CH716645A2 - Process for manufacturing a clothing component for a timepiece or piece of jewelery and clothing component made of a coated material of natural origin. - Google Patents

Process for manufacturing a clothing component for a timepiece or piece of jewelery and clothing component made of a coated material of natural origin. Download PDF

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Publication number
CH716645A2
CH716645A2 CH01239/19A CH12392019A CH716645A2 CH 716645 A2 CH716645 A2 CH 716645A2 CH 01239/19 A CH01239/19 A CH 01239/19A CH 12392019 A CH12392019 A CH 12392019A CH 716645 A2 CH716645 A2 CH 716645A2
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CH
Switzerland
Prior art keywords
piece
thickness
trim piece
covering
trim
Prior art date
Application number
CH01239/19A
Other languages
French (fr)
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CH716645B1 (en
Inventor
Pascal Bächler Bernard
Original Assignee
Sandrine Blumenthal
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 Sandrine Blumenthal filed Critical Sandrine Blumenthal
Priority to CH01239/19A priority Critical patent/CH716645B1/en
Publication of CH716645A2 publication Critical patent/CH716645A2/en
Publication of CH716645B1 publication Critical patent/CH716645B1/en

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Classifications

    • AHUMAN NECESSITIES
    • A44HABERDASHERY; JEWELLERY
    • A44CPERSONAL ADORNMENTS, e.g. JEWELLERY; COINS
    • A44C27/00Making jewellery or other personal adornments
    • A44C27/001Materials for manufacturing jewellery
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B44DECORATIVE ARTS
    • B44CPRODUCING DECORATIVE EFFECTS; MOSAICS; TARSIA WORK; PAPERHANGING
    • B44C5/00Processes for producing special ornamental bodies
    • B44C5/04Ornamental plaques, e.g. decorative panels, decorative veneers
    • B44C5/0438Ornamental plaques, e.g. decorative panels, decorative veneers containing stone elements
    • GPHYSICS
    • G04HOROLOGY
    • G04BMECHANICALLY-DRIVEN CLOCKS OR WATCHES; MECHANICAL PARTS OF CLOCKS OR WATCHES IN GENERAL; TIME PIECES USING THE POSITION OF THE SUN, MOON OR STARS
    • G04B19/00Indicating the time by visual means
    • G04B19/06Dials
    • G04B19/12Selection of materials for dials or graduations markings
    • GPHYSICS
    • G04HOROLOGY
    • G04BMECHANICALLY-DRIVEN CLOCKS OR WATCHES; MECHANICAL PARTS OF CLOCKS OR WATCHES IN GENERAL; TIME PIECES USING THE POSITION OF THE SUN, MOON OR STARS
    • G04B19/00Indicating the time by visual means
    • G04B19/06Dials
    • G04B19/14Fastening the dials to the clock or watch plates
    • GPHYSICS
    • G04HOROLOGY
    • G04DAPPARATUS OR TOOLS SPECIALLY DESIGNED FOR MAKING OR MAINTAINING CLOCKS OR WATCHES
    • G04D3/00Watchmakers' or watch-repairers' machines or tools for working materials
    • G04D3/0002Watchmakers' or watch-repairers' machines or tools for working materials for mechanical working other than with a lathe
    • G04D3/0043Watchmakers' or watch-repairers' machines or tools for working materials for mechanical working other than with a lathe for components of the time-indicating mechanisms
    • G04D3/0048Watchmakers' or watch-repairers' machines or tools for working materials for mechanical working other than with a lathe for components of the time-indicating mechanisms for dials
    • GPHYSICS
    • G04HOROLOGY
    • G04DAPPARATUS OR TOOLS SPECIALLY DESIGNED FOR MAKING OR MAINTAINING CLOCKS OR WATCHES
    • G04D3/00Watchmakers' or watch-repairers' machines or tools for working materials
    • G04D3/0074Watchmakers' or watch-repairers' machines or tools for working materials for treatment of the material, e.g. surface treatment
    • G04D3/0092Watchmakers' or watch-repairers' machines or tools for working materials for treatment of the material, e.g. surface treatment for components of the time-indicating mechanism, e.g. dials
    • GPHYSICS
    • G04HOROLOGY
    • G04DAPPARATUS OR TOOLS SPECIALLY DESIGNED FOR MAKING OR MAINTAINING CLOCKS OR WATCHES
    • G04D3/00Watchmakers' or watch-repairers' machines or tools for working materials
    • G04D3/02Lathes, with one or more supports; Burnishing machines, with one or more supports
    • G04D3/0227Lathes, with one or more supports; Burnishing machines, with one or more supports for the manufacture of special components for clockworks
    • G04D3/0272Lathes, with one or more supports; Burnishing machines, with one or more supports for the manufacture of special components for clockworks for components of the time-indicating mechanism, e.g. dials
    • GPHYSICS
    • G04HOROLOGY
    • G04BMECHANICALLY-DRIVEN CLOCKS OR WATCHES; MECHANICAL PARTS OF CLOCKS OR WATCHES IN GENERAL; TIME PIECES USING THE POSITION OF THE SUN, MOON OR STARS
    • G04B37/00Cases
    • G04B37/22Materials or processes of manufacturing pocket watch or wrist watch cases
    • G04B37/225Non-metallic cases
    • GPHYSICS
    • G04HOROLOGY
    • G04DAPPARATUS OR TOOLS SPECIALLY DESIGNED FOR MAKING OR MAINTAINING CLOCKS OR WATCHES
    • G04D3/00Watchmakers' or watch-repairers' machines or tools for working materials
    • G04D3/0002Watchmakers' or watch-repairers' machines or tools for working materials for mechanical working other than with a lathe
    • G04D3/0061Watchmakers' or watch-repairers' machines or tools for working materials for mechanical working other than with a lathe for components for protecting the mechanism against external influences
    • G04D3/0064Watchmakers' or watch-repairers' machines or tools for working materials for mechanical working other than with a lathe for components for protecting the mechanism against external influences for cases

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Adornments (AREA)

Abstract

L'invention concerne un procédé de fabrication et un composant d'habillement (100 ; 100*) pour pièce d'horlogerie ou de joaillerie, lequel composant d'habillement (100 ; 100*) comprend au moins une pièce (10) réalisée en un matériau d'origine naturelle. Le procédé comporte les étapes suivantes : (i) fourniture d'une pièce d'habillage (10) réalisée en un matériau d'origine naturelle ; (ii) préparation d'une première surface (10A), ou surface supérieure, de la pièce d'habillage (10) de façon à pouvoir recevoir un adhésif (15) ; (iii) application de l'adhésif (15) directement ou indirectement sur la première surface (10A) de la pièce d'habillage (10) ; (iv) jonction, via l'adhésif (15), d'une pièce de revêtement (20) réalisée en un matériau transparent, en particulier un verre, avec la première surface (10A) de la pièce d'habillage (10) ; (v) durcissement de l'adhésif (15) de manière à rendre la pièce de revêtement (20) solidaire de la pièce d'habillage (10) ; et (vi) usinage, en particulier par rodage, d'une seconde surface (108), ou surface inférieure, de la pièce d'habillage (10) de façon à réduire l'épaisseur de la pièce d'habillage (10) à une épaisseur cible (W10.1). Le composant d'habillement (100) peut être un cadran en pierre naturelle ou en matériau fossilisé.The invention relates to a manufacturing method and a clothing component (100; 100*) for a timepiece or piece of jewelry, which clothing component (100; 100*) comprises at least one part (10) made of a material of natural origin. The method includes the following steps: (i) providing a trim piece (10) made of a material of natural origin; (ii) preparing a first surface (10A), or top surface, of the trim piece (10) to receive an adhesive (15); (iii) applying the adhesive (15) directly or indirectly to the first surface (10A) of the trim piece (10); (iv) joining, via the adhesive (15), of a covering part (20) made of a transparent material, in particular a glass, with the first surface (10A) of the covering part (10); (v) curing the adhesive (15) so as to make the cover piece (20) integral with the trim piece (10); and (vi) machining, in particular by lapping, of a second surface (108), or lower surface, of the trim piece (10) so as to reduce the thickness of the trim piece (10) to a target thickness (W10.1). The clothing component (100) can be a dial made of natural stone or fossilized material.

Description

Description Description

DOMAINE TECHNIQUE TECHNICAL AREA

[0001] La presente Invention se rapporte de maniere generale au domaine de l'horlogerie et de la joaillerie, et plus particulierement ä un procede de fabrication d'un composant d'habillement pour piece d'horlogerie ou de joaillerie ainsi qu'ä un composant d'habillement obtenu selon ce procede. Ce composant d'habillement peut en particulier etre un cadran pour piece d'horlogerie. [0001] The present invention relates generally to the field of watchmaking and jewelry, and more particularly to a method of manufacturing a component of clothing for a piece of timepiece or jewelry as well as to a clothing component obtained by this process. This clothing component can in particular be a dial for a timepiece.

ARRIERE-PLAN TECHNOLOGIQUE TECHNOLOGICAL BACKGROUND

[0002] La fabrication de cadrans pour pieces d'horlogerie constitue une branche ä part entiere dans le domaine de l'horlogerie. Une vaste majorite des cadrans utilises dans l'horlogerie sont realises en matiere metallique et comportent classiquement un element de support sensiblement plat et mince, lequel porte typiquement des indications des heures et des minutes ainsi que divers elements decoratifs qui peuvent etre etampes, graves, imprimes et/ou appliques sur l'element de support. II est egalement courant de former des guichets et autres ouvertures traversantes au travers du cadran afin de permettre le passage ou laisser apparaitre des Organes indicateurs ou d'autres Organes mecaniques du mouvement horloger qui se trouve classiquement derriere le cadran. [0002] The manufacture of dials for timepieces constitutes a branch in its own right in the field of watchmaking. A vast majority of dials used in watchmaking are made of metallic material and conventionally comprise a substantially flat and thin support element, which typically bears hour and minute indications as well as various decorative elements which may be stamped, engraved, printed and/or applied to the support element. It is also common to form apertures and other through openings through the dial in order to allow the passage or reveal Indicator Organs or other Mechanical Organs of the watch movement which is conventionally located behind the dial.

[0003] Pour les pieces d'horlogerie de tres haut de gamme, il est egalement connu de faire usage de cadrans emailles ou decores ä la main, ainsi que de cadrans faisant appel ä des matieres d'origine naturelle, tel la nacre ou un materiau mineral provenant de pierres naturelles. Ces matieres d'origine naturelle sont tres souvent fragiles et difficiles ä usiner, en particulier en vue de realiser des elements aussi minces que des cadrans, et l'utilisation de ces matieres peut engendrer beaucoup de dechets en raison de leur fragilite. Ces matieres d'origine naturelle peuvent egalement presenter des imperfections et/ou irregularites qui sont susceptibles de conduire ä leur rejet d'un point de vue qualitatif. [0003] For very high-end timepieces, it is also known to make use of enamelled or hand-decorated dials, as well as dials using materials of natural origin, such as mother-of-pearl or a mineral material from natural stones. These materials of natural origin are very often fragile and difficult to machine, in particular with a view to producing elements as thin as dials, and the use of these materials can generate a great deal of waste because of their fragility. These materials of natural origin may also present imperfections and/or irregularities which are likely to lead to their rejection from a qualitative point of view.

[0004] La demande de brevet suisse No. CH 649 670 G A3 decrit un procede de fabrication d'un composant de l'habillement d'un garde-temps comprenant une premiere piece en un materiau non metallique difficilement usinable, teile uneplaque de cadran en verre mineral ou en une pierre semi-precieuse, liee ä demeure ä au moins une seconde piece metallique, laquelle est formee par croissance dans un bain galvanique ou chimique directement sur une portion de la surface inferieure de la premiere piece, au moins une couche de revetement mince metallique ayant ete formee au prealable sur la portion de la surface inferieure de la premiere piece par depöt de particules en phase gazeuse. Dans ce contexte, la plaque de cadran en verre mineral ou en pierre semi-precieuse est usinee au prealable de maniere ä avoir la minceur requise etetre pourvue d'au moins un trou central pour le passage des axes des aiguilles et deux faces principales paralleles qui sont polies de fapon ä presenter leur etat de surface definitif. Dans une premiere etape, cette plaque de cadran mince est collee dans une noyure menagee dans le fond d'un logement pratique dans une matrice en matiere plastique de Sorte ä etre rendue solidaire de cette matrice. Un revetement forme d'un metal conducteur d'electricite est ensuite forme sur toute la surface du logement de la matrice, en ce incluse la surface inferieure de la plaque de cadran mince, selon un procede de metallisation par evaporation sous vide ou par projection d'ions. Ce revetement est realise de Sorte ä etre suffisamment adherent et epais pour assurer la liaison avec la plaque de cadran mince et le corps de support metallique qui est forme au cours de l'operation d'electroformage subsequente. Cette Operation d'electroformage s'effectue en plapant la matrice avec la plaque de cadran mince pourvue du revetement conducteur dans un bain galvanique apte ä provoquer le depöt d'un metal, tel que du nickel ou un metal noble tel que de l'or, du platine ou de l'argent, voire un alliage presentant les proprietes et les caracteristiques desirees. Le corps metallique qui se forme au cours de l'operation galvanique presente une surface inferieure irreguliere, laquelle est usinee. Le reste de la matrice en matiere plastique est ensuite eliminee, de sorte que l'on obtient un cadran composite presentant la plaque de cadran mince et une garniture metallique qui s'etend sous la plaque de cadran mince et autour de sa peripherie, garniture metallique sur la surface inferieure de laquelle il est encore procede au soudage d'un ou plusieurs pieds pour permettre la fixation du cadran. II est explicitement evoque que la plaque de cadran mince en verre mineral ou pierre semi-precieuse peut presenter une epaisseur extremement mince del'ordre de 0.2 mm tandis que la garniture peut presenter une epaisseur de l'ordre de 0.15 mm ou meme moins, conduisant ainsi ä une epaisseur totale du cadran composite inferieure ä 0.4 mm, epaisseur usuelle des cadrans. [0004] Swiss patent application No. CH 649 670 G A3 describes a method of manufacturing a component of the clothing of a timepiece comprising a first part made of a non-metallic material that is difficult to machine, such as a dial plate of mineral glass or of a semi-precious stone, permanently bonded to at least one second metal part, which is formed by growth in a galvanic or chemical bath directly on a portion of the lower surface of the first part, at least one layer of thin metallic coating having been formed beforehand on the portion of the lower surface of the first part by deposition of particles in the gas phase. In this context, the dial plate in mineral glass or semi-precious stone is machined beforehand so as to have the required thinness and to be provided with at least one central hole for the passage of the axes of the hands and two parallel main faces which are polished so as to present their final surface condition. In a first stage, this thin dial plate is glued in a recess formed in the bottom of a practical housing in a matrix of plastic material so as to be made integral with this matrix. A coating formed of an electrically conductive metal is then formed over the entire surface of the die housing, including the lower surface of the thin dial plate, according to a process of metallization by vacuum evaporation or by spraying. ions. This coating is made so as to be sufficiently adherent and thick to bond with the thin dial plate and the metal support body which is formed during the subsequent electroforming operation. This electroforming operation is carried out by placing the matrix with the thin dial plate provided with the conductive coating in a galvanic bath capable of causing the deposit of a metal, such as nickel or a noble metal such as gold. , platinum or silver, or even an alloy having the desired properties and characteristics. The metal body which is formed during the galvanic operation has an irregular lower surface, which is machined. The rest of the plastic matrix is then eliminated, so that a composite dial is obtained having the thin dial plate and a metal trim which extends under the thin dial plate and around its periphery, metal trim on the lower surface of which it is still proceeded to the welding of one or more feet to allow the fixing of the dial. It is explicitly mentioned that the thin dial plate made of mineral glass or semi-precious stone may have an extremely thin thickness of the order of 0.2 mm while the trim may have a thickness of the order of 0.15 mm or even less, leading thus to a total thickness of the composite dial of less than 0.4 mm, the usual thickness of dials.

[0005] Le procede decrit dans la demande de brevet suisse No. CH 649 670 G A3 permet certes la production d'un cadran relativement mince, mais ce procede n'apporte aucune amelioration particuliere quant ä la fabrication et l'usinage de la plaque de cadran mince en verre mineral ou pierre semi-precieuse en tant que teile. La production d'une teile plaque decadran mince ä une epaisseur aussi faible que 0.2 mm reste en particulier un defi tres difficile ä atteindre en pratique. [0005] The process described in Swiss patent application No. CH 649 670 G A3 certainly allows the production of a relatively thin dial, but this process does not bring any particular improvement as regards the manufacture and machining of the plate. thin dial in mineral glass or semi-precious stone as a bezel. The production of such a thin dial plate at a thickness as low as 0.2 mm remains in particular a very difficult challenge to achieve in practice.

[0006] Des artifices consistant ä produire des cadrans constitues de verres ou pierres synthetiques ont egalement ete proposes, par exemple dans les brevets suisses Nos. CH 522 247 A et CH 535 983 A ou dans le brevet americain No. US 3,793,824 A, mais ces Solutions ne sont en rien satisfaisantes dans la mesure oü il n'est plus question d'utiliser des matieres minerales naturelles pour la fabrication du cadran, mais des compositions qui visent ä approcher l'apparence de matieres minerales naturelles sans toutefois parvenir ä egaler la finesse et l'elegances des matieres minerales naturelles. [0006]Artificial devices consisting in producing dials made of glass or synthetic stones have also been proposed, for example in Swiss patents Nos. CH 522 247 A and CH 535 983 A or in American patent No. US 3,793,824 A, but these Solutions are in no way satisfactory insofar as there is no longer any question of using natural mineral materials for the manufacture of the dial , but compositions that aim to approach the appearance of natural mineral materials without however managing to match the finesse and elegance of natural mineral materials.

[0007] On connait encore des Solutions qui consistent ä produire des cadrans sur la base de verres de Murano (voir le brevet americain No. US 5,109,635 A) ou de matieres vegetales, tel le bois ou de l'ivoire vegetal par exemple (voir par exemple le brevet americain No. US 5,555,535 A). [0007] Solutions are still known which consist in producing dials on the basis of Murano glass (see American patent No. US 5,109,635 A) or vegetable materials, such as wood or vegetable ivory for example (see for example US Patent No. US 5,555,535 A).

[0008] II subsiste donc un reel besoin pour proposer un procede de fabrication d'un composant d'habillement pour piece d'horlogerie ou de joaillerie qui seit plus apte ä permettre un usinage fiable de matieres d'origine naturelle, en particulier de materiaux mineraux provenant de pierres naturelles ou de matieres fossilisees. [0008]There therefore remains a real need to propose a process for manufacturing a component of clothing for a timepiece or piece of jewelery which is more suitable for allowing reliable machining of materials of natural origin, in particular materials minerals from natural stones or fossilized materials.

EXPOSE DE L'INVENTION DISCLOSURE OF THE INVENTION

[0009] Un but general de la presente Invention est donc d'ameliorer les procedes de fabrication de composants d'habillement pour pieces d'horlogerie ou de joaillerie comprenant au moins une piece realisee en un materiau d'origine naturelle. [0009] A general purpose of the present invention is therefore to improve the methods of manufacturing clothing components for timepieces or jewelry comprising at least one piece made of a material of natural origin.

[0010] Plus particulierement, un but de la presente invention est de proposer une solution qui assure un meilleur rendement de fabrication et reduise drastiquement les risques de dechets. [0010] More particularly, an object of the present invention is to provide a solution which ensures better manufacturing efficiency and drastically reduces the risk of waste.

[0011] Plus specifiquement encore, un but de la presente invention est de proposer une teile solution qui soit particulierement adaptee ä la manipulation et l'usinage de materiaux mineraux, en particulier de materiaux mineraux provenant de pierres naturelles ou de matieres fossilisees, ainsi que d'autres materiaux d'origine naturelle difficiles ä usiner selon les procedes classiques. [0011] Even more specifically, an object of the present invention is to provide such a solution which is particularly suitable for handling and machining mineral materials, in particular mineral materials originating from natural stones or fossilized materials, as well as other materials of natural origin which are difficult to machine using conventional methods.

[0012] La presente invention repond ä ces buts en proposant un procede de fabrication d'un composant d'habillement pour piece d'horlogerie ou de joaillerie dont les caracteristiques sont enumerees dans la revendication 1. Plus precisement, il est prevu un tel procede de fabrication d'un composant d'habillement pour piece d'horlogerie ou de joaillerie, lequel composant d'habillement comprend au moins une piece realisee en un materiau d'origine naturelle, le procede comportant les etapes suivantes : [0012] The present invention responds to these aims by proposing a method of manufacturing a clothing component for a timepiece or piece of jewelry, the characteristics of which are listed in claim 1. More specifically, such a method is provided manufacturing a clothing component for a timepiece or jewelry piece, which clothing component comprises at least one piece made of a material of natural origin, the process comprising the following steps:

(i) fourniture d'une piece d'habillage realisee en un materiau d'origine naturelle ; (i) supply of a trim piece made of a material of natural origin;

(ii) preparation d'une premiere surface, ou surface superieure, de la piece d'habillage de faqon ä pouvoir recevoir un adhesif; (ii) preparing a first surface, or upper surface, of the trim piece so as to be able to receive an adhesive;

(iii) application de l'adhesif directement ou indirectement sur la premiere surface de la piece d'habillage ; (iii) applying the adhesive directly or indirectly to the first surface of the trim piece;

(iv) jonction, via l'adhesif, d'une piece de revetement realisee en un materiau transparent, en particulier un verre, avec la premiere surface de la piece d'habillage ; (iv) joining, via the adhesive, of a covering piece made of a transparent material, in particular a glass, with the first surface of the covering piece;

(v) durcissement de l'adhesif de maniere ä rendre la piece de revetement solidaire de la piece d'habillage ; et (v) hardening of the adhesive so as to make the covering piece integral with the covering piece; And

(vi) usinage, en particulier par rodage, d'une seconde surface, ou surface inferieure, de la piece d'habillage de fagon ä reduire l'epaisseur de la piece d'habillage ä une epaisseur cible. (vi) machining, in particular by lapping, a second surface, or lower surface, of the trim piece so as to reduce the thickness of the trim piece to a target thickness.

[0013] Selon un Variante de realisation preferee, l'usinage (vi) de la seconde surface de la piece d'habillage est opere de fagon ä reduire l'epaisseur de la piece d'habillage ä une premiere epaisseur cible, en particulier une premiere epaisseur cible inferieure ou egale ä 0.5 mm, et un usinage ulterieur de la seconde surface de la piece d'habillage est optionnellement opere, dans une phase de finissage, de fagon ä reduire l'epaisseur de la piece d'habillage ä une seconde epaisseur cible inferieure ä la premiere epaisseur cible, en particulier une seconde epaisseur cible inferieure ou egale ä 0.2 mm. [0013] According to a preferred alternative embodiment, the machining (vi) of the second surface of the trim piece is carried out so as to reduce the thickness of the trim piece to a first target thickness, in particular a first target thickness less than or equal to 0.5 mm, and subsequent machining of the second surface of the trim piece is optionally carried out, in a finishing phase, so as to reduce the thickness of the trim piece to a second target thickness less than the first target thickness, in particular a second target thickness less than or equal to 0.2 mm.

[0014] La piece d'habillage peut avantageusement presenter une epaisseur initiale superieure ä 0.5 mm avant l'usinage (vi) de la seconde surface de la piece d'habillage. De la Sorte, le risque de rupture de la piece d'habillage est considerablement reduit. [0014] The trim piece can advantageously have an initial thickness greater than 0.5 mm before the machining (vi) of the second surface of the trim piece. In this way, the risk of breakage of the trim piece is considerably reduced.

[0015] A titre prefere, la piece de revetement presente une epaisseur initiale superieure ä une epaisseur cible, laquelle epaisseur initiale est preferablement superieure ou egale ä 1 mm, et le procede comporte en outre les etapes supplementaires suivantes : [0015] As a preference, the coating piece has an initial thickness greater than a target thickness, which initial thickness is preferably greater than or equal to 1 mm, and the method further comprises the following additional steps:

(vii) usinage, en particulier par rodage, d'une surface superieure de la piece de revetement de fagon ä reduire l'epaisseur de la piece de revetement ä une epaisseur cible ; (vii) machining, particularly by lapping, an upper surface of the liner piece so as to reduce the thickness of the liner piece to a target thickness;

(viii)polissage de la surface superieure de la piece de revetement de fagon ä presenter une finition polie ; et (viii) polishing the top surface of the liner piece to present a polished finish; And

(ix)optionnellement, application ou creation d'elements decoratifs sur la surface superieure de la piece de revetement. (ix) optionally, application or creation of decorative elements on the upper surface of the piece of covering.

[0016] Dans ce contexte, l'epaisseur cible de la piece de revetement peut en particulier etre inferieure ou egale ä 0.15 mm. [0016] In this context, the target thickness of the coating piece may in particular be less than or equal to 0.15 mm.

[0017] Par ailleurs, l'usinage (vii) de la surface superieure de la piece de revetement est preferablement realise apres l'usinage (vi) de la seconde surface de la piece d'habillage. A cet egard, la piece de revetement remplit ainsi avantageusement le röle, durant l'usinage (vi) de la seconde surface de la piece d'habillage, de support et renfort pour la piece d'habillage. La reduction de l'epaisseur de la piece d'habillage ä l'epaisseur cible souhaitee peut ainsi etre operee en reduisant drastiquement les risques de cassure de la piece d'habillage. Furthermore, the machining (vii) of the upper surface of the covering piece is preferably carried out after the machining (vi) of the second surface of the trim piece. In this respect, the covering piece thus advantageously fulfills the role, during the machining (vi) of the second surface of the trim piece, of support and reinforcement for the trim piece. The reduction of the thickness of the covering part to the desired target thickness can thus be carried out by drastically reducing the risks of breakage of the covering part.

[0018] Selon un mode de realisation avantageux de l'invention, le procede comporte en outre l'une et/ou l'autre des etapes de finissage suivantes : According to an advantageous embodiment of the invention, the method further comprises one and/or the other of the following finishing steps:

- application, sur la seconde surface de la piece d'habillage, d'une couche de contraste, preferablement opaque ; et - application, on the second surface of the trim piece, of a contrast layer, preferably opaque; And

- realisation, sur au moins la seconde surface de la piece d'habillage, d'une garniture ou structure, preferablementmetallique, destinee au montage du composant d'habillement dans la piece d'horlogerie ou de joaillerie. - production, on at least the second surface of the casing piece, of a trim or structure, preferably metallic, intended for mounting the casing component in the timepiece or jewelry piece.

[0019] Dans le cadre de la presente invention, l'adhesif est preferablement un adhesif ä durcissement aux ultraviolets (UV) et l'etape de durcissement (v) comporte l'application d'ultraviolets (UV) sur la premiere surface de la piece d'habillage. Cette exposition aux ultraviolets (UV) peut etre operee sans contrainte particuliere au travers de la piece de revetement, sous reserve que celle-ci soit realise dans un materiau transparent laissant passer sensiblement toute la gamme de longueursd'onde necessaire ä l'amorpage du processus de reticulation de l'adhesif utilise. [0019] In the context of the present invention, the adhesive is preferably an ultraviolet (UV) curing adhesive and the curing step (v) comprises the application of ultraviolet (UV) rays to the first surface of the dressing piece. This exposure to ultraviolet rays (UV) can be carried out without any particular constraint through the piece of coating, provided that the latter is made of a transparent material allowing substantially the entire range of wavelengths necessary for the priming of the process to pass. crosslinking of the adhesive used.

[0020] Selon un mode de realisation particulierement prefere, lequel est notamment mis en oeuvre dans le cadre de la production de cadrans pour pieces d'horlogerie, le procede comporte en outre une etape d'usinage supplementaire consistant ä pratiquer une ou plusieurs ouvertures traversantes, tel un trou central ou un guichet, au travers de la piece d'habillage. Dans ce contexte, il est particulierement avantageux que chaque ouverture traversante soit realisee de Sorte ä penetrer partiellement dans la piece de revetement sur une distance superieure ä une epaisseur cible de la piece de revetement. [0020] According to a particularly preferred embodiment, which is implemented in particular in the context of the production of dials for timepieces, the method also comprises an additional machining step consisting in making one or more through openings , such as a central hole or a window, through the trim piece. In this context, it is particularly advantageous for each through-opening to be made in such a way as to partially penetrate the covering piece over a distance greater than a target thickness of the covering piece.

[0021] Le materiau d'origine naturelle constitutif de la piece d'habillage est preferablement un materiau mineral, tel un materiau mineral provenant de pierres naturelles ou de matieres fossilisees, d'autres materiaux etant toutefois envisageables. Dans ce contexte, l'invention apporte des avantages considerables en rapport ä l'usinage de pierres naturelles ou de matieres fossilisees particulierement fragiles et/ou friables, en particulier les materiaux mineraux presentant des difficultes d'usinage notamment en raison de leur clivage, de leur structure fibreuse, de leur structure microcristalline, de differences de durete, de leur porosite, de la presence de fissures ou autres irregularites et/ou d'une finition polie irreguliere. The material of natural origin constituting the trim piece is preferably a mineral material, such as a mineral material from natural stones or fossilized materials, other materials being however possible. In this context, the invention provides considerable advantages in relation to the machining of natural stones or particularly fragile and/or friable fossilized materials, in particular mineral materials presenting machining difficulties in particular because of their cleavage, their fibrous structure, their microcrystalline structure, differences in hardness, their porosity, the presence of cracks or other irregularities and/or an irregular polished finish.

[0022] Le materiau d'origine naturelle constitutif de la piece d'habillage peut alternativement etre : [0022] The material of natural origin constituting the trim piece can alternatively be:

- un materiau d'origine extraterrestre, tel un materiau provenant de meteorites non differenciees ou de meteorites differenciees, parmi lesquelles les meteorites chondrites, les meteorites achondrites, les meteorites de fer, et les meteorites mixtes ; - material of extraterrestrial origin, such as material from undifferentiated meteorites or differentiated meteorites, including chondrite meteorites, achondrite meteorites, iron meteorites, and mixed meteorites;

- un materiau mineral biosynthetise, teile la nacre ; ou encore - a biosynthesized mineral material, such as mother-of-pearl; or

- un materiau organique, teile bois, l'ivoire vegetal, l'ambre, le copal, le jais, ou la mellite. - an organic material, such as wood, vegetable ivory, amber, copal, jet, or mellite.

[0023] S'agissant du materiau transparent constitutif de la piece de revetement, il est en particulier souhaitable de faire appel ä un verre ä base de silice ou ä un verre mineral, par exemple un verre saphir. L'utilisation d'un verre ä base de silice s'avere particulierement avantageuse dans la mesure oü l'usinage d'un tel verre est relativement aise et que l'execution d'un polissage de la surface d'un tel verre permet d'obtenir un excellent rendu et une grande qualite de surface, sans pour autant que cela necessite des outils et moyens de polissage complexes et coüteux. En realite, une resultante de la mise en oeuvre de l'invention est que l'operation de polissage est effectuee sur une surface de la piece de revetement, et non sur une surface de la piece d'habillage. En d'autres termes, les outils et moyens de polissage requis doivent uniquement etre adaptes au type de materiau transparent utilise comme materiau constitutif de la piece de revetement et ne sont pas impactes par le materiau d'origine naturelle constitutif de la piece d'habillage. [0023] With regard to the transparent material constituting the covering piece, it is in particular desirable to use a silica-based glass or a mineral glass, for example a sapphire glass. The use of a silica-based glass proves to be particularly advantageous insofar as the machining of such a glass is relatively easy and that the execution of a polishing of the surface of such a glass makes it possible to to obtain an excellent finish and a high surface quality, without this requiring complex and expensive tools and polishing means. In reality, one result of the implementation of the invention is that the polishing operation is carried out on a surface of the coating part, and not on a surface of the trim part. In other words, the tools and polishing means required must only be adapted to the type of transparent material used as the constituent material of the covering part and are not impacted by the material of natural origin constituting the trim part. .

[0024] L'invention permet avantageusement la production de composants d'habillement ä des epaisseurs reduites, en particulier des cadrans pour pieces d'horlogerie presentant une epaisseur totale inferieure ou egale ä 0.4 mm, epaisseur usuelle des cadrans utilises dans le domaine de l'horlogerie. [0024] The invention advantageously allows the production of clothing components with reduced thicknesses, in particular dials for timepieces having a total thickness less than or equal to 0.4 mm, the usual thickness of dials used in the field of watchmaking.

[0025] II est egalement revendique, au titre de la revendication 10, un composant d'habillement pour piece d'horlogerie ou de joaillerie, en particulier un composant d'habillement obtenu selon le procede de l'invention, le composant d'habillement comprenant une piece d'habillage realisee en un materiau d'origine naturelle et une piece de revetement realisee en un materiau transparent, en particulier un verre, laquelle piece de revetement est rendue solidaire d'une premiere surface, ou surface superieure, de la piece d'habillage au moyen d'un adhesif. Ce composant d'habillement est preferablement un cadran pour piece d'horlogerie ou un produit intermediaire employe dans la fabrication dudit cadran. [0025] There is also claimed, under claim 10, a clothing component for a timepiece or piece of jewelry, in particular a clothing component obtained according to the method of the invention, the clothing component comprising a covering part made of a material of natural origin and a covering part made of a transparent material, in particular a glass, which covering part is secured to a first surface, or upper surface, of the part covering with an adhesive. This clothing component is preferably a dial for a timepiece or an intermediate product used in the manufacture of said dial.

[0026] D'autres aspects de l'invention sont exposes dans la suite de la presente description. Other aspects of the invention are set out in the remainder of this description.

DESCRIPTION SOMMAIRE DES DESSINS BRIEF DESCRIPTION OF THE DRAWINGS

[0027] Les caracteristiques et avantages de la presente invention apparaftront plus clairement ä la lecture de la description detaillee qui suit de modes de realisation de l'invention, lesquels sont presentes uniquement ä titre d'exemples non limitatifs et sont illustres par les dessins annexes oü : The characteristics and advantages of the present invention will appear more clearly on reading the following detailed description of embodiments of the invention, which are presented solely by way of non-limiting examples and are illustrated by the appended drawings. Or :

- les Figures 1Aä 1G sont des vues en coupe laterale illustrant schematiquement une succession d'etapes defabricationconduisant ä un produit intermediaire utilise dans le cadre de la production d'un cadran pour piece d'horlogerie, selon un mode de realisation de l'invention ; - Figures 1A to 1G are side section views schematically illustrating a succession of manufacturing steps leading to an intermediate product used in the context of the production of a dial for a timepiece, according to one embodiment of the invention;

- les Figures 2A ä 2E sont des vues en coupe laterale illustrant schematiquement une succession d'etapes de fabricationsupplementaires conduisant, ä partir du produit intermediaire obtenu seien les etapes de fabrication illustrees dans les Figures 1A ä 1G, ä un cadran pour piece d'horlogerie, selon un mode de realisation prefere de l'invention ; et - Figures 2A to 2E are side section views schematically illustrating a succession of additional manufacturing steps leading, from the intermediate product obtained following the manufacturing steps illustrated in Figures 1A to 1G, to a dial for a timepiece , according to a preferred embodiment of the invention; And

- la Figure 3 est un Illustration schematique d'un cadran, en coupe laterale, obtenu selon le procede des Figures 1A ä1G et 2A ä 2E, lequel cadran est par ailleurs pourvu d'une structure destinee au montage du cadran dans une piece d'horlogerie. - Figure 3 is a schematic illustration of a dial, in lateral section, obtained according to the method of Figures 1A to 1G and 2A to 2E, which dial is also provided with a structure intended for mounting the dial in a piece of watchmaking.

MODES DE REALISATION DE L'INVENTION EMBODIMENTS OF THE INVENTION

[0028] La presente Invention sera decrite en reference ä divers modes de realisation preferes tels qu'illustres notamment par les Figures 1A-G ä 3. L'invention sera decrite dans le contexte particulier de la production d'un cadran pour pieced'horlogerie (et d'un produit intermediaire employe dans la fabrication dudit cadran), mais il est entendu que l'invention est applicable ä la production de tout composant d'habillement pour piece d'horlogerie ou de joaillerie oü le composant d'habillement comprend au moins une piece realisee en un materiau d'origine naturelle. [0028] The present invention will be described with reference to various preferred embodiments as illustrated in particular by Figures 1A-G to 3. The invention will be described in the particular context of the production of a dial for a timepiece (and an intermediate product used in the manufacture of said dial), but it is understood that the invention is applicable to the production of any clothing component for a timepiece or piece of jewelery where the clothing component comprises at least least one part made of a material of natural origin.

[0029] L'invention sera plus specifiquement decrite dans le contexte de la production d'un cadran comprenant une piece d'habillage realisee en un materiau mineral, tel un materiau mineral provenant de pierres naturelles ou de matieres fossilisees. A cet egard, differentes pierres naturelles ou matieres fossilisees peuvent etre envisagees. L'invention apporte en particulier des avantages considerables en rapport ä l'usinage de pierres naturelles ou de matieres fossilisees particulierement fragiles et/ou friables, en particulier les materiaux mineraux presentant des difficultes d'usinage notamment en raison de leur clivage, de leur structure fibreuse, de leur structure microcristalline, de differences de durete, de leur porosite ; et/ou de la presence de fissures ou autres irregularites et/ou d'une finition polie irreguliere. [0029] The invention will be more specifically described in the context of the production of a dial comprising a trim piece made of a mineral material, such as a mineral material from natural stones or fossilized materials. In this regard, different natural stones or fossilized materials can be considered. The invention brings in particular considerable advantages in relation to the machining of natural stones or particularly fragile and/or friable fossilized materials, in particular mineral materials presenting machining difficulties in particular because of their cleavage, their structure fibrous, their microcrystalline structure, differences in hardness, their porosity; and/or the presence of cracks or other irregularities and/or an uneven polished finish.

[0030] Parmi les materiaux mineraux presentant de telles difficultes d'usinage, Ton peut notamment eiter, de maniere non exhaustive, la Fluorite, la Spectrolite, la Labradorite, l'Amethyste, le Rubis, le Saphir, la Tourmaline, l'Ardoise, la Rhodochrosite, la Calcite, le Feldspath, l'Adulaire, la Pietersite, la CharoTte, le Quartz rutile, l'CEil de tigre, l'CEil de faucon, l'CEil de feu, l'CEil de taureau, la Seraphinite, la Prehnite, la Scolecite, l'Astrophyllite, l'Hematite specularite, le Mica, l'Amazonite, l'Anhydrite (ou Angelite), le Larimar, l'Algue Marine, l'Emeraude, la Sodalite, l'Or natif, la Pyrite, la Bronzite, la ZoTsite, I'Eudialyte, le Marbre, le Granite, la Malachite, la Turquoise, le Lapis Lazuli, la Sugilite, le Jaspe poreux, la Chrysoprase, la Chrysocolle, la Shattuckite, l'Azurite, la Variscite, l'Opale, et le Jaspe paysage. L'on peut ajouter ä cette liste les matieres fossilisees, tels des fossiles des plantes ou animaux (palmier, ammonites, dinosaures, etc.). [0030] Among the mineral materials presenting such machining difficulties, Your can in particular avoid, in a non-exhaustive manner, Fluorite, Spectrolite, Labradorite, Amethyst, Ruby, Sapphire, Tourmaline, Slate , Rhodochrosite, Calcite, Feldspar, Adularia, Pietersite, CharoTte, Rutilated Quartz, Tiger's Eye, Hawk's Eye, Fire's Eye, Bull's Eye, Seraphinite , Prehnite, Scolecite, Astrophyllite, Specularite Hematite, Mica, Amazonite, Anhydrite (or Angelite), Larimar, Seaweed, Emerald, Sodalite, Native Gold , Pyrite, Bronzite, ZoTsite, Eudialyte, Marble, Granite, Malachite, Turquoise, Lapis Lazuli, Sugilite, Porous Jasper, Chrysoprase, Chrysocolla, Shattuckite, Azurite, Variscite, Opal, and Landscape Jasper. One can add to this list fossilized materials, such as fossils of plants or animals (palm trees, ammonites, dinosaurs, etc.).

[0031] On comprendra cependant que l'invention est applicable par analogie ä d'autres materiaux d'origine naturelle. Le materiau d'origine naturelle constitutif de la piece d'habillage du composant d'habillement pourrait ainsi alternativement etre : [0031] It will however be understood that the invention is applicable by analogy to other materials of natural origin. The material of natural origin constituting the covering part of the clothing component could thus alternatively be:

- un materiau d'origine extraterrestre, tel un materiau provenant de meteorites non differenciees ou de meteorites differenciees, parmi lesquelles les meteorites chondrites, les meteorites achondrites, les meteorites de fer, et les meteorites mixtes ; - material of extraterrestrial origin, such as material from undifferentiated meteorites or differentiated meteorites, including chondrite meteorites, achondrite meteorites, iron meteorites, and mixed meteorites;

- un materiau mineral biosynthetise, teile la nacre ; ou encore - a biosynthesized mineral material, such as mother-of-pearl; or

- un materiau organique, teile bois, l'ivoire vegetal, l'ambre, le copal, le jais, ou la mellite. - an organic material, such as wood, vegetable ivory, amber, copal, jet, or mellite.

[0032] Tous les materiaux d'origine naturelle precites presentent potentiellement des difficultes d'usinage et/ou des caracteristiques susceptibles d'affecter leur capacite ä etre utilises comme materiau decoratif pour un composant d'habillement de piece d'horlogerie ou de joaillerie. Ceci etant dit, la presente invention offre une solution qui permet dans une tres large mesure de s'affranchir de ces difficultes. [0032] All the materials of natural origin mentioned above potentially present machining difficulties and/or characteristics liable to affect their ability to be used as a decorative material for a component of a timepiece or jewelry piece of clothing. This being said, the present invention offers a solution which makes it possible to a very large extent to overcome these difficulties.

[0033] Les Figures 1A ä 1G sont des vues en coupe laterale illustrant schematiquement une succession d'etapes de fabrication conduisant ä un produit intermediaire, designe par la reference 100* (voir Figure 1G), utilise dans le cadre de la production d'un cadran pour piece d'horlogerie, selon un mode de realisation de l'invention. Les Figures 2A ä 2E sont quant ä elles des vues en coupe laterale illustrant schematiquement une succession d'etapes de fabrication supplementaires conduisant, ä partir du produit intermediaire 100*, ä un cadran pour piece d'horlogerie, designe par la reference 100 (voir Figure 2E). La Figure 3 est une Illustration schematique d'un cadran 100, en coupe laterale, obtenu selon ce procede, lequel cadran est par ailleurs pourvu d'une structure 30 destinee au montage du cadran dans une piece d'horlogerie. [0033] Figures 1A to 1G are side section views schematically illustrating a succession of manufacturing steps leading to an intermediate product, designated by the reference 100* (see Figure 1G), used in the context of the production of a dial for a timepiece, according to one embodiment of the invention. Figures 2A to 2E are views in side section schematically illustrating a succession of additional manufacturing steps leading, from the intermediate product 100*, to a dial for a timepiece, designated by the reference 100 (see Figure 2E). Figure 3 is a schematic illustration of a dial 100, in lateral section, obtained according to this process, which dial is also provided with a structure 30 intended for mounting the dial in a timepiece.

[0034] Les Figures 1A-G ä 3 ne sont pas necessairement ä l'echelle et les epaisseurs et proportions des diverses piecesconstitutives du produit intermediaire 100* et du cadran 100 ont ete accentuees afin de permettre une meilleure comprehension de l'invention. [0034] Figures 1A-G to 3 are not necessarily to scale and the thicknesses and proportions of the various component parts of the intermediate product 100* and the dial 100 have been accentuated in order to allow a better understanding of the invention.

[0035] La Figure 1A montre schematiquement une vue laterale d'un materiau d'origine naturelle, designe par la reference 10*, en l'occurrence un bloc (ou carotte) d'un materiau mineral. Dans le contexte particulier de la fabrication d'un cadran pour piece d'horlogerie, il s'agit typiquement d'un bloc de matiere 10* obtenu par carottage, ä savoir un bloc de forme essentiellement cylindrique avec des faces irregulieres ä chaque extremite, comme illustre schematiquement dans la Figure 1A. Figure 1A schematically shows a side view of a material of natural origin, designated by the reference 10 *, in this case a block (or carrot) of a mineral material. In the particular context of the manufacture of a dial for a timepiece, it is typically a block of material 10* obtained by coring, namely a block of essentially cylindrical shape with irregular faces at each end, as schematically illustrated in Figure 1A.

[0036] Une portion adäquate du bloc de matiere 10* est debitee, par exemple par sciage, de maniere ä extraire une piece d'habillage 10 dont l'epaisseur W10.0 est teile que l'integrite structurelle du materiau reste assuree. Dans l'exemple illustre, l'on a procede au debitage d'un disque de matiere par sciage selon deux plans de coupe sensiblement paralleles [0036] A suitable portion of the block of material 10* is cut, for example by sawing, so as to extract a trim piece 10 whose thickness W10.0 is such that the structural integrity of the material remains assured. In the example shown, a disc of material is debited by sawing along two substantially parallel cutting planes

afin que la piece d'habillage resultante 10 (ici encore brüte) presente essentiellement deux faces opposees 10A, 10A* sensiblement planes. so that the resulting trim piece 10 (here again raw) essentially has two opposite faces 10A, 10A* that are substantially planar.

[0037] A titre illustratif, l'epaisseur W10.0 (ou „epaisseur initiale") de la piece d'habillage 10 est superieure ä 0.5 mm. Certains materiaux sont toutefois susceptibles d'etre trop fragiles pour etre debites sous une teile forme, et il peut ä cet egard etre necessaire de s'abstenir de proceder ä tout sciage d'un disque de matiere comme illustre. En pareil cas, II conviendra alors de travailler directement le bloc de matiere 10* comme expose ci-apres avant de debiler la pieced'habillage 10. II peut par ailleurs etre necessaire de stabiliser au prealable le materiau d'origine naturelle, par exemple par application ou impregnation d'une resine. [0037] By way of illustration, the thickness W10.0 (or "initial thickness") of the covering part 10 is greater than 0.5 mm. Certain materials are however likely to be too fragile to be debited in such a form , and it may in this respect be necessary to abstain from sawing a disk of material as illustrated. debilitate the trim piece 10. It may also be necessary to stabilize the material of natural origin beforehand, for example by applying or impregnating a resin.

[0038] Selon l'invention, une etape preliminaire du processus de fabrication consiste ä preparer une premiere surface 10A, ou surface superieure, de la piece d'habillage 10, comme illustre schematiquement par la Figure 1B. Dans le contexte particulier de la fabrication d'un cadran pour piece d'horlogerie, cette etape de preparation peut en particulier etre realisee par rodage de maniere ä former une premiere surface 10A sensiblement plane. Dans l'exemple illustre, Ton procede de meme ä un rodage de la surface opposee 10A*, de maniere ä ce que cette surface opposee 10A* soit egalement sensiblement plane et parallele ä la premiere surface 10A. [0038] According to the invention, a preliminary step in the manufacturing process consists in preparing a first surface 10A, or upper surface, of the trim piece 10, as schematically illustrated by FIG. 1B. In the specific context of manufacturing a dial for a timepiece, this preparation step can in particular be carried out by lapping so as to form a first substantially planar surface 10A. In the example illustrated, the procedure is likewise lapping the opposite surface 10A*, so that this opposite surface 10A* is also substantially flat and parallel to the first surface 10A.

[0039] La finalite de cette etape est de preparer la premiere surface 10A de maniere ä etre apte ä recevoir un adhesif. Un polissage de la premiere surface 10A n'est pas necessaire, etant releve qu'un certain degre d'asperite residuelle de la premiere surface 10A favorisera une meilleure tenue de l'adhesif. [0039] The purpose of this step is to prepare the first surface 10A so as to be able to receive an adhesive. Polishing of the first surface 10A is not necessary, it being noted that a certain degree of residual asperity of the first surface 10A will promote better adhesion of the adhesive.

[0040] Une fois la premiere surface 10A de la piece d'habillage 10 düment preparee, un adhesif 15 est applique sur la premiere surface 10A de la piece d'habillage 10, comme illustre dans la Figure 1C. II s'agit ici preferablement d'un adhesif 15 ä durcissement aux ultraviolets (UV), ä savoir d'un adhesif qui, une fois soumis ä un rayonnement UV, amorce un processus de reticulation conduisant au durcissement de l'adhesif. [0040] Once the first surface 10A of the trim piece 10 has been duly prepared, an adhesive 15 is applied to the first surface 10A of the trim piece 10, as illustrated in FIG. 1C. This is preferably an adhesive 15 with ultraviolet (UV) curing, namely an adhesive which, once subjected to UV radiation, initiates a crosslinking process leading to the curing of the adhesive.

[0041] Une fois l'adhesif 15 applique sur la premiere surface 10A de la piece d'habillage 10, l'on procede ensuite ä la jonction d'une piece de revetement 20 realisee en un materiau transparent, en particulier un verre, avec la premiere surface 10A, pourvue de l'adhesif 15, de la piece d'habillage 10, comme illustre dans la Figure 1D. II est important, lors de cette etape de jonction, d'eviter la formation de bulles d'air qui pourraient restee piegees dans l'interface entre la piece de revetement 20 et la piece d'habillage 10. [0041] Once the adhesive 15 has been applied to the first surface 10A of the covering part 10, one then proceeds to join a covering part 20 made of a transparent material, in particular a glass, with the first surface 10A, provided with the adhesive 15, of the trim piece 10, as illustrated in Figure 1D. It is important, during this joining step, to avoid the formation of air bubbles which could remain trapped in the interface between the covering part 20 and the trim part 10.

[0042] Dans le cas d'espece, le verre constitutif de la piece de revetement 20 est avantageusement un verre ä base de silice, mais d'autres verres, en particulier mineraux, sont potentiellement envisageables, tel un verre saphir. D'une maniere plus generale, l'on pourrait faire appel ä tout autre materiau transparent adequat. Dans le cadre de l'invention, l'utilisation d'un verre ä base de silice s'avere toutefois particulierement avantageuse et facilite grandement le processus de fabrication. Par ailleurs, les verres de silices sont classiquement disponibles sous la forme de plaques presentant une epaisseur dejä calibree. Ä titre d'exemple, l'epaisseur initiale W20.0 de la piece de revetement 20 est, ä ce stade de la production, superieure ou egale ä 1 mm. Des epaisseurs initiales plus faibles sont envisageables, mais cela peut potentiellement conduire ä une plus grande fragilite du verre. [0042] In this case, the constituent glass of the coating piece 20 is advantageously a silica-based glass, but other glasses, in particular mineral glasses, are potentially possible, such as a sapphire glass. More generally, any other suitable transparent material could be used. In the context of the invention, however, the use of a silica-based glass proves to be particularly advantageous and greatly facilitates the manufacturing process. Furthermore, silica glasses are conventionally available in the form of plates having an already calibrated thickness. By way of example, the initial thickness W20.0 of the covering piece 20 is, at this stage of production, greater than or equal to 1 mm. Lower initial thicknesses are possible, but this can potentially lead to greater glass brittleness.

[0043] L'on pourra relever ä ce stade qu'il Importe peu que l'adhesif 15 soit applique directement sur la premiere surface 10A de la piece d'habillage 10 ou sur la surface Interieure 20B de la piece de revetement 20. L'adhesif 15 peut ainsi etre applique directement sur la premiere surface 10A de la piece d'habillage 10 ou indirectement, en appliquant l'adhesif 15 tout d'abord sur la surface inferieure 20B de la piece de revetement, avant application de la piece de revetement 20 sur la piece d'habillage 10. II est par ailleurs parfaitement envisageable de faire appel le cas echeant ä un adhesif ä double composants oü un premier composant de l'adhesif est applique sur la premiere surface 10A de la piece d'habillage 10 et oü un second composant de l'adhesif est applique sur la surface inferieure 20B de la piece de revetement 20. [0043] It may be noted at this stage that it matters little whether the adhesive 15 is applied directly to the first surface 10A of the trim piece 10 or to the inner surface 20B of the covering piece 20. the adhesive 15 can thus be applied directly to the first surface 10A of the trim piece 10 or indirectly, by applying the adhesive 15 first of all to the lower surface 20B of the covering piece, before applying the trim piece. coating 20 on the trim piece 10. It is also perfectly possible to use, if necessary, a dual-component adhesive where a first component of the adhesive is applied to the first surface 10A of the trim piece 10 and wherein a second component of the adhesive is applied to the lower surface 20B of the liner piece 20.

[0044] Dans l'exemple illustre, le durcissement de l'adhesif 15 est initie par soumission de l'adhesif 15 ä un rayonnement ultraviolet, lequel rayonnement amorce le processus de reticulation de l'adhesif 15, conduisant ainsi ä un durcissement de l'adhesif 15 de maniere ä rendre la piece de revetement 20 solidaire de la piece d'habillage 10. Le rayonnement ultraviolet peut etre applique sur la premiere surface 10A de la piece d'habillage 10 au travers de la piece de revetement 20, comme illustre schematiquement dans la Figure 1E. Cette exposition aux ultraviolets peut etre operee sans contrainte particuliere au travers de la piece de revetement 20, sous reserve que celle-ci soit realise dans un materiau transparent laissant passersensiblement toute la gamme de longueurs d'onde necessaire ä l'amorgage du processus de reticulation de l'adhesif utilise. [0044] In the illustrated example, curing of adhesive 15 is initiated by subjecting adhesive 15 to ultraviolet radiation, which radiation initiates the process of cross-linking of adhesive 15, thereby resulting in curing of the adhesive. adhesive 15 so as to make the covering part 20 integral with the covering part 10. Ultraviolet radiation can be applied to the first surface 10A of the covering part 10 through the covering part 20, as illustrated schematically in Figure 1E. This exposure to ultraviolet light can be carried out without any particular constraint through the coating piece 20, provided that the latter is made of a transparent material allowing the entire range of wavelengths necessary to initiate the crosslinking process to pass. adhesive used.

[0045] Le processus de reticulation de l'adhesif 15 est pour ainsi dire immediat et l'etape de durcissement de l'adhesif 15 ne necessite pas un temps prolonge. Selon le type d'adhesif utilise, II pourrait cependant etre necessaire de laisser reposer l'ensemble composite constitue de la piece d'habillage 10 et de la piece de revetement 20, unies par l'adhesif 15, pour une duree süffisante au durcissement complet de l'adhesif. The crosslinking process of the adhesive 15 is virtually immediate and the curing step of the adhesive 15 does not require an extended time. Depending on the type of adhesive used, it may however be necessary to leave the composite assembly consisting of the covering part 10 and the covering part 20 to rest, united by the adhesive 15, for a period sufficient for complete curing. adhesive.

[0046] Une fois l'adhesif 15 durci, l'on procede encore ä l'usinage, en particulier par rodage, d'une seconde surface 10B, ou surface inferieure, de la piece d'habillage 10 de fagon ä reduire l'epaisseur de la piece d'habillage 10 ä une epaisseur cible. Dans le mode de realisation prefere illustre, cette Operation est realisee en deux etapes, ä savoir une premiere etape, teile qu'illustree dans les Figures 1F et 1G, oü l'usinage de la seconde surface 10B de la piece d'habillage 10 est tout d'abord opere de faqon ä reduire l'epaisseur de la piece d'habillage 10 ä une premiere epaisseur cible W10.1 (voir Figure 1G). Cette premiere epaisseur cible W10.1 est preferablement inferieure ou egale ä 0.5 mm. [0046] Once the adhesive 15 has hardened, further machining is carried out, in particular by lapping, of a second surface 10B, or lower surface, of the trim piece 10 so as to reduce the thickness of trim piece 10 to a target thickness. In the illustrated preferred embodiment, this Operation is carried out in two stages, namely a first stage, such as illustrated in Figures 1F and 1G, where the machining of the second surface 10B of the trim piece 10 is first of all operates so as to reduce the thickness of the trim piece 10 to a first target thickness W10.1 (see FIG. 1G). This first target thickness W10.1 is preferably less than or equal to 0.5 mm.

[0047] Dans une seconde etape qui sera discutee ci-apres en reference aux Figures 2A ä 2E, un usinage ulterieur dela seconde surface 10B est additionnellement opere de fagon ä reduire encore l'epaisseur de la piece d'habillage 10 ä une seconde epaisseur cible W10.2 inferieure ä la premiere epaisseur cible W10.1 (voir Figures 2B et 2C). Cette seconde epaisseur cible W10.2 est preferablement inferieure ou egale ä 0.2 mm. [0047] In a second step which will be discussed below with reference to Figures 2A to 2E, a subsequent machining of the second surface 10B is additionally operated so as to further reduce the thickness of the trim piece 10 to a second thickness. target W10.2 less than the first target thickness W10.1 (see Figures 2B and 2C). This second target thickness W10.2 is preferably less than or equal to 0.2 mm.

[0048] Dans le cadre de l'invention, Ton pourrait envisager que l'usinage de la seconde surface 10B de la piece d'habillage 10 soit opere en une seule et unique etape, ou en plus de deux etapes au besoin. In the context of the invention, one could consider that the machining of the second surface 10B of the trim piece 10 is operated in a single step, or in more than two steps as needed.

[0049] Pour en revenir ä la Figure 1G, l'on comprendra que les etapes discutees en reference aux Figures 1A ä 1G conduisent ä un produit intermediaire, designe par la reference 100*, qui doit encore subir un certain nombre d'etapes supplementaires, feiles qu'illustrees par les Figures 2A ä 2E, avant d'aboutir au cadran 100 souhaite. Ceci dit, le produit intermediaire 100* constitue de l'ensemble composite forme de la piece d'habillage 10 et de la piece de revetement 20, unies par l'adhesif 15, est beaucoup plus aise ä manipuler ainsi qu'ä transporter du fait de la presence de l'element de revetement 20. En effet, le produit intermediaire 100* presente ä ce stade une epaisseur süffisante (par exemple de l'ordre de 1.5 mm ou plus) qui facilite grandement sa manipulation et reduit drastiquement le risque de cassure de la piece d'habillage 10, cette piece d'habillage 10 etant de facto solidaire de la piece de revetement 20. La piece de revetement 20 offre ainsi l'avantage d'assurer un support et renfort pour la piece d'habillage 10. [0049] Returning to Figure 1G, it will be understood that the steps discussed with reference to Figures 1A to 1G lead to an intermediate product, designated by the reference 100*, which must still undergo a certain number of additional steps. , Feiles as illustrated by Figures 2A to 2E, before arriving at the dial 100 desired. That said, the intermediate product 100 * consists of the composite assembly formed of the covering part 10 and the covering part 20, united by the adhesive 15, is much easier to handle as well as to transport because the presence of the coating element 20. Indeed, the intermediate product 100* has at this stage a sufficient thickness (for example of the order of 1.5 mm or more) which greatly facilitates its handling and drastically reduces the risk of breakage of the covering part 10, this covering part 10 being de facto integral with the covering part 20. The covering part 20 thus offers the advantage of providing support and reinforcement for the covering part 10 .

[0050] II convient de relever que les etapes des Figures 1A ä 1G et des Figures 2A ä 2E ne seront pas necessairement realisees sur un meme site et par une meme personne. Les etapes decrites en reference aux Figures 1A ä 1G seront normalement realisees par un preparateur disposant de l'expertise et des connaissances necessaires ä la preparation, la manipulation et ä l'usinage du materiau d'origine naturelle constitutif de la piece d'habillage 10, alors que les etapes qui vont maintenant etre discutees en reference aux Figures 2A ä 2E seront typiquement effectuees par un cadranier disposant de l'expertise et des connaissances necessaires ä la fabrication et au finissage du cadran ä proprement parier. L'on comprendra que le cadranier operera des operations d'usinage de et dans la piece d'habillage 10, operations qui necessitent donc, dans le cas d'espece, une competence complementaire dans le domaine de l'usinage de cadrans en pierres naturelles. It should be noted that the stages of Figures 1A to 1G and Figures 2A to 2E will not necessarily be carried out on the same site and by the same person. The steps described with reference to Figures 1A to 1G will normally be carried out by a preparer having the expertise and knowledge necessary for the preparation, handling and machining of the material of natural origin constituting the trim piece 10 , whereas the steps which will now be discussed with reference to Figures 2A to 2E will typically be carried out by a dial maker having the expertise and knowledge necessary to manufacture and finish the dial itself. It will be understood that the dial maker will carry out machining operations of and in the covering part 10, operations which therefore require, in the case in point, additional competence in the field of machining natural stone dials .

[0051] Comme dejä evoque ci-dessus, la structure meme du produit intermediaire 100* assure un transfert optimal dupreparateur qui travaille la pierre au cadranier qui procede aux etapes de finissage du cadran ä proprement parier. [0051] As already mentioned above, the very structure of the intermediate product 100* ensures optimum transfer from the preparer who works the stone to the dial-maker who proceeds to the finishing stages of the actual dial.

[0052] La Figure 2A montre schematiquement une vue laterale du produit intermediaire 100* de la Figure 1G dans lequel l'on a procede ä une etape d'usinage supplementaire consistant ä pratiquer des ouvertures traversantes 10a, 10b au travers de la piece d'habillage 10. II est question ici en particulier d'un trou central 10a qui est classiquement realise afin de permettre le passage d'organes indicateurs d'un mouvement horloger (par exemple les axes et canons d'aiguilles des heures et des minutes) ainsi que d'un guichet 10b pour l'affichage d'une autre indication, par exemple un affichage du quantieme. II s'agit ici d'exemples purement illustratifs, et les ouvertures traversantes eventuellement pratiquees au travers de la piece d'habillage 10 pourraient le cas echeant remplir toute autre fonction desiree. II est bien evidemment entendu que la forme, la disposition, ainsi que les dimensions des ouvertures traversantes dependront essentiellement du design particulier du cadran souhaite et des indications que l'on souhaite afficher sur le cadran ou en relation avec le cadran. [0052] Figure 2A schematically shows a side view of the intermediate product 100* of Figure 1G in which an additional machining step has been carried out consisting in making through openings 10a, 10b through the dressing 10. It is a question here in particular of a central hole 10a which is conventionally made in order to allow the passage of organs indicating a watch movement (for example the axes and barrels of hour and minute hands) as well than a window 10b for displaying another indication, for example a date display. These are purely illustrative examples, and any through openings made through the trim piece 10 could, if necessary, fulfill any other desired function. It is obviously understood that the shape, the arrangement, as well as the dimensions of the through openings will essentially depend on the particular design of the desired dial and the indications that one wishes to display on the dial or in relation to the dial.

[0053] Dans I'i11ustration de la Figure 2A, l'on peut relever que les ouvertures traversantes 10a, 10b sont realisees de Sorte ä penetrer partiellement dans la piece de revetement 20. La distance de penetration des ouvertures traversantes 10a, 10b est ici choisie de Sorte ä etre superieure ä une epaisseur cible W20.1 de la piece de revetement 20 (voir notamment Figures 2D et 2E), ä savoir l'epaisseur cible W20.1 de la piece de revetement 20 du composant d'habillement termine. In the illustration of Figure 2A, it can be noted that the through openings 10a, 10b are made in such a way as to partially penetrate the covering part 20. The penetration distance of the through openings 10a, 10b is here chosen so as to be greater than a target thickness W20.1 of the covering piece 20 (see in particular FIGS. 2D and 2E), namely the target thickness W20.1 of the covering piece 20 of the finished clothing component.

[0054] L'etape d'usinage supplementaire operee sur la piece d'habillage 10 peut le cas echeant inclure la realisation d'usinages complementaires, en particulier sur la surface inferieure 10B de la piece d'habillage 10, tel par exemple que l'usinage de renfoncements destines ä recevoir les pieds de cadran 30 comme illustre ä titre d'exemple dans la Figure 3. [0054] The additional machining step carried out on the trim piece 10 can, if necessary, include the performance of additional machining operations, in particular on the lower surface 10B of the trim piece 10, such as the machining of recesses intended to receive the dial feet 30 as illustrated by way of example in Figure 3.

[0055] Une fois l'etape d'usinage supplementaire de la piece d'habillage 10 effectuee, l'on procede preferablement ä la seconde etape de reduction de l'epaisseur de la piece d'habillage 10 dejä evoquee plus haut. II s'agit ici de reduire l'epaisseur de la piece d'habillage 10 de la premiere epaisseur cible W10.1 ä la seconde epaisseur cible W10.2, comme illustre schematiquement par les Figures 2B et 2C. Cette Operation permet notamment de supprimer les eventuelles bavures ou defauts de surface present sur la seconde surface 10B de la piece d'habillage 10 resultant de l'operation d'usinage anterieure. Cette Operation permet egalement de reduire l'epaisseur de la piece d'habillage 10 ä l'epaisseur definitive souhaitee et de garantir l'etat de surface desire au dos du cadran. [0055] Once the step of additional machining of the covering part 10 has been carried out, the second step of reducing the thickness of the covering part 10 already mentioned above is preferably carried out. This involves reducing the thickness of the trim piece 10 from the first target thickness W10.1 to the second target thickness W10.2, as illustrated schematically by FIGS. 2B and 2C. This operation makes it possible in particular to remove any burrs or surface defects present on the second surface 10B of the trim piece 10 resulting from the previous machining operation. This Operation also makes it possible to reduce the thickness of the casing part 10 to the desired final thickness and to guarantee the desired surface condition on the back of the dial.

[0056] Une fois cette Operation effectuee, l'on procede alors ä un usinage, en particulier par rodage, d'une surface superieure 20Ade la piece de revetement 20 defaqon ä reduire son epaisseur ä une epaisseur cible W20.1, comme illustre dans les Figures 2D et 2E. Cette epaisseur cible W20.1 est preferablement inferieure ou egale ä 0.15 mm. L'on procede egalement au polissage de la surface superieure 20A de la piece de revetement de fagon ä presenter la finition polie desiree P. [0056] Once this operation has been performed, machining is then carried out, in particular by lapping, of an upper surface 20A of the covering piece 20 so as to reduce its thickness to a target thickness W20.1, as illustrated in Figures 2D and 2E. This target thickness W20.1 is preferably less than or equal to 0.15 mm. The upper surface 20A of the coating piece is also polished so as to present the desired polished finish P.

[0057] L'on peut relever que l'utilisation d'un verre ä base de silice s'avere particulierement avantageuse dans la mesure oü l'usinage d'un tel verre est relativement aise et que l'execution du polissage de la surface d'un tel verre permet d'obtenir un excellent rendu et une grande qualite de surface, sans pour autant que cela necessite des outils et moyens de polissage complexes et coüteux. Comme dejä evoque, une resultante de la mise en oeuvre de l'invention est que l'operation de polissage est effectuee sur la surface superieure 20A de la piece de revetement 20, et non sur une surface de la piece [0057] It can be noted that the use of a silica-based glass proves to be particularly advantageous insofar as the machining of such a glass is relatively easy and that the execution of the polishing of the surface of such a glass makes it possible to obtain an excellent finish and a high surface quality, without this requiring complex and expensive tools and polishing means. As already mentioned, a result of the implementation of the invention is that the polishing operation is carried out on the upper surface 20A of the piece of coating 20, and not on a surface of the piece.

d'habillage 10. En d'autres termes, les outils et moyens de polissage requis doivent uniquement etre adaptes au type de materiau transparent utilise comme materiau constitutif de la piece de revetement 20 et ne sont pas impactes par le materiau d'origine naturelle constitutif de la piece d'habillage 10. Pour un type de verre donne, Ton peut des lors garantir une finition polie P predeterminee qui est independante de la nature de la piece d'habillage 10. of covering 10. In other words, the tools and polishing means required must only be adapted to the type of transparent material used as the constituent material of the covering part 20 and are not impacted by the constituent material of natural origin of the trim piece 10. For a given type of glass, one can therefore guarantee a predetermined polished finish P which is independent of the nature of the trim piece 10.

[0058] Une fois le polissage de la surface superieure 20A de la piece de revetement 20 effectue, l'on peut ensuite proceder ä l'application ou la creation d'elements decoratifs sur la surface superieure 20A de la piece de revetement 20, par exemple l'apposition d'indications des heures et des minutes et/ou d'autres elements decoratifs. [0058] Once the polishing of the upper surface 20A of the covering part 20 has been carried out, one can then proceed to the application or the creation of decorative elements on the upper surface 20A of the covering part 20, by example the affixing of hour and minute indications and/or other decorative elements.

[0059] Selon une Variante de l'invention, l'on pourrait le cas echeant envisager d'appliquer des elements decoratifs entre la piece de revetement 20 et la piece d'habillage 10 avant la jonction de ces pieces au moyen de l'adhesif 15 en complement ou remplacement des elements decoratifs sur la surface superieure 20A de la piece de revetement According to a variant of the invention, one could, if necessary, consider applying decorative elements between the covering part 20 and the trim part 10 before the joining of these parts by means of the adhesive. 15 in addition to or replacement of the decorative elements on the upper surface 20A of the covering part

[0060] II est preferable que l'usinage de la surface superieure 20A de la piece de revetement 20 soit realise seulement apres l'usinage, definitif, de la seconde surface 10B de la piece d'habillage 10. Cela assure en effet que l'ensemble composite puisse etre maintenu de maniere adäquate, sur la surface de piece de revetement 20, non encore polie, lors du rodage definitif de la piece d'habillage 10. L'usinage et le polissage definitif de la piece de revetement 20 ne presente ä ce titre pas de difficulte particuliere et peut etre opere apres rodage definitif de la piece d'habillage 10. [0060] It is preferable that the machining of the upper surface 20A of the covering piece 20 be carried out only after the definitive machining of the second surface 10B of the covering piece 10. This in fact ensures that the the composite assembly can be maintained in an adequate manner, on the surface of the covering part 20, not yet polished, during the final lapping of the covering part 10. The machining and the final polishing of the covering part 20 does not present in this respect, there is no particular difficulty and can be operated on after final running in of the trim piece 10.

[0061] Une fois l'ensemble des operations supplementaires effectuees, discutees dans lecadre de l'exemple de realisation illustre par les Figures 2A ä 2E, l'on dispose alors d'un cadran 100 quasi termine. [0061] Once all the additional operations have been carried out, discussed in the context of the example embodiment illustrated in FIGS. 2A to 2E, one then has a dial 100 that is almost finished.

[0062] Des operations de finissage supplementaires sont encore envisageables. [0062] Additional finishing operations are still possible.

[0063] Une Operation de finissage supplementaire pourrait par exemple consister en l'application, sur la seconde surface 10B de la piece d'habillage 10, d'une couche de contraste, preferablement opaque. Ceci peut en particulier etre judicieux ou desirable selon le degre de transparence de la piece d'habillage 10, une fois ramenee ä son epaisseur cible definitive. An additional finishing operation could for example consist of the application, on the second surface 10B of the trim piece 10, of a contrast layer, preferably opaque. This may in particular be judicious or desirable depending on the degree of transparency of the trim piece 10, once reduced to its final target thickness.

[0064] Une autre Operation de finissage supplementaire, plus usuelle, consiste en la realisation, sur au moins la seconde surface 10B de la piece d'habillage 10, d'une garniture ou structure, preferablement metallique, destinee au montage du cadran 100 dans la piece d'horlogerie. II est question ici en particulier de creer un ou plusieurs pieds au dos du cadran 100, comme illustre dans la Figure 3 oü deux pieds 30 sont visibles. Une teile garniture peut par exemple etre formee selon l'enseignement de la demande de brevet suisse No. CH 649 670 G A3 discutee en preambule. Des pieds individuels 30, comme illustres dans la Figure 3, peuvent egalement etre formes directement sur la seconde surface 10B de la piece d'habillage 10 en appliquant par exemple un film d'accrochage, par exemple metallique, servant de base ä l'attache (par exemple par soudage) des pieds 30 comme evoque par exemple dans le brevet britannique GB 2 052 113 B. [0064] Another additional finishing operation, more usual, consists of the production, on at least the second surface 10B of the covering piece 10, of a trim or structure, preferably metallic, intended for mounting the dial 100 in the timepiece. It is a question here in particular of creating one or more feet on the back of the dial 100, as illustrated in Figure 3 where two feet 30 are visible. Such a filling can for example be formed according to the teaching of Swiss patent application No. CH 649 670 G A3 discussed in the preamble. Individual feet 30, as illustrated in FIG. 3, can also be formed directly on the second surface 10B of the trim piece 10 by applying, for example, an adhesion film, for example metallic, serving as a base for the fastener. (for example by welding) of the feet 30 as mentioned for example in British patent GB 2 052 113 B.

[0065] L'invention permet avantageusement la production d'un cadran 100 dont l'epaisseur totale W100 est inferieure ou egale ä 0.4 mm, epaisseur usuelle des cadrans utilises dans le domaine de l'horlogerie. The invention advantageously allows the production of a dial 100 whose total thickness W100 is less than or equal to 0.4 mm, the usual thickness of dials used in the field of watchmaking.

[0066] On comprendra de maniere generale que diverses modifications et/ou ameliorations evidentes pour l'homme du metier peuvent etre apportees aux modes de realisation decrits dans la presente description sans sortir du cadre de l'invention defini par les revendications annexees. Par exemple, bien que l'invention ait ete presentee dans le contexte particulier de la fabrication d'un cadran pour piece d'horlogerie, l'invention peut etre appliquee ä tout autre composant d'habillement d'une piece d'horlogerie ou de joaillerie. Le composant d'habillement pourrait ainsi faire uniquement Office de parement ou decoration pour une piece d'horlogerie ou de joaillerie, sans avoir necessairement vocation ä permettre l'affichage de l'heure ou d'une autre indication d'un mouvement horloger. II n'en reste pas moins que l'application ä la fabrication de cadrans pour pieces d'horlogerie reste une application majeure et particulierement avantageuse de l'invention. It will generally be understood that various modifications and/or improvements obvious to those skilled in the art can be made to the embodiments described in the present description without departing from the scope of the invention defined by the appended claims. For example, although the invention has been presented in the particular context of the manufacture of a dial for a timepiece, the invention can be applied to any other component of clothing for a timepiece or jewelry. The clothing component could thus serve only as a facing or decoration for a timepiece or piece of jewelry, without necessarily having the purpose of enabling the display of the time or of another indication of a timepiece movement. The fact remains that the application to the manufacture of dials for timepieces remains a major and particularly advantageous application of the invention.

LISTE DES SIGNES DE REFERENCE UTILISES DANS LA PRESENTE DESCRIPTION ET DANS LES DESSINS LIST OF REFERENCE SIGNS USED IN THIS DESCRIPTION AND IN THE DRAWINGS

[0067] [0067]

10 piece d'habillage realisee en un materiau d'origine naturelle (par exemple un materiau mineral provenant de pierres naturelles ou de matieres fossilisees) 10 piece of trim made of a material of natural origin (for example a mineral material from natural stones or fossilized materials)

10* bloc de matiere brüt, par exemple bloc obtenu par carottage 10* block of raw material, for example block obtained by coring

10A premiere surface (surface superieure) de la piece d'habillage 10 10A first surface (upper surface) of the trim piece 10

10A* surface inferieure de la piece d'habillage 10 brüte (avant usinage) 10A* lower surface of trim piece 10 raw (before machining)

10B seconde surface (surface inferieure) de la piece d'habillage 10 (apres usinage) 10B second surface (lower surface) of trim piece 10 (after machining)

10a ouverture traversante pratiquee au travers de la piece d'habillage 10 / trou central pour les passages des indicateurs des heures et des minutes d'un mouvement horloger 10a through opening made through the covering part 10/central hole for the passages of the hour and minute indicators of a watch movement

10b ouverture traversante pratiquee au travers de la piece d'habillage 10 / guichet 10b through opening made through the trim piece 10 / window

15 adhesif (par exemple adhesif ä durcissement aux UV) adhesive (eg UV curing adhesive)

20 piece de revetement realisee en un materiau transparent, en particulier un verre (par exemple un verre ä base 20 piece of coating made of a transparent material, in particular a glass (for example a glass based

de silice) silica)

20A surface superieure de la piece de revetement 20, apres usinage et polissage 20A upper surface of coating part 20, after machining and polishing

20B surface inferieure de la piece de revetement 20 rendue solidaire de la premiere surface 10A de la piece d'ha 20B lower surface of the piece of covering 20 made integral with the first surface 10A of the piece of ha

billage 10 au moyen de l'adhesif 15 beading 10 using adhesive 15

30 garniture ou structure destinee au montage du composant d'habillement 100 / pieds de cadran 30 trim or structure intended for mounting the clothing component 100 / feet of dial

Claims (10)

100 100* W10.0100 100* W10.0 W10.1W10.1 W10.2 W20.0 W20.1W10.2 W20.0 W20.1 W100W100 PP cadran pour piece d'horlogerie (composant d'habillement)dial for timepiece (clothing component) produit intermediaire employe dans la fabrication du cadran 100intermediate product used in the manufacture of dial 100 epaisseur initiale (avant usinage) de la piece d'habillage 10initial thickness (before machining) of the trim piece 10 (premiere) epaisseur cible de la piece d'habillage 10(first) target thickness of trim piece 10 (seconde) epaisseur cible de la piece d'habillage 10(second) target thickness of trim piece 10 epaisseur initiale (avant usinage) de la piece de revetementinitial thickness (before machining) of the coating part epaisseur cible de la piece de revetement 20target thickness of the coating part 20 epaisseur du cadran 100dial thickness 100 finition polie de la surface superieure 20A de la piece de revetement 20polished finish of the upper surface 20A of the liner part 20 RevendicationsClaims 1. Un procede de fabrication d'un composant d'habillement (100 ; 100*) pour piece d'horlogerie ou de joaillerie, lequel composant d'habillement (100 ; 100*) comprend au meins une piece (10) realisee en un materiau d'origine naturelle, caracterise en ce que le procede comporte les etapes suivantes :1. A method of manufacturing a clothing component (100; 100*) for a timepiece or jewelry piece, which clothing component (100; 100*) comprises at least one piece (10) made in one material of natural origin, characterized in that the process comprises the following steps: (i) fourniture d'une piece d'habillage (10) realisee en un materiau d'origine naturelle ;(i) supply of a trim piece (10) made of a material of natural origin; (ii) preparation d'une premiere surface (10A), ou surface superieure, de la piece d'habillage (10) de fapon ä pouvoir recevoir un adhesif (15) ;(ii) preparing a first surface (10A), or upper surface, of the trim piece (10) so as to be able to receive an adhesive (15); (iii) application de l'adhesif (15) directement ou indirectement sur la premiere surface (10A) de la piece d'habillage (10);(iii) applying the adhesive (15) directly or indirectly to the first surface (10A) of the trim piece (10); (iv) jonction, via l'adhesif (15), d'une piece de revetement (20) realisee en un materiau transparent, en particulier un verre, avec la premiere surface (10A) de la piece d'habillage (10) ;(iv) joining, via the adhesive (15), of a covering part (20) made of a transparent material, in particular a glass, with the first surface (10A) of the covering part (10); (v) durcissement de l'adhesif (15) de maniere ä rendre la piece de revetement (20) solidaire de la piece d'habillage (10) ; et(v) hardening of the adhesive (15) so as to make the covering piece (20) integral with the covering piece (10); And (vi) usinage, en particulier par rodage, d'une seconde surface (108), ou surface inferieure, de la piece d'habillage (10) de faqon ä reduire l'epaisseur de la piece d'habillage (10) ä une epaisseur cible (W10.1 ; W10.2). (vi) machining, in particular by lapping, of a second surface (108), or lower surface, of the trim piece (10) so as to reduce the thickness of the trim piece (10) to a target thickness (W10.1; W10.2). 2. Le procede selon la revendication 1, caracterise en ce que l'usinage (vi) de la seconde surface (1 OB) de la piece d'habillage (10) est opere de faqon ä reduire l'epaisseur de la piece d'habillage (10) ä une premiere epaisseur cible (W10.1), en particulier une premiere epaisseur cible (W10.1) inferieure ou egale ä 0.5 mm,2. The method according to claim 1, characterized in that the machining (vi) of the second surface (10B) of the trim piece (10) is operated in such a way as to reduce the thickness of the piece by covering (10) at a first target thickness (W10.1), in particular a first target thickness (W10.1) less than or equal to 0.5 mm, et en ce qu'un usinage ulterieur de la seconde surface (1 OB) de la piece d'habillage (10) est optionnellement opere, dans une phase de finissage, de faqon ä reduire l'epaisseur de la piece d'habillage (10) ä une seconde epaisseur cible (W10.2) inferieure ä la premiere epaisseur cible (W10.1), en particulier une seconde epaisseur cible (W10.2) inferieure ou egale ä 0.2 mm. and in that a subsequent machining of the second surface (1 OB) of the trim piece (10) is optionally carried out, in a finishing phase, so as to reduce the thickness of the trim piece (10 ) to a second target thickness (W10.2) less than the first target thickness (W10.1), in particular a second target thickness (W10.2) less than or equal to 0.2 mm. 3. Le procede selon la revendication 1 ou 2, caracterise en ce que la piece d'habillage (10) presente une epaisseur initiale (W10.0) superieure ä 0.5 mm avant l'usinage (vi) de la seconde surface (1 OB) de la piece d'habillage (10). 3. The method according to claim 1 or 2, characterized in that the trim piece (10) has an initial thickness (W10.0) greater than 0.5 mm before the machining (vi) of the second surface (1 OB ) of the trim piece (10). 4. Le procede selon l'une quelconque des revendications precedentes, caracterise en ce que la piece de revetement (20) presente une epaisseur initiale (W20.0) superieure ä une epaisseur cible (W20.1), laquelle epaisseur initiale (W20.0) est preferablement superieure ou egale ä 1 mm,4. The method according to any one of the preceding claims, characterized in that the coating piece (20) has an initial thickness (W20.0) greater than a target thickness (W20.1), which initial thickness (W20. 0) is preferably greater than or equal to 1 mm, et en ce que le procede comporte en outre les etapes supplementaires suivantes :and in that the method further comprises the following additional steps: (vii) usinage, en particulier par rodage, d'une surface superieure (20A) de la piece de revetement (20) de fagon ä reduire l'epaisseur de la piece de revetement (20) ä l'epaisseur cible (W20.1) ;(vii) machining, in particular by lapping, of an upper surface (20A) of the covering piece (20) so as to reduce the thickness of the covering piece (20) to the target thickness (W20.1 ); (viii)polissage de la surface superieure (20A) de la piece de revetement (20) de fagon ä presenter une finition polie(viii) polishing the top surface (20A) of the liner piece (20) to present a polished finish (P) ; et '(P); And ' (ix)optionnellement, application ou creation d'elements decoratifs sur la surface superieure (20A) de la piece de revetement (20),(ix) optionally, application or creation of decorative elements on the upper surface (20A) of the covering part (20), l'epaisseur cible (W20.1) de la piece de revetement (20) etant en particulier inferieure ou egale ä 0.15 mm, l'usinage (vii) de la surface superieure (20A) de la piece de revetement (20) etant preferablement realise apres l'usinage (vi) de la seconde surface (1 OB) de la piece d'habillage (10). the target thickness (W20.1) of the covering piece (20) being in particular less than or equal to 0.15 mm, the machining (vii) of the upper surface (20A) of the covering piece (20) being preferably carried out after the machining (vi) of the second surface (1 OB) of the covering part (10). 5. Le procede selon l'une quelconque des revendications precedentes, caracterise en ce qu'il comporte en outre l'une et/ou l'autre des etapes de finissage suivantes :5. The process according to any one of the preceding claims, characterized in that it further comprises one and/or the other of the following finishing steps: - application, sur la seconde surface (1 OB) de la piece d'habillage (10), d'une couche de contraste, preferablementopaque ; et- application, on the second surface (1 OB) of the trim piece (10), of a contrast layer, preferably opaque; And - realisation, sur au moins la seconde surface (1 OB) de la piece d'habillage (10), d'une garniture ou structure (30),preferablement metallique, destinee au montage du composant d'habillement (100) dans la piece d'horlogerie ou de joaillerie. - realization, on at least the second surface (1 OB) of the trim piece (10), of a trim or structure (30), preferably metallic, intended for mounting the clothing component (100) in the piece watchmaking or jewelry. 6. Le procede selon l'une quelconque des revendications precedentes, caracterise en ce que l'adhesif (15) est un adhesif ä durcissement aux ultraviolets (UV) et que l'etape de durcissement (v) comporte l'application d'ultraviolets (UV) sur la premiere surface (10A) de la piece d'habillage (10). 6. The method according to any preceding claim, characterized in that the adhesive (15) is an ultraviolet (UV) curing adhesive and that the curing step (v) comprises the application of ultraviolet (UV) on the first surface (10A) of the trim piece (10). 7. Le procede seien Tune quelconque des revendications precedentes caracterise en ce qu'il comporte en outre une etape d'usinage supplementaire consistant ä pratiquer une ou plusieurs ouvertures traversantes (10a, 10b), tel un treu central (10a) ou un guichet (10b), au travers de la piece d'habillage (10),7. The process according to any one of the preceding claims is characterized in that it also comprises an additional machining step consisting in making one or more through openings (10a, 10b), such as a central hole (10a) or a window ( 10b), through the trim piece (10), et en ce que chaque ouverture traversante (10a, 10b) est preferablement realisee de Sorte ä penetrer partiellement dans la piece de revetement (20) sur une distance superieure ä une epaisseur cible (W20.1) de la piece de revetement (20). and in that each through-opening (10a, 10b) is preferably made in such a way as to partially penetrate the covering piece (20) over a distance greater than a target thickness (W20.1) of the covering piece (20). 8. Le procede selon l'une quelconque des revendications precedentes, caracterise en ce que le materiau d'origine naturelle constitutif de la piece d'habillage (10) est:8. The method according to any one of the preceding claims, characterized in that the material of natural origin constituting the trim piece (10) is: - un materiau mineral, tel un materiau mineral provenant de pierres naturelles ou de matieres fossilisees ;- a mineral material, such as a mineral material from natural stones or fossilized materials; - un materiau d'origine extraterrestre, tel un materiau provenant de meteorites non differenciees ou de meteoritesdifferenciees ;- material of extraterrestrial origin, such as material from undifferentiated meteorites or differentiated meteorites; - un materiau mineral biosynthetise ; ou- a biosynthesized mineral material; Or - un materiau organique.- an organic material. 9. Le procede selon l'une quelconque des revendications precedentes, caracterise en ce que le materiau transparent constitutif de la piece de revetement (20) est un verre ä base de silice ou un verre mineral, par exemple un verre saphir. 9. The method according to any one of the preceding claims, characterized in that the transparent material constituting the coating piece (20) is a silica-based glass or a mineral glass, for example a sapphire glass. 10. Un composant d'habillement (100 ; 100*) pour piece d'horlogerie ou de joaillerie, en particulier un composant d'habillement (100 ; 100*) obtenu selon le procede de l'une quelconque des revendications precedentes, le composant d'habillement (100 ; 100*) comprenant une piece d'habillage (10) realisee en un materiau d'origine naturelle et une piece de revetement (20) realisee en un materiau transparent, en particulier un verre, laquelle piece de revetement (20) est rendue solidaire d'une premiere surface (10A), ou surface superieure, de la piece d'habillage (10) au moyen d'un adhesif (15),10. A clothing component (100; 100*) for a timepiece or jewelry piece, in particular a clothing component (100; 100*) obtained according to the method of any one of the preceding claims, the component clothing (100; 100*) comprising a covering piece (10) made of a material of natural origin and a covering piece (20) made of a transparent material, in particular a glass, which covering piece ( 20) is secured to a first surface (10A), or upper surface, of the trim piece (10) by means of an adhesive (15), le composant d'habillement (100 ; 100*) etant preferablement un cadran (100) pour piece d'horlogerie ou un produit intermediaire (100*) employe dans la fabrication dudit cadran (100). the clothing component (100; 100*) preferably being a dial (100) for a timepiece or an intermediate product (100*) used in the manufacture of said dial (100).
CH01239/19A 2019-09-30 2019-09-30 Process for manufacturing a clothing component for a timepiece or piece of jewelery and clothing component made of a coated material of natural origin. CH716645B1 (en)

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CH01239/19A CH716645B1 (en) 2019-09-30 2019-09-30 Process for manufacturing a clothing component for a timepiece or piece of jewelery and clothing component made of a coated material of natural origin.

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