The invention relates to an elastic retaining member for fixing a timepiece component on a support element.
The invention also relates to an elastic retaining member-timepiece component assembly and an assemblage of such an assembly with the support element.
The invention also relates to a method for performing such an assemblage.
The invention, in addition, relates to a horological movement comprising at least one such assemblage.
Finally, the invention relates to a timepiece comprising such a movement.
In the prior art, elastic retaining members such as timepiece collets which participate in assembling balance-springs on balance shafts in a horological movement by means of elastic clamping, are known.
However, such elastic retaining members have the major disadvantage of imposing, in the context of performing such assemblages, complex, long and expensive mounting operations due to the fact that these members have holding torques on these balance shafts which are low and limited.
The purpose of the present invention is to overcome all or part of the disadvantages mentioned above by proposing an elastic retaining member which has a high holding torque, in particular to facilitate/simplify the mounting operations of an assemblage of an elastic retaining member-timepiece component assembly with a support element as well as to ensure sufficient hold to ensure that it is retained in position in the plane and to guarantee its angular position during the life of the component.
To this end, the invention relates to an elastic retaining member for fixing a timepiece component on a support element, comprising an opening into which said support element can be inserted, the retaining member comprising rigid arms and elastic arms defined between connection areas 9 of the member 1, these arms contributing to ensure elastic clamping of the support element in the opening, each rigid arm being provided with a single flat contact area of the retaining member able to cooperate with a corresponding convex contact portion of the support element.
Thus, thanks to these features, the elastic retaining member is then able to withstand a significant elastic clamping and therefore to store a large amount of elastic energy when it is constrained in order to restore a large holding torque, in particular thanks to a high rigidity of this elastic retaining member induced in particular by significant volumes (or amounts) of material constituting its rigid arms which comprise the inner and outer structures. It should be noted that these large volumes of material are more precisely comprised in the contact areas which are placed under loads (or under stress) during the insertion of the support element into this retaining member.
In addition, it will be noted that this elastic retaining member is configured so that this storage of elastic energy leads to stresses which remain admissible with regard to the material which constitutes such a retaining member such as silicon. Indeed, the contact areas 8 have a flat surface which thus allows them to achieve with the contact portions a piano-convex-type contact configuration, thus contributing to avoid/prevent any damage to the retaining member 1 by the appearance of fractures or else cracks.
In other embodiments:
The invention also relates to an elastic retaining member-timepiece component assembly for a horological movement of a timepiece comprising such a retaining member.
In particular, the assembly is made in one piece.
The invention also relates to an assemblage for a horological movement of a timepiece comprising an elastic retaining member timepiece component assembly, said assembly being fixed to a support element.
The invention further relates to a horological movement comprising at least one such assemblage.
The invention also relates to a timepiece comprising such a horological movement.
The invention also relates to a method for performing an assemblage of an elastic retaining member timepiece component assembly with a support element according to the preceding claim, comprising:
Other features and advantages will emerge clearly from the description which is given below, in an indicative and non-limiting manner, with reference to the appended drawings, wherein:
In this embodiment, this retaining member 1 can be comprised in an elastic retaining member—timepiece component assembly 120 visible in
It will be noted that in a variant of this assembly, only the elastic retaining member 1 can be made of such a material called “fragile” material, the timepiece component 2 then being made of another material.
This assembly 120 can belong an assemblage 130 for the horological movement 110, by being fixed to the support element 3, for example by elastic clamping. It will be noted that this assemblage 130 was designed for applications in the watchmaking field. However, the invention can perfectly be implemented in other fields such as aeronautics, jewellery, or else automotive.
Such a retaining member 1 comprises an upper face and a lower face 12 which are preferably flat, respectively comprised in first and second planes P1 and P2 visible in
This retaining member 1 comprises the rigid arms 6 and elastic arms 7 connecting the outer and inner structures 4a, 4b to one another. It will be noted that this retaining member 1 comprises as many rigid arms 6 as there are elastic arms 7. The rigid arms 6 are here undeformable or almost undeformable and act as elements for stiffening the retaining member 1. Regarding the elastic arms 7, they are able to deform mainly in tension but also in torsion. These rigid arms 6 and these elastic arms 7 are defined or else distributed successively and alternately in this retaining member 1. In other words, these rigid arms 6 are connected to each other by said elastic arms 7. More specifically, each elastic arm 7 is connected at its two opposite ends at connection areas 9 to two different rigid arms 6. Such rigid and elastic arms 6, 7 comprise, in a non-limiting and non-exhaustive manner:
It will be noted that the inner faces of the elastic arms 7 are essentially flat and the inner faces of the rigid arms 6 are non-flat, for example being of convex shape. In the present embodiment, the convex inner face of each rigid arm 6 therefore comprises the flat contact area 8. This contact area 8 is able to cooperate with the corresponding contact portion 10 of the support element 3. Such a contact area 8 is defined in the inner face by extending substantially over all or part of the thickness of the retaining member 1. In addition, this contact area 8 is flat, comprising a surface which is entirely or partly flat. It will be noted that the contact areas 8 of the rigid arms 6 are provided in particular to cooperate with the contact portions 10 according to a plano-convex-type contact configuration in which configuration where the flat surface of each contact area 8 cooperates with the convex shaped contact portion 10 of the support element 3. It should be noted here that this convex shape of each contact portion 10 is assessed relative to the flat surface of each corresponding contact area 8 opposite to which this portion 10 is arranged. It will be noted that the flat surface of the contact area 8 forms a plane tangent to the diameter of the support element. In other words, the flat surface is perpendicular to the diameter and therefore to the radius R1 of the support element.
In this configuration, the presence of this flat contact area 8 in the inner face of each rigid arm 6 allows a contact pressure to be performed between the retaining member 1 and the support element 3 during the production of a mechanical connection between them, while significantly reducing the intensity of the stresses at this contact areas 8 and the corresponding contact portion 10 of the support element 3 during the assemblage and/or the fixing of this retaining member 1 with the support element 3, which stresses are liable to damage the retaining member 1 by the appearance of fractures/breaks or else cracks.
In the prior art, this contact pressure is estimated from the Hertz pressure equation conventionally but not exclusively implemented for determining a contact pressure between cylindrical or spherical parts having different diameters or radii of curvature. In the present case, this Hertz pressure is defined according to the following equation:
With:
In the present embodiment, the contact area 8 of each rigid arm 6 is flat and therefore does not have a radius of curvature R2. Such a contact area 8 is able to cooperate with the corresponding contact portion 10 of the support element 3 in the plano-convex-type contact configuration.
Thus, in such a contact configuration, the contact pressure defined by the Hertz pressure equation is less than that relating to convex-convex-type contact configurations during which the contact area 8 which then has a radius of curvature R2 is able to cooperate with the corresponding contact portion 10 of the support element 3. This contact pressure present during the plano-convex-type contact configuration is less than those implemented during the other configurations described above in particular because of the higher value in this context of the relative radius of curvature R resulting from the absence of a radius of curvature for each flat contact area 8 of the retaining member 1 of the present embodiment.
In the plano-convex-type contact configuration where the contact area 8 of each rigid arm 6 is able to cooperate with the corresponding contact portion 10 of the support element 3, the contact pressure is less than those of these other contact configurations of at least 25%.
In this embodiment, the rigid and elastic arms 6, 7 connect the outer and inner structures 4a, 4b to one another, each further comprising a portion of these outer and inner structures 4a, 4b. In this retaining member 1, these rigid and elastic arms 6, 7 essentially allow an elastic clamping-type fixing of the support element 3 to be achieved in the opening 5 made in this retaining member 1 which is defined by the inner structure 4b and in particular by the inner peripheral wall of this retaining member 1.
As seen above, these rigid arms 6 therefore comprise the only contact areas 8 of the retaining member 1 with the support element 3 which can be defined in all or part of the inner faces of these rigid arms 6. The contact area 8 of each rigid arm 6, otherwise called “contact interface”, is provided to cooperate with a peripheral wall 13 of the connecting portion of the support element 3 in particular with the corresponding contact portion 10 defined in this peripheral wall 13 of the support element 3. In this context, the retaining member 1 then comprises three contact areas 8 which participate in achieving a precise centring of the timepiece component 2, for example a balance-spring, in the horological movement 110.
With reference to
It is therefore understood here that each elastic arm 7 has a cross section which is less than a cross section of each rigid arm 6. In other words, the cross section of each elastic arm 7 has an area which is less than an area of the cross section of each rigid arm 6. It will be noted that the cross section of the elastic arm 7 is constant or substantially constant throughout the body of this elastic arm 7 while the cross section of the rigid arm 6 is inconstant/variable throughout the body of this rigid arm 6. In addition, it will be noted that:
Such a configuration of the rigid and elastic arms 6, 7 allows the retaining member 1 to store a greater amount of elastic energy for the same clamping compared to the retaining members of the prior art. Such an amount of elastic energy stored in the retaining member 1 then allows a greater holding torque of the retaining member to be obtained on the support element 3 in the assemblage 130 of the retaining member-timepiece component assembly 120 with this support element 3. In addition, it should be noted that such a configuration of the retaining member 1 allows elastic energy ratios which are 6 to 8 times greater than those of the retaining members of the prior art to be stored.
It will be noted that the arrangement of the rigid and elastic arms 6, 7 in the retaining member 1 allows, during insertion with clamping, a deformation of each elastic arm 7 allowing the deformation of the whole retaining member 1 to be accommodated with the geometry of the connecting portion of the support element 3 on which it is assembled. In addition, the mode of deformation undergone by each elastic arm is a toroidal torsion coupled with a radial expansion.
With reference to
As previously mentioned, this elastic deformation of the retaining member 1 results from the application of the contact force on the contact areas 8 of the rigid arms 6 by the contact portions 10 of the peripheral wall 13 of the support element 3. Such a deformation sub-step 14 comprises a phase of displacing 15 the rigid arms 6 under the action of the contact force which is applied thereto. Such a displacement of the rigid arms 6 is performed in a direction between a radial direction B1 relative to a central axis C common to the support element 3 and to the retaining member 1, and a direction B2 coincident with this central axis C. It will be noted that this direction B2 is perpendicular to the direction B1 and is oriented in a direction defined from the lower face 12 towards the upper face. The contact force is preferably perpendicular or substantially perpendicular to said contact area 8. During the course of this phase 12, the rigid arms 6 thus displacing under the action of this contact force, generate a double elastic deformation of the elastic arms 7.
A first deformation otherwise called “torsional elastic deformation” of these elastic arms 7. During this torsional deformation, each elastic arm 7 is driven at its two ends in the same direction of rotation B4 by the displacing rigid arms 6, to which arm 6 such ends are connected. It will be noted that only a portion of the body of these elastic arms 7 is torsion-deformable, here the ends of these arms 7. Such a first deformation contributes in particular to improving the insertion of the support element 3 into the opening 5 of the retaining member 1 by participating in preventing any fracture of the retaining member 1 and/or any appearance of a crack in this member 1 when assembled with the support element 3.
A second deformation otherwise called “tensile deformation” or else “extensional elastic deformation” of the elastic arms 7. During this extensional deformation, each elastic arm 7 is pulled at its two ends in the longitudinal direction B3 in opposite directions by the displacing rigid arms 6, to which arms 6 such ends are connected. Such a second deformation contributes in particular to ensure that the retaining member 1 stores a large amount of elastic energy.
This double elastic deformation of the elastic arms 7 can be carried out simultaneously or substantially simultaneously, or else successively or substantially successively. It will be noted in the context of the implementation of the deformation phase that when this double elastic deformation is carried out successively or substantially successively, the first deformation can then be carried out before the second deformation.
This method then comprises a step 16 of fixing the retaining member 1 on the reinforcing element 3. Such a fixing step 16 comprises a sub-step 17 of performing a radial elastic clamping of the retaining member 1 on the support element 3. It is therefore understood that in such a state of constraint, the retaining member 1 stores a large amount of elastic energy which contributes to giving it a substantial holding torque allowing in particular an optimal twist by elastic clamping.
Number | Date | Country | Kind |
---|---|---|---|
18196014 | Sep 2018 | EP | regional |
Filing Document | Filing Date | Country | Kind |
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PCT/EP2019/073513 | 9/4/2019 | WO |
Publishing Document | Publishing Date | Country | Kind |
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WO2020/057969 | 3/26/2020 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
20090135679 | Musy et al. | May 2009 | A1 |
20130047437 | Daout | Feb 2013 | A1 |
20150023140 | Daout | Jan 2015 | A1 |
20160370764 | Cusin et al. | Dec 2016 | A1 |
20180107162 | Hernandez | Apr 2018 | A1 |
20180150029 | Shibuya et al. | May 2018 | A1 |
Number | Date | Country |
---|---|---|
698 794 | Oct 2009 | CH |
706 526 | Nov 2013 | CH |
707 288 | May 2014 | CH |
714001 | Jan 2019 | CH |
101750954 | Jun 2010 | CN |
103930837 | Jul 2014 | CN |
104898398 | Sep 2015 | CN |
1680892 | Oct 2015 | CN |
106257348 | Dec 2016 | CN |
107942639 | Apr 2018 | CN |
1826635 | Aug 2007 | EP |
1 857 891 | Nov 2007 | EP |
2 219 083 | Aug 2010 | EP |
2219083 | Aug 2010 | EP |
2 372 473 | Oct 2011 | EP |
2 889 701 | Jul 2015 | EP |
3 106 931 | Dec 2016 | EP |
3 309 625 | Apr 2018 | EP |
3 327 514 | May 2018 | EP |
2013-234901 | Nov 2013 | JP |
2018-63250 | Apr 2018 | JP |
Entry |
---|
International Preliminary Report on Patentability and Written Opinion of the International Searching Authority dated Mar. 23, 2021 in PCT/EP2019/073513, 16 pages. |
International Search Report dated Nov. 4, 2019 in PCT/EP2019/073513 filed on Sep. 4, 2019, 3 pages. |
Japanese Office Action dated Apr. 26, 2022, in Japanese Patent Application No. 2021-512488 (with English translation), 8 pages. |
Combined Chinese Office Action and Search Report dated Aug. 23, 2021 in Chinese Patent Application No. 201980062071.5 (with English translation), 14 pages. |
Number | Date | Country | |
---|---|---|---|
20210216043 A1 | Jul 2021 | US |