EP1645707B1 - Carriage arrangement for heavy wings slideable in a parallel plane - Google Patents

Carriage arrangement for heavy wings slideable in a parallel plane Download PDF

Info

Publication number
EP1645707B1
EP1645707B1 EP04104920.6A EP04104920A EP1645707B1 EP 1645707 B1 EP1645707 B1 EP 1645707B1 EP 04104920 A EP04104920 A EP 04104920A EP 1645707 B1 EP1645707 B1 EP 1645707B1
Authority
EP
European Patent Office
Prior art keywords
carriage
wing
arrangement according
pair
carriage arrangement
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
EP04104920.6A
Other languages
German (de)
French (fr)
Other versions
EP1645707A1 (en
Inventor
Dirk Muegge
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.)
Hautau GmbH
Original Assignee
Hautau GmbH
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 Hautau GmbH filed Critical Hautau GmbH
Priority to PL04104920T priority Critical patent/PL1645707T3/en
Priority to EP04104920.6A priority patent/EP1645707B1/en
Priority to HUE04104920A priority patent/HUE036909T2/en
Publication of EP1645707A1 publication Critical patent/EP1645707A1/en
Application granted granted Critical
Publication of EP1645707B1 publication Critical patent/EP1645707B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05DHINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D15/00Suspension arrangements for wings
    • E05D15/06Suspension arrangements for wings for wings sliding horizontally more or less in their own plane
    • E05D15/10Suspension arrangements for wings for wings sliding horizontally more or less in their own plane movable out of one plane into a second parallel plane
    • E05D15/1005Suspension arrangements for wings for wings sliding horizontally more or less in their own plane movable out of one plane into a second parallel plane the wing being supported on arms movable in horizontal planes
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2201/00Constructional elements; Accessories therefor
    • E05Y2201/60Suspension or transmission members; Accessories therefor
    • E05Y2201/622Suspension or transmission members elements
    • E05Y2201/686Rods, links

Definitions

  • the invention relates to a carriage arrangement for a heavy AbstellSchiebeeriel a window or a door according to the preamble of claim 1. It is basically already known, for example from the EP-A 1 170 448 A1 to provide for supporting such a heavy wing more than two carriages, each carriage part is connected via a Abstellarm with a wing-side mounting part, while the successive car parts, as usual, each coupled via a rod-shaped round profile.
  • the invention has for its object to enable a reliable transmission of large sash weights on the track with simple means. It should also be achieved that regardless of the attack situation (right or left-stopability) each carriage assembly can be composed of relatively few parts.
  • a carriage arrangement for a heavy AbstellSchiebeeriel a window or a door with the features of claim 1. Further details and advantageous embodiments will become apparent from the other claims.
  • a common, the wing frame mountable elongated rail with articulation points for the two Abstellarme each pair of carriages is provided, wherein the rail has at its two ends in each case a receiving bore into which can be inserted and attached to a lower wing spar when mounting a vertical strut.
  • the large sash weight is absorbed by at least two mountable on the casement elongated rails and over the two articulation points each rail and associated Abstellarmen evenly and without bending of the lower spar of the wing securely placed on the at least four carriages of the carriage assembly.
  • This wing weights up to 200 kg and clearly above can be safely absorbed and placed on the track of the carriage assembly.
  • that one pair of carriages which is closest to the wing side with the operating handle has two identically designed carriage housings, while the other pair of carriages has a carriage housing which relative to a plane perpendicular to the sliding direction is formed in mirror image to the carriage housing of the other pair of carriages.
  • FIGS. 1 and 2 are each in FIG. 1a respectively.
  • FIG. 2a the two pairs of carriages in their respective stop position shown in perspective, while the Figures 1b and 2 B shows the associated stop position by a plan view of a corresponding window assembly.
  • the carriage pair A has two carriages 4 and 5 (with housing), which are similar to each other, but also differ, while the two carriages 30 and 31 (with housing) of the carriage pair B are identical. Details for the pair of carriages B can be the FIGS. 3 to 5 remove.
  • FIGS. 3 and 4 shows the associated carriage housing 30 (or 31), which has in its central region an opening 30a, in which the one end of the Abstellarme 6.7 inserted and articulated there is connected to the housing. At its one end, the housing 30 and 31, a connection sleeve 12 into which the one end of a connecting rod 13 can be inserted and secured therein.
  • the housing has a rivet or mounting plateau 30b, on which rivet heads 30c are provided in the example shown, in order to be able to connect the housing to a connecting part, which connecting part in FIG FIG. 5 is shown in perspective.
  • the connecting part 10 may be a cast part, but is made in the preferred example shown as a stamped and bent part.
  • the link 10 has a round rod portion 10d, preferably welded to the plate portion 10e, which can be received in the coupling sleeve 12 of an adjacent carriage 31 and fixed therein.
  • the connecting member has a flat connecting and mounting portion 10 a, which has two rivet openings 10 b in the example shown and can be riveted to the mounting portion 30 b of the housing 30.
  • the bent part has a crank 10f, which leads into the flat plate portion 10e.
  • FIGS. 1a . 2a and 6 are shown connecting member 10 and the adjacent two housing parts in the assembled state.
  • the mounting portion 30b is used at the side of the wing 2, on which the operating handle 29 is arranged next lying carriage housing for attaching the plate-shaped control member 9a serving for pressing or pressing the blade control device.
  • FIG. 1a one recognizes that the housing of the carriage 5 of the pair of carriages A - with respect to a plane perpendicular to the direction of displacement of the wing - mirror images of the housings of the carriage 30 and 31 is formed, so apart from the mirroring is the same as that in the FIGS. 3 and 4 shown carriage housing 30.
  • the connecting members 10 can, as well as FIG. 1a already shows, to be used oriented in both possible sliding directions.
  • carriage housings 30 and 31 are identical, the carriage housing 5 is the same but mirror-inverted, while the carriage housing 4, which is farthest from the wing side, at which the handle 29 differs from both in that it has at one end instead of the flat mounting portion a stop or buffer 4a, which comes into effect on reaching the full open position.
  • the control part as a plate 9a of the control device 9 has a control slot for a sliding pin of a control arm, which is articulated at 9e.
  • the carriage housing 36 is identical to the carriage housings 30 and 31, and the same could apply to the housing 37 when the buffer or abutment part 37a as a separate part to the flat mounting portion of such a car is mounted.
  • the carriage arrangement is independent of the stop position with four different types of housing, while it would be in the case of the separate buffer, not shown, even only two types of carriage housings.
  • the connecting members 10 are formed the same. The same applies to the two Abstellarme 6, 7 each pair of carriages. These can be used for both applications, with the Abstellarme must be turned by 180 °.
  • Each pair of arms 6, 7 of a pair of carriages is hingedly mounted on the wing side on an elongate common rail 8.
  • the mounting locations are designated 26.
  • two different rails 8 and 8a are required for the different types of installation (right / left), as a comparison of FIGS. 1a and 2a shows.
  • each of the carriage pairs has only one common mounting rail. It can be seen that the high sash weight initially deposited on the elongated two rails and from there can be safely transferred to the respective two pivot points 26 of the Abstellarme 6 and 7.
  • a deflection of the lower wing spar due to only a punctiform connection of carriage with wing spar is excluded.
  • the wing-side mounting rail has at its two ends in each case a receiving bore 25a into which a vertical strut can be inserted and fixed in the vertical wing spar when mounting.
  • These bores 25 and 25a are provided at both ends of each of the mounting rails 8 and 8a, respectively.
  • Each carriage housing has a pair of rollers.
  • the carriage arrangement proves to be extremely stable and stable and is very simple and composed of few parts, the individual parts are designed extremely robust. This applies both to the carriage arrangement itself and to the connecting areas to the lower spar of the wing. Deformations of the wing under its high weight are safely avoided by the elongated rails 8,8a.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Wing Frames And Configurations (AREA)

Description

Die Erfindung betrifft eine Laufwagen-Anordnung für einen schweren AbstellSchiebeflügel eines Fensters oder einer Tür nach dem Oberbegriff des Anspruches 1.
Es ist grundsätzlich bereits bekannt, zum Beispiel aus der EP-A 1 170 448 A1 , zur Abstützung eines solchen schweren Flügels mehr als zwei Laufwagen vorzusehen, wobei jeder Laufwagenteil über einen Abstellarm mit einem flügelseitigen Montageteil verbunden ist, während die aufeinanderfolgenden Wagenteile, wie üblich, jeweils über ein stangenförmiges Rundprofil miteinander gekuppelt sind.
Der Erfindung liegt die Aufgabe zugrunde, eine zuverlässige Übertragung großer Flügelgewichte auf die Laufschiene mit einfachen Mitteln zu ermöglichen. Es soll außerdem erreicht werden, dass unabhängig von der Anschlagssituation (Rechts- oder Links-Anschlagbarkeit) jede Laufwagen-Anordnung aus relativ wenigen Teilen zusammengesetzt werden kann.
Diese Aufgabe wird mit einer Laufwagen-Anordnung für einen schweren AbstellSchiebeflügel eines Fensters oder einer Tür mit den Merkmalen des Anspruches 1 gelöst.
Weitere Einzelheiten und vorteilhafte Ausbildungen ergeben sich aus den weiteren Ansprüchen.
Erfindungsgemäß ist eine gemeinsame, am Flügelrahmen montierbare langgestreckte Profilschiene mit Anlenkstellen für die beiden Abstellarme jedes Laufwagen-Paares vorgesehen, wobei die Profilschiene an ihren beiden Enden jeweils eine Aufnahmebohrung aufweist, in die beim Montieren eine Vertikalstrebe an einem unteren Flügelholm eingesteckt und befestigt werden kann. Hierbei wird das große Flügelgewicht durch zumindest zwei am Flügelrahmen montierbare langgestreckte Profilschienen aufgenommen und über die beiden Anlenkstellen jeder Profilschiene und diesen zugeordneten Abstellarmen gleichmäßig und ohne Durchbiegen des unteren Holms des Flügels sicher auf die wenigstens vier Laufwagen der Laufwagen-Anordnung abgesetzt wird. Damit können Flügelgewichte bis zu 200 kg und deutlich darüber sicher aufgenommen und auf die Laufschiene der Laufwagen-Anordnung abgesetzt werden.
Vorzugsweise weist dasjenige Laufwagen-Paar, welches der Flügelseite mit dem Betätigungsgriff am nächsten ist, zwei identisch ausgebildete Laufwagengehäuse auf, während das andere Laufwagen-Paar ein Laufwagen-Gehäuse aufweist, das bezogen auf eine Ebene senkrecht zur Schieberichtung spiegelbildlich zu dem Laufwagengehäuse des anderen Laufwagenpaares ausgebildet ist.
The invention relates to a carriage arrangement for a heavy AbstellSchiebeflügel a window or a door according to the preamble of claim 1.
It is basically already known, for example from the EP-A 1 170 448 A1 to provide for supporting such a heavy wing more than two carriages, each carriage part is connected via a Abstellarm with a wing-side mounting part, while the successive car parts, as usual, each coupled via a rod-shaped round profile.
The invention has for its object to enable a reliable transmission of large sash weights on the track with simple means. It should also be achieved that regardless of the attack situation (right or left-stopability) each carriage assembly can be composed of relatively few parts.
This object is achieved with a carriage arrangement for a heavy AbstellSchiebeflügel a window or a door with the features of claim 1.
Further details and advantageous embodiments will become apparent from the other claims.
According to the invention, a common, the wing frame mountable elongated rail with articulation points for the two Abstellarme each pair of carriages is provided, wherein the rail has at its two ends in each case a receiving bore into which can be inserted and attached to a lower wing spar when mounting a vertical strut. Here, the large sash weight is absorbed by at least two mountable on the casement elongated rails and over the two articulation points each rail and associated Abstellarmen evenly and without bending of the lower spar of the wing securely placed on the at least four carriages of the carriage assembly. This wing weights up to 200 kg and clearly above can be safely absorbed and placed on the track of the carriage assembly.
Preferably, that one pair of carriages which is closest to the wing side with the operating handle has two identically designed carriage housings, while the other pair of carriages has a carriage housing which relative to a plane perpendicular to the sliding direction is formed in mirror image to the carriage housing of the other pair of carriages.

Dabei ist die ganze Anordnung außerordentlich einfach, da unabhängig von der linksseitigen oder rechtsseitigen Anschlagart für jeweils drei Positionen der Anordnung identische Laufwagengehäuse eingesetzt werden können. Im günstigsten Fall können beide Einsatzmöglichkeiten lediglich mit einem Satz von vier verschiedenen Laufwagen-Gehäusen abgedeckt werden.In this case, the whole arrangement is extremely simple, since regardless of the left-side or right-side stop for each three positions of the arrangement identical carriage housing can be used. In the best case, both applications can be covered only with a set of four different carriage housings.

Weitere Einzelheiten und vorteilhafte Ausbildungen ergeben sich aus den abhängigen Ansprüchen.Further details and advantageous embodiments will be apparent from the dependent claims.

Die Erfindung wird nachfolgend anhand von Ausführungsbeispielen erläutert und ergänzt.

Figur la, Figur 1b, Figur 2a, Figur 2b
zeigen jeweils in gleicher Darstellung eine Laufwagen-Anordnung, und zwar in den Figuren 1 für nach links zu öffnende Schiebeflügel 2 und in den Figuren 2 für nach rechts öffnende Schiebeflügel 2.
Figur 3, Figur 4
zeigen ein Laufwagen-Gehäuse 30, in perspektivischer Ansicht und in Seitenansicht.
Figur 5
zeigt in perspektivischer Ansicht ein Verbindungselement 10, das zwischen den Laufwagen-Gehäusen eines Laufwagen-Paares eingesetzt werden kann.
Figur 6
zeigt eines der in Figuren 1 dargestellten Laufwagen-Paare bei geöffnetem Flügel in Aufsicht.
The invention is explained below with reference to examples of execution and supplemented.
Figure la, Figure 1b, Figure 2a, Figure 2b
each show in the same representation a carriage arrangement, in the FIGS. 1 for left-opening sliding sash 2 and in the Figures 2 for sliding doors 2 opening to the right
FIG. 3, FIG. 4
show a carriage housing 30, in perspective view and in side view.
FIG. 5
shows in perspective view a connecting element 10 which can be used between the carriage housings of a pair of carriages.
FIG. 6
shows one of the in FIGS. 1 shown carriage pairs with open wing in supervision.

In den Figuren 1 und 2 sind jeweils in Figur 1a bzw. Figur 2a die beiden Laufwagen-Paare in ihrer jeweiligen Anschlagposition in perspektivischer Darstellung gezeigt, während die Figuren 1b und 2b die zugehörige Anschlagposition durch eine Draufsicht auf eine entsprechende Fensteranordnung zeigt.In the FIGS. 1 and 2 are each in FIG. 1a respectively. FIG. 2a the two pairs of carriages in their respective stop position shown in perspective, while the Figures 1b and 2 B shows the associated stop position by a plan view of a corresponding window assembly.

In der Anordnung für nach links zu öffnende Flügel 2 gemäß Figur 1 sind zwei Laufwagen-Paare A und B auf einer gemeinsamen (nicht gezeigten) Laufschiene angeordnet und über eine Verbindungsstange 13, vorzugsweise mit Rundprofil, miteinander verbunden.In the arrangement for left-opening wing 2 according to FIG. 1 two pairs of carriages A and B are arranged on a common (not shown) running rail and connected to each other via a connecting rod 13, preferably with a round profile.

Das Laufwagen-Paar A weist zwei Laufwagen 4 und 5 (mit Gehäuse) auf, die zwar einander ähnlich ausgebildet sind, sich jedoch auch unterscheiden, während die beiden Laufwagen 30 und 31 (mit Gehäuse) des Laufwagen-Paares B identisch ausgebildet sind.
Einzelheiten für das Laufwagen-Paar B lassen sich den Figuren 3 bis 5 entnehmen.
Figur 3 und 4 zeigt das zugehörige Laufwagen-Gehäuse 30 (oder 31), das in seinem Mittenbereich eine Öffnung 30a aufweist, in die das eine Ende der Abstellarme 6,7 eingefügt und dort gelenkig mit dem Gehäuse verbunden wird. An seinem einen Ende weist das Gehäuse 30 bzw. 31 eine Verbindungsmuffe 12 auf, in die das eine Ende einer Verbindungsstange 13 eingeschoben und darin befestigt werden kann. Am anderen Ende weist das Gehäuse ein Niet- oder Montageplateau 30b auf, an dem im dargestellten Beispiel Nietköpfe 30c vorgesehen sind, um das Gehäuse mit einem Verbindungsteil verbinden zu können, welches Verbindungsteil in Figur 5 perspektivisch dargestellt ist.
Das Verbindungsteil 10 kann ein Gussteil sein, ist jedoch in dem gezeigten bevorzugten Beispiel als Stanzbiegeteil angefertigt. An seinem einen Ende weist das Verbindungsglied 10 einen an dem Plattenabschnitt 10e vorzugsweise angeschweißten Rundstangenabschnitt 10d auf, der in der Verbindungsmuffe 12 eines benachbarten Laufwagens 31 aufgenommen und darin befestigt werden kann. Am anderen Ende weist das Verbindungsglied einen flachen Verbindungs- und Montageabschnitt 10a auf, der im dargestellten Beispiel zwei Nietöffnungen 10b besitzt und an dem Montageabschnitt 30b des Gehäuses 30 fest-genietet werden kann. Zwischen den beiden Enden weist der Biegeteil eine Kröpfung 10f auf, die in den flachen Plattenabschnitt 10e überleitet.
In den Figuren 1a , 2a und 6 sind Verbindungsglied 10 und die benachbarten beiden Gehäuseteile im montierten Zustand gezeigt.
Der Montageabschnitt 30b dient bei dem der Seite des Flügels 2, an dem der Betätigungsgriff 29 angeordnet ist, am nächsten liegenden Laufwagen-Gehäuse zum Anbringen des plattenförmigen Steuerungsgliedes 9a der zum Abdrücken bzw. Andrücken des Flügels dienenden Steuereinrichtung 9.
The carriage pair A has two carriages 4 and 5 (with housing), which are similar to each other, but also differ, while the two carriages 30 and 31 (with housing) of the carriage pair B are identical.
Details for the pair of carriages B can be the FIGS. 3 to 5 remove.
FIGS. 3 and 4 shows the associated carriage housing 30 (or 31), which has in its central region an opening 30a, in which the one end of the Abstellarme 6.7 inserted and articulated there is connected to the housing. At its one end, the housing 30 and 31, a connection sleeve 12 into which the one end of a connecting rod 13 can be inserted and secured therein. At the other end, the housing has a rivet or mounting plateau 30b, on which rivet heads 30c are provided in the example shown, in order to be able to connect the housing to a connecting part, which connecting part in FIG FIG. 5 is shown in perspective.
The connecting part 10 may be a cast part, but is made in the preferred example shown as a stamped and bent part. At its one end, the link 10 has a round rod portion 10d, preferably welded to the plate portion 10e, which can be received in the coupling sleeve 12 of an adjacent carriage 31 and fixed therein. At the other end, the connecting member has a flat connecting and mounting portion 10 a, which has two rivet openings 10 b in the example shown and can be riveted to the mounting portion 30 b of the housing 30. Between the two ends, the bent part has a crank 10f, which leads into the flat plate portion 10e.
In the FIGS. 1a . 2a and 6 are shown connecting member 10 and the adjacent two housing parts in the assembled state.
The mounting portion 30b is used at the side of the wing 2, on which the operating handle 29 is arranged next lying carriage housing for attaching the plate-shaped control member 9a serving for pressing or pressing the blade control device. 9

Aus Figur 1a erkennt man, dass das Gehäuse des Laufwagens 5 des Laufwagen-Paares A - bezogen auf eine Ebene senkrecht zur Verschieberichtung des Flügels - spiegelbildlich zu den Gehäusen der Laufwagen 30 und 31 ausgebildet ist, also abgesehen von der Spiegelung gleich ausgebildet ist wie das in den Figuren 3 und 4 gezeigte Laufwagen-Gehäuse 30. Die Verbindungsglieder 10 können, wie das auch Figur 1a schon zeigt, in beiden möglichen Schieberichtungen orientiert verwendet werden.Out FIG. 1a one recognizes that the housing of the carriage 5 of the pair of carriages A - with respect to a plane perpendicular to the direction of displacement of the wing - mirror images of the housings of the carriage 30 and 31 is formed, so apart from the mirroring is the same as that in the FIGS. 3 and 4 shown carriage housing 30. The connecting members 10 can, as well as FIG. 1a already shows, to be used oriented in both possible sliding directions.

Es wird nochmals betont, dass die Laufwagen-Gehäuse 30 und 31 identisch sind, das Laufwagen-Gehäuse 5 diesen gleicht aber spiegelverkehrt ausgebildet ist, während sich das Laufwagen-Gehäuse 4, das am weitesten entfernt von der Flügelseite befindet, an der sich der Handgriff 29 befindet, sich von beiden dadurch unterscheidet, dass es an einem Ende statt des flachen Montageabschnittes einen Anschlag oder Puffer 4a aufweist, der bei Erreichen der vollen Öffnungsstellung zur Wirkung kommt.It is again emphasized that the carriage housings 30 and 31 are identical, the carriage housing 5 is the same but mirror-inverted, while the carriage housing 4, which is farthest from the wing side, at which the handle 29 differs from both in that it has at one end instead of the flat mounting portion a stop or buffer 4a, which comes into effect on reaching the full open position.

Es könnte allerdings auch ein solcher Anschlag oder Puffer bei sonst gleicher Ausbildung des Laufwagen-Gehäuses als zusätzlicher Teil an dem flachen Montageabschnitt 30b montiert sein, so dass auch das Laufwagen-Gehäuse 4 mit dem Laufwagen-Gehäuse 5 identisch ist.However, it could also be such an abutment or buffer with otherwise identical design of the carriage housing mounted as an additional part of the flat mounting portion 30b, so that the carriage housing 4 with the carriage housing 5 is identical.

Das Steuerungsteil als Platte 9a der Steuereinrichtung 9 weist einen Steuerungsschlitz für einen Gleitbolzen eines Steuerungslenkers auf, der bei 9e angelenkt ist.The control part as a plate 9a of the control device 9 has a control slot for a sliding pin of a control arm, which is articulated at 9e.

Vergleicht man die Figuren 2a und 1a miteinander, die sich durch die entgegengesetzte Anschlagposition unterscheiden, so wird zum Beispiel deutlich, dass die beiden Laufwagen-Gehäuse 32,33 des Laufwagen-Paares C dem Laufwagen-Gehäuse 5 des Laufwagen-Paares A identisch sind. Wenn das Pufferstück an dem Laufwagen-Gehäuse 4 als gesonderter Teil an dem flachen Montageteil 30b montiert wird, können sogar die Gehäuse 4,5 des Laufwagen-Paares A und die Gehäuse 32 und 33 des Laufwagen-Paares C identisch sein.Comparing the FIGS. 2a and 1a to each other, which differ by the opposite stop position, it is clear, for example, that the two carriage housings 32,33 of the carriage pair C are identical to the carriage housing 5 of the carriage pair A. When the buffer piece is attached to the carriage body 4 as a separate part on the flat mounting part 30b even the housings 4, 5 of the carriage pair A and the housings 32 and 33 of the carriage pair C may be identical.

Entsprechendes gilt für die Laufwagen-Paare B und D. Das Laufwagen-Gehäuse 36 ist identisch mit den Laufwagen-Gehäusen 30 und 31, und das gleiche könnte für das Gehäuse 37 gelten, wenn der Puffer oder Anschlagteil 37a als gesonderter Teil an dem flachen Montageabschnitt eines solchen Wagens montiert wird.The same applies to the carriage pairs B and D. The carriage housing 36 is identical to the carriage housings 30 and 31, and the same could apply to the housing 37 when the buffer or abutment part 37a as a separate part to the flat mounting portion of such a car is mounted.

Im dargestellten Beispiel kommt die Laufwagen-Anordnung unabhängig von der Anschlagsposition mit vier verschiedenen Gehäusetypen aus, während es im nicht dargestellten Fall des gesonderten Puffers sogar nur zwei Laufwagen-Gehäusetypen wären.In the example shown, the carriage arrangement is independent of the stop position with four different types of housing, while it would be in the case of the separate buffer, not shown, even only two types of carriage housings.

In allen Fällen sind die Verbindungsglieder 10 gleich ausgebildet. Dasselbe gilt für die beiden Abstellarme 6, 7 jedes Laufwagen-Paares. Diese können für beide Einsatzmöglichkeiten verwendet werden, wobei die Abstellarme um 180° gewendet werden müssen.In all cases, the connecting members 10 are formed the same. The same applies to the two Abstellarme 6, 7 each pair of carriages. These can be used for both applications, with the Abstellarme must be turned by 180 °.

Jedes Armpaar 6, 7 eines Laufwagen-Paares ist flügelseitig an einer langgestreckten gemeinsamen Profilschiene 8 gelenkig montiert. Die Montagestellen sind mit 26 bezeichnet. Mit der Lage der Anlenkstellen 26 sind für die unterschiedlichen Montagearten (rechts/links) zwei verschiedene Profilschienen 8 und 8a erforderlich, wie ein Vergleich der Figuren 1a und 2a zeigt. Es ist aber auch möglich, an jeder Profilschiene 8 vier mögliche Anlenkstellen 26 und 26a vorzusehen, so dass die gleiche Profilschiene 8 für beide Montagepositionen (re/li) eingesetzt werden kann.Each pair of arms 6, 7 of a pair of carriages is hingedly mounted on the wing side on an elongate common rail 8. The mounting locations are designated 26. With the location of the articulation points 26 two different rails 8 and 8a are required for the different types of installation (right / left), as a comparison of FIGS. 1a and 2a shows. But it is also possible to provide on each rail 8 four possible pivot points 26 and 26 a, so that the same rail 8 for both mounting positions (re / li) can be used.

Wesentlich ist, dass jedes der Laufwagen-Paare nur eine gemeinsame Montageprofilschiene besitzt. Man erkennt daran, dass das hohe Flügelgewicht zunächst auf die langgestreckten beiden Schienen abgesetzt und von dort sicher auf die jeweiligen beiden Anlenkpunkte 26 der Abstellarme 6 und 7 übertragen werden kann.It is essential that each of the carriage pairs has only one common mounting rail. It can be seen that the high sash weight initially deposited on the elongated two rails and from there can be safely transferred to the respective two pivot points 26 of the Abstellarme 6 and 7.

Ein Durchbiegen des unteren Flügelholms aufgrund nur einer punktförmigen Verbindung von Laufwagen mit Flügelholm wird so ausgeschlossen.A deflection of the lower wing spar due to only a punctiform connection of carriage with wing spar is excluded.

Die flügelseitige Montageprofilschiene weist an ihren beiden Enden jeweils eine Aufnahmebohrung 25a auf, in die beim Montieren eine Vertikalstrebe in dem senkrechten Flügelholm eingesteckt und befestigt werden kann. Diese Bohrungen 25 bzw. 25a sind jeweils an beiden Enden jeder der Montageschienen 8 und 8a vorgesehen.The wing-side mounting rail has at its two ends in each case a receiving bore 25a into which a vertical strut can be inserted and fixed in the vertical wing spar when mounting. These bores 25 and 25a are provided at both ends of each of the mounting rails 8 and 8a, respectively.

Nicht dargestellt sind die zugehörigen Rollen, die den einzelnen Laufwagen-Gehäusen zugeordnet sind und auf der in den Figuren 1b und 2b gezeigten Laufschiene 35 aufsitzen.Not shown are the associated roles that are assigned to the individual carriage housings and on in the Figures 1b and 2 B sit running track 35.

Jedes Laufwagen-Gehäuse weist dabei ein Rollenpaar auf.Each carriage housing has a pair of rollers.

Die Laufwagen-Anordnung erweist sich als außerordentlich stabil und tragfähig und ist sehr einfach und aus wenigen Teilen aufgebaut, wobei die einzelnen Teile ausgesprochen robust ausgebildet sind. Dies gilt sowohl für die Laufwagen-Anordnung selbst als auch für die Verbindungsbereiche zum unteren Holm des Flügels. Verformungen des Flügels unter seinem hohen Eigengewicht werden sicher durch die langgestreckten Profilschienen 8,8a vermieden.The carriage arrangement proves to be extremely stable and stable and is very simple and composed of few parts, the individual parts are designed extremely robust. This applies both to the carriage arrangement itself and to the connecting areas to the lower spar of the wing. Deformations of the wing under its high weight are safely avoided by the elongated rails 8,8a.

Claims (9)

  1. Carriage arrangement for a heavy wing, slideable in a parallel plane, of a window or door, which arrangement for supporting the heavy wing (2) has at least two carriage pairs (A, B), wherein each carriage (4, 5; 30, 31) of the pair of carriages comprises a shunt arm (6, 7; 6, 7) for connecting each carriage (4, 5; 30, 31) to the lower wing spar of the wing (2), and the carriage pairs (A, B) are connected to each other at a distance via a connecting rod (13), characterized in that two elongated profile rails (8, 8a) which can be mounted on the wing frame (2) are provided with articulation points (26) for all shunt arms (6, 7; 6, 7) and the two shunt arms (6, 7) of a respective carriage pair (A; B) are pivotably mounted at the two articulation points (26, 26 a) of a respective one of the profile rails (8, 8a), wherein the wing-side profile rails (8, 8a) have at their two ends in each case a receiving bore (25, 25a) into which a vertical strut can be inserted and fastened at a lower wing spar during mounting.
  2. Carriage arrangement according to claim 1, comprising a control device (9) for controlling the engaging and disengaging of the wing (2), wherein a control plate (9a) of the control device is provided on a flat connecting and mounting portion (30b) of the carriage (31) disposed closest to the wing side with an operating handle (29).
  3. Carriage arrangement according to claim 1, wherein each carriage (4, 5, 30, 31) comprises at one end a rivet plateau (30b) or a flat mounting element and at the other end a coupling element (12) for the connecting rod or a rod portion (13, 10d).
  4. Carriage arrangement according to one of the claims 1 to 3, wherein the carriage (4) of the carriage arrangement (A, B) furthest away from the wing side with the operating handle (29) comprises a stop or buffer element (4a) which comes into effect at the end of a wing opening operation.
  5. Carriage arrangement according to one of the claims 1 or 2, wherein between the two carriages (4, 5; 30, 31) of each carriage pair (A; B), a connecting member (10), preferably designed as a stamped and bent part, is provided, having at one end a rod portion (10d) and at the other end a flat connecting and mounting portion (10a).
  6. Carriage arrangement according to claim 5, wherein the connecting member (10) has a crank (10f) between its rod portion (10d) and its flat connecting and mounting portion (10a).
  7. Carriage arrangement according to one of the preceding claims, wherein carriage housings of the carriage pair (C, 32, 33), which is closest to the wing side with the operating handle (29), are identically formed for a stop of the carriage arrangement on the frame (1) optionally on the left or right, and a carriage housing (33) of this pair (C), in the case of an opposite stop situation, can be inserted at the penultimate position of the carriage arrangement.
  8. Carriage arrangement according to one of the preceding claims, wherein the carriages (4, 5; 30, 31) have carriage housings.
  9. Carriage arrangement according to one of the preceding claims, wherein each profile rail (8) has four possible points (26, 26a) for articulation, wherein for a respective stop situation only two points are used as articulation points (26, 26a) each with a shunt arm (6, 7), and a respective shunt arm (6, 7) is pivotably mounted at each one of the two articulation points (26, 26 a).
EP04104920.6A 2004-10-07 2004-10-07 Carriage arrangement for heavy wings slideable in a parallel plane Active EP1645707B1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
PL04104920T PL1645707T3 (en) 2004-10-07 2004-10-07 Carriage arrangement for heavy wings slideable in a parallel plane
EP04104920.6A EP1645707B1 (en) 2004-10-07 2004-10-07 Carriage arrangement for heavy wings slideable in a parallel plane
HUE04104920A HUE036909T2 (en) 2004-10-07 2004-10-07 Carriage arrangement for heavy wings slideable in a parallel plane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP04104920.6A EP1645707B1 (en) 2004-10-07 2004-10-07 Carriage arrangement for heavy wings slideable in a parallel plane

Publications (2)

Publication Number Publication Date
EP1645707A1 EP1645707A1 (en) 2006-04-12
EP1645707B1 true EP1645707B1 (en) 2018-02-14

Family

ID=34929673

Family Applications (1)

Application Number Title Priority Date Filing Date
EP04104920.6A Active EP1645707B1 (en) 2004-10-07 2004-10-07 Carriage arrangement for heavy wings slideable in a parallel plane

Country Status (3)

Country Link
EP (1) EP1645707B1 (en)
HU (1) HUE036909T2 (en)
PL (1) PL1645707T3 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ATE489527T1 (en) 2008-09-30 2010-12-15 Hautau Gmbh ADJUSTING DEVICE FOR A DISTANCE BETWEEN TWO CARRIAGES MOVING ON A COMMON RAIL AND METHOD
DE102014212461B3 (en) * 2014-06-27 2015-08-13 Roto Frank Ag Carriage assembly with an eccentric control pin and sliding or sliding window with such a carriage assembly
DE102014212463A1 (en) 2014-06-27 2015-12-31 Roto Frank Ag Carriage assembly with a spring recess and sliding door, sliding window or the like with such a carriage assembly
DE102016212449A1 (en) 2016-07-07 2018-01-11 Roto Frank Ag Carriage arrangement for a door or a window of a building with a fixed frame and a relative to the fixed frame sliding wings
CN107062721A (en) * 2017-03-08 2017-08-18 宁波舜康电器有限公司 A kind of dual-purpose ice machine
DE102018114997A1 (en) * 2018-06-21 2019-12-24 Maco Technologie Gmbh fitting assembly

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE8709235U1 (en) * 1987-07-03 1987-08-20 W. Hautau Gmbh, 3068 Helpsen, De
IT1312027B1 (en) * 1999-03-26 2002-04-04 Antonio Giovannetti MECHANISM AND COMPLEX FOR OPENING-CLOSING OF COPLANAR LEAVES, SUITABLE FOR ALLOWING A MOVEMENT OF THE LEAF PARALLELLY TO ITSELF
ATE294312T1 (en) * 2000-07-04 2005-05-15 Gretsch Unitas Gmbh CARRIAGE FOR A PARALLEL SLIDING AND TILTING FITTING OF A BUILDING WINDOW OR A BUILDING WINDOW DOOR AND BUILDING WINDOW OR BUILDING WINDOW DOOR WITH SUCH A PARALLEL SLIDING AND TILTING FITTING

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Also Published As

Publication number Publication date
EP1645707A1 (en) 2006-04-12
PL1645707T3 (en) 2018-07-31
HUE036909T2 (en) 2018-08-28

Similar Documents

Publication Publication Date Title
DE2648344C3 (en) Fitting for sliding windows, sliding doors or the like.
DE3645338C2 (en) Concealed window hinge fitting
EP3064683B1 (en) Carriage for a sliding door
EP0678636B1 (en) Connecting device for installing the sash of a skylight in the main frame
WO2020007830A1 (en) Pre-assembled fitting group and fitting assembly for a window or a door
WO2008083864A1 (en) Concealed fitting for a window or a door
EP1645707B1 (en) Carriage arrangement for heavy wings slideable in a parallel plane
EP3175068B1 (en) Fitting arrangement
WO2012095806A1 (en) Adjustable vertical reinforcement element for a sliding sash that is movable from one plane to a plane parallel to the frame
EP0276678B1 (en) Fitting for an at least pivoting door, window or the like
EP3482026A2 (en) Roller carriage array for a door or window of a building, the door or window having a fixed frame and a sash or leaf slidable relative to the fixed frame
EP0356761A1 (en) Scissor lift device, especially for a working platform
DE3343366C2 (en)
WO2016023738A1 (en) Running carriage arrangement for lift-and-slide doors or windows
AT524557B1 (en) Guide system for guiding at least one door leaf relative to a furniture body
EP3798390B1 (en) Folding installation
EP1298271A2 (en) Carriage for a fitting for lifting and sliding doors or windows and a fitting with such a carriage
EP0610557A1 (en) Guide rail system for sliding doors, sliding and folding doors, sliding windows or similar
DE8103368U1 (en) Tilt and turn window or door
EP1549801B1 (en) Articulated rail connection for rail joints of profiled sliding rails
AT411085B (en) TURNTING FITTING FOR A ROUND-ARC WINDOW
EP2690241B1 (en) Fitting for a parallel set sliding door or a parallel set sliding window
DE1584240C (en) Device for moving a gate wing that can be swiveled overhead
DE1584240B1 (en) Device for moving an overhead pivotable gate leaf
DE2254889C3 (en) Swinging garage door with stabilizer

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: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL HR LT LV MK

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

Owner name: HAUTAU GMBH

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

Owner name: HAUTAU GMBH

17P Request for examination filed

Effective date: 20060628

AKX Designation fees paid

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PL PT RO SE SI SK TR

17Q First examination report despatched

Effective date: 20130319

TPAC Observations filed by third parties

Free format text: ORIGINAL CODE: EPIDOSNTIPA

TPAC Observations filed by third parties

Free format text: ORIGINAL CODE: EPIDOSNTIPA

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

Free format text: STATUS: EXAMINATION IS IN PROGRESS

TPAC Observations filed by third parties

Free format text: ORIGINAL CODE: EPIDOSNTIPA

TPAC Observations filed by third parties

Free format text: ORIGINAL CODE: EPIDOSNTIPA

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

Owner name: HAUTAU GMBH

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

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

Free format text: STATUS: GRANT OF PATENT IS INTENDED

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

INTG Intention to grant announced

Effective date: 20171208

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

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

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

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 HU IE IT LI LU MC NL 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: DE

Ref legal event code: R096

Ref document number: 502004015647

Country of ref document: DE

Ref country code: AT

Ref legal event code: REF

Ref document number: 969938

Country of ref document: AT

Kind code of ref document: T

Effective date: 20180315

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20180214

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

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: 20180214

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: 20180214

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: 20180214

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: 20180214

REG Reference to a national code

Ref country code: HU

Ref legal event code: AG4A

Ref document number: E036909

Country of ref document: HU

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

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: 20180214

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: 20180515

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: 20180514

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

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: 20180214

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: 20180214

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502004015647

Country of ref document: DE

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

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: 20180214

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: 20180214

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: 20180214

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

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

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

26N No opposition filed

Effective date: 20181115

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

Ref country code: PL

Payment date: 20181001

Year of fee payment: 15

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: 20180214

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

Ref country code: TR

Payment date: 20181024

Year of fee payment: 15

Ref country code: IT

Payment date: 20181022

Year of fee payment: 15

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

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

Effective date: 20181007

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20181031

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: 20180214

Ref country code: LU

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

Effective date: 20181007

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: CH

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

Effective date: 20181031

Ref country code: BE

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

Effective date: 20181031

Ref country code: LI

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

Effective date: 20181031

Ref country code: FR

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

Effective date: 20181031

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: 20181007

Ref country code: GB

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

Effective date: 20181007

REG Reference to a national code

Ref country code: AT

Ref legal event code: MM01

Ref document number: 969938

Country of ref document: AT

Kind code of ref document: T

Effective date: 20181007

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: 20181007

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

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: 20180214

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

Ref country code: IT

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

Effective date: 20191007

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

Ref country code: PL

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

Effective date: 20191007

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

Ref country code: TR

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

Effective date: 20191007

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

Ref country code: HU

Payment date: 20231004

Year of fee payment: 20

Ref country code: DE

Payment date: 20230403

Year of fee payment: 20