EP2744960B1 - Bearing part of a window, door or similar - Google Patents
Bearing part of a window, door or similar Download PDFInfo
- Publication number
- EP2744960B1 EP2744960B1 EP12742869.6A EP12742869A EP2744960B1 EP 2744960 B1 EP2744960 B1 EP 2744960B1 EP 12742869 A EP12742869 A EP 12742869A EP 2744960 B1 EP2744960 B1 EP 2744960B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- bearing part
- bearing
- recess
- frame
- projection
- 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
Links
- 238000003780 insertion Methods 0.000 description 28
- 230000037431 insertion Effects 0.000 description 28
- 238000005553 drilling Methods 0.000 description 8
- 229910000831 Steel Inorganic materials 0.000 description 6
- 239000010959 steel Substances 0.000 description 6
- 238000003754 machining Methods 0.000 description 5
- 238000004512 die casting Methods 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 229910052782 aluminium Inorganic materials 0.000 description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 238000010079 rubber tapping Methods 0.000 description 2
- 229910052725 zinc Inorganic materials 0.000 description 2
- 239000011701 zinc Substances 0.000 description 2
- 238000004873 anchoring Methods 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 238000001746 injection moulding Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
Images
Classifications
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
- E05D5/00—Construction of single parts, e.g. the parts for attachment
- E05D5/02—Parts for attachment, e.g. flaps
- E05D5/0215—Parts for attachment, e.g. flaps for attachment to profile members or the like
- E05D5/0223—Parts for attachment, e.g. flaps for attachment to profile members or the like with parts, e.g. screws, extending through the profile wall or engaging profile grooves
- E05D5/023—Parts for attachment, e.g. flaps for attachment to profile members or the like with parts, e.g. screws, extending through the profile wall or engaging profile grooves with parts extending through the profile wall
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
- E05D5/00—Construction of single parts, e.g. the parts for attachment
- E05D5/02—Parts for attachment, e.g. flaps
- E05D5/0215—Parts for attachment, e.g. flaps for attachment to profile members or the like
- E05D5/0223—Parts for attachment, e.g. flaps for attachment to profile members or the like with parts, e.g. screws, extending through the profile wall or engaging profile grooves
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
- E05D15/00—Suspension arrangements for wings
- E05D15/48—Suspension arrangements for wings allowing alternative movements
- E05D15/52—Suspension arrangements for wings allowing alternative movements for opening about a vertical as well as a horizontal axis
- E05D15/5205—Suspension arrangements for wings allowing alternative movements for opening about a vertical as well as a horizontal axis with horizontally-extending checks
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
- E05D3/00—Hinges with pins
- E05D3/02—Hinges with pins with one pin
- E05D2003/025—Hinges with pins with one pin having three knuckles
- E05D2003/027—Hinges with pins with one pin having three knuckles the end knuckles being mutually connected
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
- E05D5/00—Construction of single parts, e.g. the parts for attachment
- E05D5/10—Pins, sockets or sleeves; Removable pins
- E05D5/14—Construction of sockets or sleeves
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
- E05D7/00—Hinges or pivots of special construction
- E05D7/10—Hinges or pivots of special construction to allow easy separation or connection of the parts at the hinge axis
- E05D7/1005—Hinges or pivots of special construction to allow easy separation or connection of the parts at the hinge axis by axially moving free pins, balls or sockets
- E05D7/1022—Hinges or pivots of special construction to allow easy separation or connection of the parts at the hinge axis by axially moving free pins, balls or sockets with snap-fitted pins
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05Y—INDEXING 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
- E05Y2600/00—Mounting or coupling arrangements for elements provided for in this subclass
- E05Y2600/50—Mounting methods; Positioning
- E05Y2600/51—Screwing or bolting
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05Y—INDEXING 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
- E05Y2800/00—Details, accessories and auxiliary operations not otherwise provided for
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05Y—INDEXING 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
- E05Y2900/00—Application of doors, windows, wings or fittings thereof
- E05Y2900/10—Application of doors, windows, wings or fittings thereof for buildings or parts thereof
- E05Y2900/13—Type of wing
- E05Y2900/132—Doors
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05Y—INDEXING 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
- E05Y2900/00—Application of doors, windows, wings or fittings thereof
- E05Y2900/10—Application of doors, windows, wings or fittings thereof for buildings or parts thereof
- E05Y2900/13—Type of wing
- E05Y2900/148—Windows
Definitions
- the invention relates to a bearing part according to the preamble of claim 1.
- the bearing part can be used as a band for doors, windows or the like.
- the bearing survey is preferably formed in this case as a socket for receiving a hinge pin or a bolt.
- the stock collection can also be a head start in the form of a hinge pin or the like for connection to a socket of the band member.
- the bearing parts are often exposed to high stress. For example, if bearing parts are used to mount a sash on a frame, the sash exerts a high force on the bearing part. At the same time it is difficult to firmly and reliably connect the bearing part with the frame or wing, as they are often made of plastic or aluminum. Fasteners, such as screws, are often torn out of the frame or wing in these frames or wings. The longitudinal axis of the through-hole is therefore formed obliquely to the plant side, to allow a rear grip of the connecting means to the frame or wing.
- a hinge which has a bearing part with a bearing elevation which is encompassed by a projection of a hinge part.
- the bearing part has three through-holes, of which at least one through-hole is aligned obliquely to the contact side of the bearing part.
- a screw is passed through this through-hole to secure the bearing part.
- the passage recess is opposite to the bearing survey intended. In the case of a load on the hinge therefore there is a risk that the screw is torn out by the levers acting on the bearing part.
- a tape for doors, windows and the like which has a bearing elevation, in which a bolt of a band part is guided.
- an oblique through-hole is provided in order to be able to arrange a bolt having a screw head for fastening the bearing part as close as possible to the bearing elevation.
- the CH 242 554 A discloses a hinge which is secured with a mandrel extending obliquely to the hinge axis.
- a mandrel extending obliquely to the hinge axis.
- For secure attachment of the mandrel is threaded or countered by other securing means.
- the attachment of the hinge is therefore correspondingly expensive.
- a similar hinge is also from the DE 912 902 B as well as the DE 197 48 418 A1 known.
- the disclosure CH 276 647 A a hinge with an obliquely insertable into a wing or frame mandrel.
- the spike is countered by a nail in the wing or frame.
- the attachment therefore requires a certain effort.
- the known fitting part arrangement has a bearing part with a recess into which a pivot pin of a hinge part is receivable.
- the disclosure EP 0 448 907 A1 a hinge arrangement for the door of a control cabinet.
- the hinge arrangement has a bearing part with a contact surface.
- a screw of the bearing part is obliquely introduced to the contact surface in the bearing part.
- a tape according to the preamble of claim 1 has become known, which has a plurality of passage recesses.
- the passage recesses extend obliquely to the contact surface of the band.
- the passage recesses have on their side facing away from the contact surface on an enlarged opening for receiving a screw head.
- the DE 69 39 409 U discloses a hinge strap for securing a metal profile.
- the hinge has obliquely to the contact surface of the hinge strip extending screw pins with a tapered tip.
- a hinge which has projections, wherein in each case a screw can be guided through the projections in order to fasten the hinge to a door.
- the screw fastening comprises a fitting part with a contact surface and a through-hole for guiding a fastening screw.
- the passage recess extends at an angle of 30 ° to 60 ° to the normal direction of the contact surface.
- the invention is based on the object to provide a bearing part that can be firmly connected to a structurally particularly simple manner with a wing or frame and the weight of the wing is produced.
- a connecting means such as in particular a screw can be performed by the oblique through-hole in the bearing elevation and inserted into the frame or wing.
- the connecting means engages in this way the surface of the frame or wing and allows a connection to the frame or wing, which is as close as possible to the point of connection to the band part.
- the through-hole is additionally extended by the bearing survey, whereby a better adhesion between the bearing part and frame or wing is made possible via the connecting element.
- the passage recess preferably has a round cross-section.
- the round cross section is optimally able to receive a screw or a similar connecting means with a round cross section.
- the through-hole is provided in the region of a longitudinal end of the bearing part.
- the longitudinal axis of the passage recess is preferably formed at an angle of 30 ° to 60 °, in particular at an angle of 45 ° to the contact side.
- the connecting means introduced into the through-hole does not strike a steel profile arranged in the frame or wing, so that pre-drilling in the frame or wing for the connection means is unnecessary.
- the obliquely inserted connecting means engages behind a large area of the frame or wing, so that the risk of tearing the connecting means is minimized.
- a projection in particular a round cross-section pin, be formed on the plant side.
- the projection is insertable into a recess on the frame or wing.
- the projection thereby enables a positive and / or non-positive connection between the bearing part and the frame or wing.
- the passage recess preferably extends at least partially in the projection.
- a, in particular continuous, projection recess can be provided on the projection, which is aligned with the passage recess. This allows a particularly long through-hole.
- the connecting means can be guided so well.
- a pilot hole for the connecting means on the frame or wing is not necessary. Rather, a self-tapping screw can be used as a connecting means, which is optimally guided due to the long through-hole.
- At least one connecting opening may be provided on the bearing part, the longitudinal axis of which is formed perpendicular to the contact side. Through the connection opening, a further connecting means can be introduced, which strengthens the connection between the bearing part and the frame or wing.
- the angle between the longitudinal axes of the connecting means inserted through the through-hole and the connecting means inserted through the connecting hole is preferably 45 °.
- connection opening preferably has a round cross section.
- a cross-sectionally round connecting means such as a nail or a screw can be used.
- connection opening may be slightly smaller than the cross section of a projection which is to be held by a press fit in the frame or wing.
- frame or wing holes of the same diameter can be drilled in this case for fixing the bearing part, wherein a hole for receiving the guided through the connection opening connecting means and a further hole for receiving the projection.
- a drill change during assembly of the bearing part is made unnecessary by the need of holes of the same diameter.
- connection openings For particularly secure attachment of the bearing part a plurality of connection openings are preferably provided.
- the longitudinal axes of these connection openings and the longitudinal axes of all projections provided on the bearing part preferably intersect a straight line which runs in particular parallel to the longitudinal axis of the bearing part.
- drilling units i. standardized drilling tools with equidistant drills or drilling templates.
- a uniform force transmission from the bearing part to the wing or frame can be achieved in that projections and / or connection openings are equidistant.
- the longitudinal axis of the passage recess preferably points away from the longitudinal axis of the connection opening in the direction of insertion of the connection means.
- the connecting means inserted into the through-hole can hereby engage behind a region of the surface of the frame or wing which lies outside the contact side of the bearing part. As a result, a large-area connection of the bearing part is made possible with the frame or wing. The on the bearing part As a result, attacking forces can be diverted particularly well into the frame or wing.
- the connecting means should not be visually visible for aesthetic reasons. Furthermore, bearing parts are often over-painted, the connecting means should not be swept over.
- the known bearing parts therefore have a cap or the like for covering the connecting means for the connecting means. However, such a cap can be damaged, fall off, scratched or lost.
- the through-hole therefore preferably has an enlarged cross-section on its opening facing away from the contact side. In this way, a widened end of the connecting means can be inserted into the through-hole and thereby be arranged completely in the through-hole. Due to the oblique alignment of the through hole, the connecting means is covered by the bearing survey and thus not visible from the outside.
- the bearing part is formed symmetrically to a central plane of symmetry, which is perpendicular to the system side and perpendicular to the longitudinal side of the bearing part.
- the bearing part is thus suitable for a left and right stop. Furthermore, care must be taken during the assembly of the bearing part on the orientation of the bearing part.
- the bearing part can be fixed by a fitter with little effort.
- two passage recesses are provided at the two longitudinal end portions of the bearing part.
- the longitudinal axes of the passage recesses are preferably substantially perpendicular to each other. This will be an optimal Connection between the bearing part and the wing or the frame allows.
- the bearing part on two bearing surveys in which aligned alignment bolt receptacles are provided.
- the mutually aligned bolt receptacles allow secure two-sided support of a bolt for connecting the bearing part with the band part.
- the bearing part can have at least one roller trough. This can serve to receive a roll of the band part surrounding a pin of the band part. The load of the wing can be so well supported.
- the bearing part is thereby formed in the form of a roller bearing part.
- At least one connection opening can be formed in the roller recess.
- a bolt and / or a roller of the band part can hide the roller recess. As a result, an inserted into the connection opening connecting means to the outside is invisible.
- the bearing part may be formed in one piece. Furthermore, the bearing part is preferably made of steel or manufactured as a die-cast part. As a result, the production costs and production costs can be significantly reduced.
- the bearing part has at least one insertion part in the region of a bearing elevation.
- a bearing part body of the bearing part in a metal die-casting process for example, a zinc die-casting process
- a machining (post) machining By means of the insertion part can still be a part a bolt head seat are formed for a connecting means in the form of a screw.
- the bearing part preferably has in each case an insertion part in the area of both bearing elevations.
- the insertion part can be made of plastic.
- At least one insertion part in particular both insertion parts, may be insertable in the longitudinal direction into the bearing part body.
- the bearing part body can thereby be produced in an injection molding or die-casting process, wherein in the longitudinal direction a through-hole can be provided in at least one bearing elevation for receiving a bolt for connection to the band part. At least one open end of the through-hole can then be closed by the insertion part.
- both insertion parts one, in particular continuous, recess may be provided for receiving the bolt.
- the bolt can thereby be held securely in the bearing part.
- at least one insertion part can have a latching nose for securing the bolt.
- a groove extending around the outer surface of the bolt, it can lock in any rotational position of the bolt with the locking lug.
- both insertion parts each have a recess for receiving the bolt and a latching lug.
- At least one obliquely aligned to the contact side or trained fürgangsaus principleung of the bearing part is at least partially formed by a Einschubteilausnaturalung.
- the through-hole without machining (re) machining, in particular without drilling or milling, produced.
- the Through-hole for example, by two half-shell-shaped recesses, one of which is formed by the EinschubteilausEnglishung be prepared.
- both insertion parts each have at least one insertion part recess for the formation of passage recesses of the bearing part provided obliquely to the abutment side.
- the invention further relates to a window, a door or the like with a bearing part described above.
- a first non-inventive bearing part 10 is in FIG. 1a shown.
- the bearing part 10 is mounted on a profile of a frame 14 by four connecting means 12a-d.
- the bearing part 10 is formed in the form of a roller bearing part.
- a band member is held on the bearing member 10 by a bolt (both not shown).
- the bearing part 10 has two bolt receptacles 16a, 16b.
- the bearing part 10 serves for the pivotal connection of a wing and a fixed frame of a window, a door or the like and absorbs the weight of a wing.
- the weight of the wing is in FIG. 1a represented by an arrow 18. Due to the weight of the wing, the connecting means 12b-d are subjected to shear. The connecting means 12b-d are screwed into a steel profile 20 of the frame 14.
- the frame 14 has in addition to the steel profile 20 exclusively plastic or aluminum elements. Further connecting means, which are introduced in the manner of the connecting means 12b-d in plastic or aluminum elements of the frame 14, therefore, tend to "tearing" by the weight of the wing. Furthermore, when screwed in, such connecting means tend to "spin" by applying high torques.
- a first through-passage 22a is therefore provided in the bearing part 10.
- the first through-hole 22a is aligned obliquely to a contact side 24 of the bearing part 10.
- the through-passage 22a is formed at 45 ° to the contact side 24.
- the inserted into the through-hole 22a connecting means 12a can thereby absorb the tensile forces on the bearing part 10 optimally.
- a second through-hole 22b is provided in the first through-passage 22a opposite longitudinal end portion of the bearing part 10. By introducing another connecting means (not shown) into the second through-hole 22b, the connection between the bearing part 10 and the frame 14 can be further strengthened.
- the passage recesses 22a, b extend at least partially into bearing elevations 25a, b.
- Connecting means introduced into the passage openings 22a, b, for example the first connection means 12a, can thereby be arranged as close as possible in the area of the bolt receptacles 16a, b.
- a very secure connection between the bearing part 10 and the frame 14 is achieved.
- the on the Bearing part 10 on the bolt receivers 16a, b acting leverage forces are minimized.
- the bearing part 10 also has two projections 26a, 26b, which are materially formed on the bearing part 10. Due to the formation of the projections 26a, 26b, a particularly secure connection between the bearing part 10 and the frame 14 is made possible.
- the passage recesses 22a, 22b are partially passed through the projections 26a, 26b.
- the passage recesses 22a, 22b are thereby formed particularly long.
- In the through holes 22a, 22b introduced connecting means, for example, the first connecting means 12a, are thereby performed by the bearing part 10 well.
- no holes for the connection means for example, the first connection means 12a, which are inserted into the through-holes 22a, 22b, need not be drilled in the frame 14.
- Connection openings 28a-c for receiving the connection means 12b-d are made relatively short.
- the connecting openings 28a-c are round in cross-section.
- the projections 26a, 26b in cross-section are substantially round.
- the diameter of the cross section of the projections 26a, 26b is selected so that for receiving the projections 26a, 26b bores of the same diameter in the in FIG. 1b not shown profile can be provided as needed for the connecting means 12b-d.
- the projections 26a, 26b have longitudinal axes 30a, 30b.
- the passage recesses 28a, 28b, 28c have longitudinal axes 32a-c.
- the Longitudinal axes 30a, 30b, 32a-c intersect a straight line, not shown, which runs parallel to the longitudinal axis of the bearing part 10.
- the distance between the longitudinal axes 30a and 32a and between the longitudinal axes 32a and 32b and between the longitudinal axes 32b and 32c and between the longitudinal axes 32c and 30b is the same.
- a drilling device with five drills of the same diameter can be used, which are introduced into the profile along the longitudinal axes 30a, b, 32a-c.
- a drilling template may be used in which the spacing of the bores corresponds to the spacing of the longitudinal axes 30a, b, 32a-c.
- the bearing part 10 is formed symmetrically to a plane of symmetry 34 which is perpendicular to the contact side 24 and perpendicular to the longitudinal direction of the bearing part 10.
- the partially sectioned illustration of the bearing part 10 in Figure 1c It can be seen that the first connecting means 12a is arranged completely in the first through-hole 22a.
- the through-passage 22a has an enlarged cross-section in the visible, opposite to the plant side opening.
- the head of the connecting means 12a can be completely inserted into the through-hole 22a. Therefore, no cap or the like is required to cover the first connecting means 12a to the outside.
- the connecting means 12b-d are concealed in the assembled state of the wing by the bolt of the band member (not shown). Also for the protection of the connecting means 12b-d are therefore no caps or the like necessary.
- FIG. 2 shows a Scherenarmlager 36 with another non-inventive bearing part 10 '.
- a band member 38 in the form of a scissor arm serves to expose a wing (not shown).
- the bearing part 10 ' has through holes 22a', 22b '. Longitudinal axes 40a, 40b of the passage recesses 22a ', 22b' intersect at a right angle.
- On bearing part 10 'attacking forces can be particularly well derived in the frame.
- the bearing part 10 ' has bearing elevations 25a', 25b ', in which mutually aligned bolt receivers 16a', 16b 'are formed.
- a bolt 42 of the band member 38 is guided in the bolt receivers 16a ', 16b'. Between the bearing elevations 25a ', 25b' is centrally a roller trough 44 is provided. In the roller trough 44, a roller 46, which is arranged on the bolt 42, rotate.
- the passage recesses 22a ', 22b' extend at least partially in the bearing elevations 25a ', 25b'.
- guided connection means such as a connecting means 12a 'very well managed.
- An inventive bearing part 10 is in a sectional side view in FIG. 3a shown.
- the bearing part 10 has a bearing part body 48 and two insertion parts 50a, 50b in the region of two bearing elevations 25a", 25b.
- the bearing part body 48 can be produced in a zinc die-casting process without cutting (FIG. Post-) machining become.
- the insertion parts 50a, 50b are introduced into the bearing part body 48 in the longitudinal direction of the bearing part 10 ".
- the insertion parts 50a, 50b further comprise continuous recesses 52a, 52b, in which a bolt 54 is inserted for pivotally connecting a belt part, not shown.
- this has two annular grooves 56a, 56b.
- annular grooves 56a, 56b In the annular grooves 56a, 56b locking lugs 58a, 58b of the insertion parts 50a, 50b for securing the bolt 54 are inserted.
- FIG. 3b A perspective view of the insertion part 50b is shown in FIG. 3b shown. It can be seen here that the insertion part 50b forms part of a screw head seat 60.
- the screw head seat 60 in this case represents a part of the insertion part recess 51b.
- the insertion part 50b is finally in a sectional view in Figure 3c shown. It can be seen that the latching nose 58b is part of an elastic web 62. The web 62 is formed on the one-piece insertion part 50b.
- the latching nose 58b is displaced in the direction of arrow 64 and then locked in the groove 56b (see FIG. 3a ).
- the detent 50b can be omitted on a spring ring for securing the bolt 54, as used in the prior art.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Hinges (AREA)
Description
Die Erfindung betrifft ein Lagerteil nach dem Oberbegriff des Anspruchs 1.The invention relates to a bearing part according to the preamble of claim 1.
Es ist bekannt, Lagerteile an Fensterrahmen oder Türrahmen bzw. Fensterflügeln oder Türflügeln zur Befestigung des Flügels an dem Rahmen einzusetzen. Das Lagerteil kann dabei als Band für Türen, Fenster oder dergleichen eingesetzt werden. Die Lagererhebung ist in diesem Fall vorzugsweise als Buchse zur Aufnahme eines Bandzapfens oder eines Bolzens ausgebildet. Die Lagererhebung kann aber auch einen Vorsprung in Form eines Bandzapfens oder dergleichen zur Verbindung mit einer Buchse des Bandteils aufweisen.It is known to use bearing parts on window frames or door frames or sashes or door wings for attaching the sash to the frame. The bearing part can be used as a band for doors, windows or the like. The bearing survey is preferably formed in this case as a socket for receiving a hinge pin or a bolt. The stock collection can also be a head start in the form of a hinge pin or the like for connection to a socket of the band member.
Die Lagerteile sind oftmals einer hohen Beanspruchung ausgesetzt. Werden Lagerteile beispielsweise zur Lagerung eines Flügels an einem Rahmen eingesetzt, übt der Flügel eine hohe Kraft auf das Lagerteil aus. Gleichzeitig ist es schwierig, das Lagerteil fest und zuverlässig mit dem Rahmen oder Flügel zu verbinden, da diese oftmals aus Kunststoff oder Aluminium gefertigt sind. Verbindungselemente, wie beispielsweise Schrauben, werden bei diesen Rahmen oder Flügeln dabei oftmals aus dem Rahmen oder Flügel herausgerissen. Die Längsachse der Durchgangsausnehmung wird daher schräg zur Anlageseite ausgebildet, um einen Hintergriff des Verbindungsmittels an dem Rahmen oder Flügel zu ermöglichen. Trotzdem kommt es immer wieder vor, dass die Verbindungsmittel aufgrund der von dem Verbindungsmittel distanzierten Lagererhebung und den dadurch entstehenden Hebelkräften bei hohen Belastungen aus dem Flügel oder Rahmen herausgezogen werden, insbesondere wenn das Lagerteil und das Bandteil Elemente eines Scherenarmlagers darstellen, durch das ein Flügel ausgestellt wird. Weiterhin ist eine sichere Befestigung des Lagerteils an im Rahmen oder Flügel vorgesehenen Stahlprofilen nur beschränkt möglich, da solche Stahlprofile nicht bis in die Gehrung des Rahmens oder Flügels ragen.The bearing parts are often exposed to high stress. For example, if bearing parts are used to mount a sash on a frame, the sash exerts a high force on the bearing part. At the same time it is difficult to firmly and reliably connect the bearing part with the frame or wing, as they are often made of plastic or aluminum. Fasteners, such as screws, are often torn out of the frame or wing in these frames or wings. The longitudinal axis of the through-hole is therefore formed obliquely to the plant side, to allow a rear grip of the connecting means to the frame or wing. Nevertheless, it often happens that the connecting means are pulled out due to the spaced from the connecting means bearing elevation and the resulting leverage forces at high loads from the wing or frame, especially when the bearing part and the band member represent elements of a Scherenarmlagers, exhibited by a wing becomes. Furthermore, a secure attachment of the bearing part to provided in the frame or wing steel profiles is limited, since such steel profiles do not protrude into the miter of the frame or wing.
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Der Erfindung liegt demgegenüber die Aufgabe zu Grunde, ein Lagerteil bereit zu stellen, das auf konstruktiv besonders einfache Art und Weise fest mit einem Flügel oder Rahmen verbunden werden sowie die Gewichtskraft des Flügels herstellbar ist.The invention is based on the object to provide a bearing part that can be firmly connected to a structurally particularly simple manner with a wing or frame and the weight of the wing is produced.
Diese Aufgabe wird erfindungsgemäß durch ein Lagerteil gemäß Anspruch 1 gelöst.This object is achieved by a bearing part according to claim 1.
Ein Verbindungsmittel, wie insbesondere eine Schraube, können durch die schräge Durchgangsausnehmung in der Lagererhebung durchgeführt und in den Rahmen oder Flügel eingeführt werden. Das Verbindungsmittel hintergreift auf diese Art und Weise die Oberfläche des Rahmens oder Flügels und ermöglicht eine Verbindung mit dem Rahmen oder Flügel, die möglichst nahe an der Verbindungsstelle zum Bandteil liegt. Hierdurch wird eine stabile Befestigung des Lagerteils bei minimalen Hebelkräften am Rahmen oder Flügel ermöglicht. Weiterhin wird durch die Lagererhebung die Durchgangsausnehmung zusätzlich verlängert, wodurch ein besserer Kraftschluss zwischen Lagerteil und Rahmen oder Flügel über das Verbindungselement ermöglicht wird.A connecting means, such as in particular a screw can be performed by the oblique through-hole in the bearing elevation and inserted into the frame or wing. The connecting means engages in this way the surface of the frame or wing and allows a connection to the frame or wing, which is as close as possible to the point of connection to the band part. As a result, a stable attachment of the bearing part with minimal leverage on the frame or wing is possible. Furthermore, the through-hole is additionally extended by the bearing survey, whereby a better adhesion between the bearing part and frame or wing is made possible via the connecting element.
Die Durchgangsausnehmung weist vorzugsweise einen runden Querschnitt auf. Der runde Querschnitt ist dabei optimal in der Lage, eine Schraube oder ein ähnliches Verbindungsmittel mit rundem Querschnitt aufzunehmen.The passage recess preferably has a round cross-section. The round cross section is optimally able to receive a screw or a similar connecting means with a round cross section.
In bevorzugter Ausgestaltung der Erfindung ist die Durchgangsausnehmung im Bereich eines längsseitigen Endes des Lagerteils vorgesehen. Die von dem Bandteil ausgehenden Kräfte können so besonders gut in den Rahmen oder Flügel abgeleitet werden.In a preferred embodiment of the invention, the through-hole is provided in the region of a longitudinal end of the bearing part. The forces emanating from the band part can thus be diverted particularly well into the frame or wing.
Die Längsachse der Durchgangsausnehmung ist vorzugsweise in einem Winkel von 30° bis 60°, insbesondere in einem Winkel von 45°, zur Anlageseite ausgebildet. Am Lagerteil angreifende Zugkräfte können dadurch über das Verbindungsmittel besonders gut in den Rahmen oder Flügel abgeleitet werden. Weiterhin trifft das in die Durchgangsausnehmung eingeführte Verbindungsmittel nicht auf ein im Rahmen oder Flügel angeordnetes Stahlprofil, sodass sich ein Vorbohren im Rahmen oder Flügel für das Verbindungsmittel erübrigt. Schließlich hintergreift das schräg eingeführte Verbindungsmittel eine große Fläche des Rahmen oder Flügels, sodass das Risiko des Ausreißens des Verbindungsmittels minimiert wird.The longitudinal axis of the passage recess is preferably formed at an angle of 30 ° to 60 °, in particular at an angle of 45 ° to the contact side. On the bearing part attacking tensile forces can be particularly well derived via the connecting means in the frame or wing. Furthermore, the connecting means introduced into the through-hole does not strike a steel profile arranged in the frame or wing, so that pre-drilling in the frame or wing for the connection means is unnecessary. Finally, the obliquely inserted connecting means engages behind a large area of the frame or wing, so that the risk of tearing the connecting means is minimized.
An der Anlageseite kann ein Vorsprung, insbesondere ein im Querschnitt runder Zapfen, ausgebildet sein. Der Vorsprung ist dabei in eine Ausnehmung an dem Rahmen oder Flügel einführbar. Der Vorsprung ermöglicht hierdurch eine form- und/oder kraftschlüssige Verbindung zwischen dem Lagerteil und dem Rahmen oder Flügel.On the plant side, a projection, in particular a round cross-section pin, be formed. The projection is insertable into a recess on the frame or wing. The projection thereby enables a positive and / or non-positive connection between the bearing part and the frame or wing.
Die Durchgangsausnehmung verläuft vorzugsweise zumindest teilweise in dem Vorsprung. Alternativ dazu kann an dem Vorsprung eine, insbesondere durchgängige, Vorsprungsausnehmung vorgesehen sein, die mit der Durchgangsausnehmung fluchtet. Hierdurch wird eine besonders lange Durchgangsausnehmung ermöglicht. Das Verbindungsmittel kann so besonders gut geführt werden. Eine Vorbohrung für das Verbindungsmittel an dem Rahmen oder Flügel ist dadurch nicht nötig. Als Verbindungsmittel kann vielmehr eine selbstschneidende Schraube eingesetzt werden, die aufgrund der langen Durchgangsausnehmung optimal geführt wird.The passage recess preferably extends at least partially in the projection. Alternatively, a, in particular continuous, projection recess can be provided on the projection, which is aligned with the passage recess. This allows a particularly long through-hole. The connecting means can be guided so well. A pilot hole for the connecting means on the frame or wing is not necessary. Rather, a self-tapping screw can be used as a connecting means, which is optimally guided due to the long through-hole.
An dem Lagerteil kann zumindest eine Verbindungsöffnung vorgesehen sein, deren Längsachse senkrecht zur Anlageseite ausgebildet ist. Durch die Verbindungsöffnung kann ein weiteres Verbindungsmittel eingeführt werden, das die Verbindung zwischen dem Lagerteil und dem Rahmen oder Flügel verstärkt. Der Winkel zwischen den Längsachsen des durch die Durchgangsausnehmung eingeführten Verbindungsmittels und des durch die Verbindungsöffnung eingeführten Verbindungsmittels beträgt dabei vorzugsweise 45°.At least one connecting opening may be provided on the bearing part, the longitudinal axis of which is formed perpendicular to the contact side. Through the connection opening, a further connecting means can be introduced, which strengthens the connection between the bearing part and the frame or wing. The angle between the longitudinal axes of the connecting means inserted through the through-hole and the connecting means inserted through the connecting hole is preferably 45 °.
Die Verbindungsöffnung weist vorzugsweise einen runden Querschnitt auf. Hierdurch kann ein im Querschnitt rundes Verbindungsmittel, wie beispielsweise ein Nagel oder eine Schraube eingesetzt werden.The connection opening preferably has a round cross section. As a result, a cross-sectionally round connecting means, such as a nail or a screw can be used.
Der Querschnitt der Verbindungsöffnung kann etwas kleiner ausgebildet sein als der Querschnitt eines Vorsprungs, der durch eine Presspassung im Rahmen oder Flügel gehalten werden soll. In den Rahmen oder Flügel können zur Befestigung des Lagerteils in diesem Fall Löcher gleichen Durchmessers gebohrt werden, wobei ein Loch zur Aufnahme des durch die Verbindungsöffnung geführten Verbindungsmittels und ein weiteres Loch zur Aufnahme des Vorsprungs dient. Ein Bohrerwechsel bei der Montage des Lagerteils wird durch den Bedarf der Löcher gleichen Durchmessers überflüssig.The cross section of the connection opening may be slightly smaller than the cross section of a projection which is to be held by a press fit in the frame or wing. In the frame or wing holes of the same diameter can be drilled in this case for fixing the bearing part, wherein a hole for receiving the guided through the connection opening connecting means and a further hole for receiving the projection. A drill change during assembly of the bearing part is made unnecessary by the need of holes of the same diameter.
Zur besonders sicheren Befestigung des Lagerteils sind vorzugsweise mehrere Verbindungsöffnungen vorgesehen. Die Längsachsen dieser Verbindungsöffnungen und die Längsachsen aller am Lagerteil vorgesehenen Vorsprünge schneiden vorzugsweise eine Gerade, die insbesondere parallel zur Längsachse des Lagerteils verläuft. Zur Bohrung der Löcher im Flügel oder Rahmen können dadurch Bohraggregate, d.h. standardisierte Bohrwerkzeuge mit äquidistanten Bohrern oder Bohrschablonen, eingesetzt werden. Eine gleichmäßige Kraftübertragung vom Lagerteil auf den Flügel oder Rahmen kann dabei dadurch erzielt werden, dass Vorsprünge und/oder Verbindungsöffnungen äquidistant sind.For particularly secure attachment of the bearing part a plurality of connection openings are preferably provided. The longitudinal axes of these connection openings and the longitudinal axes of all projections provided on the bearing part preferably intersect a straight line which runs in particular parallel to the longitudinal axis of the bearing part. For drilling the holes in the wing or frame, drilling units, i. standardized drilling tools with equidistant drills or drilling templates. A uniform force transmission from the bearing part to the wing or frame can be achieved in that projections and / or connection openings are equidistant.
Die Längsachse der Durchgangsausnehmung weist in Einführungsrichtung des Verbindungsmittels vorzugsweise von der Längsachse der Verbindungsöffnung weg. Das in die Durchgangsausnehmung eingeführte Verbindungsmittel kann hierdurch einen Bereich der Oberfläche des Rahmens oder Flügels hintergreifen, der außerhalb der Anlageseite des Lagerteils liegt. Hierdurch wird eine großflächige Verbindung des Lagerteils mit dem Rahmen oder Flügel ermöglicht. Die am Lagerteil angreifenden Kräfte können dadurch besonders gut in den Rahmen oder Flügel abgeleitet werden.The longitudinal axis of the passage recess preferably points away from the longitudinal axis of the connection opening in the direction of insertion of the connection means. The connecting means inserted into the through-hole can hereby engage behind a region of the surface of the frame or wing which lies outside the contact side of the bearing part. As a result, a large-area connection of the bearing part is made possible with the frame or wing. The on the bearing part As a result, attacking forces can be diverted particularly well into the frame or wing.
Das Verbindungsmittel sollte aus ästhetischen Gründen optisch nicht sichtbar sein. Weiterhin werden Lagerteile oftmals überstrichen, wobei die Verbindungsmittel dabei nicht überstrichen werden sollten. Die bekannten Lagerteile weisen daher für das Verbindungsmittel eine Kappe oder dergleichen zur Abdeckung des Verbindungsmittels vor. Eine solche Kappe kann jedoch beschädigt werden, abfallen, zerkratzen oder verloren gehen. Die Durchgangsausnehmung weist daher vorzugsweise an ihrer der Anlageseite abgewandten Öffnung einen vergrößerten Querschnitt auf. Hierdurch kann ein verbreitertes Ende des Verbindungsmittels in die Durchgangsausnehmung eingeführt werden und dadurch vollständig in der Durchgangsausnehmung angeordnet werden. Durch die schräge Aufrichtung der Durchgangsausnehmung ist das Verbindungsmittel durch die Lagererhebung abgedeckt und von außen somit nicht mehr sichtbar.The connecting means should not be visually visible for aesthetic reasons. Furthermore, bearing parts are often over-painted, the connecting means should not be swept over. The known bearing parts therefore have a cap or the like for covering the connecting means for the connecting means. However, such a cap can be damaged, fall off, scratched or lost. The through-hole therefore preferably has an enlarged cross-section on its opening facing away from the contact side. In this way, a widened end of the connecting means can be inserted into the through-hole and thereby be arranged completely in the through-hole. Due to the oblique alignment of the through hole, the connecting means is covered by the bearing survey and thus not visible from the outside.
In bevorzugter Ausgestaltung der Erfindung ist das Lagerteil symmetrisch zu einer mittigen Symmetrieebene ausgebildet, die senkrecht auf der Anlageseite steht und senkrecht zur Längsseite des Lagerteils verläuft. Das Lagerteil ist dadurch für einen Links- und Rechtsanschlag geeignet. Weiterhin muss bei der Montage des Lagerteils auf die Orientierung des Lagerteils nicht geachtet werden. Das Lagerteil kann so von einem Monteur mit geringem Aufwand befestigt werden.In a preferred embodiment of the invention, the bearing part is formed symmetrically to a central plane of symmetry, which is perpendicular to the system side and perpendicular to the longitudinal side of the bearing part. The bearing part is thus suitable for a left and right stop. Furthermore, care must be taken during the assembly of the bearing part on the orientation of the bearing part. The bearing part can be fixed by a fitter with little effort.
Vorzugsweise sind zwei Durchgangsausnehmungen an den beiden längsseitigen Endbereichen des Lagerteils vorgesehen. Die Längsachsen der Durchgangsausnehmungen stehen dabei vorzugsweise im Wesentlichen senkrecht zueinander. Hierdurch wird eine optimale Verbindung zwischen dem Lagerteil und dem Flügel oder dem Rahmen ermöglicht.Preferably, two passage recesses are provided at the two longitudinal end portions of the bearing part. The longitudinal axes of the passage recesses are preferably substantially perpendicular to each other. This will be an optimal Connection between the bearing part and the wing or the frame allows.
In bevorzugter Ausgestaltung der Erfindung weist das Lagerteil zwei Lagererhebungen auf, in denen miteinander fluchtende Bolzenaufnahmen vorgesehen sind. Die zueinander fluchtenden Bolzenaufnahmen ermöglichen die sichere beidseitige Halterung eines Bolzens zur Verbindung des Lagerteils mit dem Bandteil.In a preferred embodiment of the invention, the bearing part on two bearing surveys, in which aligned alignment bolt receptacles are provided. The mutually aligned bolt receptacles allow secure two-sided support of a bolt for connecting the bearing part with the band part.
Das Lagerteil kann zumindest eine Rollenmulde aufweisen. Diese kann zur Aufnahme einer Rolle des Bandteils dienen, die einen Bolzen des Bandteils umgibt. Die Last des Flügels kann so besonders gut abgestützt werden. Das Lagerteil wird dadurch in Form einer Rollenlagerteils ausgebildet.The bearing part can have at least one roller trough. This can serve to receive a roll of the band part surrounding a pin of the band part. The load of the wing can be so well supported. The bearing part is thereby formed in the form of a roller bearing part.
In der Rollenmulde kann zumindest eine Verbindungsöffnung ausgebildet sein. Ein Bolzen und/oder eine Rolle des Bandteils können dabei die Rollenmulde verdecken. Hierdurch ist ein in die Verbindungsöffnung eingeführtes Verbindungsmittel nach außen hin unsichtbar.At least one connection opening can be formed in the roller recess. A bolt and / or a roller of the band part can hide the roller recess. As a result, an inserted into the connection opening connecting means to the outside is invisible.
Das Lagerteil kann einteilig ausgebildet sein. Ferner ist das Lagerteil vorzugsweise aus Stahl gefertigt oder als Druckguss-Teil hergestellt. Hierdurch können der Fertigungsaufwand und die Fertigungskosten maßgeblich gesenkt werden.The bearing part may be formed in one piece. Furthermore, the bearing part is preferably made of steel or manufactured as a die-cast part. As a result, the production costs and production costs can be significantly reduced.
Das Lagerteil weist im Bereich einer Lagererhebung zumindest ein Einschubteil auf. Durch das Einschubteil kann ein Lagerteilkörper des Lagerteils in einem Metall-Druckgussverfahren, beispielsweise einem Zink-Druckgussverfahren, hergestellt werden, wobei auf eine spanende (Nach-) Bearbeitung verzichtet werden kann. Mittels des Einschubteils kann weiterhin ein Teil eines Schraubenkopfsitzes für ein Verbindungsmittel in Form einer Schraube ausgebildet werden. Das Lagerteil weist vorzugsweise im Bereich beider Lagererhebungen jeweils ein Einschubteil auf.The bearing part has at least one insertion part in the region of a bearing elevation. Through the insertion part, a bearing part body of the bearing part in a metal die-casting process, for example, a zinc die-casting process, can be produced, can be dispensed with a machining (post) machining. By means of the insertion part can still be a part a bolt head seat are formed for a connecting means in the form of a screw. The bearing part preferably has in each case an insertion part in the area of both bearing elevations.
Zur besonders kostengünstigen Fertigung des Lagerteils kann das Einschubteil aus Kunststoff gefertigt sein.For particularly cost-effective production of the bearing part, the insertion part can be made of plastic.
Zumindest ein Einschubteil, insbesondere beide Einschubteile, können in Längsrichtung in den Lagerteilkörper einführbar sein. Der Lagerteilkörper kann dadurch in einem Spritzguss- oder Druckgussverfahren hergestellt werden, wobei in Längsrichtung eine Durchgangsausnehmung in zumindest einer Lagererhebung zur Aufnahme eines Bolzens zur Verbindung mit dem Bandteil vorgesehen sein kann. Zumindest ein offenes Ende der Durchgangsausnehmung kann anschließend durch das Einschubteil verschlossen werden.At least one insertion part, in particular both insertion parts, may be insertable in the longitudinal direction into the bearing part body. The bearing part body can thereby be produced in an injection molding or die-casting process, wherein in the longitudinal direction a through-hole can be provided in at least one bearing elevation for receiving a bolt for connection to the band part. At least one open end of the through-hole can then be closed by the insertion part.
In einem oder beiden Einschubteilen kann jeweils eine, insbesondere durchgängige, Ausnehmung zur Aufnahme des Bolzens vorgesehen sein. Der Bolzen kann hierdurch sicher im Lagerteil gehalten werden. Weiterhin kann zumindest ein Einschubteil eine Rastnase zur Sicherung des Bolzens aufweisen. Im Falle einer rund um die Außenfläche verlaufenden Nut des Bolzens, kann diese in jeder beliebigen Drehstellung des Bolzens mit der Rastnase verrasten. Vorzugsweise weisen beide Einschubteile jeweils eine Ausnehmung zur Aufnahme des Bolzens sowie eine Rastnase auf.In one or both insertion parts one, in particular continuous, recess may be provided for receiving the bolt. The bolt can thereby be held securely in the bearing part. Furthermore, at least one insertion part can have a latching nose for securing the bolt. In the case of a groove extending around the outer surface of the bolt, it can lock in any rotational position of the bolt with the locking lug. Preferably, both insertion parts each have a recess for receiving the bolt and a latching lug.
Zumindest eine schräg zur Anlageseite ausgerichtete bzw. ausgebildete Durchgangsausnehmung des Lagerteils wird zumindest teilweise von einer Einschubteilausnehmung ausgebildet. Hierdurch ist die Durchgangsausnehmung ohne spanende (Nach-) Bearbeitung, insbesondere ohne Bohren oder Fräsen, herstellbar. Die Durchgangsausnehmung kann beispielsweise durch zwei halbschalenförmige Ausnehmungen, von denen eine durch die Einschubteilausnehmung ausgebildet wird, hergestellt werden. Vorzugsweise weisen beide Einschubteile jeweils zumindest eine Einschubteilausnehmung zur Ausbildung von schräg zur Anlageseite vorgesehenen Durchgangsausnehmungen des Lagerteils auf.At least one obliquely aligned to the contact side or trained Durchgangsausnehmung of the bearing part is at least partially formed by a Einschubteilausnehmung. As a result, the through-hole without machining (re) machining, in particular without drilling or milling, produced. The Through-hole, for example, by two half-shell-shaped recesses, one of which is formed by the Einschubteilausnehmung be prepared. Preferably, both insertion parts each have at least one insertion part recess for the formation of passage recesses of the bearing part provided obliquely to the abutment side.
Die Erfindung betrifft weiterhin ein Fenster, eine Tür oder dergleichen mit einem zuvor beschriebenen Lagerteil.The invention further relates to a window, a door or the like with a bearing part described above.
Weitere Merkmale und Vorteile der Erfindung ergeben sich aus der nachfolgenden detaillieren Beschreibung von Ausführungsbeispielen der Erfindung, anhand der Figuren der Zeichnung, die erfindungswesentliche Einzelheiten zeigt, sowie aus den Ansprüchen. Die dort gezeigten Merkmale sind nicht notwendig maßstäblich zu verstehen und derart dargestellt, dass die erfindungsgemäßen Besonderheiten deutlich sichtbar gemacht werden können. Die verschiedenen Merkmale können je einzeln für sich oder zu mehreren in beliebigen Kombinationen bei Varianten der Erfindung verwirklicht sein.Further features and advantages of the invention will become apparent from the following detailed description of embodiments of the invention, with reference to the figures of the drawing, which shows details essential to the invention, and from the claims. The features shown there are not necessarily to scale and presented in such a way that the features of the invention can be made clearly visible. The various features may be implemented individually for themselves or for a plurality of combinations in variants of the invention.
In der schematischen Zeichnung sind drei Ausführungsbeispiele der Lagerteile in verschiedenen Stadien der Benutzung dargestellt und in der nachfolgenden Beschreibung näher erläutert.In the schematic drawing three embodiments of the bearing parts are shown in various stages of use and explained in more detail in the following description.
Es zeigen:
- Figur 1a
- eine geschnittene Darstellung eines nicht erfindungsgemäßen Lagerteils, das an einem Rahmen montiert ist;
- Figur 1b
- das Lagerteil aus
Figur 1a in einer Seitenansicht; - Figur 1c
- eine teilweise geschnittene Ansicht der Anordnung aus
Figur 1a entlang der Linie C-C; - Figur 2
- eine geschnittene Darstellung eines zweiten, nicht erfindungsgemäßen Ausführungsbeispiels eines Lagerteils;
- Figur 3a
- eine geschnittene Darstellung eines erfindungsgemäßen Ausführungsbeispiels eines Lagerteils;
- Figur 3b
- eine perspektivische Ansicht eines Einschubteils des Lagerteils gemäß
Figur 3a ; und - Figur 3c
- eine geschnittene Seitenansicht des Einschubteils aus
Figur 3b .
- FIG. 1a
- a sectional view of a non-inventive bearing part, which is mounted on a frame;
- FIG. 1b
- the bearing part
FIG. 1a in a side view; - Figure 1c
- a partially sectioned view of the arrangement
FIG. 1a along the line CC; - FIG. 2
- a sectional view of a second, non-inventive embodiment of a bearing part;
- FIG. 3a
- a sectional view of an embodiment of a bearing part according to the invention;
- FIG. 3b
- a perspective view of an insertion part of the bearing part according to
FIG. 3a ; and - Figure 3c
- a sectional side view of the insertion part
FIG. 3b ,
Ein erstes nicht erfindungsgemäßes Lagerteil 10 ist in
Das Lagerteil 10 dient der schwenkbaren Verbindung eines Flügels und eines festen Rahmens eines Fensters, einer Tür oder dergleichen und nimmt das Gewicht eines Flügels auf. Die Gewichtskraft des Flügels ist in
Der Rahmen 14 weist neben dem Stahlprofil 20 ausschließlich Kunststoff oder Aluminiumelemente auf. Weitere Verbindungsmittel, die in Art und Weise der Verbindungsmittel 12b-d in Kunststoff- bzw. Aluminiumelemente des Rahmens 14 eingebracht werden, neigen daher zum "Ausreißen" durch die Gewichtskraft des Flügels. Weiterhin tendieren solche Verbindungsmittel beim Einschrauben zu einem "Durchdrehen" durch das Anlegen hoher Drehmomente.The
Zur besseren Befestigung des Lagerteils 10 am Rahmen 14 ist daher in dem Lagerteil 10 eine erste Durchgangsausnehmung 22a vorgesehen. Die erste Durchgangsausnehmung 22a ist schräg zu einer Anlageseite 24 des Lagerteils 10 ausgerichtet. Im vorliegenden Fall ist die Durchgangsausnehmung 22a unter 45° zur Anlageseite 24 ausgebildet. Das in die Durchgangsausnehmung 22a eingeführte Verbindungsmittel 12a kann dadurch die Zugkräfte auf das Lagerteil 10 optimal aufnehmen. In dem der ersten Durchgangsausnehmung 22a gegenüberliegenden längsseitigen Endbereich des Lagerteils 10 ist eine zweite Durchgangsausnehmung 22b vorgesehen. Durch Einführung eines weiteren Verbindungsmittels (nicht gezeigt) in die zweite Durchgangsausnehmung 22b kann die Verbindung zwischen dem Lagerteil 10 und dem Rahmen 14 weiter verstärkt werden.For better attachment of the bearing
Die Durchgangsausnehmungen 22a, b verlaufen zumindest teilweise in Lagererhebungen 25a, b. In die Durchgangsausnehmungen 22a, b eingeführte Verbindungsmittel, beispielsweise das erste Verbindungsmittel 12a, können dadurch so nah wie möglich im Bereich der Bolzenaufnahmen 16a, b angeordnet werden. Hierdurch wird eine sehr sichere Verbindung zwischen dem Lagerteil 10 und dem Rahmen 14 erzielt. Die auf das Lagerteil 10 über die Bolzenaufnahmen 16a, b wirkenden Hebelkräfte werden minimiert.The passage recesses 22a, b extend at least partially into bearing
Das Lagerteil 10 weist weiterhin zwei Vorsprünge 26a, 26b auf, die materialschlüssig am Lagerteil 10 ausgebildet sind. Durch die Ausbildung der Vorsprünge 26a, 26b wird eine besonders sichere Verbindung zwischen dem Lagerteil 10 und dem Rahmen 14 ermöglicht. Die Durchgangsausnehmungen 22a, 22b sind teilweise durch die Vorsprünge 26a, 26b hindurchgeführt. Die Durchgangsausnehmungen 22a, 22b sind dadurch besonders lang ausgebildet. In die Durchgangsausnehmungen 22a, 22b eingeführte Verbindungsmittel, beispielsweise das erste Verbindungsmittel 12a, werden dadurch von dem Lagerteil 10 gut geführt. Trotz der Schräge der Durchgangsausnehmungen 22a, 22b müssen dadurch keine Löcher für die Verbindungsmittel, beispielsweise das erste Verbindungsmittel 12a, die in die Durchgangsausnehmungen 22a, 22b eingeführt werden, in den Rahmen 14 gebohrt werden. Stattdessen können selbstschneidende Verbindungsmittel eingesetzt werden. Verbindungsöffnungen 28a-c zur Aufnahme der Verbindungsmittel 12b-d sind demgegenüber verhältnismäßig kurz ausgeführt. Zur optimalen Führung der Verbindungsmittel 12b-d sind die Verbindungsöffnungen 28a-c im Querschnitt rund ausgeführt.The bearing
Wie aus
Um das Lagerteil 10 sowohl für Links- als auch Rechtsanschlag einsetzen zu können, ist das Lagerteil 10 symmetrisch zu einer Symmetrieebene 34 ausgebildet, die senkrecht auf der Anlageseite 24 und senkrecht zur Längsrichtung des Lagerteils 10 verläuft.In order to use the bearing
Der teilweise geschnittenen Darstellung des Lagerteils 10 in
Ein Bolzen 42 des Bandteils 38 wird in den Bolzenaufnahmen 16a', 16b' geführt. Zwischen den Lagererhebungen 25a', 25b' ist mittig eine Rollenmulde 44 vorgesehen. In der Rollenmulde 44 kann eine Rolle 46, die auf dem Bolzen 42 angeordnet ist, drehen.A
Die Durchgangsausnehmungen 22a', 22b' verlaufen zumindest teilweise in den Lagererhebungen 25a', 25b'. Hierdurch werden in den Durchgangsausnehmungen 22a', 22b' geführte Verbindungsmittel, beispielsweise ein Verbindungsmittel 12a' besonders gut geführt.The passage recesses 22a ', 22b' extend at least partially in the
Ein erfindungsgemäßes Lagerteil 10" ist in einer geschnittenen Seitenansicht in
Schräg zur Anlageseite 24' vorgesehene Durchgangsausnehmungen 22a", 22b" des Lagerteils 10" werden teilweise von im Wesentlichen halbschalenförmigen Einschubteilausnehmungen 51a, 51b ausgebildet. Hierdurch wird eine stark vereinfachte Fertigung der Durchgangsausnehmungen 22a", 22b" ermöglicht.Through
Die Einschubteile 50a, 50b weisen weiterhin durchgängige Ausnehmungen 52a, 52b auf, in die ein Bolzen 54 zur schwenkbaren Verbindung eines nicht dargestellten Bandteils eingeführt ist. Zur Verankerung des Bolzens 54 weist dieser zwei Ringnuten 56a, 56b auf. In die Ringnuten 56a, 56b sind Rastnasen 58a, 58b der Einschubteile 50a, 50b zur Sicherung des Bolzens 54 eingeführt.The
Eine perspektivische Darstellung des Einschubteils 50b ist in
Das Einschubteil 50b ist schließlich in einer Schnittdarstellung in
Claims (11)
- Bearing part (10") for a frame (14) or a leaf of a window, a door or the like, which can be placed at an abutment face (24') of the bearing part (10") on the frame (14) or leaf, wherein the bearing part (10") has at least one bearing projection (25a", 25b") for connecting the bearing part (10") to a hinge part (38) and the bearing part (10") has at least one through recess (22a", 22b") into which a connecting means for connecting the bearing part (10") to the frame (14) or leaf can be inserted, wherein the longitudinal axis of the through recess (22a", 22b") is oriented obliquely with respect to the abutment face (24'), wherein the through recess (22a", 22b") extends at least in part in the bearing projection (25a", 25b"), wherein the bearing part (10") has at least one slide-in part (50a, 50b) in the region of one bearing projection (25a", 25b"), in particular in the region of two bearing projections (25a", 25b"), characterised in that the at least one through recess (22a", 22b") oriented or formed obliquely with respect to the abutment face (24') is formed at least in part by a slide-in part recess (51 a, 51 b).
- Bearing part according to claim 1, characterised in that the longitudinal axis of the through recess (22a", 22b") is formed at an angle of from 30° to 60°, in particular of 45°, with respect to the abutment face (24').
- Bearing part according to claim 1 or 2, characterised in that a projection (26a, 26b), in particular a pin having a round cross-section, is formed on the abutment face (24').
- Bearing part according to claim 3, characterised in that the through recess (22a", 22b") extends at least in part in the projection (26a, 26b) or there is provided on the projection (26a, 26b) a projection recess, in particular a continuous projection recess, which is in alignment with the through recess (22a", 22b").
- Bearing part according to any one of the preceding claims, characterised in that there is provided on the bearing part (10") at least one connecting opening, the longitudinal axis of which is perpendicular to the abutment face (24').
- Bearing part according to any one of the preceding claims, characterised in that the through recess (22a", 22b") has an enlarged cross-section at its opening remote from the abutment face (24').
- Bearing part according to any one of the preceding claims, characterised in that it is formed symmetrically with respect to a central plane of symmetry (34) which is perpendicular on the abutment face (24') and extends perpendicularly to the long side of the bearing part (10").
- Bearing part according to any one of the preceding claims, characterised in that it has two bearing projections (25a", 25b") in which mutually aligned bolt receivers are provided.
- Bearing part according to any one of the preceding claims, characterised in that it has at least one roller trough.
- Bearing part according to any one of the preceding claims, characterised in that at least one slide-in part (50a, 50b) can be inserted in the length direction of the bearing part (10") into a bearing part body (48) of the bearing part (10").
- Window, door or the like having a bearing part (10") according to any one of the preceding claims.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL12742869T PL2744960T3 (en) | 2011-08-19 | 2012-07-26 | Bearing part of a window, door or similar |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102011081284A DE102011081284B3 (en) | 2011-08-19 | 2011-08-19 | Bearing part of a window, a door or the like |
PCT/EP2012/064660 WO2013026648A1 (en) | 2011-08-19 | 2012-07-26 | Bearing part of a window, door or similar |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2744960A1 EP2744960A1 (en) | 2014-06-25 |
EP2744960B1 true EP2744960B1 (en) | 2015-09-09 |
Family
ID=46603937
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP12742869.6A Active EP2744960B1 (en) | 2011-08-19 | 2012-07-26 | Bearing part of a window, door or similar |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP2744960B1 (en) |
DE (1) | DE102011081284B3 (en) |
PL (1) | PL2744960T3 (en) |
WO (1) | WO2013026648A1 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102020100411B3 (en) * | 2020-01-10 | 2021-02-11 | Dr. Hahn Gmbh & Co. Kg | Hinge flaps of a hinge for the hinge-joint connection of a wing profile with a frame profile and such a hinge |
DE102020102026A1 (en) | 2020-01-28 | 2021-07-29 | Hautau Gmbh | sliding door |
DE102022105163A1 (en) * | 2022-03-04 | 2023-09-07 | ELRAM Baubeschläge GmbH | Hinged strap with support head screws |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH108891A (en) * | 1924-05-26 | 1925-02-16 | Vuagniaux Max | Hardware for doors and windows called plug. |
CH242554A (en) * | 1942-10-19 | 1946-05-31 | Bolz Jakob | Hinge. |
CH276647A (en) * | 1949-03-17 | 1951-07-31 | Held Hermann | Hinge. |
DE912902C (en) * | 1952-07-26 | 1954-06-03 | Walter Pfaeffli | Hinge, especially for doors and windows, the supporting bolts of which are fastened with a fine thread in pre-drilled holes |
DE1945028A1 (en) * | 1969-09-05 | 1971-03-11 | Ver Baubeschlag Gretsch Co | Arrangement of fittings in profile frames of windows, doors or the like. |
DE6939409U (en) * | 1969-10-08 | 1970-01-15 | Aluminiumwerke Wutoeschingen G | HINGE STRAP FOR FASTENING TO A METAL PROFILE |
AT324882B (en) * | 1971-02-22 | 1975-09-25 | Lautenschlaeger Kg Karl | MOUNTING PLATE FOR FURNITURE HINGES |
DE2117645A1 (en) * | 1971-04-10 | 1972-10-19 | Baumgärtner, Eugen, 6750 Kaiserslautern | Door frame with wall closure provided on both sides |
DE7145404U (en) * | 1971-12-02 | 1972-02-24 | Hettich F Kg | HINGE |
EP0448907A1 (en) * | 1990-03-01 | 1991-10-02 | Siemens Aktiengesellschaft | Hinge arrangement for the door of a switchboard and mounting procedure |
DE9314572U1 (en) * | 1993-09-27 | 1995-02-02 | Dr. Hahn GmbH & Co. KG., 41189 Mönchengladbach | Tape for doors, windows and the like |
DE19748418A1 (en) * | 1997-11-03 | 1999-05-12 | Schneider Gmbh | Door strip for wood cladding of steel door frames |
GB2458935B (en) * | 2008-04-03 | 2013-01-23 | Raptorgrip Ltd | A fastening assembly |
DE202008016430U1 (en) * | 2008-12-11 | 2009-04-23 | Lautenschläger, Horst | Screw fastening for furniture fittings |
DE102009044020B3 (en) * | 2009-09-16 | 2011-04-28 | Dr. Hahn Gmbh & Co. Kg | Method of assembling a hinge for hinged mounting of a wing, door, window or the like, tape and mounting system |
GB2474046B (en) * | 2009-10-02 | 2012-04-04 | Raptorgrip Ltd | A fastening assembly |
-
2011
- 2011-08-19 DE DE102011081284A patent/DE102011081284B3/en not_active Expired - Fee Related
-
2012
- 2012-07-26 WO PCT/EP2012/064660 patent/WO2013026648A1/en active Application Filing
- 2012-07-26 PL PL12742869T patent/PL2744960T3/en unknown
- 2012-07-26 EP EP12742869.6A patent/EP2744960B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
PL2744960T3 (en) | 2016-02-29 |
WO2013026648A1 (en) | 2013-02-28 |
EP2744960A1 (en) | 2014-06-25 |
DE102011081284B3 (en) | 2012-09-20 |
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