EP2450757B1 - Antischwingungsvorrichtung für Uhrenhemmungsmechanismus - Google Patents

Antischwingungsvorrichtung für Uhrenhemmungsmechanismus Download PDF

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Publication number
EP2450757B1
EP2450757B1 EP10190000.9A EP10190000A EP2450757B1 EP 2450757 B1 EP2450757 B1 EP 2450757B1 EP 10190000 A EP10190000 A EP 10190000A EP 2450757 B1 EP2450757 B1 EP 2450757B1
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EP
European Patent Office
Prior art keywords
balance
bistable
rotor
lever
trip device
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EP10190000.9A
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English (en)
French (fr)
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EP2450757A1 (de
Inventor
Arthur Queval
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Nivarox Far SA
Nivarox SA
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Nivarox Far SA
Nivarox SA
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Priority to EP10190000.9A priority Critical patent/EP2450757B1/de
Priority to TW100137739A priority patent/TWI531879B/zh
Priority to US13/287,558 priority patent/US8556499B2/en
Priority to RU2011144808/12A priority patent/RU2567681C2/ru
Priority to CN201110345372.4A priority patent/CN102467073B/zh
Priority to JP2011242021A priority patent/JP5411911B2/ja
Publication of EP2450757A1 publication Critical patent/EP2450757A1/de
Priority to HK12111953.8A priority patent/HK1171272A1/xx
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Publication of EP2450757B1 publication Critical patent/EP2450757B1/de
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    • GPHYSICS
    • G04HOROLOGY
    • G04BMECHANICALLY-DRIVEN CLOCKS OR WATCHES; MECHANICAL PARTS OF CLOCKS OR WATCHES IN GENERAL; TIME PIECES USING THE POSITION OF THE SUN, MOON OR STARS
    • G04B15/00Escapements
    • G04B15/06Free escapements
    • GPHYSICS
    • G04HOROLOGY
    • G04BMECHANICALLY-DRIVEN CLOCKS OR WATCHES; MECHANICAL PARTS OF CLOCKS OR WATCHES IN GENERAL; TIME PIECES USING THE POSITION OF THE SUN, MOON OR STARS
    • G04B17/00Mechanisms for stabilising frequency
    • G04B17/20Compensation of mechanisms for stabilising frequency
    • G04B17/26Compensation of mechanisms for stabilising frequency for the effect of variations of the impulses
    • 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
    • G04B43/00Protecting clockworks by shields or other means against external influences, e.g. magnetic fields
    • G04B43/002Component shock protection arrangements

Definitions

  • the invention relates to an anti-gallop device for an escape mechanism, arranged to cooperate with a rocker pivoting about a first axis of pivoting of fixed position relative to a platen.
  • the invention also relates to an escapement mechanism comprising, pivotally movable with respect to a plate, at least one pivoting arm about a balance shaft
  • the invention also relates to a watch movement comprising at least one such escape mechanism.
  • the invention also relates to a timepiece comprising at least one such watch movement or / and at least one such escape mechanism.
  • the invention relates to the field of watchmaking, in particular the field of escape mechanisms, and more particularly the field of relaxation escapements.
  • the trigger escapement mechanisms are considered the most accurate, and have long been reserved for marine chronometers.
  • gallop has the effect of distorting the isochronism of the oscillator.
  • the patent EP 1 708 047 in the name of WATCHES BREGUET SA describes a rocker having an arm carrying both a first finger to cooperate with the second actuating finger, and a beaked probe cooperating with a notched cam similar to the previous.
  • the first finger drives the second finger to disengage the pallets or rest of the escape wheel.
  • the spout of the arm-probe is then driven by a rising edge of the notched cam, to re-engage the locking means in the escape wheel.
  • the rocker pivots in the opposite direction the first finger drives the second finger to maintain the locking means engaged in the escape wheel.
  • this mechanism comprises two juxtaposed rest palettes comprising contiguous but non-aligned resting planes, which makes it possible to accommodate the tip of the wheel tooth. exhaust on a line of rest at the junction of these rest planes, creating a pull effect to overcome any stop pin.
  • the rest plan of the stopping pallet closest to the escape wheel is in effect before the tooth, and prevents him from continuing on his way.
  • the patent EP 1 708 046 on behalf of WATCHES BREGUET SA discloses a safety finger fixed on the balance plate, and arranged to cooperate with the teeth of the escape wheel and block if the pulse pallet was to be released by accident of the teeth of wheel. This arrangement prevents any panic of the escape wheel in the event of shock resulting in the reversal of the direction of rotation of the trays at the precise moment of the impulse of the wheel. The encounter of a tooth of the wheel with this safety finger blocks the wheel, brings back the trays in the correct direction of rotation.
  • a first mobile is subjected to a periodic torque, obtained for example by a rotor mounted in a stator.
  • This first mobile comprises, firstly in a base plane a first wheel having teething gaps on its periphery, and secondly on a second plane a first blocker having a plurality of fingers and adapted to block a release lever that includes a balance plate, in a first pivoting direction of this last.
  • This first mobile cooperates, depending on its position, either by the first blocker, or by its first wheel, with a second mobile.
  • This second mobile comprises, in the base plane, a second wheel having teething gaps, in the second plane a shaped piece having a plurality of fingers and adapted to lock the release lever of the balance plate, in a second pivoting direction. opposed to the first, and the second mobile further comprises, in a first plane parallel to the previous plans a locking piece.
  • This second mobile cooperates, depending on its position, either by the locking piece or by its second wheel, with an escape wheel, which comprises, in the base plane, a toothed wheel having teething gaps, and in the first plan impulse wheel receiving a continuous mechanical torque such as that of a cylinder, similar to a conventional escape wheel, and adapted to cooperate with a lever pulse that includes the balance plate, to maintain the movement of oscillation of this denier.
  • the locking pieces, or of shape, or the teeth cooperate with each other, so that the device has, for each revolution of rotation of the first axis, four stable locking positions, between which it has so many unlocking positions.
  • the combination of two locking means and two means of unlocking the mechanical torque, and the particular sequence imposing an unlocking operation between two blocking operations realize the prevention of any runaway or gallop in case of impact on the mechanism.
  • Such a mechanism is complex, relatively expensive, and unfolds in several planes, which makes its thickness significant.
  • a large platform of the balance typically carries a pulse pallet, preceded by a first recess, and followed by a second recess, to allow the release of the pallet rest when the release pallet rotates the trigger rocker.
  • the choice of a particular geometry both in terms of the positioning of the pallet of rest and the pallet of impulse in quasi-symmetry of the line of the centers of the escape wheel and the pendulum during the phase of rest, which 'at the fork formed by the finger and the free end of the leaf spring, limit the disruptive effect related to the inertia of the trigger on the pendulum oscillations.
  • the amplitude of the pivoting movements of the trigger in case of shock, is limited by the interaction of the pallet rest and large plateau.
  • this mechanism comprises an anti-gallop rocker, in the vicinity of the small plate, pivotally mounted on the movement between two stable end positions held by a jumper on stops with which can cooperate a first end, and a fork-shaped second end interacts with the release pallet: at each passage through the fork, the release pallet exerts pressure to tilt the anti-gallop rocker from one to the other of its stable positions.
  • the fork is thus two stops for the small plateau in case of galloping, and prevents the pendulum to do more than one turn in pivoting.
  • the document EP 1 860 511 in the name of Christophe Claret SA describes a moving bridge movement, providing protection against side impacts of a detent escapement.
  • This movable bridge carries the pivot axis of the sprung balance, the pivot axis of the escape wheel, the pivot axis of the trigger, and a part of the finishing gear. It is rotated elastically on the axis of one of the wheels of the cogwheel finishing, for example the second wheel. Forces, such as a side impact, capable of disengaging the pallet of rest, then drive the movable bridge in its entirety, and the relative positions of the trigger and the escape wheel are maintained. Thus, a constant step of the exhaust is ensured.
  • This movable bridge can, again, be damped by a damping system that allows to dissipate some of the energy due to impact.
  • the patent application CH 700 091 in the name of Christophe Claret SA describes a detent escapement, with a trigger rocker pivotally mounted on a spiral spring and cooperating at the other end with a first recessed spring blade in the vicinity of the pivot.
  • the balance plate has two separate pallets.
  • a movable member disposed on the opposite side of the escape wheel, relative to the trigger rocker, carries a pivoting cam, holding a cam spring blade, and biased toward the trigger by a spiral spring at a stop position. This cam is arranged to cooperate the cam spring-blade, or in a first state with the end of the load-bearing latch of the leaf spring, or in a second state with the pallets of release of the balance.
  • the first release pallet is arranged to cooperate with the first leaf spring and operate the trigger when the first paddle crosses the first blade in a first direction, and to cooperate only with the first blade and without actuating the trigger when it crosses in the opposite direction.
  • the cam in its first state, cooperates with the trigger to limit the movements thereof.
  • the second clearance pallet is arranged to move the cam into its second state where the trigger is free to perform its release and release the exhaust wheel tooth of the pallet rest.
  • the two clearance pallets are close together, and arranged in such a way that the cam is brought into its second state just before the detent makes its release.
  • the spiral return cam spring stronger than the cam spring blade, tends to return the cam to its first state.
  • the cam in its first state, is positioned to oppose everything inadvertent movement of the trigger that would result in an untimely release of the pallet rest, and the exhaust is less sensitive to the effects of a shock.
  • the adjustment of this mechanism is difficult because it depends on the characteristics of the springs it comprises, the number of at least three.
  • the patent application EP 2,224,292 in the name of Rolex SA discloses a direct impulse escapement, including expansion. Its trigger rocker is arranged in a particular way, pivoting between two stops, it has, turned towards the escape wheel, a finger successively comprising a stop surface serving as a pallet of rest, a safety surface which, depending on the position of pivoting of the rocker, interferes or not with the trajectory of the escape wheel, and a sliding surface which forces the rocker to tilt, during the pivoting of the escape wheel, in order to reduce the sliding surface and therefore the stop surface in the interference zone with the escape wheel to stop the pivoting thereof.
  • the balance plate conventionally comprises a pulse pallet and a release finger.
  • the rocker During the alternation in a first pivoting direction of the balance, the rocker is in a first pivoted position in abutment which leaves the passage to the release finger, while in the other alternation in the other direction of pivoting, the pivoted rocker in another abutment position encounters, at a resilient clearance element that it comprises, the release finger.
  • the elastic travel of this resilient release member allows the balance to continue its course, the pulse pallet passes between two adjacent teeth of the escape wheel. Shortly afterwards, the balance is stopped by its spring-spiral and pivots in opposite directions.
  • the rocker remains braced on its stop, and the stop surface of the rocker slides on the tooth of the escape wheel that keeps it in stop.
  • the safety of this mechanism is ensured by the arrangement of the finger of the rocker, with a stop surface and a sliding surface which penetrate alternately in the path of the toothing of the escape wheel.
  • the length of the safety surface between the stop surface and the sliding surface corresponds to the angle traveled by the wheel to communicate the driving energy to the balance, to prevent the premature return of the stop element in the path of the wheel , which constitutes a complementary security. Part of the energy of the cylinder is however consumed in friction during the sliding phase.
  • the document EP 1 645 918 in the name of MONTRES BREGUET SA describes such a mechanism, comprising a finger fixed on an arm of the balance.
  • the balance bridge has two columns, between which can pass this finger.
  • a locking arm is fixed on the outer turn of the spiral, in particular by pinching, and is likely, when the pendulum tends to pack under the effect of a shock, and exceed its normal amplitude, to come in support on the columns to prohibit the passage of the finger.
  • the invention proposes to overcome the shortcomings of the prior art, by proposing a mechanism that is both simple and reliable, inexpensive, and easily adaptable to existing exhaust mechanisms.
  • the invention relates to an anti-gallop device for an escape mechanism, arranged to cooperate with a rocker pivoting about a first axis of pivoting of fixed position relative to a plate, characterized in that said device comprises a limiting pin arranged to be fixed to said plate, as well as at least one mobile bistable assembly which comprises, on the one hand at least one rotor arranged to be fixed on said balance and to rotate synchronously with it, and secondly a bistable flip-flop pivotally movable relative to said rotor about a second pivot axis parallel to said first pivot axis on a limited angular sector between two indexing positions that can occupy indexing means that includes said bistable assembly for memorizing the position of said balance, at least a part of the trajectory of said flip-flop when pivoting said balance being interfering with ec said peg, and said bistable assembly further
  • said amplitude limitation means comprise at least first abutment means between said flip-flop and said pin, arranged to constitute, on the one hand, a pivot limit end stop when a pivoting of normal amplitude of the balance and on which a support of said bistable assembly generates a change of position of said indexing means, and secondly an abutment stop of said balance in case of rebate during an impact on said pendulum or on a set including said pendulum.
  • said first abutment means comprise at least one first abutment abutment surface that comprises said bistable flip-flop and which is arranged to cooperate with a first front surface that comprises said peg and directed towards said first axis of pivoting, and they also comprise at least a second rebate abutment surface that comprises said flip-flop and which is arranged to cooperate with a second lateral surface that comprises said pin and directed in a direction substantially orthogonal to that joining said pin to said first pivot axis.
  • said amplitude limitation means comprise at least second stop means between said flip-flop and said rotor.
  • said second stop means comprise at least a third abutment surface that comprises said flip-flop and which is arranged to cooperate in abutment position with at least one rotor abutment surface that includes said rotor.
  • said indexing means comprise, at said bistable flip-flop, for each said indexing position, a rocker arm, respectively a rocker notch, arranged to cooperate with a rotor notch, respectively a rotor arm, which comprises said rotor.
  • said flip-flop comprises at least a first rocker arm and a second rocker arm corresponding to said indexing positions between which said flip-flop can pivot, each recalled by elastic return means towards said second pivot axis, arranged to cooperate each in turn with said rotor notch formed at the periphery of said rotor.
  • said bistable assembly is made integrally, and that the connection between said rotor and said flip-flop is made by elastic return means.
  • said bistable assembly is made integrally with a balance.
  • said bistable assembly is made integrally with said balance which is itself integrally formed with a spiral spring.
  • said rotor or / and said flip-flop is made of silicon, or quartz or one of their compounds, or an at least partially amorphous material.
  • the invention also relates to an escapement mechanism comprising, pivotally movable relative to a plate, at least one rocker pivoting about a balance shaft, characterized in that it is a trigger escapement mechanism, and in that it comprises such an anti-gallop device, said limiting pin is fixed to said plate, said rotor is fixed to a shaft that includes said balance, and said flip-flop is mounted pivotally mounted around a second pivot axis parallel to said first pivot axis.
  • the invention also relates to a watch movement comprising at least one such escape mechanism.
  • the invention also relates to a timepiece comprising at least one such watch movement or / and at least one such escape mechanism.
  • the invention relates to the field of watchmaking.
  • the invention relates to an anti-gallop device 1 for escape mechanism 10:
  • This anti-gallop device 1 is arranged to cooperate with a rocker 2, which pivots about a first pivot axis D1 of fixed position with respect to a platinum 3.
  • the anti-gallop device 1 is very simple because it is composed of three components at most: an anchor 5 fixed to the plate of the escapement mechanism, or movement, or the timepiece, a rotor 9 attached to the balance 9, and a flip-flop 11. It will be seen later that in a particular version, it can be reduced to two components.
  • the device 1 comprises a limiting pin 5 arranged to be fixed to the plate 3, as well as at least one mobile bistable assembly 8.
  • This bistable assembly 8 comprises, firstly at least one rotor 9 arranged to be fixed on the rocker 2 and to pivot synchronously with it, and secondly a bistable rocker 11, which is pivotally movable relative to the rotor 9 about a second pivot axis D2 parallel to the first pivot axis D1.
  • This relative mobility is done on a limited angular sector, of opening ⁇ , between two extreme indexing positions that can occupy indexing means 12 that includes the bistable assembly 8 to memorize the state of the balance 2.
  • bistable assembly 8 on the balance 2 makes it possible to memorize the position of the latter, and thus to limit the over-amplitudes in the event of an impact, which represents a notable improvement over the prior art.
  • the flip-flop 11 pivots with a limited stroke on a center of rotation off-center with respect to that of the balance.
  • the bistable assembly 8 further comprises amplitude limiting means 15 for limiting the amplitude of the angular pivoting. balance 2 in case of shock.
  • the bistable set 8 can occupy two stable states: a so-called hour state whose figure 3 illustrates activation, and a so-called counter-clockwise state, whose figure 4 illustrates the activation. In normal operation, only these two states are used, except during the transition from one state to another. This transition occurs when one end of the rocker 11 encounters the pin 5, thus toggling the rocker 11 in the opposite state to the one it previously occupied.
  • the bistable assembly 8 changes state twice by complete oscillation of the balance.
  • These amplitude limiting means 15 comprise at least first abutment means 16 between the flip-flop 11 and the peg 5, which are arranged to constitute, on the one hand, a pivot limit stop when pivoting. of normal amplitude of the balance and on which a support of this bistable assembly 8 generates a change of position of the indexing means 12, and secondly a stop stop of the balance 2 in case of rebate during a shock on the balance 2 or on a set including the pendulum 2.
  • the first abutment means 16 comprise at least a first abutment abutment surface 17, which comprises the flip-flop 11, and which is arranged to cooperate with a first front surface 6 that includes the pin 5 and which is directed towards the first pivot axis D1.
  • the first abutment means 16 also comprise at least a second rebate abutment surface 18, which comprises the flip-flop 11, and which is arranged to cooperate with a second lateral surface 7 that comprises the pin 5, this second surface 7 being directed in a direction substantially orthogonal to that joining the pin 5 to the first pivot axis D1. Stopping the balance is obtained in this stop position, if the balance 2 tends to pack in case of shock.
  • the amplitude limiting means 15 comprise at least second stop means 20 between the flip-flop 11 and the rotor 9, which constitute an additional safety in the event of an impact.
  • the second abutment means 20 comprise at least one third abutment surface 21, which comprises the flip-flop 11, and which is arranged to cooperate in an abutment position with at least a rotor abutment surface 22 that includes the rotor 9.
  • Returning means such as leaf springs, preferably symmetrical, and integral with the bistable assembly 8, are integral with the flip-flop 11 as shown in the figures, or integral with the rotor 9 in another embodiment not shown in the figures, allow to maintain the state of the rocker clipping to the next half-oscillation. It should be noted that any change in state of the bistable assembly 8, which would not be caused by the action of the ankle 5, causes an immediate stop of the exhaust mechanism, for example in the event of rupture of such blades -spring.
  • the indexing means 12 comprise, at the level of the flip-flop 11, for the extreme indexing positions, and preferably for each indexing position, a rocker arm 13, respectively a rocker notch, arranged to cooperate with a rotor notch 14, respectively a rotor arm, that includes the rotor 9.
  • Intermediate indexing positions may be useful to mobilize the resistant torque, exhaust efficiency destroyer, only gradually .
  • the preferred embodiment is that shown in the figures, with only two extreme indexing positions, each relating to a specific state of the pendulum 2.
  • the flip-flop 11 comprises at least a first rocker arm 13A and a second rocker arm 13B corresponding to the indexing positions between which the flip-flop 11 can pivot, each recalled by means of FIG. elastic return to the second pivot axis D2, arranged to cooperate each in turn with the rotor notch 14 formed at the periphery of the rotor 9.
  • the rotor 9 is symmetrical with respect to an axis passing through the two axes pivoting D1 and D2
  • the flip-flop 11 is also symmetrical with respect to a plane passing through the pivot axis D2. This symmetry facilitates the balancing, particularly dynamic, of the bistable assembly 8.
  • the arms 13A and 13B are leaf springs, each having an arranged end to cooperate with the rotor notch 14. Their dimensioning is carried out so that their active length is sufficient to consume the least energy possible during the change of state, and so that the maintenance of the position of the rocker is ensured in case of shock.
  • the flip-flop 11 comprises a first so-called right lug abutment surface 17A on the side of the first flip-flop arm 13A, and a first so-called left lug abutment surface 17B on the side of the second flip-flop arm 13B, each arranged to cooperate, during the pivoting of the rocker 2, with the first end surface 6 of the pin 5 to bow-flip the flip-flop 11 on the latter while allowing the continuation of the stroke of the balance 2 to change position indexing. While the rocker 2 continues its course, successively it picks up the rocker arm which was engaged in the rotor notch 14, continues its pivoting stroke during a limited angular sector of amplitude ⁇ to hang the other rocker arm in the rotor notch 14.
  • the flip-flop 11 comprises a second right rebate abutment surface 18A on the side of the first latch arm 13A, and a second left rebate abutment surface 18B on the side of the second latch arm 13B, each arranged to cooperate, during the pivoting of the balance 2, with a second lateral surface 7 of the peg 5, to bow-flip the flip-flop 11 on the latter while allowing the continuation of the stroke of the balance 2 to change indexing position.
  • the bistable assembly 8 comprises resilient damping means at the level of the second rebate abutment surface 18A; 18B, or / and at the level of the third abutment surface 21A. ; 21B, or / and a rotor abutment surface 22A; 22B, to provide additional security when the energy imparted by a shock pendulum 2 tends to rotate the latter beyond an extreme indexing position.
  • the bistable assembly 8 is dynamically balanced around the first pivot axis D1 of the balance 2 as a function of the maximum angular speed of pivoting of the balance 2 around the first pivot axis D1.
  • the bistable assembly 8 is made integrally, and the connection between the rotor 9 and the flip-flop 11 is made by a connecting surface 24 preferably constituted by elastic return means, arranged to rotate the rocker bistable 11 around a virtual pivot axis D2.
  • the bistable assembly 8 is made in one piece with a rocker 2, or even the bistable assembly 8 is made in one piece with the rocker 2 which is itself integrally formed with a spring -spiral.
  • the rotor 9 or / and the flip-flop 11 is made of a micro-machinable material, or silicon, or quartz or one of their compounds, or an alloy derived from MEMS technology, or an alloy as obtained by the method DRIE or "LIGA", or at least partially amorphous material.
  • the invention also relates to an escapement mechanism 10 comprising, pivotally movable relative to a plate 3, at least one rocker 2 pivoting about a balance shaft D1.
  • it is a trigger escapement mechanism, and it comprises an anti-gallop device 1 according to the invention, whose limiting pin 5 is fixed to the plate 3, the rotor 9 is fixed, in particular by shrinking or similar, at a bore 19 that includes this rotor, a shaft 4 that includes the balance 2, and whose flip-flop 11 is pivotally mounted to pivot about a second pivot axis D2 parallel to the first axis pivoting D1.
  • the assembly consisting of the rocker 2 and the rocker 3 is preferably monobloc, and is made of a micro-machinable material, or silicon, or quartz or one of their compounds , or an alloy derived from MEMS technology, or an alloy as obtained by the DRIE or "LIGA” method, or an at least partially amorphous material.
  • This assembly can also be made in one piece with a spiral spring, as described in the European patent application. EP 2 104 008 in the name of the plaintiff.
  • the invention also relates to a watch movement comprising at least one such escape mechanism, or at least one anti-gallop device 1.
  • the invention also relates to a timepiece comprising at least one such watch movement and / or at least one such escapement mechanism, or at least one such anti-gallop device 1.
  • the invention thus offers a reliable solution, very easy to implement, which has the advantage of being applicable to any existing expansion escapement model at the cost of minor modifications consisting in the attachment of a rotor to the rotor. balance shaft, and the fixing of a limiting pin on the plate.
  • This anti-gallop device is elegant, integrates easily, has few components, and is especially reliable, and allows the exhaust mechanism to resume normal operation after a shock.

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Micromachines (AREA)
  • Transmission Devices (AREA)
  • Vibration Prevention Devices (AREA)
  • Mechanical Control Devices (AREA)
  • Lock And Its Accessories (AREA)
  • Vibration Dampers (AREA)

Claims (18)

  1. Antigalopp-Vorrichtung (1) für einen Hemmungsmechanismus (10), welche Vorrichtung derart beschaffen ist, dass sie mit einer Unruh (2) zusammenwirkt, die um eine erste Drehachse (D1) schwenkt, die in fester Position im Verhältnis zu einer Werkplatte (3) ist, und welche Vorrichtung einen Begrenz-Stift (5) umfasst, der derart vorgesehen ist, dass er an der Werkplatte (3) befestigt wird, dadurch gekennzeichnet, dass sie wenigstens eine bewegliche bistabile Einheit (8) umfasst, die einerseits wenigstens einen Rotor (9) umfasst, der derart vorgesehen ist, dass er an der Unruh (2) befestigt wird und synchron mit ihr dreht, und die andererseits eine bistabile Wippe (11) umfasst, die drehbeweglich im Verhältnis zum Rotor (9) um eine zweite Drehachse (D2), die parallel zur ersten Drehachse (D1) ist, über einen Winkelsektor ist, der zwischen zwei Index-Positionen begrenzt ist, die von Index-Mitteln (12), die zur bistabilen Einheit (8) gehören, eingenommen werden können, um die Position der Unruh (2) zu speichern, wobei wenigstens ein Teil des Wegs der bistabilen Wippe (11) beim Schwenken der Unruh (2) mit dem Stift (5) interferiert und wobei die bistabile Einheit (8) noch Amplitudenbegrenz-Mittel (15) umfasst, um die Amplitude der Winkelschwenkung der Unruh (2) im Fall eines Schlags zu begrenzen.
  2. Antigalopp-Vorrichtung (1) nach vorhergehendem Anspruch, dadurch gekennzeichnet, dass die Amplitudenbegrenz-Mittel (15) wenigstens erste Anschlagmittel (16) zwischen der bistabilen Wippe (11) und dem Stift (5) umfassen, die derart vorgesehen sind, dass sie einerseits bei einer Schwenkbewegung von normaler Amplitude der Unruh einen Schwenkendlage-Anschlag bilden, der bei einer Abstützung der bistabilen Einheit (8) eine Positionsänderung der Index-Mittel (12) erzeugt, und dass sie andererseits einen Anschlag zum Anhalten der Unruh (2) im Fall eines Prellens bei einem Schlag auf die Unruh (2) oder auf die die Unruh (2) enthaltende Einheit bilden.
  3. Antigalopp-Vorrichtung (1) nach vorhergehendem Anspruch, dadurch gekennzeichnet, dass die ersten Anschlagmittel (16) wenigstens eine erste Längsspiel-Anschlagfläche (17) umfassen, die zur bistabilen Wippe (11) gehört und derart beschaffen ist, dass sie mit einer ersten Stirnfläche (6) zusammenwirkt, die zum Stift (5) gehört und auf die erste Drehachse (D1) gerichtet ist, und dass diese ersten Anschlagmittel noch wenigstens eine zweite Prell-Anschlagfläche (18) umfassen, die zur bistabilen Wippe (11) gehört und derart beschaffen ist, dass sie mit einer zweiten Seitenfläche (7) zusammenwirkt, die zum Stift (5) gehört und gemäss einer Richtung ausgerichtet ist, die merklich orthogonal zu derjenigen ist, die den Stift (5) mit der ersten Drehachse (D1) verbindet.
  4. Antigalopp-Vorrichtung (1) nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass die Amplitudenbegrenz-Mittel (15) wenigstens zweite Anschlagmittel (20) zwischen der bistabilen Wippe (11) und dem Rotor (9) umfassen.
  5. Antigalopp-Vorrichtung (1) nach vorhergehendem Anspruch, dadurch gekennzeichnet, dass die zweiten Anschlagmittel (20) wenigstens eine dritte Anschlagfläche (21) umfassen, die zur bistabilen Wippe (11) gehört und derart beschaffen ist, dass sie in Anschlagposition mit wenigstens einer Rotor-Anschlagfläche (22), die zum Rotor (9) gehört, zusammenwirkt, um eine zweite Sicherheitsvorrichtung zu bilden, wenn die Energie, die durch einen Schlag auf die Unruh (2) übertragen wird, dazu tendiert, diese Letztere über eine Index-Grenzposition hinaus schwenken zu lassen.
  6. Antigalopp-Vorrichtung (1) nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass die Index-Mittel (12) im Bereich der bistabilen Wippe (11) für jede Index-Position einen Wippenarm (13) bzw. eine Wippenkerbe umfassen, die derart beschaffen sind, dass sie mit einer Rotorkerbe (14) bzw. mit einem Rotorarm, die zum Rotor (9) gehören, zusammenwirken.
  7. Antigalopp-Vorrichtung (1) nach vorhergehendem Anspruch, dadurch gekennzeichnet, dass die bistabile Wippe (11) wenigstens einen ersten Wippenarm (13A) und einen zweiten Wippenarm (13B) umfasst, die den Index-Positionen entsprechen, zwischen denen die bistabile Wippe (11) schwenken kann, wobei beide Wippenarme durch elastische Rückstellmittel gegen die zweite Drehachse (D2) zurückgebracht werden und derart beschaffen sind, dass sie nacheinander mit der am Umfang des Rotors (9) ausgebildeten Rotorkerbe (14) zusammenwirken.
  8. Antigalopp-Vorrichtung (1) nach den Ansprüchen 3 und 7, dadurch gekennzeichnet, dass die bistabile Wippe (11) eine erste rechte Längsspiel-Anschlagfläche (17A) seitens des ersten Wippenarms (13A) und eine erste linke Längsspiel-Anschlagfläche (17B) seitens des zweiten Wippenarms (13B) umfasst, die beide derart beschaffen sind, dass sie beim Schwenken der Unruh (2) mit der ersten Stirnfläche (6) des Stifts (5) zusammenwirken, um die bistabile Wippe (11) gegen diesen Letzteren zu stemmen, wobei sie dennoch die Fortsetzung des Laufs der Unruh (2) zulassen, um die Index-Position zu ändern.
  9. Antigalopp-Vorrichtung (1) nach den Ansprüchen 5 und 8, dadurch gekennzeichnet, dass die bistabile Wippe (11) eine zweite rechte Prell-Anschlagfläche (18A) seitens des ersten Wippenarms (13A) und eine zweite linke Prell-Anschlagfläche (18B) seitens des zweiten Wippenarms (13B) umfasst, die beide derart beschaffen sind, dass sie beim Schwenken der Unruh (2) mit einer zweiten Seitenfläche (7) des Stifts (5) zusammenwirken, um die bistabile Wippe (11) gegen diesen Letzteren zu stemmen, wobei sie dennoch die Fortsetzung des Laufs der Unruh (2) zulassen, um die Index-Position zu ändern.
  10. Antigalopp-Vorrichtung (1) nach den Ansprüchen 3, 5 und 7, dadurch gekennzeichnet, dass sie elastische Dämpfungsmittel im Bereich der zweiten Prell-Anschlagfläche (18A; 18B) oder/und im Bereich der dritten Anschlagfläche (21A; 21 B) oder/und im Bereich einer Rotor-Anschlagfläche (22A; 22B) umfasst.
  11. Antigalopp-Vorrichtung (1) nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass der Rotor (9) symmetrisch im Verhältnis zu einer Achse ist, die durch die erste Drehachse (D1) und die zweite Drehachse (D2) läuft, und dass die bistabile Wippe (11) symmetrisch im Verhältnis zu einer Ebene ist, die durch die zweite Drehachse (D2) läuft.
  12. Antigalopp-Vorrichtung (1) nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass die bistabile Einheit (8) monoblockartig ausgeführt ist und dass die Verbindung zwischen dem Rotor (9) und der bistabilen Wippe (11) durch elastische Rückstellmittel realisiert ist.
  13. Antigalopp-Vorrichtung (1) nach vorhergehendem Anspruch, dadurch gekennzeichnet, dass die bistabile Einheit (8) monoblockartig mit einer Unruh (2) ausgeführt ist.
  14. Antigalopp-Vorrichtung (1) nach vorhergehendem Anspruch, dadurch gekennzeichnet, dass die bistabile Einheit (8) monoblockartig mit der Unruh (2) ausgeführt ist, die ihrerseits monoblockartig mit einer Spiralfeder ausgeführt ist.
  15. Antigalopp-Vorrichtung (1) nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass der Rotor (9) oder/und die bistabile Wippe (11) aus Silizium oder Quarz, oder einer ihrer Verbindungen, oder aus einem wenigstens teilweise amorphen Werkstoff ausgeführt ist.
  16. Hemmungsmechanismus (10), der wenigstens eine Unruh (2) umfasst, die drehbeweglich im Verhältnis zu einer Werkplatte (3) ist und um eine Unruhachse (D1) schwenkt, dadurch gekennzeichnet, dass er ein Chronometer-Hemmungsmechanismus ist und dass er eine Antigalopp-Vorrichtung (1) nach einem der vorhergehenden Ansprüche umfasst, deren Begrenz-Stift (5) an der Werkplatte (3) befestigt ist, deren Rotor (9) an einer zur Unruh (2) gehörigen Welle (4) befestigt ist und deren bistabile Wippe (11) drehbeweglich um eine zweite Drehachse (D2) montiert ist, die parallel zur ersten Drehachse (D1) ist.
  17. Uhrwerk, das wenigstens einen Hemmungsmechanismus nach Anspruch 16 oder wenigstens eine Antigalopp-Vorrichtung (1) nach einem der Ansprüche 1 bis 15 umfasst.
  18. Zeitmessgerät, das wenigstens ein Uhrwerk nach Anspruch 17 oder/und wenigstens einen Hemmungsmechanismus nach Anspruch 16 oder wenigstens eine Antigalopp-Vorrichtung (1) nach einem der Ansprüche 1 bis 15 umfasst.
EP10190000.9A 2010-11-04 2010-11-04 Antischwingungsvorrichtung für Uhrenhemmungsmechanismus Active EP2450757B1 (de)

Priority Applications (7)

Application Number Priority Date Filing Date Title
EP10190000.9A EP2450757B1 (de) 2010-11-04 2010-11-04 Antischwingungsvorrichtung für Uhrenhemmungsmechanismus
TW100137739A TWI531879B (zh) 2010-11-04 2011-10-18 用於擒縱機構的防脫扣裝置
US13/287,558 US8556499B2 (en) 2010-11-04 2011-11-02 Anti-trip device for an escape mechanism
RU2011144808/12A RU2567681C2 (ru) 2010-11-04 2011-11-03 Антиблокировочное устройство для спускового механизма
CN201110345372.4A CN102467073B (zh) 2010-11-04 2011-11-04 用于擒纵机构的抗脱扣装置
JP2011242021A JP5411911B2 (ja) 2010-11-04 2011-11-04 脱進機構用の歯飛び防止装置
HK12111953.8A HK1171272A1 (en) 2010-11-04 2012-11-22 Anti-trip device for an escape mechanism

Applications Claiming Priority (1)

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EP10190000.9A EP2450757B1 (de) 2010-11-04 2010-11-04 Antischwingungsvorrichtung für Uhrenhemmungsmechanismus

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EP2450757B1 true EP2450757B1 (de) 2014-10-15

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Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2690506B1 (de) * 2012-07-25 2015-01-14 Nivarox-FAR S.A. Antischwingungsspirale für Uhr
CH706766A2 (fr) * 2012-07-26 2014-01-31 Nivarox Sa Spiral d'horlogerie anti-galop.
EP2706416B1 (de) 2012-09-07 2015-11-18 The Swatch Group Research and Development Ltd Flexibler Anker mit konstanter Kraft
EP2730980B1 (de) * 2012-11-09 2018-08-29 Nivarox-FAR S.A. Uhrmechanismus zur Begrenzung oder Übertragung
CH707811A2 (fr) 2013-03-19 2014-09-30 Nivarox Sa Composant monobloc indémontable d'horlogerie.
CH710759A2 (fr) * 2015-02-20 2016-08-31 Nivarox Far Sa Oscillateur pour une pièce d'horlogerie.
EP3136187B1 (de) * 2015-08-31 2018-02-28 Glashütter Uhrenbetrieb GmbH Mechanisches uhrwerk mit einem tourbillon
EP3182213B2 (de) * 2015-12-16 2020-10-21 Société anonyme de la Manufacture d'Horlogerie Audemars Piguet & Cie Einstellmechanismus der mittleren geschwindigkeit in einem uhrwerk, und entsprechendes uhrwerk
CN109254517B (zh) * 2017-07-12 2023-11-07 天津海鸥表业集团有限公司 一种手表的擒纵调速模块及应用

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US180290A (en) 1876-07-25 Improvement in chronometer-escapements for watches
US361850A (en) * 1886-06-12 1887-04-26 A Van Strait Regulator pin for watches
US710823A (en) * 1901-12-04 1902-10-07 Frederick Hermann Voigt Escapement for timepieces.
US867015A (en) * 1906-10-15 1907-09-24 Henri Coullery Escapement mechanism for timepieces.
CH251930A (fr) * 1945-03-29 1947-11-30 Co Benrus Watch Dispositif amortisseur de chocs pour pivots de balancier de montre.
US2698509A (en) * 1951-11-23 1955-01-04 Rhodes Inc M H Balance spring for clockwork mechanisms
US3704582A (en) * 1970-10-15 1972-12-05 Timex Corp Indexing mechanism for horological instrument
EP1522001B1 (de) 2002-07-11 2006-08-09 Detra SA Hemmung
DE60334916D1 (de) * 2003-12-04 2010-12-23 Montres Breguet Sa Chronometerhemmung für Uhren
EP1666990B1 (de) * 2004-10-05 2011-12-28 Montres Breguet S.A. Vorrichtung zum Galoppschutz für Uhrenhemmung
EP1645918A1 (de) * 2004-10-05 2006-04-12 Montres Breguet S.A. Vorrichtung zum Galoppschutz für Uhrenhemmung
EP1708046B1 (de) 2005-03-30 2008-03-26 Montres Breguet S.A. Chronometerhemmung für Uhren
DE602005005633T2 (de) 2005-03-30 2009-04-16 Montres Breguet S.A. Chronometerhemmung für Uhren
EP1708053A1 (de) * 2005-03-31 2006-10-04 Montres Breguet S.A. Vorrichtung zur Stossdämpfung für einen Drehzapfen einer Unruh, und ein Uhrwerk damit
EP1770452A1 (de) 2005-09-30 2007-04-04 Peter Baumberger Chronometerhemmung für Uhren
ATE388428T1 (de) * 2005-12-20 2008-03-15 Montres Breguet Sa Vorrichtung zum galoppschutz für uhrenhemmung
ATE555427T1 (de) 2006-05-23 2012-05-15 Manuf Claret Sa Uhrwerk mit einer mobilen brücke
EP2104008A1 (de) 2008-03-20 2009-09-23 Nivarox-FAR S.A. Monoblock-Regulierungsorgan und sein Herstellungsverfahren
CH700091A8 (fr) 2009-01-15 2010-08-31 Christophe Claret S A Échappement à détente.
EP2224292B1 (de) * 2009-02-26 2012-10-10 Rolex Sa Chronometerhemmung für Uhrwerk
EP2233988B1 (de) * 2009-03-23 2012-02-08 Montres Breguet SA Uhrwerk mit Tourbillon, das mit einer stoßfesten Schutzvorrichtung ausgestattet ist

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CN102467073A (zh) 2012-05-23
CN102467073B (zh) 2013-09-04
US8556499B2 (en) 2013-10-15
EP2450757A1 (de) 2012-05-09
HK1171272A1 (en) 2013-03-22
US20120113765A1 (en) 2012-05-10
RU2567681C2 (ru) 2015-11-10
TW201237572A (en) 2012-09-16
JP2012098290A (ja) 2012-05-24
JP5411911B2 (ja) 2014-02-12
RU2011144808A (ru) 2013-05-10
TWI531879B (zh) 2016-05-01

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