HK40011137B - Rotary resonator with a flexible guide system based on a detached lever escapement - Google Patents

Description

Rotary resonator with compliant bearing maintained by free-form escapement

Technical Field

The invention concerns a timepiece regulating mechanism comprising a resonator mechanism with a quality factor Q arranged on a plate and an escapement mechanism subjected to the torque of a drive comprised by the movement, said resonator mechanism comprising an inertial element arranged to oscillate with respect to said plate, said inertial element being subjected to the action of an elastic return means fixed directly or indirectly to said plate, and said inertial element being arranged to cooperate with an escape wheel set comprised by said escapement mechanism.

The invention also relates to a timepiece movement including drive means and such a regulating mechanism, the escapement of which is subjected to the torque of these drive means.

The invention also relates to a watch, in particular a mechanical watch, comprising such a movement and/or such a regulating mechanism.

The present invention relates to the field of timepiece regulating mechanisms, in particular for watches.

Background

Most mechanical watches include a balance/balance spring type oscillator cooperating with a swiss lever escapement. The balance/hairspring device forms the time base of the watch. This is referred to herein as a resonator. The escapement performs two main functions, namely, maintaining the reciprocating motion of the resonator and counting these reciprocating motions. The escapement must be robust, not interfere with the balance far from its balance point, resist shocks, avoid jamming the movement (for example in the case of excessive inclinations), and thus form an important component of the timepiece movement.

Typically, the balance/balance spring device oscillates with an amplitude of 300 ° and a lead angle of 50 °. The lead angle is the angle through which the balance travels when the lever fork interacts with the impulse pin (also called a tumbler pin) of the balance. In most existing swiss lever escapements, the rise angle is divided on either side of the balance point (+/-25 °) and the lever is tilted +/-7 °.

Swiss lever escapements belong to the class of free escapements, since beyond a half-lift angle the resonator no longer contacts the lever. This feature is critical to achieving good timing performance.

The mechanical resonator includes an inertial element, a guide member, and a resilient return element. Typically, the balance forms an inertial element and the balance spring forms an elastic return element. The balance is guided in rotation by a pivot rotating in a smooth ruby bearing. The associated friction results in energy loss and travel time difference damage. It is desirable to seek to eliminate these disruptions, which, in addition, depend on the orientation of the watch in the gravitational field. The loss is characterized by the quality factor Q of the resonator. It is also generally sought to maximize the quality factor Q in order to obtain the best possible power reserve. Obviously, the guide member is an important factor of the loss.

Using a rotating flexible bearing instead of a pivot and a traditional balance spring is a solution to maximize the quality factor Q. Flexible strip resonators have promising timing properties in the case of their very good design, independent of orientation in the gravitational field, and have a high quality factor, in particular due to the absence of pivot friction. Furthermore, the use of compliant bearings eliminates the problem of pivot wear.

However, the flex-band typically used for such a rotary flexible bearing is stiffer than the balance spring. This results in operation at higher frequencies, e.g. about 20Hz, and with lower amplitudes, e.g. 10 ° to 20 °. At first sight this seems incompatible with swiss lever escapements.

The working amplitude compatible with resonators with a rotary flexible bearing, in particular with resonators with a rotary flexible bearing comprising strips, is typically 6 ° to 15 °. This results in the lift angle having to be twice the minimum working amplitude.

Without special precautions, an escapement with a small lift may have a moderate efficiency and result in a loss rate that is too large. However, the combination of high frequency and low amplitude makes the speed of movement of the balance acceptable and not too high, so that the efficiency of the escapement does not automatically become moderate.

The resonator must be of acceptable dimensions, compatible with being housed inside the timepiece movement. To date, it has not been possible to manufacture a rotating flexible bearing of very large diameter or with several pairs of strip levels, which theoretically would allow oscillation amplitudes of the inertial elements of tens of degrees by placing successive flexible bearings in series: therefore, a flexible bearing with one or two levels of tape should be used, as is known for example from european patent No.3035126 in the name of THE SWATCH GROUP RESEARCH AND DEVELOPMENT Ltd.

In short, the effect of choosing a rotating flexible bearing is that the amplitude of the balance is reduced and it is no longer possible to use a traditional swiss lever escapement, which requires the balance to have an amplitude much higher than half the lift angle, i.e. higher than 25 °. Thus, a governor comprising a resonator with a flexible bearing requires a specific escapement mechanism of a different size than a conventional swiss lever escapement designed to work with the same inertial element of the resonator.

Disclosure of Invention

The general object of the present invention is to increase the power reserve and accuracy of current mechanical watches. To achieve this, the invention combines a resonator with a rotationally compliant bearing with a lever escapement optimized to maintain acceptable dynamic losses and limit the timing effect of the unlocking phase.

Without the teaching in the prior art regarding the dimensioning of both the resonator and the escapement, analytical model calculations and a series of simulations have revealed parameters of the resonator and the escapement that are compatible with acceptable losses and acceptable efficiencies.

These calculations and simulations show that the ratio of the inertia of the inertial element, in particular of the balance, to the inertia of the escapement lever is decisive.

To this end, the invention relates to a governor mechanism according to claim 1.

These resonators with rotating flexible bearings have a very high quality factor, for example of the order of 3000, compared to the quality factor of 200 of a normal watch. The dynamic losses (kinetic energy from the escape wheel and lever at the end of the impulse) are independent of the quality factor. These losses can therefore become too high with a high quality factor, relatively speaking, compared to the energy transferred to the balance.

For the correct operation of the mechanism, the striker pin integral with the inertial element must be inserted into the opening of the lever fork to a certain value, called "depth". Moreover, in order to ensure safety during the unlocking phase, once the striker pin is unlocked, it must be able to maintain a certain distance, called safety distance, from the horn of the fork head, which is opposite to the one it was in contact with before the striker pin was unlocked.

The invention therefore also aims to impose a specific relationship between the dimensions, depth and safety distance values of the lever fork and the lift angle values of the lever and the inertia element, according to claim 4, to ensure that the striker pin is correctly removed from the fork once the travel through the half lift angle is completed.

The invention also relates to a timepiece movement including drive means and such a regulating mechanism, the escapement of which is subjected to the torque of these drive means.

The invention also relates to a watch, in particular a mechanical watch, comprising such a movement and/or such a regulating mechanism.

Drawings

Other features and advantages of the present invention will become apparent upon reading the following detailed description and upon reference to the drawings in which:

figure 1 comprises a hyperbola including, on the same abscissa, the ratio between the inertia of the inertial element of the resonator and the inertia of the lever, and on the ordinate, for a particular exemplary mechanism, on the one hand the efficiency of the governor in% in the positive part of the upper graph and the loss rate in seconds/day in the negative part of the lower graph; the upper and lower graphs are plotted for the same given escapement geometry with a particular value of quality factor, lever lift angle and working amplitude.

Fig. 2 represents a schematic partial perspective view of a timepiece movement in which the plate carries a regulating mechanism according to the invention comprising a resonator with a flexible bearing having two flexible strips arranged on two parallel levels and whose projections intersect, the resonator being fixed to the plate by means of an elastic element, the resonator comprising an extended inertial element shaped like the letter ω, the central part of which is carried by the two flexible strips and carries an impulse pin arranged to cooperate with a symmetrical lever (not shown by means of the pivoting of the latter on the plate by means of a metal arbour), which in turn cooperates with a conventional escape wheel.

Figure 3 shows a plan view of the governor mechanism of figure 2 arranged on the plate of the movement.

Figure 4 shows a plan view of a detail of the governor mechanism of figure 2.

Fig. 5 shows a partially exploded perspective view of the governor mechanism of fig. 2.

Figure 6 represents a plan view of a detail of the area of engagement between the striker pin of the inertial element of the resonator and the lever fork shown in the stop position on the stop pin.

Fig. 7 shows a plan view of the lever of the mechanism of fig. 2 shaped like the corner of a watt cow (Watusi cat).

Figure 8 shows a plan view of the flexible bearing of the mechanism of figure 2.

Figure 9 represents a plan view of a particular embodiment of a level of flexible bearings of the mechanism of figure 2.

Fig. 10 shows a side view of the governor mechanism of fig. 2.

Fig. 11 shows a detail of the governor mechanism of fig. 2 in a perspective view, showing the damper stop on its deck.

Figures 12 to 14 are graphs comprising, on the abscissa, the moment applied to the escape wheel set and, on the ordinate, the amplitude measured in degrees in figure 12, the loss measured in seconds/day in figure 13 and the efficiency of the speed regulator measured in% in figure 14, respectively.

Figure 15 is a block diagram representing a watch comprising a movement with a drive and a regulating mechanism according to the invention.

Detailed Description

The invention combines a resonator with a rotary compliant bearing to increase power reserve and accuracy with an optimized lever escapement to maintain acceptable dynamic losses and limit the timing effect of the unlocking phase.

The invention therefore concerns a timepiece regulating mechanism 300, the timepiece regulating mechanism 300 comprising a resonator mechanism 100 and an escapement mechanism 200 arranged on a plate 1, the resonator mechanism 100 having a quality factor Q, the escapement mechanism 200 being subjected to the torque of a drive 400 comprised by a movement 500.

The resonator mechanism 100 comprises an inertial element 2, the inertial element 2 being arranged to oscillate with respect to the plate 1. The inertia element 2 is subjected to the action of elastic return means 3 fixed directly or indirectly to the plate 1. The inertial element 2 is arranged to cooperate indirectly with an escape wheel set 4, in particular an escape wheel, comprised in the escapement 200 and pivoting about an escapement axis DE.

According to the invention, the resonator mechanism 100 is a resonator with a virtual pivot rotating about the main axis DP, the resonator mechanism 100 having a flexible bearing comprising at least two flexible strips 5 and comprising an impact pin 6 integral with the inertial element 2. Escapement 200 comprises a lever 7, this lever 7 pivoting about a secondary axis DS and comprising a lever fork 8, lever fork 8 being arranged to cooperate with impulse pin 6, so this escapement 200 is a free escapement in which, during its working cycle, resonator mechanism 100 has at least one free phase in which impulse pin 6 is at a distance from lever fork 8. The resonator has a lead angle β of less than 10 °, during which the striker pin 6 is in contact with the lever fork 8.

The efficiency and losses of such escapements can be evaluated by multibody dynamics simulations (i.e. involving a set of several components, each assigned a specific mass and distribution of inertia) for a specific escapement geometry and a specific operating amplitude, in particular 8 °, according to the ratio of the inertia of the inertial element to the inertia of the lever, which cannot be determined using standard kinematic simulations. As shown in fig. 1, it can be observed that, under simulated conditions, there is a threshold of good efficiency higher than 35% and a threshold of low loss of less than 8 seconds per day, in which the inertia of the inertial element, in particular of the balance, is 10000 times that of the lever.

Thus, an analytical model of the system shows that if it is desired to limit the dynamic losses, the specific conditions will be the inertia of the lever, the inertia of the inertial element, the resonator quality factor, and the lever and inertiaThe lift angles of the elements are related to: with regard to the dynamic loss coefficient, on the one hand, the inertias I of all the inertial elements 2 with respect to the main axis DP_BAnd on the other hand the inertia I of the lever 7 with respect to the secondary axis DS_AIs such that the ratio I_B/I_AGreater than 2 Q. α²/(·π·β²) Where α is the lead angle of the lever, which corresponds to the maximum angular travel of lever fork 8.

More specifically, if it is desired to limit the dynamic losses by a factor of 10%, on the one hand the inertia I of the inertial element 2 with respect to the main axis DP_BAnd on the other hand the inertia I of the lever 7 with respect to the secondary axis DS_AThis is: ratio I_B/I_AGreater than 2 Q. α²/(0.1·π·β²) Where α is the lead angle of the lever, which corresponds to the maximum angular travel of lever fork 8.

More specifically, the lift angle β of the resonator is the whole angle taken from both sides of the rest position, which is less than twice the amplitude angle of the inertial element 2 when it is furthest away from the rest position in only one direction of motion.

More specifically, the amplitude angle at which the inertial element 2 deviates furthest from the rest position is between 5 ° and 40 °.

More specifically, during each oscillation, impact pin 6 is inserted into lever fork 8 with a travel depth P greater than 100 microns during the contact phase, and impact pin 6 is kept at a safety distance S greater than 25 microns from lever fork 8 during the unlocking phase.

The strike pin 6 and the lever fork 8 are dimensioned such that the width L of the lever fork 8 is greater than (P + S)/sin (α/2+ β/2), the stroke depth P and the safety distance S being measured radially with respect to the main axis DP.

The useful width L1 of the striker pin 6 shown in fig. 6 is slightly less than the width L of the lever fork 8, more specifically less than or equal to 98% of L. The striker pin 6 is advantageously tapered behind its useful width surface L1, and in particular it may have a prismatic shape with a triangular cross-section as shown in the figures or the like.

Thus, by design, the present invention defines a new strike pin/prong layout having very special features where the horns of the prongs are farther apart and the pin is wider than in known types of swiss lever mechanisms having a normal lift angle of 50 °.

Thus, by considerably enlarging the lever fork compared to usual proportions, it is also possible to design a swiss lever escapement with a very small lift angle (for example of the order of 10 °).

More specifically, this lever 7 is in the form of a single-layer stage made of silicon, mounted on a metal spindle that pivots with respect to the plate 1.

More specifically, escape wheel set 4 is a silicon escape wheel.

More specifically, escape wheel set 4 is an escape wheel perforated with holes to minimize its inertia with respect to its pivot axis DE.

More specifically, the lever 7 is perforated so as to have its inertia I with respect to the secondary axis DS_AAnd (4) minimizing.

Preferably, the lever 7 is symmetrical about the secondary axis DS, so as to avoid any unbalance and to avoid the generation of undesirable moments in the case of linear shocks.

Fig. 7 shows two horns 81 and 82 arranged to cooperate with impulse pin 6, pallet stones 72 and 73 arranged to cooperate with the teeth of escape wheel set 4, and horn element 80 and pallet stone element 70 whose sole function is to achieve perfect balance.

More specifically, the maximum dimension of the inertial element 2 is greater than half the maximum dimension of the plate 1.

More specifically, the main axis DP, the secondary axis DS and the pivot axis of the escape wheel set 4 are arranged centered at a right angle, the vertex of which is on the secondary axis DS.

More specifically, the flexible bearing comprises two flexible strips 5, the projections of which 5 on a plane perpendicular to the main axis DP intersect at a virtual pivot defining the main axis DP and are located on two parallel and distinct levels. Still more specifically, the projections of the two flexible strips 5 on a plane perpendicular to the main axis DP form an angle comprised between 59.5 ° and 69.5 °, and the two flexible strips 5 intersect at between 10.75% and 14.75% of their length, so that the resonator mechanism 100 has an intentional isochronous error which is the additive inverse of the loss error of the escapement movement of the escapement mechanism 200.

The resonator therefore has a non-isochronous curve which compensates for the losses caused by the escapement. This means that the free resonator is designed to have an isochronous error, which is the additive inverse of the error caused by the lever escapement. The design of the resonator thus compensates for losses at the escapement.

More specifically, the two flexible strips 5 are identical and symmetrically positioned. Still more specifically, each flexible strip 5 forms part of a unitary assembly 50, each flexible strip 5 being integral with its first alignment structure 52A, 52B and with an attachment structure 54 attached to the plate 1 or, advantageously as shown in fig. 10, to an intermediate elastic suspension strip 9, the intermediate elastic suspension strip 9 being attached to the plate 1 and arranged to allow the displacement of the flexible bearing and of the inertial element 2 in the direction of the main axis DP.

In the non-limiting variation shown in the figures, the first alignment structure is a first V-shaped portion 52A and a first flat portion 52B, and the first attachment structure includes at least one first aperture 54. The first bead 53 presses against the first attachment structure. Moreover, the integral assembly 50 comprises a second alignment structure for attaching it to the inertia element 2, the second alignment structure being a second V-shaped portion 56A and a second flat portion 56B, and the second attachment structure comprising at least one second hole 58. The second bead 57 presses against the second attachment structure.

The flexible bearing 3 with crossed strips 5 is advantageously formed by two identical integral assemblies 50 made of silicon, assembled symmetrically to form the crossings of the strips and precisely aligned with each other by means of integrated alignment structures and auxiliary means, not shown in the figures, such as pins and screws.

Thus, more specifically, at least the resonator mechanism 100 is attached on an intermediate elastic suspension strip 9, which intermediate elastic suspension strip 9 is attached to the machine plate 1 and arranged to allow displacement of the resonator mechanism 100 in the direction of the main axis DP, and the machine plate 1 comprises at least one shock absorber stop 11, 12 at least in the direction of the main axis DP, and preferably at least two such shock absorber stops 11, 12, the shock absorber stops 11, 12 being arranged to cooperate with a rigid element of the inertia element 2, such as a flange 21 or 22 added during assembly of the inertia element on the flexible bearing 3 comprising the strip 5.

The elastic suspension strips 9 or similar means allow the entire resonator 100 to be displaced substantially in the direction defined by the virtual axis of rotation DP of the bearing. The purpose of the device is to avoid the breakage of the strip 5 in the event of a transverse shock in the direction DP.

Fig. 11 shows the damper stop limiting the travel of the inertia element 2 in three directions in the event of a shock, but the damper stop is positioned at a sufficient distance so that the inertia element does not contact the stop under the influence of gravity. For example, flange 21 or 22 includes a bore 211 and a face 212 that are capable of mating with a trunnion 121 in a shock absorber stop arrangement and a complementary surface 122 on stop 21 or 22, respectively.

More specifically, the inertial member 2 includes an inertial mass 20 for adjusting the travel time difference and the unbalance.

More specifically, the striker pin 6 is integral with the flexible strip 5 or, more specifically, with the integral assembly 50 as shown.

More specifically, lever 7 comprises a bearing surface arranged to cooperate in abutment with a tooth comprised by escape wheel set 4 and limit the angular travel of lever 7. These bearing surfaces limit the angular travel of the lever, as do the solid stop members. The angular travel of the lever 78 may also be limited in a conventional manner by a stop pin 700.

More specifically, the flexible bearing 3 is made of silicon, which is oxidized to compensate for the influence of temperature on the travel time difference of the governor mechanism 300.

The invention also relates to a timepiece movement 500 comprising a driving device 400 and such a regulating mechanism 300, the escapement mechanism 200 of the regulating mechanism 300 being subjected to the moments of these driving devices 400.

The graphs of fig. 12 to 14 list a series of simulation results, where Q2000, I_B＝26550mg·mm²The frequency is 20Hz, the escape wheel set has 20 teeth, more specifically the lift α of the lever is 14 ° and the lift β of the resonator is 10 °.

The invention also relates to a watch 1000, in particular a mechanical watch, comprising such a movement 500 and/or such a regulating mechanism 300.

In short, the invention makes it possible to increase the power reserve and the accuracy of current mechanical watches. For a given movement size, the autonomy of the watch can be increased by a factor of four, and the speed governing capacity of the watch can be doubled. This means that the present invention provides a gain of 8 times in terms of core performance.

Claims (22)

1. Timepiece governing mechanism (300) comprising a resonator mechanism (100) and an escapement mechanism (200) arranged on a plate (1), the resonator mechanism (100) having a quality factor Q, the escapement mechanism (200) being subjected to the moments of a drive means (400) comprised by a timepiece movement (500), the resonator mechanism (100) comprising an inertial element (2) arranged to oscillate with respect to the plate (1), the inertial element (2) being subjected to the action of an elastic return means (3) attached directly or indirectly to the plate (1), and the inertial element (2) being arranged to cooperate indirectly with an escapement wheel set (4) comprised by the escapement mechanism (200), characterized in that the resonator mechanism (100) is a resonator having a virtual pivot rotating about a main axis (DP), the resonator mechanism (100) having a flexible bearing comprising at least two flexible strips (5), and comprising an impact pin (6) integral with said inertial element (2); -the escapement mechanism (200) comprises a lever (7), said lever (7) pivoting about a secondary axis (DS) and comprising a lever fork (8), said lever fork (8) being arranged in cooperation with the impulse pin (6), and-the escapement mechanism (200) is a free escapement mechanism, wherein, during a working cycle, the resonator mechanism (100) has at least one free phase in which the impulse pin (6) is at a distance from the lever fork (8); the resonator has a lead angle beta of less than 10 DEG, during which the striker pin (6) is in contact with the lever fork (8),

wherein, on the one hand, the inertia element (2)Inertia I relative to the main axis (DP)_BAnd on the other hand the inertia I of the lever (7) relative to the secondary axis (DS)_AThis is: ratio I_B/I_AGreater than 2 Q. α²/(0.1·π·β²) Wherein α is the lead angle of the lever and α corresponds to the maximum angular travel of the lever fork (8).

2. The timepiece movement mechanism (300) according to claim 1, wherein the lift angle β of the resonator is less than twice the amplitude angle of the inertial element (2) when it is furthest away from a rest position in only one direction of movement.

3. Timepiece regulating mechanism (300) according to claim 1, characterized in that the amplitude angle at which the inertial element (2) deviates furthest from the rest position is between 5 ° and 40 °.

4. Timepiece movement mechanism (300) according to claim 1, wherein during each oscillation, during a contact phase the strike pin (6) is inserted into the lever fork (8) with a travel depth P greater than 100 microns, and during an unlocking phase the strike pin (6) is kept at a safety distance S greater than 25 microns from the lever fork (8), and the strike pin (6) and the lever fork (8) are dimensioned so that the width L of the lever fork (8) is greater than (P + S)/sin (α/2+ β/2), the travel depth P and the safety distance S being measured radially with respect to the main axis (DP).

5. Timepiece movement mechanism (300) according to claim 1, characterised in that the lever (7) is in the form of a single-layer stage made of silicon and is mounted on a metal spindle that pivots with respect to the plate (1).

6. Timepiece regulating mechanism (300) according to claim 1, characterized in that the escape wheel set (4) is a silicon escape wheel.

7. Timepiece regulating mechanism (300) according to claim 1, wherein the escape wheel set (4) is an escape wheel perforated with holes to minimize its inertia with respect to its pivot axis.

8. Timepiece regulating mechanism (300) according to claim 1, wherein the lever (7) is perforated so as to have its inertia (I) with respect to the minor axis (DS)_A) And (4) minimizing.

9. Timepiece regulating mechanism (300) according to claim 1, characterized in that the lever (7) is symmetrical about the secondary axis (DS).

10. Timepiece regulating mechanism (300) according to claim 1, characterised in that the maximum dimension of the inertial element (2) is greater than half the maximum dimension of the plate (1).

11. Timepiece regulating mechanism (300) according to claim 1, wherein the main axis (DP), the secondary axis (DS) and the pivot axis (DE) of the escape wheel set (4) are arranged centered at a right angle, the vertex of which is on the secondary axis (DS).

12. Timepiece regulating mechanism (300) according to claim 1, wherein the flexible bearing comprises two flexible strips (5), the projections of the two flexible strips (5) on a plane perpendicular to the main axis (DP) intersecting at the virtual pivot defining the main axis (DP), and the two flexible strips (5) being located on two parallel and different levels.

13. The timepiece movement mechanism (300) according to claim 12, wherein the projections of the two flexible strips (5) on a plane perpendicular to the main axis (DP) form an angle between 59.5 ° and 69.5 °, and the two flexible strips (5) intersect at between 10.75% and 14.75% of their length, so that the resonator mechanism (100) has an intentional isochronous error which is the additive inverse of the loss error of the escapement movement of the escapement mechanism (200).

14. Timepiece regulating mechanism (300) according to claim 12, characterized in that the two flexible strips (5) are identical and symmetrically positioned.

15. Timepiece movement mechanism (300) according to claim 12, wherein each flexible strap (5) forms part of a unitary assembly (50) and is integral with a structure for aligning and attaching each flexible strap (5) on the plate (1) or an intermediate elastic suspension strap (9), the intermediate elastic suspension strap (9) being attached on the plate (1) and arranged to allow the displacement of the flexible bearing and the inertial element (2) in the direction of the main axis (DP).

16. Timepiece movement mechanism (300) according to claim 1, characterised in that at least the resonator mechanism (100) is attached on an intermediate elastic suspension strap (9), the intermediate elastic suspension strap (9) being attached on the plate (1) and arranged to allow displacement of the resonator mechanism (100) in the direction of the main axis (DP), and the plate (1) comprises at least one damper stop (11, 12) at least in the direction of the main axis (DP), the damper stop (11, 12) being arranged to cooperate with a rigid element of the inertia element (2).

17. Timepiece regulating mechanism (300) according to claim 1, characterised in that the inertial element (2) comprises an inertial mass for regulating travel time differences and imbalances.

18. Timepiece regulating mechanism (300) according to claim 1, characterized in that the strike pin (6) is integral with the flexible strip (5).

19. Timepiece regulating mechanism (300) according to claim 1, wherein the lever (7) comprises a bearing surface arranged to engage in abutment with a tooth comprised by the escape wheel set (4) and limit the angular travel of the lever (7).

20. The timepiece movement (300) of claim 1, wherein the compliant bearing is made of oxidized silicon to compensate for the effects of temperature on travel time differences of the timepiece movement (300).

21. A timepiece movement (500) comprising a drive device (400) and a timepiece regulating mechanism (300) according to claim 1, wherein the escapement mechanism (200) withstands the torque of the drive device (400).

22. A watch (1000) comprising a timepiece movement (500) according to claim 21 and/or a timepiece regulating mechanism (300) according to claim 1.