EP1309256A1 - Eyelet for reinforcing the edge of a hole in a carrier strip and device for attaching an eyelet to a carrier strip - Google Patents

Eyelet for reinforcing the edge of a hole in a carrier strip and device for attaching an eyelet to a carrier strip

Info

Publication number
EP1309256A1
EP1309256A1 EP01960266A EP01960266A EP1309256A1 EP 1309256 A1 EP1309256 A1 EP 1309256A1 EP 01960266 A EP01960266 A EP 01960266A EP 01960266 A EP01960266 A EP 01960266A EP 1309256 A1 EP1309256 A1 EP 1309256A1
Authority
EP
European Patent Office
Prior art keywords
eyelet
carrier web
neck
ring
pressure ring
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP01960266A
Other languages
German (de)
French (fr)
Other versions
EP1309256B1 (en
Inventor
Heinz-Dieter Kopatz
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.)
William Prym GmbH and Co KG
Original Assignee
William Prym GmbH and Co KG
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=26006681&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=EP1309256(A1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Priority claimed from DE10039462A external-priority patent/DE10039462C5/en
Application filed by William Prym GmbH and Co KG filed Critical William Prym GmbH and Co KG
Publication of EP1309256A1 publication Critical patent/EP1309256A1/en
Application granted granted Critical
Publication of EP1309256B1 publication Critical patent/EP1309256B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • AHUMAN NECESSITIES
    • A44HABERDASHERY; JEWELLERY
    • A44BBUTTONS, PINS, BUCKLES, SLIDE FASTENERS, OR THE LIKE
    • A44B13/00Hook or eye fasteners
    • A44B13/0058Eyelets or grommets
    • AHUMAN NECESSITIES
    • A41WEARING APPAREL
    • A41HAPPLIANCES OR METHODS FOR MAKING CLOTHES, e.g. FOR DRESS-MAKING OR FOR TAILORING, NOT OTHERWISE PROVIDED FOR
    • A41H37/00Machines, appliances or methods for setting fastener-elements on garments
    • A41H37/02Setting hooks or eyes
    • AHUMAN NECESSITIES
    • A44HABERDASHERY; JEWELLERY
    • A44BBUTTONS, PINS, BUCKLES, SLIDE FASTENERS, OR THE LIKE
    • A44B13/00Hook or eye fasteners
    • A44B13/0058Eyelets or grommets
    • A44B13/0076Eyelets or grommets characterised by their way of fastening to the support
    • A44B13/0082Eyelets or grommets characterised by their way of fastening to the support by riveting
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T24/00Buckles, buttons, clasps, etc.
    • Y10T24/34Combined diverse multipart fasteners
    • Y10T24/3427Clasp
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T24/00Buckles, buttons, clasps, etc.
    • Y10T24/36Button with fastener
    • Y10T24/3628Integral or rigid stud
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T24/00Buckles, buttons, clasps, etc.
    • Y10T24/36Button with fastener
    • Y10T24/3681Tufting type
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T24/00Buckles, buttons, clasps, etc.
    • Y10T24/37Drawstring, laced-fastener, or separate essential cooperating device therefor
    • Y10T24/3742Drawstring, laced-fastener, or separate essential cooperating device therefor having eyelet type directing means
    • Y10T24/3745Drawstring, laced-fastener, or separate essential cooperating device therefor having eyelet type directing means with permanently deformed mounting structure
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T24/00Buckles, buttons, clasps, etc.
    • Y10T24/37Drawstring, laced-fastener, or separate essential cooperating device therefor
    • Y10T24/3742Drawstring, laced-fastener, or separate essential cooperating device therefor having eyelet type directing means
    • Y10T24/3745Drawstring, laced-fastener, or separate essential cooperating device therefor having eyelet type directing means with permanently deformed mounting structure
    • Y10T24/3747Mounting structure formed from different material than directing passage
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T24/00Buckles, buttons, clasps, etc.
    • Y10T24/37Drawstring, laced-fastener, or separate essential cooperating device therefor
    • Y10T24/3768Drawstring, laced-fastener, or separate essential cooperating device therefor having loop or sleeve shaped directing means
    • Y10T24/3779Drawstring, laced-fastener, or separate essential cooperating device therefor having loop or sleeve shaped directing means with permanently deformed mounting structure
    • Y10T24/3782Loop or sleeve closed when mounted

Definitions

  • Eyelet for reinforcing the edge area around a hole in a carrier web and device for attaching the eyelet to a carrier web
  • the invention is initially directed to an eyelet of the type specified in the preamble of claim 1.
  • One-piece and two-piece eyelets are known.
  • the eyelet is formed by a single eyelet part, which consists of a plate with a short neck. At the front end of the neck there are spikes that sit at a radial distance from one another and act as projections of the neck.
  • This rivet part is riveted via an additional sleeve-shaped rivet element, which can also be part of a rivet press. Only the prongs and not the neck of the eyelet are bent against the plate on which the sheet to be punched is located. The sheet is perforated through the front end of the tubular rivet element. After attaching the eyelet, the rivet element is removed and can be used again.
  • the strength of the attachment of the eyelet to the leaf is unsatisfactory because only the occasional prongs are involved.
  • the folded tines cannot prevent the leaf from pulling out at the eyelet-reinforced hole, because the points of the points point in the direction of such a pull-out movement.
  • eyelets of another type which have no projections, in which the end piece of the neck is flanged.
  • These eyelets are mainly used for inflexible carrier webs, such as cardboard boxes.
  • flexible carrier webs such as car tarpaulins.
  • the box had to be pre-punched, which was cumbersome and time-consuming.
  • the eyelet supported itself on the face with its plate, penetrated the pre-cut hole in the box with its neck and its approximately L-shaped border came to rest on the back of the carrier web.
  • a pre-perforation of the carrier ba n is not necessary with other types of eyelets, namely two-part eyelets, which consist of an eyelet on one side and a disc part on the other side of the carrier web (DIN 7332).
  • two-part eyelets canvas can also be used as a carrier sheet, but a higher amount of material in the manufacture and a greater amount of work in the attachment are required. This is because both the eyelet part and the disk part have to be produced separately, and both parts have to be arranged in the associated upper and lower tools of the attachment device. The production, warehousing and feeding of two parts each is space and time consuming. The pull-out strength of the eyelets is also limited.
  • the ring-shaped disk part has individual prongs on both the inner edge and the outer edge, which are pressed axially against the plate of the eye part during the flanging and thereby perforate the carrier web. These prongs are on the face side
  • the carrier web, in the plate area of the eyelet is bent or flanged by the transition between the neck and the plate from the eyelet and, on the other hand, by a peripheral chamber on the plate of the eyelet This eyelet is also very complex to manufacture and process.
  • the invention has for its object to develop an inexpensive, quickly attachable eyelet, which after its attachment to the carrier web by a high Excellent tear resistance. This is achieved according to the invention by the measures set out in claim 1, which have the following meaning.
  • the invention gives a surprisingly high pull-out strength, namely a 30 to 75% higher strength. This occurs particularly with the previously so critical flexible or stretchable carrier webs that could not be processed with a one-piece eyelet. Because of the one-piece design of the invention, one saves the pane part and thus material, storage costs, freight costs and handling during the preparation work.
  • the one-piece eyelet part in the invention allows rapid processing, which lowers the cost of attaching the eyelet. Taking into account the ring profile during the flanging, it is sufficient to make the neck of the eyelet according to the invention sufficiently long. Of course, the thickness of the support wall must also be taken into account. Then only the axial or radial projections need to be arranged in the free end piece of the neck, which can be created in different ways.
  • the projections for example, by radial perforations in the tube wall of the neck.
  • these radial projections penetrate into the gripped edge area of the carrier web, where they dig in and create the pressure points with respect to the opposite abutment surface on the plate.
  • the toothed or corrugated end edge of the neck mentioned in claim 2 is suitable for this.
  • the entire edge of the neck is continuously profiled and not, as in the prior art mentioned at the outset, provided with individual projections which are spaced apart from one another. In the ring profile, both the neck and its projections are deformed together in the invention.
  • the invention further relates to a device for attaching the eyelet according to the invention.
  • the resulting peculiarities can be found in claim 10.
  • pulling pins are used on the end face of an axially movable central insert in the upper tool. This made it possible to cut the hole in the carrier web larger during the flaring stroke of the two tool parts in order to obtain problem-free riveting with the disk part.
  • the invention takes a completely different path here.
  • the invention does not use disc parts but only eyelet parts, a device is used which is customary for the two-part eyelets.
  • no pulling pin is used on the central insert of the upper tool, because the invention wants to make the hole in the carrier web as small as possible. This is important because, as has already been mentioned, in the formation of the essentially closed ring profile of the flange, an excess length from the hole edge region of the carrier web is desired, which continues inside the ring profile beyond the pressure points mentioned. A particularly reliable mode of operation is obtained if the pressure ring mentioned in claim 11 and the in Claim 13 counter pressure ring used. The profiles of these pressure and counter pressure rings mentioned in the further subclaims are also useful.
  • FIG. 4 shows an axial section through the special eyelet part of the diskless eyelet according to the invention in the initial state, namely before it is processed on the carrier web,
  • FIG. 6 in axial half section, fragments of a two-part device according to the invention for processing the eyepiece shown in Fig. 4, wherein the upper tool is located opposite the lower tool in the upper end point of its lifting movement.
  • an eyelet is intended to reinforce the edge region 21 of a hole 22 cut in a carrier web 20.
  • the carrier web 20 is generally a flexible and possibly stretchable structure, for example a motor vehicle tarpaulin.
  • the invention achieves the desired hole reinforcement with a one-piece eyelet part 10.
  • FIGS. 4 and 5 the eyelet part 10 is shown in its initial state before Processing. 1, 2 and 3, on the other hand, show the eyelet part 10 'after its processing, in the finished state of use, during its hole reinforcement function.
  • the eyelet 10 can be divided into a curved, essentially radially extending plate 11 and an axially extending tubular neck 12.
  • the plate 11 has a curvature profile
  • the free end piece 15 of the neck is provided with axial projections 16, that is to say in the direction in which the neck 12 extends.
  • these consist of an arc-toothed end edge 17 which can be seen in FIG. 5. This has the following special appearance.
  • the tooth tips 17 are provided with convex curves 27, while the tooth gaps 18 have concave curves 28. This creates a wave shape from the tooth profile 19.
  • the waveform is asymmetrical. That is, the radius of curvature of the curves 27 of the tooth tips 17 is smaller than that of the curves 28 of the tooth gaps.
  • This eyelet part 17 is attached to the carrier web 20 in the device 30 shown in FIG. 6.
  • the device 30 consists of essentially five parts which are axially displaceable with respect to one another in time. First of all, this includes a lower tool 32 which in the present case is stationary and which, on the other hand, carries a pressure ring 34 which is passively axially movable. Furthermore, the device 30 includes an upper tool 31 that is actively movable relative to the lower tool 32, with a central insert 33 arranged coaxially therein, which, in contrast, is also passively axially movable. Finally, the upper tool 31 is enclosed in the circumferential area by a counter pressure ring 54, which is also passively axially movable.
  • the central insert 33 and the counterpressure ring 54 are force-loaded in the sense of the force arrows 35 and 55 against the lower tool 32, while the pressure ring 34 in the lower tool 32, also mirror image, in the sense of the force arrow 36 against the upper tool 31 under the action of a group of springs 56 stands, which are mounted in axial bores of the lower tool 32.
  • the springs 56 are as Coil springs are formed, in the inside of which the pins 57 which are seated on the pressure ring 34 engage.
  • the tool group 31, 33, 54 on the one hand and 32, 34 on the other hand are reciprocally movable, as illustrated by the movement arrow 37 of the upper tool group 31, 33, 54.
  • the counter pressure ring 54 is guided on the peripheral surface 63 of the upper tool 31.
  • the force load 55 from the counter pressure ring 54 is generated by a compression spring 64, which is supported between a flank of a peripheral flange 65 of the upper tool 31 and the abutment surface of a cutout 66 in the counter pressure ring 54.
  • the extension position of the counter pressure ring 54 is determined by end stops. In the present case, these consist of the head 67 of a family of guide rods 68, which can be adjusted in length by thread 69 and a locking nut 71. The rod head 67 is supported at rest on the upper flank of flange 65. The desired extension length 70 of the counter pressure ring 54 with respect to the upper tool 31 is thereby determined.
  • FIG. 6 shows the upper reversal point of the lifting movement 37, where the upper tool 31 is located at a maximum lifting distance 38 with respect to the lower tool 32.
  • an eyelet part 10 can be conveniently inserted onto the receiving profile of the upper tool 31 and central insert 33.
  • the upper tool 31 has a receptacle 39 corresponding to the profile of the plate 11.
  • the area provided with the receptacle 39 is subject to wear when used as intended.
  • the lower region of the upper tool is therefore provided with an insert 31 ′, which is detachably connected to the upper region of the upper tool 31 by the indicated screw or the like.
  • This insert 31 ' has the receptacle 39.
  • the central insert 33 is provided with a flat end surface 43.
  • a holding element 44 is arranged in the circumferential area of the central insert 33, which in the present case consists of a pin which is spring-loaded radially outwards.
  • the carrier web 20 is inserted, which is initially unperforated.
  • the aforementioned springs 56 hold the pressure ring 34 in a defined starting position, which can be seen in FIG. 6.
  • the relevant upper side 45 of the pressure ring 34 is above or expediently at the same height with a cutting edge 42 provided in the cutting tool 32. This results in the pressure ring 34, a horizontal support plane 60 for the carrier web 20, which is illustrated in FIG.
  • the leading counter-pressure ring 54 first meets the carrier web 20 lying above the pressure ring 34.
  • the two rings 34, 54 are provided with bevels 58 and 59 which run essentially parallel to one another and which support the carrier web 20 grasp between them, whereby the carrier web 20 is initially slightly tensioned.
  • the inclined surface 58 of the pressure ring 34 extends at an acute angle 61 with respect to the support plane 60 illustrated in dash-dot lines in FIG. 6, which is determined by the end face 45 of the pressure ring 34 serving to support the carrier web 20.
  • the counter pressure surface 59 of the pressure ring 54 mentioned runs essentially parallel to the pressure surface 58.
  • the carrier web 20 is therefore drawn around the edge 62, which is formed between the end face 45 and the inclined surface 58 of the pressure ring 34. As a result, the carrier web is pulled smooth in the area 29 to be punched. The carrier web 20 consequently assumes an extended position in the support plane 60 mentioned.
  • the central insert 33 loaded by the press ram hits the upward facing side 23 of the carrier web 20 and presses it against the cutting edge 42 of the lower tool 32 resting on the carrier underside 24.
  • a circular punched hole is thereby cut out of the carrier web 20.
  • the hole radius 46 determined by the cutting edge 42 is smaller than the neck radius 26 of the eyelet neck 12 identified by 26 in FIG. 6.
  • the carrier web 20 becomes firmer between the two bevels 58, 59 of the two rings 34, 54 clamped.
  • the neck 12 moves from the eyelet 10 through the hole formed in the lower tool until the plate 11 from the eyelet 10, with the interposition of the carrier web 20, touches the pressure ring 34.
  • the upper tool 31 overcomes the spring force 36 from the lower pressure ring 34 and the eyelet neck 12 and the axial projections 16 on the flanged profile 47 of the lower tool 32 are flattened.
  • the spring force 54 from the upper pressure ring 54 is smaller than that on the Thrust ring 34 acting ejection force 36.
  • the lower tool 32 also has an insert 32 'which is positioned in the axial region and which has the relevant flanged profile 47. This flared profile 47 wears out after prolonged use. Then it is sufficient to replace this insert 32 '.
  • the special riveting relationships shown in FIG. 3 result from the bordering. Practically the entire neck length 48 of the eyelet part shown in FIG. 4 is rolled into an annular profile 50 recognizable in FIG. 3 on the rear side 24 of the carrier web 20.
  • the neck projections 16 are included in this ring formation 50. With the interposition of the hole edge region 21 of the carrier web 20 mentioned and also indicated in FIG. 6, these neck projections 16 are pressed against an abutment surface 49 generated by the described curvature 13 of the plate 11.
  • the ring-shaped circumferential pressure points 40 can be seen there from FIG. 3.
  • the carrier web 20 continues with an end zone 41, which adapts to the profile 50 in the manner of a ring segment. Even when the end zone 41 rolls in during the riveting process, the bevels 58, 59 hold the carrier web 20 in place.
  • the web 40 is in fact endeavored to rise back to its original web thickness 25 at 53. With the tensile loads 52 of the web 20, these step-like elevations 53 of the web material 20 cling to the wavy edges of the neck projections 16. This increases the positive fit and achieves a surprisingly high tensile strength of the riveted eyelet part 10 ′ on the web 20.

Abstract

The invention relates to a ringless eyelet ( 10 ') comprising a plate ( 11 ) arranged on the display side ( 23 ) of the carrier strip ( 20 ), and a tube-shaped collar penetrating the hole in the carrier strip. The hem of the collar of the eyelet element ( 10 ') is supported on the rear side ( 24 ) of the carrier strip ( 20 ). The aim of the invention is to connect the eyelet to the carrier strip ( 20 ) faster and in a more cost-effective manner. In order to achieve this, the free end part of the collar of the eyelet element ( 10 ') is provided with projections ( 16 ). An essentially closed ring profile ( 50 ), into which the collar projections ( 16 ) are integrated, is created when the collar is hemmed. After hemming, pressure points ( 40 ) are created on the carrier strip ( 20 ) between the collar projections ( 16 ) and the abutment surfaces ( 49 ) formed by the plate ( 11 ), said pressure points reliably holding the carrier strip ( 20 ). Said carrier strip ( 20 ) extends namely inside ( 51 ) the ring profile ( 50 ) beyond the pressure points ( 40 ). An eyelet is obtained using only one.

Description

Öse zum Verstärken des Randbereichs um ein Loch in einer Trägerbahn und Vorrichtung zum Ansetzen der Öse an einer Trägerbahn Eyelet for reinforcing the edge area around a hole in a carrier web and device for attaching the eyelet to a carrier web
Die Erfindung richtet sich zunächst auf eine Öse der im Oberbegriff des Anspruches 1 angegebenen Art. Es sind einteilige und zweiteilige Ösen bekannt.The invention is initially directed to an eyelet of the type specified in the preamble of claim 1. One-piece and two-piece eyelets are known.
Bei der bekannten einteiligen Öse der im Oberbegriff des Anspruches 1 angegebenen Art (US-PS 2,901,800, Fig. 5) wird die Öse von einem einzigen Osenteil gebildet, welcher aus einem Teller mit einem kurzen Hals besteht. Am Stirnende des Halses befinden sich in radialem Abstand zueinander sitzende Zacken, die als Vorsprünge des Halses fungieren. Die Vernietung dieses Osenteils erfolgt über ein zusätzliches hülsenförmiges Nietelement, welches auch Teil einer Nietpresse sein kann. Dabei werden nur die Zacken und nicht den Hals des Osenteils gegen den Teller umgebogen, auf welchem sich das zu lochende Blatt befindet. Die Lochung des Blatts erfolgt dabei durch das Stirnende des hülsenförmigen Nietelements. Nach der Befestigung des Osenteils wird das Nietelement entfernt und kann erneut verwendet werden. Die Festigkeit der Anbringung des Osenteils am Blatt ist nicht befriedigend, weil daran nur die vereinzelten Zacken beteiligt sind. Die umgelegten Zacken können eine Auszugbewegung des Blatts am ösenverstärkten Loch nicht verhindern, weil die Zackenspitzen in Richtung einer solchen Auszugsbewegung weisen.In the known one-piece eyelet of the type specified in the preamble of claim 1 (US Pat. No. 2,901,800, Fig. 5), the eyelet is formed by a single eyelet part, which consists of a plate with a short neck. At the front end of the neck there are spikes that sit at a radial distance from one another and act as projections of the neck. This rivet part is riveted via an additional sleeve-shaped rivet element, which can also be part of a rivet press. Only the prongs and not the neck of the eyelet are bent against the plate on which the sheet to be punched is located. The sheet is perforated through the front end of the tubular rivet element. After attaching the eyelet, the rivet element is removed and can be used again. The strength of the attachment of the eyelet to the leaf is unsatisfactory because only the occasional prongs are involved. The folded tines cannot prevent the leaf from pulling out at the eyelet-reinforced hole, because the points of the points point in the direction of such a pull-out movement.
Es gibt einteilige Ösen anderer Art (DIN 7333), die keine Vorsprünge aufweisen, bei denen das Endstück des Halses umbördelt wird. Diese Ösen werden im wesentlichen bei unflexiblen Trägerbahnen verwendet, wie Kartonagen. Bisher war die Anwendung auf flexible Trägerbahnen, wie Autoplanen, nicht möglich. Vor dem Ansetzen der bekannten einteiligen Öse musste der Karton vorgelocht werden, was umständlich und zeitaufwendig war. Nach dem Ansetzen stützte sich der Osenteil auf der Schauseite mit seinem Teller ab, durchsetzte mit seinem Hals das vorgeschnittene Loch im Karton und seine etwa L-förmige Bordelung kam auf der Rückseite der Trägerbahn zu liegen.There are one-piece eyelets of another type (DIN 7333), which have no projections, in which the end piece of the neck is flanged. These eyelets are mainly used for inflexible carrier webs, such as cardboard boxes. Until now, application on flexible carrier webs, such as car tarpaulins, was not possible. Before the Attaching the well-known one-piece eyelet, the box had to be pre-punched, which was cumbersome and time-consuming. After attaching, the eyelet supported itself on the face with its plate, penetrated the pre-cut hole in the box with its neck and its approximately L-shaped border came to rest on the back of the carrier web.
Eine Vorlochung der Trägerba n entfällt bei Ösen anderer Art, nämlich zweiteiligen Ösen, welche aus einem Osenteil auf der einen Seite und einem Scheibenteil auf der anderen Seite der Trägerbahn bestehen (DIN 7332). Mit diesen zweiteiligen Ösen können als Trägerbahn zwar auch Segeltuche benutzt werden, doch sind ein höherer Materialaufwand beim Herstellen und ein größerer Arbeitsaufwand beim Ansetzen erforderlich. Es müssen nämlich sowohl der Osenteil und der Scheibenteil für sich hergestellt als auch beide Teile in die zugehörigen Ober- und Unterwerkzeuge der Ansetzvorrichtung angeordnet werden. Die Herstellung, Lagerhaltung und Zuführung von jeweils zwei Teilen ist platz- und zeitaufwendig. Außerdem ist die Ausziehfestigkeit der Ösen begrenzt. Falls man versuchen wollte bei dieser bekannten zweiteiligen Öse den Scheibenteil wegzulassen, und nur, wie beim vorerwähnten ersten Stand der Technik, mit einem Osenteil zu arbeiten, so würde man eine völlig unbrauchbare Ausziehfestigkeit der Tragbahn an der angesetzten Öse erhalten.A pre-perforation of the carrier ba n is not necessary with other types of eyelets, namely two-part eyelets, which consist of an eyelet on one side and a disc part on the other side of the carrier web (DIN 7332). With these two-part eyelets, canvas can also be used as a carrier sheet, but a higher amount of material in the manufacture and a greater amount of work in the attachment are required. This is because both the eyelet part and the disk part have to be produced separately, and both parts have to be arranged in the associated upper and lower tools of the attachment device. The production, warehousing and feeding of two parts each is space and time consuming. The pull-out strength of the eyelets is also limited. If one wanted to try to omit the disc part from this known two-part eyelet, and only to work with an eyelet part, as in the aforementioned first prior art, one would obtain a completely unusable pull-out strength of the supporting track on the attached eyelet.
Bei zweiteiligen Ösen, die als sogenannte „Grommets" ausgebildet sind, besitzt der ringförmige Scheibenteil sowohl am Innenrand als auch am Außenrand vereinzelte Zacken, die beim Bördeln axial gegen den Teller des Osenteils gedrückt werden und dabei die Trägerbahn perforieren. Diese Zacken werden auf der Schauseite der Trägerbahn, im Tellerbereich des Osenteils, umgebogen bzw. umbördelt. Dazu dient einerseits der Übergang zwischen Hals und Teller vom Osenteil und andererseits eine umfangsseitig Kammer am Teller des Osenteils. Diese Zacken arbeiten nach Art eines sogenannten Zackenrings, wie .er z.B. bei Druckknopfteilen verwendet wird. Auch diese Öse ist sehr aufwendig in der Herstellung und Verarbeitung.In the case of two-part eyelets, which are designed as so-called "grommets", the ring-shaped disk part has individual prongs on both the inner edge and the outer edge, which are pressed axially against the plate of the eye part during the flanging and thereby perforate the carrier web. These prongs are on the face side The carrier web, in the plate area of the eyelet, is bent or flanged by the transition between the neck and the plate from the eyelet and, on the other hand, by a peripheral chamber on the plate of the eyelet This eyelet is also very complex to manufacture and process.
Der Erfindung liegt die Aufgabe zugrunde, eine preiswerte, schnell ansetzbare Öse zu entwickeln, die sich nach ihrer Anbringung an der Trägerbahn durch eine hohe Reißfestigkeit auszeichnet. Dies wird erfmdungsgemäß durch die im Anspruch 1 angeführten Maßnahmen erreicht, denen folgende Bedeutung zukommt.The invention has for its object to develop an inexpensive, quickly attachable eyelet, which after its attachment to the carrier web by a high Excellent tear resistance. This is achieved according to the invention by the measures set out in claim 1, which have the following meaning.
Mit den axialen bzw. radialen Vorsprüngen am freien Endstück des Halses erhält man Haltemittel, die bei einer ein Ringprofil erzeugenden Umbördelung des Halses besondere Andruckstellen an der erfassten Trägerbahn erzeugen, gegen welche sich die Trägerbahn bei Zugbeanspruchungen stellt. In das Ringprofil der Umbördelung des Halses sind die endseitigen Halsvorsprünge integriert und liegen unter Zwischenschaltung des Lochrandbereichs der Trägerbahn an Widerlagerflächen an, die bei diesem Ringprofil vom Teller oder vom Übergang zwischen Teller und Hals des Osenteils gebildet werden. Die Trägerbahn läuft im Ringprofiϊinneren über die Andruckstellen hinaus bis zu ihrer Lochkante weiter. Beanspruchungen der Trägerbahn wirken sich an den Andruckstellen der ins Ringprofilinnere mit eingerollten Rändern der Lochbahn als Hindernisse aus. Die erfindungsgemäße Öse ist gegenüber dem eingangs erwähnten Stand der Technik wesentlich auszugssicherer.With the axial or radial projections on the free end piece of the neck, holding means are obtained which, when the neck is flanged, produce special pressure points on the detected carrier web, against which the carrier web is subject to tensile stresses. In the ring profile of the flanging of the neck, the end-side neck projections are integrated and, with the interposition of the hole edge region of the carrier web, lie against abutment surfaces which are formed in this ring profile by the plate or by the transition between plate and neck of the neck part. The carrier web runs inside the ring professional beyond the pressure points up to its perforated edge. Stresses on the carrier web act as obstacles at the pressure points on the inside of the ring profile with rolled-up edges of the perforated web. The eyelet according to the invention is considerably more reliable than the prior art mentioned at the outset.
Im Vergleich mit den sehr viel aufwendigeren zweiteiligen Ösen erhält man bei der Erfindung eine überraschend hohe Ausreißfestigkeit, nämlich eine 30 bis 75% höhere Festigkeit. Diese tritt gerade bei den bisher so kritischen flexiblen oder dehnbaren Trägerbahnen auf, die mit einer einteiligen Öse gar nicht verarbeitet werden konnten. Wegen der Einteiligkeit bei der Erfindung spart man den Scheibenteil und damit Material, Lagerkosten, Frachtkosten und das Handling bei den Ansetzarbeiten. Der einteilige Osenteil bei der Erfindung erlaubt eine schnelle Verarbeitung, was die Kosten zum Ansetzen der Öse erniedrigt. Unter Berücksichtigung des Ringprofils bei der Umbördelung genügt es, den Hals des erfindungsgemäßen Osenteils ausreichend lang auszubilden. Dabei ist natürlich auch die Dicke der Trägerwand zu berücksichtigen. Im freien Endstück des Halses brauchen dann nur noch die axialen bzw. radialen Vorsprünge angeordnet, zu werden, die in verschiedener Weise erstellt werden können.In comparison with the much more complex two-part eyelets, the invention gives a surprisingly high pull-out strength, namely a 30 to 75% higher strength. This occurs particularly with the previously so critical flexible or stretchable carrier webs that could not be processed with a one-piece eyelet. Because of the one-piece design of the invention, one saves the pane part and thus material, storage costs, freight costs and handling during the preparation work. The one-piece eyelet part in the invention allows rapid processing, which lowers the cost of attaching the eyelet. Taking into account the ring profile during the flanging, it is sufficient to make the neck of the eyelet according to the invention sufficiently long. Of course, the thickness of the support wall must also be taken into account. Then only the axial or radial projections need to be arranged in the free end piece of the neck, which can be created in different ways.
Eine Möglichkeit besteht darin, die Vorsprünge z.B. durch radiale Lochungen in der Rohrwand des Halses auszubilden. Beim Umbördeln des Halses dringen diese radialen Vorsprünge in den erfassten Lochrandbereich der Trägerbahn ein, wo sie sich eingraben und die Andruckstellen bezüglich der gegenüberliegenden Widerlagerfläche am Teller erzeugen. Herstellungsmäßig einfacher ist es aber, die andere Möglichkeit, nämlich die Vorsprünge axial auszubilden. Es eignet sich hierfür die in Anspruch 2 erwähnte gezahnte oder gewellte Endkante des Halses. In diesem Fall ist die ganze Kante des Halses durchgehend profiliert und nicht, wie im eingangs erwähnten Stand der Technik, mit vereinzelten, in Abstand zueinander sitzenden Vorsprüngen versehen. Bei der Ringprofilgebung werden bei der Erfindung sowohl der Hals als auch seine Vorsprünge gemeinsam verformt. Beim Ziehen der Ringform während der Umbördelung gräbt sich der Zahn in das Bahnmaterial ein und es kommt nicht nur zu einer Klemmung zwischen dem Zahn und der Widerlagerfläche vom Teller, sondern auch zu einem Formschluss zwischen Zahn und Trägerbahn. Je größer der auf die Trägerbahn ausgeübte Zug ist, umso sicherer gräbt sich der Zahn in die Trägerbahn ein. Das erklärt die überraschend hohe Reißfestigkeit der erfindungs gemäßen Öse.One possibility is to form the projections, for example, by radial perforations in the tube wall of the neck. When the neck is flanged over, these radial projections penetrate into the gripped edge area of the carrier web, where they dig in and create the pressure points with respect to the opposite abutment surface on the plate. In terms of production, however, it is simpler to form the other possibility, namely the projections axially. The toothed or corrugated end edge of the neck mentioned in claim 2 is suitable for this. In this case, the entire edge of the neck is continuously profiled and not, as in the prior art mentioned at the outset, provided with individual projections which are spaced apart from one another. In the ring profile, both the neck and its projections are deformed together in the invention. When the ring shape is pulled during the flanging, the tooth digs into the web material and there is not only a clamping between the tooth and the abutment surface from the plate, but also a positive fit between the tooth and the carrier web. The greater the tension exerted on the carrier web, the more reliably the tooth digs into the carrier web. This explains the surprisingly high tear strength of the eyelet according to the invention.
Die Erfindung richtet sich ferner auf eine Vorrichtung zum Ansetzen der Öse nach der Erfindung. Die sich dabei ergebenden Besonderheiten sind aus Anspruch 10 zu entnehmen. Bei den bekannten Ansetzvorrichtungen für Ösen an flexiblen Trägerbahnen, wie Planen, verwendet man Vorziehzapfen an der Stirnfläche eines axial beweglichen Zentraleinsatzes im Oberwerkzeug. Damit war es möglich, beim Bördelhub der beiden Werkzeugteile das Loch in der Trägerbahn größer zu schneiden, um eine problemlose Vernietung mit dem Scheibenteil zu erhalten. Die Erfindung geht hier einen ganz anderen Weg.The invention further relates to a device for attaching the eyelet according to the invention. The resulting peculiarities can be found in claim 10. In the known attachment devices for eyelets on flexible carrier webs, such as tarpaulins, pulling pins are used on the end face of an axially movable central insert in the upper tool. This made it possible to cut the hole in the carrier web larger during the flaring stroke of the two tool parts in order to obtain problem-free riveting with the disk part. The invention takes a completely different path here.
Obwohl bei der Erfindung, wie bereits gesagt wurde, keine Scheibenteile sondern nur Ösenteile verwendet werden, wird eine Vorrichtung verwendet, wie sie bei den zweiteiligen Ösen üblich ist. Im Gegensatz dazu wird aber kein Vorziehzapfen am Zentraleinsatzes des Oberwerkzeugs benutzt, weil die Erfindung das Loch in der Trägerbahn so klein wie möglich ausbilden will. Dies ist deswegen wichtig, weil, wie schon erwähnt wurde, bei der Bildung des im wesentlichen geschlossenen Ringprofils der Umbördelung eine Überschusslänge vom Lochrandbereich der Trägerbahn erwünscht ist, die sich im Ringprofilinneren jenseits der erwähnten Andruckstellen fortsetzt. Eine besonders zuverlässige Arbeitsweise ergibt sich, wenn man bei der Vorrichtung den im Anspruch 11 erwähnten Druckring und den in Anspruch 13 beschriebenen Gegendruckring verwendet. Nützlich sind auch die in den weiteren Unteransprüchen erwähnten Profilierungen dieser Druck- und Geg endru ckring e .Although, as has already been said, the invention does not use disc parts but only eyelet parts, a device is used which is customary for the two-part eyelets. In contrast, however, no pulling pin is used on the central insert of the upper tool, because the invention wants to make the hole in the carrier web as small as possible. This is important because, as has already been mentioned, in the formation of the essentially closed ring profile of the flange, an excess length from the hole edge region of the carrier web is desired, which continues inside the ring profile beyond the pressure points mentioned. A particularly reliable mode of operation is obtained if the pressure ring mentioned in claim 11 and the in Claim 13 counter pressure ring used. The profiles of these pressure and counter pressure rings mentioned in the further subclaims are also useful.
Weitere Maßnahmen und Vorteile der Erfindung ergeben sich aus den Unteransprüchen, der nachfolgenden Beschreibung und den Zeichnungen. In den Zeichnungen ist die Erfindung in einem Ausführungsbeispiel dargestellt. Es zeigen:Further measures and advantages of the invention result from the subclaims, the following description and the drawings. In the drawings, the invention is shown in one embodiment. Show it:
Fig. 1 und 2, jeweils in Draufsicht, die Schauseite bzw. die Rückseite einer mit der erfindungsgemäßen Öse ausgerüsteten Trägerbahn,1 and 2, each in plan view, the front or the back of a carrier web equipped with the eyelet according to the invention,
Fig. 3, in starker Vergrößerung, eine Querschnittansicht durch die inFig. 3, in high magnification, a cross-sectional view through the in
Fig. 1 gezeigte angesetzte Öse längs der dortigen Schnittlinie III - III,1 shown attached eyelet along the section line III - III,
Fig. 4 einen Axialschnitt durch den besonderen Osenteil der erfindungsgemäßen scheibenlosen Öse im Ausgangszustand, nämlich vor seiner Verarbeitung an der Trägerbahn,4 shows an axial section through the special eyelet part of the diskless eyelet according to the invention in the initial state, namely before it is processed on the carrier web,
Fig. 5, in Vergrößerung, eine ebene Abwinklung eines Teilstücks des mit Ziff. V in Fig. 4 gekennzeichneten Randbereichs vom erfindungsgemäßen Osenteil undFig. 5, in enlargement, a flat bend of a portion of the section. V in Fig. 4 marked edge area of the inventive eyelet and
Fig. 6, in axialem Halbschnitt, Bruchstücke einer zweiteiligen erfindungsgemäßen Vorrichtung zur Verarbeitung des in Fig. 4 gezeigten Osenteils, wobei das Oberwerkzeug sich gegenüber dem Unterwerkzeug im oberen Endpunkt seiner Hubbewegung befindet.Fig. 6, in axial half section, fragments of a two-part device according to the invention for processing the eyepiece shown in Fig. 4, wherein the upper tool is located opposite the lower tool in the upper end point of its lifting movement.
Eine Öse soll, wie Fig. 1 und 2 zeigen, den Randbereich 21 eines in einer Trägerbahn 20 geschnittenen Loches 22 verstärken. Die Trägerbahn 20 ist in der Regel ein flexibles und gegebenenfalls dehnfähiges Gebilde, z.B. eine Kraftfahrzeugplane. Die Erfindung erreicht die gewünschte Lochverstärkung mit einem einteiligen Osenteil 10. In Fig. 4 und 5 ist der Osenteil 10 in seinem Ausgangszustand gezeigt, vor der Verarbeitung. Die Fig. 1, 2 und 3 dagegen zeigen den Osenteil 10' nach seiner Verarbeitung, im fertigen Gebrauchszustand, während seiner Lochverstärkungs- Funktion.1 and 2, an eyelet is intended to reinforce the edge region 21 of a hole 22 cut in a carrier web 20. The carrier web 20 is generally a flexible and possibly stretchable structure, for example a motor vehicle tarpaulin. The invention achieves the desired hole reinforcement with a one-piece eyelet part 10. In FIGS. 4 and 5, the eyelet part 10 is shown in its initial state before Processing. 1, 2 and 3, on the other hand, show the eyelet part 10 'after its processing, in the finished state of use, during its hole reinforcement function.
Der Osenteil 10 lässt sich in einen gewölbten, im wesentlichen radial verlaufenden Teller 1 1 und in einen axial verlaufenden rohrformigen Hals 12 gliedern. Aus Gründen einer besseren Formsteifigkeit und zur noch näher zu beschreibenden ringförmigen Umbördelung des Halses 12 ist der Teller 11 mit einem WölbungsprofilThe eyelet 10 can be divided into a curved, essentially radially extending plate 11 and an axially extending tubular neck 12. For reasons of better dimensional stability and for the annular flanging of the neck 12 to be described in more detail, the plate 11 has a curvature profile
13 versehen. Dadurch ergibt sich ein besonders auffälliger bogenförmiger Übergang13 provided. This results in a particularly striking arch-shaped transition
14 zwischen Teller 11 und dem Hals 12. Der Hals ist in seinem freien Endstück 15 mit axialen, also in Verlaufsrichtung des Halses 12 sich erstreckenden Vorsprüngen 16 versehen. Diese bestehen im vorliegenden Fall aus einer in Fig. 5 erkennbaren bogenförmig gezahnten Endkante 17. Diese hat folgendes besonderes Aussehen.14 between the plate 11 and the neck 12. The free end piece 15 of the neck is provided with axial projections 16, that is to say in the direction in which the neck 12 extends. In the present case, these consist of an arc-toothed end edge 17 which can be seen in FIG. 5. This has the following special appearance.
Die Zahnspitzen 17 sind mit konvexen Rundungen 27 versehen, während die Zahnlücken 18 konkave Rundungen 28 aufweisen. Dadurch entsteht aus dem Zahnprofil 19 ein Wellenverlauf. Der Wellenverlauf ist unsymmetrisch ausgebildet ist. Das heißt, der Krümmungs-Radius der Rundungen 27 der Zahnspitzen 17 ist kleiner als derjenige der Rundungen 28 der Zahnlücken ausgebildet.The tooth tips 17 are provided with convex curves 27, while the tooth gaps 18 have concave curves 28. This creates a wave shape from the tooth profile 19. The waveform is asymmetrical. That is, the radius of curvature of the curves 27 of the tooth tips 17 is smaller than that of the curves 28 of the tooth gaps.
Dieser Osenteil 17 wird in der aus Fig. 6 ersichtlichen Vorrichtung 30 an die Trägerbahn 20 angesetzt. Die Vorrichtung 30 besteht aus im wesentlichen fünf zueinander in zeitlichem Versatz axial beweglichen Teilen. Dazu gehört zunächst ein im vorliegenden Fall ruhendes Unterwerkzeug 32, das einen demgegenüber passiv axial beweglichen Druckring 34 trägt. Ferner gehört zur Vorrichtung 30 ein aktiv gegenüber dem Unterwerkzeug 32 bewegliches Oberwerkzeug 31 mit einem darin koaxial angeordneten Zentral einsatz 33, der demgegenüber ebenfalls passiv axial beweglich ist. Schließlich ist das Oberwerkzeug 31 im Umfangsb ereich von einem ebenfalls passiv axial beweglichen Gegendruckring 54 umschlossen. Der Zentraleinsatz 33 sowie der Gegendruckring 54 sind im Sinne der Kraftpfeile 35 bzw. 55 gegen das Unterwerkzeug 32 kraftbelastet, während der Druckring 34 im Unterwerkzeug 32, dazu spiegelbildlich, im Sinne des Kraftpfeils 36 gegen das Oberwerkzeug 31 unter der Wirkung einer Schar von Federn 56 steht, die in axialen Bohrungen des Unterwerkzeugs 32 montiert sind. Die Federn 56 sind als Wendelfedern ausgebildet, in deren Wendelinneres am Druckring 34 sitzende Stifte 57 eingreifen. Die Werkzeuggruppe 31, 33, 54 einerseits und 32, 34 andererseits sind gegeneinander hubbeweglich, wie durch den Bewegungspfeil 37 der oberen Werkzeuggruppe 31, 33, 54 veranschaulicht ist.This eyelet part 17 is attached to the carrier web 20 in the device 30 shown in FIG. 6. The device 30 consists of essentially five parts which are axially displaceable with respect to one another in time. First of all, this includes a lower tool 32 which in the present case is stationary and which, on the other hand, carries a pressure ring 34 which is passively axially movable. Furthermore, the device 30 includes an upper tool 31 that is actively movable relative to the lower tool 32, with a central insert 33 arranged coaxially therein, which, in contrast, is also passively axially movable. Finally, the upper tool 31 is enclosed in the circumferential area by a counter pressure ring 54, which is also passively axially movable. The central insert 33 and the counterpressure ring 54 are force-loaded in the sense of the force arrows 35 and 55 against the lower tool 32, while the pressure ring 34 in the lower tool 32, also mirror image, in the sense of the force arrow 36 against the upper tool 31 under the action of a group of springs 56 stands, which are mounted in axial bores of the lower tool 32. The springs 56 are as Coil springs are formed, in the inside of which the pins 57 which are seated on the pressure ring 34 engage. The tool group 31, 33, 54 on the one hand and 32, 34 on the other hand are reciprocally movable, as illustrated by the movement arrow 37 of the upper tool group 31, 33, 54.
Der Gegendruckring 54 ist an der Umfangsfläche 63 des Oberwerkzeugs 31 geführt. Die Kraftbelastung 55 vom Gegendruckring 54 wird durch eine Druckfeder 64 erzeugt, welche sich zwischen einer Flanke eines umfangsseitigen Flansches 65 vom Oberwerkzeug 31 und der Stoßfläche eines Ausschnitts 66 im Gegendruckring 54 abstützt. Die Ausschubposition des Gegendruckrings 54 ist durch Endanschläge bestimmt. Diese bestehen im vorliegenden Fall aus dem Kopf 67 einer Schar von Führungsstangen 68, die durch Gewinde eingriff 69 und eine Sicherungsmutter 71 längeneinstellbar sind. Der Stangenkopf 67 stützt sich im Ruhefall an der oberen Flanke von Flansch 65 ab. Dadurch wird die gewünschte Ausschublänge 70 des Gegendruckrings 54 bezüglich des Oberwerkzeugs 31 bestimmt.The counter pressure ring 54 is guided on the peripheral surface 63 of the upper tool 31. The force load 55 from the counter pressure ring 54 is generated by a compression spring 64, which is supported between a flank of a peripheral flange 65 of the upper tool 31 and the abutment surface of a cutout 66 in the counter pressure ring 54. The extension position of the counter pressure ring 54 is determined by end stops. In the present case, these consist of the head 67 of a family of guide rods 68, which can be adjusted in length by thread 69 and a locking nut 71. The rod head 67 is supported at rest on the upper flank of flange 65. The desired extension length 70 of the counter pressure ring 54 with respect to the upper tool 31 is thereby determined.
In Fig. 6 ist, wie bereits erwähnt wurde, der obere Umkehrpunkt der Hubbewegung 37 gezeigt, wo sich das Oberwerkzeug 31 gegenüber dem Unterwerkzeug 32 in maximalem Hubabstand 38 befindet. Dadurch kann ein Osenteil 10 bequem auf das Aufnahmeprofil vom Oberwerkzeug 31 und Zentraleinsatz 33 eingesetzt werden. Dazu besitzt das Oberwerkzeug 31 eine dem Profil des Tellers 11 entsprechende Aufnahme 39. Der mit der Aufnahme 39 versehene Bereich ist bei bestimmungsgemäßem Gebrauch einem Verschleiß unterworfen. Zur leichteren Instandsetzung einer verschlissenen Vorrichtung 30 wird daher der untere Bereich des Oberwerkzeugs mit einem Einsatz 31' versehen, der durch die angedeutete Schraube od. dgl. mit dem oberen Bereich des Oberwerkzeugs 31 lösbar verbunden ist. Dieser Einsatz 31 ' besitzt die Aufnahme 39.As already mentioned, FIG. 6 shows the upper reversal point of the lifting movement 37, where the upper tool 31 is located at a maximum lifting distance 38 with respect to the lower tool 32. As a result, an eyelet part 10 can be conveniently inserted onto the receiving profile of the upper tool 31 and central insert 33. For this purpose, the upper tool 31 has a receptacle 39 corresponding to the profile of the plate 11. The area provided with the receptacle 39 is subject to wear when used as intended. To make it easier to repair a worn device 30, the lower region of the upper tool is therefore provided with an insert 31 ′, which is detachably connected to the upper region of the upper tool 31 by the indicated screw or the like. This insert 31 'has the receptacle 39.
Nach dem Einsetzen des Osenteils 10 stützt sich das Ende des Halses 20 an der Umfangsfläche des Zentraleinsatzes 33 ab. Der Zentraleinsatz 33 ist mit einer ebenen Endfläche 43 versehen. Zur Lagesicherung des Osenteils in den Werkzeugen 31, 33 dient ein im Umfangsb er eich des Zentraleinsatzes 33 angeordnetes Halteelement 44, welches im vorliegenden Fall aus einem radial nach außen federbelasteten Stift besteht. Zwischen die beiden Werkzeugteile 31, 32 wird die Trägerbahn 20 eingelegt, die zunächst ungelocht ist. Die vorerwähnten Federn 56 halten den Druckring 34 in einer definierten, aus Fig. 6 erkennbare Ausgangslage Beim Hubmaximum der Werkzeuge befindet sich die maßgebliche Oberseite 45 des Druckrings 34 oberhalb oder zweckmäßigerweise in gleicher Höhe mit einer im Schneidwerkzeug 32 vorgesehenen Schneidkante 42. Dadurch entsteht am Druckring 34 eine aus Fig. 6 erkennbare strichpunktiert verdeutlichte horizontale Stützebene 60 für die Trägerbahn 20.After the insertion of the eyelet 10, the end of the neck 20 is supported on the peripheral surface of the central insert 33. The central insert 33 is provided with a flat end surface 43. To secure the position of the eyelet in the tools 31, 33, a holding element 44 is arranged in the circumferential area of the central insert 33, which in the present case consists of a pin which is spring-loaded radially outwards. Between the two tool parts 31, 32, the carrier web 20 is inserted, which is initially unperforated. The aforementioned springs 56 hold the pressure ring 34 in a defined starting position, which can be seen in FIG. 6. At the maximum stroke of the tools, the relevant upper side 45 of the pressure ring 34 is above or expediently at the same height with a cutting edge 42 provided in the cutting tool 32. This results in the pressure ring 34, a horizontal support plane 60 for the carrier web 20, which is illustrated in FIG.
Beim Abwärtshub 37 der oberen Werkzeuggruppe 31, 33, 54 trifft zunächst der voreilende Gegendruckring 54 auf die über dem Druckring 34 liegende Trägerbahn 20. Die beiden Ringe 34, 54 sind mit im wesentlichen zueinander parallel verlaufenden Schrägen 58 und 59 versehen, welche die Trägerbahn 20 zwischen sich fassen, wodurch die Trägerbahn 20 zunächst leicht gespannt wird. Die Schrägfläche 58 des Druckrings 34 verläuft in einem spitzen Winkel 61 gegenüber der strichpunktiert in Fig. 6 verdeutlichten Stützebene 60, welche von der zur Auflage der Trägerbahn 20 dienenden Stirnfläche 45 des Druckrings 34 bestimmt ist. Die Gegendruckfläche 59 des erwähnten Druckrings 54 verläuft im wesentlichen parallel zur Druckfläche 58. Beim Gegeneinanderfahren 37 der beiden Werkzeuge 31, 32 wird daher die Trägerbahn 20 um die Kante 62 gezogen, welche zwischen der Stirnfläche 45 und der Schrägfläche 58 des Druckrings 34 entsteht. Dadurch wird die Trägerbahn im zu lochenden Bereich 29 glatt gezogen. Die Trägerbahn 20 nimmt folglich eine Strecklage in der erwähnten Stützebene 60 ein.During the downward stroke 37 of the upper tool group 31, 33, 54, the leading counter-pressure ring 54 first meets the carrier web 20 lying above the pressure ring 34. The two rings 34, 54 are provided with bevels 58 and 59 which run essentially parallel to one another and which support the carrier web 20 grasp between them, whereby the carrier web 20 is initially slightly tensioned. The inclined surface 58 of the pressure ring 34 extends at an acute angle 61 with respect to the support plane 60 illustrated in dash-dot lines in FIG. 6, which is determined by the end face 45 of the pressure ring 34 serving to support the carrier web 20. The counter pressure surface 59 of the pressure ring 54 mentioned runs essentially parallel to the pressure surface 58. When the two tools 31, 32 move against one another, the carrier web 20 is therefore drawn around the edge 62, which is formed between the end face 45 and the inclined surface 58 of the pressure ring 34. As a result, the carrier web is pulled smooth in the area 29 to be punched. The carrier web 20 consequently assumes an extended position in the support plane 60 mentioned.
Dann trifft der durch den Pressenstößel belastete Zentraleinsatz 33 auf die nach oben weisende Schauseite 23 der Trägerbahn 20 und drückt diese gegen die auf der Trägerunterseite 24 ruhende Schneidkante 42 vom Unterwerkzeug 32. Dadurch wird ein kreisförmiger Loch-Stanzling aus der Trägerbahn 20 ausgeschnitten. Dabei ist der von der Schneidkante 42 bestimmte Lochradius 46 kleiner als der mit 26 in Fig. 6 gekennzeichnete Halsradius 26 des Ösen-Halses 12.Then the central insert 33 loaded by the press ram hits the upward facing side 23 of the carrier web 20 and presses it against the cutting edge 42 of the lower tool 32 resting on the carrier underside 24. A circular punched hole is thereby cut out of the carrier web 20. The hole radius 46 determined by the cutting edge 42 is smaller than the neck radius 26 of the eyelet neck 12 identified by 26 in FIG. 6.
Wenn das Oberwerkzeug 31 weiter in Richtung des Hubbewegungspfeils 37 sich absenkt, wird die Trägerbahn 20 fester zwischen den beiden Schrägen 58, 59 der beiden Ringe 34, 54 eingespannt. Dabei fährt der Hals 12 vom Osenteil 10 durch das entstehende Loch ins Unterwerkzeug, bis der Teller 11 vom Osenteil 10, unter Zwischenschaltung der Trägerbahn 20, auf den Druckring 34 aufsetzt. Bei dieser Abwärtsbewegung 37 überwindet das Oberwerkzeug 31 die Federkraft 36 vom unterseitigen Druckring 34 und es erfolgt die Bordelung vom Ösen-Hals 12 und der axialen Vorsprünge 16 am Bördelprofil 47 des Unterwerkzeugs 32. Die Federkraft 54 vom oberseitigen Druckring 54 ist kleiner als die auf den Druckring 34 wirkende Ausschubkraft 36. Ähnlich wie beim Oberwerkzeug 31 besitzt auch das Unterwerkzeug 32 einen im Axialbereich positionierten Einsatz 32', welcher das maßgebliche Bördelprofil 47 besitzt. Dieses Bördelprofil 47 verschleißt nämlich nach längerem Gebrauch. Dann genügt es lediglich diesen Einsatz 32' zu ersetzen.If the upper tool 31 lowers further in the direction of the lifting movement arrow 37, the carrier web 20 becomes firmer between the two bevels 58, 59 of the two rings 34, 54 clamped. The neck 12 moves from the eyelet 10 through the hole formed in the lower tool until the plate 11 from the eyelet 10, with the interposition of the carrier web 20, touches the pressure ring 34. During this downward movement 37, the upper tool 31 overcomes the spring force 36 from the lower pressure ring 34 and the eyelet neck 12 and the axial projections 16 on the flanged profile 47 of the lower tool 32 are flattened. The spring force 54 from the upper pressure ring 54 is smaller than that on the Thrust ring 34 acting ejection force 36. Similar to the upper tool 31, the lower tool 32 also has an insert 32 'which is positioned in the axial region and which has the relevant flanged profile 47. This flared profile 47 wears out after prolonged use. Then it is sufficient to replace this insert 32 '.
Bei der Bordelung ergeben sich die besonderen, aus Fig. 3 ersichtlichen Nietverhältnisse. Es wird praktisch die ganze, aus Fig. 4 ersichtliche Halslänge 48 des Osenteils zu einem aus Fig. 3 erkennbaren Ringprofil 50 auf der Rückseite 24 der Trägerbahn 20 eingerollt. Dabei werden die Halsvorsprünge 16 in diese Ringbildung 50 einbezogen. Unter Zwischenschaltung des erwähnten und auch in Fig. 6 angedeuteten Lochrandbereichs 21 der Trägerbahn 20 werden diese Halsvorsprünge 16 gegen eine von der geschilderten Wölbung 13 des Tellers 11 erzeugten Widerlagerfläche 49 angedrückt. Es kommt dort zu den aus Fig. 3 erkennbaren ringförmig umlaufenden Andruckstellen 40. Im Ringprofilinneren 51 läuft die Trägerbahn 20 mit einer Endzone 41 weiter, die sich ringsegmentartig dem Profil 50 anpasst. Auch beim Einrollen der Endzone 41 während des Nietvorgangs halten die Schrägen 58, 59 die Trägerbahn 20 fest.The special riveting relationships shown in FIG. 3 result from the bordering. Practically the entire neck length 48 of the eyelet part shown in FIG. 4 is rolled into an annular profile 50 recognizable in FIG. 3 on the rear side 24 of the carrier web 20. The neck projections 16 are included in this ring formation 50. With the interposition of the hole edge region 21 of the carrier web 20 mentioned and also indicated in FIG. 6, these neck projections 16 are pressed against an abutment surface 49 generated by the described curvature 13 of the plate 11. The ring-shaped circumferential pressure points 40 can be seen there from FIG. 3. In the ring profile interior 51, the carrier web 20 continues with an end zone 41, which adapts to the profile 50 in the manner of a ring segment. Even when the end zone 41 rolls in during the riveting process, the bevels 58, 59 hold the carrier web 20 in place.
Beim bestimmungsgemäßen Gebrauch des an der Trägerbahn 20 angesetzten Osenteils ergeben sich durch die Kraftpfeile 52 in den Fig. 1 bis 3 verdeutlichte Zugbelastungen. Diese Zugbelastungen 52 werden von den Andruckstellen 40 aufgenommen. An den Andruckstellen 40 liegt zunächst eine Klemmwirkung zwischen den Halsvorsprüngen 16 und der Widerlagerfläche 49 vor. Darüber hinaus ist wegen der beschriebenen Profilierung 19 dieser Vorsprünge 16 auch eine Formschlüssigkeit gegeben. Die Zahnspitzen 17 dringen in das Bahnmaterial ein, jedoch kommt es wegen der Rundungen 27, 28 des Zahnprofils 19 zu keiner Rissbildung in der Bahn 20. Eine Kerbwirkung wird dadurch vermieden. Vor den Zahnspitzen und auch in den gewölbten Zahnlücken 18 entsteht jenseits dieser Andruckstellen 40 eine mit 53 in Fig. 3 bezeichnete stufenartige Erhöhung der Bahnstärke. Die Bahn 40 ist nämlich bei 53 bestrebt wieder auf ihre ursprüngliche Bahnstärke 25 sich zu erheben. Bei den Zugbelastungen 52 der Bahn 20 verkrallen sich diese stufenartigen Erhöhungen 53 des Bahnmaterials 20 an den wellenförmigen Kanten der Halsvorsprünge 16. Dadurch wird der Formschluss erhöht und eine überraschend hohe Zugfestigkeit des angenieteten Osenteils 10' an der Bahn 20 erreicht. When the eyelet part attached to the carrier web 20 is used as intended, the force arrows 52 in FIGS. 1 to 3 show tensile loads which are illustrated. These tensile loads 52 are absorbed by the pressure points 40. At the pressure points 40 there is initially a clamping effect between the neck projections 16 and the abutment surface 49. In addition, because of the described profiling 19 of these projections 16, there is also a positive fit. The tooth tips 17 penetrate into the web material, however, because of the curves 27, 28 of the tooth profile 19, there is no formation of cracks in the web 20. A notching effect is thereby avoided. Before Tooth tips and also in the arched tooth gaps 18, beyond these pressure points 40, there is a step-like increase in the web thickness designated 53 in FIG. 3. The web 40 is in fact endeavored to rise back to its original web thickness 25 at 53. With the tensile loads 52 of the web 20, these step-like elevations 53 of the web material 20 cling to the wavy edges of the neck projections 16. This increases the positive fit and achieves a surprisingly high tensile strength of the riveted eyelet part 10 ′ on the web 20.
B e z u g s z e i c h e n l i s t e :B e z u g s z e i c h e n l i s t e:
Osenteil (Ausgangszustand; Fig. 4) ' Nietzustand von 10 (Fig. 1 bis 3) Teller von 10 Hals von 10, Ösenhals Wölbungsprofil von 11 bogenförmiger Übergang zwischen 11, 12 Endstück von 12 axialer Halsvorsprung bei 15 (Fig. 4) Zahnspitze (Fig. 5) Zahnlücke Zahnprofil bei 15 (Fig. 5) Trag erb ahn Lo chrandb er eich von 20 Loch in 20 (Fig. 1, 2) Schauseite von 20 Rückseite von 20 Bahnstärke von 20 (Fig. 6) Halsradius von 12 (Fig. 6) konvexe Rundung von 17 (Fig. 5) konkave Rundung von 18 (Fig. 5) Lochstanzling aus 20 (Fig. 6) Vorrichtung Oberwerkzeug von 30 ' austauschbarer Einsatz in 31 Unterwerkzeug von 30 ' austauschbarer Einsatz in 32 Zentral einsatz in 31 Druckring in 33 Kraftbelastungspfeil von 33 Pfeil der Federkraft von 34 Hubewegungspfeil von 31 gegenüber 32 (Fig. 6) maximaler Hubabstand zwischen 31, 32 Aufnahme in 31 für 11 Andruckstelle von 20 zwischen 16, 49 (Fig. 3) Endzone von 20 jenseits von 40 (Fig. 3) Schneidkante an 32 ebene Stirnfläche von 33 (Fig. 6) Halteelement für 10 bei 33 (Fig. 6) Stirnfläche für 20 an 34 Lochradius von 29 (Fig. 6) Bördelprofil in 32 (Fig. 6) Halslänge von 12 (Fig. 4) Widerlagerfläche an 11 für 16 (Fig. 3) Ringprofil von 12 bei 10' (Fig. 3) Ringprofil-Inneres von 50 (Fig. 4) Pfeil der Zugbelastung auf 20 stufenförmige Erhöhung von 20 hinter 40 (Fig. 3) Gegendruckring Kraftbelastung von 54 Feder für 36 Stift an 34 für 56 Schräge von 34, Schrägfläche Gegenschräge von 54, Gegenschrägfläche Stützebene Winkelverlauf von 58 gegenüber von 45 Kante zwischen 45, 58 von 34 Umfangsfläche von 31 Druckfeder Flansch Ausschnitt Kopf von 68 Führungsstange Gewindeeingriff Ausschublänge Sicherungsmutter Outer part (initial state; Fig. 4) 'riveted state of 10 (Fig. 1 to 3) plate of 10 neck of 10, eyelet neck arch profile of 11 arcuate transition between 11, 12 end piece of 12 axial neck protrusion at 15 (Fig. 4) tooth tip ( Fig. 5) Tooth gap tooth profile at 15 (Fig. 5) Wear Erb ahn Lo chrandb er eich of 20 holes in 20 (Fig. 1, 2) face of 20 back of 20 web thickness of 20 (Fig. 6) neck radius of 12 ( Fig. 6) convex rounding of 17 (Fig. 5) concave rounding of 18 (Fig. 5) punched die from 20 (Fig. 6) device upper tool from 30 'interchangeable insert in 31 lower tool from 30' interchangeable insert in 32 central insert in 31 pressure ring in 33 force load arrow of 33 arrow of spring force of 34 stroke movement arrow of 31 versus 32 (FIG. 6) maximum stroke distance between 31, 32 receptacle in 31 for 11 pressure point of 20 between 16, 49 (Fig. 3) end zone of 20 beyond 40 (Fig. 3) cutting edge on 32 flat end face of 33 (Fig. 6) holding element for 10 at 33 (FIG. 6) end face for 20 to 34 hole radius of 29 (FIG. 6) flare profile in 32 (FIG. 6) neck length of 12 (FIG. 4) abutment surface on 11 for 16 (FIG. 3) ring profile of 12 at 10 '(Fig. 3) ring profile interior of 50 (Fig. 4) arrow of tensile load on 20 step increase from 20 behind 40 (Fig. 3) counter pressure ring force load of 54 spring for 36 pin on 34 for 56 slope of 34, slope slope counter slope of 54, counter bevel surface support plane angle course of 58 opposite 45 edge between 45, 58 of 34 circumferential surface of 31 compression spring flange cutout head of 68 guide rod threaded engagement extension length lock nut

Claims

Patentansprüche Patent claims
1.) Öse zum Verstärken des Randbereichs (21) um ein Loch (22) in einer Trägerbahn (20),1.) Eyelet for reinforcing the edge area (21) around a hole (22) in a carrier web (20),
mit einem scheibenlosen Osenteil (10, 10'), der aus einem auf der Schauseite (23) der Trägerbahn (20) aufliegenden Teller (11), aus einem das Loch (22) durchsetzenden rohrformigen Hals (12) und aus einem bogenförmigen Übergang (14) zwischen Teller (11) und Hals (12) besteht,with a discless eyelet part (10, 10'), which consists of a plate (11) resting on the visible side (23) of the carrier web (20), a tubular neck (12) passing through the hole (22) and an arcuate transition ( 14) exists between the plate (11) and neck (12),
wobei das freie Endstück (15) des Halses (12) mit Vorsprüngen (16) versehen ist,wherein the free end piece (15) of the neck (12) is provided with projections (16),
und mit einer auf der Rückseite (24) der Trägerbahn (20) sich abstützenden Bordelung des Halses (12) des Osenteils (10'),and with a border of the neck (12) of the eyelet part (10') which is supported on the back (24) of the carrier web (20),
dadurch gekennzeichnet ,characterized ,
dass die Halsvorsprünge (16) in axialer und/oder radialer Richtung verlaufen,that the neck projections (16) run in the axial and/or radial direction,
dass die vollzogene Umbördelung des Halses (12) ein im wesentlichen in sich geschlossenes Ringprofil (50) aufweist, in welches das die Halsvorsprünge (16) aufweisende Endstück (15) integriert ist,that the completed flanging of the neck (12) has a substantially self-contained ring profile (50) into which the end piece (15) having the neck projections (16) is integrated,
dass unter Zwischenschaltung des Lochrandbereiches (21) der Trägerbahn (20) die Halsvorsprünge (16) im Ringprofil (50) an vom Teller (11) oder vom Übergang (14) gebildeten Widerlagerflächen (49) angedrückt sind und Andruckstellen (40) an der erfassten Trägerbahn (20) erzeugen, gegen die sich die Trägerbahn (20) bei Zugbelastungen (52) stellt,that with the interposition of the hole edge area (21) of the carrier web (20), the neck projections (16) in the ring profile (50) are pressed against abutment surfaces (49) formed by the plate (11) or the transition (14) and pressure points (40) on the detected Generate a carrier web (20) against which the carrier web (20) stands under tensile loads (52),
und dass die Trägerbahn (20) im Ringprofil-Inneren (51) über die Andruckstellen (40) hinaus bis zu ihrer Lochkante weiterläuft (41). and that the carrier web (20) continues in the ring profile interior (51) beyond the pressure points (40) to its hole edge (41).
2.) Öse nach Anspruch 1, dadurch gekennzeichnet, dass die axialen Halsvorsprünge (16) aus einer gezahnten Endkante (19) des Halses (12) bestehen.2.) Eyelet according to claim 1, characterized in that the axial neck projections (16) consist of a toothed end edge (19) of the neck (12).
3.) Öse nach Anspruch 2, dadurch gekennzeichnet, dass die Zahnspitzen (17) konvex und die Zahnlücken (18) konkav gerundet sind3.) Eyelet according to claim 2, characterized in that the tooth tips (17) are convex and the tooth gaps (18) are concavely rounded
und dass beide Rundungen (27, 28) einen Wellenverlauf der Zahnkante (19) bestimmen.and that both curves (27, 28) determine a wave shape of the tooth edge (19).
4.) Öse nach Anspruch 3, dadurch gekennzeichnet, dass die Zahnkante (19) einen unsymmetrischen Wellenverlauf aufweist.4.) Eyelet according to claim 3, characterized in that the toothed edge (19) has an asymmetrical wave shape.
5.) Öse nach Anspruch 3 oder 4, dadurch gekennzeichnet, dass die konvexen Rundungen (27) der Zahnspitzen (17) kleiner als die konkaven Rundungen (28) der Zahnlücken (18) ausgebildet sind.5.) Eyelet according to claim 3 or 4, characterized in that the convex curves (27) of the tooth tips (17) are smaller than the concave curves (28) of the tooth gaps (18).
6.) Öse nach einem der Ansprüche 1 bis 5, dadurch gekennzeichnet, dass das Material der Trägerbahn (20) flexibel und/oder dehnfähig ausgebildet ist.6.) Eyelet according to one of claims 1 to 5, characterized in that the material of the carrier web (20) is designed to be flexible and / or stretchable.
7.) Öse nach Anspruch 6, dadurch gekennzeichnet, dass die Trägerbahn (20) aus einer Segeltuch-Plane besteht.7.) Eyelet according to claim 6, characterized in that the carrier web (20) consists of a canvas tarpaulin.
>.) Öse nach Anspruch 6, dadurch gekennzeichnet, dass die Trägerbahn (20) aus einer verstärkten Kunststoff-Folie besteht. >.) Eyelet according to claim 6, characterized in that the carrier web (20) consists of a reinforced plastic film.
.) Öse nach einem der Ansprüche 1 bis 8, dadurch gekennzeichnet, dass gegenüber der lichten Weite zwischen den diametralen Ringprofilen (50) des umbördelten Halses (12) der Lochdurchmesser (49) der Trägerbahn (20) kleiner ausgebildet ist..) Eyelet according to one of claims 1 to 8, characterized in that the hole diameter (49) of the carrier web (20) is smaller compared to the clear width between the diametrical ring profiles (50) of the flanged neck (12).
10.) Vorrichtung (30) zum Ansetzen von Osenteilen (10) an einer Trägerbahn (20) nach einem der Ansprüche 1 bis 9,10.) Device (30) for attaching eyelet parts (10) to a carrier web (20) according to one of claims 1 to 9,
mit einem das Bördelprofil (47) für den Hals (12) des Osenteils (10) aufweisenden Unterwerkzeug (32),with a lower tool (32) having the flanged profile (47) for the neck (12) of the eyelet part (10),
mit einem das Osenteil (10) aufnehmenden Oberwerkzeug (31), welches relativ zum Unterwerkzeug (32) hubbeweglich (37) ist,with an upper tool (31) which accommodates the eye part (10) and is movable (37) relative to the lower tool (32),
wobei zwischen den beiden Werkzeugen (31, 32) die Trägerbahn (20) positioniert wird,the carrier web (20) being positioned between the two tools (31, 32),
d a d u r c h g e k e n n z e i c h n e t ,characterized ,
dass das Oberwerkzeug (31) mit einem gegen eine Federkraft (35) axialbeweglichen Zentraleinsatz (33) versehen ist, der eine Stirnfläche (43) aufweist,that the upper tool (31) is provided with a central insert (33) which is axially movable against a spring force (35) and has an end face (43),
dass die Stirnfläche (43) des Zentraleinsatzes (33) im wesentlichen eben ausgebildet und frei von die Trägerbahn (20) tief ziehenden Vorziehzapfen ist,that the end face (43) of the central insert (33) is essentially flat and free of the pulling pins that pull the carrier web (20) deep,
dass das Unterwerkzeug (32) eine ringförmige Schneidkante (42) aufweist, die mit der Stirnfläche (43) des Zentraleinsatzes (33) lochschneidend (29) auf die dazwischenliegende Trägerbahn (20) wirkt,that the lower tool (32) has an annular cutting edge (42), which acts with the end face (43) of the central insert (33) to cut holes (29) on the carrier web (20) in between,
und dass der Lochradius (46) der Schneidkante (42) kleiner als der Außenradius (26) vom Hals (12) des Osenteils (10) ausgebildet ist. and that the hole radius (46) of the cutting edge (42) is smaller than the outer radius (26) of the neck (12) of the eye part (10).
1.) Vorrichtung nach Anspruch 10, dadurch gekennzeichnet, dass im Unterwerkzeug (32) ein Druckring (34) in radialem Abstand zum Bördelprofil (47) angeordnet und in Richtung des Oberwerkzeugs (31) kraftbelastet (36) ist,1.) Device according to claim 10, characterized in that a pressure ring (34) is arranged in the lower tool (32) at a radial distance from the flanged profile (47) and is force-loaded (36) in the direction of the upper tool (31),
dass - im Hubmaximum der beiden Werkzeuge (31, 32) gesehen - der Druckring (34) sich im wesentlichen im Höhenbereich der Schneidkante (42) vom Unterwerkzeug (32) befindetthat - seen at the maximum stroke of the two tools (31, 32) - the pressure ring (34) is essentially in the height range of the cutting edge (42) of the lower tool (32).
und dass der Druckring (34) eine Stützebene (60) für die zwischen die beiden Werkzeuge (31, 32) zu platzierende Trägerbahn (20) erzeugt.and that the pressure ring (34) creates a support plane (60) for the carrier web (20) to be placed between the two tools (31, 32).
12.) Vorrichtung nach Anspruch 11, dadurch gekennzeichnet, dass eine wendeiförmige Druckfeder eine ringförmige Endfläche aufweist12.) Device according to claim 11, characterized in that a helical compression spring has an annular end surface
und dass diese Ringendfläche den Druckring (34) bildet und die Druckfeder die Kraftbelastung (36) erzeugt.and that this ring end surface forms the pressure ring (34) and the compression spring generates the force load (36).
13.) Vorrichtung nach einem der Ansprüche 10 bis 12, dadurch gekennzeichnet, dass dem Druckring (34) ein Gegendruckring (54) im Oberwerkzeug (31) zugeordnet und auf das Unterwerkzeug (32) hin kraftbelastet (55) ist13.) Device according to one of claims 10 to 12, characterized in that the pressure ring (34) is assigned a counter-pressure ring (54) in the upper tool (31) and is force-loaded (55) on the lower tool (32).
und dass die Trägerbahn (20) bei der Hubbewegung (37) zwischen den beiden Ringen (34, 54) eingespannt wird.and that the carrier web (20) is clamped between the two rings (34, 54) during the lifting movement (37).
14.) Vorrichtung nach Anspruch 13, dadurch gekennzeichnet, dass zum Einspannen der Trägerbahn (20) die beiden Ringe (34, 54) mit zwei gegeneinander weisenden Schräg- und Gegenschrägflächen (58, 59) versehen sind. 14.) Device according to claim 13, characterized in that for clamping the carrier web (20), the two rings (34, 54) are provided with two mutually facing inclined and counter-inclined surfaces (58, 59).
5.) Vorrichtung nach Anspruch 14, dadurch gekennzeichnet, dass die Schrägfläche (58) in einem in Hubrichtung (37) weisenden spitzen Winkel (61) gegenüber der Stützebene (60) verläuft, welche von der Stützfläche (45) des Druckrings (34) bestimmt,5.) Device according to claim 14, characterized in that the inclined surface (58) runs at an acute angle (61) pointing in the lifting direction (37) with respect to the support plane (60), which extends from the support surface (45) of the pressure ring (34). certainly,
und dass die Gegenschrägfläche (59) des Gegendruckrings (54) im wesentlichen parallel zur Schrägfläche (58) des Druckrings (34) verläuft.and that the counter-inclined surface (59) of the counter-pressure ring (54) runs essentially parallel to the oblique surface (58) of the pressure ring (34).
16.) Vorrichtung nach einem der Ansprüche 10 bis 15, dadurch gekennzeichnet, dass das Oberwerkzeug (31) und/oder das Unterwerkzeug (32) mit Einsätzen (31 ' bzw. 32') versehen sind, welche die Aufnahme (39) und/oder die Bördelprofile (47) für den Osenteil (10) aufweisen. 16.) Device according to one of claims 10 to 15, characterized in that the upper tool (31) and / or the lower tool (32) are provided with inserts (31 'or 32') which hold the receptacle (39) and / or have the flanged profiles (47) for the eyelet part (10).
EP01960266A 2000-08-12 2001-06-02 Eyelet for reinforcing the edge of a hole in a carrier strip and device for attaching an eyelet to a carrier strip Expired - Lifetime EP1309256B1 (en)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
DE10039462A DE10039462C5 (en) 2000-08-12 2000-08-12 An eyelet for reinforcing the edge area around a hole in a carrier web and a device for attaching the eyelet to a carrier web
DE10039462 2000-08-12
DE20104102U DE20104102U1 (en) 2000-08-12 2001-03-09 Eyelet for reinforcing the edge area around a hole in a carrier web and device for attaching the eyelet to a carrier web
DE20104102U 2001-03-09
PCT/EP2001/006316 WO2002013646A1 (en) 2000-08-12 2001-06-02 Eyelet for reinforcing the edge of a hole in a carrier strip and device for attaching an eyelet to a carrier strip

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EP1309256A1 true EP1309256A1 (en) 2003-05-14
EP1309256B1 EP1309256B1 (en) 2004-12-29

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EP (1) EP1309256B1 (en)
CN (1) CN1209987C (en)
AT (1) ATE285688T1 (en)
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CA (1) CA2418293A1 (en)
CZ (1) CZ200370A3 (en)
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JP5808346B2 (en) * 2011-01-13 2015-11-10 Ykk株式会社 Eyelet installation method
JP5996245B2 (en) * 2012-04-17 2016-09-21 モリト株式会社 How to install the eyelet on the fabric
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JP6634098B2 (en) * 2015-06-30 2020-01-22 サン−ゴバン パフォーマンス プラスティックス コーポレイション Sliding bearing
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CN1446061A (en) 2003-10-01
US6907647B2 (en) 2005-06-21
CA2418293A1 (en) 2003-02-04
CN1209987C (en) 2005-07-13
DE20112908U1 (en) 2001-11-08
PL360079A1 (en) 2004-09-06
ES2230351T3 (en) 2005-05-01
WO2002013646A1 (en) 2002-02-21
EP1309256B1 (en) 2004-12-29
ATE285688T1 (en) 2005-01-15
MXPA03000586A (en) 2004-12-13
US20030167610A1 (en) 2003-09-11
CZ200370A3 (en) 2003-06-18
PL203329B1 (en) 2009-09-30
AU2001281804A1 (en) 2002-02-25

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