The invention relates to a composite gear system, for example silicon-metal, for a timepiece, and, more specifically, a system of this type that includes a securing device that can prevent shearing stress.
In order to prevent shearing stress, it is known within the field of horology to use arbours that have a polygonal, i.e. non circular section so as to drive in rotation a part whose arbour hole has a shape that matches said polygonal section. However, this configuration, particularly in the case of a gear train, induces asymmetry in the arbour, which is detrimental to the isochronism of the timepiece movement and requires the other gear trains, secured to the same arbour, to adopt arbour holes of the same shape.
Moreover, in the case of a composite timepiece member, i.e. one that includes two types of material, such as a gear system of the toothed wheel-pinion type, it is difficult to attach the member to a polygonal arbour without breaking it, if one of the materials includes a very restricted plastic range area, like crystalline silicon, crystalline alumina or crystalline silica.
It is an object of the present invention to overcome all or part of the aforementioned drawbacks by proposing a gear system that includes a securing device, which can prevent shearing stress, yet can be adapted to a cylindrical arbour of circular section.
The invention therefore relates to a gear system comprising a pinion and a toothed wheel coaxially mounted relative to a pivoting arbour, characterized in that it includes a securing device between said pinion and said wheel to prevent any relative movement of one in relation to the other.
According to other advantageous features of the invention:
The invention also relates to a timepiece, characterized in that it includes a gear system in accordance with one of the preceding variants.
The invention relates finally to a method of manufacturing a timepiece member in micro-machinable material with several levels, which includes the following steps:
According to other advantageous features of the invention:
Other peculiarities and advantages will appear clearly from the following description, given by way of non-limiting illustration, with reference to the annexed drawings, in which:
As illustrated in
As illustrated in
Pinion 5 has a main body of cylindrical shape, whose inner diameter section approximately matches the external diameter of arbour 3. Pinion 5 includes wings 9 that extend radially from said main body to cooperate with another toothed member (not shown). In the example illustrated in
Wheel 7 includes a felloe 11, a hub 13 pierced with a polygonal or cylindrical arbour hole 15 and four arms 17 connecting said hub and said felloe. As illustrated in
According to the invention, hub 13 preferably includes a securing device 21, for preventing any relative movement of wheel 7 with respect to pinion 5 so as to reduce shearing stress. According to the invention, securing device 21 mainly includes a pattern cavity 23 formed on hub 13 for cooperating with the low part of pinion 5 by partially covering the same.
Preferably, as illustrated in
In the example illustrated in
Preferably, gear system 1 is of the composite type, i.e. it is formed of at least two types of material. Thus, one of the members is preferably formed of a micro-machinable material and the others of metallic materials. According to the invention, a micro-machinable material is used in order to benefit from manufacturing precision of less than a micron. This material may comprise crystalline silicon, crystalline alumina or crystalline silica. The other members are preferably made of metallic materials, when they do not need to have more precise dimensions than is possible with said metallic materials.
According to the invention, wheel 7 is preferably formed from a micro-machinable material whereas arbour 3 and pinion 5 are made from a metallic material, such as, for example, steel or brass. This configuration may be useful, in particular, for an application of the escape wheel type so as to obtain an impulse toothing 19 and also a pattern cavity 23 that are very precise. Indeed, as can be seen in
According to a variant of the invention, securing device 21 further includes an adhesive material mounted between impression 23 and pinion 5, so as to improve the securing force of said device. This material may be, for example, a solder, or an adhesive. Indeed, a connection using an adhesive material generally performs well in traction but poorly in shearing. It is thus clear that, because of the configuration of securing device 21, the securing force therefore benefits from said traction advantages of the adhesive material and the shearing advantages of the partial covering by pattern cavity 23.
The adhesive material may be, for example, placed between the bottom of pattern cavity 23 and the bottom of pinion 5. The adhesive material may equally well be placed between the periphery of wings 9 and the toothing of pattern cavity 23. This latter configuration is particularly advantageous when the shape of pattern cavity 23 does not match the section of pinion 5 exactly, as explained above.
The method of manufacturing the member in micro-machinable material and with several levels will now be explained with reference to
In a first step, as illustrated in
In a second step, a first protective mask 33 is structured on the top of substrate 31. This step may be achieved for example by selective oxidation at the surface of substrate 31 in order to grow silicon oxide to form said mask to a determined height. As seen in
In a third step, a second protective mask 35 is structured overlapping mask 33 made in the second step. This step may be performed by photolithography of a photosensitive resin. Then in a first phase, a photosensitive resin is deposited on substrate 31 and on protective mask 33. Then, in a second phase, the resin is selectively exposed using radiation through a partially opaque mask. Finally, the selectively illuminated photosensitive resin is developed so as to leave only a protective mask 35, as shown in
According to a variant, the second mask 35 can also be made by selective oxidation of the surface of substrate 31 in order to grow silicon oxide to form said mask to a predetermined height.
In a fourth step, as shown in
In a fifth step, the second mask 35 is removed. Depending upon the nature of second mask 35, this may consist respectively in removing the structured resin or etching the silicon oxide layer until pattern 32 is exposed.
In a sixth step, a second anisotropic etch is performed on substrate 31 along to pattern 32 of the first protective mask 33. The etch may also be dry or wet. In a similar manner to the fourth step, the second etch continues the etch of arbour hole 15, but also of the other throughout holes of wheel 7 and starts the etch of pattern cavity 23. As shown in
Preferably according to the invention, the section of pattern 34 of second mask 35 is smaller at hub 13, as shown in
It is clear from reading the manufacturing method for timepiece member 7 that, depending upon the total thickness eT of substrate 31 and the depth e2 of pattern cavity 23, one can deduce therefrom the minimum etch depth e1 that has to be performed in the fourth step so that arbour hole 15 and the other cavities delimiting hub 11, arms 17, felloe 11 and toothing 19 are etched in the entire thickness of substrate 31. It is also clear that, advantageously, the manufacturing method allows several members 7 to be made on the same substrate 31.
The final assembly method will now be explained with reference to
In a second step, the pinion 5—arbour 3 assembly is mounted on timepiece member 7 made in accordance with the manufacturing method explained above, a toothed wheel in the example, so as to form the composite gear system 1. In a first phase, the pinion 5—arbour 3 assembly is moved towards member 7 so that the low end of arbour 3 is opposite arbour hole 15 of wheel 7 as illustrated in
As explained above, according to a variant of the invention, an adhesive material can be used to improve the force securing pinion 5 and wheel 7. In this variant, two additional phases could be added. An intermediate phase between the second and third phases of the final assembly method could consist in depositing said material in the bottom of pattern cavity 23. This material could be a solder and/or an adhesive such as a polymer adhesive. A final phase could then follow the third phase and would activate the adhesive material, for example, by melting said solder and/or polymerising said adhesive.
Two final phases could also be envisaged. The first could consist in depositing said material between the toothings of pattern cavity 23 and the wings 9 of pinion 5. This material could also be a solder and/or an adhesive such as a polymer adhesive. The second final phase would then activate the adhesive material, for example, by melting said solder and/or polymerising said adhesive. This embodiment is particularly advantageous when the shape of pattern cavity 23 does not exactly match the section of pinion 5 as explained above.
As illustrated in
Of course, the present invention is not limited to the illustrated example but may be subject to various variants and alterations, which will appear to those skilled in the art. In particular, pattern cavity 23 may project at least partially from hub 13. Indeed, this would increase the contact zone between arbour 3 and hub 13, which would improve the guiding of wheel 7 relative to arbour 3. Said contact zone could even match the total height of wheel 7, and pattern cavity 23 would then project entirely from hub 13 of wheel 7, instead of being at least partially indented.
Number | Date | Country | Kind |
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08162475.1 | Aug 2008 | EP | regional |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/EP2009/059477 | 7/23/2009 | WO | 00 | 2/15/2011 |