EP2037335A2 - Anchor for a timepiece escapement - Google Patents

Anchor for a timepiece escapement Download PDF

Info

Publication number
EP2037335A2
EP2037335A2 EP08164108A EP08164108A EP2037335A2 EP 2037335 A2 EP2037335 A2 EP 2037335A2 EP 08164108 A EP08164108 A EP 08164108A EP 08164108 A EP08164108 A EP 08164108A EP 2037335 A2 EP2037335 A2 EP 2037335A2
Authority
EP
European Patent Office
Prior art keywords
anchor
arms
fork
anchor according
armature
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
EP08164108A
Other languages
German (de)
French (fr)
Other versions
EP2037335A3 (en
EP2037335B1 (en
Inventor
August Enzler
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.)
VON GUNTEN, STEPHANE
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to EP13187564.3A priority Critical patent/EP2687916B1/en
Publication of EP2037335A2 publication Critical patent/EP2037335A2/en
Publication of EP2037335A3 publication Critical patent/EP2037335A3/en
Application granted granted Critical
Publication of EP2037335B1 publication Critical patent/EP2037335B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

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
    • G04B15/00Escapements
    • G04B15/14Component parts or constructional details, e.g. construction of the lever or the escape wheel
    • 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
    • G04B15/00Escapements
    • G04B15/06Free escapements
    • G04B15/08Lever escapements

Definitions

  • the present invention relates to an anchor for a watch escapement with escape wheel of a mechanical watch according to the preamble of claim 1.
  • the basic features of the function of a mechanical watch are today well known and well documented.
  • the movements of mechanical watches generally draw their energy from a spring, usually a coil spring, the elevator spring or the so-called Barillet.
  • This energy is delivered to a gear transmission, which in turn via pointer elements, for example, the information for the display of the hour reproduces, to the last element, the so-called inhibition.
  • the latter has three functions, namely to count the number of oscillations of the balance, that is, to measure the time, to block the energy of the gear during the additional turn of the balance and to give the balance an impulse to maintain its oscillating motion.
  • the so-called Swiss lever escapement where each of the pallets held in the anchor alternatively provides a boost from the Escapement wheel gets to pass it on to the balance, which is the most widely used in the watch industry.
  • the flow of force is subject to friction.
  • the energy that has been collected in the elevator spring experiences losses in the transmission from the mainspring via the transmission to the last element, the balance.
  • the elevator spring must be increased in order to obtain a sufficient service life of the clock and the drain reserve.
  • the vibration frequency or the inertia of the balance could be increased.
  • the improvement in accuracy achieved in this way would have to be bought in turn with the enlargement of the balance or the mainspring, which is undesirable.
  • each stage of the gear train has an efficiency of about 90% to 95%.
  • the tooth engagement and profile of the teeth have been optimized as a result.
  • lubricants have the disadvantage of deteriorating over time, namely aging, oxidizing, cracking and rancidity.
  • lubricants are susceptible to the absorption of dust and tend to harden.
  • Lubricants are therefore hardly used for bearing journals of the anchor.
  • the anchor as a whole is denoted by A.
  • the anchor has two anchor arms B, in each of whose ends a pallet C is held.
  • a fork D In the middle between the two armature arms in the connecting region engages a fork D, which extends virtually perpendicular or at least on an angle bisector of the two armature arms.
  • the fork D ends in tines E and the pivotal movement of the armature or the fork D is limited by two lateral anchor boundary pins F in the pivoting movement. This pivoting movement takes place about a bearing axis G with bilateral bearing journals H, which rest in bearing stones, not shown here.
  • the anchor according to the invention is always designated 1. Also, this anchor has like two anchor arms 2 like a conventional anchor. The pallets 3 are held at the end in the two anchor arms 2. These two armature arms 2 are integrally connected to each other and in the connection area, the fork 4 engages the armature. The fork 4 is practically perpendicular to the two armature arms 2, when they are stretched aligned with each other.
  • the fork 4 lies on the bisector of said angle. Terminally, the fork 4 forks 5 and the fork horn on. This part again corresponds to the conventional style.
  • the region in which the fork 4 is connected to the two armature arms 2 is defined here as the connection region 6.
  • two fastening arms 7 engage. These attachment arms 7 extend exactly straight in the simplest embodiment shown here. With respect to the central axis through the fork 4, the two attachment arms 7 extend mirror-symmetrically. Consequently, so forms the fork 4 and the center axis of the Angle bisector with respect to the angle, the two mounting arms 7 include each other.
  • fasteners 8 Terminal at the two mounting arms 7 are fasteners 8, which are configured in the preferred embodiment here as an annular eyelets. Accordingly, the following is also spoken of eyelets 8, the expert will understand, of course, other fastener forms underneath.
  • the choice of fasteners as eyelets is therefore preferred because they are both suitable to be connected by means of screws with a corresponding fixed part of the movement, for example, the movement board.
  • the eyelets 8 are also suitable for a soldered or welded connection as well as for an adhesive connection. For the latter types of connection but simple disc-shaped embodiments of the fasteners would be just as suitable.
  • the smoothest possible embodiment of the inventive anchor is achieved by making the attachment arms as long as possible and as thin as possible in width.
  • the height of the attachment arm is of course not free, since this must be sufficiently large so as not to obtain rotational degrees of freedom that are not in the plane of the anchor. If you would also choose the height of the mounting arm also very small, so the mounting arms would behave like threads and would be stiff only on train and pressure but otherwise very flexible in all bending directions. But this is not wanted but the freedom of movement should be limited to a bending movement of the mounting arms 7 within the extension plane in which the anchor is located.
  • the simplest embodiment of the inventive anchor described so far with two flexible mounting arms 7 still has a relative disadvantage.
  • This anchor has a so-called parasitic motion. This is the unwanted, albeit small, erroneous movement of the rotation center, so called the virtual axis.
  • the third embodiment of the subject invention as shown in the FIGS. 5 and 6 is shown, also solves this problem.
  • the armature should rotate about a given virtual axis without offset movement of the center. This problem can be largely reduced, for example, by allowing the mounting arms 7, as in the FIGS. 5 and 6 represented, designed.
  • the fastening arms 7 are designed with two parallel elastic sections 70 and 71. These two sections 70 and 71 are hairpin-like.
  • the two sections are parallel and arranged in opposite directions.
  • the two elastic partial sections 70, 71 are connected to one another via a thickened connection point 72.
  • the first elastic section 70 thus extends between the thickened connection point 72 and the connection region 6 of the armature 1 or to a thickened part of the Mounting arms 7 which is referred to here as the connecting part 73.
  • the second elastic section 71 extends from the thickened connection point 72 to a thickened fastening arm part 74, on which the fastening element or fastening eye 8 is formed at the end.
  • the elastic spring element 10 lies in the same plane as the fastening arms 7 and the remaining parts of the armature 1 according to the invention.
  • the fastening arms 7 must be fastened with their fastening element 8 either on the same board of the movement or at least on another fixed part of the movement, which lies in the same plane.
  • the zugelastician spring element 10 has a much smaller width b in relation to height h.
  • the zugelastician spring element 10 may in principle have any shape that deviates from a straight line.
  • the zugelastician spring element 10 could be as simple, arcuate arched arm be designed or as shown here, as in the plane meandering route.
  • the two fastening arms 7 are arranged mirror-symmetrically with respect to the central longitudinal axis of the fork 4, a different solution is shown here.
  • the elastic attachment arms 7 are in turn as elongated elements between the connecting portion 6 and the terminal fasteners 8, which in turn are configured here as eyelets, extending.
  • These two fastening arms 7 are now both arranged on the same side of the fork 4 between these and an armature arm 2.
  • the zugelastician spring element 10 is now placed so that the connecting line between the center of the elongated hole 12 and the point of attachment of the zugelastischen spring element 10 at the connecting portion 6, the bisecting line between the two mounting arms 7.
  • the virtual axis of rotation is always at the intersection of the extensions of the two mounting arms 7. While in the examples described above, where the mounting arms 7 are arranged mirror-symmetrically with respect to the fork 4, this virtual axis of rotation can also lie outside the connection area 6, it is in the Embodiment according to the FIGS. 7 and 8 preferably such that the virtual axis of rotation lies in the center of the connecting region 6. In other words, the place of virtual axis of rotation can thus be determined virtually free by the choice of the arrangement of the mounting arms 7.
  • FIG. 7 is contrary to FIG. 8 also shown the possibility that the pallets 3 also monolithic one piece and thus made of the same material as the anchor 1 in one operation.
  • a manufacturing method for the production of the inventive anchor in which the boundary edges of the armature are extremely regularly finished with a very low roughness, friction losses are thus reduced.
  • two methods are suitable for the production.
  • One method is called a DRIE method.
  • DRIE Deep Reactive Ion Etching. This procedure was by the company Bosch develops and in this regard, for example, on the documents DE-3927163 or DE-4420962-A directed.
  • fastening arms 7 can be produced with a very small width.
  • the attachment arms 7 are made with a width of 15-50 microns.
  • the geometry of an inventive anchor produced in this way has an extreme accuracy, with deviations that are usually less than one micrometer.
  • silicon in the form of wafers may be considered as the material of manufacture for this process.
  • This material is particularly suitable for the production of the anchor.
  • this material has ideal properties for this application. It has a high mechanical strength and a very low plastic deformability, so that the areas with large thickness in the loading direction have virtually no deformation. This leads to extremely low losses. Material fatigue practically does not occur as long as the applied stresses at the alternating stresses are kept below the elastic breaking point.
  • silicon has a very low coefficient of friction. The only problem is that the parts etched by the DRIE method have very sharp edges. For the watchmaker who works with the tweezers, it is thus possible for the watchmaker to produce very high pressures locally on the sharp edges. This can lead to the destruction of the anchor.
  • material is deposited around the edges or material is removed, so that the edges undergo certain curves.
  • the silicon oxide and the silicon nitride also have tribological advantages in which in turn the coefficient of friction is positively influenced.
  • silicon is the preferred material for the anchor, it can also be made of quartz, pyrex glass, sapphire or diamond. All these materials can be produced synthetically, are accordingly hard and abrasion resistant. In addition, these materials can be at least partially processed by the DRIE method.
  • Another preferred manufacturing method is known from the so-called LIGA technology. With regard to the LIGA process, reference is made, for example, to the European patents EP-0183910A or the EP-1431844-A as well as on the U.S. Patent 6458263-B directed. In particular, nickel or nickel phosphorus compounds are used for the LIGA process. Also by means of this method can be an inventive anchor with the required dimensions and manufacture accuracy having the desired physical properties.
  • the LIGA process is a lithographic-galvanic etching process.

Abstract

The anchor (1) has two anchor arms (2) in each of which a pallet (3) is held. A fork (4) and a fork clamp are provided at its end, which acts on a balance wheel. The exit pallets carrying anchor arms and fork together with two fastening arms (7) are integrally manufactured. The fastening arms, which run in the same plane as the other anchor units, are elastically shaped with a certain length. An independent claim is included for a method for manufacturing an anchor.

Description

Die vorliegende Erfindung betrifft einen Anker für eine Uhrenhemmung mit Hemmungsrad einer mechanischen Uhr gemäss Oberbegriff des Patentanspruches 1.The present invention relates to an anchor for a watch escapement with escape wheel of a mechanical watch according to the preamble of claim 1.

Die Grundzüge der Funktion einer mechanischen Uhr sind heute allgemein bekannt und gut dokumentiert. Die Uhrwerke der mechanischen Uhren schöpfen im allgemeinen ihre Energie aus einer Feder, meist einer Spiralfeder, der Aufzugsfeder beziehungsweise der so genannten Barillet. Diese Energie wird auf ein Zahnradgetriebe abgegeben, welches wiederum über Zeigerelemente, zum Beispiel die Information für die Anzeige der Stunde wiedergibt, bis zum letzten Element, der so genannten Hemmung. Letztere hat drei Funktionen, nämlich die Anzahl der Oszillationen der Unruh zu zählen, das heisst die Zeit zu messen, die Energie des Räderwerks während des zusätzlichen Drehweges der Unruh zu blockieren und der Unruh einen Impuls zu übermitteln um ihre oszillierende Bewegung zu erhalten. Die so genannte Schweizer Ankerhemmung, wo jede der im Anker gehaltenen Paletten alternativ einen Impuls vom Hemmungsrad erhält um ihn an die Unruh weiterzugeben, ist das am meisten benutzte in der Uhrenindustrie.The basic features of the function of a mechanical watch are today well known and well documented. The movements of mechanical watches generally draw their energy from a spring, usually a coil spring, the elevator spring or the so-called Barillet. This energy is delivered to a gear transmission, which in turn via pointer elements, for example, the information for the display of the hour reproduces, to the last element, the so-called inhibition. The latter has three functions, namely to count the number of oscillations of the balance, that is, to measure the time, to block the energy of the gear during the additional turn of the balance and to give the balance an impulse to maintain its oscillating motion. The so-called Swiss lever escapement, where each of the pallets held in the anchor alternatively provides a boost from the Escapement wheel gets to pass it on to the balance, which is the most widely used in the watch industry.

Wie jedes mechanische System ist der Kraftfluss mit Reibung behaftet. Die Energie, die in der Aufzugsfeder gesammelt wurde erfährt Verluste bei der Übertragung von der Aufzugsfeder über das Getriebe bis zum letzten Element, der Unruh. Dies hat mehrere Nachteile. Zur Kompensation der Energieverluste muss die Aufzugsfeder vergrössert werden um eine genügende Funktionsdauer der Uhr sowie der Ablaufreserve zu erhalten. Um den Einfluss der Reibungsverluste relativ zu reduzieren, liesse sich die Schwingfrequenz oder die Trägheit der Unruh erhöhen. Die so erzielte Verbesserung der Ganggenauigkeit müsste man sich aber wiederum mit der Vergrösserung der Unruh oder der Aufzugsfeder erkaufen, was unerwünscht ist.Like any mechanical system, the flow of force is subject to friction. The energy that has been collected in the elevator spring experiences losses in the transmission from the mainspring via the transmission to the last element, the balance. This has several disadvantages. To compensate for the energy losses, the elevator spring must be increased in order to obtain a sufficient service life of the clock and the drain reserve. In order to reduce the influence of the friction losses relatively, the vibration frequency or the inertia of the balance could be increased. The improvement in accuracy achieved in this way would have to be bought in turn with the enlargement of the balance or the mainspring, which is undesirable.

Ein Teil der Energie, die in der Aufzugsfeder gespeichert wurde, geht durch Reibung im Zahneingreifvorgang und beim Drehen des Räderwerkes in deren Lager verloren. Typisch hat jede Stufe des Räderwerks einen Wirkungsgrad von ungefähr 90% bis 95%. Der Zahneingreifvorgang und das Profil der Zähne wurden in Folge dessen optimiert.Part of the energy stored in the elevator spring is lost due to friction in the tooth meshing process and when turning the gear train into its bearing. Typically, each stage of the gear train has an efficiency of about 90% to 95%. The tooth engagement and profile of the teeth have been optimized as a result.

Ein anderer Teil der Energie geht an der Hemmung, vor allem durch Gleitreibung, verloren. Typisch beträgt der Wirkungsgrad letzterer ungefähr 40%. Die Verluste an der Hemmung können in mehreren Teilen getrennt werden:

  • ■ Übertragung der Energie des Hemmungsrades an die Paletten des Ankers;
  • ■ Führung des Ankers durch seine Achse in den Lagersteinen;
  • ■ Übertragung der Energie des Ankers an die Unruh und Reibungsverluste der Lagerung der Spindel der Unruh in einem entsprechenden Lagerstein.
Another part of the energy is lost at the inhibition, especially by sliding friction. Typically this is Efficiency of the latter about 40%. The losses at the inhibition can be separated in several parts:
  • ■ transmission of the energy of the escape wheel to the pallets of the anchor;
  • ■ Guide the anchor through its axis in the jewels;
  • ■ Transfer of the energy of the armature to the balance and friction losses of the bearing of the spindle of the balance in a corresponding jewel.

Um den Wirkungsgrad der Hemmung zu verbessern, wurden viele Lösungen vorgeschlagen, bei der Anpassungen vorgenommen wurden um die energiesparendste Möglichkeit der Übertragung vom Hemmungsrad auf die Paletten des Ankers zu erreichen. So offenbaren die Dokumente CH-570644-A und CH-342897-A , das Dokument CH-342897 oder auch die WO-2007/003539 Lösungen, die auf die optimierte Geometrie der Palette Bezug nehmen.In order to improve the efficiency of the inhibition, many solutions have been proposed in which adjustments have been made to achieve the most energy efficient way of transferring the escape wheel to the pallets of the anchor. This is how the documents reveal CH-A-570644 and CH-342897-A , the document CH-342 897 or even the WO-2007/003539 Solutions that refer to the optimized geometry of the pallet.

Andere Dokumente, wie die DE-2050013-A und die CH-510285-A richten sich auf die Verbesserung der Übertragung der Energie vom Anker auf die Unruh.Other documents, like the DE-2050013-A and the CH-A-510 285 are aimed at improving the transfer of energy from the anchor to the balance.

Die Lagerung und Führung des Ankers beziehungsweise ihrer Achse in Lagersteinen (meist Rubinen) ist seit den ersten Uhren mit Ankerhemmungen wesentlich verbessert worden. Man hat natürliche Rubine und später synthetische Rubine als Werkstoff genommen, um die Reibung und den Verschleiss der Lagerzapfen der Achsen zu reduzieren. Man hat auch die Durchmesser der Lagerzapfen der Achse des Ankers reduziert und angepasst. Ebenfalls wurden Schmiermittel an den Lagerzapfen eingesetzt und die Schmiermittel wurden fortlaufend verbessert.The storage and leadership of the anchor or its axis in jewels (usually rubies) has been substantially improved since the first watches with anchor inhibitors. Natural rubies and later synthetic rubies have been used as a material to reduce friction and wear To reduce the journal of the axles. It has also reduced the diameter of the journals of the axis of the anchor and adapted. Also, lubricants were used on the journal and the lubricants were continually improved.

Die Schmiermittel haben jedoch den Nachteil, dass sie sich mit der Zeit verschlechtern, nämlich altern, oxidieren, cracken und ranzig werden. Ausserdem sind Schmiermittel empfänglich für die Aufnahme von Staub und neigen dazu zu verharzen. Schmiermittel werden deshalb kaum noch für Lagerzapfen des Ankers benutzt. Trotz allen Vorkehrungen sind Reibung und Spiel zwischen den Lagerzapfen der Ankerachse und ihren Lagersteinen bis heute vorhanden mit den wohlbekannten Nachteilen. Es ist somit die Aufgabe der vorliegenden Erfindung einen Anker zu schaffen, der sich praktisch spielfrei und reibungsfrei oszillierend bewegt wodurch der Wirkungsgrad der Hemmung verbessert werden soll.The lubricants, however, have the disadvantage of deteriorating over time, namely aging, oxidizing, cracking and rancidity. In addition, lubricants are susceptible to the absorption of dust and tend to harden. Lubricants are therefore hardly used for bearing journals of the anchor. Despite all precautions friction and play between the journals of the anchor axle and their jewels are still present with the well-known disadvantages. It is therefore the object of the present invention to provide an anchor that oscillates virtually free of play and friction-free movement whereby the efficiency of the inhibition is to be improved.

Diese Aufgabe löst ein Anker der eingangs genannten Art mit den Merkmalen des Patentanspruches 1. Die Erfindung zeigt ferner zwei Verfahren zur Herstellung des erfindungsgemässen Ankers gemäss den Ansprüchen 18 und 19 auf.This object is achieved by an anchor of the type mentioned above with the features of claim 1. The invention also shows two methods for producing the inventive anchor according to claims 18 and 19.

Weitere vorteilhafte Ausgestaltungsformen des Erfindungsgegenstandes gehen aus den abhängigen Patentansprüchen hervor und deren Bedeutung und Wirkungsweise sind in der nachfolgenden Beschreibung mit Bezug auf die anliegenden Zeichnungen erläutert. Es zeigt:

Figur 1:
Eine Aufsicht auf eine erste Ausführungsform des erfindungsgemässen Ankers und
Figur 2:
denselben Anker in einer perspektivischen Ansicht.
Figur 3:
zeigt eine zweite Ausführungsform des erfindungsgemässen Ankers in der Aufsicht, wobei die Schwenkbewegung des Ankers beziehungsweise dessen Gabel beschränkt ist und
Figur 4:
zeigt wiederum diese zweite Ausführungsform in einer perspektivischen Darstellung.
Figur 5:
zeigt abermals in einer Aufsicht eine dritte Ausführungsform des erfindungsgemässen Ankers der so gestaltet ist, dass er gewisse parasitäre Bewegungen zu kompensieren vermag, und auch hier ist in der
Figur 6:
dieser Anker in perspektivischer Lage gezeigt. Eine nochmals andere, vierte Ausführungsform zeigt die
Figur 7:
in der diese vierte Ausführungsform des erfindungsgemässen Ankers in der Aufsicht und
Figur 8:
in perspektivischer Darstellung gezeigt ist. Die
Figuren 9 - 11:
zeigen einen herkömmlichen Anker in der Seitenansicht in der Aufsicht und in perspektivischer Darstellung.
Further advantageous embodiments of the subject invention will become apparent from the dependent claims and their meaning and effect are explained in the following description with reference to the accompanying drawings. It shows:
FIG. 1:
A plan view of a first embodiment of the inventive anchor and
FIG. 2:
the same anchor in a perspective view.
FIG. 3:
shows a second embodiment of the inventive anchor in the plan view, wherein the pivoting movement of the armature or the fork is limited and
FIG. 4:
again shows this second embodiment in a perspective view.
FIG. 5:
shows again in a plan view a third embodiment of the inventive anchor which is designed so that it is able to compensate for certain parasitic movements, and here is in the
FIG. 6:
this anchor shown in perspective. Yet another, fourth embodiment shows the
FIG. 7:
in this fourth embodiment of the inventive anchor in the plan view and
FIG. 8:
is shown in perspective view. The
Figures 9-11:
show a conventional anchor in the side view in plan view and in perspective.

Vorerst wird mit Bezug auf die Figuren 9 - 11 ein herkömmlicher Anker beschrieben. Der Anker insgesamt ist mit A bezeichnet. Der Anker besitzt zwei Ankerarme B, in deren Enden jeweils eine Palette C gehalten ist. Mittig zwischen den beiden Ankerarmen in deren Verbindungsbereich greift eine Gabel D an, die praktisch senkrecht oder zumindest auf einer Winkelhalbierenden der beiden Ankerarme verläuft. Die Gabel D endet in Zinken E und die Schwenkbewegung des Ankers beziehungsweise der Gabel D wird durch zwei seitliche Ankerbegrenzungsstifte F in der Schwenkbewegung begrenzt. Diese Schwenkbewegung erfolgt um eine Lagerachse G mit beidseitigen Lagerzapfen H, die in hier nicht dargestellten Lagersteinen ruhen. Es ist selbstverständlich, dass diese Lagerzapfen H mit einer gewissen Reibung und damit mit Energieverlust in den Lagersteinen lagern und es ist ebenso klar, dass diese Lagerzapfen in den Lagersteinen nicht spielfrei lagern können. Wie eingangs erwähnt führt dies zu den entsprechenden Energieverlusten und einer Gangungenauigkeit.For now, with respect to the FIGS. 9-11 a conventional anchor described. The anchor as a whole is denoted by A. The anchor has two anchor arms B, in each of whose ends a pallet C is held. In the middle between the two armature arms in the connecting region engages a fork D, which extends virtually perpendicular or at least on an angle bisector of the two armature arms. The fork D ends in tines E and the pivotal movement of the armature or the fork D is limited by two lateral anchor boundary pins F in the pivoting movement. This pivoting movement takes place about a bearing axis G with bilateral bearing journals H, which rest in bearing stones, not shown here. It goes without saying that these journals H store with a certain friction and thus with loss of energy in the jewels and it is also clear that these journals can not be stored without clearance in the jewels. As mentioned above, this leads to the corresponding energy losses and a gear inaccuracy.

In allen nun folgenden Ausführungsformen des erfindungsgemässen Ankers fällt sogleich auf, dass dieser in keiner der hier dargestellten Ausführungsformen eine konkrete Lagerachse aufweist. Dies trifft auch entsprechend bei der ersten Ausführungsform gemäss den Figuren 1 und 2 zu. Der erfindungsgemässe Anker wird insgesamt immer mit 1 bezeichnet. Auch dieser Anker besitzt wie ein herkömmlicher Anker zwei Ankerarme 2. Endständig in den beiden Ankerarmen 2 sind die Paletten 3 gehalten. Diese beiden Ankerarme 2 sind einstückig miteinander verbunden und in dem Verbindungsbereich greift die Gabel 4 des Ankers an. Die Gabel 4 steht praktisch senkrecht auf den beiden Ankerarmen 2, wenn diese gestreckt fluchtend miteinander verbunden sind. Schliessen die beiden Ankerarme 2 einen vom Winkel 180° abweichenden Winkel ein, so liegt die Gabel 4 auf der Winkelhalbierenden des genannten Winkels. Endständig weist die Gabel 4 Gabelzinken 5 beziehungsweise das Gabelhorn auf. Dieser Teil entspricht wiederum der herkömmlichen Machart. Der Bereich, in dem die Gabel 4 mit den beiden Ankerarmen 2 verbunden ist, wird hier als Verbindungsbereich 6 definiert. In diesem Verbindungsbereich 6 greifen zwei Befestigungsarme 7 an. Diese Befestigungsarme 7 verlaufen in der hier dargestellten einfachsten Ausführungsform exakt gerade. Bezüglich der Mittelachse durch die Gabel 4 verlaufen die beiden Befestigungsarme 7 spiegelsymmetrisch. Folglich bildet so die Gabel 4 beziehungsweise deren Mittelachse die Winkelhalbierende bezüglich den Winkel, den die beiden Befestigungsarme 7 miteinander einschliessen.In all of the following embodiments of the inventive armature is immediately apparent that this has in any of the embodiments shown here a concrete bearing axis. This also applies correspondingly in the first embodiment according to the Figures 1 and 2 to. Overall, the anchor according to the invention is always designated 1. Also, this anchor has like two anchor arms 2 like a conventional anchor. The pallets 3 are held at the end in the two anchor arms 2. These two armature arms 2 are integrally connected to each other and in the connection area, the fork 4 engages the armature. The fork 4 is practically perpendicular to the two armature arms 2, when they are stretched aligned with each other. If the two anchor arms 2 enclose an angle deviating from the angle 180 °, the fork 4 lies on the bisector of said angle. Terminally, the fork 4 forks 5 and the fork horn on. This part again corresponds to the conventional style. The region in which the fork 4 is connected to the two armature arms 2 is defined here as the connection region 6. In this connection region 6, two fastening arms 7 engage. These attachment arms 7 extend exactly straight in the simplest embodiment shown here. With respect to the central axis through the fork 4, the two attachment arms 7 extend mirror-symmetrically. Consequently, so forms the fork 4 and the center axis of the Angle bisector with respect to the angle, the two mounting arms 7 include each other.

Endständig an den beiden Befestigungsarmen 7 sind Befestigungselemente 8, die in der hier bevorzugten Ausführungsform als ringförmige Ösen ausgestaltet sind. Entsprechend wird nachfolgend auch von Befestigungsösen 8 gesprochen, wobei der Fachmann selbstverständlich auch andere Befestigungselementformen darunter verstehen wird. Die Wahl der Befestigungselemente als Befestigungsösen wird daher bevorzugt, da diese sowohl geeignet sind um mittels Schrauben mit einem entsprechenden feststehenden Teil des Uhrwerkes, beispielsweise der Uhrwerksplatine, verbunden zu werden. Die Befestigungsösen 8 sind aber ebenso geeignet für eine Löt-oder Schweissverbindung wie auch für eine Klebeverbindung. Für die letztgenannten Verbindungsarten wären aber einfache scheibenförmige Ausgestaltungen der Befestigungselemente genau so geeignet.Terminal at the two mounting arms 7 are fasteners 8, which are configured in the preferred embodiment here as an annular eyelets. Accordingly, the following is also spoken of eyelets 8, the expert will understand, of course, other fastener forms underneath. The choice of fasteners as eyelets is therefore preferred because they are both suitable to be connected by means of screws with a corresponding fixed part of the movement, for example, the movement board. But the eyelets 8 are also suitable for a soldered or welded connection as well as for an adhesive connection. For the latter types of connection but simple disc-shaped embodiments of the fasteners would be just as suitable.

Auch beim erfindungsgemässen Anker erfolgt die Krafteinleitung wie bei einem herkömmlichen Anker vom Hemmungsrad über die Paletten, die auch oft Ausgangspaletten genannt werden. Der gesamte Anker 1 besteht meist mit Ausnahme der beiden Ausgangspalletten einstückig aus einem plattenförmigen Material. Es wird bevorzugterweise ein Material mit hohem E-Modul gewählt. Die vom Hemmungsrad auf die Paletten 3 ausgeübte Kraft führt zu einer Biegeverformung der Befestigungsarme 7. Dabei ist die Breite b der Befestigungsarme möglichst klein gehalten. Die Höhe h der Befestigungsarme 7 ist ein mehrfaches der Breite b dieser Arme. Bezüglich der Biegefestigkeit der Befestigungsarme ergibt sich folgende Formel: K = 3 E 1 / I 3

Figure imgb0001
Hierbei gilt, dass I = b × h 3 / 12.
Figure imgb0002
In dieser Formel gilt:

E =
E-Modul des Materials
b =
Breite des Befestigungsarmes
h =
Höhe des Befestigungsarmes
l =
Länge des Befestigungsarmes
I =
Flächenträgheitsmoment des Balkens
K =
Die Gesteifigkeit des Balkens.
Also in the inventive anchor, the force is introduced as in a conventional anchor from the escape wheel on the pallets, which are also often called exit pallets. The entire armature 1 is usually in one piece with the exception of the two output pallets of a plate-shaped material. It is preferable to choose a high modulus material. The force exerted by the escape wheel on the pallets 3 leads to a bending deformation the mounting arms 7. The width b of the mounting arms is kept as small as possible. The height h of the attachment arms 7 is a multiple of the width b of these arms. With regard to the flexural strength of the attachment arms, the following formula results: K = 3 e 1 / I 3
Figure imgb0001
It is true that I = b × H 3 / 12th
Figure imgb0002
In this formula:
E =
Modulus of elasticity of the material
b =
Width of the attachment arm
h =
Height of the attachment arm
l =
Length of the attachment arm
I =
Area moment of inertia of the beam
K =
The stiffness of the beam.

Aus dieser Formel ersieht man, dass eine möglichst leichtgängige Ausgestaltung des erfindungsgemässen Ankers dadurch erreicht wird, dass man die Befestigungsarme möglichst lang und in der Breite möglichst dünn gestalten sollte. Bezüglich der Höhe des Befestigungsarmes ist man selbstverständlich nicht frei, da diese genügend gross sein muss um dadurch nicht Dreh-Freiheitsgrade zu erhalten, die nicht in der Ebene des Ankers liegen. Würde man die Höhe des Befestigungsarmes ebenfalls sehr klein wählen, so würden die Befestigungsarme sich gleich Fäden verhalten und wären lediglich auf Zug und Druck steif aber ansonsten in alle Biegerichtungen sehr flexibel. Dies ist aber nicht erwünscht, sondern die Bewegungsfreiheit soll begrenzt sein auf eine Biegebewegung der Befestigungsarme 7 innerhalb der Erstreckungsebene in der der Anker liegt.From this formula it can be seen that the smoothest possible embodiment of the inventive anchor is achieved by making the attachment arms as long as possible and as thin as possible in width. With regard to the height of the attachment arm is of course not free, since this must be sufficiently large so as not to obtain rotational degrees of freedom that are not in the plane of the anchor. If you would also choose the height of the mounting arm also very small, so the mounting arms would behave like threads and would be stiff only on train and pressure but otherwise very flexible in all bending directions. But this is not wanted but the freedom of movement should be limited to a bending movement of the mounting arms 7 within the extension plane in which the anchor is located.

Die bisher beschriebene einfachste Ausführungsform des erfindungsgemässen Ankers mit zwei flexiblen Befestigungsarmen 7 besitzt jedoch noch immer einen relativen Nachteil. Dieser Anker weist eine so genannte parasitäre Bewegung auf. Hierunter wird die unerwünschte, wenn auch kleine, Fehlbewegung des Rotationszentrums, also der virtuellen Achse bezeichnet. Die dritte Ausführungsform des Erfindungsgegenstandes, wie sie in den Figuren 5 und 6 dargestellt ist, löst auch dieses Problem. Idealerweise sollte sich der Anker ohne eine Offsetbewegung des Zentrums um eine vorgegebene, virtuelle Achse drehen. Diese Problematik lässt sich beispielsweise dadurch weitgehend reduzieren, dass man die Befestigungsarme 7, wie in den Figuren 5 und 6 dargestellt, gestaltet. Hier sind die Befestigungsarme 7 mit zwei parallelen, elastischen Teilstrecken 70 und 71 gestaltet. Diese beiden Teilstrecken 70 und 71 verlaufen haarnadelartig. Die beiden Teilstrecken sind parallel und gegenläufig angeordnet. Die beiden elastischen Teilstrecken70, 71 sind über eine verdickte Verbindungsstelle 72 miteinander verbunden. Die erste elastische Teilstrecke 70 verläuft somit zwischen der verdickten Verbindungsstelle 72 und dem Verbindungsbereich 6 des Ankers 1 beziehungsweise zu einem verdickten Teil der Befestigungsarme 7 der hier als Verbindungsteil 73 bezeichnet ist. Die zweite elastische Teilstrecke 71 verläuft von der verdickten Verbindungsstelle 72 zu einem verdickten Befestigungsarmteil 74, an dem endständig das Befestigungselement beziehungsweise die Befestigungsöse 8 angeformt ist.However, the simplest embodiment of the inventive anchor described so far with two flexible mounting arms 7 still has a relative disadvantage. This anchor has a so-called parasitic motion. This is the unwanted, albeit small, erroneous movement of the rotation center, so called the virtual axis. The third embodiment of the subject invention, as shown in the FIGS. 5 and 6 is shown, also solves this problem. Ideally, the armature should rotate about a given virtual axis without offset movement of the center. This problem can be largely reduced, for example, by allowing the mounting arms 7, as in the FIGS. 5 and 6 represented, designed. Here, the fastening arms 7 are designed with two parallel elastic sections 70 and 71. These two sections 70 and 71 are hairpin-like. The two sections are parallel and arranged in opposite directions. The two elastic partial sections 70, 71 are connected to one another via a thickened connection point 72. The first elastic section 70 thus extends between the thickened connection point 72 and the connection region 6 of the armature 1 or to a thickened part of the Mounting arms 7 which is referred to here as the connecting part 73. The second elastic section 71 extends from the thickened connection point 72 to a thickened fastening arm part 74, on which the fastening element or fastening eye 8 is formed at the end.

Die bei der erst beschriebenen Ausführungsform gemäss den Figuren 1 und 2 aufgezeigt Lösung ergibt wie erwähnt eine leichte Verschiebung des Zentrums der virtuellen Drehachse. Diese Verschiebung wird durch die Deformationsbewegung der Befestigungsarme 7 ausgelöst. Die Befestigungsarme verkürzen ihre Länge etwas, wenn sie durchgebogen werden. Die Stärke dieser Verschiebung hängt sowohl von der Länge der Befestigungsarme 7 als auch von der angulären Position, der Auslenkung, des Ankers ab. Diese parasitäre Bewegung wird nun weitgehend kompensiert durch die hier aufgezeigt dritte Ausführungsform des Erfindungsgegenstandes gemäss den Figuren 5 und 6. Ein weiterer Vorteil dieser Ausgestaltungsform besteht darin, dass durch die beiden elastischen Teilstrecken 70 und 71 praktisch bei gleichem Platzbedarf die doppelte Länge des beweglichen Teils der Befestigungsarme 7 erreicht wird. Folglich führt diese Lösung nicht nur zu einer Kompensation der parasitären Bewegungen, sondern reduziert gleichzeitig auch die Steifigkeit der Befestigungsarme so dass die erforderliche Energie für die Verformung geringer ist.The in the first described embodiment according to the Figures 1 and 2 As mentioned, the solution results in a slight shift of the center of the virtual axis of rotation. This shift is triggered by the deformation movement of the attachment arms 7. The attachment arms shorten their length somewhat when they are bent. The strength of this displacement depends both on the length of the attachment arms 7 and on the angular position, the deflection, of the armature. This parasitic movement is now largely compensated by the third embodiment of the subject invention according to FIGS FIGS. 5 and 6 , A further advantage of this embodiment is that twice the length of the movable part of the fastening arms 7 is achieved by the two elastic partial sections 70 and 71 practically with the same space requirement. Consequently, this solution not only compensates for the parasitic movements, but also reduces the stiffness of the attachment arms, so that the energy required for deformation is less.

Es sind auch andere Ausgestaltungsformen zur Reduktion der parasitären Bewegungen bekannt, die sich ebenfalls eignen würden. Hierzu wird beispielsweise auf die Lösung gemäss der EP-1013949 Abbildung 4 verwiesen. Andere Vorschläge gehen auch aus der Publikation von W.H. Wittrick "The properties of crosslecture pivots and the influence of the point at which strips cross" (The aeronautique, Jahrgang 1951 ). Normalerweise und insbesondere bei herkömmlichen Anker wird deren Bewegung mittels Ankerbegrenzungsstiften begrenzt. In einer zweiten bevorzugten Ausführungsform, wie sie in den Figuren 3 und 4 dargestellt ist, sind nun die Befestigungselemente 8 derart gestaltet, dass diese selbst Anschläge bilden, welche die oszilierende Drehbewegung der Gabel begrenzen. Hierzu weisen die Befestigungsösen 8 Bewegungsbegrenzungsanschläge 9 auf, die in der Form von Ausbuchtungen in Richtung zur Gabel 4 hin gestaltet sind. Auch hier sind wiederum diese Befestigungsbegrenzungsanschläge 9 einstückig monolytisch als Teil der Befestigungselemente beziehungsweise Befestigungsösen 8 gestaltet. Damit erübrigt es sich im Uhrwerk selber Ankerbegrenzungsstifte vorzusehen.There are also other embodiments for the reduction of parasitic movements known, which would also be suitable. For this purpose, for example, the solution according to the EP-1013949 Figure 4 directed. Other suggestions also go from the publication by WH Wittrick "The properties of crosslecture pivots and the influence of crosses" (The aeronautique, born 1951 ). Normally, and in particular with conventional armatures, their movement is limited by means of anchor-limiting pins. In a second preferred embodiment, as shown in the FIGS. 3 and 4 is shown, the fastening elements 8 are now designed such that they themselves form stops which limit the oszilierende rotational movement of the fork. For this purpose, the attachment lugs 8 movement limiting stops 9, which are designed in the form of bulges in the direction of the fork 4 out. Again, these attachment limit stops 9 are monolithically designed as part of the fasteners or eyelets 8 in turn. Thus, it is unnecessary in the clockwork itself provide anchor limit pins.

Letztlich sei auch noch auf die 4. Ausführungsform wie sie in den Figuren 7 und 8 dargestellt ist verwiesen. Die bisher beschriebenen Ausführungsformen weisen auch in der Bewegungsrichtung noch eine kleine Reststeifigkeit auf.Finally, let me also to the 4th embodiment as in the FIGS. 7 and 8 is shown referenced. The embodiments described so far also have a small residual rigidity in the direction of movement.

Obwohl ein Teil des Impulses den der Anker an die Unruh abgibt auch von dieser wiederum zurückerstattet wird, wird ein Teil der Arbeit für die Bewegung des Ankers selber sowie für die elastische Deformationsarbeit seiner Befestigungsarme aufgewendet. Diese Arbeit ist deutlich niedriger als die Engerie die vom Hemmungsrad geliefert wird. Um nun die Federsteifigkeit des Ankers zu reduzieren, wird bei dieser Ausführungsform vorgeschlagen, am Anker wieder monolytisch einstückig ein zugelastisches Federelement 10 anzuformen. Am freien Ende des zugelastischen Federelementes 10 ist eine Befestigungsplatte 11 angebracht. Die Befestigungsplatte 11 besitzt ein Langloch 12. Durch dieses Langloch 12 kann die Befestigungsplatte 11 justierbar mittels einer Schraube auf die Platine des Uhrwerkes geschraubt sein. Hierdurch lässt sich die Vorspannung des zugelastischen Federelementes 10 einstellen. Das zugelastische Federelement 10 liegt in derselben Ebene wie auch die Befestigungsarme 7 und die übrigen Teile des erfindungsgemässen Ankers 1.
Selbstverständlich müssen die Befestigungsarme 7 mit ihren Befestigungselement 8 entweder auf derselben Platine des Uhrwerkes befestigt sein oder zumindest auf einen anderen fixen Teil des Uhrwerkes, das in derselben Ebene liegt. Auch das zugelastische Federelement 10 weist eine wesentlich geringere Breite b auf im Verhältnis zu Höhe h. Das zugelastische Federelement 10 kann im Prinzip eine beliebige Form besitzen, die von einer Geraden abweicht. So könnte das zugelastische Federelement 10 als einfacher, bogenförmig gewölbter Arm gestaltet sein oder wie hier dargestellt, als in der Ebene mäanderförmig verlaufende Strecke.
Although part of the momentum given by the armature to the balance is reimbursed by it, part of the work is spent on the movement of the armature itself and on the elastic deformation work of its attachment arms. This work is significantly lower than the energy delivered by the escapement wheel. In order to reduce the spring stiffness of the armature, it is proposed in this embodiment, again monolithically integrally form a zugelastisches spring element 10 at anchor again. At the free end of the elastic spring element 10, a mounting plate 11 is attached. Through this slot 12, the mounting plate 11 can be adjustably screwed by means of a screw on the board of the clockwork. As a result, the bias of the zugelastischen spring element 10 can be adjusted. The elastic spring element 10 lies in the same plane as the fastening arms 7 and the remaining parts of the armature 1 according to the invention.
Of course, the fastening arms 7 must be fastened with their fastening element 8 either on the same board of the movement or at least on another fixed part of the movement, which lies in the same plane. Also, the zugelastische spring element 10 has a much smaller width b in relation to height h. The zugelastische spring element 10 may in principle have any shape that deviates from a straight line. Thus, the zugelastische spring element 10 could be as simple, arcuate arched arm be designed or as shown here, as in the plane meandering route.

Während bei den zuvor beschriebenen Ausführungsformen die beiden Befestigungsarme 7 spiegelsymmetrisch bezüglich der mittigen Längsachse der Gabel 4 verlaufend angeordnet sind, ist hier eine davon abweichende Lösung gezeigt. Die elastischen Befestigungsarme 7 sind wiederum als gestreckte Elemente zwischen dem Verbindungsbereich 6 und den endständigen Befestigungselementen 8, die hier wiederum als Befestigungsösen ausgestaltet sind, verlaufend. Diese beiden Befestigungsarme 7 sind nun beide auf derselben Seite der Gabel 4 zwischen diesen und einem Ankerarm 2 angeordnet. Das zugelastische Federelement 10 ist nun so gelegt, dass die Verbindungslinie zwischen dem Zentrum des Langloches 12 und der Anbindungsstelle des zugelastischen Federelementes 10 am Verbindungsbereich 6 die Winkelhalbierende zwischen den beiden Befestigungsarmen 7 darstellt. Die virtuelle Drehachse liegt immer auf dem Schnittpunkt der Verlängerungen der beiden Befestigungsarme 7. Während bei den zuvor beschriebenen Beispielen bei, denen die Befestigungsarme 7 spiegelsymmetrisch bezüglich der Gabel 4 angeordnet sind, diese virtuelle Drehachse auch ausserhalb des Verbindungsbereiches 6 liegen kann, ist es bei der Ausführungsform gemäss den Figuren 7 und 8 bevorzugterweise so, dass die virtuelle Drehachse im Zentrum des Verbindungsbereiches 6 liegt. Mit anderen Worten der Ort der virtuellen Drehachse kann somit durch die Wahl der Anordnung der Befestigungsarme 7 praktisch frei bestimmt werden.While in the embodiments described above, the two fastening arms 7 are arranged mirror-symmetrically with respect to the central longitudinal axis of the fork 4, a different solution is shown here. The elastic attachment arms 7 are in turn as elongated elements between the connecting portion 6 and the terminal fasteners 8, which in turn are configured here as eyelets, extending. These two fastening arms 7 are now both arranged on the same side of the fork 4 between these and an armature arm 2. The zugelastische spring element 10 is now placed so that the connecting line between the center of the elongated hole 12 and the point of attachment of the zugelastischen spring element 10 at the connecting portion 6, the bisecting line between the two mounting arms 7. The virtual axis of rotation is always at the intersection of the extensions of the two mounting arms 7. While in the examples described above, where the mounting arms 7 are arranged mirror-symmetrically with respect to the fork 4, this virtual axis of rotation can also lie outside the connection area 6, it is in the Embodiment according to the FIGS. 7 and 8 preferably such that the virtual axis of rotation lies in the center of the connecting region 6. In other words, the place of virtual axis of rotation can thus be determined virtually free by the choice of the arrangement of the mounting arms 7.

Dank der Verwendung eines zugelastischen Federelementes 10, wie zuvor beschrieben, wird nunmehr auf die Befestigungsarme 7 eine Vorspannkraft ausgeübt. Dank dieser Vorspannkraft lässt sich die angulare Steifigkeit des Ankers 1 verändern beziehungsweise dank dem Langloch 12 einstellen. Diese Vorspannung lässt sich soweit erhöhen, dass im Prinzip der Anker in eine instabilen Lage gelangt. Der Anker wird dann im so genannten bistabilen bucklingmode betrieben. Mit anderen Worten bei geringer Krafteinwirkung springt der Anker um die virtuelle Drehachse schwenkend von der einen Endlage in die andere Endlage.Thanks to the use of an elastic spring element 10, as described above, a preload force is now exerted on the attachment arms 7. Thanks to this biasing force, the angular stiffness of the armature 1 can be changed or set thanks to the slot 12. This bias can be increased so far that, in principle, the anchor gets into an unstable position. The anchor is then operated in the so-called bistable buckling mode. In other words, with little force, the armature jumps about the virtual axis of rotation pivoting from one end position to the other end position.

In der Figur 7 ist im Gegensatz zur Figur 8 auch noch die Möglichkeit aufgezeigt, dass man die Paletten 3 ebenfalls einstückig monolytisch und somit aus demselben Material wie der Anker 1 in einem Arbeitsgang herstellt. Da man zur Fertigung des erfindungsgemässen Ankers erfindungsgemäss und bevorzugterweise ein Herstellungsverfahren wählt, bei dem die Begrenzungskanten des Ankers ausserordentlich regelmässig mit einer sehr geringen Rauhigkeit zu fertigen sind, werden so auch Reibungsverluste reduziert. Für die Fertigung kommen insbesondere zwei Verfahren in Frage. Das eine Verfahren wird als DRIE-Verfahren bezeichnet. Hierbei steht DRIE für Deep Reactive Ion Etching. Dieses Verfahren wurde von der Firma Bosch entwickelt und diesbezüglich wird beispielsweise auf die Dokumente DE-3927163 oder DE-4420962-A verwiesen. Mittels diesem Verfahren lassen sich Befestigungsarme 7 mit einer sehr kleinen Breite herstellen. Typischerweise werden die Befestigungsarme 7 mit einer Breite von 15 - 50 Mikrometern hergestellt. Die Geometrie eines so hergestellten erfindungsgemässen Ankers, weist eine extreme Genauigkeit auf, mit Abweichungen die üblicherweise unter ein Mikrometer liegen.In the FIG. 7 is contrary to FIG. 8 also shown the possibility that the pallets 3 also monolithic one piece and thus made of the same material as the anchor 1 in one operation. Since one chooses according to the invention and preferably a manufacturing method for the production of the inventive anchor, in which the boundary edges of the armature are extremely regularly finished with a very low roughness, friction losses are thus reduced. In particular, two methods are suitable for the production. One method is called a DRIE method. DRIE stands for Deep Reactive Ion Etching. This procedure was by the company Bosch develops and in this regard, for example, on the documents DE-3927163 or DE-4420962-A directed. By means of this method, fastening arms 7 can be produced with a very small width. Typically, the attachment arms 7 are made with a width of 15-50 microns. The geometry of an inventive anchor produced in this way has an extreme accuracy, with deviations that are usually less than one micrometer.

Als Herstellungsmaterial für dieses Verfahren kommt unter anderem Silizium in Form von Wafern in Frage. Dieses Material eignet sich besonders gut für die Herstellung des Ankers. In der Tat besitzt dieses Material ideale Eigenschaften für diese Anwendung. Es besitzt eine hohe mechanische Festigkeit und eine sehr geringe plastische Verformbarkeit, so dass die Bereiche mit grosser Dicke in Belastungsrichtung praktisch keine Verformung aufweisen. Dies führt zu äusserst geringen Verlusten. Eine Materialermüdung tritt praktisch nicht auf so lang die angelegten Spannungen bei den Wechselbelastungen unterhalb der elastischen Bruchgrenze gehalten sind. Schliesslich weist Silizium einen sehr kleinen Reibungskoeffizienten auf. Problematisch kann lediglich sein, dass die durch das DRIE-Verfahren geätzte Teile sehr scharfe Kanten aufweisen. Für den Uhrmacher, der mit der Pinzette arbeitet, können somit an den scharfen Kanten lokal sehr hohe Drucke entstehen. Dies kann zur Zerstörung des Ankers führen.Among other things, silicon in the form of wafers may be considered as the material of manufacture for this process. This material is particularly suitable for the production of the anchor. In fact, this material has ideal properties for this application. It has a high mechanical strength and a very low plastic deformability, so that the areas with large thickness in the loading direction have virtually no deformation. This leads to extremely low losses. Material fatigue practically does not occur as long as the applied stresses at the alternating stresses are kept below the elastic breaking point. Finally, silicon has a very low coefficient of friction. The only problem is that the parts etched by the DRIE method have very sharp edges. For the watchmaker who works with the tweezers, it is thus possible for the watchmaker to produce very high pressures locally on the sharp edges. This can lead to the destruction of the anchor.

Um diesem Nachteil abzuhelfen, kann man die Oberfläche des Werkstückes verändern in dem man die Oberfläche entweder oxidiert oder nitriert. Hierbei lagert sich um die Kanten Material an oder wird Material abgetragen, so dass die Kanten gewisse Rundungen erfahren. Das Siliziumoxyd und das Siliziumnitrid haben zudem tribologische Vorteile in dem wiederum der Reibungskoeffizient positiv beeinflusst wird.To remedy this disadvantage, one can change the surface of the workpiece by either oxidizing or nitriding the surface. Here, material is deposited around the edges or material is removed, so that the edges undergo certain curves. The silicon oxide and the silicon nitride also have tribological advantages in which in turn the coefficient of friction is positively influenced.

Es ist ferner auch möglich auf der Siliziumoberfläche eine harte Schicht aufzubringen in dem man hierauf einen synthetischen Diamant oder Saphir wachsen lässt. Auch dies sind bekannte Beschichtungsverfahren.It is also possible to apply a hard layer to the silicon surface by growing a synthetic diamond or sapphire thereon. These are also known coating methods.

Auch wenn Silizium das bevorzugte Material für den Anker ist, so kann dieser auch aus Quarz, Pyrexglas, Saphir oder Diamant hergestellt werden. All diese Materialien lassen sich synthetisch herstellen, sind entsprechend hart und abreibfest. Zudem lassen sich diese Materialien mindestens teilweise durch das DRIE-Verfahren bearbeiten. Ein weiteres bevorzugtes Herstellungsverfahren ist aus der so genannten LIGA-Technologie bekannt. Bezüglich dem LIGA-Verfahren wird beispielsweise auf die Europäischen Patentschriften EP-0183910A oder die EP-1431844-A sowie auf das US-Patent 6458263-B verwiesen. Für das LIGA-Verfahren werden insbesondere Nickel oder Nickelphosphorverbindungen verwendet. Auch mittels diesem Verfahren lässt sich ein erfindungsgemässer Anker mit den erforderlichen Dimensionen und Genauigkeit fertigen, der die gewünschten physikalischen Eigenschaften aufweist. Das LIGA-Verfahren ist ein lithographisch-galvanisches Aetzverfahren.Although silicon is the preferred material for the anchor, it can also be made of quartz, pyrex glass, sapphire or diamond. All these materials can be produced synthetically, are accordingly hard and abrasion resistant. In addition, these materials can be at least partially processed by the DRIE method. Another preferred manufacturing method is known from the so-called LIGA technology. With regard to the LIGA process, reference is made, for example, to the European patents EP-0183910A or the EP-1431844-A as well as on the U.S. Patent 6458263-B directed. In particular, nickel or nickel phosphorus compounds are used for the LIGA process. Also by means of this method can be an inventive anchor with the required dimensions and manufacture accuracy having the desired physical properties. The LIGA process is a lithographic-galvanic etching process.

Neben den beiden hier beschriebenen bevorzugten Herstellungsverfahren kommen selbstverständlich auch weitere geeignete Verfahren in Frage mit den jeweils dazu passenden Materialien. Lediglich der Vollständigkeit halber seien hier als Beispiel noch die Möglichkeit der Draht-Elektro-Erosion erwähnt, wobei dann der Anker aus einem entsprechenden Stahl geformt wird oder die Herstellung von metallischen Gläsern mit dem so genannten Mikrostrukturierungs-Verfahren (Mikro moulding) erwähnt.In addition to the two preferred production methods described here, of course, other suitable methods come into question with the respectively suitable materials. Merely for the sake of completeness, the possibility of wire-electric erosion may be mentioned here as an example, in which case the armature is formed from a corresponding steel or the production of metallic glasses is mentioned by the so-called micro-structuring method (micro-molding).

Bezugszeichenliste:LIST OF REFERENCE NUMBERS

AA
herkömmlicher Ankerconventional anchor
BB
Ankerarmeanchor arms
CC
Palettenpallets
DD
Gabelfork
Ee
Zinkenprong
FF
AnkerbegrenzungsstifteAnchor limit pins
GG
Lagerachsebearing axle
HH
Lagerzapfenpivot
11
erfindungsgemässer Ankeranchor according to the invention
22
Ankerarmeanchor arms
33
Palettepalette
44
Gabelfork
55
Gabelzinkenforks
66
Verbindungsbereichconnecting area
77
Befestigungsarmemounting arms
88th
Befestigungselement, BefestigungsösenFastener, eyelets
99
BewegungsbegrenzungsanschlägeMotion limiting stops
1010
zugelastisches Federelementelastic spring element
1111
Befestigungsplattemounting plate
1212
LanglochLong hole
7070
erste elastische Teilstreckenfirst elastic sections
7171
zweite elastische Teilstreckensecond elastic sections
7272
verdichtete Verbindungsstellecompacted junction
7373
Verbindungsteilconnecting part
7474
Befestigungsarmteilbracket portion

Claims (20)

Anker (1) für eine Uhrenhemmung einer mechanischen Uhr mit Hemmungsrad, umfassend zwei Ankerarme (2) in der je eine Palette (3) gehalten ist und einer Gabel (4) an der endseitig ein Gabelhorn vorhanden ist welches auf die Unruh wirkt, dadurch gekennzeichnet, dass die die Ausgangspaletten tragenden Ankerarme (2) und die Gabel (4) zusammen mit zwei Befestigungsarmen (7) einstückig gefertigt sind, wobei die Befestigungsarme (7), die in derselben Ebene verlaufen wie die übrigen Ankerteile, mindestens mit einer Teilstrecke so biegeelastisch gestaltet sind, dass der Anker in der Ebene um eine virtuelle Achse unter Einwirkung der vom Hemmungsrad auf sie übertragene Energie zu schwingen vermag, wobei die Mittelachsen der beiden Befestigungsarme (7) sich in der virtuellen Achse schneiden.Anchor (1) for a clock escapement of a mechanical watch with escapement wheel, comprising two armature arms (2) in each of which a pallet (3) is held and a fork (4) at the end a fork horn is present which acts on the balance, characterized in that the armature arms (2) and the fork (4) carrying the output pallets are made in one piece together with two fastening arms (7), the fastening arms (7) extending in the same plane as the other armature parts having at least one partial stretch so that they are elastically flexible are designed such that the anchor in the plane about a virtual axis under the action of the escape wheel on the energy transmitted to them can vibrate, the central axes of the two attachment arms (7) intersect in the virtual axis. Anker nach Anspruch 1, dadurch gekennzeichnet, dass die virtuelle Achse im Verbindungsbereich (6) von Ankerarmen (2) und Ankergabel (4) liegt.Anchor according to claim 1, characterized in that the virtual axis in the connecting region (6) of anchor arms (2) and anchoring fork (4). Anker nach Anspruch 1, dadurch gekennzeichnet, dass die virtuelle Achse ausserhalb des Ankers (1) liegt.Anchor according to claim 1, characterized in that the virtual axis is outside the armature (1). Anker nach Anspruch 1, dadurch gekennzeichnet, dass die beiden Befestigungsarme (7) symmetrisch zur Ankergabel (4) angeordnet sind, so dass die Ankergabel auf den Winkelhalbierenden des von den beiden Befestigungsarmen (7) beziehungsweise deren beiden elastischen Teilstrecken eingeschlossenen Winkels liegt.Anchor according to claim 1, characterized in that the two fastening arms (7) are arranged symmetrically to the anchor fork (4), so that the anchor fork is located on the bisector of the enclosed by the two mounting arms (7) or their two elastic sections angle. Anker nach Anspruch 1, dadurch gekennzeichnet, dass an den freien Enden der beiden Befestigungsarme (7) Befestigungselement (8) angeformt sind.Anchor according to claim 1, characterized in that at the free ends of the two fastening arms (7) fastening element (8) are integrally formed. Anker nach Anspruch 5, dadurch gekennzeichnet, dass sich die beiden Befestigungsarme (7) von den Befestigungselement (8) bis zu dem Bereich der Verbindung (6) von Ankergabel (4) und Ankerarmen (2) sich erstrecken und auf der gesamten Länge elastisch gestaltet sind.Anchor according to claim 5, characterized in that the two attachment arms (7) extend from the attachment element (8) to the region of the connection (6) of the anchor fork (4) and anchor arms (2) and are elastic over the entire length are. Anker nach Anspruch 5, dadurch gekennzeichnet, dass die Befestigungselementen (8) so angeordnet sind, dass deren periphere Bewegungsbegrenzungsanschläge bilden, die eine maximale Auslenkung der Ankergabel definieren.Anchor according to claim 5, characterized in that the fastening elements (8) are arranged so that form their peripheral movement limit stops which define a maximum deflection of the armature fork. Anker nach Anspruch 5, dadurch gekennzeichnet, dass die Befestigungselement (8) eine Form aufweisen mit zu der Ankergabel hin gerichteten Ausformungen, die Bewegungsbegrenzungsanschläge (9) bilden, die eine maximale Auslenkung der Ankergabel (4) definieren.Anchor according to claim 5, characterized in that the fastening elements (8) have a shape with the anchor fork directed toward formations that form Bewegungsbegrenzungsanschläge (9), which define a maximum deflection of the anchor fork (4). Anker nach Anspruch 1, dadurch gekennzeichnet, dass beide Befestigungsarme (7) auf derselben Seite zwischen der Ankergabel und einem Ankerarm (2) liegen.Anchor according to claim 1, characterized in that both fastening arms (7) lie on the same side between the anchor fork and an anchor arm (2). Anker nach Anspruch 9, dadurch gekennzeichnet, dass auf der Winkelhalbierenden zwischen den beiden Befestigungsarmen (7) ein zugelastisches Federelement (10) einstückig angeformt ist, welches mit einer Befestigungsplatte (11) zur Befestigung versehen ist, um die Drehsteifigkeit des Ankers (1) zu vermindern.Anchor according to claim 9, characterized in that on the bisector between the two mounting arms (7) a zugelastisches spring element (10) is integrally formed, which is provided with a mounting plate (11) for attachment to the torsional stiffness of the armature (1) Reduce. Anker nach Anspruch 10, dadurch gekennzeichnet, dass die Befestigungsplatte (11) ein Langloch (12) aufweist, zur Befestigung des Federelementes (10) mit einstellbarer Vorspannung um die Drehsteifigkeit des Ankers (1) zu justieren.Anchor according to claim 10, characterized in that the mounting plate (11) has a slot (12) for fixing the spring element (10) with adjustable bias to adjust the torsional stiffness of the armature (1). Anker nach Anspruch 1, dadurch gekennzeichnet, dass die Befestigungsarme (7) je zwei elastische Teilstrecken (70, 71) aufweisen, die parallel gegenläufig angeordnet sind.Anchor according to claim 1, characterized in that the fastening arms (7) each have two elastic partial sections (70, 71) which are arranged parallel in opposite directions. Anker nach Anspruch 12, dadurch gekennzeichnet, dass die beiden Teilstrecken (70, 71) haarnadelartig gestaltet sind und über einer verdickten Verbindungsstelle (72) die beiden Teilstrecken (70, 71) miteinander verbunden sind.Anchor according to claim 12, characterized in that the two partial sections (70, 71) are designed hairpin-like and over a thickened connection point (72), the two partial sections (70, 71) are interconnected. Anker nach Anspruch 1, dadurch gekennzeichnet, dass die Befestigungsarme (7) an einem unbeweglichen Teil des Uhrwerkes befestigt sind.Anchor according to claim 1, characterized in that the fastening arms (7) are fixed to an immovable part of the movement. Anker nach den Ansprüchen 5 und 14, dadurch gekennzeichnet, dass die Befestigungselemente (8) mittels Schrauben am Uhrwerk befestigt sind.Anchor according to claims 5 and 14, characterized in that the fastening elements (8) are fastened by means of screws on the movement. Anker nach den Ansprüchen 5 und 14, dadurch gekennzeichnet, dass die Befestigungselemente (8) unlösbar mittels Schweissen, Löten oder Kleben am Uhrwerk befestigt sind.Anchor according to claims 5 and 14, characterized in that the fastening elements (8) are permanently attached by welding, soldering or gluing the movement. Anker nach Anspruch 12, dadurch gekennzeichnet, dass dieser monolithisch aus sprödem Material gefertigt ist, insbesondere aus der Auswahl von - synthetischem Edelstein, insbesondere Diamant - synthetischem Halbedelstein - Silizium oder Siliziumverbindung Anchor according to claim 12, characterized in that it is monolithically made of brittle material, in particular from the selection of - synthetic gemstone, especially diamond - Synthetic semi-precious stone - Silicon or silicon compound Anker nach Anspruch 17, dadurch gekennzeichnet, dass der Anker aus Silizium-Wafer hergestellt ist, dessen Oberfläche nitriert oder oxidiert ist.Anchor according to claim 17, characterized in that the armature is made of silicon wafer whose surface is nitrided or oxidized. Verfahren zur Herstellung eines Ankers nach Anspruch 1, dadurch gekennzeichnet, dass dieser aus Silizium nach dem DRIE-Verfahren (Deep Reactive-Ion Etching), insbesondere nach dem cryo-DRIE-Verfahren hergestellt wird.A method for producing an anchor according to claim 1, characterized in that this is made of silicon after the DRIE method (Deep Reactive Ion Etching), in particular according to the cryo-DRIE method is produced. Verfahren zur Herstellung eines Ankers, dadurch gekennzeichnet, dass dass dieser nach dem lithographisch galvanischen Abformverfahren (LIGA-Verfahren) hergestellt wird.Method for producing an anchor, characterized in that it is produced by the lithographic galvanic molding method (LIGA method).
EP08164108.6A 2007-09-13 2008-09-11 Anchor for a timepiece escapement Active EP2037335B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP13187564.3A EP2687916B1 (en) 2007-09-13 2008-09-11 Anchor for an escapement in a mechanical clock

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH14292007A CH708113B1 (en) 2007-09-13 2007-09-13 Anchor for a watch escapement.

Related Child Applications (2)

Application Number Title Priority Date Filing Date
EP13187564.3A Division EP2687916B1 (en) 2007-09-13 2008-09-11 Anchor for an escapement in a mechanical clock
EP13187564.3 Division-Into 2013-10-07

Publications (3)

Publication Number Publication Date
EP2037335A2 true EP2037335A2 (en) 2009-03-18
EP2037335A3 EP2037335A3 (en) 2012-08-29
EP2037335B1 EP2037335B1 (en) 2014-01-08

Family

ID=39768809

Family Applications (2)

Application Number Title Priority Date Filing Date
EP13187564.3A Active EP2687916B1 (en) 2007-09-13 2008-09-11 Anchor for an escapement in a mechanical clock
EP08164108.6A Active EP2037335B1 (en) 2007-09-13 2008-09-11 Anchor for a timepiece escapement

Family Applications Before (1)

Application Number Title Priority Date Filing Date
EP13187564.3A Active EP2687916B1 (en) 2007-09-13 2008-09-11 Anchor for an escapement in a mechanical clock

Country Status (2)

Country Link
EP (2) EP2687916B1 (en)
CH (1) CH708113B1 (en)

Cited By (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011120180A1 (en) 2010-04-01 2011-10-06 Rolex S.A. Immobilizing device for a toothed wheel
WO2012010408A1 (en) * 2010-07-19 2012-01-26 Nivarox-Far S.A. Oscillating mechanism with elastic pivot and mobile for the transmission of energy
EP2431823A1 (en) * 2010-09-16 2012-03-21 Blancpain S.A. Blancpain escapement with improved anchor for a timepiece movement
EP2466395A1 (en) * 2010-12-14 2012-06-20 Chopard Technologies SA Pallet and escapement equipped with said pallet
WO2012079976A1 (en) * 2010-12-14 2012-06-21 Chopard Technologies Sa Lever, and escapement provided with such a lever
EP2645189A1 (en) * 2012-03-29 2013-10-02 Nivarox-FAR S.A. Flexible escapement mechanism
WO2013144238A1 (en) 2012-03-29 2013-10-03 Nivarox-Far S.A. Flexible escapement mechanism having a plate-free balance
WO2013144237A1 (en) 2012-03-29 2013-10-03 Nivarox-Far S.A. Flexible lever-free escapement mechanism
WO2013144236A1 (en) 2012-03-29 2013-10-03 Nivarox-Far S.A. Flexible escapement mechanism having a mobile frame
EP2730980A1 (en) * 2012-11-09 2014-05-14 Nivarox-FAR S.A. Clockwork limitation or transmission mechanism
EP2887151A2 (en) 2013-12-12 2015-06-24 Richemont International S.A. Oscillating element for a clockwork
EP2455821B1 (en) 2010-11-18 2015-10-21 Nivarox-FAR S.A. Power transmission gear wheel
EP2998800A2 (en) 2014-09-16 2016-03-23 Patek Philippe SA Genève Timepiece component with flexible pivot
EP3037894A1 (en) 2014-12-22 2016-06-29 Manufacture et fabrique de montres et chronomètres Ulysse Nardin Le Locle SA Mechanism and method for adjusting a speed in a watch movement
EP3037893A1 (en) 2014-12-22 2016-06-29 Patek Philippe SA Genève Micromechanical or clock component with flexible guidance
EP3059641A1 (en) * 2015-02-20 2016-08-24 Nivarox-FAR S.A. Oscillator with a detent escapement
EP3076244A1 (en) 2015-03-11 2016-10-05 CSEM Centre Suisse d'Electronique et de Microtechnique SA - Recherche et Développement Shock-absorbing device for rotary parts
WO2017055987A1 (en) 2015-09-29 2017-04-06 Patek Philippe Sa Geneve Mechanical component with flexible guidance, particularly for a time-keeping movement
WO2017055986A1 (en) 2015-09-29 2017-04-06 Patek Philippe Sa Geneve Time-keeping movement comprising a flexible guidance system
EP3200029A1 (en) * 2016-01-29 2017-08-02 ETA SA Manufacture Horlogère Suisse Timepiece resonator mechanism
WO2018002778A1 (en) * 2016-06-29 2018-01-04 Patek Philippe Sa Geneve Mechanical clock movement
CH713288A1 (en) * 2016-12-23 2018-06-29 Sa De La Manufacture Dhorlogerie Audemars Piguet & Cie Flexible monolithic component for timepiece.
US10234823B2 (en) * 2014-05-20 2019-03-19 Sociétéanonyme de la Manufacture d'horlogerie Audemars Piguet & Cie Timepiece pallet fork for mechanical oscillator and timepiece time-delay release mechanism
WO2021053501A1 (en) 2019-09-16 2021-03-25 Richemont International Sa Method for manufacturing a plurality of resonators in a wafer
NL2023822B1 (en) * 2019-09-12 2021-05-17 Flexous Mech Ip B V Chronograph watch

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH713143A1 (en) 2016-11-17 2018-05-31 Richemont Int Sa Exhaust for timepiece.
CH713144A1 (en) * 2016-11-17 2018-05-31 Richemont Int Sa Exhaust for timepiece.

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH342897A (en) 1956-11-08 1959-11-30 Huguenin Pierre Louis Anchor escapement device for a watch movement
CH510285A (en) 1969-10-22 1971-03-31 Far Fab Assortiments Reunies Anchor escapement for timepiece
CH570644B5 (en) 1972-09-01 1975-12-15 Far Fab Assortiments Reunies
EP0183910A2 (en) 1984-11-02 1986-06-11 Kernforschungszentrum Karlsruhe Gmbh Process for the manufacture of deformable multiconnectors for the electrical connection of micro-electronic components, and multiconnectors manufactured by this process
DE3927163A1 (en) 1989-08-17 1991-02-21 Bosch Gmbh Robert Structuring disc-shaped monocrystalline semiconductor - using photomask for ion-etching of recess(es), orthogonal to semiconductor main surfaces
DE4420962A1 (en) 1994-06-16 1995-12-21 Bosch Gmbh Robert Process for processing silicon
EP1013949A1 (en) 1998-12-17 2000-06-28 Sysmelec SA Flexible pivot with large pivot angle and elevated rigidity
US6458263B1 (en) 2000-09-29 2002-10-01 Sandia National Laboratories Cantilevered multilevel LIGA devices and methods
EP1431844A1 (en) 2002-12-19 2004-06-23 SFT Services SA Assembly for the regulating organ of a watch movement
WO2007003539A2 (en) 2005-07-04 2007-01-11 Montres Breguet S.A. High-efficiency pallet escapement

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH437146A (en) * 1965-08-11 1967-11-30 Far Fab Assortiments Reunies Device for maintaining an escape anchor against the limit stops
CH588105B5 (en) * 1973-07-03 1977-05-31 Far Fab Assortiments Reunies
SE426511B (en) 1978-06-13 1983-01-24 Linden Alimak Ab DEVICE FOR AUTOMATED BULTISETING IN MOUNTAIN REINFORCEMENT
FR2731715B1 (en) * 1995-03-17 1997-05-16 Suisse Electronique Microtech MICRO-MECHANICAL PART AND METHOD FOR PRODUCING THE SAME
EP1538490B1 (en) * 2003-12-04 2007-05-30 Montres Breguet S.A. Detent escapement for wrist-watches
EP1770452A1 (en) * 2005-09-30 2007-04-04 Peter Baumberger Detent escapement for timepieces

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH342897A (en) 1956-11-08 1959-11-30 Huguenin Pierre Louis Anchor escapement device for a watch movement
CH510285A (en) 1969-10-22 1971-03-31 Far Fab Assortiments Reunies Anchor escapement for timepiece
DE2050013A1 (en) 1969-10-22 1971-04-29 Dassortiments Reunies Sa Fab Lever escapement for clockworks
CH570644B5 (en) 1972-09-01 1975-12-15 Far Fab Assortiments Reunies
EP0183910A2 (en) 1984-11-02 1986-06-11 Kernforschungszentrum Karlsruhe Gmbh Process for the manufacture of deformable multiconnectors for the electrical connection of micro-electronic components, and multiconnectors manufactured by this process
DE3927163A1 (en) 1989-08-17 1991-02-21 Bosch Gmbh Robert Structuring disc-shaped monocrystalline semiconductor - using photomask for ion-etching of recess(es), orthogonal to semiconductor main surfaces
DE4420962A1 (en) 1994-06-16 1995-12-21 Bosch Gmbh Robert Process for processing silicon
EP1013949A1 (en) 1998-12-17 2000-06-28 Sysmelec SA Flexible pivot with large pivot angle and elevated rigidity
US6458263B1 (en) 2000-09-29 2002-10-01 Sandia National Laboratories Cantilevered multilevel LIGA devices and methods
EP1431844A1 (en) 2002-12-19 2004-06-23 SFT Services SA Assembly for the regulating organ of a watch movement
WO2007003539A2 (en) 2005-07-04 2007-01-11 Montres Breguet S.A. High-efficiency pallet escapement

Cited By (62)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102971678A (en) * 2010-04-01 2013-03-13 劳力士有限公司 Immobilizing device for a toothed wheel
EP2818941A1 (en) 2010-04-01 2014-12-31 Rolex Sa Device for locking a sprocket wheel
CN102971678B (en) * 2010-04-01 2015-07-22 劳力士有限公司 Immobilizing device for a toothed wheel
WO2011120180A1 (en) 2010-04-01 2011-10-06 Rolex S.A. Immobilizing device for a toothed wheel
US8882339B2 (en) 2010-04-01 2014-11-11 Rolex S.A. Immobilizing device for a toothed wheel
JP2013524173A (en) * 2010-04-01 2013-06-17 ロレックス・ソシエテ・アノニム Gear fixing device
EP2894520A3 (en) * 2010-07-19 2016-06-22 Nivarox-FAR S.A. Oscillating mechanism with mobile, resilient pivot for energy transmission
US20130176829A1 (en) * 2010-07-19 2013-07-11 Nivarox-Far S.A. Oscillating mechanism with an elastic pivot and mobile element for transmitting energy
JP2013531257A (en) * 2010-07-19 2013-08-01 ニヴァロックス−ファー ソシエテ アノニム Oscillation mechanism with elastic pivot and movable element for energy transfer
US9201398B2 (en) 2010-07-19 2015-12-01 Nivarox-Far S.A. Oscillating mechanism with an elastic pivot and mobile element for transmitting energy
WO2012010408A1 (en) * 2010-07-19 2012-01-26 Nivarox-Far S.A. Oscillating mechanism with elastic pivot and mobile for the transmission of energy
WO2012034810A3 (en) * 2010-09-16 2012-06-14 Blancpain Sa Improved blancpain escapement with a pallet fork for a clock/watch movement
WO2012034810A2 (en) 2010-09-16 2012-03-22 Blancpain Sa Improved blancpain escapement with a pallet fork for a clock/watch movement
EP2431823A1 (en) * 2010-09-16 2012-03-21 Blancpain S.A. Blancpain escapement with improved anchor for a timepiece movement
EP2455821B1 (en) 2010-11-18 2015-10-21 Nivarox-FAR S.A. Power transmission gear wheel
WO2012079976A1 (en) * 2010-12-14 2012-06-21 Chopard Technologies Sa Lever, and escapement provided with such a lever
EP2466395A1 (en) * 2010-12-14 2012-06-20 Chopard Technologies SA Pallet and escapement equipped with said pallet
CN103261975A (en) * 2010-12-14 2013-08-21 萧邦科技公司 Lever, and escapement provided with such a lever
WO2013144236A1 (en) 2012-03-29 2013-10-03 Nivarox-Far S.A. Flexible escapement mechanism having a mobile frame
EP2645189A1 (en) * 2012-03-29 2013-10-02 Nivarox-FAR S.A. Flexible escapement mechanism
CN104204966B (en) * 2012-03-29 2017-02-22 尼瓦洛克斯-法尔股份有限公司 Flexible escapement mechanism having a mobile frame
KR20140135810A (en) * 2012-03-29 2014-11-26 니바록스-파 에스.에이. Flexible lever-free escapement mechanism
RU2607339C2 (en) * 2012-03-29 2017-01-10 Ниварокс-Фар С.А. Flexible anchor escapement mechanism with movable frame
US9304493B2 (en) 2012-03-29 2016-04-05 Nivarox-Far S.A. Flexible escapement mechanism having a balance with no roller
RU2607339C9 (en) * 2012-03-29 2017-02-22 Ниварокс-Фар С.А. Flexible anchor escapement mechanism with movable frame
US9207640B2 (en) 2012-03-29 2015-12-08 Nivarox-Far S.A. Flexible escape mechanism with no pallet lever
WO2013144238A1 (en) 2012-03-29 2013-10-03 Nivarox-Far S.A. Flexible escapement mechanism having a plate-free balance
WO2013144237A1 (en) 2012-03-29 2013-10-03 Nivarox-Far S.A. Flexible lever-free escapement mechanism
US9075394B2 (en) 2012-03-29 2015-07-07 Nivarox-Far S.A. Flexible escapement mechanism with movable frame
US9310771B2 (en) 2012-11-09 2016-04-12 Nivarox-Far S.A. Pallet lever mechanism for timepiece escapement
RU2605502C1 (en) * 2012-11-09 2016-12-20 Ниварокс-Фар С.А. Method of making flexible multistable-element
CN104737080B (en) * 2012-11-09 2017-05-24 尼瓦洛克斯-法尔股份有限公司 Pallet mechanism for a timepiece escapement
KR20150041138A (en) * 2012-11-09 2015-04-15 니바록스-파 에스.에이. Pallet mechanism for a timepiece escapement
KR20150036635A (en) * 2012-11-09 2015-04-07 니바록스-파 에스.에이. Method for the production of a multistable flexible element
KR101505325B1 (en) 2012-11-09 2015-03-23 니바록스-파 에스.에이. Timepiece anti-trip mechanism
CN104737080A (en) * 2012-11-09 2015-06-24 尼瓦洛克斯-法尔股份有限公司 Pallet mechanism for a timepiece escapement
US9317015B2 (en) 2012-11-09 2016-04-19 Nivarox-Far S.A. Timepiece anti-trip mechanism
EP2730980A1 (en) * 2012-11-09 2014-05-14 Nivarox-FAR S.A. Clockwork limitation or transmission mechanism
WO2014072317A2 (en) 2012-11-09 2014-05-15 Nivarox-Far S.A. Method for the production of a multistable flexible element
CN103809421A (en) * 2012-11-09 2014-05-21 尼瓦洛克斯-法尔股份有限公司 Timepiece anti-trip mechanism
WO2014072319A1 (en) * 2012-11-09 2014-05-15 Nivarox-Far S.A. Pallet mechanism for a timepiece escapement
US9778620B2 (en) 2012-11-09 2017-10-03 Nivarox-Far S.A. Method for creating a flexible, multistable element
RU2629546C2 (en) * 2012-11-09 2017-08-29 Ниварокс-Фар С.А. Detachment obstructing clock mechanism
EP2887151A2 (en) 2013-12-12 2015-06-24 Richemont International S.A. Oscillating element for a clockwork
US10234823B2 (en) * 2014-05-20 2019-03-19 Sociétéanonyme de la Manufacture d'horlogerie Audemars Piguet & Cie Timepiece pallet fork for mechanical oscillator and timepiece time-delay release mechanism
EP3457221A2 (en) 2014-09-16 2019-03-20 Patek Philippe SA Genève Timepiece oscillator with flexible pivot
EP2998800A2 (en) 2014-09-16 2016-03-23 Patek Philippe SA Genève Timepiece component with flexible pivot
EP3037893A1 (en) 2014-12-22 2016-06-29 Patek Philippe SA Genève Micromechanical or clock component with flexible guidance
EP3040783A1 (en) 2014-12-22 2016-07-06 Manufacture et fabrique de montres et chronomètres Ulysse Nardin Le Locle SA Sub-assembly for a mechanism for adjusting a speed in a clock movement and such a mechanism
EP3037894A1 (en) 2014-12-22 2016-06-29 Manufacture et fabrique de montres et chronomètres Ulysse Nardin Le Locle SA Mechanism and method for adjusting a speed in a watch movement
US9465362B2 (en) 2015-02-20 2016-10-11 Nivarox-Far S.A. Oscillator with a detent escapement
EP3059641A1 (en) * 2015-02-20 2016-08-24 Nivarox-FAR S.A. Oscillator with a detent escapement
EP3076244A1 (en) 2015-03-11 2016-10-05 CSEM Centre Suisse d'Electronique et de Microtechnique SA - Recherche et Développement Shock-absorbing device for rotary parts
WO2017055986A1 (en) 2015-09-29 2017-04-06 Patek Philippe Sa Geneve Time-keeping movement comprising a flexible guidance system
WO2017055987A1 (en) 2015-09-29 2017-04-06 Patek Philippe Sa Geneve Mechanical component with flexible guidance, particularly for a time-keeping movement
EP3356891B1 (en) * 2015-09-29 2023-10-04 Patek Philippe SA Genève Clockwork comprising a flexible guidance system
EP3200029A1 (en) * 2016-01-29 2017-08-02 ETA SA Manufacture Horlogère Suisse Timepiece resonator mechanism
WO2018002778A1 (en) * 2016-06-29 2018-01-04 Patek Philippe Sa Geneve Mechanical clock movement
CH713288A1 (en) * 2016-12-23 2018-06-29 Sa De La Manufacture Dhorlogerie Audemars Piguet & Cie Flexible monolithic component for timepiece.
NL2023822B1 (en) * 2019-09-12 2021-05-17 Flexous Mech Ip B V Chronograph watch
WO2021053501A1 (en) 2019-09-16 2021-03-25 Richemont International Sa Method for manufacturing a plurality of resonators in a wafer
US11709431B2 (en) 2019-09-16 2023-07-25 Richemont International Sa Method for manufacturing a plurality of resonators in a wafer

Also Published As

Publication number Publication date
EP2037335A3 (en) 2012-08-29
CH708113B1 (en) 2014-12-15
EP2687916B1 (en) 2016-06-08
EP2037335B1 (en) 2014-01-08
EP2687916A1 (en) 2014-01-22

Similar Documents

Publication Publication Date Title
EP2037335B1 (en) Anchor for a timepiece escapement
EP2107434B1 (en) Mechanical timer
DE69836411T2 (en) Clock or music box
EP2511229B1 (en) Micromechanical component with reinforced flanks
DE60225779T2 (en) Device with movement and chronograph module
EP1319997B1 (en) Constant force device
DE202015009912U1 (en) Monolithic clock regulator, movement and clock with such a clock regulator
AT505739B1 (en) SPRING FOR THE FEDER HOUSE OF A MOVEMENT WITH ENHANCED DURATION
DE102008029429A1 (en) Method for producing mechanical functional elements for movements as well as functional element produced by this method
DE202015009914U1 (en) Clock regulating mechanism, a movement for a clock, and a clock with such a mechanism
WO2017141222A1 (en) Pinion shaft, clockwork, clock or measuring device without magnetic signature
CH703781A2 (en) Escape wheel for timepiece e.g. mechanical timepiece has gear part formed from photolithography possible material having hardness and toughness comparable to silicon
EP1233314A1 (en) Clockwork
DE102010049290A1 (en) Clock part and clock
DE4417132C2 (en) Resonant sensor and its use
DE202013006409U1 (en) Time measuring mechanism for micrometric displacement
DE10158216A1 (en) Mirrors, optical imaging systems and their use
DE2502403A1 (en) CHARGE
CH339142A (en) Magnetic escapement
DE2733810A1 (en) CLOCK PART AND METHOD OF ITS MANUFACTURING
EP1596259A1 (en) Method of manufacture of thin metallic bodies, particularly watch parts
DE102014102081A1 (en) Micromechanical component and method for producing a micromechanical component
CH710169B1 (en) Escapement.
CH716172A2 (en) Constant force device.
DE102023107683A1 (en) anchor escapement

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MT NL NO PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA MK RS

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: VON GUNTEN, STEPHANE

RIN1 Information on inventor provided before grant (corrected)

Inventor name: AUGUST ENZLER

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MT NL NO PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA MK RS

RIC1 Information provided on ipc code assigned before grant

Ipc: G04B 15/14 20060101ALI20120725BHEP

Ipc: G04B 15/08 20060101AFI20120725BHEP

17P Request for examination filed

Effective date: 20121011

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

INTG Intention to grant announced

Effective date: 20130405

AKX Designation fees paid

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MT NL NO PL PT RO SE SI SK TR

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

INTG Intention to grant announced

Effective date: 20130802

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MT NL NO PL PT RO SE SI SK TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 649094

Country of ref document: AT

Kind code of ref document: T

Effective date: 20140215

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 502008011184

Country of ref document: DE

Effective date: 20140220

REG Reference to a national code

Ref country code: CH

Ref legal event code: NV

Representative=s name: BOVARD AG, CH

REG Reference to a national code

Ref country code: NL

Ref legal event code: VDEP

Effective date: 20140108

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140108

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140408

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140508

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140108

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140508

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140108

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140108

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140108

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140108

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140108

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140108

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502008011184

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140108

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140108

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140108

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140108

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

REG Reference to a national code

Ref country code: CH

Ref legal event code: PCOW

Free format text: NEW ADDRESS: CHEMIN DES VIRETTES 11, 2035 CORCELLES (CH)

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140108

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140108

26N No opposition filed

Effective date: 20141009

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502008011184

Country of ref document: DE

Effective date: 20141009

REG Reference to a national code

Ref country code: FR

Ref legal event code: CA

Effective date: 20150202

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140108

Ref country code: LU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140911

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140108

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20140930

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20140911

REG Reference to a national code

Ref country code: AT

Ref legal event code: MM01

Ref document number: 649094

Country of ref document: AT

Kind code of ref document: T

Effective date: 20140911

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20140911

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140108

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140108

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140409

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20080911

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140108

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 9

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20160920

Year of fee payment: 9

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20160921

Year of fee payment: 9

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IT

Payment date: 20160923

Year of fee payment: 9

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20170911

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20180531

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20170911

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20171002

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20170911

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20230920

Year of fee payment: 16

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: CH

Payment date: 20231001

Year of fee payment: 16