EP0677019B1 - Winding device - Google Patents

Winding device Download PDF

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Publication number
EP0677019B1
EP0677019B1 EP94903769A EP94903769A EP0677019B1 EP 0677019 B1 EP0677019 B1 EP 0677019B1 EP 94903769 A EP94903769 A EP 94903769A EP 94903769 A EP94903769 A EP 94903769A EP 0677019 B1 EP0677019 B1 EP 0677019B1
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EP
European Patent Office
Prior art keywords
plane
thread
winding
cross
stroke
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
Application number
EP94903769A
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German (de)
French (fr)
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EP0677019A1 (en
Inventor
Herbert Turk
Herbert Schiminski
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Oerlikon Barmag AG
Original Assignee
Barmag AG
Barmag Barmer Maschinenfabrik AG
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Publication of EP0677019A1 publication Critical patent/EP0677019A1/en
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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65HHANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H54/00Winding, coiling, or depositing filamentary material
    • B65H54/02Winding and traversing material on to reels, bobbins, tubes, or like package cores or formers
    • B65H54/28Traversing devices; Package-shaping arrangements
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65HHANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H54/00Winding, coiling, or depositing filamentary material
    • B65H54/02Winding and traversing material on to reels, bobbins, tubes, or like package cores or formers
    • B65H54/28Traversing devices; Package-shaping arrangements
    • B65H54/2836Traversing devices; Package-shaping arrangements with a rotating guide for traversing the yarn
    • B65H54/2839Traversing devices; Package-shaping arrangements with a rotating guide for traversing the yarn counter rotating guides, e.g. wings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65HHANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H59/00Adjusting or controlling tension in filamentary material, e.g. for preventing snarling; Applications of tension indicators
    • B65H59/005Means compensating the yarn tension in relation with its moving due to traversing arrangements
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65HHANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H2701/00Handled material; Storage means
    • B65H2701/30Handled filamentary material
    • B65H2701/31Textiles threads or artificial strands of filaments

Definitions

  • the invention relates to a winding machine according to the preamble of claim 1.
  • a winding machine is, for. B. known from DE-A-34 04 303, EP-A-120 216, DE-C-34 17 457, DE-A-37 03 731 A1.
  • the guide ruler has the following function:
  • the driver arms have a constant angular velocity, but in the traversing direction, in which the thread is to be moved back and forth parallel to the bobbin axis, the guiding speed differs between the stroke ends.
  • the guiding speed depends on the constantly changing angular position of the wings and is therefore meaningful.
  • the main guideline deflects the thread out of the traversing plane in such a way that these speed differences are compensated for in the desired manner.
  • the traversing plane is the tangential plane that is created by the head thread guide and the next rotating cylinder. on which the thread runs, is stretched.
  • the head thread guide lies in the middle above the traverse stroke. It is at such a distance from the rotary cylinder that the thread accommodates the thread tension fluctuations caused by the traversing movement can endure. These thread tension fluctuations result from the fact that the thread length between the head thread guide and the rotating body changes continuously as a result of the traversing movement, that is to say increases and decreases.
  • the rotating body is generally a contact roller, on which the thread runs and which the thread partially wraps around, in order to then run towards the bobbin.
  • the object of the invention is. to avoid these large differences in the wrap angle, which also lead to different thread tensions, and thereby enable large traversing strokes.
  • the maximum wrap angles which naturally occur in the area of the greatest deviation of the guide rulers from the traversing plane, can be reduced very greatly.
  • An arrangement is preferred in which the maximum wrap angles are approximately the same size, so that the thread tension within certain Limits remain.
  • the advantage of the invention is that an inadmissible reduction in the thread tension in the end regions of the traverse stroke can be avoided.
  • the thread tension In the known winding machine, the thread tension must be chosen so high that it does not fall below a minimum value even in the stroke end areas. On the other hand, this means that the thread tension is relatively high in the central region of the traversing stroke.
  • the development according to claim 2 also brings about an equalization of the thread tension.
  • the bobbin When winding a multifilament thread, the bobbin must be manufactured in such a way that the thread can run off the bobbin even at high speed. It becomes possible in particular when the thread is deposited on the bobbin in a closed form, ie: as if it were a uniform, essentially round body. The opposite of this is that the individual filaments that make up the thread are placed side by side on the spool. In this case, when the thread runs off, there is a risk that the individual filament elements belonging together will not come loose from the winding surface simultaneously and uniformly. The thread then runs unevenly and thread breakage or filament breakage can occur.
  • Claim 3 has the particular advantage that in this embodiment of the invention the thread is deposited on the bobbin as a closed body - and not as a wide band consisting of individual filaments. In particular, it is avoided in this embodiment that a connection of the individual filaments that was previously through Blow out a sharp air flow on the thread has been made (tangling), is picked up and dissolved again.
  • the embodiment according to claim 4 allows a particularly exact thread transfer from one wing to the other in the reversal areas and avoids the mechanical engineering problem of the tight response of the guidelines.
  • the main guide In principle, it is possible to arrange the main guide on one or the other side of the thread plane. However, it is preferred that the main guide lies between the thread running plane and the rotor axis plane (claim 5). This is particularly advantageous for the operation and application of the thread.
  • the respective guide rule consists of a frame attached to the machine frame and circumscribing a window. The part of the frame that projects into the traversing plane forms the guideline. For the rest, the window is cut out so far that especially the end regions of the traversing stroke, in which the thread is transferred from one wing to the other, are visible.
  • a thread runs over a head thread guide 13 to a traversing device and from there to a contact roller 12.
  • the thread loops around the contact roller 12 partially, e.g. B. at 60 ° and then runs on the coil 16.
  • the contact roller is in circumferential contact with the coil 16.
  • the coil 16 is formed on a cardboard sleeve or plastic sleeve 15.
  • the plastic sleeve 15 is clamped on a spindle 14.
  • the spindle 14 will driven at a speed. which decreases in the course of the winding travel.
  • the spindle drive is controlled as a function of the speed of the contact roller 12, which is measured for this purpose.
  • the control of the spindle or the spindle drive is done in this way. that the speed of the contact roller 12 remains constant.
  • the traversing device consists of the rotors 1 and 2, on which several driver arms - also called wings in the context of this application - are attached.
  • the rotor 1 has z. B. two drive arms 5 and 6, which are each offset by 180 ° to each other.
  • the rotor 2 has the driver arms 3 and 4, which are also offset from one another by 180 °.
  • the rotors are arranged so that the driver arms 6 on the one hand and 3, 4 on the other hand rotate in two closely adjacent, mutually parallel planes of rotation. However, as can be seen from FIG. 5, the rotor axes are arranged eccentrically parallel to the coil.
  • the rotors are driven with the opposite direction of rotation and a phase shift of 90 °. If each of the rotors z. B. has three driver arms, these are offset by 120 ° to each other.
  • the thread is guided along a guide ruler 9 (main guide ruler).
  • a guide ruler 9 main guide ruler
  • Such a traversing device is described, for example, in EP-A-114 642 (Bag. 1321).
  • FIGS. 1 and 5 The following is shown in FIGS. 1 and 5:
  • Each of the rotors 1 and 2 of FIG. 5 has two to each other by 180 ° offset driver arms 3 and 4 or 5 and 6.
  • the driving arm 5 currently has the thread guide and guides the thread to the left. At the traversing stroke end (line 7), it delivers the thread to the oncoming driver arm 7 of the rotor 2 rotating in opposite directions.
  • the main guide ruler 9 projects into the traversing plane with a certain shape, which is indicated here as line 10; ie: The thread comes from the direction of the viewer and the traversing plane is perpendicular to the paper plane.
  • the auxiliary guide rulers 11 are arranged in two planes that are closely adjacent to both the rotational planes of the driver arms and to one another.
  • the main guideline protrudes from the same side into the traversing plane as the drive arms.
  • the auxiliary guidelines 11 protrude from the opposite side into the traversing plane 10.
  • the main guide ruler 9 and the auxiliary guide ruler 11 overlap in the stroke end regions.
  • the auxiliary guidelines take over approximately or preferably - viewed from the center of the traversing stroke - somewhat before the intersection of the traversing plane 10 with the Main guideline 9. This ensures that the wrap angles on the main and auxiliary rulers are approximately the same size.
  • the main guide 9 and the auxiliary guides 11 do not necessarily have to be arranged such that an overlap (view in the thread direction) takes place. Rather, the relative arrangement of the guide lines depends on the overall geometric arrangement of the thread path, the traversing device, the contact roller and the bobbin.
  • phase IV the main ruler has completely withdrawn from the traversing level.
  • the thread is now guided exclusively by the auxiliary guide.
  • the traversing stroke end is shown in phase V.
  • the thread is transferred from one wing 4 of one rotor to the other wing 6 of the other rotor.
  • the auxiliary guide also has the sole guidance of the thread in the traversing direction.
  • FIGS. 6 and 7 Another special feature of the exemplary embodiment according to FIGS. 6 and 7 is that the main guide 9 and the auxiliary guides 11 are arranged in closely spaced parallel planes in front of the wing planes. This arrangement ensures that the thread does not break down into its individual filaments when it is lifted off on the contact roller 12 or the bobbin. Rather, the thread is deposited on the spool as a closed bundle of filaments and consequently also pulled off the spool as a closed bundle of filaments during unwinding. In the described wing maneuvering, it is necessary to adjust the wings on the rotors exactly so that the thread is transferred from one wing to the other wing at a certain point. For this you have to be able to watch the wings. Windows 17 of the main guideline and 18 of the auxiliary guideline serve this purpose. The guidelines are designed as a frame that leaves one window open.

Abstract

A winding machine for winding a continuously supplied thread into a cross-wound bobbin has a cross-winding device which conveys the thread back and forth along a predetermined section which lies across the running direction of the thread. The winding machine has the following characteristics: the thread guide is centrally fixed above the cross-winding stroke and defines a tangential plane to a rotary cylinder that follows the cross-winding device. Driving arms (5, 6, 7, 8) are secured to two rotors (1, 2) that rotate in opposite directions. The axes of the rotors are arranged in a common plane (12). The wings move in two closely adjacent, parallel planes which perpendicularly intersect the planes (12) of the rotor axes. On one side of the thread running plane (10), a first template (9) is arranged in a plane which is closely adjacent and parallel to one of the planes of the wings and projects into the cross-winding plane, deflecting the head thread guide (13) in such a way that the thread is conveyed back and forth in the cross-winding direction at a substantially constant cross-winding speed or at a cross-winding speed predetermined according to a determined law of motion. Auxiliary templates (11) in the area of the ends of the cross-winding stroke lie in a plane parallel to the plane of the wings and are arranged on the side of the cross-winding plane (10) opposite to the main template (9). The planes (12) of the rotor axes and the main template (9) are arranged with respect to the cross-winding plane (10) in such a way that the main template does not project into the cross-winding plane in the area of the ends of the stroke, whereas the auxiliary templates (11) project into the cross-winding plane in the areas of the ends of the stroke, taking over the functions of guiding the thread and determining the cross-winding speed.

Description

Die Erfindung betrifft eine Aufspulmaschine nach dem Oberbegriff des Anspruches 1. Eine derartige Aufspulmaschine ist z. B. bekannt durch die DE-A-34 04 303, EP-A-120 216, DE-C-34 17 457, DE-A-37 03 731 A1.The invention relates to a winding machine according to the preamble of claim 1. Such a winding machine is, for. B. known from DE-A-34 04 303, EP-A-120 216, DE-C-34 17 457, DE-A-37 03 731 A1.

Bei den Changiereinrichtungen dieser Aufspulmaschinen hat das Leitlineal folgende Funktion: Die Mitnehmerarme haben konstante Winkelgeschwindigkeit, besitzen jedoch in Changierrichtung, in der der Faden parallel zur Spulenachse hin- und herzuführen ist, zwischen den Hubenden unterschiedliche Führungsgeschwindigkeit. Die Führungsgeschwindigkeit ist von der sich ständig ändernden Winkelstellung der Flügel abhängig und daher sinnsförmig. Das Hauptleitlineal lenkt den Faden aus der Changierebene derart aus, daß diese Geschwindigkeitsunterschiede in gewünschter Weise kompensiert werden. Durch entsprechende Formgebung des Leitlineals läßt sich erreichen, daß die Changiergeschwindigkeit zwischen den Hubenden - d. h. abgesehen von den kurzen Umkehrbereichen, in denen die Bewegungsrichtung umgekehrt wird - konstant ist. Es können durch die Formgebung des Leitlinieals und der Flügel aber auch gewünschte Bewegungsgesetze vorgegeben werden. Dabei ist als Changierebene die Tangentialebene bezeichnet, die durch den Kopffadenführer und den nächsten Drehzylinder. auf welchen der Faden aufläuft, aufgespannt wird. Der Kopffadenführer liegt mittig über dem Changierhub. Er hat einen solchen Abstand von dem Drehzylinüer, daß der Faden die Fadenspannungsschwankungen, die durch die Changierbewegung entstehen, ertragen kann. Diese Fadenspannungsschwankungen entstehen dadurch, daß sich die Fadenlänge zwischen Kopffadenführer und Drehkörper infolge der Changierbewegung laufend ändert, d.h. vergrößert und verkleinert. Bei dem Drehkörper handelt es sich im allgemeinen um eine Kontaktwalze, auf die der Faden aufläuft und die der Faden teilweise umschlingt, um sodann der Spule zuzulaufen.In the traversing devices of these winding machines, the guide ruler has the following function: The driver arms have a constant angular velocity, but in the traversing direction, in which the thread is to be moved back and forth parallel to the bobbin axis, the guiding speed differs between the stroke ends. The guiding speed depends on the constantly changing angular position of the wings and is therefore meaningful. The main guideline deflects the thread out of the traversing plane in such a way that these speed differences are compensated for in the desired manner. By appropriate shaping of the guide ruler it can be achieved that the traversing speed between the stroke ends - ie apart from the short reversing areas in which the direction of movement is reversed - is constant. The shape of the guideline and the wings can also be used to specify desired laws of motion. The traversing plane is the tangential plane that is created by the head thread guide and the next rotating cylinder. on which the thread runs, is stretched. The head thread guide lies in the middle above the traverse stroke. It is at such a distance from the rotary cylinder that the thread accommodates the thread tension fluctuations caused by the traversing movement can endure. These thread tension fluctuations result from the fact that the thread length between the head thread guide and the rotating body changes continuously as a result of the traversing movement, that is to say increases and decreases. The rotating body is generally a contact roller, on which the thread runs and which the thread partially wraps around, in order to then run towards the bobbin.

Bei den Changiereinrichtungen nach dem Stand der Technik ist es möglich, den Faden über einen großen Changierhub, z.B. 250 mm mit nur einem Rotor für jede Bewegungsrichtung jeweils hin- und herzuführen. Dadurch müssen jedoch große Unterschiede der Führungsgeschwindigkeit kompensiert werden. Deshalb ragt das Leitlineal namentlich im mittleren Bereich des Chanigerhubes weit in die Changierebene hinein, während es im Bereich der Changierhubenden nahe an der Changierebene liegt. Entsprechend groß ist der Umschlingungswinkel des Fadens am Leitlineal im mittleren Bereich des Changierhubs und entsprechend klein ist der Umschlingungswinkel des Fadens am Leitlineal im Bereich der Hubenden.In the traversing devices according to the prior art, it is possible to thread the thread over a large traversing stroke, e.g. 250 mm back and forth with just one rotor for each direction of movement. However, this has to compensate for large differences in the guiding speed. That is why the guideline protrudes far into the traversing plane, especially in the middle area of the Chaniger stroke, while it is close to the traversing plane in the area of the traversing stroke ends. The wrap angle of the thread on the guide ruler is correspondingly large in the central region of the traversing stroke and the wrap angle of the thread on the guide ruler is correspondingly small in the region of the stroke ends.

Aufgabe der Erfindung ist. diese großen Unterschiede des Umschlingungswinkels, die auch zu unterschiedlichen Fadenspannungen führen, zu vermeiden, und dadurch große Changierhübe zu ermöglichen.The object of the invention is. to avoid these large differences in the wrap angle, which also lead to different thread tensions, and thereby enable large traversing strokes.

Die Lösung ergibt sich aus dem Anspruch 1.The solution results from claim 1.

Mit dieser Lösung lassen sich die maximalen Umschlingungswinkel, die naturgemäß in dem Bereich der größten Abweichung der Leitlineale aus der Changierebene auftreten, sehr stark reduzieren. Bevorzugt ist eine Anordnung, bei der die maximalen Umschlingungswinkel in etwa gleich groß sind, so daß die Fadenspannung innerhalb bestimmter Grenzen bleibt. Der Vorteil der Erfindung ist, daß eine unzulässige Verminderung der Fadenspanung in den Endbereichen des Changierhubs vermieden werden kann. Bei der bekannten Aufspulmaschine muß die Fadenspannung so hoch gewählt werden, daß sie auch in den Hubendbereichen einen Mindestwert nicht unterschreitet. Das bedeutet andererseits, daß die Fadenspannung im mittleren Bereich des Changierhubes relativ hoch liegt. Mit der Erfindung gelingt es dagegen, in den Hubendbereichen der Tendenz zur Verminderung der Fadenspannung entgegenzuwirken und auch bei niedrig gewählter Fadenspannung oberhalb des Minimalwertes zu bleiben.With this solution, the maximum wrap angles, which naturally occur in the area of the greatest deviation of the guide rulers from the traversing plane, can be reduced very greatly. An arrangement is preferred in which the maximum wrap angles are approximately the same size, so that the thread tension within certain Limits remain. The advantage of the invention is that an inadmissible reduction in the thread tension in the end regions of the traverse stroke can be avoided. In the known winding machine, the thread tension must be chosen so high that it does not fall below a minimum value even in the stroke end areas. On the other hand, this means that the thread tension is relatively high in the central region of the traversing stroke. With the invention, on the other hand, it is possible to counteract the tendency to decrease the thread tension in the stroke end regions and to remain above the minimum value even with a low thread tension.

Auch die Weiterbildung nach Anspruch 2 bewirkt eine Vergleichmäßigung der Fadenspannung.The development according to claim 2 also brings about an equalization of the thread tension.

Beim Aufwickeln eines multifilen Fadens muß die Spule so hergestellt werden, daß der Faden auch mit hoher Geschwindigkeit wieder von der Spule ablaufen kann. Es wird insbesondere dann möglich, wenn der Faden in geschlossener Form auf der Spule abgelegt wird, d.h.: als ob er ein einheitlicher, im wesentlichen runder Körper wäre. Das Gegenteil davon ist, daß die einzelnen Filamente, aus denen der Faden besteht, nebeneinander auf der Spule abgelegt werden. In diesem Falle besteht beim Ablaufen des Fadens die Gefahr, daß sich die einzelnen zusammengehörenden Filamtente nicht gleichzeitig und gleichmäßig von der Wickeloberfläche lösen. Der Faden läuft dann ungleichmäßig ab und es kann zum Fadenbruch oder Filamentbruch kommen. Anspruch 3 hat den besonderen Vorteil, daß bei dieser Ausgestaltung der Erfindung der Faden als geschlossener Körper - und nicht als breites, aus einzelnen Filamenten bestendes Band - auf der Spule abgelegt wird. Insbesondere wird bei dieser Ausgesaltung vermieden, daß eine Verbindung der einzelnen Filamente, die zuvor durch Ausblasen eines scharfen Luftstromes auf den Faden vorgenommen worden ist (Tangelung), wieder aufgehoben und aufgelöst wird.When winding a multifilament thread, the bobbin must be manufactured in such a way that the thread can run off the bobbin even at high speed. It becomes possible in particular when the thread is deposited on the bobbin in a closed form, ie: as if it were a uniform, essentially round body. The opposite of this is that the individual filaments that make up the thread are placed side by side on the spool. In this case, when the thread runs off, there is a risk that the individual filament elements belonging together will not come loose from the winding surface simultaneously and uniformly. The thread then runs unevenly and thread breakage or filament breakage can occur. Claim 3 has the particular advantage that in this embodiment of the invention the thread is deposited on the bobbin as a closed body - and not as a wide band consisting of individual filaments. In particular, it is avoided in this embodiment that a connection of the individual filaments that was previously through Blow out a sharp air flow on the thread has been made (tangling), is picked up and dissolved again.

Voraussetzung hier - wie auch bei allen sonstigen Ausführungen - ist, daß die beiden Leitlineale sehr dicht zueinander und zu den Drehebenen der Mitnehmerarme angeordnet sind.A prerequisite here - as with all other versions - is that the two guide lines are arranged very close to one another and to the rotational planes of the driving arms.

Die Ausgestaltung nach Anspruch 4 erlaubt eine besonders exakte Fadenübergabe von einem Flügel auf den anderen in den Umkehrbereichen und vermeidet das maschinenbauliche Problem der dichten Anwordnung der Leitlineale.The embodiment according to claim 4 allows a particularly exact thread transfer from one wing to the other in the reversal areas and avoids the mechanical engineering problem of the tight response of the guidelines.

Es ist grundsätzlich möglich, das Hauptleitlineal auf der einen oder der anderen Seite der Fadenlaufebene anzuordnen. Bevorzugt ist jedoch, daß das Hauptleitlineal zwischen der Fadenlaufebene und der Rotorachsebene liegt (Anspruch 5). Dies ist insbesondere für die Bedienung und das Anlegen des Fadens von Vorteil.In principle, it is possible to arrange the main guide on one or the other side of the thread plane. However, it is preferred that the main guide lies between the thread running plane and the rotor axis plane (claim 5). This is particularly advantageous for the operation and application of the thread.

Es wurde bereits zuvor ausgeführt, daß es zweckmäßig ist, zumindest das Hauptleitlineal - in Fadenlaufrichtung - vor der Flügelebene anzuordnen. In diesem Falle verdeckt das Hauptleitlineal die Flügel, wenn es gleichzeitg zwischen der Anlaufebene und der Rotorachsebene angeordnet ist. Dadurch wird die richtige Relativeinstellung der Rotoren erschwert. Zur Vermeidung dient die weitere Ausgestaltung nach Anspruch 6. Dabei besteht das jeweilige Leitlineal aus einem am Maschinengestellt befestigten Rahmen, der ein Fenster umschreibt. Der Teil des Rahmens, der in die Changierebene ragt, bildet das Leitlineal. Im übrigen ist das Fenster so weit ausgeschnitten, daß vor allem die Endbereiche des Changierhubes, in denen die Übergabe des Fadens von dem einen Flügel auf den anderen erfolgt, sichtbar sind.It has already been stated that it is expedient to arrange at least the main guide - in the thread running direction - in front of the wing plane. In this case, the main guideline hides the wings if it is simultaneously arranged between the approach plane and the rotor axis plane. This makes the correct relative setting of the rotors difficult. The further embodiment according to claim 6 serves to avoid this. The respective guide rule consists of a frame attached to the machine frame and circumscribing a window. The part of the frame that projects into the traversing plane forms the guideline. For the rest, the window is cut out so far that especially the end regions of the traversing stroke, in which the thread is transferred from one wing to the other, are visible.

Im folgenden wird ein Ausführungsbeispiel der Erfindung anhand der Zeichnung beschrieben.In the following an embodiment of the invention is described with reference to the drawing.

Es zeigen

Fig. 1 und Fig. 2
Seitenansichten einer konventionellen Aufspulmaschine, wobei unterschiedliche Fadenstellungen bzgl. des Changierhubes dargestellt sind;
Fig. 3 und Fig. 4
ein Ausführungsbeispiel der Erfindung mit unterschiedlichen Fadenstellungen längs des Changierhubes;
Fig. 5
die Aufsicht (schematisch) auf eine Changiereinrichtung mit Hauptleitlineal und Hilfsleitlinealen;
Fig. 6
die Aufsicht weiterer Ausführungsbeispiele;
Fig. 7
die Seitenansicht eines Ausführungsbeispiels in mehreren Phasen der Changierbewegung.
Show it
1 and 2
Side views of a conventional winding machine, different thread positions are shown with respect to the traverse stroke;
3 and 4
an embodiment of the invention with different thread positions along the traversing stroke;
Fig. 5
the supervision (schematic) of a traversing device with a main guide and auxiliary guides;
Fig. 6
the supervision of further exemplary embodiments;
Fig. 7
the side view of an embodiment in several phases of the traversing movement.

Die in dieser Anmeldung dargestellten Ausführungsbeispiele von Aufspulmaschinen haben das folgende gemeinsam: Ein Faden läuft über einen Kopffadenführer 13 einer Changiereinrichtung zu und von dort einer Kontaktwalze 12. Der Faden umschlingt die Kontaktwalze 12 teilweise, z. B. mit 60° und läuft sodann auf die Spule 16 auf. Die Kontaktwalze liegt im Umfangskontakt mit der Spule 16. Die Spule 16 wird auf einer Papphülse oder Kunststoffhülse 15 gebildet. Die Kunststoffhülse 15 ist auf einer Spindel 14 aufgespannt. Die Spindel 14 wird mit einer Drehzahl angetrieben. die im Verlaufe der Spulreise abnimmt. Die Steuerung des Spindelantriebes geschieht in Abhängigkeit von der Drehzahl der Kontaktwalze 12, die hierzu gemessen wird. Die Steuerung der Spindel bzw. des Spindelantriebes geschieht so. daß die Drehzahl der Kontaktwalze 12 konstant bleibt. Die Changiereinrichtung besteht aus den Rotoren 1 und 2, an denen mehrere Mitnehmerarme - im Rahmen dieser Anmeldung auch Flügel genannt - befestigt sind. Der Rotor 1 weist z. B. zwei Mitnehmerarme 5 und 6 auf, die jeweils um 180° zueinander versetzt sind. Der Rotor 2 weist die Mitnehmerarme 3 und 4 auf, die ebenfalls um 180° zueinander versetzt sind. Die Rotoren sind so angeordnet, daß die Mitnehmerarme 6 einerseits und 3, 4 andererseits in zwei eng benachbarten, zueinander parallelen Drehebenen umlaufen. Dabei sind jedoch die Rotorachsen - wie aus Fig. 5 ersichtlich - achsparallel zur Spule exzentrisch angeordnet.The embodiments of winding machines shown in this application have the following in common: a thread runs over a head thread guide 13 to a traversing device and from there to a contact roller 12. The thread loops around the contact roller 12 partially, e.g. B. at 60 ° and then runs on the coil 16. The contact roller is in circumferential contact with the coil 16. The coil 16 is formed on a cardboard sleeve or plastic sleeve 15. The plastic sleeve 15 is clamped on a spindle 14. The spindle 14 will driven at a speed. which decreases in the course of the winding travel. The spindle drive is controlled as a function of the speed of the contact roller 12, which is measured for this purpose. The control of the spindle or the spindle drive is done in this way. that the speed of the contact roller 12 remains constant. The traversing device consists of the rotors 1 and 2, on which several driver arms - also called wings in the context of this application - are attached. The rotor 1 has z. B. two drive arms 5 and 6, which are each offset by 180 ° to each other. The rotor 2 has the driver arms 3 and 4, which are also offset from one another by 180 °. The rotors are arranged so that the driver arms 6 on the one hand and 3, 4 on the other hand rotate in two closely adjacent, mutually parallel planes of rotation. However, as can be seen from FIG. 5, the rotor axes are arranged eccentrically parallel to the coil.

Die Rotoren werden mit entgegengesetzter Drehrichtung und einer Phasenversetzung von 90° angetrieben. Sofern jeder der Rotoren z. B. drei Mitnehmerarme hat, sind diese um 120° zueinander versetzt. Durch die Flügel 3 bis 6 wird der Faden an einem Leitlineal 9 (Hauptleitlineal) entlangeführt. Bei jedem Weg wird der Faden durch einen Flügel des einen Rotors geführt. An den Hubenden taucht dieser Flügel unter das Leitlineal und die Fadenführung in der entgegengesetzten Richtung wird sodann von einem der Flügel des anderen Rotors übernommen, der in diesem Augenblick unter dem Leitlineal hervorkommt. Eine derartige Changiereinrichtung ist zum Beispiel beschrieben in der EP-A-114 642 (Bag. 1321).The rotors are driven with the opposite direction of rotation and a phase shift of 90 °. If each of the rotors z. B. has three driver arms, these are offset by 120 ° to each other. Through the wings 3 to 6, the thread is guided along a guide ruler 9 (main guide ruler). Each time the thread is passed through a wing of one rotor. At the end of the stroke, this wing dips under the guide ruler and the thread guide in the opposite direction is then taken over by one of the wings of the other rotor, which comes out from under the guide ruler at this moment. Such a traversing device is described, for example, in EP-A-114 642 (Bag. 1321).

Hierzu ist in Fig. 1 und Fig. 5 folgendes dargestellt:The following is shown in FIGS. 1 and 5:

Jeder der Rotoren 1 und 2 nach Fig. 5 weist zwei um 180° zueinander versetzte Mitnehmerarme 3 und 4 bzw. 5 und 6 auf. Der Mitnehmerarm 5 hat derzeit die Fadenführung und führt den Faden nach links. An dem Changierhubende (Linie 7) gibt er den Faden an den entgegenkommenden Mitnehmerarm 7 des gegensinnig rotierenden Rotors 2 ab. Das Hauptleitlineal 9 ragt mit einer bestimmten Formgebung in die Changierebene hinein, die hier als Linie 10 angedeutet ist; d. h.: Der Faden kommt aus der Richtung des Betrachters und die Changierebene liegt senkrecht auf der Papierebene. In dem Bereich der Changierhubenden sind die Hilfsleitlineale 11 angeordnet, und zwar in zwei Ebenen, die sowohl den Drehebenen der Mitnehmerarme als auch zueinander dicht benachbart sind. Das Hauptleitlineal ragt von derselben Seite her in die Changierebene wie die Mitnehmerarme. Die Hilfsleitlineale 11 ragen von der entgegengesetzten Seite in die Changierebene 10 hinein.Each of the rotors 1 and 2 of FIG. 5 has two to each other by 180 ° offset driver arms 3 and 4 or 5 and 6. The driving arm 5 currently has the thread guide and guides the thread to the left. At the traversing stroke end (line 7), it delivers the thread to the oncoming driver arm 7 of the rotor 2 rotating in opposite directions. The main guide ruler 9 projects into the traversing plane with a certain shape, which is indicated here as line 10; ie: The thread comes from the direction of the viewer and the traversing plane is perpendicular to the paper plane. In the area of the traversing stroke ends, the auxiliary guide rulers 11 are arranged in two planes that are closely adjacent to both the rotational planes of the driver arms and to one another. The main guideline protrudes from the same side into the traversing plane as the drive arms. The auxiliary guidelines 11 protrude from the opposite side into the traversing plane 10.

Es zeigt nun die Aufspulmaschine nach dem Stand der Technik (Fig. 1), daß das Hauptleitlineal 9 in den Figuren 1 und 2 sowohl am Ende des Changierhubes (Darstellung nach Fig. 1) wie auch in der Mitte des Changierhubes (Darstellung nach Fig. 2) den Faden aus der gestrichelt dargestellten Changierebene 10 ablenkt.It now shows the winding machine according to the prior art (Fig. 1) that the main guide 9 in Figures 1 and 2 both at the end of the traversing stroke (representation according to Fig. 1) and in the middle of the traversing stroke (representation according to Fig. 2) deflects the thread from the traversing plane 10 shown in dashed lines.

Dadurch ergibt sich - wie Fig. 2 zeigt - im mittleren Bereich des Changierhubes eine sehr große Umschlingung des Fadens an dem Hauptleitlineal. In den Endbereichen ist - wie Fig. 1 zeigt - nur eine recht geringe Umschlingung übrig. Dieser Wechsel der Umschlingung hat auch eine entsprechende Änderung der Fadenzugkraft zur Folge, mit der der Faden auf die Kontaktwalze 12 bzw. auf der Spule 16 aufläuft. Über die wird der Faden in den Endbereichen - wie Fig. 1 zeigt - nicht mehr oder nur noch gering aus der Changierebene 10 ausgelenkt. Diese Auslenkung ist im mittleren Bereich des Changierhubes - wie Fig. 2 zeigt - sehr groß. Diese Auslenkung bewirkt eine große Fadenzugkraft, da der Faden von einem Lieferwerk mit fester Geschwindigkeit angeliefert wird und sich daher jede Auslenkung in eine entsprechende Dehnung und Vergrößerung der Fadenzugkraft umsetzt. Andererseits muß die Fadenspannung in den Endbereichen so groß sein, daß ein störungsfreier Spulbetrieb möglich ist. Folglich ist die Fadenspannung im mittleren Bereich umso größer und es läßt sich nicht immer vermeiden, daß die Fadenspannung im mittleren Bereich die Schädigungsgrenze übersteigt.As shown in FIG. 2, this results in a very large looping of the thread on the main guide in the central region of the traversing stroke. In the end areas, as shown in FIG. 1, there is only a very small wrap. This change in the wrap also results in a corresponding change in the thread tension with which the thread runs onto the contact roller 12 or onto the bobbin 16. The thread in the end regions - as shown in FIG. 1 - is no longer or only slightly deflected out of the traversing plane 10. This deflection is in the middle of the traversing stroke - As Fig. 2 shows - very large. This deflection results in a large thread tension, since the thread is delivered by a delivery device at a fixed speed and therefore each deflection translates into a corresponding extension and increase in the thread tension. On the other hand, the thread tension in the end regions must be so great that trouble-free winding operation is possible. Consequently, the thread tension in the middle area is all the greater and it cannot always be avoided that the thread tension in the middle area exceeds the damage limit.

Demgegenüber ist bei den Ausführungsbeispielen nach den Figuren 3 und 4 sowie 6 und 7 Abhilfe geschaffen.In contrast, the exemplary embodiments according to FIGS. 3 and 4 and 6 and 7 provide a remedy.

Aus den Figuren 3 und 4 mit dem ersten Ausführungsbeispiel nach der Erfindung ist ersichtlich, daß die gemeinsame Rotorachsebene 12 mit dem Hauptleitlineal soweit von der ebenfalls gestrichelt dargestellten Changierebene 10 entfernt ist, daß das Hauptleitlineal 9 an den Changierhubenden (s. Fig. 3) nicht mehr in die Changierebene hineinragt. Vielmehr ragen dort von der gegenüberliegenden Seite die Hilfsleitlineale 11 in die Changierebene hinein und übernehmen an den Changierhubenden, neben der Fadenführung und ggf. der Kompensation der Führungsgeschwindigkeit der Mitnehmerarme im Sinne eines gewünschten Verlaufs der Changiergeschwindigkeit, auch die Kompensation des Umschlingungswinkels, der an dem Hauptleitlineal verlorengeht sowie die Kompensation der Auslenkung des Fadens aus der Changierebene 10. Wie die Figuren 3 bis 5 zeigen, überlappen sich das Hauptleitlineal 9 und das Hilfsleitlineal 11 in den Hubendbereichen. Wie Fig. 5 zeigt, übernehmen die Hilfsleitlineale die Führung ungefähr oder vorzugsweise - von der Changierunghubmitte aus betrachtet - etwas vor dem Schnittpunkt der Changierebene 10 mit dem Hauptleitlineal 9. Dadurch wird erreicht, daß die Umschlingungswinkel an dem Haupt- und den Hilfslinealen annähernd gleich groß sind.From Figures 3 and 4 with the first embodiment according to the invention it can be seen that the common rotor axis plane 12 with the main guide ruler is so far removed from the traversing plane 10, also shown in broken lines, that the main guide ruler 9 at the traversing stroke ends (see FIG. 3) is not protrudes more into the traversing plane. Rather, the auxiliary guide rulers 11 protrude from the opposite side into the traversing plane and take over at the traversing stroke ends, in addition to the thread guidance and, if necessary, the compensation of the guiding speed of the driving arms in the sense of a desired course of the traversing speed, also the compensation of the wrap angle, which is on the main guiding ruler is lost as well as the compensation of the deflection of the thread from the traversing plane 10. As FIGS. 3 to 5 show, the main guide ruler 9 and the auxiliary guide ruler 11 overlap in the stroke end regions. As FIG. 5 shows, the auxiliary guidelines take over approximately or preferably - viewed from the center of the traversing stroke - somewhat before the intersection of the traversing plane 10 with the Main guideline 9. This ensures that the wrap angles on the main and auxiliary rulers are approximately the same size.

Wie die Figuren 6 und 7 zeigen, müssen das Hauptleitlineal 9 und die Hilfsleitlineale 11 nicht notwendigerweise so angeordnet sein, daß eine Überlappung (Sicht in Fadenrichtung) stattfindet. Vielmehr hängt die relative Anordnung der Leitlineale von der gesamten geometrischen Anordnung des Fadenlaufes, der Changiereinrichtung, der Kontaktwalze und der Spule ab.As FIGS. 6 and 7 show, the main guide 9 and the auxiliary guides 11 do not necessarily have to be arranged such that an overlap (view in the thread direction) takes place. Rather, the relative arrangement of the guide lines depends on the overall geometric arrangement of the thread path, the traversing device, the contact roller and the bobbin.

Die einzelnen Phasen sind in Fig. 6 durch die gestrichelten Linien I - V markiert. Fig. 7 zeigt dieselbe Aufspulmaschine in verschiedenen, in Pfeilrichtung aufeinander folgenden Phasen I - V der Changierbewegung. In Fig. 7 I ist die Situation in der Mitte des Changierhubes dargestellt. Der Flügel 4 führt den Faden während dieser durch das Hauptleitlineal 9 ausgelenkt wird. In der Phase II ist der Faden im Endbereich des Changierhubs bereits in den Führungsschlitz zwischen dem Hauptlineal 9 und dem Hilfslineal 11 eingetaucht. In dieser Phase berührt das Hilfsleitlineal 11 erstmalig den Faden. In der Phase III ist zu sehen, daß der Faden sowohl von dem Hauptlineal als auch von dem Hilfslineal ausgelenkt wird. Daher bleibt der Umschlingungswinkel im wesentlichen konstant.The individual phases are marked in FIG. 6 by the dashed lines IV. 7 shows the same winding machine in different phases I - V of the traversing movement which follow one another in the direction of the arrow. 7 I shows the situation in the middle of the traversing stroke. The wing 4 guides the thread while it is deflected by the main guide 9. In phase II, the thread in the end region of the traversing stroke is already immersed in the guide slot between the main ruler 9 and the auxiliary ruler 11. In this phase, the auxiliary guide 11 touches the thread for the first time. In phase III it can be seen that the thread is deflected by both the main ruler and the auxiliary ruler. Therefore, the wrap angle remains essentially constant.

In der Phase IV hat sich das Hauptlineal vollkommen aus der Changierebene zurückgezogen. Die Fadenführung erfolgt nunmehr ausschließlich durch das Hilfsleitlineal. In Phase V ist das Changierhubende dargestellt. Der Faden wird von dem einen Flügel 4 des einen Rotors auf den anderen Flügel 6 des anderen Rotors übergeben. In dieser Phase V hat ebenfalls das Hilfsleitlineal die alleinige Führung des Fadens in Changierrichtung.In phase IV, the main ruler has completely withdrawn from the traversing level. The thread is now guided exclusively by the auxiliary guide. The traversing stroke end is shown in phase V. The thread is transferred from one wing 4 of one rotor to the other wing 6 of the other rotor. In this phase V, the auxiliary guide also has the sole guidance of the thread in the traversing direction.

Eine weitere Besonderheit des Ausführungsbeispiels nach den Fig. 6 und 7 besteht darin, daß das Hauptleitlineal 9 und die Hilfsleitlineale 11 in eng beieinander gelegenen parallelen Ebenen vor den Flügelebenen angeordnet sind. Durch diese Anordnung wird erreicht, daß der Faden sich nicht beim Abheben auf der Kontaktwalze 12 bzw. der Spule in seine einzelnen Filamente zerlegt. Vielmehr wird der FAden als geschlossenes Filamentbündel auf der Spule abgelegt und folglich auch wieder als geschlossenes Filamentbündel beim Abwickeln von der Spule abgezogen. Bei der beschriebenen Flügelchangierung ist es erforderlich, die Flügel an den Rotoren exakt so zu justieren, daß der Faden an einem bestimmten Punkt von dem einen Flügel an den anderen Flügel übergeben wird. Hierzu muß man die Flügel beobachten können. Dazu dienen die Fenster 17 des Hauptleitlineals und 18 des Hilfsleitlineals. Die Leitlineale sind also als Rahmen ausgeführt, der jeweils ein Fenster freiläßt.Another special feature of the exemplary embodiment according to FIGS. 6 and 7 is that the main guide 9 and the auxiliary guides 11 are arranged in closely spaced parallel planes in front of the wing planes. This arrangement ensures that the thread does not break down into its individual filaments when it is lifted off on the contact roller 12 or the bobbin. Rather, the thread is deposited on the spool as a closed bundle of filaments and consequently also pulled off the spool as a closed bundle of filaments during unwinding. In the described wing maneuvering, it is necessary to adjust the wings on the rotors exactly so that the thread is transferred from one wing to the other wing at a certain point. For this you have to be able to watch the wings. Windows 17 of the main guideline and 18 of the auxiliary guideline serve this purpose. The guidelines are designed as a frame that leaves one window open.

BEZUGSZEICHENAUFSTELLUNGREFERENCE SIGN LISTING

11
Rotorrotor
22nd
Rotorrotor
33rd
MitnehmerarmDrive arm
44th
MitnehmerarmDrive arm
55
MitnehmerarmDrive arm
66
MitnehmerarmDrive arm
77
ChangierhubendeTraverse stroke end
88th
ChangierhubendeTraverse stroke end
99
HauptleitlinealMain guideline
1010th
ChangierebeneTraversing plane
1111
HilfsleitlinealeAuxiliary guidelines
1212th
KontaktwalzeContact roller
1313
KopffadenführerHead thread guide
1414
Spindelspindle
1515
HülseSleeve
1616
SpuleKitchen sink
1717th
Fensterwindow
1818th
Fensterwindow

Claims (6)

  1. A winding machine for winding a continuously running thread to form a cross-wound bobbin (16), with a reciprocating device, which reciprocates the thread over a given distance (reciprocation stroke), transversely to the running direction of the thread (reciprocation direction), and having the following features:
    a thread guide (13) (top thread guide), which is arranged in a fixed manner centrally above the reciprocation stroke and which sets up a tangential plane (10) (reciprocation plane) to a rotary cylinder (16) (bobbin or contact roller) following the reciprocating device;
    two rotors (1, 2) rotating in opposite directions with driving arms (3-6) (blades) secured thereon; the rotor axes are arranged in a common plane (rotor axis plane); the blades move in two closely adjacent, parallel planes (blade planes), which intersect the rotor axis planes at right angles;
    a first guide bar (9) (main guide bar), which is arranged on one side of the thread running plane in a plane (main guide bar plane) which lies closely adjacent and parallel to the blade planes, the guide bar projecting into the reciprocation plane and thereby deflecting the top thread guide (13) in such a manner that the thread is reciprocated in the reciprocation direction at a substantially constant reciprocating velocity or a velocity determined according to a specific law of motion;
    auxiliary guide bars (11) in the region of the ends of the reciprocation stroke (stroke ends), which lie in a plane (auxiliary bar plane) parallel to the blade planes and which are arranged on the side of the reciprocation plane opposite the main guide bar;
    characterised in that the rotor axis plane and the main guide plane (9) are arranged relative to the reciprocation plane (10) in such a manner that the main guide bar (9) does not project into the reciprocation plane (10) in the region of the stroke ends, and in the region of the stroke ends the auxiliary guide bars (11) project into the reciprocation plane (10) and thereby take over the thread guidance and the determining of the reciprocation velocity.
  2. A winding machine according to claim 1, characterised in that the rotor axis plane and the main guide bar (9) are arranged relative to the reciprocation plane (10) in such a manner that the angle of contact in the stroke centre of the main guide bar (9) and the angle of contact at the stroke ends of the auxiliary guide bars (11) are approximately equal.
  3. A winding machine according to claim 1 or claim 2, characterised in that the main guide bar (9) and the auxiliary guide bars (11) lie in planes (main bar plane; auxiliary bar plane), which - in the thread running direction - lie in front of the blade planes and closely adjacent to one another.
  4. A winding machine according to claim 1 or 2, characterised in that the main guide bar (9) - viewed in the thread running direction - and the auxiliary guide bar (11) - viewed in the thread running direction - lie on opposite sides of the blade planes.
  5. A winding machine according to one of the preceding claims, characterised in that the main guide bar (9) is arranged on the same side of the thread running plane as the rotor axis plane.
  6. A winding machine according to claim 5, characterised in that the guide bar (main guide bar 9 and/or auxiliary guide bar 11) arranged in front of the blade planes - viewed in the thread running direction - circumscribe a window (17, 18) for viewing the blades.
EP94903769A 1992-12-23 1993-12-14 Winding device Expired - Lifetime EP0677019B1 (en)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
DE4243671 1992-12-23
DE4243671 1992-12-23
DE4308989 1993-03-20
DE4308989 1993-03-20
PCT/EP1993/003527 WO1994014694A1 (en) 1992-12-23 1993-12-14 Winding device

Publications (2)

Publication Number Publication Date
EP0677019A1 EP0677019A1 (en) 1995-10-18
EP0677019B1 true EP0677019B1 (en) 1996-05-22

Family

ID=25921662

Family Applications (1)

Application Number Title Priority Date Filing Date
EP94903769A Expired - Lifetime EP0677019B1 (en) 1992-12-23 1993-12-14 Winding device

Country Status (8)

Country Link
US (1) US5624081A (en)
EP (1) EP0677019B1 (en)
JP (1) JPH08504728A (en)
KR (1) KR100197180B1 (en)
CN (1) CN1031933C (en)
DE (1) DE59302712D1 (en)
TW (1) TW295102U (en)
WO (1) WO1994014694A1 (en)

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Publication number Priority date Publication date Assignee Title
WO2015007339A1 (en) 2013-07-19 2015-01-22 SSM Schärer Schweiter Mettler AG Thread laying device and winding machine

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KR19990072105A (en) * 1996-10-12 1999-09-27 이.파우. 뢰르허 Spooling Device
WO1998016457A1 (en) * 1996-10-12 1998-04-23 Barmag Ag Winding-up machine for continuously arriving threads
DE19845325A1 (en) * 1997-10-10 1999-04-15 Barmag Barmer Maschf Bobbin winding assembly
WO2001030677A1 (en) * 1998-09-29 2001-05-03 Murata Kikai Kabushiki Kaisha Vane traverse device
JP2012012137A (en) * 2010-06-29 2012-01-19 Murata Machinery Ltd Yarn winding device
DE102014117678A1 (en) 2014-12-02 2016-06-02 Dietze & Schell Maschinenfabrik Gmbh & Co. Kg Wickelgutführungsvorrichtung
CN111910308A (en) * 2020-08-01 2020-11-10 陈勇 Abrasion-proof yarn tensioning structure

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US4505436A (en) * 1983-01-19 1985-03-19 Barmag Barmer Maschinenfabrik Ag Yarn winding apparatus
EP0120216B1 (en) * 1983-01-28 1986-10-29 b a r m a g Barmer Maschinenfabrik Aktiengesellschaft Traversing device with rotating fingers for a winding machine
CA1243257A (en) * 1983-10-18 1988-10-18 Masakazu Ito Multi-layer film or sheet material
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JP2560918B2 (en) * 1990-12-28 1996-12-04 村田機械株式会社 Traverse equipment
JP2850541B2 (en) * 1990-12-29 1999-01-27 東レ株式会社 Yarn traverse device

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Publication number Priority date Publication date Assignee Title
WO2015007339A1 (en) 2013-07-19 2015-01-22 SSM Schärer Schweiter Mettler AG Thread laying device and winding machine

Also Published As

Publication number Publication date
TW295102U (en) 1997-01-01
WO1994014694A1 (en) 1994-07-07
JPH08504728A (en) 1996-05-21
US5624081A (en) 1997-04-29
DE59302712D1 (en) 1996-06-27
CN1089569A (en) 1994-07-20
KR100197180B1 (en) 1999-06-15
KR960700190A (en) 1996-01-19
CN1031933C (en) 1996-06-05
EP0677019A1 (en) 1995-10-18

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