EP3435173B1 - Mechanisches uhrwerk mit sich drehendem isochronem resonator, der positionsunempfindlich ist - Google Patents
Mechanisches uhrwerk mit sich drehendem isochronem resonator, der positionsunempfindlich ist Download PDFInfo
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- EP3435173B1 EP3435173B1 EP17183211.6A EP17183211A EP3435173B1 EP 3435173 B1 EP3435173 B1 EP 3435173B1 EP 17183211 A EP17183211 A EP 17183211A EP 3435173 B1 EP3435173 B1 EP 3435173B1
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- movement
- axis
- inertial element
- inertial
- central
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- 230000009975 flexible effect Effects 0.000 claims description 34
- 238000004146 energy storage Methods 0.000 claims description 3
- 229910052710 silicon Inorganic materials 0.000 claims description 3
- 239000010703 silicon Substances 0.000 claims description 3
- 230000036316 preload Effects 0.000 claims description 2
- 230000007246 mechanism Effects 0.000 description 16
- 230000005484 gravity Effects 0.000 description 6
- 230000008901 benefit Effects 0.000 description 4
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 3
- 230000001629 suppression Effects 0.000 description 3
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- 238000006243 chemical reaction Methods 0.000 description 2
- 230000036461 convulsion Effects 0.000 description 2
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- 238000003379 elimination reaction Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 230000010349 pulsation Effects 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 241001080024 Telles Species 0.000 description 1
- 240000008042 Zea mays Species 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 230000034373 developmental growth involved in morphogenesis Effects 0.000 description 1
- 229910003460 diamond Inorganic materials 0.000 description 1
- 239000010432 diamond Substances 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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Images
Classifications
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- G—PHYSICS
- G04—HOROLOGY
- G04B—MECHANICALLY-DRIVEN CLOCKS OR WATCHES; MECHANICAL PARTS OF CLOCKS OR WATCHES IN GENERAL; TIME PIECES USING THE POSITION OF THE SUN, MOON OR STARS
- G04B17/00—Mechanisms for stabilising frequency
- G04B17/04—Oscillators acting by spring tension
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03G—SPRING, WEIGHT, INERTIA OR LIKE MOTORS; MECHANICAL-POWER PRODUCING DEVICES OR MECHANISMS, NOT OTHERWISE PROVIDED FOR OR USING ENERGY SOURCES NOT OTHERWISE PROVIDED FOR
- F03G7/00—Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for
- F03G7/08—Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for recovering energy derived from swinging, rolling, pitching or like movements, e.g. from the vibrations of a machine
-
- G—PHYSICS
- G04—HOROLOGY
- G04B—MECHANICALLY-DRIVEN CLOCKS OR WATCHES; MECHANICAL PARTS OF CLOCKS OR WATCHES IN GENERAL; TIME PIECES USING THE POSITION OF THE SUN, MOON OR STARS
- G04B17/00—Mechanisms for stabilising frequency
- G04B17/20—Compensation of mechanisms for stabilising frequency
- G04B17/26—Compensation of mechanisms for stabilising frequency for the effect of variations of the impulses
-
- G—PHYSICS
- G04—HOROLOGY
- G04B—MECHANICALLY-DRIVEN CLOCKS OR WATCHES; MECHANICAL PARTS OF CLOCKS OR WATCHES IN GENERAL; TIME PIECES USING THE POSITION OF THE SUN, MOON OR STARS
- G04B17/00—Mechanisms for stabilising frequency
- G04B17/20—Compensation of mechanisms for stabilising frequency
- G04B17/28—Compensation of mechanisms for stabilising frequency for the effect of imbalance of the weights, e.g. tourbillon
-
- G—PHYSICS
- G04—HOROLOGY
- G04B—MECHANICALLY-DRIVEN CLOCKS OR WATCHES; MECHANICAL PARTS OF CLOCKS OR WATCHES IN GENERAL; TIME PIECES USING THE POSITION OF THE SUN, MOON OR STARS
- G04B17/00—Mechanisms for stabilising frequency
- G04B17/30—Rotating governors, e.g. centrifugal governors, fan governors
-
- G—PHYSICS
- G04—HOROLOGY
- G04B—MECHANICALLY-DRIVEN CLOCKS OR WATCHES; MECHANICAL PARTS OF CLOCKS OR WATCHES IN GENERAL; TIME PIECES USING THE POSITION OF THE SUN, MOON OR STARS
- G04B17/00—Mechanisms for stabilising frequency
- G04B17/04—Oscillators acting by spring tension
- G04B17/045—Oscillators acting by spring tension with oscillating blade springs
Definitions
- the invention relates to a mechanical clockwork movement comprising at least one energy storage means arranged to drive a gear train, an output mobile of which is arranged to pivot around a motor axis, and comprising a rotary resonator which comprises at least a central mobile, arranged to pivot about a central axis, and comprising an input mobile arranged to cooperate with the output mobile.
- the invention also relates to a watch comprising such a movement.
- the invention relates to the field of time bases for mechanical watch movements.
- the exhaust must be robust, withstand shocks, avoid jamming the movement (overturning), and foolproof over time.
- the most commonly used Swiss lever escapement has a low energy efficiency, around 30%. This low efficiency comes from the fact that the movements of the exhaust are jerky, that there are falls or lost paths that are necessary to accommodate the machining dispersions, and also from the fact that several components transmit their movement. via inclined planes which rub against each other. Such mechanisms are disclosed in the documents CH293180 A and FR630831A .
- the present invention aims to eliminate the jerks of the exhaust, in order to increase the yield.
- a rotary resonator is proposed, characterized in particular by the possibility of maintaining rotation by a torque applied directly to the axis of the resonator, thus avoiding the dynamic losses of a conventional anchor escapement.
- a mechanism like the Watt regulator can form a basis for a rotary resonator, but at the cost of modifications to make it isochronous and insensitive to gravity.
- the Watt regulator is sensitive to its orientation in the gravity field, because the global center of mass of the two weights moves when the amplitude changes: the weights rise along the axis when the amplitude increases. Consequently, the contribution of gravity to the restoring force fluctuates with orientation.
- the watt regulator is anisochronous because the return force of the weights, by spring and / or by gravity does not meet certain conditions.
- the invention relates to a mechanical clockwork movement according to claim 1.
- the invention also relates to a watch comprising such a movement.
- Requirement EP16195399 by the same applicant relates to a resonator mechanism for a clockwork movement, comprising an input mobile mounted pivoting about an axis of rotation and subjected to a motor torque, and comprising a central mobile, integral in rotation with this input mobile about the axis of rotation and arranged to rotate continuously.
- This resonator mechanism comprises a plurality of N inertial elements, each mobile according to at least one degree of freedom relative to the central mobile, and returned towards the axis of rotation by elastic return means, which are arranged to cause a return force. on the center of mass of the inertial element.
- This resonator mechanism has a symmetry of rotation of order N.
- This resonator mechanism comprises means of kinematic connection between all the inertial elements, and which are arranged to maintain, at all times, all the centers of mass of the inertial elements at the same distance from the axis of rotation, and the elastic return means cause an elastic potential characterized by a particular relationship. More particularly, this resonator mechanism has a pantograph type structure.
- the aim here is to improve such a mechanism. Indeed, the drive torque and the aerodynamic resistance torque generate a radial force which adds to the elastic potential, and disturbs the isochronism.
- the present invention proposes to orient the pivoting of the inertial elements differently, so as not to disturb the isochronism by the drive or tangential aerodynamic forces.
- the figure 1 illustrates a variant of a resonator mechanism according to the invention, in which the pivoting of the inertial elements takes place orthogonally to the pivoting of the drive.
- the figure 2 shows that the complex articulated link of the mechanism of the figure 1 , arising directly from the request EP16195399 , may disappear in favor of a very simple structure: the present invention has the advantage of combining the driving mobile and the resonator in a single entity which is very simple to produce.
- This mechanism avoids the shocks and friction inherent in badly tuned groove or connecting rod-crank mechanisms.
- the invention avoids the unnecessary multiplication of elastic elements, between the plate and the inertial element on the one hand, and between the driving mobile and the inertial element on the other hand.
- the invention relates to a mechanical clockwork movement 100 comprising at least one energy storage means 200, such as a barrel or the like, arranged to drive a gear train 300 of which an output mobile is arranged to pivot around d 'a motor axis.
- This movement 100 comprises a rotary resonator 10, which comprises at least one central mobile 1, arranged to pivot around a central axis A.
- this central axis A is parallel or perpendicular to the motor axis.
- the central mobile 1 comprises an input mobile 2, which is arranged to cooperate with the output mobile.
- the rotary resonator 10 comprises at least one inertial element 3 arranged to pivot relative to the central mobile 1 around a secondary axis B perpendicular to the central axis A and intersecting with it, and returned to a position of rest, relative to the central mobile 1, by at least one elastic return element 4, and this secondary axis B passes through the center of mass of the inertial element 3 which is associated with it.
- the rotary resonator 10 comprises a plurality of inertial elements 3, each arranged to pivot relative to the central mobile 1 around a secondary axis B perpendicular to the central axis A and intersecting with it, and each recalled towards a rest position, relative to the central mobile 1, by at least one elastic return element 4.
- each secondary axis B passes through the center of mass of the inertial element 3 which is associated with it.
- this rotary resonator 10 has, in a rest position, a rotational symmetry about the central axis A, of order N, where N is an integer, greater than or equal to 2.
- the inertial elements 3 that the rotary resonator 10 comprises are, in a rest position, in rotational symmetry about the central axis A, of order N, where N is an integer, greater than or equal to 2.
- each inertial element 3 has a symmetry of rotation of order 2 around its secondary axis B.
- At least one elastic return element 4 is fixed at a first end to the central mobile 1, and at a second end to the inertial element 3.
- At least one elastic return element 4 is fixed at a first end to an inertial element 3, and at a second end to another inertial element 3.
- each elastic return element 4 is fixed at a first end to the central mobile 1, and at a second end to an inertial element 3.
- all the inertial elements 3 of the same rotary resonator 10 are arranged to pivot around a common secondary axis B.
- At least one said inertial element 3 is at least 5 times longer than wide, and at least 5 times wider than thick.
- the rotary resonator 10 comprises at least one flexible guide, to ensure the pivoting and the elastic return of at least one inertial element 3 relative to the central mobile 1.
- This flexible guidance can be achieved in different ways: flexible blades or necked blades, arranged in a crossed plane, or in parallel and crossed planes projected onto one of these parallel planes, or else arranged in an RCC (Remote Center) configuration. Compliance), that is to say with a remote center of rotation, the blades making a vee between them, or others.
- RCC Remote Center
- these flexible guides can either be attached to the central mobile 1 and / or on an inertial element 3, or be in one piece with at least one, or both.
- the monobloc executions can be in micro-machinable material, implemented by “Liga” or “Mems” process or similar, in at least partially amorphous material, in silicon and silicon oxide, in “DLC” (diamond like carbon), Or other.
- this flexible guide is a pivot with blades which are, or crossed coplanar, or crossed in projection on a projection plane perpendicular to the central axis A as in the embodiment of the figure 4 .
- This configuration has the advantage of guaranteeing excellent walking performance.
- the overall center of mass remains fixed, and that the cumulation of any parasitic displacements of the individual centers of mass of the inertial elements, during their pivoting, vanishes.
- the overall center of mass of the entire rotary resonator 10 remains fixed regardless of the amplitude. This can be obtained in particular by the combination of geometric symmetry in rotation, and by the choice of identical flexible guidance for the entire rotary resonator 10: each inertial element 3 which composes it is recalled by the same flexible guidance.
- the figure 5 shows a pivot with asymmetrical crossed blades: this flexible guide is arranged to impart to the inertial element 3 a return torque proportional to the sine of twice the pivot angle of said inertial element 3.
- This flexible guide comprises two flexible blades 31, 32, asymmetrical each joining a first recess 41, 42, of the central mobile 1 to a second recess 51, 52 of the inertial element 3. These first recesses 41, 42, define with the second recesses 51, 52, respectively two main directions DL1, DL2 blades.
- the central mobile 1 and the inertial element 3 are each more rigid than each of the flexible blades 31, 32.
- the two main directions of blades DL1, DL2, define a theoretical pivot axis D, at their crossing when these two flexible blades 31 , 32 are coplanar, or at the crossroads of their projections on the projection plane when the two flexible blades 31, 32 develop on two levels parallel to the projection plane but are not coplanar as in the case of the figure 4 , and at an angle at the top ⁇ equal to 112.5 °.
- the second 32 of these blades has, between its opposite recesses, a second total length L2 three times the first total length L1 of the first 31 of the blades.
- the distances between the first recesses 41, 42, and the theoretical pivot axis D are, for the second blade 32 a second axial distance D2 equal to 0.875 times the second total length L2, and, for the first blade 31, a first axial distance D1 equal to 0.175 times the first total length L1.
- the figure 6 shows a configuration RCC, with offset center of rotation, which is not produced in a single piece, but where the blades are angularly constrained by a small angle, in the vicinity of at least one of their ends, for example by introduction of 'A laterally offset slot relative to the theoretical blade direction.
- the flexible guidance produced by this particular RCC pivot also makes it possible to create a torque proportional to the sine of twice the angle, said flexible guidance is produced by a pivot pivot with offset center of rotation constituting a virtual pivot, the embedding of which blades 31, 32, in housings 51, 52, which comprises the central mobile 1 and / or the inertial element 3 results from an angular preload of 0.15 radian, with a torsion at the embedding, the angle at the top which form the directions of the recesses of the blades 31, 32, at the level of the virtual pivot is 52.642 °, and the distance between the virtual pivot and the nearest recess is equal to 0.268864 times the length of each of the blades 31, 32, which are identical here, between their recesses in the free state before the prestressing of their end.
- this flexible guide is thermally compensated.
- this flexible guide comprises blades of oxidized silicon, on which a differential growth of silicon dioxide during a heat treatment makes it possible to put under strong prestressing elements of smaller section, such as blades within a one-piece assembly.
- the rotary resonator 10 comprises, articulated with certain inertial elements 3, additional kinetic connecting elements 5, which constitute with these inertial elements 3 a structure articulated pantograph type, and which are arranged to increase the radial deployment of the rotary resonator 10 by limiting its height along the central axis A.
- the movement 100 comprises at least one main axis P of display by needles or discs, and the central axis A is parallel to this main axis P.
- the central axis A is this time perpendicular to the main axis P.
- the gearbox output mobile 300 is an endless screw, arranged to cooperate with a pinion which constitutes the input mobile 2.
- the rotary resonator 10 comprises only two or three inertial elements 3.
- a compromise is to be found between performance and size, and a resonator with two inertial elements in rotation symmetry ensures the required performance.
- the pivoting of the central mobile 1 is carried out on at least one magnetic pivot, so as to obtain the best efficiency.
- the invention also relates to a mechanical watch 1000 comprising at least one such movement.
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Micromachines (AREA)
- General Electrical Machinery Utilizing Piezoelectricity, Electrostriction Or Magnetostriction (AREA)
- Electromechanical Clocks (AREA)
- Electric Clocks (AREA)
Claims (25)
- Mechanisches Uhrwerk (100), umfassend mindestens eine Energiespeichereinrichtung (200), die dazu vorgesehen ist, ein Räderwerk (300) anzutreiben, von dem ein Ausgangsdrehteil so angeordnet ist, dass es um eine Antriebsachse dreht, und umfassend einen Drehresonator (10), der mindestens ein Mitteldrehteil (1), das so angeordnet ist, dass es um eine Mittelachse (A) dreht, und ein Eingangsdrehteil (2) aufweist, das so angeordnet ist, dass es mit dem Ausgangsdrehteil zusammenwirkt, wobei der Drehresonator (10) mindestens ein Trägheitselement (3) umfasst, das dazu vorgesehen ist, in Bezug auf das Mitteldrehteil (1) um eine Nebenachse (B) zu drehen, die zu der Mittelachse (A) senkrecht ist und diese schneidet, und dadurch gekennzeichnet, dass das Trägheitselement (3) durch mindestens ein elastisches Rückstellelement (4) in eine Ruheposition in Bezug auf das Mitteldrehteil (1) zurückgestellt wird, und ferner dadurch gekennzeichnet, dass die Nebenachse (B) durch den Massenschwerpunkt des ihr zugeordneten Trägheitselements (3) verläuft.
- Werk (100) nach Anspruch 1, dadurch gekennzeichnet, dass der Drehresonator (10) mehrere Trägheitselemente (3) umfasst, von denen jedes dazu vorgesehen ist, in Bezug auf das Mitteldrehteil (1) um eine Nebenachse (B) zu drehen, die zu der Mittelachse (A) senkrecht ist und diese schneidet, und von denen jedes durch mindestens ein elastisches Rückstellelement (4) in eine Ruheposition in Bezug auf das Mitteldrehteil (1) zurückgestellt wird, und ferner dadurch gekennzeichnet, dass jede Nebenachse (B) durch den Massenschwerpunkt des ihr zugeordneten Trägheitselements (3) verläuft.
- Werk (100) nach Anspruch 1 oder 2, dadurch gekennzeichnet, dass das mindestens eine elastische Rückstellelement (4) dazu vorgesehen ist, auf das Trägheitselement (3) ein Drehmoment mit elastischem Rückstellmoment gemäß der folgenden Beziehung auszuüben:
- Werk (100) nach einem der Ansprüche 1 bis 3, dadurch gekennzeichnet, dass der Drehresonator (100) in einer Ruheposition eine Rotationssymmetrie um die Mittelachse (A) der Ordnung N besitzt, wobei N größer oder gleich 2 ist.
- Werk (100) nach Anspruch 2, dadurch gekennzeichnet, dass die Trägheitselemente (3), die der Drehresonator (10) aufweist, in einer Ruheposition rotationssymmetrisch um die Mittelachse (A) der Ordnung N sind, wobei N größer oder gleich 2 ist.
- Werk (100) nach einem der Ansprüche 1 bis 5, dadurch gekennzeichnet, dass mindestens ein Trägheitselement (3) eine Rotationssymmetrie der Ordnung 2 um seine Nebenachse (B) aufweist.
- Werk (100) nach Anspruch 6, dadurch gekennzeichnet, dass jedes Trägheitselement (3) eine Rotationssymmetrie der Ordnung 2 um seine Nebenachse (B) aufweist.
- Werk (100) nach einem der Ansprüche 1 bis 7, dadurch gekennzeichnet, dass mindestens ein elastisches Rückstellelement (4) an einem ersten Ende an dem Mitteldrehteil (1) und an einem zweiten Ende an dem Trägheitselement (3) befestigt ist.
- Werk (100) nach einem der Ansprüche 1 bis 8, dadurch gekennzeichnet, dass mindestens ein elastisches Rückstellelement (4) an einem ersten Ende an einem Trägheitselement (3) befestigt ist und an einem zweiten Ende an einem anderen Trägheitselement (3) befestigt ist.
- Werk (100) nach Anspruch 8, dadurch gekennzeichnet, dass jedes elastische Rückstellelement (4) an einem ersten Ende an dem Mitteldrehteil (1) und an einem zweiten Ende an dem Trägheitselement (3) befestigt ist.
- Werk (100) nach einem der Ansprüche 1 bis 10, dadurch gekennzeichnet, dass alle Trägheitselemente (3) so angeordnet sind, dass sie um eine gemeinsame Nebenachse (B) drehen.
- Werk (100) nach einem der Ansprüche 1 bis 11, dadurch gekennzeichnet, dass mindestens ein Trägheitselement (3) mindestens 5 mal länger als breit und mindestens 5 mal breiter als dick ist.
- Werk (100) nach einem der Ansprüche 1 bis 12, dadurch gekennzeichnet, dass der Drehresonator (10) mindestens eine flexible Führung aufweist, um das Drehen und die elastische Rückstellung mindestens eines Trägheitselements (3) in Bezug auf das Mitteldrehteil (1) sicherzustellen.
- Werk (100) nach Anspruch 13, dadurch gekennzeichnet, dass die flexible Führung ein Gelenk mit Lamellen ist, die entweder koplanar gekreuzt oder in der Projektion auf eine zu der Mittelachse (A) senkrechte Projektionsebene gekreuzt sind oder ein versetztes Drehzentrum aufweisen.
- Werk (100) nach Anspruch 13 oder 14, dadurch gekennzeichnet, dass die flexible Führung so angeordnet ist, dass sie auf das Trägheitselement (3) ein zum Sinus des doppelten Drehwinkels des Trägheitselements (3) proportionales Rückstelldrehmoment ausübt.
- Werk (100) nach den Ansprüchen 14 und 15, dadurch gekennzeichnet, dass die flexible Führung zwei asymmetrisch flexible Lamellen (31; 32) umfasst, die jeweils einen ersten Einbau (41; 42) des Mitteldrehteils (1) mit einem zweiten Einbau (51; 52) des Trägheitselements (3) verbinden, wobei die ersten Einbauten (41; 42) mit den entsprechenden zweiten Einbauten (51; 52) zwei Hauptrichtungen (DL1, DL2) der Lamellen definieren, wobei das Mitteldrehteil (1) und das Trägheitselement (3) jeweils steifer sind als jedes der flexiblen Lamellen (31; 32) und die beiden Hauptrichtungen (DL1; DL2) der Lamellen eine theoretische Drehachse (D) definieren, und zwar an ihrem Schnittpunkt, wenn die beiden flexiblen Lamellen (31; 32) koplanar sind, oder am Schnittpunkt ihrer Projektion auf die Projektionsebene, wenn die beiden flexiblen Lamellen (31; 32) sich auf zwei Niveaus parallel zu der Projektionsebene erstrecken, jedoch nicht koplanar sind, und sich längs eines Winkels am Scheitelpunkt (α) gleich 112,5° erstrecken, dass die zweite (32) der Lamellen zwischen ihren gegenüberliegenden Einbauten eine zweite Gesamtlänge (L2) gleich dem Dreifachen der ersten Gesamtlänge (L1) der ersten (31) der Lamellen aufweist, und dass die Abstände zwischen den ersten Einbauten (41; 42) und der theoretischen Drehachse (D) für die zweite (32) der Lamellen ein zweiter axialer Abstand (D2) gleich dem 0,875-Fachen der zweiten Gesamtlänge (L2), und für die erste (31) der Lamellen ein erster axialer Abstand (D1) gleich dem 0,175-Fachen der ersten Gesamtlänge (L1) sind.
- Werk (100) nach Anspruch 13 oder 14, dadurch gekennzeichnet, dass die flexible Führung aus einem Lamellengelenk mit einem versetzten Drehzentrum gebildet ist, das einen virtuellen Drehpunkt bildet, dessen Einbau der Lamellen (31; 32) in Aufnahmen (51; 52), die das Mitteldrehteil (1) oder das Trägheitselement (3) aufweist, aus einer winkelförmigen Vorspannung von 0,15 Radiant resultiert, dass der Winkel am Scheitelpunkt, den die Richtungen der Einbauten der Lamellen (31; 32) auf Höhe des virtuellen Drehpunkts bilden, gleich 52,642° ist und dass der Abstand zwischen dem virtuellen Drehpunkt und dem nächsten Einbau gleich der 0,268864-fachen Länge jedes der Lamellen (31; 32) zwischen ihren Einbauten im freien Zustand vor der Vorspannung ihres Endes ist.
- Werk (100) nach einem der Ansprüche 13 bis 17, dadurch gekennzeichnet, dass die flexible Führung wärmekompensiert ist und Lamellen aus Siliciumoxid umfasst.
- Werk (100) nach einem der Ansprüche 1 bis 18, dadurch gekennzeichnet, dass der Drehresonator (10) zusätzliche kinetische Verbindungselemente (5) umfasst, die an bestimmten Trägheitselementen (3) angelenkt sind und mit den Trägheitselementen (3) eine Pantographenstruktur bilden und so angeordnet sind, dass sie die radiale Entfaltung des Drehresonators (10) durch Begrenzen seiner Höhe entlang der Mittelachse (A) erhöhen.
- Werk (100) nach einem der Ansprüche 1 bis 19, dadurch gekennzeichnet, dass das Werk (100) mindestens eine Hauptanzeigeachse (P) für Zeiger oder Scheiben umfasst und dass die Mittelachse (A) zu der Hauptachse (P) parallel ist.
- Werk (100) nach einem der Ansprüche 1 bis 20, dadurch gekennzeichnet, dass das Werk (100) mindestens eine Hauptanzeigeachse (P) für Zeiger oder Scheiben umfasst und dass die Mittelachse (A) zu der Hauptachse (P) senkrecht ist.
- Werk (100) nach einem der Ansprüche 1 bis 21, dadurch gekennzeichnet, dass das Ausgangsdrehteil des Räderwerks (300) eine Schnecke ist.
- Werk (100) nach einem der Ansprüche 1 bis 22, dadurch gekennzeichnet, dass der Drehresonator (10) nur zwei oder drei Trägheitselemente (3) umfasst.
- Werk (100) nach einem der Ansprüche 1 bis 23, dadurch gekennzeichnet, dass die Drehung des Mitteldrehteils (1) auf mindestens einem magnetischen Drehpunkt erfolgt.
- Mechanische Uhr (1000), umfassend mindestens ein Werk (100) nach einem der Ansprüche 1 bis 24.
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP17183211.6A EP3435173B1 (de) | 2017-07-26 | 2017-07-26 | Mechanisches uhrwerk mit sich drehendem isochronem resonator, der positionsunempfindlich ist |
CH00968/17A CH714019A2 (fr) | 2017-07-26 | 2017-07-26 | Mouvement mécanique d'horlogerie avec résonateur rotatif. |
JP2018133946A JP6676708B2 (ja) | 2017-07-26 | 2018-07-17 | 等時性で、姿勢に影響されない回転共振器を有する機械式ムーブメント |
US16/039,828 US10927824B2 (en) | 2017-07-26 | 2018-07-19 | Mechanical movement with rotary resonator, which is isochronous and positionally insensitive |
RU2018127092A RU2687510C1 (ru) | 2017-07-26 | 2018-07-24 | Механический часовой механизм с поворотным резонатором, являющийся изохронным и не чувствительным к расположению |
CN201810825408.0A CN109307998B (zh) | 2017-07-26 | 2018-07-25 | 具有同步且位置不敏感的旋转谐振器的机械机芯 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP17183211.6A EP3435173B1 (de) | 2017-07-26 | 2017-07-26 | Mechanisches uhrwerk mit sich drehendem isochronem resonator, der positionsunempfindlich ist |
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EP3435173A1 EP3435173A1 (de) | 2019-01-30 |
EP3435173B1 true EP3435173B1 (de) | 2020-04-29 |
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EP17183211.6A Active EP3435173B1 (de) | 2017-07-26 | 2017-07-26 | Mechanisches uhrwerk mit sich drehendem isochronem resonator, der positionsunempfindlich ist |
Country Status (6)
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US (1) | US10927824B2 (de) |
EP (1) | EP3435173B1 (de) |
JP (1) | JP6676708B2 (de) |
CN (1) | CN109307998B (de) |
CH (1) | CH714019A2 (de) |
RU (1) | RU2687510C1 (de) |
Families Citing this family (2)
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EP3812843A1 (de) | 2019-10-25 | 2021-04-28 | ETA SA Manufacture Horlogère Suisse | Flexible führung und gesamtheit von übereinander angeordneten flexiblen führungen für sich drehenden resonatormechanismus, insbesondere für uhrwerk |
EP4009113A1 (de) * | 2020-12-02 | 2022-06-08 | The Swatch Group Research and Development Ltd | Gesamtheit von flexiblen führungen für sich drehenden resonatormechanismus, insbesondere für uhrwerk |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH113025A (de) * | 1924-04-28 | 1925-12-16 | Heinrich Schieferstein Georg | Verfahren zur Steuerung eines Drehbewegungen ausführenden Mechanismus. |
CH293180A (fr) * | 1951-08-18 | 1953-09-15 | Martenet Louis | Régulateur centrifuge pour pièce d'horlogerie. |
CH421827A (de) * | 1964-07-31 | 1967-04-15 | Centre Electron Horloger | Mechanischer Resonator für Normalfrequenzoszillatoren in Zeitmessgeräten |
CH699081A2 (fr) * | 2008-07-04 | 2010-01-15 | Swatch Group Res & Dev Ltd | Résonateurs couplés pour pièce d'horlogerie. |
DE602008006057D1 (de) * | 2008-07-04 | 2011-05-19 | Swatch Group Res & Dev Ltd | Gekoppelte Resonatoren für Uhr |
CH702843B1 (fr) * | 2010-03-17 | 2014-08-29 | Complitime Sa | Mouvement pour pièce d'horlogerie à remontoir d'égalité. |
JP2015143673A (ja) * | 2013-12-27 | 2015-08-06 | セイコーインスツル株式会社 | てんぷ、ムーブメント、および時計 |
CH710115A2 (fr) * | 2014-09-09 | 2016-03-15 | Swatch Group Res & Dev Ltd | Mobile coupleur pour la synchronisation de résonateurs d'horlogerie de même fréquence. |
CH710691A2 (fr) * | 2015-02-03 | 2016-08-15 | Eta Sa Mft Horlogere Suisse | Résonateur isochrone d'horlogerie. |
EP3054357A1 (de) * | 2015-02-03 | 2016-08-10 | ETA SA Manufacture Horlogère Suisse | Oszillatormechanismus für Uhr |
CN106662839B (zh) * | 2015-02-03 | 2019-03-29 | Eta瑞士钟表制造股份有限公司 | 等时钟表谐振器 |
CH713069A2 (fr) * | 2016-10-25 | 2018-04-30 | Eta Sa Mft Horlogere Suisse | Montre mécanique avec résonateur rotatif isochrone, insensible aux positions. |
-
2017
- 2017-07-26 EP EP17183211.6A patent/EP3435173B1/de active Active
- 2017-07-26 CH CH00968/17A patent/CH714019A2/fr unknown
-
2018
- 2018-07-17 JP JP2018133946A patent/JP6676708B2/ja active Active
- 2018-07-19 US US16/039,828 patent/US10927824B2/en active Active
- 2018-07-24 RU RU2018127092A patent/RU2687510C1/ru active
- 2018-07-25 CN CN201810825408.0A patent/CN109307998B/zh active Active
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Also Published As
Publication number | Publication date |
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EP3435173A1 (de) | 2019-01-30 |
US10927824B2 (en) | 2021-02-23 |
JP6676708B2 (ja) | 2020-04-08 |
CN109307998B (zh) | 2020-09-15 |
RU2687510C1 (ru) | 2019-05-14 |
US20190032644A1 (en) | 2019-01-31 |
CN109307998A (zh) | 2019-02-05 |
JP2019039908A (ja) | 2019-03-14 |
CH714019A2 (fr) | 2019-01-31 |
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