Timepiece assembly and method for manufacturing the same

Abstract

A timepiece assembly including a first component and a second component assembled under stress, wherein at least one part of the surface of the assembly is coated with a protective layer intended to cover defects such as cracks or incipient cracks after assembly. It also relates to the method for manufacturing this assembly.

Claims

1. A method for manufacturing a timepiece assembly, the method comprising, successively: assembling an inertia screw to a balance, the balance comprising a resilient arm delimiting a slot configured to receive the inertia screw, under mechanical stress by elastic deformation of the resilient arm and insertion of the inertia screw into the slot, to obtain a component assembly; and depositing, under stress on the resilient arm, a protective layer on at least one part of a surface of a stressed area of the component assembly configured for the timepiece assembly, wherein the timepiece assembly comprises the balance comprising the resilient arm delimiting the slot; and the inertia screw assembled under mechanical stress, and wherein the slot is configured to receive the inertia screw.

2. The method of claim 1, further comprising, prior to the assembling: depositing a first layer at least partially on the balance and/or the inertia screw.

3. The method of claim 2, further comprising, prior to the depositing of the first layer: depositing a sub-layer at least partially on the balance and/or the inertia screw.

4. The method of claim 3, wherein the first layer and the sub-layer are deposited by ALD, PVD, CVD, chemical deposition, or electroplating deposition.

5. The method of claim 3, wherein the sublayer comprises Ni or Au.

6. The method of claim 3, wherein the sub-layer has a thickness in a range of from 100 nm to 2 m.

7. The method of claim 2, further comprising, before the assembling and after the depositing of the first layer: heat treating the first layer at a temperature in a range of from 150 to 300 C. for a time in a range of from 30 minutes to 5 hours.

8. The method of claim 2, wherein the first layer comprises Au or Rh.

9. The method of claim 2, wherein the first layer has a thickness in a range of from 100 nm to 2 m.

10. The method of claim 1, further comprising, after the depositing of the protective layer: heat treating the protective layer at a temperature in a range of from 150 to 300 C. for a time in a range of from 30 minutes to 5 hours.

11. The method of claim 10, wherein the protective layer is deposited by ALD, PVD, CVD, chemical deposition, or electroplating deposition.

12. The method of claim 1, wherein the protective layer comprises SiO.sub.2, Al.sub.2O.sub.3, Rh, Au, Ni, or NiP.

13. The method of claim 1, wherein the protective layer is formed of a stack of layers respectively comprising SiO.sub.2, Al.sub.2O.sub.3, Rh, Au, Ni, or NiP.

14. The method of claim 1, wherein the protective layer has a thickness in a range of from 20 nm to 3 m.

15. A method for manufacturing a timepiece assembly, the method comprising, successively: assembling a first component and a second component under mechanical stress; and depositing, under stress on the first component, a protective layer at least partially on a surface in an area stressed of a first assembly comprising the first component and the second component, wherein the timepiece assembly comprises the first component and the second component, assembled under mechanical stress, wherein the first component is an element assembled by press fit onto the second component, and wherein (i) the first component is an impulse pin and the second component is a roller or (ii) wherein the first component is a balance and the second component is a shaft.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) Other features and advantages will appear clearly from the following description, given by way of non-limiting illustration, with reference to the annexed drawings.

(2) FIG. 1 is a plan view of the timepiece assembly according to the invention comprising the balance and two inertia screws.

(3) FIG. 2 is a three-dimensional view of the inertia screw of the timepiece assembly of FIG. 1.

(4) FIG. 3 is a schematic cross-sectional view of a component of the timepiece assembly coated with several layers according to the method of the invention.

(5) FIG. 4A is an electron microscope view of a cross-section of the balance of the timepiece assembly according to the invention.

(6) FIG. 4B is a schematic diagram of FIG. 4A.

DESCRIPTION OF THE INVENTION

(7) The invention relates to a timepiece assembly comprising at least two components assembled under stress. By way of example, as represented in FIG. 1, the first component is a balance 2 comprising a resilient arm 2a delimiting a slot 4 which, during assembly, receives the second component which is an inertia screw 3 also visible in FIG. 2. This could also be a pressed-in element, like an impulse pin in a roller or a balance on a staff, etc.

(8) The components can be made of a material chosen from the list including copper, copper alloys such as brass or nickel silver, aluminium, aluminium alloys, titanium, titanium alloys, carbon steel and ferritic and austenitic stainless steels.

(9) According to the invention, the timepiece assembly is at least partially coated with a protective layer after assembly, intended to cover any defects such as cracks, incipient cracks, peeling, resulting from the assembly process or possibly already present prior to assembly. FIGS. 4A and 4B respectively represent, in an electron microscope view and a schematic view of said electron microscope view, the formation of cracks 8 in the base material of one of the components (referenced 2) and in a protective layer, called first layer 6, deposited prior to assembly. According to the invention, a protective layer 7, called the second layer, is deposited on the cracked surface to form a barrier impermeable to the external environment after assembly.

(10) FIG. 3 schematically represents the layers deposited on timepiece assembly 1. Prior to assembly, one or more layers can optionally be deposited on at least one of the two components of the timepiece assembly. The base material of the timepiece assembly can thus be coated with a first layer 6 and, also optionally, with a sublayer 5 underneath first layer 6. First layer 6 may comprise rhodium or pure gold or gold comprising traces of elements such as cobalt or nickel, and sublayer 5 can comprise nickel, such as NiP or pure electroplated Ni, or pure gold or gold with trace elements. The first layer has a thickness comprised between 100 nm and 2 m, and the sublayer has a thickness comprised between 100 nm and 2 m.

(11) Protective layer 7, which is more particularly the subject of the invention, is a barrier layer deposited after assembly. This layer is formed of a single layer or of a stack of layers. Each layer respectively comprises SiO.sub.2, Al.sub.2O.sub.3, Rh, Au, Ni or NiP with low P (2-4% by weight), medium P (5-9% by weight) or high P (10-13% weight). Preferably, each layer respectively consists of SiO.sub.2, Al.sub.2O.sub.3, Rh, Au, Ni or NiP with low P (2-4% by weight), medium P (5-9% by weight) or high P (10-13% weight). The protective layer has a thickness comprised between 20 nm and 3 m, and preferably between 100 nm and 500 nm. For the variant with a stack of layers, all the layers have a thickness comprised between 20 nm and 3 m, preferably between 100 nm and 500 nm.

(12) According to the invention, at least one part of the surface of the assembly is coated with the protective layer intended to cover defects at the end of the assembly process. Advantageously, at least the surface of the component subjected to deformation during assembly is coated. Preferably, the entire external surface of the timepiece assembly is coated with the protective layer.

(13) Protective layer 7 deposited after assembly is thus devoid of defects and more particularly of cracks and incipient cracks.

(14) The present invention also relates to the method of manufacturing the timepiece assembly including the following steps: a) Providing the first component and the second component, b) Assembling the first component and the second component under stress, c) Depositing protective layer 7, also called the second layer, on at least one part of the surface of the assembly comprising the first component and the second component.

(15) According to the invention, the protective layer is deposited by ALD (Atomic Layer Deposition), PVD (Physical Vapour Deposition), CVD (Chemical Vapour Deposition), chemical or electroplating deposition.

(16) The method may also comprise a step a) of depositing first layer 6 on at least one part of the first component and/or of the second component prior to assembly step b).

(17) The method may also include a step a) of depositing sublayer 5 on said at least one part of the first component and/or of the second component prior to step a).

(18) The sublayer and the first layer can also be deposited by ALD, PVD, CVD, chemical or electroplating deposition.

(19) The method may also include a heat treatment step a) intended to improve the adherence of the first layer and the sublayer if these latter are present. This step occurs prior to assembly step b). The heat treatment is carried out between 150 and 300 C. for 30 minutes to 5 hours. In a variant, the method includes a step d) of this same heat treatment after step c) of depositing the protective layer. According to another variant, the method includes a step a) of this heat treatment prior to assembly step b) and a step d) of this heat treatment after step c) of depositing the protective layer.

KEY

(20) (1) Timepiece assembly (2) Balance a. Resilient arm (3) Inertia screw a. Shaft (4) Slot (5) Sublayer deposited prior to assembly (6) Layer deposited prior to assembly, also called the first layer (7) Layer deposited after assembly, also called the protective layer or second layer (8) Crack or incipient crack (9) Coating material of the sample seen in an electron microscope view