EP1309256B1 - 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 Download PDFInfo
- Publication number
- EP1309256B1 EP1309256B1 EP01960266A EP01960266A EP1309256B1 EP 1309256 B1 EP1309256 B1 EP 1309256B1 EP 01960266 A EP01960266 A EP 01960266A EP 01960266 A EP01960266 A EP 01960266A EP 1309256 B1 EP1309256 B1 EP 1309256B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- eyelet
- carrier web
- neck
- ring
- edge
- 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.)
- Expired - Lifetime
Links
Classifications
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- A—HUMAN NECESSITIES
- A44—HABERDASHERY; JEWELLERY
- A44B—BUTTONS, PINS, BUCKLES, SLIDE FASTENERS, OR THE LIKE
- A44B13/00—Hook or eye fasteners
- A44B13/0058—Eyelets or grommets
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- A—HUMAN NECESSITIES
- A41—WEARING APPAREL
- A41H—APPLIANCES OR METHODS FOR MAKING CLOTHES, e.g. FOR DRESS-MAKING OR FOR TAILORING, NOT OTHERWISE PROVIDED FOR
- A41H37/00—Machines, appliances or methods for setting fastener-elements on garments
- A41H37/02—Setting hooks or eyes
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- A—HUMAN NECESSITIES
- A44—HABERDASHERY; JEWELLERY
- A44B—BUTTONS, PINS, BUCKLES, SLIDE FASTENERS, OR THE LIKE
- A44B13/00—Hook or eye fasteners
- A44B13/0058—Eyelets or grommets
- A44B13/0076—Eyelets or grommets characterised by their way of fastening to the support
- A44B13/0082—Eyelets or grommets characterised by their way of fastening to the support by riveting
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- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T24/00—Buckles, buttons, clasps, etc.
- Y10T24/34—Combined diverse multipart fasteners
- Y10T24/3427—Clasp
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T24/00—Buckles, buttons, clasps, etc.
- Y10T24/36—Button with fastener
- Y10T24/3628—Integral or rigid stud
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T24/00—Buckles, buttons, clasps, etc.
- Y10T24/36—Button with fastener
- Y10T24/3681—Tufting type
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T24/00—Buckles, buttons, clasps, etc.
- Y10T24/37—Drawstring, laced-fastener, or separate essential cooperating device therefor
- Y10T24/3742—Drawstring, laced-fastener, or separate essential cooperating device therefor having eyelet type directing means
- Y10T24/3745—Drawstring, laced-fastener, or separate essential cooperating device therefor having eyelet type directing means with permanently deformed mounting structure
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T24/00—Buckles, buttons, clasps, etc.
- Y10T24/37—Drawstring, laced-fastener, or separate essential cooperating device therefor
- Y10T24/3742—Drawstring, laced-fastener, or separate essential cooperating device therefor having eyelet type directing means
- Y10T24/3745—Drawstring, laced-fastener, or separate essential cooperating device therefor having eyelet type directing means with permanently deformed mounting structure
- Y10T24/3747—Mounting structure formed from different material than directing passage
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T24/00—Buckles, buttons, clasps, etc.
- Y10T24/37—Drawstring, laced-fastener, or separate essential cooperating device therefor
- Y10T24/3768—Drawstring, laced-fastener, or separate essential cooperating device therefor having loop or sleeve shaped directing means
- Y10T24/3779—Drawstring, laced-fastener, or separate essential cooperating device therefor having loop or sleeve shaped directing means with permanently deformed mounting structure
- Y10T24/3782—Loop or sleeve closed when mounted
Definitions
- the invention is initially directed to an eyelet for reinforcing the rim around a hole in a track.
- two-part eyelets (EP 0 655 205 B1, US Pat. No. 4,479,287 A, FIGS. 1, 12) which consist of an eyelet part and a disk part are used for this purpose.
- the eyelet has a plate that comes to rest on the show side of the carrier side when riveting, while sitting on a plate tubular neck cuts a hole in the carrier web and is crimped more or less C-shaped with its free end. By flanging the tail of the neck is stiffened. The rigid end piece is supported on the disc part, whereby the carrier web is compressed between the disc part and the plate.
- a riveted two-piece eyelet has insufficient tear resistance.
- the carrier web assumes a labyrinth course between the annular rib and the neck end edge in the interior between the arcuate plate and the C-profile of the neck.
- DE 669 779 A the C-shaped neck flared with its smooth End edge pressed substantially vertically into the carrier web. To avoid bursting the neck end piece when crimping, the neck od without any incision. The like. Be formed. When flanging radial riveting in the folded eyelet edge are impressed by the riveting tool, which should strengthen the crimp end. Due to the corrugated flanging end, the bending stiffness of the neck end piece already produced by the C profile is further increased, so that the folded loop edge can penetrate vertically into the surface of the carrier web.
- the pull-out strength of such one-piece eyelets with a C-shaped flared neck has no higher tear resistance than the two-part eyelet mentioned at the outset.
- the invention has for its object to develop an inexpensive, quickly attachable eyelet specified in the preamble of claim 1 species, which is characterized by a high pull-out strength after Annieten on the carrier web. This is inventively achieved by the measures listed in claim 1, which have the following special significance.
- the flexural rigidity of the beaded edge is reduced in the eyelet according to the invention.
- the bendable neck projections are taken, spread apart with respect to the axis of the riveted eyelet apart and against the circumferential Abutment surface of the plate pressed.
- the tongue-like neck projections thus act as "spreading clamps", which are increasingly pressed against the carrier web with increasing pull-out force.
- a 30% to 75% higher tear resistance is especially true when riveting in flexible or stretchable carrier webs that could not be satisfactorily equipped with a one-piece eyelet so far.
- the neck projections are already co-produced in the production of the eyelet, whereby special operations or processing tools for profiling can be saved.
- the tooth digs into the web material and it can come to a step-like increase along the tooth profile. Apart from the aforementioned Sp Schwarzklemmung it then comes to a positive connection between the tooth and the carrier web. The higher the tensile load applied to the carrier web, the stronger the carrier web digs in front of the antiparallel tooth.
- the invention is further directed to a device for attaching the eyelet according to the invention.
- the known device (US 1,838,973 A), which is, however, intended for two-piece eyelets, jump the pressure ring in the lower tool against the local cutting edge.
- the upper tool has an axially movable central insert with a bore that projects axially relative to the adjacent surfaces of the upper tool.
- the carrier web is pressed into the pressure ring by the central insert of the upper tool; before the central insert hits the cutting edge of the lower tool and thereby cuts the hole in the carrier web.
- the carrier web is in the local two-piece eyelet, which also has the part already mentioned above except the eyelet unsightly attached. It comes to wrinkles in the carrier web.
- the invention is therefore based on the further object of developing a device for the one-piece eyelet mentioned in claim 1, which can be fastened beautiful and tear-resistant to the carrier web.
- This is inventively achieved by the measures mentioned in the characterizing part of claim 9, which have the following special significance.
- the pressure ring in the lower tool in the opposite direction kraftbetasteter counter-pressure ring in the upper tool is assigned. It is recommended, according to claim 10, to provide these two rings with mutually facing oblique and Gegenschrägvid.
- the carrier web is clamped between these two rings, wherein the inclined surfaces provide for an additional smooth pulling of the carrier web. This will maintain a smooth course of the carrier web during subsequent crimping of the one-piece eyelet, resulting in a proper attachment of the eyelet to the carrier web. Clamping minimizes material feed. This has the consequence that the pitches between the eyelets can be maintained exactly and the tolerance deviations are greatly limited even over long tarpaulin lengths.
- FIGS. 1 and 2 An eye should, as shown in FIGS. 1 and 2, reinforce the edge region 21 of a hole 22 cut in a carrier web 20.
- the carrier web 20 is usually a flexible and optionally stretchable structure, eg a motor vehicle tarpaulin.
- the invention achieves the desired hole reinforcement with a one-piece eyelet 10.
- Fig. 4 and 5 the eyelet 10 is shown in its initial state, before the Processing.
- FIGS. 1, 2 and 3 show the eyelet part 10 'after its processing, in the finished state of use, during its hole reinforcing function.
- the eyelet 10 can be divided into a curved, substantially radially extending plate 11 and an axially extending tubular neck 12.
- annular flange of the neck 12 of the plate 11 is provided with a buckling profile 13. This results in a particularly conspicuous arcuate transition 14 between the plate 11 and the neck 12.
- the neck is provided in its free end 15 with axial, so in the direction of the neck 12 extending projections 16. These consist in the present case of a recognizable in Fig. 5 arcuate toothed end edge 17. This has the following special appearance.
- the tooth tips 17 are provided with convex curves 27, while the tooth spaces 18 have concave curves 28. This results in the tooth profile 19 a waveform.
- the waveform is unbalanced. That is, the radius of curvature of the curves 27 of the tooth tips 17 is made smaller than that of the curves 28 of the tooth spaces.
- the device 30 consists of essentially five mutually axially displaceable parts with respect to time. This first includes a stationary in the present case lower tool 32, which carries a contrast axially movable pressure ring 34. Furthermore, the device 30 includes an upper tool 31 which is actively movable relative to the lower tool 32 and has a central insert 33 arranged coaxially therein, which, in contrast, is also passively axially movable. Finally, the upper tool 31 is enclosed in the peripheral region by a likewise axially passively axially movable counter-pressure ring 54.
- the central insert 33 and the counter-pressure 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, to a mirror image, in the sense of the force arrow 36 against the upper tool 31 under the action of a crowd of springs 56th stands, which are mounted in axial bores of the lower tool 32.
- the springs 56 are as Spiral springs formed in the helical interior of the pressure ring 34 seated pins 57 engage.
- the tool group 31, 33, 54 on the one hand and 32, 34 on the other hand are lift-movable relative to one another, as illustrated by the movement arrow 37 of the upper tool group 31, 33, 54.
- the counter-pressure ring 54 is guided on the circumferential 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 an edge of a peripheral flange 65 of the upper tool 31 and the abutting surface of a cutout 66 in the counter-pressure ring 54.
- the Ausschubposition of the counter-pressure ring 54 is determined by end stops. These consist in the present case of the head 67 of a family of guide rods 68 which are adjustable in length by threaded engagement 69 and a lock nut 71. The rod end 67 is supported at rest on the upper flank of the flange 65. As a result, the desired extension 70 of the counter-pressure ring 54 with respect to the upper tool 31 is determined.
- the upper reversal point of the lifting movement 37 is shown, where the upper tool 31 is opposite the lower tool 32 in the maximum stroke distance 38.
- an eyelet 10 can be easily used on the receiving profile of the upper tool 31 and central insert 33.
- the upper tool 31 has a profile of the plate 11 corresponding receptacle 39.
- the area provided with the receptacle 39 is subject to wear under normal use.
- the lower portion of the upper tool is provided with an insert 31 ', the od by the indicated screw.
- This insert 31 ' has the receptacle 39.
- the end of the neck 20 is supported on the peripheral surface of the central insert 33 from.
- the central insert 33 is provided with a flat end surface 43.
- 33 is used in the peripheral region of the central insert 33 arranged holding element 44, which consists in the present case of a spring-loaded pin radially outward.
- the carrier web 20 is inserted, which is initially unperforated.
- the above-mentioned springs 56 hold the pressure ring 34 in a defined, recognizable from Fig. 6 starting position
- the relevant top 45 of the pressure ring 34 is above or expediently at the same height with a provided cutting tool 32 cutting edge 42. This results in the pressure ring 34 a recognizable from Fig. 6 dash-dotted lines illustrated horizontal support plane 60 for the carrier web 20th
- the leading counterpressure ring 54 strikes the carrier web 20 lying above the pressure ring 34.
- the two rings 34, 54 are provided with ramps 58 and 59 extending essentially parallel to one another, which support web 20 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 relative to the dot-dash line in Fig. 6 clarified support plane 60, which is determined by the serving for supporting the carrier web 20 end face 45 of the pressure ring 34.
- the counter-pressure surface 59 of the mentioned pressure ring 54 extends substantially parallel to the pressure surface 58.
- the carrier web 20 is pulled 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 smoothly in the region 29 to be punched. The carrier web 20 thus assumes an extended position in the mentioned support plane 60.
- the loaded by the press ram central insert 33 hits the upwardly facing display side 23 of the carrier web 20 and presses against the resting on the support base 24 cutting edge 42 from the lower tool 32.
- a circular hole punched from the carrier web 20 is cut out.
- the hole radius 46 determined by the cutting edge 42 is smaller than the neck radius 26 of the eyelet neck 12 marked 26 in FIG. 6.
- the carrier web 20 is fixed between the two bevels 58, 59 of the clamped two rings 34, 54.
- the neck 12 moves from the eyelet 10 through the resulting hole in the lower tool until the plate 11 of 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-side pressure ring 34 and there is the curling of eyelet neck 12 and the axial projections 16 on the flaring profile 47 of the lower tool 32.
- the spring force 54 from the upper-side pressure ring 54 is smaller than that on the Pressure ring 34 acting Ausschubkraft 36.
- Similar to the upper tool 31 and the lower tool 32 has a positioned in the axial region insert 32 ', which has the relevant flare 47. This hemming profile 47 wears out after prolonged use. Then it is sufficient only to replace this insert 32 '.
- the web 40 is namely at 53 anxious again to raise their original track thickness 25 itself.
- these step-like elevations 53 of the web material 20 dig into the wavy edges of the neck projections 16.
- the positive connection is increased and a surprisingly high tensile strength of the riveted eyelet 10 'on the web 20 is achieved.
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- Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Insertion Pins And Rivets (AREA)
- Connection Of Plates (AREA)
- Clamps And Clips (AREA)
- Catalysts (AREA)
- Storage Of Web-Like Or Filamentary Materials (AREA)
- Adhesive Tape Dispensing Devices (AREA)
- Sewing Machines And Sewing (AREA)
- Purses, Travelling Bags, Baskets, Or Suitcases (AREA)
Abstract
Description
Die Erfindung richtet sich zunächst auf eine Öse zum Verstärken des Randbereichs um ein Loch in einer Tragbahn.The invention is initially directed to an eyelet for reinforcing the rim around a hole in a track.
Dazu verwendet man normalerweise zweiteilige Ösen (EP 0 655 205 B1; US 4,479,287 A, Fig. 1, Fig. 12), die aus einem Ösenteil und einem Scheibenteil bestehen. Der Ösenteil besitzt einen Teller, der beim Vernieten auf der Schauseite der Trägerseite zu liegen kommt, während ein am Teller sitzender rohrförmiger Hals ein Loch in der Trägerbahn schneidet und mit seinem freien Endstück mehr oder weniger C-förmig umbördelt wird. Durch die Umbördelung wird das Endstück des Halses versteift. Das biegesteife Endstück stützt sich am Scheibenteil ab, wodurch die Trägerbahn zwischen dem Scheibenteil und dem Teller zusammengedrückt wird. Trotz ihres hohen Materialaufwands besitzt eine solche vernietete zweiteilige Öse eine unzureichende Ausreißfestigkeit.Normally, two-part eyelets (EP 0 655 205 B1, US Pat. No. 4,479,287 A, FIGS. 1, 12) which consist of an eyelet part and a disk part are used for this purpose. The eyelet has a plate that comes to rest on the show side of the carrier side when riveting, while sitting on a plate tubular neck cuts a hole in the carrier web and is crimped more or less C-shaped with its free end. By flanging the tail of the neck is stiffened. The rigid end piece is supported on the disc part, whereby the carrier web is compressed between the disc part and the plate. Despite its high material cost, such a riveted two-piece eyelet has insufficient tear resistance.
Es sind auch einteilige Ösen bekannt, die keinen Scheibenteil aufweisen und nur aus einem Ösenteil bestehen. In einem Fall (US 4 479 287 A, Fig. 8) wird der Hals eines solchen Ösenteils U-förmig umgelegt, wodurch das freie Endstück des umbördelten Halses im wesentlichen parallel zum ebenen Teller des Ösenteils verläuft. In einem anderen Fall (DE 299 03 124 Ul, Fig. 3b) wird während des Nietvorgangs das Endstück des Halses nicht nur umgelegt, sondern durch Schneiden im Nietwerkzeug in laschenartige Halteelemente zergliedert. Die umgefalteten Enden des Halses sind nicht biegesteif, zumal wenn sie in Laschen geschnitten sind. Dadurch wird die Trägerbahn nicht ausreichend zusammengepresst, was sich in einer gegenüber der eingangs erwähnten zweiteiligen Öse geringeren Ausreißfestigkeit der angenieteten Öse bemerkbar macht.There are also one-piece eyelets are known which have no disc part and consist only of an eyelet. In one case (US 4,479,287 A, FIG. 8), the neck of a such Ösenteils folded over in a U-shape, whereby the free end of the beaded neck extends substantially parallel to the flat plate of the eyelet. In another case (DE 299 03 124 Ul, Fig. 3b), the end of the neck is not only folded during the riveting process, but dissected by cutting in the riveting tool in tab-like holding elements. The folded ends of the neck are not rigid, especially when they are cut in tabs. As a result, the carrier web is not sufficiently compressed, which is noticeable in a comparison with the aforementioned two-piece eyelet less tear resistance of the riveted eyelet.
Es sind aber auch einteilige Ösen der im Oberbegriff von Anspruch 1 genannten Art bekannt (US 4 479 287 A, Fig. 2), bei denen die beim Vernieten entstehende Umbördelung ein im wesentlichen in sich geschlossenes Ringprofil aufweist, in welches praktisch die ganze Halslänge einrollt. Der Hals dieses bekannten Ösenteils hat eine glatte Endkante. Obwohl der Hals durch seine ringförmige Umbördelung versteift ist, besitzt diese scheibenlose Öse gegenüber der eingangs erwähnten zweiteiligen Öse eine geringere Ausreißfestigkeit. Auch diese einteilige Öse konnte sich in der Praxis nicht durchsetzen.But there are also one-piece eyelets of the type mentioned in the preamble of claim 1 known (US 4,479,287 A, Fig. 2), in which the beading produced during riveting has a substantially self-contained annular profile, in which practically rolls up the entire neck length , The neck of this known eyelet has a smooth end edge. Although the neck is stiffened by its annular bead, this discless eyelet has a lower pull-out strength compared to the two-part eyelet mentioned above. Even this one-piece eyelet could not prevail in practice.
Es gibt einteilige Ösen anderer Art, wo beim Umbördeln das Endstück des Halses C-förmig verformt wird. In einem Fall (EP 0 673 611 A2) bleibt zwischen der glatten Endkante des C-förmig gebogenen Halses und dem bogenförmig profilierten Teller ein Spalt, wo die Trägerbahn eingeklemmt wird. Im Scheitelbogen des Tellers ist eine umlaufende Ringrippe mit stellenweise aufgesetzten Spitzen angeordnet. Der Übergangsbereich zwischen dem Teller und dem Hals ist mit konischen Stabilisierungsrippen versehen, die eine Umbördelung dieses Bereiches verhindern. Die Spitzen und die Ringrippe im Inneren des gekrümmten Tellers sollen eine Verdrehungssicherung der Trägerbahn bewirken. Die Trägerbahn nimmt einen Labyrinthverlauf zwischen der Ringrippe und der Hals-Endkante im Inneren zwischen dem bogenförmigem Teller und dem C-Profil des Halses ein. In einem anderen Fall (DE 669 779 A) wird. der C-förmig umbördelte Hals mit seiner glatten Endkante im wesentlichen vertikal in die Trägerbahn eingedrückt. Um beim Umbördeln ein Platzen des Halsendstücks zu vermeiden, soll der Hals ohne jegliche Einschnitt od. dgl. ausgebildet sein. Beim Umbördeln werden vom Nietwerkzeug radiale Einschnürungen im umgelegten Ösenrand eingeprägt, die das Bördelende verstärken sollen. Durch das gewellte Bördelende wird die bereits vom C-Profil erzeugte Biegesteifigkeit des Hals-Endstücks weiter erhöht, damit der umgelegte Ösenrand in die Oberfläche der Trägerbahn vertikal eindringen kann. Die Ausreißfestigkeit solcher einteiliger Ösen mit C-förmig umbördelten Hals haben keine höhere Ausreißfestigkeit als die eingangs erwähnte zweiteilige Öse.There are one-piece eyelets of another type, where the end piece of the neck is deformed C-shaped during beading. In one case (EP 0 673 611 A2), a gap remains between the smooth end edge of the C-shaped neck and the arcuately profiled plate, where the carrier web is clamped. In the crest of the plate, a circumferential ring rib is arranged with spikes in places. The transition area between the plate and the neck is provided with conical stabilizing ribs, which prevent beading of this area. The tips and the annular rib in the interior of the curved plate should cause a security against rotation of the carrier web. The carrier web assumes a labyrinth course between the annular rib and the neck end edge in the interior between the arcuate plate and the C-profile of the neck. In another case (DE 669 779 A) is. the C-shaped neck flared with its smooth End edge pressed substantially vertically into the carrier web. To avoid bursting the neck end piece when crimping, the neck od without any incision. The like. Be formed. When flanging radial riveting in the folded eyelet edge are impressed by the riveting tool, which should strengthen the crimp end. Due to the corrugated flanging end, the bending stiffness of the neck end piece already produced by the C profile is further increased, so that the folded loop edge can penetrate vertically into the surface of the carrier web. The pull-out strength of such one-piece eyelets with a C-shaped flared neck has no higher tear resistance than the two-part eyelet mentioned at the outset.
Bei einer weiteren einteiligen Öse, bei der der Hals des Ösenteils ebenfalls nur ein C-Profil aufweist (US 2107 375) kommt es auf ein stumpfes Halsende an, um ein Bersten des Halsendes zu vermeiden. Deshalb verstärkt man das Halsende fallweise mit einer umlaufenden Randwulst. Ferner wird das Halsende vor dem Vernieten mittels eines Sonderwerkzeugs gestaucht, wodurch im Stauchungsbereich abgeflachte Berge und bogenförmige Durchgänge entstehen. Beim Stauchen entstehen endseitig radiale Verbreiterungen, die die Wanddicke des Halses zusätzlich zur Randwulst vergrößern und daher die Biegesteifigkeit der Umbördelung erhöhen. Dennoch ist die Ausreißfestigkeit einer solchen angenieteten Öse gegenüber der eingangs erwähnten zweiteiligen Öse geringer.In another one-piece eyelet, in which the neck of the eyelet also has only one C-profile (US Pat. No. 2107,375), a blunt neck end is important in order to avoid bursting of the neck end. Therefore you strengthen the neck end occasionally with a circumferential bead. Furthermore, the neck end is compressed prior to riveting by means of a special tool, whereby in the compression area flattened mountains and arcuate passages arise. When upsetting arise radial end extensions, which increase the wall thickness of the neck in addition to the edge bead and therefore increase the flexural rigidity of the bead. Nevertheless, the pull-out strength of such a riveted eyelet with respect to the two-part eyelet mentioned above is lower.
Soweit im Stand der Technik (DE 669 779 A; US 2 107 375 A) am Bördelrand bzw. am Stirnende des Halses radiale oder axiale Profilierungen vorgesehen sind, dienen sie zur Verstärkung und Versteifung des umbördelten Hals-Endstücks. Diese profilierten Halsenden werden, wie gesagt, nur im Zusammenhang mit einem C-Profil verwendet und stoßen daher im wesentlichen vertikal und stumpf auf die Oberfläche der Trägerbahn. Dadurch verlaufen die profilierten Halsenden lediglich quer zu den im Gebrauchsfall auf die Trägerbahn ausgeübten Zugbelastungen, was die geringe Ausreißfestigkeit dieser bekannten Ösen erklärt.Insofar as radial or axial profilings are provided in the prior art (DE 669 779 A, US Pat. No. 2,107,375 A) at the beaded edge or at the front end of the neck, they serve to reinforce and stiffen the beaded neck end piece. These profiled neck ends are, as stated, used only in connection with a C-profile and therefore encounter substantially vertical and blunt on the surface of the carrier web. As a result, the profiled neck ends extend only transversely to the tensile loads exerted on the carrier web in the case of use, which explains the low pull-out strength of these known eyelets.
Der Erfindung liegt die Aufgabe zugrunde, eine preiswerte, schnell ansetzbare Öse der im Oberbegriff des Anspruches 1 angegebenen Art zu entwickeln, die nach dem Annieten an der Trägerbahn sich durch eine hohe Ausreißfestigkeit auszeichnet. Dies wird erfindungsgemäß durch die im Anspruch 1 angeführten Maßnahmen erreicht, denen folgende besondere Bedeutung zukommt.The invention has for its object to develop an inexpensive, quickly attachable eyelet specified in the preamble of claim 1 species, which is characterized by a high pull-out strength after Annieten on the carrier web. This is inventively achieved by the measures listed in claim 1, which have the following special significance.
Bereits im unverarbeiteten Ausgangszustand sind am freien Endstück des Halses axiale Vorsprünge angeordnet und der Hals wird beim Umbördeln praktisch mit seiner ganzen Halslänge zu einem in ein im wesentlichen in sich geschlossenes Ringprofil verformt, in welches die Vorsprünge einbezogen sind. Dadurch ergeben sich Haltemittel, bei denen die Halsvorsprünge besondere Andruckstellen an der erfassten Trägerbahn erzeugen, gegen welche sich die Trägerbahn bei Zugbeanspruchungen stellt. Die im Ringprofil integrierten Halsvorsprünge liegen unter Zwischenschaltung des Lochrandbereiches der Trägerbahn an Widerlagerflächen an, die von der Wölbung des Tellers oder vom Übergang zwischen dem Teller und dem Hals des Ösenteils gebildet werden. In der ringförmigen Umbördelung weisen die Halsvorsprünge in Gegenrichtung zu der im Gebrauchsfall auf die Trägerbahn ausgeübten Zugbelastungen, was die erfindungsgemäße Öse gegenüber dem Stand der Technik wesentlich auszugsicherer macht. Dieses überraschende Ergebnis lässt sich folgendermaßen erklären.Already in the unprocessed initial state axial projections are arranged at the free end of the neck and the neck is practically deformed during beading with its entire neck length to a substantially self-contained ring profile, in which the projections are included. This results in holding means in which the neck projections produce special pressure points on the detected carrier web, against which the carrier web is subject to tensile stresses. The integrated in the ring profile neck projections are the interposition of the hole edge portion of the carrier web to abutment surfaces, which are formed by the curvature of the plate or the transition between the plate and the neck of the eyelet. In the annular beading, the neck projections point in the opposite direction to the tensile loads exerted on the carrier web in the case of use, which makes the eyelet according to the invention considerably safer than the prior art. This surprising result can be explained as follows.
Im Gegensatz zum Stand der Technik, der eine möglichst hohe Steifigkeit am Halsende anstrebt, wird bei der erfindungsgemäßen Öse die Biegesteifigkeit des umbördelten Randes herabgesetzt. Das erreicht man durch die im Ausgangszustand axial verlaufenden Halsvorsprünge, die gegenüber dem im wesentlichen steif bleibenden, zu einem Ringprofil geformten Halsrest wie ein Kranz biegsamer Zungen wirken und nach der Umbördelung, wie gesagt, den Zugbelastungen entgegengerichtet sind. An den Andruckstellen kommt es vor den Halsvorsprüngen zu einer stufenförmigen Erhöhung des Bahnmaterials. Bei Zugbelastungen werden die biegefähigen Halsvorsprünge mitgenommen, spreizen sich gegenüber der Achse der angenieteten Öse auseinander und werden gegen die umlaufende Widerlagerfläche des Tellers angedrückt. Die zungenartigen Halsvorsprünge wirken also wie "Spreizklemmen", die mit wachsender Ausreißkraft zunehmend fester an die Trägerbahn angedrückt werden. Im Vergleich mit den sehr viel aufwendigeren zweiteiligen Ösen erhält man bei der Erfindung eine um 30% bis 75% höhere Ausreißfestigkeit. Das gilt insbesondere bei Vernietung in flexiblen oder dehnbaren Trägerbahnen, die bisher mit einer einteiligen Öse gar nicht befriedigend ausgerüstet werden konnten.In contrast to the prior art, which aims at the highest possible stiffness at the neck end, the flexural rigidity of the beaded edge is reduced in the eyelet according to the invention. This is achieved by the initial axial extending neck projections, which act compared to the substantially rigid, shaped to a ring profile neck rest like a wreath flexible tongues and after the beading, as I said, the tensile loads are directed opposite. At the pressure points, there is a step-shaped increase of the web material in front of the neck projections. For tensile loads, the bendable neck projections are taken, spread apart with respect to the axis of the riveted eyelet apart and against the circumferential Abutment surface of the plate pressed. The tongue-like neck projections thus act as "spreading clamps", which are increasingly pressed against the carrier web with increasing pull-out force. In comparison with the much more expensive two-piece eyelets obtained in the invention, a 30% to 75% higher tear resistance. This is especially true when riveting in flexible or stretchable carrier webs that could not be satisfactorily equipped with a one-piece eyelet so far.
Für die Ausbildung der axialen Halsvorsprünge empfiehlt es sich, den Hals des Ösenteils mit einer gezahnten Endkante zu versehen. Die Halsvorsprünge werden bereits bei der Herstellung des Ösenteils miterzeugt, wodurch besondere Arbeitsgänge oder Bearbeitungswerkzeuge zur Profilgebung eingespart werden. Beim Ziehen der Ringform während der Umbördelung gräbt sich der Zahn in das Bahnmaterial ein und es kann zu einer stufenförmigen Erhöhung entlang des Zahnprofils kommen. Außer der vorerwähnten Spreizklemmung kommt es dann auch zu einem Formschluss zwischen dem Zahn und der Trägerbahn. Je höher die auf die Trägerbahn ausgeübte Zugbelastung ist, umso fester verkrallt sich die Trägerbahn vor dem dazu antiparallel verlaufenden Zahn.For the formation of the axial neck projections, it is recommended to provide the neck of the eyelet with a serrated end edge. The neck projections are already co-produced in the production of the eyelet, whereby special operations or processing tools for profiling can be saved. When pulling the ring mold during the beading, the tooth digs into the web material and it can come to a step-like increase along the tooth profile. Apart from the aforementioned Spreizklemmung it then comes to a positive connection between the tooth and the carrier web. The higher the tensile load applied to the carrier web, the stronger the carrier web digs in front of the antiparallel tooth.
Die Erfindung richtet sich ferner auf eine Vorrichtung zum Ansetzen der Öse nach der Erfindung. Bei der bekannten Vorrichtung (US 1,838,973 A), die allerdings für zweiteilige Ösen bestimmt ist, spring der Druckring im Unterwerkzeug gegenüber der dortigen Schneidkante vor. Das Oberwerkzeug besitzt einen axialbeweglichen Zentraleinsatz mit einer Bohrung, der gegenüber den angrenzenden Flächen des Oberwerkzeugs axial vorauseilt. Beim Arbeitshub der beiden Werkzeuge wird die Trägerbahn vom Zentraleinsatz des Oberwerkzeugs in den Druckring hineingedrückt; bevor der Zentraleinsatz auf die Schneidkante des Unterwerkzeugs trifft und dadurch das Loch in die Trägerbahn schneidet. Die Trägerbahn wird in der dortigen zweiteiligen Öse, die außer dem Ösenteil auch noch den bereits eingangs erwähnten Scheibenteil besitzt, unschön befestigt. Es kommt zu Falten in der Trägerbahn.The invention is further directed to a device for attaching the eyelet according to the invention. In the known device (US 1,838,973 A), which is, however, intended for two-piece eyelets, jump the pressure ring in the lower tool against the local cutting edge. The upper tool has an axially movable central insert with a bore that projects axially relative to the adjacent surfaces of the upper tool. During the working stroke of the two tools, the carrier web is pressed into the pressure ring by the central insert of the upper tool; before the central insert hits the cutting edge of the lower tool and thereby cuts the hole in the carrier web. The carrier web is in the local two-piece eyelet, which also has the part already mentioned above except the eyelet unsightly attached. It comes to wrinkles in the carrier web.
Der Erfindung liegt daher die weitere Aufgabe zugrunde, eine Vorrichtung für die im Anspruch 1 genannte einteilige Öse zu entwickeln, die sich schöner und reißfester an der Trägerbahn befestigen lässt. Dies wird erfindungsgemäß durch die im Kennzeichen des Anspruches 9 genannten Maßnahmen erreicht, denen folgende besondere Bedeutung zukommt.The invention is therefore based on the further object of developing a device for the one-piece eyelet mentioned in claim 1, which can be fastened beautiful and tear-resistant to the carrier web. This is inventively achieved by the measures mentioned in the characterizing part of claim 9, which have the following special significance.
Bei der Erfindung ist dem Druckring im Unterwerkzeug ein in Gegenrichtung kraftbetasteter Gegendruckring im Oberwerkzeug zugeordnet. Dabei empfiehlt es sich, gemäß Anspruch 10, diese beiden Ringe mit gegeneinander weisenden Schräg- und Gegenschrägflächen zu versehen. Bei der Hubbewegung der beiden Werkzeuge wird die Trägerbahn zwischen diesen beiden Ringen eingespannt, wobei die Schrägflächen für ein zusätzliches Glattziehen der Trägerbahn sorgen. Dadurch wird beim nachfolgenden Bördelvorgang der einteiligen Öse ein glatter Verlauf der Trägerbahn aufrechterhalten, was zu einer einwandfreien Befestigung der Öse an der Trägerbahn führt. Durch das Einspannen wird der Materialeinzug minimiert. Das hat zur Folge, dass die Teilungsabstände zwischen den Ösen exakt eingehalten werden können und die Toleranzabweichungen auch über große Planenlängen stark eingeschränkt werden.In the invention, the pressure ring in the lower tool in the opposite direction kraftbetasteter counter-pressure ring in the upper tool is assigned. It is recommended, according to claim 10, to provide these two rings with mutually facing oblique and Gegenschrägflächen. During the stroke movement of the two tools, the carrier web is clamped between these two rings, wherein the inclined surfaces provide for an additional smooth pulling of the carrier web. This will maintain a smooth course of the carrier web during subsequent crimping of the one-piece eyelet, resulting in a proper attachment of the eyelet to the carrier web. Clamping minimizes material feed. This has the consequence that the pitches between the eyelets can be maintained exactly and the tolerance deviations are greatly limited even over long tarpaulin lengths.
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:
- Fig. 1 und 2,
- jeweils in Draufsicht, die Schauseite bzw. die Rückseite einer mit der erfindungsgemäßen Öse ausgerüsteten Trägerbahn,
- Fig. 3,
- in starker Vergrößerung, eine Querschnittansicht durch die in Fig. 1 gezeigte angesetzte Öse längs der dortigen Schnittlinie III - III,
- Fig. 4
- einen Axialschnitt durch den besonderen Ösenteil der erfindungsgemäßen scheibenlosen Öse im Ausgangszustand, nämlich vor seiner Verarbeitung an der Trägerbahn,
- Fig. 5,
- in Vergrößerung, eine ebene Abwinklung eines Teilstücks des mit Ziff. V in Fig. 4 gekennzeichneten Randbereichs vom erfindungsgemäßen Ösenteil und
- Fig. 6,
- in axialem Halbschnitt, Bruchstücke einer zweiteiligen erfindungsgemäßen Vorrichtung zur Verarbeitung des in Fig. 4 gezeigten Ösenteils, wobei das Oberwerkzeug sich gegenüber dem Unterwerkzeug im oberen Endpunkt seiner Hubbewegung befindet.
- 1 and 2,
- each in plan view, the show side or the back of a equipped with the eyelet invention carrier web,
- 3,
- in high magnification, a cross-sectional view through the attached eyelet shown in Figure 1 along the section line III - III there,
- Fig. 4
- an axial section through the special Ösenteil the discless eyelet according to the invention in the initial state, namely before its processing on the carrier web,
- Fig. 5,
- in magnification, a flat bend of a section of the with ziff. V in Fig. 4 marked edge portion of the eyelet according to the invention and
- 6,
- in axial half-section, fragments of a two-part device according to the invention for processing the eyelet shown in Fig. 4, wherein the upper tool is opposite to the lower tool in the upper end point of its stroke 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 Ösenteil 10. In Fig. 4 und 5 ist der Ösenteil 10 in seinem Ausgangszustand gezeigt, vor der Verarbeitung. Die Fig. 1, 2 und 3 dagegen zeigen den Ösenteil 10' nach seiner Verarbeitung, im fertigen Gebrauchszustand, während seiner Lochverstärkungs-Funktion.An eye should, as shown in FIGS. 1 and 2, reinforce the edge region 21 of a hole 22 cut in a carrier web 20. The carrier web 20 is usually a flexible and optionally stretchable structure, eg a motor vehicle tarpaulin. The invention achieves the desired hole reinforcement with a one-piece eyelet 10. In Fig. 4 and 5, the eyelet 10 is shown in its initial state, before the Processing. By contrast, FIGS. 1, 2 and 3 show the eyelet part 10 'after its processing, in the finished state of use, during its hole reinforcing function.
Der Ösenteil 10 lässt sich in einen gewölbten, im wesentlichen radial verlaufenden Teller 11 und in einen axial verlaufenden rohrförmigen 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 Wölbungsprofil 13 versehen. Dadurch ergibt sich ein besonders auffälliger bogenförmiger Übergang 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.The eyelet 10 can be divided into a curved, substantially radially extending plate 11 and an axially extending tubular neck 12. For reasons of a better dimensional stability and to be described in more detail annular flange of the neck 12 of the plate 11 is provided with a buckling profile 13. This results in a particularly conspicuous arcuate transition 14 between the plate 11 and the neck 12. The neck is provided in its free end 15 with axial, so in the direction of the neck 12 extending projections 16. These consist in the present case of a recognizable in Fig. 5 arcuate toothed end edge 17. 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 spaces 18 have concave curves 28. This results in the tooth profile 19 a waveform. The waveform is unbalanced. That is, the radius of curvature of the curves 27 of the tooth tips 17 is made smaller than that of the curves 28 of the tooth spaces.
Dieser Ösenteil 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 Zentraleinsatz 33, der demgegenüber ebenfalls passiv axial beweglich ist. Schließlich ist das Oberwerkzeug 31 im Umfangsbereich 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 17 is attached to the carrier web 20 in the device 30 shown in FIG. The device 30 consists of essentially five mutually axially displaceable parts with respect to time. This first includes a stationary in the present case lower tool 32, which carries a contrast axially movable pressure ring 34. Furthermore, the device 30 includes an upper tool 31 which is actively movable relative to the lower tool 32 and has a central insert 33 arranged coaxially therein, which, in contrast, is also passively axially movable. Finally, the upper tool 31 is enclosed in the peripheral region by a likewise axially passively axially movable counter-pressure ring 54. The central insert 33 and the counter-pressure 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, to a mirror image, in the sense of the force arrow 36 against the upper tool 31 under the action of a crowd of springs 56th stands, which are mounted in axial bores of the lower tool 32. The springs 56 are as Spiral springs formed in the helical interior of the pressure ring 34 seated pins 57 engage. The tool group 31, 33, 54 on the one hand and 32, 34 on the other hand are lift-movable relative to one another, 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 Gewindeeingriff 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 circumferential 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 an edge of a peripheral flange 65 of the upper tool 31 and the abutting surface of a cutout 66 in the counter-pressure ring 54. The Ausschubposition of the counter-pressure ring 54 is determined by end stops. These consist in the present case of the head 67 of a family of guide rods 68 which are adjustable in length by threaded engagement 69 and a lock nut 71. The rod end 67 is supported at rest on the upper flank of the flange 65. As a result, the desired extension 70 of the counter-pressure ring 54 with respect to the upper tool 31 is 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 Ösenteil 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.In Fig. 6, as already mentioned, the upper reversal point of the lifting movement 37 is shown, where the upper tool 31 is opposite the lower tool 32 in the maximum stroke distance 38. Thereby, an eyelet 10 can be easily used on the receiving profile of the upper tool 31 and central insert 33. For this purpose, the upper tool 31 has a profile of the plate 11 corresponding receptacle 39. The area provided with the receptacle 39 is subject to wear under normal use. For ease of repair of a worn device 30, therefore, the lower portion of the upper tool is provided with an insert 31 ', the od by the indicated screw. Like. With the upper portion of the upper tool 31 is detachably connected. This insert 31 'has the receptacle 39.
Nach dem Einsetzen des Ösenteils 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 Ösenteils in den Werkzeugen 31, 33 dient ein im Umfangsbereich des Zentraleinsatzes 33 angeordnetes Halteelement 44, welches im vorliegenden Fall aus einem radial nach außen federbelasteten Stift besteht.After insertion of the eyelet 10, the end of the neck 20 is supported on the peripheral surface of the central insert 33 from. The central insert 33 is provided with a flat end surface 43. To secure the position of the Ösenteils in the tools 31, 33 is used in the peripheral region of the central insert 33 arranged holding element 44, which consists in the present case of a spring-loaded pin radially outward.
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.Between the two tool parts 31, 32, the carrier web 20 is inserted, which is initially unperforated. The above-mentioned springs 56 hold the pressure ring 34 in a defined, recognizable from Fig. 6 starting position At maximum stroke of the tools, the relevant top 45 of the pressure ring 34 is above or expediently at the same height with a provided cutting tool 32 cutting edge 42. This results in the pressure ring 34 a recognizable from Fig. 6 dash-dotted lines illustrated horizontal support plane 60 for the carrier web 20th
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, first the leading counterpressure ring 54 strikes the carrier web 20 lying above the pressure ring 34. The two rings 34, 54 are provided with ramps 58 and 59 extending essentially parallel to one another, which support web 20 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 relative to the dot-dash line in Fig. 6 clarified support plane 60, which is determined by the serving for supporting the carrier web 20 end face 45 of the pressure ring 34. The counter-pressure surface 59 of the mentioned pressure ring 54 extends substantially parallel to the pressure surface 58. When Gegengegenfahren 37 of the two tools 31, 32, therefore, the carrier web 20 is pulled 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 smoothly in the region 29 to be punched. The carrier web 20 thus assumes an extended position in the mentioned support plane 60.
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 loaded by the press ram central insert 33 hits the upwardly facing display side 23 of the carrier web 20 and presses against the resting on the support base 24 cutting edge 42 from the lower tool 32. As a result, a circular hole punched from the carrier web 20 is cut out. In this case, the hole radius 46 determined by the cutting edge 42 is smaller than the neck radius 26 of the eyelet neck 12 marked 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 Ösenteil 10 durch das entstehende Loch ins Unterwerkzeug, bis der Teller 11 vom Ösenteil 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 Bördelung 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.When the upper tool 31 continues to lower in the direction of the lifting arrow 37, the carrier web 20 is fixed between the two bevels 58, 59 of the clamped two rings 34, 54. The neck 12 moves from the eyelet 10 through the resulting hole in the lower tool until the plate 11 of the eyelet 10, with the interposition of the carrier web 20, touches the pressure ring 34. In this downward movement 37, the upper tool 31 overcomes the spring force 36 from the lower-side pressure ring 34 and there is the curling of eyelet neck 12 and the axial projections 16 on the flaring profile 47 of the lower tool 32. The spring force 54 from the upper-side pressure ring 54 is smaller than that on the Pressure ring 34 acting Ausschubkraft 36. Similar to the upper tool 31 and the lower tool 32 has a positioned in the axial region insert 32 ', which has the relevant flare 47. This hemming profile 47 wears out after prolonged use. Then it is sufficient only to replace this insert 32 '.
Bei der Bördelung ergeben sich die besonderen, aus Fig. 3 ersichtlichen Nietverhältnisse. Es wird praktisch die ganze, aus Fig. 4 ersichtliche Halslänge 48 des Ösenteils 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.When flanging, the particular, apparent from Fig. 3 riveting arise. Virtually all of the neck length 48 of the eyelet part shown in FIG. 4 is rolled into a ring profile 50 recognizable from FIG. 3 on the back side 24 of the carrier web 20. The neck projections 16 are included in this ring formation 50. With the interposition of the mentioned and also indicated in Fig. 6 hole edge portion 21 of the carrier web 20, these neck projections 16 are pressed against a generated by the described curvature 13 of the plate 11 abutment surface 49. There comes to the recognizable from Fig. 3 annular peripheral Andruckstellen 40. In the inner ring profile 51, the carrier web 20 continues with an end zone 41 on, which adapts to the profile 50 like an annular segment. Even when rolling the end zone 41 during the riveting process, the bevels 58, 59 hold the carrier web 20 firmly.
Beim bestimmungsgemäßen Gebrauch des an der Trägerbahn 20 angesetzten Ösenteils 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 Ösenteils 10' an der Bahn 20 erreicht.During proper use of attached to the carrier web 20 Ösenteils arise by the force arrows 52 in Figs. 1 to 3 illustrated tensile loads. These tensile loads 52 are absorbed by the pressure points 40. At the pressure points 40 is initially a clamping action between the neck projections 16 and the abutment surface 49 before. In addition, because of the described profiling 19 of these projections 16 is also given a positive engagement. The tooth tips 17 penetrate into the web material, but because of the curves 27, 28 of the tooth profile 19, no cracking occurs in the web 20. A notch effect is thereby avoided. Before Tooth tips and also in the curved tooth spaces 18 created beyond these Andruckstellen 40 with a 53 in Fig. 3 designated step-like increase in the web thickness. The web 40 is namely at 53 anxious again to raise their original track thickness 25 itself. At the tensile loads 52 of the web 20, these step-like elevations 53 of the web material 20 dig into the wavy edges of the neck projections 16. As a result, the positive connection is increased and a surprisingly high tensile strength of the riveted eyelet 10 'on the web 20 is achieved.
- 1010
- Ösenteil (Ausgangszustand; Fig. 4)Eyelet (initial state, Fig. 4)
- 10'10 '
- Nietzustand von 10 (Fig. 1 bis 3)Rinse state of 10 (FIGS. 1 to 3)
- 1111
- Teller von 10Plate of 10
- 1212
- Hals von 10, ÖsenhalsNeck of 10, eyelet neck
- 1313
- Wölbungsprofil von 11Arching profile of 11
- 1414
- bogenförmiger Übergang zwischen 11, 12arcuate transition between 11, 12
- 1515
- Endstück von 12Tail of 12
- 1616
- axialer Halsvorsprung bei 15 (Fig. 4)axial neck protrusion at 15 (Figure 4)
- 1717
- Zahnspitze (Fig. 5)Tooth tip (Fig. 5)
- 1818
- Zahnlückegap
- 1919
- Zahnprofil bei 15 (Fig. 5)Tooth profile at 15 (Figure 5)
- 2020
- Trägerbahnsupport web
- 2121
- Lochrandbereich von 20Hole edge area of 20
- 2222
- Loch in 20 (Fig. 1, 2)Hole in 20 (Fig. 1, 2)
- 2323
- Schauseite von 20Show side of 20
- 2424
- Rückseite von 20Back of 20
- 2525
- Bahnstärke von 20 (Fig. 6)Web thickness of 20 (Figure 6)
- 2626
- Halsradius von 12 (Fig. 6)Neck radius of 12 (Figure 6)
- 2727
- konvexe Rundung von 17 (Fig. 5)convex rounding of 17 (Fig. 5)
- 2828
- konkave Rundung von 18 (Fig. 5)concave rounding of 18 (Figure 5)
- 2929
- Lochstanzling aus 20 (Fig. 6)Punch from 20 (Fig. 6)
- 3030
- Vorrichtungcontraption
- 3131
- Oberwerkzeug von 30Upper tool of 30
- 31'31 '
- austauschbarer Einsatz in 31replaceable insert in 31
- 3232
- Unterwerkzeug von 30Bottom tool of 30
- 32'32 '
- austauschbarer Einsatz in 32replaceable insert in 32
- 3333
- Zentraleinsatz in 31Central employment in 31
- 3434
- Druckring in 33Pressure ring in 33
- 3535
- Kraftbelastungspfeil von 33Force load arrow of 33
- 3636
- Pfeil der Federkraft von 34Arrow of the spring force of 34
- 3737
- Hubewegungspfeil von 31 gegenüber 32 (Fig. 6)Stroke movement arrow from 31 to 32 (FIG. 6)
- 3838
- maximaler Hubabstand zwischen 31, 32maximum stroke distance between 31, 32
- 3939
- Aufnahme in 31 für 11Recording in 31 for 11
- 4040
- Andruckstelle von 20 zwischen 16, 49 (Fig. 3)Pressure location of 20 between 16, 49 (FIG. 3)
- 4141
- Endzone von 20 jenseits von 40 (Fig. 3)End zone of 20 beyond 40 (Figure 3)
- 4242
- Schneidkante an 32Cutting edge at 32
- 4343
- ebene Stirnfläche von 33 (Fig. 6)flat face of 33 (Figure 6)
- 4444
- Halteelement für 10 bei 33 (Fig. 6)Retaining element for 10 at 33 (FIG. 6)
- 4545
- Stirnfläche für 20 an 34Face for 20 to 34
- 4646
- Lochradius von 29 (Fig. 6)Hole radius of 29 (Figure 6)
- 4747
- Bördelprofil in 32 (Fig. 6)Beading profile in 32 (FIG. 6)
- 4848
- Halslänge von 12 (Fig. 4)Neck length of 12 (Fig. 4)
- 4949
- Widerlagerfläche an 11 für 16 (Fig. 3)Abutment surface at 11 for 16 (FIG. 3)
- 5050
- Ringprofil von 12 bei 10' (Fig. 3)Ring profile of 12 at 10 '(Figure 3)
- 5151
- Ringprofil-Inneres von 50 (Fig. 4)Ring profile inside of 50 (Figure 4)
- 5252
- Pfeil der Zugbelastung auf 20Arrow of the tensile load on 20
- 5353
- stufenförmige Erhöhung von 20 hinter 40 (Fig. 3)incremental increase of 20 past 40 (FIG. 3)
- 5454
- GegendruckringCounterpressure ring
- 5555
- Kraftbelastung von 54Force load of 54
- 5656
- Feder für 36Spring for 36
- 5757
- Stift an 34 für 56Pin at 34 for 56
- 5858
- Schräge von 34, SchrägflächeSlope of 34, bevel
- 5959
- Gegenschräge von 54, GegenschrägflächeCounter bevel of 54, counter bevel
- 6060
- Stützebenesupport plane
- 6161
- Winkelverlauf von 58 gegenüber von 45Angular course of 58 opposite 45
- 6262
- Kante zwischen 45, 58 von 34Edge between 45, 58 of 34
- 6363
- Umfangsfläche von 31Circumferential area of 31
- 6464
- Druckfedercompression spring
- 6565
- Flanschflange
- 6666
- Ausschnittneckline
- 6767
- Kopf von 68Head of 68
- 6868
- Führungsstangeguide rod
- 6969
- Gewindeeingriffthread engagement
- 7070
- Ausschublängeextension length
- 7171
- Sicherungsmutterlocknut
Claims (12)
- Eyelet for reinforcing the area (21) around the edge of a hole (22) in a carrier web (20),- with a diskless eyelet part (10, 10'), consisting of a plate (11), which rests on the visible side (23) of the carrier web (20) during riveting, a tubular neck (12) which passes through the hole (22), and an arc-shaped transition area (14) between the plate (11) and the neck (12);- wherein, during riveting, the neck is flanged on the rear surface (24) of the carrier web (20) and the flanging of the neck (12) essentially comprises an inherently closed ring-shaped profile (50) into which virtually the entire length (48) of the neck is rolled,characterised in that
the free end part (15) of the neck (12) is provided with projections (16), which extend in the axial direction before the riveting of the eyelet part (10) and are included in the ring-shaped profile (50) after the flanging,
in that support surfaces (49) are formed inside the ring-shaped profile (51) by the convexity (13) of the plate (11) or transition area (14), against which the neck projections (16) are pressed, thereby intercalating the area (21) of the carrier web (20) around the edge of the hole, and produce compression points (40) on the gripped carrier web against which the carrier web bears under tensile stress,
in that the neck projections (16) at the compression points (40) oppose the tensile stresses (52) exerted on the carrier web (20) during use and grip the carrier web (20), and
in that, in the interior (51) of the ring-shaped profile, the end part (41) of the carrier web (20) extends beyond the flat compression points (40) to the edge of the hole and conforms to the shape of the ring-shaped profile (50) as a ring segment. - Eyelet according to claim 1, characterised in that the axial projections (16) on the neck consist of a pronged edge (19) at the end of the neck (12).
- Eyelet according to claim 2, characterised in that the tips (17) of the prongs are convexly rounded, in that the gaps (18) between the prongs are concavely rounded, and
in that the two rounded areas (27, 28) define a wave-like course of the pronged edge (19). - Eyelet according to claim 3, characterised in that the pronged edge (19) is asymmetrically wave-like.
- Eyelet according to claim 3 or 4, characterised in that the convexly rounded areas (27) of the prong tips (17) are smaller than the concavely rounded areas (28) of the prong gaps (18).
- Eyelet according to one of claims 1 to 5, characterised in that the material of the carrier web (20) is flexible and/or stretchable.
- Eyelet according to claim 6, characterised in that the carrier web (20) consists of a canvas tarpaulin.
- Eyelet according to claim 6, characterised in that the carrier web (20) consists of a reinforced plastic sheet.
- Device (30) for installing eyelet parts (10) in a carrier web (20) according to one of claims 1 to 8,
with a lower tool (32), which comprises the flanging profile (47) for the neck (12) of the eyelet part (10) and which also has a ring-shaped cutting edge (42);
with an upper tool (31), which holds the eyelet part (10), can move up and down (37) relative to the lower tool (32), and has a central insert (33), which is able to move in the axial direction against spring force (35);
where the carrier web (20) is positioned between the two tools (31, 32), and the cutting edge (42) of the lower tool (32) works with the end surface (43) of the central insert (33) to perform a hole-cutting action (29) on the carrier web (20) situated between them;
with a thrust ring (34) in the lower tool (32), which is located a certain radial distance away from the flanging profile (47) and is subjected to a force (36) directed toward the upper tool (31);
where the radius (46) of the hole of the cutting edge (42) is smaller than the outside radius (26) of the neck (12) of the eyelet part (10),
characterised in that
the end surface (43) of the central insert (33) is essentially flat and free of pretensioning pins which prestretch the carrier web (20);
in that, at the point of maximum stroke between the two tools (31, 32), the thrust ring (34) is located essentially on the same level as the cutting edge (42) of the lower tool (32) and together with the cutting edge (42) forms a support plane (60) for the carrier web (20) to be placed between the two tools (31,32);
in that a counter-thrust ring (54) in the upper tool (31) is associated with the thrust ring (34) and is subject to a force (55) directed toward the lower tool (32); and
in that the carrier web (20) is tensioned between the two rings (34, 54) during the stroke movement (37). - Device according to claim 9, characterised in that the two rings (34, 54) are provided with two opposing bevelled surfaces (58, 59), which face each other, and which tension the carrier web (20) between them during the working stroke of the tools (31, 32).
- Device according to claim 10, characterised in that the bevelled surface (58) and the support plane (60) form an acute angle (61) pointing in the direction (37) of the stroke, the support plane being determined by the support surface (45) of the thrust ring (34); and
in that the opposing bevelled surface (59) of the counter-thrust ring (54) is essentially parallel to the bevelled surface (58) of the thrust ring (34). - Device according to one of claims 9-11, characterised in that a helical compression spring has a ring-shaped end surface, and
in that this terminal ring-shaped surface forms the thrust ring (34), while the compression spring produces the force (36).
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10039462 | 2000-08-12 | ||
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 |
DE20104102U | 2001-03-09 | ||
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 |
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 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1309256A1 EP1309256A1 (en) | 2003-05-14 |
EP1309256B1 true EP1309256B1 (en) | 2004-12-29 |
Family
ID=26006681
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP01960266A Expired - Lifetime EP1309256B1 (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 |
Country Status (12)
Country | Link |
---|---|
US (1) | US6907647B2 (en) |
EP (1) | EP1309256B1 (en) |
CN (1) | CN1209987C (en) |
AT (1) | ATE285688T1 (en) |
AU (1) | AU2001281804A1 (en) |
CA (1) | CA2418293A1 (en) |
CZ (1) | CZ200370A3 (en) |
DE (1) | DE20112908U1 (en) |
ES (1) | ES2230351T3 (en) |
MX (1) | MXPA03000586A (en) |
PL (1) | PL203329B1 (en) |
WO (1) | WO2002013646A1 (en) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10202998C1 (en) * | 2002-01-26 | 2003-08-21 | Prym William Gmbh & Co Kg | Manual flaring tool for eyelets to be attached to pre-punched sheets |
WO2011007450A1 (en) * | 2009-07-17 | 2011-01-20 | Ykk株式会社 | Eyelet |
CN103298363A (en) * | 2011-01-13 | 2013-09-11 | Ykk株式会社 | Eyelet washer and eyelet-fastening method |
JP5996245B2 (en) * | 2012-04-17 | 2016-09-21 | モリト株式会社 | How to install the eyelet on the fabric |
US9987816B2 (en) * | 2014-03-19 | 2018-06-05 | E.L. Hatton Sales Co. | Banner making machine |
CN107771253B (en) * | 2015-06-30 | 2020-03-13 | 美国圣戈班性能塑料公司 | Sliding bearing |
ITUB20156087A1 (en) * | 2015-12-02 | 2017-06-02 | Douglas Marine Srl | PRESS FOR SHEETS OR THE LIKE, IN PARTICULAR FOR THE LOOK OF SAILS OR THE LIKE |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1565523A (en) * | 1924-07-28 | 1925-12-15 | Stuart Machine Co | Grommet making and setting machine |
US1838973A (en) | 1930-02-17 | 1931-12-29 | Wilder Leland Raynsford | Grommet setting device |
US2101060A (en) * | 1935-04-16 | 1937-12-07 | United Shoe Machinery Corp | Eyelet |
US2107375A (en) * | 1935-07-19 | 1938-02-08 | United Shoe Machinery Corp | Eyelet |
US2143087A (en) * | 1937-03-12 | 1939-01-10 | Stimpson Edwin B Co | Clamp grommet |
US2901800A (en) * | 1953-09-10 | 1959-09-01 | C E M Company | Self coring grommet |
US3328854A (en) * | 1965-04-26 | 1967-07-04 | Hettrick Mfg Co | Grommet reinforcement for canvas material |
FR1577474A (en) * | 1968-06-04 | 1969-08-08 | ||
US4479287A (en) * | 1981-05-10 | 1984-10-30 | Hitoshi Asaka | Eye hole for roping reinforced by grommet metal fittings as in sheet-like articles |
US4890362A (en) * | 1988-12-23 | 1990-01-02 | Morito Co., Ltd. | Eyelet and method of attaching the same |
DK169822B1 (en) * | 1992-10-20 | 1995-03-06 | Polysheet As | Anchorage eye for press openings and similar covers. |
DE9405177U1 (en) | 1994-03-26 | 1994-06-09 | Leifheit Ag, 56377 Nassau | Eyelet for curtains |
DE29903124U1 (en) | 1999-02-20 | 1999-05-06 | Franz Miederhoff Ohg, 59846 Sundern | Tool for inserting an eyelet into a flexible workpiece |
-
2001
- 2001-06-02 CA CA002418293A patent/CA2418293A1/en not_active Abandoned
- 2001-06-02 MX MXPA03000586A patent/MXPA03000586A/en unknown
- 2001-06-02 ES ES01960266T patent/ES2230351T3/en not_active Expired - Lifetime
- 2001-06-02 PL PL360079A patent/PL203329B1/en unknown
- 2001-06-02 CZ CZ200370A patent/CZ200370A3/en unknown
- 2001-06-02 EP EP01960266A patent/EP1309256B1/en not_active Expired - Lifetime
- 2001-06-02 WO PCT/EP2001/006316 patent/WO2002013646A1/en active IP Right Grant
- 2001-06-02 CN CNB018140831A patent/CN1209987C/en not_active Expired - Fee Related
- 2001-06-02 AT AT01960266T patent/ATE285688T1/en active
- 2001-06-02 US US10/333,873 patent/US6907647B2/en not_active Expired - Fee Related
- 2001-06-02 AU AU2001281804A patent/AU2001281804A1/en not_active Abandoned
- 2001-08-09 DE DE20112908U patent/DE20112908U1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
DE20112908U1 (en) | 2001-11-08 |
CA2418293A1 (en) | 2003-02-04 |
ATE285688T1 (en) | 2005-01-15 |
MXPA03000586A (en) | 2004-12-13 |
PL360079A1 (en) | 2004-09-06 |
AU2001281804A1 (en) | 2002-02-25 |
CN1209987C (en) | 2005-07-13 |
PL203329B1 (en) | 2009-09-30 |
ES2230351T3 (en) | 2005-05-01 |
CZ200370A3 (en) | 2003-06-18 |
US20030167610A1 (en) | 2003-09-11 |
EP1309256A1 (en) | 2003-05-14 |
US6907647B2 (en) | 2005-06-21 |
WO2002013646A1 (en) | 2002-02-21 |
CN1446061A (en) | 2003-10-01 |
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