EP2018601A2 - Spiral-/spiralrollenanordnung für uhrwerk - Google Patents

Spiral-/spiralrollenanordnung für uhrwerk

Info

Publication number
EP2018601A2
EP2018601A2 EP07734401A EP07734401A EP2018601A2 EP 2018601 A2 EP2018601 A2 EP 2018601A2 EP 07734401 A EP07734401 A EP 07734401A EP 07734401 A EP07734401 A EP 07734401A EP 2018601 A2 EP2018601 A2 EP 2018601A2
Authority
EP
European Patent Office
Prior art keywords
spiral
ferrule
assembly according
ferrule assembly
point
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP07734401A
Other languages
English (en)
French (fr)
Other versions
EP2018601B1 (de
Inventor
Jean-Pierre Musy
Frédéric Maier
Stéphane von Gunten
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Patek Philippe SA Geneve
Original Assignee
Patek Philippe SA Geneve
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 Patek Philippe SA Geneve filed Critical Patek Philippe SA Geneve
Priority to EP07734401.8A priority Critical patent/EP2018601B1/de
Publication of EP2018601A2 publication Critical patent/EP2018601A2/de
Application granted granted Critical
Publication of EP2018601B1 publication Critical patent/EP2018601B1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • G04B17/00Mechanisms for stabilising frequency
    • G04B17/32Component parts or constructional details, e.g. collet, stud, virole or piton
    • G04B17/34Component parts or constructional details, e.g. collet, stud, virole or piton for fastening the hairspring onto the balance
    • G04B17/345Details of the spiral roll
    • 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
    • G04B43/00Protecting clockworks by shields or other means against external influences, e.g. magnetic fields
    • G04B43/002Component shock protection arrangements

Definitions

  • the present invention relates to a spiral-ferrule assembly for a watch movement, more specifically a spiral whose inner end is attached to a ferrule, ferrule which can be driven on the axis of a balance to form the movement control device .
  • the patent CH 500 523 describes a ferrule having on its periphery three stops against which the inner turn of the spring can come to bear in case of radial shock to limit the deformation of the spiral. These three stops are equidistant from the center of the balance shaft. One of these stops is necessarily closer to the inner coil than the other two. This arrangement can cause problems in that the nearest stop may be touched by the inner turn during normal operation of the movement, which can disrupt said operation, especially if the amplitude of oscillations of the pendulum is large, and / or that the farthest abutment may be too far away to, in the event of an impact, serve as a support for the inner coil before its elastic limit is exceeded.
  • the present invention aims to remedy the aforementioned drawbacks of the state of the art and proposes for this purpose a spiral-ferrule assembly according to claim 1 attached, that is to say a spiral-ferrule assembly comprising a ferrule and a spiral attached by its inner end to the ferrule, the ferrule being adapted to be mounted on an axis, the outer contour of the ferrule defining abutments against which the inner coil of the spiral can come to rest during an impact before the limit elastic band of the inner coil is exceeded, characterized in that said stops are located at respective distances from the center of the axis which are increasing in the direction of the hairspring going from the inside to the outside from the junction point of the hairspring to the hoop.
  • This spiral-ferrule assembly is defined in the appended dependent claims 2 to 13.
  • the present invention also proposes a clockwork movement comprising this spiral-ferrule assembly.
  • a spiral-ferrule assembly for a watch movement according to a first embodiment of the invention comprises a ferrule 1 intended to be mounted on a balance shaft 2 and a spiral 3 attached by its end.
  • the spiral 3 is partially shown, only its inner turn being visible.
  • the ferrule 1 comprises three elastic arms 4 arranged in a triangle.
  • the elastic arms 4 define an equilateral triangular central opening 5 whose diameter of the inscribed circle is slightly smaller than the diameter of a cylindrical or slightly conical bearing surface 6 of the axis 2, so that the axis 2 can be driven into the ferrule 1, hunting which elastically deforms the arms 4 to the outside. Due to its triangular shape, the outline of the opening 5 defines three discrete contact points 7 with the axis 2.
  • the width L of each arm 4 is variable, in the manner of the elastic arms of the ferrule according to EP 1 637 940, to make more homogeneous the distribution of the stresses exerted in this arm 4 by the axis 2.
  • the point 8 joining the hairspring 3 and the collar 1 is defined by one, 9c, of the three zones 9a, 9b and 9c of junction between the arms 4.
  • the inner end of the spiral 3 is integral with the axis 2 and thus follows the oscillating movements of the balance.
  • the outer end of the hairspring 3, not shown, is fixed by a pin to a fixed part of the movement, typically the rooster, in a known manner.
  • the ferrule 1 is preferably formed integrally with the spiral 3.
  • the spiral-ferrule assembly 1, 3 is typically made of a brittle material, that is to say of a material that can not deform plastically , such as a material based on silicon, glass, quartz or diamond.
  • a suitable manufacturing method for the spiral-ferrule assembly 1, 3 is the deep reactive ion etching (DRIE) ionic etching method.
  • the spiral-ferrule assembly 1, 3 may however, alternatively, be made of a ductile material, such as a metal material.
  • discrete portions 10a, 10b and 10c of the outer contour of the ferrule 1 constitute abutments against which the inner coil of the spiral 3 can come to bear during an impact suffered by the movement.
  • These stops 10a, 10b and 10c are defined by the zones 9a, 9b and 9c of junction between the elastic arms 4 and are thus arranged in a substantially regular angular distribution.
  • These abutments 10a, 10b and 10c are located, respectively, at distances Ra, Rb and Rc from the center O of the axis 2 in the plane of the ferrule 1, and more precisely have an arcuate shape with a center O and of Ra, Rb and Rc respectively.
  • the distances or radii Ra, Rb and Rc are chosen sufficiently small so that the hairspring 3 is not obstructed by the abutments 10a, 10b and 10c during normal oscillations of the pendulum and sufficiently large to, in the event of impact suffered by the movement, allow the inner coil of the spiral 3 to come to bear against one or more stops 10a, 10b and 10c before the elastic limit of this inner coil, at any point of this turn including at the junction point 8, exceeded ( Figure 2).
  • the inner turn is in abutment against one or more abutments 10a, 10b and 10c under the effect of a shock, each of the other turns can come to bear against the turn which precedes it.
  • the risk of damage to the hairspring 3 by breaking, in cases where the hairspring 3 is made of a brittle material, or by permanent deformation, in cases where the hairspring 3 is made of a ductile material, are thus reduced.
  • the distances or radii Ra, Rb and Rc grow in the winding direction of the spiral 3 going from the inside to the outside from the junction point 8 of the spiral 3 to the ferrule 1, this to take account because the radius of the inner turn of the spiral 3, like that of all the other turns, increases in this direction D.
  • the stop 10a closest to the junction point 8 in the direction D is at a distance Ra from center O which is smaller than the distance Rb separating the next stop 10b from the center O, which is smaller than the distance Rc separating the next stop 10c from the center O.
  • the distance R8 separating the point 8 of junction between the hairspring 3 and the ferrule 1 of the center O is it typically greater than or equal to the distance Ra and less than the distances Rb and Rc.
  • the distances Ra, Rb and Rc are determined by defining a certain number of radial forces F oriented towards the center O, by calculating, for example by the finite element method, the maximum elastic deformation that the inner turn can undergo under the effect of each of the radial forces F, and choosing distances Ra, Rb and Rc sufficiently large so that this maximum elastic deformation can not be reached, or at least not exceeded, and sufficiently small so that the spiral 3 does not touch the stops 10a, 10b and 10c during normal operation. Deformation of the inner coil of the spiral 3 in each of the points 3a,
  • 3b and 3c located opposite the abutments 10a, 10b and 10c respectively, in a configuration where this point bears against the corresponding abutment 10a, 10b or 10c under the effect of a radial force F applied at this point, is thus a percentage, less than or equal to 100%, of the maximum elastic deformation can undergo the inner turn at this point, which confers a safety factor (ratio between the maximum elastic deformation and the elastic deformation when the inner coil bears against a stop 10a, 10b or 10c) greater than or equal to 1.
  • the above percentage is preferably substantially the same for all abutments 10a, 10b and 10c.
  • this percentage is about 50% (safety factor of about 2), while the percentage of deformation of the inner coil in normal operation of the hairspring relative to the maximum elastic deformation this inner turn is about 25%, this for a spiral pitch 3 of about 93 microns and a thickness or width of spiral turns 3 of about 30 microns.
  • the distances Ra, Rb and Rc are equal to the same percentage, respectively, of the rays r, rb and corresponding rc of the inner turn at rest, that is to say distances between the points 3a, 3b, 3c and the center O.
  • This percentage is for example equal to about 90%, for a step of the spiral 3 of about 93 microns and a thickness or width of the coils of the spiral 3 of about 30 microns.
  • the safety factors for the abutments 10a, 10b and 10c may be the same or may less be close to each other.
  • the shell 1 can therefore reliably protect the hairspring 3 in the event of a radial impact, whatever the direction of said impact, without disturbing the normal operation of the balance-spring balance device, even if the amplitude of the oscillations of the balance is big.
  • FIG. 3 shows another embodiment of the invention, in which the ferrule 1 comprises, in addition to the abutments 10a, 10b, 10c defined by the zones 9a, 9b, 9c of junction between the arms 4, stops 10d, 10e. , 10f defined by elements 11 protruding radially from the outer side of the arms 4 in the zone center of the arms 4 in contact with the axis 2.
  • the stops 10a, 10b, 10c 1 the abutments 10d, 10e, 10f are in a center circle of the center of the center of the axis 2.
  • the opening 5 of the ferrule 1 in which the axis 2 is driven may have a shape other than triangular, such as another polygonal shape, regular or not, defined by a number of elastic arms greater than three.
  • the ferrule could be in the form of a split ring having radial projections defining the stops.
  • the abutments could be contiguous rather than discrete, and more particularly a large continuous portion of the outer contour of the ferrule could serve as a stop.
  • the outer contour would then have a shape similar to that of the inner coil, that is to say a radius increasing in the direction D of winding of the spiral going from the inside to the outside from the point of junction between the spiral and the ferrule.
  • the outer contour could in this case be defined by a frame surrounding elastic arms, or could be the outline of a ferrule "full", without lights of elasticity.

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Springs (AREA)
  • Toys (AREA)
  • Gripping On Spindles (AREA)
EP07734401.8A 2006-05-17 2007-04-26 Spiralfeder-spiralrollegesamtheit für ein uhrwerk Active EP2018601B1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP07734401.8A EP2018601B1 (de) 2006-05-17 2007-04-26 Spiralfeder-spiralrollegesamtheit für ein uhrwerk

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP06010169A EP1857891A1 (de) 2006-05-17 2006-05-17 Spiralfeder-Spiralrollegesamtheit für ein Uhrwerk
PCT/IB2007/001083 WO2007132306A2 (fr) 2006-05-17 2007-04-26 Ensemble spiral-virole pour mouvement d'horlogerie
EP07734401.8A EP2018601B1 (de) 2006-05-17 2007-04-26 Spiralfeder-spiralrollegesamtheit für ein uhrwerk

Publications (2)

Publication Number Publication Date
EP2018601A2 true EP2018601A2 (de) 2009-01-28
EP2018601B1 EP2018601B1 (de) 2018-12-05

Family

ID=37776552

Family Applications (2)

Application Number Title Priority Date Filing Date
EP06010169A Withdrawn EP1857891A1 (de) 2006-05-17 2006-05-17 Spiralfeder-Spiralrollegesamtheit für ein Uhrwerk
EP07734401.8A Active EP2018601B1 (de) 2006-05-17 2007-04-26 Spiralfeder-spiralrollegesamtheit für ein uhrwerk

Family Applications Before (1)

Application Number Title Priority Date Filing Date
EP06010169A Withdrawn EP1857891A1 (de) 2006-05-17 2006-05-17 Spiralfeder-Spiralrollegesamtheit für ein Uhrwerk

Country Status (5)

Country Link
US (1) US7758237B2 (de)
EP (2) EP1857891A1 (de)
JP (1) JP5235869B2 (de)
CN (1) CN101375218B (de)
WO (1) WO2007132306A2 (de)

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JP3143882B2 (ja) 1997-12-11 2001-03-07 音羽電機工業株式会社 電気施設の防雷方法
EP1445670A1 (de) * 2003-02-06 2004-08-11 ETA SA Manufacture Horlogère Suisse Spiralfeder der Resonatorunruh und Fabrikationsmethode
EP1818736A1 (de) * 2006-02-09 2007-08-15 The Swatch Group Research and Development Ltd. Stossfeste Spiralrolle
EP1868045B1 (de) * 2006-06-12 2019-02-20 Patek Philippe SA Genève Spiralrolle für Uhr
CH705276B1 (fr) * 2007-12-28 2013-01-31 Chopard Technologies Sa Organe d'entraînement et de transmission pour un échappement à ancre, plateau et échappement en étant équipés, et pièce d'horlogerie les comportant.
EP2317407A1 (de) * 2009-10-29 2011-05-04 Nivarox-FAR S.A. System zum Befestigen eines Teils ohne Eintreiben oder Kleben
CH702156B1 (fr) * 2009-11-13 2017-08-31 Nivarox Far Sa Résonateur balancier-spiral pour une pièce d'horlogerie.
US9250610B2 (en) 2010-03-25 2016-02-02 Rolex S.A. Split collet with a non-circular opening
CH704764A2 (fr) * 2011-03-31 2012-10-15 Cartier Creation Studio Sa Mécanisme d'échappement notamment pour mouvement d'horlogerie.
EP2590325A1 (de) * 2011-11-04 2013-05-08 The Swatch Group Research and Development Ltd. Thermokompensierter Resonator aus Keramik
JP5932380B2 (ja) * 2012-02-15 2016-06-08 セイコーインスツル株式会社 ひげ玉、てんぷおよび時計
JP6118037B2 (ja) * 2012-05-08 2017-04-19 セイコーインスツル株式会社 ひげ玉、てんぷおよび時計
EP2690507B1 (de) * 2012-07-26 2014-12-31 Nivarox-FAR S.A. Spiralfeder einer Uhr
HK1186057A2 (en) 2013-01-14 2014-03-07 Master Dynamic Limited Stress-relief elastic structure of hairspring collet
EP2916177B1 (de) * 2014-03-05 2018-11-07 Nivarox-FAR S.A. Spirale, die mit einer Federscheibe gesichert werden muss
EP2952977A1 (de) * 2014-06-03 2015-12-09 Nivarox-FAR S.A. Uhrkomponente aus geschweißten Materialien
CH709792A2 (fr) * 2014-06-18 2015-12-31 Eta Sa Manufacture Horlogère Suisse Mobile d'horlogerie.
EP3023844B1 (de) * 2014-11-20 2017-06-28 Nivarox-FAR S.A. Flexible Spiralrolle
EP3106928A1 (de) * 2015-06-16 2016-12-21 Nivarox-FAR S.A. Herstellungsverfahren, das einen modifizierten automatendreh-schritt umfasst
EP3106935A1 (de) * 2015-06-16 2016-12-21 Nivarox-FAR S.A. Herstellungsverfahren eines werstücks, das einen modifizierten polierschritt umfasst
EP3106932A1 (de) * 2015-06-16 2016-12-21 Nivarox-FAR S.A. Herstellungsverfahren, das einen modifizierten montageschritt umfasst
EP3106931A1 (de) * 2015-06-16 2016-12-21 Nivarox-FAR S.A. Werkstück mit entkoppelter schweissoberfläche
EP3159746B1 (de) * 2015-10-19 2018-06-06 Rolex Sa Hochdotierte siliziumfeder für uhr
EP3176650B1 (de) * 2015-12-02 2019-02-06 Nivarox-FAR S.A. Schutz einer uhrkomponente aus mikro-bearbeitbarem material
EP3309625B1 (de) 2016-10-13 2020-07-29 Nivarox-FAR S.A. Spirale zur befestigung mit einer federscheibe
CN108801138A (zh) * 2018-06-19 2018-11-13 哈尔滨工业大学 一种利用外切圆法测量圆柱形构造物中心坐标的装置
EP3627238A1 (de) * 2018-09-21 2020-03-25 Nivarox-FAR S.A. Elastisches halterungsorgan für die befestigung einer uhrenkomponente auf einem halteelement
EP3627236A1 (de) * 2018-09-21 2020-03-25 Nivarox-FAR S.A. Elastisches halterungsorgan für die befestigung einer uhrenkomponente auf einem halteelement
EP3627235A1 (de) * 2018-09-21 2020-03-25 Nivarox-FAR S.A. Elastisches halterungsorgan für die befestigung einer uhrenkomponente auf einem halteelement

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Also Published As

Publication number Publication date
US7758237B2 (en) 2010-07-20
CN101375218B (zh) 2011-06-29
US20090135679A1 (en) 2009-05-28
WO2007132306A3 (fr) 2008-04-17
JP2009537813A (ja) 2009-10-29
EP1857891A1 (de) 2007-11-21
CN101375218A (zh) 2009-02-25
EP2018601B1 (de) 2018-12-05
WO2007132306A2 (fr) 2007-11-22
JP5235869B2 (ja) 2013-07-10

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