Swatch Group Research and Development SA
Priority to EP19187333.0A priority Critical patent/EP3767397B1/en
Priority to US16/891,168 priority patent/US11822294B2/en
Priority to JP2020108538A priority patent/JP6982139B2/en
Priority to CN202010691556.5A priority patent/CN112241120B/en
Publication of EP3767397A1 publication Critical patent/EP3767397A1/en
Application granted granted Critical
Publication of EP3767397B1 publication Critical patent/EP3767397B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • GPHYSICS
    • G04HOROLOGY
    • G04CELECTROMECHANICAL CLOCKS OR WATCHES
    • G04C5/00Electric or magnetic means for converting oscillatory to rotary motion in time-pieces, i.e. electric or magnetic escapements
    • G04C5/005Magnetic or electromagnetic means
    • GPHYSICS
    • G04HOROLOGY
    • G04BMECHANICALLY-DRIVEN CLOCKS OR WATCHES; MECHANICAL PARTS OF CLOCKS OR WATCHES IN GENERAL; TIME PIECES USING THE POSITION OF THE SUN, MOON OR STARS
    • G04B15/00Escapements
    • G04B15/14Component parts or constructional details, e.g. construction of the lever or the escape wheel
    • GPHYSICS
    • G04HOROLOGY
    • G04BMECHANICALLY-DRIVEN CLOCKS OR WATCHES; MECHANICAL PARTS OF CLOCKS OR WATCHES IN GENERAL; TIME PIECES USING THE POSITION OF THE SUN, MOON OR STARS
    • G04B17/00Mechanisms for stabilising frequency
    • G04B17/32Component parts or constructional details, e.g. collet, stud, virole or piton
    • GPHYSICS
    • G04HOROLOGY
    • G04CELECTROMECHANICAL CLOCKS OR WATCHES
    • G04C3/00Electromechanical clocks or watches independent of other time-pieces and in which the movement is maintained by electric means
    • G04C3/08Electromechanical clocks or watches independent of other time-pieces and in which the movement is maintained by electric means wherein movement is regulated by a mechanical oscillator other than a pendulum or balance, e.g. by a tuning fork, e.g. electrostatically
    • G04C3/10Electromechanical clocks or watches independent of other time-pieces and in which the movement is maintained by electric means wherein movement is regulated by a mechanical oscillator other than a pendulum or balance, e.g. by a tuning fork, e.g. electrostatically driven by electromagnetic means
    • G04C3/101Electromechanical clocks or watches independent of other time-pieces and in which the movement is maintained by electric means wherein movement is regulated by a mechanical oscillator other than a pendulum or balance, e.g. by a tuning fork, e.g. electrostatically driven by electromagnetic means constructional details
    • GPHYSICS
    • G04HOROLOGY
    • G04CELECTROMECHANICAL CLOCKS OR WATCHES
    • G04C3/00Electromechanical clocks or watches independent of other time-pieces and in which the movement is maintained by electric means
    • G04C3/08Electromechanical clocks or watches independent of other time-pieces and in which the movement is maintained by electric means wherein movement is regulated by a mechanical oscillator other than a pendulum or balance, e.g. by a tuning fork, e.g. electrostatically
    • G04C3/10Electromechanical clocks or watches independent of other time-pieces and in which the movement is maintained by electric means wherein movement is regulated by a mechanical oscillator other than a pendulum or balance, e.g. by a tuning fork, e.g. electrostatically driven by electromagnetic means
    • G04C3/101Electromechanical clocks or watches independent of other time-pieces and in which the movement is maintained by electric means wherein movement is regulated by a mechanical oscillator other than a pendulum or balance, e.g. by a tuning fork, e.g. electrostatically driven by electromagnetic means constructional details
    • G04C3/104Electromechanical clocks or watches independent of other time-pieces and in which the movement is maintained by electric means wherein movement is regulated by a mechanical oscillator other than a pendulum or balance, e.g. by a tuning fork, e.g. electrostatically driven by electromagnetic means constructional details of the pawl or the ratched-wheel
    • G04C3/105Electromechanical clocks or watches independent of other time-pieces and in which the movement is maintained by electric means wherein movement is regulated by a mechanical oscillator other than a pendulum or balance, e.g. by a tuning fork, e.g. electrostatically driven by electromagnetic means constructional details of the pawl or the ratched-wheel pawl and ratched-wheel being magnetically coupled

Definitions

  • the invention relates to watch movements provided with at least one rotating element participating in at least one magnetic system of the watch movement, this rotating element being provided with an annular magnetized structure having an angular variation of at least one physical parameter which defines.
  • Rotating element means an element arranged in the watch movement so as to be able to undergo a certain rotation, in a given direction or in both directions. Thus, this expression applies for example as much to an escape wheel as to a balance wheel.
  • watch movements comprising at least one magnetic system intervening in the operation of the watch movement are known from the prior art.
  • watch movements equipped with a magnetic escapement formed by a magnetic system in which participate at least one magnet carried by an anchor and at least one magnet carried by an escape wheel are known.
  • Such magnetic escapements are described in particular in the documents EP_2887157 , EP_3128379 , EP_3128379 , EP_3208667 , EP_3217227 and CH_712154 .
  • Such watch movements are described in particular in the documents CH_709031 and CH_713070 .
  • a rotating element supports an annular magnetized structure and when the latter exhibits an angular variation of at least one physical parameter which defines it
  • the inventors have observed that, in the presence of at least one ferromagnetic part located in particular at the periphery of the rotating element, not only does this ferromagnetic part exert a radial attraction on the annular magnetized structure, so that a parasitic friction force is generated in the bearings of the shaft of the rotating element, but in addition the element rotating is subjected to a parasitic magnetic torque varying according to the angular position of the rotating element.
  • a parasitic magnetic torque disturbs the proper functioning of the magnetic system in which the rotating element participates, in particular in the case of a magnetic escapement having an escape wheel of the type of the aforementioned rotating element.
  • an anchor magnet having a steel axis must remain at the periphery of the magnetic escape wheel to which this magnetic anchor is associated.
  • the inventors have decided to seek a technical solution to solve the particular technical problem, namely the manifestation of a disturbing magnetic torque, which neither requires nor having to change the nature of magnetic elements in the environment of an element. revolving fitted with a magnetic structure presenting an angular variation of at least one physical parameter, nor having to modify the design of the watch movement, that is to say its various functional parts and their interactions.
  • the present invention relates to a watch movement comprising a mechanism formed by a rotating element, provided with an annular magnetic structure having an angular variation of at least one physical parameter which defines it, and by a first set of elements magnetic elements which consists of a functional magnetic element or of a plurality of functional magnetic elements, this first set of magnetic elements not being integral in rotation with the rotating element and having with the annular magnetized structure generally a first magnetic interaction which generates on the rotating element a first parasitic magnetic torque.
  • the watch movement further comprises a second set of magnetic elements which consists of a magnetic compensation element or of a plurality of magnetic compensation elements not belonging to any mechanism of the watch movement, this second set of magnetic being not integral in rotation with the rotating element and having with the globally annular magnetized structure a second magnetic interaction which generates on the rotating element a second parasitic magnetic torque.
  • the second set of magnetic elements is arranged relative to the first set of magnetic elements so that the maximum absolute value of the torque resulting from the addition of the first parasitic magnetic torque with the second parasitic magnetic torque is less than the maximum absolute value of the first parasitic magnetic couple.
  • the first parasitic magnetic torque as a function of the angular position of the rotating element defines a first curve of the sinusoidal type having an angular period equal to 360°/N with N being an integer greater than one ( N > 1).
  • the second set of magnetic elements is arranged relative to the first set of magnetic elements so that the second parasitic magnetic torque as a function of the angular position of the rotating element defines a second curve of the sinusoidal type also having said period angular, and so that the first and second parasitic magnetic couples have between them an angular phase shift substantially equal to 180°.
  • the second set of magnetic elements consists of K magnetic compensation elements or K groups of magnetic compensation elements having substantially the same configuration, K being an integer greater than one (K>1) .
  • the overall parasitic magnetic torque is therefore reduced, which is exerted by at least one functional magnetic element on the rotating element provided with an annular magnetic structure, by adding in the surrounding space of this rotating element at least one magnetic compensation element.
  • the annular magnetized structure is configured and the compensation magnetic element is arranged so that the maximum absolute value of said resulting torque is less than 15% of the maximum value of the first parasitic magnetic torque.
  • Claim 1 defines a horological movement according to the present invention. Preferred embodiments are defined in claims 2-14.
  • a mechanical watch movement 2 of the prior art will be described below in order to better highlight the technical problem posed by such a watch movement which is provided with a balance wheel 4 and a magnetic escapement formed by a magnetic lever 8 and an escape wheel referenced 6 in the variant of the Figure 1 , respectively 6A in the variant of Figure 2 and 3 .
  • the magnetic anchor is provided with two magnetic pallets 9, 10 arranged at the free ends of two arms.
  • the escapement wheel 6 comprises a non-magnetic support 11 on which is arranged a structured magnetic layer 12 which alone forms an annular magnetic structure of the escapement wheel.
  • This structured magnetic layer has a magnetic track 14 which surrounds the shaft 20 of the escape wheel along a generally circular path but with convex portions 14a, that is to say outgoing, and concave portions 14b, i.e. incoming.
  • the structured magnetic layer 12 has external magnetic pads 16 and internal magnetic pads 17 which are located respectively on both sides of the magnetic track 14 and which define magnetic barriers for the magnetic pallets of the anchor 8. Operation of such a magnetic escapement is described in the documents cited above in the technological background, so that reference will be made to these documents to know it.
  • the escapement wheel 6A comprises two structured magnetic layers 12A and 12B which are each identical to the layer 12 of the Figure 1 and which are arranged axially opposite each other with the pads 16 and 17 of the layer 12A superimposed on the corresponding pads of the layer 12B.
  • the two layers 12A and 12B are arranged on two respective supports 11A and 11B, made of non-magnetic material, which are fixedly mounted on the shaft 20, which comprises a pinion 22 for driving the escape wheel 6A.
  • the two structured magnetic layers are located on the side of an intermediate space defined by the two supports 11A, 11B and into which the two respective ends of the two arms of the anchor 8 penetrate, so as to allow magnetic interaction of the magnetic pallets of the anchor with the two layers 12A and 12B.
  • the two structured magnetized layers 12A, 12B together form an annular magnetized structure of the magnetic escape wheel 6A.
  • the two layers 12A, 12B each have a constant thickness, so that the annular magnetized structure also has a constant thickness axially.
  • a watch movement is considered comprising a mechanism formed by a rotating element, provided with an annular magnetized structure having an angular variation of at least one physical parameter defining this annular magnetized structure, and by a first set of magnetic elements which consists of at least one functional magnetic element, this first set of magnetic elements not being integral in rotation with the rotating element and generally having a first magnetic interaction with the annular magnetized structure .
  • the rotating element is a magnetic escape wheel.
  • the rotating element can be another component, in particular a pendulum.
  • the first set of magnetic elements consists of at least one axis made of ferromagnetic material, in particular the axis of the lever associated with the escape wheel and/or the axis an intermediate mobile located close to this wheel and forming a gear train which transmits the torque from a barrel to the escapement wheel.
  • the invention is not limited solely to axes made of ferromagnetic materials, but that it applies to any other magnetic element capable of being arranged at the immediate periphery of the rotating element in question, in particular to a magnetic escape wheel, and to present a significant magnetic interaction with its annular magnetized structure.
  • 'magnetic element' is meant a magnet, a ferromagnetic element or a combination of both.
  • annular magnetized structure exhibits an angular variation, namely the radial width of each structured magnetized layer 12A, 12B and the average distance of each structured magnetized layer from the axis of rotation 21 of the escape wheel 6A.
  • the angular variations of the radial width and the average distance to the axis of rotation of the two layers 12A, 12B, and therefore of the annular magnetized structure are periodic so that the annular magnetized structure has an angular period equal to 360°/N with N being an integer greater than one (N > 1).
  • the ferromagnetic axis 18 forms a body of revolution so that the volume of magnetic material that it defines remains invariant whatever the angular position of the anchor 8.
  • the first magnetic interaction between the magnetic axis 18 and the annular magnetic structure 12A-12B of wheel 6A generates on this wheel, because it comprises a periodic annular magnetic structure, a first parasitic magnetic torque which depends substantially only on the angular position of wheel 6A and which varies periodically in function of the angular position of the wheel 6A by having, in the variant considered, the same angular period PA, here 60° or ⁇ /3 [rad], as the annular magnetized structure 12A-12B.
  • PA angular period
  • a curve that is alternately positive and negative with positive extreme values which are close, normally identical but which may differ slightly, and negative extreme values which are close, normally identical but which may differ slightly .
  • the positive extreme values and the negative values are, in absolute values, close to each other, preferably almost identical but they can differ to a certain extent, for example by 10% to 20%.
  • a periodic character can be recognized in such a curve with the period as the angular distance between two positive extreme values or, equivalently, two negative extreme values.
  • the two half-periods forming the period of such a curve can have different values, as is the case of curve 30 at the Figure 4 , although it is advantageous for the two half-periods to have substantially the same value.
  • the watch movement is similar to that of the prior art described above as regards the mechanism(s) which compose it and it further comprises a magnetic compensation element 32 which is similar in shape to the magnetic axis 18 or, more generally, configured to generate on the annular magnetized structure, in particular on the structured magnetic layer 12A which forms it, a torque having substantially the same intensity as that of the torque generated by the axis 18 ( Figure 4 ).
  • This magnetic compensation element 32 is here formed by a magnetic pin, arranged at the periphery of the magnetic escape wheel and formed by a ferromagnetic material, and it is arranged so as to present an angular offset relative to the magnetic axis, related to an angular period of the periodic structured magnetized layer 12A and therefore to the angular period of the periodic annular magnetized structure.
  • a second parasitic magnetic torque generated by the magnetic pin 32 defines a curve similar to the curve 30 of the Figure 4 , but the first and second parasitic magnetic couples have between them a phase shift of about 180°, preferably 180°.
  • the magnetic pin 32 is arranged on the side diametrically opposite to the functional magnetic axis 18 to also compensate for the major part of the magnetic attraction force exerted by this axis 18 on escape wheel 6A.
  • the torque resulting from the addition of the first and second parasitic magnetic torques is shown in Figure 6 . It is first observed that the maximum absolute value V2 of this resulting torque is lower than the maximum absolute value V1 of the first parasitic magnetic torque represented in Figure 4 . In the example treated here, the maximum absolute value V2 of the resulting torque is slightly less than half the maximum absolute value V1 of the first parasitic magnetic torque.
  • the curve 34 of the resulting torque has a period equal to half the angular period PA of the structured magnetized layer 12A and therefore of the annular magnetized structure.
  • the watch movement comprises a second set of magnetic elements which consists of a magnetic compensation element or a plurality of magnetic compensation elements not belonging to any mechanism of the watch movement, this second set of magnetic elements being non-rotatably connected to the rotating element and having with the globally annular magnetized structure a second magnetic interaction which generates on the rotating element a second parasitic magnetic torque.
  • the second set of magnetic elements is arranged relative to the first set of magnetic elements so that the maximum absolute value of the torque resulting from the addition of the first and second parasitic magnetic torque is less than the maximum absolute value of the first parasitic magnetic torque.
  • the first parasitic magnetic torque as a function of the angular position of the rotating element defines a first curve of the sinusoidal type having an angular period equal to 360°/N , with N being an integer greater than one (N > 1).
  • the second set of magnetic elements is arranged relative to the first set of magnetic elements so that the second parasitic magnetic torque as a function of the angular position of said rotating element defines a second curve of the sinusoidal type also exhibiting said angular period, and so that the first and second parasitic magnetic couples have between them an angular phase shift substantially equal to 180°.
  • the watch movement shown partially on the Picture 7 , comprises a magnetic escape wheel 36 provided with an annular magnetized structure formed, as in Figure 2 , of two structured magnetic layers of which only the lower layer 38A appears at the Picture 7 .
  • the escape wheel comprises a shaft 20 and a non-magnetic support 40 carrying the lower magnetic layer 38A.
  • This escape wheel is arranged to rotate around an axis of rotation 21. It is associated with a magnetic anchor 8A, which is formed by a magnetic axis 18A and two non-magnetic arms, shown in broken lines, which carry at their ends free respectively two magnetic pallets 9, 10.
  • the structured magnetic layer 38A and the annular magnetic structure formed by this structured magnetic layer differ from the layer 12 A and from the annular magnetic structure of the Figure 5 by a new configuration.
  • the annular magnetized structure formed of the structured magnetized layer 38A or of two such superimposed layers, as shown in Figure 2 defines magnetic barriers 17A for the magnetic anchor which are angularly offset by the angular period PA. It will be noted that only internal magnetic pads 17A have been provided in the advantageous variant considered.
  • Layer 38A has a constant thickness and defines a magnetic track 14A with variable radial width.
  • the annular magnetized structure is configured so that its outer profile is substantially circular and continuous, as in the case of the advantageous variant of the Picture 7 .
  • By 'circular external profile' in the case of a structure having two structured magnetic layers, it is understood that each layer has an external profile which is substantially circular.
  • the diameters of the two structured magnetic layers are equal, so that the external profiles of these two layers define a cylindrical geometric surface.
  • Such an arrangement of the annular magnetized structure makes it possible, on the one hand, to reduce the first parasitic magnetic torque generated by the functional magnetic element or elements at the periphery of the escape wheel 36 and, on the other hand, to reduce the ratio between the maximum absolute value of the resulting torque (from the addition of the first parasitic magnetic torque and the parasitic magnetic torque generated by the compensation pin) and that of the first parasitic magnetic torque.
  • the second embodiment is distinguished from the first again by the fact that two functional magnetic elements at the direct periphery of the escape wheel are considered here, namely the magnetic axis 18A of the lever 8A and the magnetic axis 42 an intermediate mobile forming a cog between the escapement wheel and a barrel of the watch movement and meshing with the pinion of the escapement wheel.
  • the individual magnetic couples which are generated respectively by the two magnetic axes 18A and 42 (at least partly in ferromagnetic material).
  • the individual magnetic torque generated by the axis 42 is predominant.
  • the first parasitic magnetic torque ( Figure 8C ) has a curve 44 close to that of the Figure 8B , also with a period PA, these two curves having a certain phase difference between them.
  • the magnetic compensation pin 32A is arranged so that the individual magnetic torque, constituting the second parasitic magnetic torque, which it exerts on the escape wheel has an angular phase shift of 180° with the first magnetic torque. parasitic, and not with the individual magnetic torque of the ferromagnetic axis 42 ( Figure 8B ), although the latter is largely predominant.
  • the pin 32A is dimensioned so as to optimize the compensation that it produces, in particular its diameter and/or its distance from the axis of rotation 21 is/are adjusted so that the maximum absolute value of the second parasitic magnetic torque, generated by the compensation pin 32A, best compensates for the first parasitic magnetic torque and that the resulting torque, whose curve 46 is given at the Figure 8D , from the addition of first and second parasitic magnetic couples thus have the smallest possible amplitude, that is to say the smallest possible maximum absolute value.
  • the maximum absolute value V4 of the torque resulting from the addition of the first and second aforementioned parasitic magnetic torques is less than 30% of the maximum absolute value V3 of the first parasitic magnetic torque. Indeed, in the example described, it is observed that the ratio between the maximum absolute value V4 of the curve 46 and the maximum absolute value V3 of the curve 44 gives approximately 1/5.
  • the compensation pin 32A is arranged so that its position relative to the axis of rotation 21 can be adjusted to adjust the angular phase shift and/or the value maximum absolute value of the second parasitic magnetic torque (curve 44) and thus optimize the curve of the resulting torque (curve 46), in particular the maximum absolute value V4 of this resulting torque, that is to say reduce this maximum absolute value at the smallest possible value.
  • the pin 32A forms an eccentric that the watchmaker can turn using a tool to adjust its distance from the axis of rotation and therefore from the annular magnetic structure. If it is desired not to vary the angular position of the compensation pin, it is possible in a variant to arrange the compensation pin in a kind of radial slide. A person skilled in the art will know how to provide the means necessary for adjusting the radial and/or angular position of this compensation pin.
  • This third embodiment differs from the first embodiment only in that the single pin of compensation of the second embodiment is replaced by two compensation pins 50, 52 similar to the magnetic axis 18 which here constitutes all the functional magnetic elements considered (this magnetic axis considered can be either the axis of the anchor, or the axis of an intermediate mobile meshing with the escapement wheel 6A).
  • the two compensation pins are arranged so that the two individual magnetic torques which they respectively exert on the escape wheel are out of phase respectively by 120° and 240° (equivalent to -120°) relative to the first parasitic magnetic torque generated by the magnetic axis 18.
  • the two magnetic compensation pins 50 and 52 are arranged so as to distribute these two compensation pins and the magnetic axis 18 as evenly as possible around the axis of rotation to minimize friction in the bearings of the wheel. exhaust due to the magnetic attraction exerted by each of them on the annular magnetized structure of this wheel.
  • the curve 54 of the resultant torque exerted overall by the two compensating pins and the functional magnetic element of the Figure 9 is given.
  • the maximum absolute value V5 of curve 54 is relatively low. It is less than 20% of the maximum absolute value V1 of the first parasitic magnetic torque (see Figure 4 ).
  • the curve 54 is periodic and has a period angular period equal to one third of the angular period PA of the annular magnetized structure, ie an angular period equal to PA/3.
  • This fourth embodiment differs from the second embodiment in that the single magnetic compensation pin of the second embodiment is replaced here by two magnetic compensation pins 32B and 32C which are arranged in an equivalent manner to the third embodiment .
  • the first set of magnetic elements comprises a plurality of functional magnetic elements, i.e. two magnetic axes in the variant described
  • the second set of magnetic elements comprises a plurality of magnetic compensation elements, i.e. two pins in this variant.
  • the two compensation pins are arranged so that the two individual magnetic torques which they respectively exert on the escape wheel are out of phase respectively by 120° and 240° relative to the first parasitic magnetic torque generated globally by the two magnetic axes 18A and 42.
  • This remainder is therefore equal to 10° so that the angle DA5 between the two pins 32B and 32C is equal to 40° in the example shown in Picture 11 , or at an angular period (equal to 30°) to which the remainder of 10° is added.
  • the angle DA6 between the axis 42 and the pin 32B does not correspond to an integer period PA to which one adds or subtracts 10°, although this angle DA6 approaches it due to the fact that the axis 42 is predominant in the first parasitic magnetic torque generated by the two functional magnetic elements on the escape wheel.
  • the curve 60 of the torque resulting from the addition of the first parasitic magnetic torque, globally generated by the first set of magnetic elements, with the second parasitic magnetic torque, globally generated by the second set of magnetic elements, is shown in Picture 12 .
  • the resulting torque is the result of the addition of all the individual parasitic magnetic torques that are considered.
  • the annular magnetized structure of the fourth embodiment is configured and the two magnetic compensation elements are arranged so that the maximum absolute value V6 of the resulting torque is less than 15%, or even 12% of the maximum absolute value V3 (see Figure 8C ) of the first parasitic magnetic couple.
  • a person skilled in the art can optimize the system by specifically configuring the two compensation pins which are preferably identical, in particular their respective diameters and their respective distances from the axis of rotation.
  • the two pins 32B and 32C are not here respectively identical, in their respective configurations and their relative arrangement on the periphery of the escapement wheel 36, to the two axes 18A and 42. If such were the case, one would in fact be in a variant of the second embodiment in which the two pins would together form a group of magnetic elements to be considered as an inseparable whole and not individually, that is to say not as two distinct compensation elements whose individual parasitic magnetic couples could present different phase shifts relative to the first magnetic couple parasite and selected as described above.
  • the two compensation pins to be in their respective configurations, in particular their dimensions and the material from which they are made, and their respective arrangements relative to the axis of rotation, in particular the distance to this axis of rotation, substantially identical to the compensation pin 32A of the second embodiment which optimizes the result of this second embodiment or that they have the same effect as this compensation pin 32A on the annular magnetic structure.
  • the second set of magnetic elements consists of K magnetic compensation elements or K groups of magnetic compensation elements having substantially the same configuration, K being an integer greater than one (K>1).

Description

Domaine techniqueTechnical area

L'invention concerne les mouvements horlogers munis d'au moins un élément tournant participant à au moins un système magnétique du mouvement horloger, cet élément tournant étant muni d'une structure aimantée annulaire présentant une variation angulaire d'au moins un paramètre physique qui la définit.The invention relates to watch movements provided with at least one rotating element participating in at least one magnetic system of the watch movement, this rotating element being provided with an annular magnetized structure having an angular variation of at least one physical parameter which defines.

Par 'élément tournant', on comprend un élément agencé dans le mouvement horloger de manière à pouvoir subir une certaine rotation, dans un sens donné ou dans les deux sens. Ainsi, cette expression s'applique par exemple autant à une roue d'échappement qu'à un balancier.“Rotating element” means an element arranged in the watch movement so as to be able to undergo a certain rotation, in a given direction or in both directions. Thus, this expression applies for example as much to an escape wheel as to a balance wheel.

Arrière-plan technologiqueTechnology background

Divers mouvements horlogers comprenant au moins un système magnétique intervenant dans le fonctionnement du mouvement horloger sont connus de l'art antérieur. On connaît notamment des mouvements horlogers équipés d'un échappement magnétique formé par un système magnétique auquel participent au moins un aimant porté par une ancre et au moins un aimant porté par une roue d'ancre. De tels échappements magnétiques sont notamment décrits dans les documents EP_2887157 , EP_3128379 , EP_3128379 , EP_3208667 , EP_3217227 et CH_712154 . On connaît aussi des mouvements horlogers ayant un échappement magnétique sans arrêtoir dont une partie du système magnétique est portée par le résonateur mécanique du mouvement horloger et l'autre partie est portée par une roue d'échappement. De tels mouvements horlogers sont notamment décrits dans les documents CH_709031 et CH_713070 .Various watch movements comprising at least one magnetic system intervening in the operation of the watch movement are known from the prior art. In particular, watch movements equipped with a magnetic escapement formed by a magnetic system in which participate at least one magnet carried by an anchor and at least one magnet carried by an escape wheel are known. Such magnetic escapements are described in particular in the documents EP_2887157 , EP_3128379 , EP_3128379 , EP_3208667 , EP_3217227 and CH_712154 . Also known are watch movements having a magnetic escapement without a stopper, part of the magnetic system of which is carried by the mechanical resonator of the watch movement and the other part is carried by an escape wheel. Such watch movements are described in particular in the documents CH_709031 and CH_713070 .

Résumé de l'inventionSummary of the invention

Lorsqu'un élément tournant supporte une structure aimantée annulaire et que cette dernière présente une variation angulaire d'au moins un paramètre physique qui la définit, les inventeurs ont observé que, en présence d'au moins une partie ferromagnétique situées notamment à la périphérie de l'élément tournant, non seulement cette partie ferromagnétique exerce une attraction radiale sur la structure aimantée annulaire, de sorte qu'une force de frottement parasite est engendrée dans les paliers de l'arbre de l'élément tournant, mais en plus l'élément tournant est soumis à un couple magnétique parasite variant en fonction de la position angulaire de l'élément tournant. Un tel couple magnétique parasite perturbe le bon fonctionnement du système magnétique auquel participe l'élément tournant, en particulier dans le cas d'un échappement magnétique ayant une roue d'échappement du type de l'élément tournant susmentionné.When a rotating element supports an annular magnetized structure and when the latter exhibits an angular variation of at least one physical parameter which defines it, the inventors have observed that, in the presence of at least one ferromagnetic part located in particular at the periphery of the rotating element, not only does this ferromagnetic part exert a radial attraction on the annular magnetized structure, so that a parasitic friction force is generated in the bearings of the shaft of the rotating element, but in addition the element rotating is subjected to a parasitic magnetic torque varying according to the angular position of the rotating element. Such a parasitic magnetic torque disturbs the proper functioning of the magnetic system in which the rotating element participates, in particular in the case of a magnetic escapement having an escape wheel of the type of the aforementioned rotating element.

Ayant mis en lumière ce problème technique additionnel, les inventeurs ont cherché une solution technique. La première pensée qui vient à l'esprit est de supprimer les éléments magnétiques (aimants et éléments en matériaux ferromagnétiques) à proximité de l'élément tournant ou de les éloigner suffisamment de ce dernier pour rendre négligeable leur interaction avec la structure aimantée annulaire. Cependant, il n'est souvent pas aisé de changer les matériaux sélectionnés pour les divers éléments et composants du mouvement horloger. Ainsi, bien qu'on connaisse des matériaux non ferromagnétiques pour fabriquer des axes / arbres d'éléments tournants, il est parfois préférable pour d'autres raisons techniques ou pour des questions de coûts de fabrication de conserver notamment l'acier pour de tels axes / arbres. Ensuite, il n'est souvent pas possible d'éloigner les éléments magnétiques dans l'environnement de l'élément tournant en question sans modifier la conception du mouvement horloger. Par exemple, une ancre magnétique ayant un axe en acier doit rester à la périphérie de la roue d'échappement magnétique à laquelle cette ancre magnétique est associée. Ainsi, les inventeurs ont décidé de chercher une solution technique pour résoudre le problème technique particulier, à savoir la manifestation d'un couple magnétique perturbateur, qui ne nécessite ni de devoir changer la nature d'éléments magnétiques dans l'environnement d'un élément tournant muni d'une structure aimantée présentant une variation angulaire d'au moins un paramètre physique, ni de devoir modifier la conception du mouvement horloger, c'est-à-dire ses diverses parties fonctionnelles et leur interactions.Having brought to light this additional technical problem, the inventors sought a technical solution. The first thought that comes to mind is to remove the magnetic elements (magnets and elements made of ferromagnetic materials) close to the rotating element or to move them far enough from the latter to make their interaction with the annular magnetized structure negligible. However, it is often not easy to change the materials selected for the various elements and components of the watch movement. Thus, although non-ferromagnetic materials are known for manufacturing axes / shafts of rotating elements, it is sometimes preferable for other technical reasons or for questions of manufacturing costs to keep steel in particular for such axes. / trees. Then, it is often not possible to remove the magnetic elements in the environment of the rotating element in question without modifying the design of the watch movement. For example, an anchor magnet having a steel axis must remain at the periphery of the magnetic escape wheel to which this magnetic anchor is associated. Thus, the inventors have decided to seek a technical solution to solve the particular technical problem, namely the manifestation of a disturbing magnetic torque, which neither requires nor having to change the nature of magnetic elements in the environment of an element. revolving fitted with a magnetic structure presenting an angular variation of at least one physical parameter, nor having to modify the design of the watch movement, that is to say its various functional parts and their interactions.

A cet effet, la présente invention concerne un mouvement horloger comprenant un mécanisme formé par un élément tournant, muni d'une structure aimantée annulaire présentant une variation angulaire d'au moins un paramètre physique qui la définit, et par un premier ensemble d'éléments magnétiques qui est constitué d'un élément magnétique fonctionnel ou d'une pluralité d'éléments magnétiques fonctionnels, ce premier ensemble d'éléments magnétiques étant non solidaire en rotation de l'élément tournant et ayant avec la structure aimantée annulaire globalement une première interaction magnétique qui engendre sur l'élément tournant un premier couple magnétique parasite. Le mouvement horloger comprend en outre un deuxième ensemble d'éléments magnétiques qui est constitué d'un élément magnétique de compensation ou d'une pluralité d'éléments magnétiques de compensation n'appartenant à aucun mécanisme du mouvement horloger, ce deuxième ensemble d'éléments magnétiques étant non solidaire en rotation de l'élément tournant et ayant avec la structure aimantée annulaire globalement une deuxième interaction magnétique qui engendre sur l'élément tournant un deuxième couple magnétique parasite. Le deuxième ensemble d'éléments magnétiques est agencé relativement au premier ensemble d'éléments magnétiques de manière que la valeur absolue maximale du couple résultant de l'addition du premier couple magnétique parasite avec le deuxième couple magnétique parasite est inférieure à la valeur absolue maximale du premier couple magnétique parasite.To this end, the present invention relates to a watch movement comprising a mechanism formed by a rotating element, provided with an annular magnetic structure having an angular variation of at least one physical parameter which defines it, and by a first set of elements magnetic elements which consists of a functional magnetic element or of a plurality of functional magnetic elements, this first set of magnetic elements not being integral in rotation with the rotating element and having with the annular magnetized structure generally a first magnetic interaction which generates on the rotating element a first parasitic magnetic torque. The watch movement further comprises a second set of magnetic elements which consists of a magnetic compensation element or of a plurality of magnetic compensation elements not belonging to any mechanism of the watch movement, this second set of magnetic being not integral in rotation with the rotating element and having with the globally annular magnetized structure a second magnetic interaction which generates on the rotating element a second parasitic magnetic torque. The second set of magnetic elements is arranged relative to the first set of magnetic elements so that the maximum absolute value of the torque resulting from the addition of the first parasitic magnetic torque with the second parasitic magnetic torque is less than the maximum absolute value of the first parasitic magnetic couple.

Selon un mode de réalisation principal, le premier couple magnétique parasite en fonction de la position angulaire de l'élément tournant définit une première courbe du type sinusoïdal présentant une période angulaire égale à 360°/N avec N étant un nombre entier supérieur à un (N > 1). De plus, le deuxième ensemble d'éléments magnétiques est agencé relativement au premier ensemble d'éléments magnétiques de manière que le deuxième couple magnétique parasite en fonction de la position angulaire de l'élément tournant définit une deuxième courbe du type sinusoïdal présentant également ladite période angulaire, et de manière que les premier et deuxième couples magnétiques parasites présentent entre eux un déphasage angulaire sensiblement égal à 180°.According to a main embodiment, the first parasitic magnetic torque as a function of the angular position of the rotating element defines a first curve of the sinusoidal type having an angular period equal to 360°/N with N being an integer greater than one ( N > 1). In addition, the second set of magnetic elements is arranged relative to the first set of magnetic elements so that the second parasitic magnetic torque as a function of the angular position of the rotating element defines a second curve of the sinusoidal type also having said period angular, and so that the first and second parasitic magnetic couples have between them an angular phase shift substantially equal to 180°.

Selon un mode de réalisation amélioré, le deuxième ensemble d'éléments magnétiques est constitué de K éléments magnétiques de compensation ou K groupes d'éléments magnétiques de compensation présentant sensiblement une même configuration, K étant un nombre entier supérieur à un (K > 1). Les K éléments magnétiques de compensation ou groupes d'éléments magnétiques de compensation sont agencés de manière que K couples magnétiques parasites, engendrés sur l'élément tournant respectivement par ces K éléments magnétiques de compensation ou groupes d'éléments magnétiques de compensation, présentent relativement au premier couple magnétique parasite respectivement K déphasages angulaires qui sont respectivement égaux à sensiblement J·360°/(K+1) avec J étant un nombre entier allant de un jusqu'à K, soit J = 1, ..., K.According to an improved embodiment, the second set of magnetic elements consists of K magnetic compensation elements or K groups of magnetic compensation elements having substantially the same configuration, K being an integer greater than one (K>1) . The K magnetic compensation elements or groups of magnetic compensation elements are arranged in such a way that K parasitic magnetic couples, generated on the rotating element respectively by these K magnetic compensation elements or groups of magnetic compensation elements, present relative to the first parasitic magnetic torque respectively K angular phase shifts which are respectively equal to substantially J 360°/(K+1) with J being an integer ranging from one to K, i.e. J = 1, ..., K.

Grâce aux caractéristiques de l'objet de l'invention, on diminue donc le couple magnétique parasite global, qui s'exerce par au moins un élément magnétique fonctionnel sur l'élément tournant muni d'une structure aimantée annulaire, en ajoutant dans l'espace environnant de cet élément tournant au moins un élément magnétique de compensation.Thanks to the characteristics of the object of the invention, the overall parasitic magnetic torque is therefore reduced, which is exerted by at least one functional magnetic element on the rotating element provided with an annular magnetic structure, by adding in the surrounding space of this rotating element at least one magnetic compensation element.

Dans un mode de réalisation avantageux où le nombre entier K est prévu égal à deux (K = 2), la structure aimantée annulaire est configurée et l'élément magnétique de compensation est agencé de manière que la valeur absolue maximale dudit couple résultant est inférieure à 15% de la valeur maximale du premier couple magnétique parasite. La revendication 1 définit un mouvement horloger selon la présente invention. Des modes de réalisation préférés sont définis dans les revendications 2-14.In an advantageous embodiment where the integer K is provided equal to two (K = 2), the annular magnetized structure is configured and the compensation magnetic element is arranged so that the maximum absolute value of said resulting torque is less than 15% of the maximum value of the first parasitic magnetic torque. Claim 1 defines a horological movement according to the present invention. Preferred embodiments are defined in claims 2-14.

Brève description des figuresBrief description of figures

L'invention sera décrite ci-après de manière plus détaillée à l'aide des dessins annexés, donnés à titre d'exemples nullement limitatifs, dans lesquels :

  • La Figure 1 est un vue partielle et simplifiée d'un mouvement horloger mécanique muni d'un échappement magnétique divulgué dans le document EP_3208667 ,
  • La Figure 2 est une coupe transversale d'un échappement magnétique du type divulgué dans le document EP_3208667 ,
  • La Figure 3 est une vue partielle, en coupe horizontale, de l'échappement magnétique de la Figure 2,
  • La Figure 4 montre la courbe d'un couple perturbateur engendré par l'axe magnétique de l'ancre sur la roue d'échappement en fonction de la position angulaire de cette dernière avec l'échappement magnétique des Figures 2 et 3,
  • La Figure 5 montre partiellement un premier mode de réalisation d'un mouvement mécanique selon l'invention,
  • La Figure 6 montre une courbe d'un couple perturbateur restant qui s'exerce sur la roue d'échappement en fonction de sa position angulaire dans le premier mode de réalisation,
  • La Figure 7 montre partiellement un deuxième mode de réalisation d'un mouvement mécanique selon l'invention,
  • Les Figures 8A et 8B montrent respectivement les deux courbes de couples perturbateurs engendrés, en fonction de la position angulaire de la roue d'échappement, individuellement par l'axe de l'ancre et l'axe d'un mobile intermédiaire sur la roue d'échappement dans le deuxième mode de réalisation,
  • La Figure 8C montre un couple perturbateur exercé globalement par les éléments magnétiques fonctionnels que sont l'axe de l'ancre et l'axe du mobile intermédiaire sur la roue d'échappement dans le deuxième mode de réalisation,
  • La Figure 8D montre le couple perturbateur restant qui s'exerce sur la roue d'échappement en fonction de sa position angulaire dans le deuxième mode de réalisation,
  • La Figure 9 montre partiellement un troisième mode de réalisation d'un mouvement mécanique selon l'invention,
  • La Figure 10 montre le couple perturbateur restant qui s'exerce sur la roue d'échappement en fonction de sa position angulaire dans le troisième mode de réalisation.
  • La Figure 11 montre partiellement un quatrième mode de réalisation d'un mouvement mécanique selon l'invention, et
  • La Figure 12 montre le couple perturbateur résiduel qui s'exerce sur la roue d'échappement en fonction de sa position angulaire dans le quatrième mode de réalisation.
The invention will be described below in more detail using the accompanying drawings, given by way of non-limiting examples, in which:
  • The Figure 1 is a partial and simplified view of a mechanical watch movement provided with a magnetic escapement disclosed in the document EP_3208667 ,
  • The Figure 2 is a cross-section of a magnetic escapement of the type disclosed in the document EP_3208667 ,
  • The Figure 3 is a partial view, in horizontal section, of the magnetic escapement of the Figure 2 ,
  • The Figure 4 shows the curve of a disturbing torque generated by the magnetic axis of the pallet on the escapement wheel as a function of the angular position of the latter with the magnetic escapement of the Figure 2 and 3 ,
  • The Figure 5 partially shows a first embodiment of a mechanical movement according to the invention,
  • The Figure 6 shows a curve of a remaining disturbing torque which is exerted on the escape wheel as a function of its angular position in the first embodiment,
  • The Picture 7 partially shows a second embodiment of a mechanical movement according to the invention,
  • The Figures 8A and 8B show respectively the two curves of disturbing torques generated, as a function of the angular position of the escape wheel, individually by the axis of the lever and the axis of a mobile intermediate on the escape wheel in the second embodiment,
  • The Figure 8C shows a disturbing torque exerted overall by the functional magnetic elements which are the axis of the lever and the axis of the intermediate wheel set on the escape wheel in the second embodiment,
  • The Figure 8D shows the remaining disturbing torque which is exerted on the escape wheel as a function of its angular position in the second embodiment,
  • The Figure 9 partially shows a third embodiment of a mechanical movement according to the invention,
  • The Picture 10 shows the remaining disturbing torque exerted on the escape wheel as a function of its angular position in the third embodiment.
  • The Picture 11 partially shows a fourth embodiment of a mechanical movement according to the invention, and
  • The Picture 12 shows the residual disturbing torque exerted on the escape wheel as a function of its angular position in the fourth embodiment.

Description détaillée de l'inventionDetailed description of the invention

En référence aux Figures 1 à 4, on décrira ci-après un mouvement horloger mécanique 2 de l'art antérieur pour mieux mettre en lumière le problème technique posé par un tel mouvement horloger qui est muni d'un balancier 4 et d'un échappement magnétique formé par une ancre magnétique 8 et une roue d'échappement référencée 6 dans la variante de la Figure 1, respectivement 6A dans la variante des Figures 2 et 3. L'ancre magnétique est munie de deux palettes magnétiques 9, 10 agencées aux extrémités libres de deux bras.With reference to Figures 1 to 4 , a mechanical watch movement 2 of the prior art will be described below in order to better highlight the technical problem posed by such a watch movement which is provided with a balance wheel 4 and a magnetic escapement formed by a magnetic lever 8 and an escape wheel referenced 6 in the variant of the Figure 1 , respectively 6A in the variant of Figure 2 and 3 . The magnetic anchor is provided with two magnetic pallets 9, 10 arranged at the free ends of two arms.

Dans la variante de la Figure 1, la roue d'échappement 6 comprend un support amagnétique 11 sur lequel est agencée une couche aimantée structurée 12 qui forme à elle seule une structure aimantée annulaire de la roue d'échappement. Cette couche aimantée structurée présente une piste aimantée 14 qui entoure l'arbre 20 de la roue d'échappement selon un tracé généralement circulaire mais avec des portions convexes 14a, c'est-à-dire sortantes, et des portions concaves 14b, c'est-à-dire entrantes. De plus, la couche aimantée structurée 12 présente des plages aimantées externes 16 et des plages aimantées internes 17 qui sont situées respectivement des deux côtés de la piste aimantée 14 et qui définissent des barrières magnétiques pour les palettes magnétiques de l'ancre 8. Le fonctionnement d'un tel échappement magnétique est décrit dans les documents cités précédemment dans l'arrière-plan technologique, de sorte qu'on se réfèrera à ces documents pour le connaître.In the variant of Figure 1 , the escapement wheel 6 comprises a non-magnetic support 11 on which is arranged a structured magnetic layer 12 which alone forms an annular magnetic structure of the escapement wheel. This structured magnetic layer has a magnetic track 14 which surrounds the shaft 20 of the escape wheel along a generally circular path but with convex portions 14a, that is to say outgoing, and concave portions 14b, i.e. incoming. In addition, the structured magnetic layer 12 has external magnetic pads 16 and internal magnetic pads 17 which are located respectively on both sides of the magnetic track 14 and which define magnetic barriers for the magnetic pallets of the anchor 8. Operation of such a magnetic escapement is described in the documents cited above in the technological background, so that reference will be made to these documents to know it.

Dans la variante des Figures 2 et 3, la roue d'échappement 6A comprend deux couches aimantées structurées 12A et 12B qui sont chacune identiques à la couche 12 de la Figure 1 et qui sont agencées axialement l'une en regard de l'autre avec les plages 16 et 17 de la couche 12A superposées aux plages correspondantes de la couche 12B. Les deux couches 12A et 12B sont agencées sur deux supports respectifs 11A et 11B, en matériau amagnétique, qui sont montés fixement sur l'arbre 20, lequel comporte un pignon 22 d'entraînement de la roue d'échappement 6A. Les deux couches aimantées structurées sont situées du côté d'un espace intermédiaire défini par les deux supports 11A, 11B et dans lequel pénètre les deux extrémités respectives des deux bras de l'ancre 8, de manière à permettre une interaction magnétique des palettes magnétiques de l'ancre avec les deux couches 12A et 12B. Les deux couches aimantées structurées 12A, 12B forment ensemble une structure aimantée annulaire de la roue d'échappement magnétique 6A. Les deux couches 12A, 12B ont chacune une épaisseur constante, de sorte que la structure aimantée annulaire a aussi axialement une épaisseur constante.In the variant of Figure 2 and 3 , the escapement wheel 6A comprises two structured magnetic layers 12A and 12B which are each identical to the layer 12 of the Figure 1 and which are arranged axially opposite each other with the pads 16 and 17 of the layer 12A superimposed on the corresponding pads of the layer 12B. The two layers 12A and 12B are arranged on two respective supports 11A and 11B, made of non-magnetic material, which are fixedly mounted on the shaft 20, which comprises a pinion 22 for driving the escape wheel 6A. The two structured magnetic layers are located on the side of an intermediate space defined by the two supports 11A, 11B and into which the two respective ends of the two arms of the anchor 8 penetrate, so as to allow magnetic interaction of the magnetic pallets of the anchor with the two layers 12A and 12B. The two structured magnetized layers 12A, 12B together form an annular magnetized structure of the magnetic escape wheel 6A. The two layers 12A, 12B each have a constant thickness, so that the annular magnetized structure also has a constant thickness axially.

Comme indiqué dans le résumé de l'invention, pour diverses raisons, l'axe 18 de l'ancre est prévu ici en matériau ferromagnétique. De manière générale, dans le cadre de l'invention, on considère un mouvement horloger comprenant un mécanisme formé par un élément tournant, muni d'une structure aimantée annulaire présentant une variation angulaire d'au moins un paramètre physique définissant cette structure aimantée annulaire, et par un premier ensemble d'éléments magnétiques qui est constitué d'au moins un élément magnétique fonctionnel, ce premier ensemble d'éléments magnétiques étant non solidaire en rotation de l'élément tournant et ayant globalement une première interaction magnétique avec la structure aimantée annulaire. Dans les exemples considérés dans la description détaillée de l'invention, l'élément tournant est une roue d'échappement magnétique. Cependant, l'élément tournant peut être un autre composant, notamment un balancier. Ensuite, dans les exemples considérés, le premier ensemble d'éléments magnétiques est constitué d'au moins un axe en matériau ferromagnétique, en particulier de l'axe de l'ancre associée à la roue d'échappement et/ou de l'axe d'un mobile intermédiaire situé à proximité de cette roue et formant un rouage qui transmet le couple d'un barillet à la roue d'échappement. On comprendra que l'invention ne se limite pas aux seuls axes en matériaux ferromagnétiques, mais qu'elle s'applique à tout autre élément magnétique susceptible d'être agencé à la périphérie immédiate de l'élément tournant en question, en particulier d'une roue d'échappement magnétique, et de présenter une interaction magnétique significative avec sa structure aimantée annulaire. Par 'élément magnétique', on comprend un aimant, un élément ferromagnétique ou une combinaison des deux.As indicated in the summary of the invention, for various reasons, the axis 18 of the anchor is provided here in ferromagnetic material. In general, within the scope of the invention, a watch movement is considered comprising a mechanism formed by a rotating element, provided with an annular magnetized structure having an angular variation of at least one physical parameter defining this annular magnetized structure, and by a first set of magnetic elements which consists of at least one functional magnetic element, this first set of magnetic elements not being integral in rotation with the rotating element and generally having a first magnetic interaction with the annular magnetized structure . In the examples considered in the detailed description of the invention, the rotating element is a magnetic escape wheel. However, the rotating element can be another component, in particular a pendulum. Next, in the examples considered, the first set of magnetic elements consists of at least one axis made of ferromagnetic material, in particular the axis of the lever associated with the escape wheel and/or the axis an intermediate mobile located close to this wheel and forming a gear train which transmits the torque from a barrel to the escapement wheel. It will be understood that the invention is not limited solely to axes made of ferromagnetic materials, but that it applies to any other magnetic element capable of being arranged at the immediate periphery of the rotating element in question, in particular to a magnetic escape wheel, and to present a significant magnetic interaction with its annular magnetized structure. By 'magnetic element' is meant a magnet, a ferromagnetic element or a combination of both.

On remarquera que dans la variante considérée aux Figures 2 et 3, essentiellement deux paramètres physiques de la structure aimantée annulaire présentent une variation angulaire, à savoir la largeur radiale de chaque couche aimantée structurée 12A, 12B et la distance moyenne de chaque couche aimantée structurée à l'axe de rotation 21 de la roue d'échappement 6A. Les variations angulaires de la largeur radiale et de la distance moyenne à l'axe de rotation des deux couches 12A, 12B, et donc de la structure aimantée annulaire, sont périodiques de sorte que la structure aimantée annulaire présente une période angulaire égale à 360°/N avec N étant un nombre entier supérieur à un (N > 1). En particulier, dans la variante considérée, la structure aimantée annulaire présente une période angulaire PA égale à 360°/N avec N = 6, soit une période angulaire de 60° ou π/3 [rad].Note that in the variant considered in Figure 2 and 3 , essentially two physical parameters of the annular magnetized structure exhibit an angular variation, namely the radial width of each structured magnetized layer 12A, 12B and the average distance of each structured magnetized layer from the axis of rotation 21 of the escape wheel 6A. The angular variations of the radial width and the average distance to the axis of rotation of the two layers 12A, 12B, and therefore of the annular magnetized structure, are periodic so that the annular magnetized structure has an angular period equal to 360°/N with N being an integer greater than one (N > 1). In particular, in the variant considered, the annular magnetized structure has an angular period PA equal to 360°/N with N=6, ie an angular period of 60° or π/3 [rad].

L'axe ferromagnétique 18 forme un corps de révolution de sorte que le volume de matière magnétique qu'il définit reste invariant quelle que soit la position angulaire de l'ancre 8. Ainsi, la première interaction magnétique entre l'axe magnétique 18 et la structure aimantée annulaire 12A-12B de la roue 6A engendre sur cette roue, du fait qu'elle comprend une structure aimantée annulaire périodique, un premier couple magnétique parasite qui ne dépend substantiellement que de la position angulaire de la roue 6A et qui varie périodiquement en fonction de la position angulaire de la roue 6A en présentant, dans la variante considérée, la même période angulaire PA, ici 60° ou π/3 [rad], que la structure aimantée annulaire 12A-12B. Une portion de la courbe 30 du premier couple magnétique parasite est donnée à la Figure 4.The ferromagnetic axis 18 forms a body of revolution so that the volume of magnetic material that it defines remains invariant whatever the angular position of the anchor 8. Thus, the first magnetic interaction between the magnetic axis 18 and the annular magnetic structure 12A-12B of wheel 6A generates on this wheel, because it comprises a periodic annular magnetic structure, a first parasitic magnetic torque which depends substantially only on the angular position of wheel 6A and which varies periodically in function of the angular position of the wheel 6A by having, in the variant considered, the same angular period PA, here 60° or π/3 [rad], as the annular magnetized structure 12A-12B. A portion of the curve 30 of the first parasitic magnetic torque is given at the Figure 4 .

La courbe 30, bien que ne définissant pas exactement une fonction F(θ) = A·sinθ, est du type sinusoïdal. Par 'courbe du type sinusoïdal', on comprend une courbe alternativement positive et négative, avec des valeurs extrêmes positives qui sont proches, normalement identiques mais pouvant différer un peu, et des valeurs extrêmes négatives qui sont proches, normalement identiques mais pouvant différer un peu. Ensuite, les valeurs extrêmes positives et les valeurs négatives sont, en valeurs absolues, proches les unes des autres, de préférence quasi identiques mais elles peuvent différer dans une certaine mesure, par exemple de 10% à 20%. On peut reconnaître un caractère périodique à une telle courbe avec comme période la distance angulaire entre deux valeurs extrêmes positives ou, de manière équivalente, deux valeurs extrêmes négatives. Finalement, les deux demi-périodes formant la période d'une telle courbe peuvent présenter des valeurs différentes, comme c'est le cas de la courbe 30 à la Figure 4, bien qu'il soit avantageux que les deux demi-périodes aient sensiblement une même valeur.The curve 30, although not defining exactly a function F(θ)=A·sinθ, is of the sinusoidal type. By 'curve of the sinusoidal type', we understand a curve that is alternately positive and negative, with positive extreme values which are close, normally identical but which may differ slightly, and negative extreme values which are close, normally identical but which may differ slightly . Then, the positive extreme values and the negative values are, in absolute values, close to each other, preferably almost identical but they can differ to a certain extent, for example by 10% to 20%. A periodic character can be recognized in such a curve with the period as the angular distance between two positive extreme values or, equivalently, two negative extreme values. Finally, the two half-periods forming the period of such a curve can have different values, as is the case of curve 30 at the Figure 4 , although it is advantageous for the two half-periods to have substantially the same value.

Dans un premier mode de réalisation de l'invention représenté à la Figure 5, le mouvement horloger est semblable à celui de l'art antérieur décrit précédemment pour ce qui concerne le ou les mécanisme(s) qui le compose(nt) et il comprend en outre un élément magnétique de compensation 32 qui est semblable dans sa forme à l'axe magnétique 18 ou, plus généralement, configuré pour engendrer sur la structure aimantée annulaire, en particulier sur la couche aimantée structurée 12A qui la forme, un couple ayant sensiblement une même intensité que celle du couple engendré par l'axe 18 (Figure 4). Cet élément magnétique de compensation 32 est formé ici par une goupille magnétique, agencée à la périphérie de la roue d'échappement magnétique et formée par un matériau ferromagnétique, et il est agencé de manière à présenter un décalage angulaire relativement à l'axe magnétique, rapporté à une période angulaire de la couche aimantée structurée périodique 12A et donc à la période angulaire de la structure aimantée annulaire périodique. Un deuxième couple magnétique parasite engendré par la goupille magnétique 32 définit une courbe semblable à la courbe 30 de la Figure 4, mais les premier et deuxième couples magnétiques parasites présentent entre eux un déphasage d'environ 180°, de préférence de 180°. Ce déphasage de 180° correspond à un décalage angulaire entre l'axe magnétique 18 et la goupille magnétique 32 qui est égal à [(2M-1)/N]·180°, avec N étant le nombre de périodes angulaire de la structure aimantée annulaire, soit N=6 dans l'exemple représenté, et M étant un nombre entier positif qui est inférieur ou égal à N.In a first embodiment of the invention shown in Figure 5 , the watch movement is similar to that of the prior art described above as regards the mechanism(s) which compose it and it further comprises a magnetic compensation element 32 which is similar in shape to the magnetic axis 18 or, more generally, configured to generate on the annular magnetized structure, in particular on the structured magnetic layer 12A which forms it, a torque having substantially the same intensity as that of the torque generated by the axis 18 ( Figure 4 ). This magnetic compensation element 32 is here formed by a magnetic pin, arranged at the periphery of the magnetic escape wheel and formed by a ferromagnetic material, and it is arranged so as to present an angular offset relative to the magnetic axis, related to an angular period of the periodic structured magnetized layer 12A and therefore to the angular period of the periodic annular magnetized structure. A second parasitic magnetic torque generated by the magnetic pin 32 defines a curve similar to the curve 30 of the Figure 4 , but the first and second parasitic magnetic couples have between them a phase shift of about 180°, preferably 180°. This 180° phase shift corresponds to an angular shift between the magnetic axis 18 and the magnetic pin 32 which is equal to [(2M-1)/N] 180°, with N being the number of angular periods of the magnetized structure ring, or N=6 in the example shown, and M being a positive integer which is less than or equal to N.

De préférence, la goupille magnétique 32 est agencée du côté diamétralement opposé à l'axe magnétique fonctionnel 18 pour compenser également en majeure partie la force d'attraction magnétique exercée par cet axe 18 sur la roue d'échappement 6A. Le couple résultant de l'addition des premier et deuxième couples magnétiques parasites est représenté à la Figure 6. On observe premièrement que la valeur absolue maximale V2 de ce couple résultant est inférieure à la valeur absolue maximale V1 du premier couple magnétique parasite représenté à la Figure 4. Dans l'exemple traité ici, la valeur absolue maximale V2 du couple résultant est légèrement inférieure à la moitié de la valeur absolue maximale V1 du premier couple magnétique parasite. Ensuite, on observe encore que la courbe 34 du couple résultant présente une période égale à la moitié de la période angulaire PA de la couche aimantée structurée 12A et donc de la structure aimantée annulaire. Ceci se comprend aisément du fait que l'agencement d'un axe de compensation déphasé de 180° engendre des configurations magnétiques qui sont identiques pour une rotation d'une demi-période PA/2 de la roue d'échappement 6A. Si on décompose la courbe 30 en série de Fourier, l'addition de deux telles courbes déphasées de 180° annule l'harmonique de rang n = 1 (aussi nommée la fondamentale), mais on double l'harmonique de rang n=2 qui présente une période égale à la moitié de la période de la fondamentale, cette dernière période étant égale à la période PA de la courbe 30 du premier couple magnétique parasite.Preferably, the magnetic pin 32 is arranged on the side diametrically opposite to the functional magnetic axis 18 to also compensate for the major part of the magnetic attraction force exerted by this axis 18 on escape wheel 6A. The torque resulting from the addition of the first and second parasitic magnetic torques is shown in Figure 6 . It is first observed that the maximum absolute value V2 of this resulting torque is lower than the maximum absolute value V1 of the first parasitic magnetic torque represented in Figure 4 . In the example treated here, the maximum absolute value V2 of the resulting torque is slightly less than half the maximum absolute value V1 of the first parasitic magnetic torque. Then, it is further observed that the curve 34 of the resulting torque has a period equal to half the angular period PA of the structured magnetized layer 12A and therefore of the annular magnetized structure. This is easily understood from the fact that the arrangement of a compensation axis out of phase by 180° generates magnetic configurations which are identical for a rotation of a half-period PA/2 of the escapement wheel 6A. If we decompose curve 30 into a Fourier series, the addition of two such curves out of phase by 180° cancels the harmonic of order n = 1 (also called the fundamental), but we double the harmonic of order n=2 which has a period equal to half the period of the fundamental, this last period being equal to the period PA of the curve 30 of the first parasitic magnetic couple.

De manière générale, le mouvement horloger comprend un deuxième ensemble d'éléments magnétiques qui est constitué d'un élément magnétique de compensation ou d'une pluralité d'éléments magnétiques de compensation n'appartenant à aucun mécanisme du mouvement horloger, ce deuxième ensemble d'éléments magnétiques étant non solidaire en rotation de l'élément tournant et ayant avec la structure aimantée annulaire globalement une deuxième interaction magnétique qui engendre sur l'élément tournant un deuxième couple magnétique parasite. Selon l'invention, le deuxième ensemble d'éléments magnétiques est agencé relativement au premier ensemble d'éléments magnétiques de manière que la valeur absolue maximale du couple résultant de l'addition des premier et deuxième couples magnétiques parasites est inférieure à la valeur absolue maximale du premier couple magnétique parasite.In general, the watch movement comprises a second set of magnetic elements which consists of a magnetic compensation element or a plurality of magnetic compensation elements not belonging to any mechanism of the watch movement, this second set of magnetic elements being non-rotatably connected to the rotating element and having with the globally annular magnetized structure a second magnetic interaction which generates on the rotating element a second parasitic magnetic torque. According to the invention, the second set of magnetic elements is arranged relative to the first set of magnetic elements so that the maximum absolute value of the torque resulting from the addition of the first and second parasitic magnetic torque is less than the maximum absolute value of the first parasitic magnetic torque.

Dans un mode de réalisation principal, auquel correspond le premier mode de réalisation décrit avant, le premier couple magnétique parasite en fonction de la position angulaire de l'élément tournant définit une première courbe du type sinusoïdal présentant une période angulaire égale à 360°/N, avec N étant un nombre entier supérieur à un (N > 1). Ensuite, le deuxième ensemble d'éléments magnétiques est agencé relativement au premier ensemble d'éléments magnétiques de manière que le deuxième couple magnétique parasite en fonction de la position angulaire dudit élément tournant définit une deuxième courbe du type sinusoïdal présentant également ladite période angulaire, et de manière que les premier et deuxième couples magnétiques parasites présentent entre eux un déphasage angulaire sensiblement égal à 180°.In a main embodiment, to which the first embodiment described before corresponds, the first parasitic magnetic torque as a function of the angular position of the rotating element defines a first curve of the sinusoidal type having an angular period equal to 360°/N , with N being an integer greater than one (N > 1). Then, the second set of magnetic elements is arranged relative to the first set of magnetic elements so that the second parasitic magnetic torque as a function of the angular position of said rotating element defines a second curve of the sinusoidal type also exhibiting said angular period, and so that the first and second parasitic magnetic couples have between them an angular phase shift substantially equal to 180°.

En référence aux Figures 7 et 8A à 8D, on décrira un deuxième mode de réalisation correspondant également au mode de réalisation principal susmentionné. Le mouvement horloger, représenté partiellement à la Figure 7, comprend une roue d'échappement magnétique 36 munie d'une structure aimantée annulaire formée, comme à la Figure 2, de deux couches aimantées structurées dont seule la couche inférieure 38A apparaît à la Figure 7. La roue d'échappement comprend un arbre 20 et un support amagnétique 40 portant la couche aimantée inférieure 38A. Cette roue d'échappement est agencée pour tourner autour d'un axe de rotation 21. Elle est associée à une ancre magnétique 8A, laquelle est formée par un axe magnétique 18A et deux bras amagnétiques, représentés en traits interrompus, qui portent à leurs extrémités libres respectivement deux palettes aimantées 9, 10. La couche aimantée structurée 38A et la structure aimantée annulaire formée par cette couche aimantée structurée diffèrent de la couche 12 A et de de la structure aimantée annulaire de la Figure 5 par une nouvelle configuration.With reference to Figure 7 and 8A at 8D, a second embodiment also corresponding to the aforementioned main embodiment will be described. The watch movement, shown partially on the Picture 7 , comprises a magnetic escape wheel 36 provided with an annular magnetized structure formed, as in Figure 2 , of two structured magnetic layers of which only the lower layer 38A appears at the Picture 7 . The escape wheel comprises a shaft 20 and a non-magnetic support 40 carrying the lower magnetic layer 38A. This escape wheel is arranged to rotate around an axis of rotation 21. It is associated with a magnetic anchor 8A, which is formed by a magnetic axis 18A and two non-magnetic arms, shown in broken lines, which carry at their ends free respectively two magnetic pallets 9, 10. The structured magnetic layer 38A and the annular magnetic structure formed by this structured magnetic layer differ from the layer 12 A and from the annular magnetic structure of the Figure 5 by a new configuration.

La structure aimantée annulaire formée de la couche aimantée structurée 38A ou de deux telles couches superposées, comme représenté à la Figure 2, définit des barrières magnétiques 17A pour l'ancre magnétique qui sont décalées angulairement de la période angulaire PA. On remarquera que seules des plages aimantées internes 17A ont été prévues dans la variante avantageuse considérée. La couche 38A présente une épaisseur constante et définit une piste aimantée 14A présentant une largeur radiale variable. De préférence, la structure aimantée annulaire est configurée de manière que son profil extérieur est sensiblement circulaire et continu, comme dans le cas de la variante avantageuse de la Figure 7. Par 'profil extérieur circulaire', dans le cas d'une structure ayant deux couches aimantées structurées, on comprend que chaque couche présente un profil extérieur qui est sensiblement circulaire. Dans ce cas, de préférence, les diamètres des deux couches aimantées structurées sont égaux, de sorte que les profils extérieurs de ces deux couches définissent une surface géométrique cylindrique. Un tel agencement de la structure aimantée annulaire permet, d'une part, de diminuer le premier couple magnétique parasite engendré par le ou les éléments magnétiques fonctionnels à la périphérie de la roue d'échappement 36 et, d'autre part, de diminuer le rapport entre la valeur absolue maximale du couple résultant (de l'addition du premier couple magnétique parasite et du couple magnétique parasite engendré par la goupille de compensation) et celle du premier couple magnétique parasite.The annular magnetized structure formed of the structured magnetized layer 38A or of two such superimposed layers, as shown in Figure 2 , defines magnetic barriers 17A for the magnetic anchor which are angularly offset by the angular period PA. It will be noted that only internal magnetic pads 17A have been provided in the advantageous variant considered. Layer 38A has a constant thickness and defines a magnetic track 14A with variable radial width. Preferably, the annular magnetized structure is configured so that its outer profile is substantially circular and continuous, as in the case of the advantageous variant of the Picture 7 . By 'circular external profile', in the case of a structure having two structured magnetic layers, it is understood that each layer has an external profile which is substantially circular. In this case, preferably, the diameters of the two structured magnetic layers are equal, so that the external profiles of these two layers define a cylindrical geometric surface. Such an arrangement of the annular magnetized structure makes it possible, on the one hand, to reduce the first parasitic magnetic torque generated by the functional magnetic element or elements at the periphery of the escape wheel 36 and, on the other hand, to reduce the ratio between the maximum absolute value of the resulting torque (from the addition of the first parasitic magnetic torque and the parasitic magnetic torque generated by the compensation pin) and that of the first parasitic magnetic torque.

Le deuxième mode de réalisation se distingue du premier encore par le fait que deux éléments magnétiques fonctionnels à la périphérie directe de la roue d'échappement sont considérés ici, à savoir l'axe magnétique 18A de l'ancre 8A et l'axe magnétique 42 d'un mobile intermédiaire formant un rouage entre la roue d'échappement et un barillet du mouvement horloger et engrenant avec le pignon de la roue d'échappement. Aux Figures 8A et 8B sont représentés les couples magnétiques individuels qui sont engendrés respectivement par les deux axes magnétiques 18A et 42 (au moins partiellement en matériau ferromagnétique). A la Figure 8C est représentée la courbe 44 du premier couple magnétique parasite engendré globalement par les éléments magnétiques fonctionnels, autres que les palettes magnétiques de l'ancre, qui se trouvent à proximité de la structure aimantée annulaire de la roue d'échappement 36. On constate que les couples magnétiques individuels présentent des courbes périodiques avec la période angulaire PA de la structure aimantée annulaire, cette période angulaire PA étant égale à 30°, soit 360°/N avec N=12 correspondant au nombre de périodes angulaires de la structure aimantée annulaire de la Figure 7. Ensuite, on constate que le couple magnétique individuel engendré par l'axe 42 est prédominant. Finalement, étant donné que les deux axes 18A et 42 présentent entre eux un relativement petit décalage angulaire par rapport à la période angulaire PA de la couche aimantée structurée 38A, le premier couple magnétique parasite (Figure 8C) présente une courbe 44 proche de celle de la Figure 8B, également avec une période PA, ces deux courbes présentant un certain déphasage entre elles.The second embodiment is distinguished from the first again by the fact that two functional magnetic elements at the direct periphery of the escape wheel are considered here, namely the magnetic axis 18A of the lever 8A and the magnetic axis 42 an intermediate mobile forming a cog between the escapement wheel and a barrel of the watch movement and meshing with the pinion of the escapement wheel. To the Figures 8A and 8B are represented the individual magnetic couples which are generated respectively by the two magnetic axes 18A and 42 (at least partly in ferromagnetic material). To the Figure 8C is represented the curve 44 of the first parasitic magnetic torque generated globally by the functional magnetic elements, other than the magnetic pallets of the anchor, which are close to the annular magnetized structure of the escape wheel 36. It is noted that the individual magnetic pairs exhibit periodic curves with the angular period PA of the annular magnetized structure, this angular period PA being equal to 30°, i.e. 360°/N with N=12 corresponding to the number of angular periods of the annular magnetized structure of the Picture 7 . Then, we see that the individual magnetic torque generated by the axis 42 is predominant. Finally, given that the two axes 18A and 42 have between them a relatively small angular offset with respect to the angular period PA of the structured magnetic layer 38A, the first parasitic magnetic torque ( Figure 8C ) has a curve 44 close to that of the Figure 8B , also with a period PA, these two curves having a certain phase difference between them.

De préférence, la goupille magnétique de compensation 32A est agencée de manière à ce que le couple magnétique individuel, constituant le deuxième couple magnétique parasite, qu'elle exerce sur la roue d'échappement présente un déphasage angulaire de 180° avec le premier couple magnétique parasite, et non avec le couple magnétique individuel de l'axe ferromagnétique 42 (Figure 8B), bien que ce dernier soit largement prédominant. Ensuite, étant donné que le premier ensemble d'éléments magnétiques, lequel est constitué d'éléments magnétiques fonctionnels, comporte deux éléments magnétiques fonctionnels, la goupille 32A est dimensionnée de manière à optimiser la compensation qu'elle produit, notamment son diamètre et/ou sa distance à l'axe de rotation 21 est/sont ajusté(s) pour que la valeur absolue maximale du deuxième couple magnétique parasite, engendré par la goupille de compensation 32A, compense au mieux le premier couple magnétique parasite et que le couple résultant, dont la courbe 46 est donnée à la Figure 8D, de l'addition des premier et deuxième couples magnétiques parasites ait ainsi la plus petite amplitude possible, c'est-à-dire la plus petite valeur absolue maximale possible.Preferably, the magnetic compensation pin 32A is arranged so that the individual magnetic torque, constituting the second parasitic magnetic torque, which it exerts on the escape wheel has an angular phase shift of 180° with the first magnetic torque. parasitic, and not with the individual magnetic torque of the ferromagnetic axis 42 ( Figure 8B ), although the latter is largely predominant. Then, given that the first set of magnetic elements, which consists of functional magnetic elements, comprises two functional magnetic elements, the pin 32A is dimensioned so as to optimize the compensation that it produces, in particular its diameter and/or its distance from the axis of rotation 21 is/are adjusted so that the maximum absolute value of the second parasitic magnetic torque, generated by the compensation pin 32A, best compensates for the first parasitic magnetic torque and that the resulting torque, whose curve 46 is given at the Figure 8D , from the addition of first and second parasitic magnetic couples thus have the smallest possible amplitude, that is to say the smallest possible maximum absolute value.

Grâce à la configuration de la couche aimantée structurée 38A, donc de la structure aimantée annulaire qu'elle forme, et à l'agencement de la goupille magnétique de compensation 32A, la valeur absolue maximale V4 du couple résultant de l'addition des premier et deuxième couples magnétiques parasites susmentionnés est inférieure à 30% de la valeur absolue maximale V3 du premier couple magnétique parasite. En effet, dans l'exemple décrit, on observe que le rapport entre la valeur absolue maximale V4 de la courbe 46 et la valeur absolue maximale V3 de la courbe 44 donne environ 1/5.Thanks to the configuration of the structured magnetic layer 38A, therefore of the annular magnetic structure that it forms, and to the arrangement of the magnetic compensation pin 32A, the maximum absolute value V4 of the torque resulting from the addition of the first and second aforementioned parasitic magnetic torques is less than 30% of the maximum absolute value V3 of the first parasitic magnetic torque. Indeed, in the example described, it is observed that the ratio between the maximum absolute value V4 of the curve 46 and the maximum absolute value V3 of the curve 44 gives approximately 1/5.

Une amélioration est proposée dans la variante décrite du deuxième mode de réalisation par le fait que la goupille de compensation 32A est agencée de manière que sa position relativement à l'axe de rotation 21 peut être ajustée pour régler le déphasage angulaire et/ou la valeur absolue maximale du deuxième couple magnétique parasite (courbe 44) et ainsi optimiser la courbe du couple résultant (courbe 46), en particulier la valeur absolue maximale V4 de ce couple résultant, c'est-à-dire diminuer cette valeur absolue maximale à la plus petite valeur possible. Plus précisément, la goupille 32A forme un excentrique que l'horloger pourra tourner à l'aide d'un outil pour ajuster sa distance à l'axe de rotation et donc à la structure aimantée annulaire. Si on désire ne pas varier la position angulaire de la goupille de compensation, on peut dans une variante agencer la goupille de compensation dans une sorte de glissière radiale. L'homme du métier saura prévoir les moyens nécessaires à l'ajustement de la position radiale et/ou angulaire de cette goupille de compensation.An improvement is proposed in the described variant of the second embodiment in that the compensation pin 32A is arranged so that its position relative to the axis of rotation 21 can be adjusted to adjust the angular phase shift and/or the value maximum absolute value of the second parasitic magnetic torque (curve 44) and thus optimize the curve of the resulting torque (curve 46), in particular the maximum absolute value V4 of this resulting torque, that is to say reduce this maximum absolute value at the smallest possible value. More specifically, the pin 32A forms an eccentric that the watchmaker can turn using a tool to adjust its distance from the axis of rotation and therefore from the annular magnetic structure. If it is desired not to vary the angular position of the compensation pin, it is possible in a variant to arrange the compensation pin in a kind of radial slide. A person skilled in the art will know how to provide the means necessary for adjusting the radial and/or angular position of this compensation pin.

En référence aux Figures 9 et 10, on décrira ci-après un troisième mode réalisation de l'invention. Ce troisième mode de réalisation se distingue du premier mode de réalisation seulement en ce que l'unique goupille de compensation du deuxième mode de réalisation est remplacée par deux goupilles de compensation 50, 52 semblables à l'axe magnétique 18 qui constitue ici l'ensemble des éléments magnétiques fonctionnels considérés (cet axe magnétique considéré peut être soit l'axe de l'ancre, soit l'axe d'un mobile intermédiaire engrenant avec la roue d'échappement 6A). Les deux goupilles de compensation sont agencées de manière que les deux couples magnétiques individuels qu'elles exercent respectivement sur la roue d'échappement soient déphasées respectivement de 120° et 240° (équivalent à -120°) relativement au premier couple magnétique parasite engendré par l'axe magnétique 18. En d'autres termes, dans le présent cas, les deux éléments magnétiques de compensation 50, 52 présentent l'un relativement à l'autre un décalage angulaire dont le reste de la division entière par la période angulaire PA est égal à 360°/(3·N) où N est le nombre de période angulaire de la structure aimantée annulaire, soit N=6 dans l'exemple considéré. Ensuite, comme ici seul un élément magnétique fonctionnel 18 est considéré, les deux éléments magnétiques de compensation sont agencés de manière à présenter relativement à l'élément magnétique fonctionnel deux décalages angulaires dont les deux restes de la division entière de chacun d'eux par la période angulaire PA sont respectivement égaux à 360°/3·N et 720°/3·N, soit 20° et 40° (à noter que PA = 60°). De plus, les deux goupilles magnétiques de compensation 50 et 52 sont agencées de manière à répartir le plus régulièrement possible ces deux goupilles de compensation et l'axe magnétique 18 autour de l'axe de rotation pour minimiser les frottements dans les paliers de la roue d'échappement dus à l'attraction magnétique exercée par chacun d'eux sur la structure aimantée annulaire de cette roue.With reference to Figures 9 and 10 , a third embodiment of the invention will be described below. This third embodiment differs from the first embodiment only in that the single pin of compensation of the second embodiment is replaced by two compensation pins 50, 52 similar to the magnetic axis 18 which here constitutes all the functional magnetic elements considered (this magnetic axis considered can be either the axis of the anchor, or the axis of an intermediate mobile meshing with the escapement wheel 6A). The two compensation pins are arranged so that the two individual magnetic torques which they respectively exert on the escape wheel are out of phase respectively by 120° and 240° (equivalent to -120°) relative to the first parasitic magnetic torque generated by the magnetic axis 18. In other words, in the present case, the two magnetic compensation elements 50, 52 have relative to each other an angular offset whose remainder of the integer division by the angular period PA is equal to 360°/(3·N) where N is the number of angular periods of the annular magnetized structure, ie N=6 in the example considered. Then, as here only a functional magnetic element 18 is considered, the two compensating magnetic elements are arranged so as to present, relative to the functional magnetic element, two angular offsets including the two remainders of the integer division of each of them by the angular period PA are respectively equal to 360°/3·N and 720°/3·N, i.e. 20° and 40° (note that PA = 60°). In addition, the two magnetic compensation pins 50 and 52 are arranged so as to distribute these two compensation pins and the magnetic axis 18 as evenly as possible around the axis of rotation to minimize friction in the bearings of the wheel. exhaust due to the magnetic attraction exerted by each of them on the annular magnetized structure of this wheel.

A la Figure 10 est donné la courbe 54 du couple résultant exercé globalement par les deux goupilles de compensation et l'élément magnétique fonctionnel de la Figure 9. Premièrement, on observe que la valeur absolue maximale V5 de la courbe 54 est relativement faible. Elle est inférieure à 20% de la valeur absolue maximale V1 du premier couple magnétique parasite (voir Figure 4). Ensuite la courbe 54 est périodique et présente une période angulaire égale au tiers de la période angulaire PA de la structure aimantée annulaire, soit une période angulaire égale à PA/3. On réalise ainsi que l'agencement de deux goupilles de compensation, avec les décalages angulaires susmentionnés relativement à l'axe magnétique 18, engendre un deuxième couple magnétique parasite qui permet de compenser les deux premières harmoniques (n=1, 2) de la décomposition en série de Fourier du premier couple magnétique parasite engendré par l'axe magnétique fonctionnel. Par contre, la troisième harmonique est renforcée, raison pour laquelle on obtient une courbe périodique 54 avec une période égale à PA/3. Comme la troisième harmonique (n = 3) présente une relativement faible amplitude, la courbe du couple résultant a une valeur absolue maximale V5 qui est bien inférieure aux valeurs correspondantes V2 et V4 des deux modes de réalisation précédents. En prenant la roue d'échappement 36 du deuxième mode de réalisation, on peut encore diminuer cette valeur absolue maximale, comme ceci apparaît à la Figure 12.To the Picture 10 is given the curve 54 of the resultant torque exerted overall by the two compensating pins and the functional magnetic element of the Figure 9 . First, it is observed that the maximum absolute value V5 of curve 54 is relatively low. It is less than 20% of the maximum absolute value V1 of the first parasitic magnetic torque (see Figure 4 ). Then the curve 54 is periodic and has a period angular period equal to one third of the angular period PA of the annular magnetized structure, ie an angular period equal to PA/3. It is thus realized that the arrangement of two compensation pins, with the aforementioned angular offsets relative to the magnetic axis 18, generates a second parasitic magnetic torque which makes it possible to compensate for the two first harmonics (n=1, 2) of the decomposition in Fourier series of the first parasitic magnetic torque generated by the functional magnetic axis. On the other hand, the third harmonic is reinforced, which is why a periodic curve 54 is obtained with a period equal to PA/3. As the third harmonic (n=3) has a relatively low amplitude, the resulting torque curve has a maximum absolute value V5 which is much lower than the corresponding values V2 and V4 of the two preceding embodiments. By taking the escapement wheel 36 of the second embodiment, it is possible to further reduce this maximum absolute value, as appears at Picture 12 .

En référence aux Figures 11 et 12, on décrira un quatrième mode de réalisation. Ce quatrième mode de réalisation se distingue du deuxième mode de réalisation en ce que l'unique goupille magnétique de compensation du deuxième mode de réalisation est remplacé ici par deux goupilles magnétiques de compensation 32B et 32C qui sont agencées de manière équivalente au troisième mode de réalisation. On est donc dans un cas où le premier ensemble d'éléments magnétiques comprend une pluralité d'éléments magnétiques fonctionnels, soit deux axes magnétiques dans la variante décrite, et le deuxième ensemble d'éléments magnétiques comprend une pluralité d'éléments magnétiques de compensation, soit deux goupilles dans cette variante. Les deux goupilles de compensation sont agencées de manière que les deux couples magnétiques individuels qu'elles exercent respectivement sur la roue d'échappement soient déphasées respectivement de 120° et 240° relativement au premier couple magnétique parasite engendré globalement par les deux axes magnétiques 18A et 42. En d'autres termes, les deux éléments magnétiques de compensation présentent ici l'un relativement à l'autre un décalage angulaire dont le reste de la division entière par la période angulaire PA est égal à 360°/(3·N) où N est le nombre de période angulaire de la structure aimantée annulaire, soit N=12 dans l'exemple considéré. Ce reste est donc égal à 10° de sorte que l'angle DA5 entre les deux goupilles 32B et 32C est égal à 40° dans l'exemple représenté à la Figure 11, soit à une période angulaire (égale à 30°) à laquelle on ajoute le reste de 10°. On notera que du fait que l'on tient compte de l'effet de l'axe 18A de l'ancre, l'angle DA6 entre l'axe 42 et la goupille 32B ne correspond pas à un nombre entier de période PA auquel on ajoute ou retranche 10°, bien que cet angle DA6 s'en approche du fait que l'axe 42 est prédominant dans le premier couple magnétique parasite engendré par les deux éléments magnétiques fonctionnels sur la roue d'échappement.With reference to Figures 11 and 12 , a fourth embodiment will be described. This fourth embodiment differs from the second embodiment in that the single magnetic compensation pin of the second embodiment is replaced here by two magnetic compensation pins 32B and 32C which are arranged in an equivalent manner to the third embodiment . We are therefore in a case where the first set of magnetic elements comprises a plurality of functional magnetic elements, i.e. two magnetic axes in the variant described, and the second set of magnetic elements comprises a plurality of magnetic compensation elements, i.e. two pins in this variant. The two compensation pins are arranged so that the two individual magnetic torques which they respectively exert on the escape wheel are out of phase respectively by 120° and 240° relative to the first parasitic magnetic torque generated globally by the two magnetic axes 18A and 42. In other words, the two magnetic compensating elements present here relative to each other an angular offset whose remainder of the integer division by the angular period PA is equal to 360°/(3·N) where N is the number of angular periods of the annular magnetized structure, or N=12 in the example considered. This remainder is therefore equal to 10° so that the angle DA5 between the two pins 32B and 32C is equal to 40° in the example shown in Picture 11 , or at an angular period (equal to 30°) to which the remainder of 10° is added. It will be noted that since the effect of the axis 18A of the anchor is taken into account, the angle DA6 between the axis 42 and the pin 32B does not correspond to an integer period PA to which one adds or subtracts 10°, although this angle DA6 approaches it due to the fact that the axis 42 is predominant in the first parasitic magnetic torque generated by the two functional magnetic elements on the escape wheel.

La courbe 60 du couple résultant de l'addition du premier couple magnétique parasite, engendré globalement par le premier ensemble d'éléments magnétiques, avec le deuxième couple magnétique parasite, engendré globalement par le deuxième ensemble d'éléments magnétiques, est représentée à la Figure 12. En d'autres termes, le couple résultant est le résultat de l'addition de tous les couples magnétiques parasites individuels qui sont considérés. La structure aimantée annulaire du quatrième mode de réalisation est configurée et les deux éléments magnétiques de compensation sont agencés de manière que la valeur absolue maximale V6 du couple résultant est inférieure à 15%, voire à 12% de la valeur absolue maximale V3 (voir Figure 8C) du premier couple magnétique parasite. L'homme du métier peut optimiser le système en configurant spécifiquement les deux goupilles de compensation qui sont de préférence identiques, notamment leurs diamètres respectifs et leurs distances respectives à l'axe de rotation. On remarquera en particulier que les deux goupilles 32B et 32C ne sont pas ici respectivement identiques, dans leurs configurations respectives et leur agencement relatif en périphérie de la roue d'échappement 36, aux deux axes 18A et 42. Si tel était le cas, on serait de fait dans une variante du deuxième mode de réalisation dans laquelle les deux goupilles formeraient ensemble un groupe d'éléments magnétiques à considérer comme un tout indissociable et non individuellement, c'est-à-dire non comme deux éléments de compensation distincts dont les couples magnétiques parasites individuels pourraient présenter des déphasages différents relativement au premier couple magnétique parasite et sélectionnés comme exposé précédemment. En effet, dans le cadre du quatrième mode de réalisation, pour obtenir l'effet recherché, à savoir compenser au mieux les deux premières harmoniques de la courbe du premier couple magnétique parasite (voir Figure 8C) et minimiser ainsi l'amplitude du couple perturbateur sur la roue d'échappement, il faut de préférence que les deux goupilles de compensation soient dans leurs configurations respectives, notamment leurs dimensions et le matériau qui les constitue, et leurs agencements respectifs relativement à l'axe de rotation, notamment la distance à cet axe de rotation, sensiblement identiques à la goupille de compensation 32A du deuxième mode de réalisation qui optimise le résultat de ce deuxième mode de réalisation ou qu'elles présentent un même effet que cette goupille de compensation 32A sur la structure aimantée annulaire.The curve 60 of the torque resulting from the addition of the first parasitic magnetic torque, globally generated by the first set of magnetic elements, with the second parasitic magnetic torque, globally generated by the second set of magnetic elements, is shown in Picture 12 . In other words, the resulting torque is the result of the addition of all the individual parasitic magnetic torques that are considered. The annular magnetized structure of the fourth embodiment is configured and the two magnetic compensation elements are arranged so that the maximum absolute value V6 of the resulting torque is less than 15%, or even 12% of the maximum absolute value V3 (see Figure 8C ) of the first parasitic magnetic couple. A person skilled in the art can optimize the system by specifically configuring the two compensation pins which are preferably identical, in particular their respective diameters and their respective distances from the axis of rotation. It will be noted in particular that the two pins 32B and 32C are not here respectively identical, in their respective configurations and their relative arrangement on the periphery of the escapement wheel 36, to the two axes 18A and 42. If such were the case, one would in fact be in a variant of the second embodiment in which the two pins would together form a group of magnetic elements to be considered as an inseparable whole and not individually, that is to say not as two distinct compensation elements whose individual parasitic magnetic couples could present different phase shifts relative to the first magnetic couple parasite and selected as described above. Indeed, in the context of the fourth embodiment, to obtain the desired effect, namely to best compensate the first two harmonics of the curve of the first parasitic magnetic torque (see Figure 8C ) and thus minimize the amplitude of the disturbing torque on the escape wheel, it is preferably necessary for the two compensation pins to be in their respective configurations, in particular their dimensions and the material from which they are made, and their respective arrangements relative to the axis of rotation, in particular the distance to this axis of rotation, substantially identical to the compensation pin 32A of the second embodiment which optimizes the result of this second embodiment or that they have the same effect as this compensation pin 32A on the annular magnetic structure.

De manière générale, dans le cadre des troisième et quatrième modes de réalisation, le deuxième ensemble d'éléments magnétiques est constitué de K éléments magnétiques de compensation ou K groupes d'éléments magnétiques de compensation présentant sensiblement une même configuration, K étant un nombre entier supérieur à un (K>1). Les K éléments magnétiques de compensation ou groupes d'éléments magnétiques de compensation sont agencés de manière que K couples magnétiques parasites, engendrés sur l'élément tournant muni de la structure aimantée annulaire respectivement par ces K éléments magnétiques de compensation ou groupes d'éléments magnétiques de compensation, présentent relativement au premier couple magnétique parasite, engendré par des éléments magnétiques fonctionnels, respectivement K déphasages angulaires qui sont respectivement égaux à sensiblement J·360°/(K+1) avec J étant un nombre entier allant de un jusqu'à K, soit J = 1, ..., K.Generally, in the context of the third and fourth embodiments, the second set of magnetic elements consists of K magnetic compensation elements or K groups of magnetic compensation elements having substantially the same configuration, K being an integer greater than one (K>1). The K magnetic compensation elements or groups of magnetic compensation elements are arranged so that K parasitic magnetic couples, generated on the rotating element provided with the annular magnetized structure respectively by these K magnetic compensation elements or groups of magnetic elements compensation, have relative to the first parasitic magnetic torque, generated by functional magnetic elements, respectively K phase shifts angles which are respectively equal to substantially J 360°/(K+1) with J being an integer ranging from one to K, i.e. J = 1, ..., K.

Dans un mode préféré, le nombre entier K est égal à deux (K = 2) et les deux éléments magnétiques de compensation ou groupes d'éléments magnétiques de compensation sont semblables entre eux, un des deux éléments magnétiques de compensation ou groupes d'éléments magnétiques de compensation présentant relativement à l'autre un décalage angulaire dont le reste de la division entière par ladite période angulaire est égal à 360°/(3·N), N étant le nombre de périodes dans une plage de 360° de la courbe du premier couple magnétique parasite.In a preferred mode, the integer K is equal to two (K=2) and the two magnetic compensation elements or groups of magnetic compensation elements are similar to each other, one of the two magnetic compensation elements or groups of elements compensation magnets having relative to each other an angular offset whose remainder of the integer division by said angular period is equal to 360°/(3·N), N being the number of periods in a range of 360° of the curve of the first parasitic magnetic couple.

Dans d'autres modes de réalisation, dans lesquels le nombre entier K est supérieur à deux (K>2), les K éléments magnétiques de compensation ou groupes d'éléments magnétiques de compensation sont semblables entre eux et un certain élément magnétique de compensation ou groupe d'éléments magnétiques de compensation, parmi lesdits K éléments magnétiques de compensation ou groupes d'éléments magnétiques de compensation, présente relativement aux autres éléments magnétiques de compensation ou groupes d'éléments magnétiques de compensation K-1 décalages angulaires dont les K-1 restes de la division entière de chacun d'eux par la période angulaire sont respectivement égaux à J·360°/[(K+1)·N] avec J étant un nombre entier allant de un à K-1, soit J = 1, ..., K-1.In other embodiments, in which the integer K is greater than two (K>2), the K compensating magnetic elements or groups of compensating magnetic elements are similar to each other and a certain compensating magnetic element or group of magnetic compensation elements, among said K magnetic compensation elements or groups of magnetic compensation elements, has relative to the other magnetic compensation elements or groups of magnetic compensation elements K-1 angular offsets whose K-1 remainders of the integer division of each of them by the angular period are respectively equal to J 360°/[(K+1) N] with J being an integer ranging from one to K-1, i.e. J = 1 , ..., K-1.

Finalement, dans un mode de réalisation particulier dans lequel le premier ensemble d'éléments magnétiques considérés est constitué d'un unique élément magnétique fonctionnel, le nombre entier positif N est ainsi égal à un nombre de périodes angulaires que présente la structure aimantée annulaire et les K éléments magnétiques de compensation sont agencés de manière à présenter relativement à l'unique élément magnétique fonctionnel K décalages angulaires dont les K restes de la division entière de chacun d'eux par la période angulaire sont respectivement égaux à J·360°/[(K+1)·N] avec J étant un nombre entier allant de un à K, soit J = 1, ..., K.Finally, in a particular embodiment in which the first set of magnetic elements considered consists of a single functional magnetic element, the positive integer N is thus equal to a number of angular periods that the annular magnetized structure and the K compensating magnetic elements are arranged in such a way as to present, relative to the single functional magnetic element, K angular offsets whose K remainders of the integer division of each of them by the angular period are respectively equal to J 360°/[( K+1) N] with J being an integer ranging from one to K, i.e. J = 1, ..., K.

Claims (14)

  1. Timepiece movement comprising a mechanism consisting of a rotating element (6A; 36), provided with an annular magnetized structure (12A-12B; 38A) exhibiting an angular variation of at least one physical parameter defining said annular magnetized structure, and of a first set of magnetic elements which is formed of one functional magnetic element (18) or of a plurality of functional magnetic elements (18A, 42), this first set of magnetic elements not being integral in rotation with said rotating element and having overall with the annular magnetized structure a first magnetic interaction which generates on said rotating element a first magnetic disturbance torque (30; 44); characterized in that the timepiece movement further comprises a second set of magnetic elements which consists of a magnetic compensation element (32; 32A) or of a plurality of magnetic compensation elements (32B,32C; 50,52) not forming part of any timepiece movement mechanism, this second set of magnetic elements not being integral in rotation with said rotating element and having overall with the annular magnetized structure a second magnetic interaction which generates on said rotating element a second magnetic disturbance torque; and in that the second set of magnetic elements is arranged relative to the first set of magnetic elements such that the maximum absolute torque value (34; 46) resulting from the addition of the first and second magnetic disturbance torques is lower than the maximum absolute value of the first magnetic disturbance torque.
  2. Timepiece movement according to claim 1, characterized in that the first magnetic disturbance torque (30; 44) as a function of the angular position of said rotating element (6; 6A, 36) defines a first sinusoidal type curve having an angular period (PA) equal to 360°/N, with N being an integer number greater than one (N > 1); and in that the second set of magnetic elements is arranged relative to the first set of magnetic elements such that the second magnetic disturbance torque as a function of the angular position of said rotating element defines a second sinusoidal type curve also having said angular period, and such that the first and second magnetic disturbance torques exhibit therebetween an angular phase shift substantially equal to 180°.
  3. Timepiece movement according to claim 2, characterized in that the second set of magnetic elements consists only of said magnetic compensation element (32A); and in that the annular magnetized structure (38A) is configured and said magnetic compensation element is arranged such that the maximum absolute value of said resultant torque is less than 30% of the maximum absolute value of the first magnetic disturbance torque.
  4. Timepiece movement according to claim 2, characterized in that the second set of magnetic elements consists of K magnetic compensation elements (32B, 32C; 50, 52) or K groups of magnetic compensation elements substantially having the same configuration, K being an integer number greater than one (K > 1); and in that said K magnetic compensation elements or groups of magnetic compensation elements are arranged such that K individual magnetic disturbance torques generated on the rotating element respectively by said K magnetic compensation elements or groups of magnetic compensation elements, exhibit relative to said first magnetic disturbance torque respectively K angular phase shifts which are respectively equal to substantially J·360°/(K+1) with J being an integer number ranging from one to K, i.e. J = 1, ..., K.
  5. Timepiece movement according to claim 4, wherein the integer number K is equal to two (K = 2), characterized in that the two magnetic compensation elements (32B, 32C; 50, 52) or groups of magnetic compensation elements are similar to each other, one of the two magnetic compensation elements or groups of magnetic compensation elements exhibiting relative to the other an angular offset whereby the remainder of the integer division by said angular period is equal to 360°/(3·N).
  6. Timepiece movement according to claim 5, characterized in that the annular magnetized structure (38A) is configured and the two magnetic compensation elements are arranged such that the maximum absolute value of said resultant torque is less than 15% of the maximum absolute value of the first magnetic disturbance torque.
  7. Timepiece movement according to claim 4, wherein the integer number K is greater than two (K > 2), characterized in that said K magnetic compensation elements or groups of magnetic compensation elements are similar to each other, a certain magnetic compensation element or group of magnetic compensation elements among said K magnetic compensation elements or groups of magnetic compensation elements exhibiting relative to the other magnetic compensation elements or groups of magnetic compensation elements K-1 angular offsets whereby the K-1 remainders of the integer division of each by the angular period are respectively equal to J·360°l[(K+1)·N] where J is an integer number ranging from one K-1, i.e. J = 1, ..., K-1.
  8. Timepiece movement according to any of claims 4 to 7, wherein the first set of magnetic elements considered consists only of said functional magnetic element (18), the positive integer number N thus being equal to a number of angular periods exhibited by the annular magnetized structure; characterized in that said K magnetic compensation elements (50, 52) are arranged to exhibit relative to said functional magnetic element K angular offsets whereby the K remainders of the integer division of each by said angular period are respectively equal to J·360°/[(K+1)·N] where J is an integer number ranging from one to K, namely J = 1, ..., K.
  9. Timepiece movement according to any of the preceding claims, characterized in that said rotating element is a magnetic escape wheel (6A, 36) forming a magnetic escapement.
  10. Timepiece movement according to claim 9, characterized in that said functional magnetic element is a shaft (18; 18A) of a magnetic pallet fork (8; 8A) also forming said magnetic escapement, said shaft being formed by a ferromagnetic material; and in that the annular magnetized structure defines magnetic barriers (16, 17; 17A) for the magnetic pallet fork which are angularly offset by said angular period (PA).
  11. Timepiece movement according to claim 9 or 10, characterized in that said magnetic compensation element is a pin arranged at the periphery of the magnetic escape wheel and formed by a ferromagnetic material.
  12. Timepiece movement according to any of claims 9 to 11, characterized in that the annular magnetized structure has a constant thickness, said angularly variable physical parameter being the radial width of said annular magnetized structure.
  13. Timepiece movement according to any of claims 9 to 12, characterized in that the annular magnetized structure (38A) is configured such that the external profile thereof is circular and continuous.
  14. Timepiece movement according to any of the preceding claims, characterized in that said magnetic compensation element (32A) is arranged such that the position thereof relative to said rotating element can be adjusted to regulate said angular phase shift and to optimise said maximum intensity of said resultant torque.
EP19187333.0A 2019-07-19 2019-07-19 Clock movement comprising a rotary element provided with a magnetic structure having a periodic configuration Active EP3767397B1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
EP19187333.0A EP3767397B1 (en) 2019-07-19 2019-07-19 Clock movement comprising a rotary element provided with a magnetic structure having a periodic configuration
US16/891,168 US11822294B2 (en) 2019-07-19 2020-06-03 Timepiece movement comprising a rotating element provided with a magnetized structure having a periodic configuration
JP2020108538A JP6982139B2 (en) 2019-07-19 2020-06-24 Timekeeper movement with rotating elements provided by a magnetized structure with a periodic configuration
CN202010691556.5A CN112241120B (en) 2019-07-19 2020-07-17 Timepiece movement including a rotating element provided with a periodically shaped magnetizing structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP19187333.0A EP3767397B1 (en) 2019-07-19 2019-07-19 Clock movement comprising a rotary element provided with a magnetic structure having a periodic configuration

Publications (2)

Publication Number Publication Date
EP3767397A1 EP3767397A1 (en) 2021-01-20
EP3767397B1 true EP3767397B1 (en) 2022-04-20

Family

ID=67438194

Family Applications (1)

Application Number Title Priority Date Filing Date
EP19187333.0A Active EP3767397B1 (en) 2019-07-19 2019-07-19 Clock movement comprising a rotary element provided with a magnetic structure having a periodic configuration

Country Status (4)

Country Link
US (1) US11822294B2 (en)
EP (1) EP3767397B1 (en)
JP (1) JP6982139B2 (en)
CN (1) CN112241120B (en)

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1825382A (en) * 1927-01-25 1931-09-29 Arthur K Kempton Magnetic clock escapement
DE602005023633D1 (en) * 2004-10-26 2010-10-28 Tag Heuer Sa WATCH CLOCK REGULATOR AND MECHANICAL MOVEMENT WITH SUCH A REGULATOR
EP2466401B1 (en) 2010-12-15 2013-08-14 Asgalium Unitec SA Magnetic resonator for mechanical timepiece
CH707471B1 (en) * 2013-08-05 2014-07-31 Rd Engineering Rudolf Dinger controller system for mechanical watch.
CH710025B1 (en) 2013-12-23 2018-06-29 Eta Sa Mft Horlogere Suisse Mechanical watch movement with magnetic escapement.
US9465366B2 (en) 2013-12-23 2016-10-11 The Swatch Group Research And Development Ltd Angular speed regulating device for a wheel set in a timepiece movement including a magnetic escapement mechanism
EP2887157B1 (en) 2013-12-23 2018-02-07 The Swatch Group Research and Development Ltd. Optimised escapement
EP2998801A1 (en) * 2014-09-19 2016-03-23 The Swatch Group Research and Development Ltd. Magnetic clock escapement and device for controlling the operation of a clock movement
EP3087435B1 (en) 2013-12-23 2020-04-22 The Swatch Group Research and Development Ltd. Device intended to control the angular speed of a train in a timepiece movement and including a magnetic escapement
EP2911015B1 (en) 2013-12-23 2017-08-23 The Swatch Group Research and Development Ltd. Natural escapement
JP6652956B2 (en) * 2014-03-21 2020-02-26 ウブロ ソシエテ アノニム, ジュネーブHublot S.A., Geneve Vibrating member, assembly, clock oscillator, clock speed adjuster, clock movement, clock, and operation method of clock mechanism
EP3128379B1 (en) * 2015-08-04 2019-10-02 The Swatch Group Research and Development Ltd. Escapement with escape wheel with field rramps and a non-return device
EP3185083B1 (en) * 2015-12-23 2018-11-14 Montres Breguet S.A. Mechanical timepiece mechanism with anchor escapement
EP3208667A1 (en) 2016-02-18 2017-08-23 The Swatch Group Research and Development Ltd Magnetic escapement mobile for timepiece
CH712154B1 (en) 2016-02-18 2019-12-13 Swatch Group Res & Dev Ltd Watchmaking magnetic escapement.
EP3217227B1 (en) * 2016-03-11 2019-02-27 The Swatch Group Research and Development Ltd. Timepiece regulator mechanism with optimised magnetic escapement
EP3316046B1 (en) 2016-10-25 2019-07-31 The Swatch Group Research and Development Ltd Optimised clock movement
CH713070B1 (en) 2016-10-25 2022-02-28 Swatch Group Res & Dev Ltd Mechanical watch movement comprising a blade resonator mechanism and a magnetic escapement mechanism.
EP3339982B1 (en) * 2016-12-23 2021-08-25 The Swatch Group Research and Development Ltd Regulation by mechanical breaking of a horological mechanical oscillator
EP3489767A1 (en) * 2017-11-27 2019-05-29 Montres Breguet S.A. Magnetic device for centring an arbour in a clock movement

Also Published As

Publication number Publication date
CN112241120B (en) 2021-12-24
JP6982139B2 (en) 2021-12-17
US11822294B2 (en) 2023-11-21
US20210018876A1 (en) 2021-01-21
CN112241120A (en) 2021-01-19
JP2021018237A (en) 2021-02-15
EP3767397A1 (en) 2021-01-20

Similar Documents

Publication Publication Date Title
EP2891930B1 (en) Device for regulating the angular speed of a mobile in a clock movement comprising a magnetic escapement
EP3457221B1 (en) Timepiece oscillator with flexible pivot
EP3191899B1 (en) Magnetic clock escapement and device for controlling the operation of a clock movement
WO2005111742A1 (en) Watch comprising at least two tourbillons
EP0811269A1 (en) Two-phase motor, particularly a time piece motor or a motor for driving the hand of a display
EP2823364B1 (en) Barrel
EP3208667A1 (en) Magnetic escapement mobile for timepiece
EP2255257A1 (en) Pivot member
EP4009115A1 (en) Hairspring for timepiece resonator mechanism provided with a means for adjusting rigidity
CH715049A2 (en) Timepiece including a tourbillon.
EP2172815A1 (en) Timepiece gear-train
EP0587031B1 (en) Timepiece with driving means consisting of a piezoelectric motor
EP3792700B1 (en) Timepiece oscillator with flexible pivot
EP3767397B1 (en) Clock movement comprising a rotary element provided with a magnetic structure having a periodic configuration
CH711020B1 (en) Bearing and method of assembling such a bearing.
CA2194792A1 (en) Electromagnetic claw-pole rotor
EP3191898B1 (en) Regulator device for the operation of a mechanical timepiece movement
CH690632A5 (en) electromagnetic motor with two coaxial rotors.
EP2407832A1 (en) Timepiece movement
EP3955063A1 (en) Mechanism provided with a magnetic gear
CH716414A2 (en) Watch movement comprising a rotating element provided with a magnetic structure having a periodic configuration.
CH699679A2 (en) Gear train e.g. finishing gear train, for watch, has toothed elements provided with gear teeth, where each tooth is composed of N coaxial toothed rings that are angularly offset with respect to each other by fraction of pitch of teeth
CH712154B1 (en) Watchmaking magnetic escapement.
CH710817B1 (en) Watch movement with resonant regulator with magnetic interaction.
EP4020100A1 (en) Timepiece including a rotating bezel

Legal Events

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

Free format text: ORIGINAL CODE: 0009012

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

Free format text: STATUS: THE APPLICATION HAS BEEN PUBLISHED

AK Designated contracting states

Kind code of ref document: A1

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

AX Request for extension of the european patent

Extension state: BA ME

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

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20210720

RBV Designated contracting states (corrected)

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

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

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

Free format text: STATUS: GRANT OF PATENT IS INTENDED

RIC1 Information provided on ipc code assigned before grant

Ipc: G04C 3/10 20060101ALI20211125BHEP

Ipc: G04C 5/00 20060101AFI20211125BHEP

INTG Intention to grant announced

Effective date: 20211215

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

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

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

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

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: FRENCH

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602019013825

Country of ref document: DE

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 1485644

Country of ref document: AT

Kind code of ref document: T

Effective date: 20220515

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG9D

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20220420

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 1485644

Country of ref document: AT

Kind code of ref document: T

Effective date: 20220420

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

Ref country code: NL

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

Effective date: 20220420

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

Ref country code: SE

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

Effective date: 20220420

Ref country code: PT

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

Effective date: 20220822

Ref country code: NO

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

Effective date: 20220720

Ref country code: LT

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

Effective date: 20220420

Ref country code: HR

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

Effective date: 20220420

Ref country code: GR

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

Effective date: 20220721

Ref country code: FI

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

Effective date: 20220420

Ref country code: ES

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

Effective date: 20220420

Ref country code: BG

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

Effective date: 20220720

Ref country code: AT

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

Effective date: 20220420

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

Ref country code: RS

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

Effective date: 20220420

Ref country code: PL

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

Effective date: 20220420

Ref country code: LV

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

Effective date: 20220420

Ref country code: IS

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

Effective date: 20220820

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602019013825

Country of ref document: DE

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

Ref country code: SM

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

Effective date: 20220420

Ref country code: SK

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

Effective date: 20220420

Ref country code: RO

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

Effective date: 20220420

Ref country code: EE

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

Effective date: 20220420

Ref country code: DK

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

Effective date: 20220420

Ref country code: CZ

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

Effective date: 20220420

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

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

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

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

Ref country code: MC

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

Effective date: 20220420

26N No opposition filed

Effective date: 20230123

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20220731

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

Ref country code: AL

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

Effective date: 20220420

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

Ref country code: LU

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

Effective date: 20220719

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

Ref country code: SI

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

Effective date: 20220420

Ref country code: BE

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

Effective date: 20220731

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

Effective date: 20230615

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

Ref country code: IE

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

Effective date: 20220719

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

Ref country code: FR

Payment date: 20230621

Year of fee payment: 5

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

Ref country code: CH

Payment date: 20230801

Year of fee payment: 5

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

Ref country code: DE

Payment date: 20230620

Year of fee payment: 5

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

Ref country code: IT

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

Effective date: 20220420

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

Effective date: 20230719