EP1970778B1 - Pièce d'horlogerie comprenant un dispositif indicateur de réserve de marche - Google Patents

Pièce d'horlogerie comprenant un dispositif indicateur de réserve de marche Download PDF

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Publication number
EP1970778B1
EP1970778B1 EP07104055A EP07104055A EP1970778B1 EP 1970778 B1 EP1970778 B1 EP 1970778B1 EP 07104055 A EP07104055 A EP 07104055A EP 07104055 A EP07104055 A EP 07104055A EP 1970778 B1 EP1970778 B1 EP 1970778B1
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EP
European Patent Office
Prior art keywords
barrel
wheel
timepiece according
differential gear
timepiece
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
EP07104055A
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German (de)
English (en)
French (fr)
Other versions
EP1970778A1 (fr
Inventor
Alain Zaugg
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.)
Montres Breguet SA
Original Assignee
Montres Breguet SA
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 Montres Breguet SA filed Critical Montres Breguet SA
Priority to DE602007002471T priority Critical patent/DE602007002471D1/de
Priority to EP07104055A priority patent/EP1970778B1/fr
Priority to AT07104055T priority patent/ATE443282T1/de
Priority to US12/043,342 priority patent/US7490977B2/en
Priority to JP2008059047A priority patent/JP5436788B2/ja
Priority to CN2008100864408A priority patent/CN101281386B/zh
Publication of EP1970778A1 publication Critical patent/EP1970778A1/fr
Application granted granted Critical
Publication of EP1970778B1 publication Critical patent/EP1970778B1/fr
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Anticipated expiration legal-status Critical

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    • 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
    • G04B9/00Supervision of the state of winding, e.g. indicating the amount of winding

Definitions

  • the present invention relates to a timepiece comprising a power reserve indicator device, that is to say a device for indicating to the wearer the degree of winding of the mainspring of a mechanical timepiece. .
  • Timepieces comprising devices for providing this power reserve indication are designed to take into account the rotation of the ratchet wheel during the winding of the mainspring as well as the rotation of the barrel during disarming of the spring. barrel.
  • most of these known devices implement a differential gear.
  • a device of this type is described, for example, in the patent EP 1 074 897 wherein the two inputs of the differential gear are respectively connected to the toothing of the barrel drum and that of the ratchet wheel, the output of the differential gear being connected to an indicator member.
  • Utility model is also known DE1638800U a power reserve indicator device using a dual-satellite planar differential gear disposed between the barrel bridge and the barrel cover to eliminate the gearing and disarming gear,
  • the gear ratio provided by this type Differential gearing does not make it possible to display the power reserve on a slightly extended arc, for example of the order of 30 °, without a display reduction gear.
  • this power reserve device has a limited footprint in the plane, it has a large footprint that hinders its height in its movement in small thickness.
  • the present invention aims to remedy the problems and disadvantages above as well as others by proposing a timepiece comprising a power reserve indicator device having a small footprint in the plane and height as well as a great simplicity of construction by creating a more judicious arrangement of the elements of the power reserve indicator device.
  • Another object of the invention is also to provide a timepiece comprising a power reserve indication device to limit or even eliminate the gearing reduction, arming, disarming and display of the power reserve.
  • Another object of the invention is also to provide a timepiece comprising a power reserve indication device having an improved accuracy of the display of the power reserve.
  • Yet another object of the invention is to provide a timepiece comprising a power reserve indication device for displaying without gear reduction, the power reserve on are are less than 30 ° circle.
  • the present invention relates to a timepiece as defined by claim 1 of the patent.
  • the present invention provides a compact and simple power-reserve indicating device which can minimize the reduction of arming and disarming workings.
  • This solution also provides a power reserve indicator at least partially integrated into the lid or the bottom of the barrel, which significantly reduces its size.
  • the indicator member is directly carried by said ring gear to form the output of the differential gear.
  • This embodiment makes it possible to eliminate the display reduction gear in the sense that the display member of the power reserve is integrated with the differential gear.
  • FIG. 1 to 5 partially illustrate a timepiece of the wristwatch type for example, equipped with a power reserve indicator device according to the present invention and generally designated by the general numerical reference 1.
  • the watch comprises a watch movement M comprising a plate P on which is mounted a cylinder 2 in which is housed a cylinder spring 4.
  • the cylinder 2 conventionally comprises a drum 6 closed by a cover 8 and a bottom 10.
  • the cylinder 2 is freely rotatably mounted on the 12 barrel shaft secured to the bung 14.
  • the spring 4 is hooked by its inner end to the plug 14 and its outer end to the inner wall of the drum 6.
  • the barrel 2 is conventionally mounted between the plate P of the movement and a bridge 3 comprising a central portion 3a from which extend a bridge branch 3b and a bridge branch 3c.
  • the power reserve indicator device 1 is applied a cylinder associated with a rocket F also mounted on the plate P via the bridge arm 3c.
  • a chain C of which only one link is shown in the drawing, is attached by a first end to the barrel drum 6.
  • the chain C is progressively wound on the drum 6 from the rocket F to which it is fixed by a second end during disarming of the barrel.
  • the rocket F is conventionally associated with a ratchet R and comprises a toothed portion D engaged on the one hand with a work train and on the other hand with a winding train.
  • the barrel shaft 12 is fixed relative to the plate of the movement P.
  • the barrel shaft 12 is mounted between the plate P and the bridge leg 3b.
  • the bridge arm 3b also bears on its face disposed opposite the cover 8 a toothed wheel 16 forming a first input of a differential gear which will be described in more detail below.
  • the toothed wheel 16 is frictionally mounted on the branch of the bridge 3b by means of a spring ring 17 secured to the bridge branch 3b.
  • the second input of the differential gear is formed by the barrel 4 and more precisely by the cover 8 integral with the drum 6 which can pivot around the barrel shaft 12 with the barrel when the barrel disarms.
  • the cover 8 which thus forms the frame of the differential gear is thus arranged coaxially with the barrel shaft.
  • the cover 8 carries a first satellite mobile 18 comprising a first wheel 18a and a second wheel 18b coaxial with the wheel 18a.
  • the wheel 18a is engaged with the wheel 16 while the wheel 18b is engaged with a second satellite mobile 20 which is in turn engaged with a movable ring gear 22 which forms the output of the differential gear.
  • the crown 22 carries a display member formed of a power reserve needle 24 which, depending on the relative position it occupies with respect to a mark 26 carried by the plate P via a foot 26a, indicates carrying the power reserve available according to the number of winding turns of the mainspring.
  • the power reserve indication device further comprises means 28, 30 for limiting the angular travel of the internal gear wheel 22 so that the needle 24 moves between two positions of fixed and defined extreme arming and disarming corresponding to the degrees of arming respectively extreme disarming of the mark 26.
  • the limiting means 28, 30 comprise in the illustrated example three studs 28 integral with the bridge 3, the studs 28 moving each in an opening 30 formed in the internal gear wheel 22.
  • the openings 30 are outwardly open cuts formed in the circumferential periphery of the wheel 22, these openings 30 each defining two radial abutment surfaces 30a and 30b for the stud 28 associated with it.
  • the barrel cover 8 comprises a central recess 8a set back relative to its peripheral rim 8b and that the internal gear wheel 22 extends substantially in the plane of the rim 8b of the cover 8
  • This arrangement advantageously makes it possible to integrate the display device of the power reserve into the barrel and to limit as far as possible its overall height in the movement.
  • the wheels of the differential gear and in particular the gear ratios of the wheels 16, 18a, 18b, 20, and 22 are provided to provide, between the input 16 and the output 22 of the differential a gear ratio of between 60 and 120 and preferably 80.
  • a gear ratio of between 60 and 120 and preferably 80 By way of example, with a wheel 54 of 54 teeth, a wheel 18a of 10 teeth, a wheel 18b of 15 teeth, a wheel 20 11 teeth and a wheel 22 of 80 teeth is obtained a ratio of 1/80 e , for 6 turns of the barrel is obtained an angular displacement of 27 ° of the needle 22 linked to the wheel 22 and without gear reduction arming, and display.
  • the barrel shaft 12 and the wheel are fixed.
  • the drum 6 is rotated by the barrel spring 4 in the anti-clockwise direction (arrow F D , figure 2 ).
  • the chain C connected to the drum 6 is then wound progressively on the drum 6 from the rocket F which is in turn rotated to provide the finishing gear its driving force.
  • the wheel 18a of the satellite mobile 18 carried by the barrel cover 8 rolls on the toothing of the fixed wheel 16 also in the counterclockwise direction.
  • the wheel 18b of the mobile 18, integral in rotation with the wheel 18a then drives, in the clockwise direction, the wheel 20 in engagement with the internal toothing of the ring gear 22.
  • the ring 22 then drives the needle of the wheel in a counterclockwise direction. power reserve 24 opposite the mark 26.
  • the barrel drum 6 continues to drive the power reserve needle 24 as just described until the pads 28 come into contact with the radial surfaces of stop 30a of the openings 30.
  • the power reserve needle 24 is opposite the zero mark of the mark 26, that is to say in the position in which the mainspring 4 is totally disarmed.
  • the display needle 24 during disarming thus performs a gradual angular displacement from the indication representative of the complete winding of the mainspring, depending on the power reserve which can still be provided by the winding from the mainspring spring 4 to the indication representative of the complete disarming of the spring 4.
  • the chain C initially wound on the rocket was completely unrolled from the latter and wound on the barrel drum 6.
  • the rocket is actuated via its toothed portion in order to rewind the chain C on the rocket from the cylinder 6 on which it is wound.
  • the drum 6 is rotated about the barrel shaft 12 which is fixed relative to the platen of the movement.
  • the drum 6 then rotates clockwise (arrow A figure 2 ).
  • the wheel 18a of the satellite mobile 18 carried by the barrel cover 8 rolls on the toothing of the fixed wheel 16 also in the clockwise direction.
  • the wheel 18b of the mobile 18, integral in rotation with the wheel 18a then drives, in the counterclockwise direction, the wheel 20 in engagement with the internal toothing of the ring gear 22.
  • the ring gear 22 then drives in the clockwise direction.
  • the barrel drum 6 continues to drive the power reserve needle 24 as just described until the studs 28 come into contact with the surfaces. In this position, the power reserve needle 24 is opposite the 100% scale of the mark 26, that is to say in the position in which the mainspring 4 is totally rearmed.
  • the display needle 24 thus performs an angular displacement in the opposite direction to the previous one as a function of the power reserve provided by the number of winding turns of the mainspring. At this time, the chain C initially wound on the barrel drum 6 completely unrolled from the latter and wound on the rocket F.
  • the invention can in particular be used with a conventional barrel movement that the latter is manual or automatic winding.
  • a disengaging mechanism must be provided in order not to distort the power reserve indication when the mainspring is fully armed and the flange slides into the barrel.
  • the barrel shaft is pivotally mounted on the plate and is associated with a ratchet wheel controlled by a gear train.
  • the power reserve indication device therefore operates in a manner identical to that just described above.
  • the barrel drum that can be considered fixed.
  • the barrel shaft 12 is therefore rotated clockwise by a rearming gear so that it drives the mobile 18 in the counterclockwise direction.
  • the gear train 18 in turn drives the wheel 20 clockwise.
  • the wheel 22, carrying the power reserve indication needle, which is directly engaged with the wheel 20, is therefore driven in a counter-clockwise direction relative to the mark 26.

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Measurement Of Unknown Time Intervals (AREA)
  • Transmission Devices (AREA)
  • Gear Transmission (AREA)
  • Electromechanical Clocks (AREA)
  • Retarders (AREA)
  • Electric Clocks (AREA)
EP07104055A 2007-03-13 2007-03-13 Pièce d'horlogerie comprenant un dispositif indicateur de réserve de marche Active EP1970778B1 (fr)

Priority Applications (6)

Application Number Priority Date Filing Date Title
DE602007002471T DE602007002471D1 (de) 2007-03-13 2007-03-13 Uhr mit Anzeige der Gangreserve
EP07104055A EP1970778B1 (fr) 2007-03-13 2007-03-13 Pièce d'horlogerie comprenant un dispositif indicateur de réserve de marche
AT07104055T ATE443282T1 (de) 2007-03-13 2007-03-13 Uhr mit anzeige der gangreserve
US12/043,342 US7490977B2 (en) 2007-03-13 2008-03-06 Timepiece including a power reserve indicator device
JP2008059047A JP5436788B2 (ja) 2007-03-13 2008-03-10 パワーリザーブ表示機構を有する時計
CN2008100864408A CN101281386B (zh) 2007-03-13 2008-03-12 包括动力储备指示器装置的计时器

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP07104055A EP1970778B1 (fr) 2007-03-13 2007-03-13 Pièce d'horlogerie comprenant un dispositif indicateur de réserve de marche

Publications (2)

Publication Number Publication Date
EP1970778A1 EP1970778A1 (fr) 2008-09-17
EP1970778B1 true EP1970778B1 (fr) 2009-09-16

Family

ID=38846888

Family Applications (1)

Application Number Title Priority Date Filing Date
EP07104055A Active EP1970778B1 (fr) 2007-03-13 2007-03-13 Pièce d'horlogerie comprenant un dispositif indicateur de réserve de marche

Country Status (6)

Country Link
US (1) US7490977B2 (zh)
EP (1) EP1970778B1 (zh)
JP (1) JP5436788B2 (zh)
CN (1) CN101281386B (zh)
AT (1) ATE443282T1 (zh)
DE (1) DE602007002471D1 (zh)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3333637A1 (fr) 2016-12-12 2018-06-13 ETA SA Manufacture Horlogère Suisse Mouvement d'horlogerie mecanique a detection de reserve de marche

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2339410B1 (fr) * 2009-12-28 2013-03-27 Blancpain S.A. Dispositif dynamométrique indicateur de réserve de couple de barillet de pièce d'horlogerie
CN102591188B (zh) * 2012-03-15 2013-08-14 烟台北极星股份有限公司 一种机械时钟机芯的设计方法及其机芯
CH707136B1 (fr) 2012-10-30 2016-12-30 Parmigiani Fleurier S A Pièce d'horlogerie destinée à indiquer la réserve de marche.
EP2735919B1 (fr) * 2012-11-27 2015-07-22 Montres Breguet SA Mouvement de montre comportant une fusée
CN104049520B (zh) * 2013-03-15 2016-08-31 天津海鸥表业集团有限公司 一种链条传动式手表时间指示机构
EP2869135A1 (fr) 2013-11-04 2015-05-06 Chronometres Ferdinand Berthoud Neuchatel SA, Val-de-Travers Système de fusée
EP2869134B1 (fr) 2013-11-04 2020-02-26 Chronometrie Ferdinand Berthoud SA Système de barillet pour pièce d'horlogerie
EP2977827B1 (fr) * 2014-07-22 2017-11-15 Montres Breguet SA Barillet d'horlogerie à transmission d'effort améliorée
EP3098668B1 (fr) 2015-05-29 2018-10-31 ETA SA Manufacture Horlogère Suisse Indicateur de reserve de marche pour piece d'horlogerie
EP3217227B1 (fr) * 2016-03-11 2019-02-27 The Swatch Group Research and Development Ltd. Mecanisme regulateur d'horlogerie a echappement magnetique optimise
EP3306416B1 (fr) * 2016-10-04 2019-08-21 ETA SA Manufacture Horlogère Suisse Mouvement d'horlogerie mécanique à détection de réserve de marche
EP3382468B1 (fr) * 2017-03-30 2020-01-15 The Swatch Group Research and Development Ltd Mouvement avec prolongateur de réserve de marche
KR102172820B1 (ko) * 2017-07-25 2020-11-03 불랑패인쏘시에떼아노님 특히 스트라이킹 메카니즘을 가진 타임피스를 위한 토크 스무싱
EP3435169B1 (fr) * 2017-07-25 2023-03-01 Blancpain SA Mécanisme d'arrêtage pour mécanisme de sonnerie d'horlogerie
EP3627233B1 (fr) * 2018-09-19 2022-03-30 ETA SA Manufacture Horlogère Suisse Mecanisme indicateur de reserve de marche d'horlogerie
JP7347103B2 (ja) * 2019-10-16 2023-09-20 セイコーエプソン株式会社 時計
EP3992727A1 (fr) * 2020-10-30 2022-05-04 ETA SA Manufacture Horlogère Suisse Mouvement d'horlogerie mecanique a detection de reserve de marche
EP4057080A1 (fr) * 2021-03-09 2022-09-14 ETA SA Manufacture Horlogère Suisse Dispositif d'affichage d'horlogerie sur plusieurs mobiles

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Publication number Priority date Publication date Assignee Title
US790510A (en) * 1904-08-16 1905-05-23 Joseph Mazer Winding-indicator for watches.
US790509A (en) * 1904-08-16 1905-05-23 Joseph Mazer Watch.
US942659A (en) * 1908-04-10 1909-12-07 Waltham Watch Co Winding-indicator.
FR425795A (fr) * 1911-02-09 1911-06-20 Adolphe Bourgeat Dispositif indicateur de remontage pour mouvements d'horlogerie
US1937310A (en) * 1928-07-07 1933-11-28 Bornfriend Louis Winding indicator and limiting mechanism
CH284137A (fr) * 1950-04-19 1952-07-15 Jeanneret Herbert Dispositif indicateur de développement du ressort d'une pièce d'horlogerie.
DE1638800U (de) 1952-01-28 1952-05-21 Junghans Geb Ag Vorrichtung an uhrwerken.
CH313605A (de) * 1953-04-01 1956-04-30 Felsa Ag Uhrwerk mit einem mit dem Federhaus und mit der Federhauswelle in Antriebsverbindung stehenden Differentialgetriebe
JPH11183642A (ja) * 1997-12-22 1999-07-09 Seiko Instruments Inc ぜんまい巻き状態表示装置付き時計
JPH11183643A (ja) * 1997-12-25 1999-07-09 Seiko Instruments Inc パワーリザーブ機構およびパワーリザーブ機構の表示ユニット
JP2002148363A (ja) * 1998-11-27 2002-05-22 Seiko Epson Corp 時 計
ATE428958T1 (de) 1999-08-04 2009-05-15 Piguet Frederic Sa Vorrichtung zur anzeige der gangreserve einer uhr
JP4475630B2 (ja) * 2004-01-27 2010-06-09 セイコーインスツル株式会社 変形セグメント歯車を含むぜんまい巻き状態表示装置付き時計
JP2005274420A (ja) * 2004-03-25 2005-10-06 Seiko Epson Corp 時計
CN1252139C (zh) * 2004-08-24 2006-04-19 四川大学 聚苯硫醚的纯化方法

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3333637A1 (fr) 2016-12-12 2018-06-13 ETA SA Manufacture Horlogère Suisse Mouvement d'horlogerie mecanique a detection de reserve de marche

Also Published As

Publication number Publication date
EP1970778A1 (fr) 2008-09-17
CN101281386B (zh) 2011-12-14
DE602007002471D1 (de) 2009-10-29
US7490977B2 (en) 2009-02-17
CN101281386A (zh) 2008-10-08
ATE443282T1 (de) 2009-10-15
JP2008224668A (ja) 2008-09-25
JP5436788B2 (ja) 2014-03-05
US20080225646A1 (en) 2008-09-18

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