EP2656150B1 - Montageverfahren einer komponente ohne kunststoffbereich - Google Patents

Montageverfahren einer komponente ohne kunststoffbereich Download PDF

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Publication number
EP2656150B1
EP2656150B1 EP11787857.9A EP11787857A EP2656150B1 EP 2656150 B1 EP2656150 B1 EP 2656150B1 EP 11787857 A EP11787857 A EP 11787857A EP 2656150 B1 EP2656150 B1 EP 2656150B1
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EP
European Patent Office
Prior art keywords
aperture
opening
flared portion
assembly method
assembly
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
EP11787857.9A
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English (en)
French (fr)
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EP2656150A2 (de
Inventor
Thierry Conus
Marco Verardo
Igor Saglini
Frédéric Kohler
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
ETA SA Manufacture Horlogere Suisse
Original Assignee
ETA SA Manufacture Horlogere Suisse
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by ETA SA Manufacture Horlogere Suisse filed Critical ETA SA Manufacture Horlogere Suisse
Priority to EP11787857.9A priority Critical patent/EP2656150B1/de
Publication of EP2656150A2 publication Critical patent/EP2656150A2/de
Application granted granted Critical
Publication of EP2656150B1 publication Critical patent/EP2656150B1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • 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
    • G04B13/00—Gearwork
    • G04B13/02—Wheels; Pinions; Spindles; Pivots
    • G04B13/021—Wheels; Pinions; Spindles; Pivots elastic fitting with a spindle, axis or shaft
    • G04B13/022—Wheels; Pinions; Spindles; Pivots elastic fitting with a spindle, axis or shaft with parts made of hard material, e.g. silicon, diamond, sapphire, quartz and the like
    • 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
    • G04B1/00—Driving mechanisms
    • G04B1/10—Driving mechanisms with mainspring
    • G04B1/14—Mainsprings; Bridles therefor
    • G04B1/145—Composition and manufacture of the springs
    • 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
    • G04B13/00—Gearwork
    • G04B13/02—Wheels; Pinions; Spindles; Pivots
    • 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
    • G04B13/00—Gearwork
    • G04B13/02—Wheels; Pinions; Spindles; Pivots
    • G04B13/021—Wheels; Pinions; Spindles; Pivots elastic fitting with a spindle, axis or shaft
    • 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
    • G04B15/00—Escapements
    • G04B15/14—Component parts or constructional details, e.g. construction of the lever or the escape wheel
    • 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
    • G04B17/32—Component parts or constructional details, e.g. collet, stud, virole or piton
    • 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
    • G04B17/32—Component parts or constructional details, e.g. collet, stud, virole or piton
    • G04B17/325—Component parts or constructional details, e.g. collet, stud, virole or piton for fastening the hairspring in a fixed position, e.g. using a block
    • 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
    • G04B17/32—Component parts or constructional details, e.g. collet, stud, virole or piton
    • G04B17/34—Component parts or constructional details, e.g. collet, stud, virole or piton for fastening the hairspring onto the balance
    • G04B17/345—Details of the spiral roll
    • G—PHYSICS
    • G04—HOROLOGY
    • G04D—APPARATUS OR TOOLS SPECIALLY DESIGNED FOR MAKING OR MAINTAINING CLOCKS OR WATCHES
    • G04D1/00—Gripping, holding, or supporting devices
    • G04D1/0007—Gripping, holding, or supporting devices for assembly entirely by hand
    • G04D1/0042—Gripping, holding, or supporting devices for assembly entirely by hand tools for setting, riveting or pressing, e.g. nippers for this purpose
    • G—PHYSICS
    • G04—HOROLOGY
    • G04D—APPARATUS OR TOOLS SPECIALLY DESIGNED FOR MAKING OR MAINTAINING CLOCKS OR WATCHES
    • G04D3/00—Watchmakers' or watch-repairers' machines or tools for working materials
    • G04D3/04—Devices for placing bearing jewels, bearing sleeves, or the like in position
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49579—Watch or clock making
    • Y10T29/49581—Watch or clock making having arbor, pinion, or balance

Definitions

  • the invention relates to an assembly of a part whose material does not comprise a plastic field with a member comprising another type of material.
  • Document CH 700 260 gives an example of a current assembly. It discloses a rocker mounted elastically and then stuck on a tree.
  • the object of the present invention is to overcome all or part of the disadvantages mentioned above by proposing a glueless assembly capable of securing a part whose material does not include a plastic field with a member comprising a ductile material such as, for example, a metal or a metal alloy.
  • This method advantageously makes it possible to radially fasten the member and the workpiece without any axial force being applied to the workpiece. Indeed, advantageously according to the invention, only a radial elastic deformation is applied to the workpiece. Finally, such a method makes it possible to secure the whole piece - organ by adapting to the manufacturing dispersions of the various constituents.
  • the invention relates to an assembly and its method for joining a fragile material, that is to say not having a plastic domain such as a material based on silicon, with a ductile material such as a metal or a metal alloy.
  • This assembly was designed for applications in the watchmaking field. However, other areas can be perfectly imagined such as aeronautics, jewelery, automotive and tableware.
  • this assembly is made necessary by the growing share of fragile materials such as those based on silicon, quartz, corundum or more generally ceramic.
  • fragile materials such as those based on silicon, quartz, corundum or more generally ceramic.
  • the invention relates to an assembly between an axially extending member made of a first material, for example ductile such as steel, in the opening of a part made of a second material that does not include a domain.
  • plastic as a silicon-based material, by deformation of a portion of the member which is mounted in the opening of said piece.
  • said member comprises a radially flaring portion and elastically and plastically deformed in order to clamp radially the wall of said part surrounding the opening by biasing its elastic deformation means to non-destructively fasten the assembly for said part.
  • the outer wall of the radially flaring portion of the member present in the opening is substantially of corresponding shape to the opening of the part in order to exert a radial stress. substantially uniformly on the wall of the room surrounding said opening. Indeed, during the research carried out, it appeared preferable that the flared portion of the member present in the opening evenly distribute the radial stresses induced by its deformation on the wall of the room surrounding the opening.
  • the opening in the fragile part is circular, it is preferable that the outer wall of the flared part of the member present in the opening is in substantially continuous cylinder shape, that is to say without radial slot or axial opening, to avoid localized stresses on part of the wall of the room surrounding the opening which are suitable for initiating break points.
  • the shape of the opening in the fragile part may differ in being, for example, asymmetrical in order to avoid relative displacements between the elements of the assembly.
  • Such an asymmetric opening can thus be, for example, substantially elliptical.
  • the flared portion of the member present in the opening with a shape corresponding to the opening can be interpreted, if the section of the opening is circular, as a solid disc whose outer wall is continuous, c that is to say without groove or more generally material discontinuity.
  • the corresponding shape of the flared part of the member present in the opening thus makes it possible, by elastic and plastic deformation, to generating only substantially uniform radial stress on a maximized surface of the wall of the workpiece around the opening.
  • the piece comprises perforations forming elastic deformation means which are distributed around and away from its opening and which are intended to absorb said radial forces to restore them once the stress of the tools released in order to, in the end, fasten the assembly non-destructively for said part.
  • the anchor 1 as an example comprises two assemblies 2, 12 according to the invention intended respectively to secure the stinger 7 and the member, here a pivot axis 17, with its rod 5.
  • each assembly 2, 12 comprises a radially flaring portion 4, 14, substantially discoidal shaped with the stinger 7 or the member 17 and cooperating with the rod 5 of the anchor 1.
  • each assembly 2, 12 comprises perforations 6, 16 made in the rod 5 around an opening 8, 18 and which are intended to form elastic deformation means. It is therefore understood that the assembly 2, 12 is sufficiently strong not to generate relative movements between its components.
  • the escape wheel 3, and more generally the mobile 3, comprises, by way of example, an assembly 22 intended to secure the member, here a pivot axis 27, with the body 25 of the wheel 3.
  • the assembly 22 comprises a radially flaring portion 24, substantially discoidal in shape with the member 27 and cooperating with the body 25 of the wheel 3.
  • the assembly 22 comprises cut-outs 26 made in the hub around an opening 28 of the wheel 3 and which are intended to form elastic deformation means.
  • the example of the assembly 22 can be applied to any type of mobile.
  • the member 27 may comprise, in addition to the flared portion 24, in one piece a pinion to form the finished mobile.
  • Cut-outs 66 are formed in ferrule 63 of hairspring 61 and a disc-shaped portion 64 formed integrally with member 67 is mounted in aperture 68 of ferrule 63, similarly to the explanations above.
  • FIG. 3 to 8 Examples of openwork are presented to Figures 3 to 8 .
  • the perforations are formed at a distance and around the opening by two series of diamond-shaped holes distributed in a staggered manner to form beams divided into V secants.
  • the figure 3 is a representation of the perforations 6, 16, 26, 66 of figures 1 and 2 .
  • the latter shows cutouts 26 which, preferably, completely cross the thickness of the body 25 of fragile material.
  • the perforations 26 are distributed at a distance and around the opening 28 formed, preferably, also completely through in the thickness of the body 25 of fragile material.
  • the perforations 26 form a first series of holes 31, furthest from the opening 28, and a second series of holes 33 which are diamond-shaped and distributed in staggered rows.
  • the perforations 31, 33 thus form V-shaped beams 32 which are intersecting with each other.
  • the perforations 26 take up the first and second series of holes 31, 33 with, in addition, a third series which, formed of holes 35 in the form of a triangle, is located between the first two series and the opening 28, c' that is to say the closest to the opening 28.
  • the third set of holes 35 is staggered with one of the first two sets to form beams 34 distributed in intersecting X's.
  • the cut-outs 26 "repeat the cut-outs 26 'of the figure 4 with, in addition, slots 36 for communicating the third set of holes 35 with the opening 28.
  • the series of holes 31, 33 and 35 and the slots 36 are used to form elastic deformation means capable of absorbing radial stresses, that is to say forces exerted from the center of the opening 28 to the wall of the body 25 surrounding said circular opening.
  • the two or three series may be more or less close to each other and / or different shapes and / or different dimensions depending on the desired maximum displacement and the desired stress to deform the beams 32, 34.
  • FIG. 5 For example, an alternative of the figure 5 is presented to the figure 6 . It can be seen that the cut-outs 26 '"are similar to those 26" of the figure 5 however, the three sets of holes are spaced apart from each other. In addition, it is visible that the shapes and dimensions of both holes and slots are different. So we understand that the alternative of figure 6 modifies the rigidity of the elastic deformation means in the brittle material.
  • the cut-outs 26, 26 ', 26 ", 26"' extend over a width of between 100 ⁇ m and 500 ⁇ m from the wall of the body 25 surrounding the opening 28.
  • the slots 36 are between 15 microns and 40 microns.
  • the section of the opening 28 is between 0.5 and 2 mm.
  • the perforations are formed at a distance and around the opening by a first series of oblong holes distributed in staggered rows with a second series of triangular shaped holes, the second series being the closest to the circular opening, each form hole triangular communicating with the opening by a notch to form radially movable beams according to the thickness of the oblong holes.
  • the figure 7 shows cutouts 46 which, preferably, completely cross the thickness of the body 25 of fragile material.
  • the perforations 46 are distributed at a distance and around the opening 28 formed, preferably, also completely through in the thickness of the body 25 of fragile material.
  • the perforations 46 form a first series of oblong holes 51 and a second series of holes 53 of triangular shape. According to the second embodiment, the two sets of holes 51, 53 are distributed in staggered rows.
  • each hole 53 of triangular shape communicates with the opening 28 by a notch 57. It can be seen at figure 7 that the perforations 46 thus form substantially trapezoidal beams 52 which are separated from each other by the notches 57. It is also noted that each beam 52 is centered on an oblong hole 51 which makes each beam 52 mobile radially according to the thickness an oblong hole 51.
  • the openwork 46 'reproduce the cut-outs 46 of the figure 7 with, in addition, a third series of holes 55 in the form of a triangle.
  • each hole 55 of the third series is distributed between two holes 53 of triangular shape of the second series and communicates with the opening 28 by a slot 56.
  • the perforations 46 'thus form beams 54 with two independent arms symmetrical and substantially L-shaped which are movable radially according to the thickness of the holes 51 oblong and tangentially according to the thickness of slots 56 and notches 57.
  • the two or three series may be more or less close to each other and / or different shapes and / or different dimensions depending on the desired maximum travel and the desired stress for deform the beams 52, 54.
  • the slots 56 and the notches 57 are between 15 ⁇ m. and 40 ⁇ m.
  • the section of the opening 28 is between 0.5 and 2 mm.
  • a first step consists in forming the part 3 in a material having no plastic domain with an opening 28 and perforations 26 distributed around the opening 28 intended to form elastic deformation means according to, for example, for example, the embodiments explained above.
  • the opening 28 has a section e 1 and the perforations 26 include in particular holes of section e 2 .
  • Such a step can be carried out by etching in dry or wet form, such as, for example, a deep reactive ion etching (also known as the English abbreviation "DRIE").
  • DRIE deep reactive ion etching
  • the method consists in forming the axially extending member, a pivot axis 27 in the example of the Figures 9 to 11 , in a second material with a main section e 3 and a radially flared portion 24 intended to be deformed with a maximum section e 4 .
  • the portion 24 may have a thickness between 100 and 300 microns.
  • the second step can be performed according to the usual processes for producing axes.
  • the member 27 is preferably metallic and may, for example, be formed of steel.
  • the first two steps have no consecutivity to respect and can even be performed at the same time.
  • the flared portion 24 is introduced without contact into the opening 28. This means as visible at the figure 10 that the section e 1 of the opening 28 is greater than or equal to the outer section e 4 of the flared portion 24 of the member 27.
  • the difference between the section e 1 of the opening 28 and the outer section e 4 of the flared portion 24 is about 10 ⁇ m, that is to say a gap of about 5 ⁇ m which separates the body 25 of the piece 3 with respect to the flared portion 24 of the member 27.
  • the flared portion 24 and, incidentally, the member 27, is held in the opening 28 with a 21 of the tools 20, 21 used for the deformation step.
  • the tool 21 comprises a recess 29 intended to receive a part of the member 27.
  • the method comprises a fourth step of elastically and plastically deforming the flared portion 24 of the member 27 by bringing the tools 20, 21 in the axial direction A in order to exert a uniform radial stress B against the wall of the part 3 surrounding the opening 28 by biasing the means of elastic deformation of the part 3, that is to say the cut-outs 26.
  • the deformation is parameterized so that the tightening is greater than the gap between the undeformed flared portion 24 and the wall of the body 25 surrounding the opening 28.
  • the tightening is between 8 and 20 ⁇ m.
  • the elastic and plastic deformation of the flared portion 24 exerts the elastic deformation of the body 25 around the opening 28 in order to secure together the member 27 and therefore its flared portion 24 deformed, with the body 25 of the wheel 3 as visible to the figure 11 .
  • this embodiment allows in particular an automatic centering of the entire body 27 - body 25.
  • the perforations 26 comprise a section referenced e 5 and no longer e 2 .
  • no axial force by definition likely to be destructive
  • a radial elastic deformation is applied to the body 25.
  • the use of the radially flared portion 24 allows, during the radial deformation B of the flared portion 24, to exert a uniform stress on a maximized surface of the wall of the body 25 around the opening 28 to prevent any breakage of the wheel 3 of fragile material and adapt to the manufacturing dispersions of the various elements.
  • the present invention is not limited to the illustrated example but is susceptible of various variations and modifications that will occur to those skilled in the art.
  • the perforations of the piece of fragile material may comprise more or fewer series of holes than the modes of realization presented above.
  • the presented embodiments are capable of being combined with one another according to the intended applications.
  • the radially flared portion 24 may also comprise a different geometry in order to optimize or "program" the deformation towards the body 25. It may be, for example, considered to minimize or locally increase the thickness of the flared portion 24 in order to favor one direction of deformation with respect to the other in the direction B. For example, it is thus possible to make a conical recess and coaxial with the member 27 to facilitate the radial orientation B but also to make the progressive induced stress.
  • the figures 1 and 2 have applications for an exhaust system such as the anchor 1 and the escape wheel 3 or a hairspring 61 of a watch movement.
  • an exhaust system such as the anchor 1 and the escape wheel 3 or a hairspring 61 of a watch movement.
  • the present assembly 2, 12, 22, 62 can be applied to other elements.
  • the assembly 2, 12, 22, 62 according to the invention can also allow the joining of any type of watchmaking member or not whose body is formed of a material having no plastic field (silicon, quartz, etc.) with an axis such as, for example, a resonator of the type tuning fork or more generally a MEMS (acronym from the English term "Micro-Electro-Mechanical System").

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Metallurgy (AREA)
  • Micromachines (AREA)
  • Manufacturing & Machinery (AREA)
  • Electromechanical Clocks (AREA)

Claims (14)

  1. Verfahren zum Verbinden eines Organs (7, 17, 27, 67) aus einem ersten Material, das sich in einem Teil (1, 3, 61) aus einem zweiten Material, das keinen Kunststoffanteil aufweist, axial erstreckt, wobei das Verfahren die folgenden Schritte umfasst:
    a) Ausbilden des Teils (1, 3, 61) mit einer Öffnung (8, 18, 28, 68) und mit Durchbrüchen (6, 16, 26, 26', 26", 26"', 46, 46', 66), die um die Öffnung (8, 18, 28, 68) verteilt sind und dazu bestimmt sind, Mittel zur elastischen Verformung zu bilden;
    b) spannungsfreies Einführen eines radial erweiterten Teils (4, 14, 24, 64) des Organs in die Öffnung (8, 18, 28, 68);
    c) elastisches und plastisches Verformen des erweiterten Teils (4, 14, 24, 46) des Organs in der Öffnung durch axiale Annäherung von zwei Werkzeugen (20, 21) auf Höhe jeweils des oberen und unteren Teils des erweiterten Teils, damit dieses Letztere eine radiale Spannung (B) auf die Wand des die Öffnung (8, 18, 28, 68) umgebenden Teils (1, 3, 61) durch Belasten der Mittel zur elastischen Verformung des Teils (1, 3, 61) ausübt, um ein Befestigen der Verbindung (2, 12, 22, 62) in für das Teil zerstörungsfreier Weise zu ermöglichen.
  2. Verfahren nach dem vorhergehenden Anspruch, dadurch gekennzeichnet, dass die Außenwand des erweiterten Teils (4, 14, 24, 64) des Organs in der Öffnung eine der Öffnung (8, 18, 28, 68) des Teils (1, 3, 61) im Wesentlichen entsprechende Form besitzt, um eine im Wesentlichen gleichmäßige radiale Spannung (B) auf die Wand des die Öffnung (4, 14, 24, 64) umgebenden Teils (1, 3, 61) auszuüben.
  3. Verfahren nach Anspruch 1 oder 2, dadurch gekennzeichnet, dass die Öffnung (8, 18, 28, 68) des Teils (1, 3, 61) kreisförmig ist.
  4. Verfahren nach Anspruch 1 oder 2, dadurch gekennzeichnet, dass die Öffnung (8, 18, 28, 68) des Teils (1, 3, 61) asymmetrisch ist, um relative Verlagerungen zwischen den Elementen der Verbindung zu vermeiden.
  5. Verbindungsverfahren nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass im Schritt b) die Differenz zwischen dem Querschnitt (e1) der kreisförmigen Öffnung (8, 18, 28, 68) und dem äußeren Querschnitt (e4) des erweiterten Teils (4, 14, 24, 64) des Organs in der Öffnung ungefähr 10 µm beträgt.
  6. Verbindungsverfahren nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass im Schritt c) die Verformung eine Verdichtung im Bereich von 8 bis 20 µm bewirkt.
  7. Verbindungsverfahren nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass in den Schritten b) und c) der erweiterte Teil (4, 14, 24, 64) des Organs (7, 17, 27, 76) in der Öffnung mit Hilfe eines von zwei Werkzeugen (20, 21) in der Öffnung (8, 18, 28, 68) gehalten wird.
  8. Verbindungsverfahren nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass das zweite Material auf Siliciumbasis gebildet ist.
  9. Verbindungsverfahren nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass das erste Material auf Basis eines Metalls oder einer Metalllegierung gebildet ist.
  10. Verbindungsverfahren nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass das Teil ein Drehteil (3) einer Uhr ist.
  11. Verbindungsverfahren nach einem der Ansprüche 1 bis 9, dadurch gekennzeichnet, dass das Teil ein Anker (1) einer Uhr ist.
  12. Verbindungsverfahren nach einem der Ansprüche 1 bis 9, dadurch gekennzeichnet, dass das Teil eine Spiralfeder (61) einer Uhr ist.
  13. Verbindungsverfahren nach einem der Ansprüche 1 bis 9, dadurch gekennzeichnet, dass das Teil ein Resonator ist.
  14. Verbindungsverfahren nach einem der Ansprüche 1 bis 9, dadurch gekennzeichnet, dass das Teil ein MEMS ist.
EP11787857.9A 2010-12-22 2011-11-22 Montageverfahren einer komponente ohne kunststoffbereich Active EP2656150B1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP11787857.9A EP2656150B1 (de) 2010-12-22 2011-11-22 Montageverfahren einer komponente ohne kunststoffbereich

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP10196597A EP2469353A1 (de) 2010-12-22 2010-12-22 Zusammenbau eines Teils, das keinen Plastikbereich enthält
PCT/EP2011/070693 WO2012084384A2 (fr) 2010-12-22 2011-11-22 Assemblage d'une pièce ne comportant pas de domaine plastique
EP11787857.9A EP2656150B1 (de) 2010-12-22 2011-11-22 Montageverfahren einer komponente ohne kunststoffbereich

Publications (2)

Publication Number Publication Date
EP2656150A2 EP2656150A2 (de) 2013-10-30
EP2656150B1 true EP2656150B1 (de) 2017-01-04

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EP10196597A Withdrawn EP2469353A1 (de) 2010-12-22 2010-12-22 Zusammenbau eines Teils, das keinen Plastikbereich enthält
EP11787857.9A Active EP2656150B1 (de) 2010-12-22 2011-11-22 Montageverfahren einer komponente ohne kunststoffbereich

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EP10196597A Withdrawn EP2469353A1 (de) 2010-12-22 2010-12-22 Zusammenbau eines Teils, das keinen Plastikbereich enthält

Country Status (7)

Country Link
US (1) US9128463B2 (de)
EP (2) EP2469353A1 (de)
JP (1) JP5671155B2 (de)
CN (1) CN103299245B (de)
HK (1) HK1189281A1 (de)
TW (1) TWI564107B (de)
WO (1) WO2012084384A2 (de)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
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CH704016B1 (fr) * 2010-10-15 2019-01-31 Eta Sa Mft Horlogere Suisse Assemblage d'une pièce ne comportant pas de domaine plastique.
EP2469352A1 (de) * 2010-12-22 2012-06-27 Nivarox-FAR S.A. Zusammenbau eines Teils, das keinen Plastikbereich enthält
CH704258A2 (fr) * 2010-12-22 2012-06-29 Nivarox Sa Assemblage d'une pièce ne comportant pas de domaine plastique.
CH707503A2 (fr) * 2013-01-17 2014-07-31 Omega Sa Axe de pivotement pour mouvement horloger.
EP2952971B1 (de) * 2014-06-05 2016-10-12 Nivarox-FAR S.A. Anker für Hemmungsmechanismus eines Uhrwerks
US9753433B2 (en) 2014-09-12 2017-09-05 Seiko Instruments Inc. Mechanical component, movement, and timepiece
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TW201240763A (en) 2012-10-16
TWI564107B (zh) 2017-01-01
WO2012084384A3 (fr) 2012-08-16
WO2012084384A2 (fr) 2012-06-28
HK1189281A1 (zh) 2014-05-30
JP2014501923A (ja) 2014-01-23
CN103299245B (zh) 2016-06-15
US9128463B2 (en) 2015-09-08
US20130286795A1 (en) 2013-10-31
JP5671155B2 (ja) 2015-02-18
EP2469353A1 (de) 2012-06-27
EP2656150A2 (de) 2013-10-30
CN103299245A (zh) 2013-09-11

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