EP0810972B1 - Cross-winding device - Google Patents
Cross-winding device Download PDFInfo
- Publication number
- EP0810972B1 EP0810972B1 EP95942164A EP95942164A EP0810972B1 EP 0810972 B1 EP0810972 B1 EP 0810972B1 EP 95942164 A EP95942164 A EP 95942164A EP 95942164 A EP95942164 A EP 95942164A EP 0810972 B1 EP0810972 B1 EP 0810972B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- rotors
- housing
- guide
- rotation
- pct
- 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
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
- B65H54/00—Winding, coiling, or depositing filamentary material
- B65H54/02—Winding and traversing material on to reels, bobbins, tubes, or like package cores or formers
- B65H54/28—Traversing devices; Package-shaping arrangements
- B65H54/2836—Traversing devices; Package-shaping arrangements with a rotating guide for traversing the yarn
- B65H54/2839—Traversing devices; Package-shaping arrangements with a rotating guide for traversing the yarn counter rotating guides, e.g. wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
- B65H2701/00—Handled material; Storage means
- B65H2701/30—Handled filamentary material
- B65H2701/31—Textiles threads or artificial strands of filaments
Definitions
- the invention relates to a traversing device according to the preamble of Claim 1.
- wing traversing devices the alternating movement of the thread not by one and moving the thread guide, but by moving in opposite directions Alternately grasping and guiding the rotating wings with their tips.
- the thread-guiding wing tip sweeps over the ruler, so that the thread goes back and forth glides along the leading edge.
- the distance between the endpoints of the The leading edge therefore corresponds essentially to the traversing stroke. Near the End points intersect the turning circles of the wings of the leading edge.
- the Speed component with which the thread is transverse to its direction of travel on the one hand depends on the angular velocity with which the wings revolve, on the other hand by the radial distance between the axis of rotation and the point of the wing tip where the thread is currently resting.
- the leading edge becomes a radial with respect to the turning circles of the wings Movement component imposed. This allows the course of the The speed at which the thread moves along the traversing path be influenced, e.g. B. in the sense that the speed component in The direction of the traversing stroke is essentially constant all the way.
- the exact position of the ruler is therefore of the utmost importance for the Coil structure.
- a traversing device in which in one Housing a drivable hollow shaft of one rotor is mounted. Concentric or eccentrically to this, the shaft of the second rotor is mounted in the housing. This is achieved by a toothing in the inner circumference of the hollow shaft countershaft also supported in the housing.
- the shaft of the second rotor in a rotatable eccentric bush, as well as the countershaft.
- the twist of the two eccentric bushes has the side effect that the Connection line between the axes of rotation of the two rotors relative to the ruler is shifted.
- elongated holes are in the cover to which the housing is attached intended.
- DE-OS 38 26 130 describes a device in which the position of the ruler changed regularly during the coil travel at predetermined time intervals becomes. Depending on the type of change in position, this will result in at least one stroke end shifted. This is intended to suppress bead formation at the winding ends.
- the document contains no information on the structural features that the Enable or change the position of the ruler.
- the invention has for its object a device according to the Preamble of claim 1 to create, in which the ruler during Operation is manually adjustable.
- Figure 1 shows a side view of a winding device with a traversing device according to the invention, partially cut.
- FIG. 2 shows a top view of two traversing units lying next to one another a multi-digit winding machine, the left in the drawing Traversing unit schematically only the position of the rotors and the ruler without Representing housing and without gear.
- Figure 3 shows a front view
- Figures 4a and 4b show the adjusting bolt in the locked or released position.
- Figures 5a and 5c illustrate various settings of the ruler.
- Over the winding spindle 1 is one Traversing device 4 for a thread F, which is perpendicular from above via a Thread guide 5 is fed, also attached to the machine frame.
- a contact roller 6 is located between winding spindle 1 and traversing device 4 arranged, the axis of which is horizontal and parallel to the axis of the winding spindle 1 is aligned.
- the traversing device 4 includes two rotors 7, 8, which are in a housing 9 are rotatably mounted. Your axes of rotation are such. B. from DE-93 07 746 U known, arranged parallel to each other at short intervals. By means of a Drive, of which only one toothed disk 12 belonging to the rotor 7 in FIG It can be seen that the rotors 7, 8 are opposite each other at the same speed drivable.
- the blades 13 of the rotor 7 rotate in a lower plane of rotation 15, the blades 14 of the rotor 8 in an upper plane of rotation 16.
- the short distance between the two levels of rotation 15, 16 is d.
- the axes of the rotors 7, 8 are inclined, so that the two planes of rotation 15, 16 with the plane of the traversing triangle in Figure 1 enclose an acute angle.
- a ruler 17 is arranged between the two planes of rotation 15, 16. It has on the side which is remote from the axes of rotation of the rotors 7, 8, a leading edge 41, essentially in the form of a convex arc.
- the leading edge 41 extends over the traverse stroke H, which is essentially (i.e. apart from small, in particular due to the inclination of the chaging device, Deviations) is defined by the position of the points at which the turning circles the wing 13, 14 cut the leading edge 41.
- the perpendicular to the line connecting the two end points of the leading edge 41 are aligned.
- the ruler 17 is attached to side arms 42 which mirror-symmetrical to each other on the front wall of the housing 9 screwed and arranged at a distance above the upper rotary plane 16.
- the distance between the two arms 42 is only slightly larger than that Changierhub H.
- Each An 42 has one down at its free end directed block-shaped approach 43. This is close to its lower End face provided with a slot 44 parallel to this end face. By doing Slit 44 is the tab 33 with little lateral play. It is with a provided transverse slot 45.
- the approach 43 has a through bore 46.
- an adjusting bolt 47 In this is an adjusting bolt 47, its upper end face in the manner of a screw head with a slot 48 is provided. On the lower end face, an eccentric pin 49 is attached, which in the slot 45 engages.
- the adjusting bolt 47 has a circumferential, V-shaped in section Groove 50.
- the conical tip of a clamping screw 51 engages therein. Of the Cone angle corresponds to the angle between the side surfaces of the groove 50 and is about 90 °.
- the clamping screw 51 is seated in a threaded Bore which penetrates the end face of the extension 43.
- the clamping screw 51 is loosened, i. H. from the 4a position brought into the position shown in FIG. 4b. Your Tip no longer engages in the groove 50, so that the adjusting bolt 47 is now free is rotatable.
- the adjusting bolt e.g. B. in one of the figures 5a to 5c illustrated positions, the end of the ruler 17 in the Direction in which the tab 33 extends, in which the eccentricity of the Eccentric pin 49 move the specified frame.
- a corresponding Adjustment is also possible at the other end of the ruler 17.
- the ruler 17 can therefore not only shifted parallel to itself, but also in a small one Angular range can be pivoted.
- a particular advantage is that the adjusting bolts 47 with the Clamping screws 51 - as best seen in Fig. 2 - outside of Rotary circles of the wings lie and from the operating side - d. H. from that Machine frame opposite side of the traversing level - free during operation are accessible. The effect of the adjustment is directly on the thread run and on the Thread transfer visible. Therefore, an iterative optimization process is not required. It also proves advantageous that the ruler 17 very is easily interchangeable.
Landscapes
- Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Winding Filamentary Materials (AREA)
- Manufacture Of Motors, Generators (AREA)
- Polarising Elements (AREA)
- Mechanical Treatment Of Semiconductor (AREA)
- Processing Of Stones Or Stones Resemblance Materials (AREA)
- Massaging Devices (AREA)
- Valve Device For Special Equipments (AREA)
- Vehicle Body Suspensions (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Description
Die Erfindung betrifft eine Changiervorichtung gemäß dem Oberbegriff des
Anspruchs 1.The invention relates to a traversing device according to the preamble of
Anders als bei herkömmlichen Changiervorrichtungen wird bei Flügelchangiervorrichtungen die alternierende Bewegung des Fadens nicht durch einen einzigen hin und her bewegten Fadenführer bewirkt, sondern dadurch, daß gegensinning rotierende Flügel abwechelnd mit ihren Spitzen den Faden erfassen und führen. Die fadenführende Flügelspitze überstreicht das Lineal, so daß der Faden hin und her an der Leitkante entlang gleitet. Der Abstand zwischen den Endpunkten der Leitkante entspricht daher im wesentlichen dem Changierhub. In der Nähe der Endpunkte schneiden die Drehkreise der Flügel die Leitkante. Die Geschwindigkeitskomponente, mit der der Faden quer zu seiner Laufrichtung bewegt wird, hängt einerseits von der Winkelgeschwindigkeit ab, mit der die Flügel umlaufen, andererseits von dem radialen Abstand zwischen der Drehachse und dem Punkt der Flügelspitze, an dem der Faden momentan anliegt. Durch die Form der Leitkante wird dem Faden eine in bezug auf die Drehkreise der Flügel radiale Bewegungskomponente aufgezwungen. Dadurch kann der Verlauf der Geschwindigkeit, mit der sich der Faden längs des Changierweges bewegt, beeinflußt werden, z. B. in dem Sinn, daß die Geschwindigkeitkomponente in Richtung des Changierhubes auf dem ganzen Weg im wesentlichen konstant ist. Die exakte Lage des Lineals ist daher von größter Wichtigkeit für den Spulenaufbau.Unlike conventional traversing devices, wing traversing devices the alternating movement of the thread not by one and moving the thread guide, but by moving in opposite directions Alternately grasping and guiding the rotating wings with their tips. The thread-guiding wing tip sweeps over the ruler, so that the thread goes back and forth glides along the leading edge. The distance between the endpoints of the The leading edge therefore corresponds essentially to the traversing stroke. Near the End points intersect the turning circles of the wings of the leading edge. The Speed component with which the thread is transverse to its direction of travel on the one hand depends on the angular velocity with which the wings revolve, on the other hand by the radial distance between the axis of rotation and the point of the wing tip where the thread is currently resting. By the shape the leading edge becomes a radial with respect to the turning circles of the wings Movement component imposed. This allows the course of the The speed at which the thread moves along the traversing path be influenced, e.g. B. in the sense that the speed component in The direction of the traversing stroke is essentially constant all the way. The exact position of the ruler is therefore of the utmost importance for the Coil structure.
Aus DE-85 07 650 U ist eine Changiervorrichtung bekannt, bei der in einem Gehäuse eine antreibbare Hohlwelle des einen Rotors gelagert ist. Konzentrisch oder exzentrisch dazu ist die Welle des zweiten Rotors in dem Gehäuse gelagert.. Diese wird von einer Verzahnung im Innenumfang der Hohlwelle über eine ebenfalls in dem Gehäuse gelagerte Vorgelegewelle angetrieben. Um bei der Montage eine spielfreie Getriebeeinstellung zu ermöglichen, sitzt die Welle des zweiten Rotors in einer verdrehbaren Exzenterbuchse, ebenso die Vorgelegewelle. Die Verdrehung der beiden Exzenterbuchsen hat den Nebeneffekt, daß die Verbindungslinie zwischen den Drehachsen der beiden Rotoren relativ zum Lineal verlagert wird. Um diese unerwünschte Verlagerung zu kompensieren, ist das Gehäuse relativ zum Lineal um die Achse der Hohlwelle drehbar und feststellbar. Hierzu sind in dem Deckel, an dem das Gehäuse befestigt ist, Langlöcher vorgesehen.From DE-85 07 650 U a traversing device is known, in which in one Housing a drivable hollow shaft of one rotor is mounted. Concentric or eccentrically to this, the shaft of the second rotor is mounted in the housing. This is achieved by a toothing in the inner circumference of the hollow shaft countershaft also supported in the housing. To at the Assembly to allow a gear adjustment without play, the shaft of the second rotor in a rotatable eccentric bush, as well as the countershaft. The twist of the two eccentric bushes has the side effect that the Connection line between the axes of rotation of the two rotors relative to the ruler is shifted. To compensate for this unwanted shift, that is Housing rotatable and lockable relative to the ruler around the axis of the hollow shaft. For this purpose, elongated holes are in the cover to which the housing is attached intended.
Die DE-OS 38 26 130 beschreibt eine Vorrichtung, bei der die Lage des Lineals während der Spulenreise regelmäßig in vorbestimmten Zeitabständen verändert wird. Je nach Art der Lageänderung wird dadurch jeweils mindestens ein Hubende verlagert. Dadurch soll an den Wickelenden die Wulstbildung unterdrückt werden. Die Schrift enthält keine Angaben über die baulichen Merkmale, die die Lageänderung des Lineals ermöglichen oder bewirken.DE-OS 38 26 130 describes a device in which the position of the ruler changed regularly during the coil travel at predetermined time intervals becomes. Depending on the type of change in position, this will result in at least one stroke end shifted. This is intended to suppress bead formation at the winding ends. The document contains no information on the structural features that the Enable or change the position of the ruler.
Der Erfindung liegt die Aufgabe zugrunde, eine Vorrichtung gemäß dem
Oberbegriff des Anspruchs 1 zu schaffen, bei der das Lineal während des
Betriebes von Hand justierbar ist.The invention has for its object a device according to the
Preamble of
Diese Aufgabe wird durch die kennzeichnenden Merkmale des Anspruchs 1 gelöst.This object is achieved by the characterizing features of
Weitere vorteilhafte Merkmale der Erfindung sind Gegenstände der Ansprüche 2
bis 5.Further advantageous features of the invention are the subject matter of
Die Zeichnung dient zur Erläuterung der Erfindung anhand eines vereinfacht dargestellten Ausführungsbeispiels.The drawing serves to explain the invention with reference to a simplified illustrated embodiment.
Figur 1 zeigt eine Seitenansicht einer Aufspulvorrichtung mit einer erfindungsgemäßen Changiervorrichtung, teilweise geschnitten.Figure 1 shows a side view of a winding device with a traversing device according to the invention, partially cut.
Figur 2 zeigt eine Draufsicht auf zwei nebeneinander liegende Changiereinheiten einer mehrstelligen Aufspulmaschine, wobei die in der Zeichnung linke Changiereinheit schematisch nur die Lage der Rotoren und des Lineals ohne Gehäuse und ohne Getriebe darstellt. FIG. 2 shows a top view of two traversing units lying next to one another a multi-digit winding machine, the left in the drawing Traversing unit schematically only the position of the rotors and the ruler without Representing housing and without gear.
Figur 3 zeigt eine Frontansicht.Figure 3 shows a front view.
Die Figuren 4a und 4b zeigen den Stellbolzen in arretierter bzw. gelöster Stellung.Figures 4a and 4b show the adjusting bolt in the locked or released position.
Die Figuren 5a und 5c veranschaulichen verschiedene Einstellungen des Lineals.Figures 5a and 5c illustrate various settings of the ruler.
Eine Spulspindel 1, auf der eine Spulenhülse 2 einer gerade im Aufbau
befindlichen Spule 3 aufgespannt ist, ist in bekannter Weise mit einem in Fig. 1
nicht dargestellten Maschinengestellt verbunden. Über der Spulspindel 1 ist eine
Changiervorrichtung 4 für einen Faden F, der senkrecht von oben über einen
Fadenführer 5 zugeführt wird, ebenfalls an dem Maschinengestellt befestigt.
Zwischen Spulspindel 1 und Changiervorrichtung 4 ist eine Kontaktwalze 6
angeordnet, deren Achse waagerecht und parallel zur Achse der Spulspindel 1
ausgerichtet ist.A
Zu der Changiervorrichtung 4 gehören zwei Rotoren 7, 8, die in einem Gehäuse 9
drehbar gelagert sind. Ihre Drehachsen sind, wie z. B. aus DE-93 07 746 U
bekannt, parallel in kurzen Abständen zueinander angeordnet. Mittels eines
Antriebs, von dem in Figur nur eine zu dem Rotor 7 gehörenden Zahnscheibe 12
zu erkennen ist, sind die Rotoren 7, 8 gegensinning mit gleicher Drehzahl
antreibbar. Der Rotor 7 hat - wie in Figur 2 erkennbar - drei propellerartig
angeordnete Flügel 13, der Rotor 8 hat entsprechend angeordnete Flügel 14.
Gemäß Figur 2 hat jeder Flügel 13 an der Seite, die in Drehrichtung vome liegt, in
der Nähe seiner Spitze eine Fadenführungskante 13a, jeder Flügel 14 eine
Fadenführungskante 14a.The traversing
Die Flügel 13 des Rotors 7 laufen in einer unteren Drehebene 15 um, die Flügel 14
des Rotors 8 in einer oberen Drehebene 16. Der kurze Abstand zwischen den
beiden Drehebenen 15, 16 ist d. Die Achsen der Rotoren 7, 8 sind schräggestellt,
so daß die beiden Drehebenen 15, 16 mit der Ebene des Changierdreiecks in Figur
1 einen spitzen Winkel einschließen. The
Zwischen den beiden Drehebenen 15, 16 ist ein Lineal 17 angeordnet. Es hat auf
der Seite, die von den Drehachsen der Rotoren 7, 8 abgekehrt ist, eine Leitkante
41, im wesentlichen in Form eines konvexen Bogens. Die Leitkante 41 erstreckt
sich über den Changierhub H, der im wesentlichen (d. h. abgesehen von kleinen,
insbesondere durch die Schrägstellung der Chagiervorrichtung bedingten,
Abweichungen) durch die Lage der Punkte definiert ist, an denen die Drehkreise
der Flügel 13, 14 die Leitkante 41 schneiden. An den beiden Enden des Lineals 17
sind auf der von den Drehachsen angewandten Seite Laschen 33 angebracht, die
rechtwinklig zu der Linie, welche die beiden Endpunkte der Leitkante 41 verbindet,
ausgerichtet sind. Das Lineal 17 ist an seitlichen Armen 42 befestigt, die
spiegelsymmetrisch zueinander an der Vorderwand des Gehäuses 9
festgeschraubt und mit Abstand über der oberen Drehebene 16 angeordnet sind.
Der Abstand zwischen den beiden Armen 42 ist nur wenig größer als der
Changierhub H. Jeder An 42 hat an seinem freien Ende einen nach unten
gerichteteten blockförmigen Ansatz 43. Dieser ist in der Nähe seiner unteren
Endfläche mit einem zu dieser Endfläche parallelen Schlitz 44 versehen. In dem
Schlitz 44 liegt mit geringem seitlichen Spiel die Lasche 33. Sie ist mit einem
querliegenden Langloch 45 versehen.A
Der Ansatz 43 hat eine durchgehende Bohrung 46. Darin steckt ein Stellbolzen 47,
dessen obere Stirnfläche nach Art eines Schraubenkopfes mit einem Schlitz 48
versehen ist. An der unteren Stirnfläche ist ein Exzenterstift 49 angebracht, der in
das Langloch 45 eingreift. Der Stellbolzen 47 hat eine umlaufende, im Schnitt V-fömige
Nut 50. Darin greift die konische Spitze einer Klemmschraube 51 ein. Der
Konuswinkel entspricht dem Winkel zwischen den Seitenflächen der Nut 50 und
beträgt etwa 90°. Die Klemmschraube 51 sitzt in einer mit Gewinde versehenen
Bohrung, welche die Stirnfläche des Ansatzes 43 durchdringt.The
Um das Lineal 17 zu justieren, wird die Klemmschraube 51 gelockert, d. h. aus der
in Fig. 4a veranschaulichten Stellung in die Stellung gemäß Fig. 4b gebracht. Ihre
Spitze greift nun nicht mehr in die Nut 50 ein, so daß nun der Stellbolzen 47 frei
drehbar ist. Durch Verdrehen des Stellbolzens, z. B. in eine der in den Figuren 5a
bis 5c veranschaulichten Stellungen, läßt sich das Ende des Lineals 17 in der
Richtung, in der sich die Lasche 33 erstreckt, in dem durch die Exzentrizität des
Exzenterstiftes 49 vorgegebenen Rahmen verschieben. Eine entsprechende
Justierung ist auch am anderen Ende des Lineals 17 möglich. Das Lineal 17 kann
daher nicht nur parallel zu sich selbst verschoben, sondern auch in einem kleinen
Winkelbereich verschwenkt werden. Das seitliche Spiel, mit dem die Laschen 33 in
den Nuten 44 liegen, ist so bemessen, daß diese Verschwenkung nicht behindert
wird. Andererseits ist es aber so gering, daß keine merkliche Verschiebung in
Hubrichtung auftreten kann. Wenn die optimale Stellung des Lineals 17 erreicht
ist, werden auf beiden Seiten die Klemmschrauben 51 angezogen, so daß die
konischen Spitzen wieder in die Nuten 50 der Stellbolzen 47 eingreifen. Die
konische Form der Spitze bewirkt in Verbindung mit dem V-förmigen
Nutenquerschnitt, daß der Stellbolzen 47 mit seiner unteren Stirnfläche fest auf die
Lasche 33 gedrückt wird. Auf diese Weise ist die Einstellung arretiert.To adjust the
Ein besonderer Vorteil besteht darin, daß die Stellbolzen 47 mit den
Klemmschrauben 51 - wie am besten aus Fig. 2 ersichtlich - außerhalb der
Drehkreise der Flügel liegen und von der Bedienungsseite - d. h. von der dem
Maschinengestell gegenüberliegenden Seite der Changierebene - im Betrieb frei
zugänglich sind. Der Effekt der Justierung ist unmittelbar an Fadenlauf und an der
Fadenübergabe sichtbar. Daher ist ein iterativer Optimierungsprozeß nicht
erforderlich. Es erweist sich also auch als vorteilhaft, daß das Lineal 17 sehr
einfach austauschbar ist.A particular advantage is that the adjusting
Claims (5)
- A cross-winding device (4) with the following featurescharacterised by the following further features:a) two rotors (7, 8) are supported in a housing (9), the axles of which rotors are aligned parallel to each other and have at most a slight distance between themb) each rotor has at least two blades (13, 14) which are arranged in the manner of a propellerc) there is a short distance (d) between the planes of rotation (15, 16) of the two blade arrangementsd) the two rotors (7, 8) are actuable and coupled by a transmission in such a way, that one rotor (7) is rotatable in the opposite direction to the other rotor (8)e) a guide (17) is arranged in a parallel plane adjacent to both planes of rotation, which guide has a leading edge whose end points correspond substantially to the reversal points of the cross-winding motionf) the guide (17) is connected to the housing (9) by holding members and attachment means, which allow a relative displacement,g) the guide (17) is attached to holding members (42) so as to be adjustable, the holding members being connected rigidly to the housing (9)h) outside the turning circles of the blades (13, 14), adjustment means (47) for carrying out the adjustment are arranged so as to be freely accessible.
- A device according to claim 1, characterised by the following further features:i) the adjustment means is formed as a setting pin (47), which fits in a bore (46) of the holding member (42) so as to be rotatable and stoppablej) an eccentric pin (49) is attached on the end face of the setting pin (47)k) the eccentric pin (49) engages into an opening (45) of the guide (47).
- A device according to claim 2 with the following further features:l) the leading edge (41) is located on the side of the guide (17) facing away from the rotation axles of the rotors (7, 8)m) brackets (33) are arranged at the ends of the guide (17) on the side facing away from the rotation axles, which brackets are directed at right angles to the connecting line of the end points of the leading edge (41)n) the bracket (33) is provided with a transverse slot (45) for the eccentric pin (49).
- A device according to claim 2 or 3, characterised in that the setting pin (47) is secured against twisting by a clamping screw (51).
- A device according to claim 4, characterised in that the setting pin (47) has an encircling groove (50) with a v-shaped cross-section, and in that the clamping screw (51) engages in the groove (50) with a conical point.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE29503084U | 1995-02-24 | ||
| DE29503084U DE29503084U1 (en) | 1995-02-24 | 1995-02-24 | Traversing device |
| PCT/EP1995/004962 WO1996026149A1 (en) | 1995-02-24 | 1995-12-15 | Cross-winding device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP0810972A1 EP0810972A1 (en) | 1997-12-10 |
| EP0810972B1 true EP0810972B1 (en) | 1998-11-11 |
Family
ID=8004402
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP95942164A Expired - Lifetime EP0810972B1 (en) | 1995-02-24 | 1995-12-15 | Cross-winding device |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US5887817A (en) |
| EP (1) | EP0810972B1 (en) |
| JP (1) | JP2895242B2 (en) |
| CN (1) | CN1062237C (en) |
| AT (1) | ATE173231T1 (en) |
| DE (2) | DE29503084U1 (en) |
| WO (1) | WO1996026149A1 (en) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR19990072085A (en) * | 1996-10-12 | 1999-09-27 | 이.파우. 뢰르허 | Continuous winding machine |
| WO2001030677A1 (en) * | 1998-09-29 | 2001-05-03 | Murata Kikai Kabushiki Kaisha | Vane traverse device |
| DE102004003173A1 (en) * | 2004-01-22 | 2005-08-11 | Saurer Gmbh & Co. Kg | Fadenchangiereinrichtung for a winding device of a cheese-producing textile machine |
| JP2006335483A (en) * | 2005-05-31 | 2006-12-14 | Murata Mach Ltd | Yarn traverse device, and textile machine therewith |
| WO2015007339A1 (en) * | 2013-07-19 | 2015-01-22 | SSM Schärer Schweiter Mettler AG | Thread laying device and winding machine |
| DE102015005177A1 (en) | 2015-04-23 | 2016-10-27 | Oerlikon Textile Gmbh & Co. Kg | Device for adjusting a Flügelchangierung |
| CN115096149B (en) * | 2022-08-09 | 2024-04-19 | 重庆交通大学 | Automatic belt winding device for explosive package manufacturing |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1131884A (en) * | 1966-05-30 | 1968-10-30 | Chatillon Italiana Fibre | Device for winding yarn and thread |
| GB1269533A (en) * | 1968-04-29 | 1972-04-06 | Leesona Corp | Winding apparatus |
| US3595494A (en) * | 1969-05-23 | 1971-07-27 | Leesona Corp | Winding machine |
| US4505437A (en) * | 1983-01-29 | 1985-03-19 | Barmag Barmer Maschinenfabrik Ag | Apparatus for winding a plurality of yarns |
| EP0194648B1 (en) * | 1985-03-15 | 1989-06-28 | B a r m a g AG | Winding machine |
| DE8507650U1 (en) * | 1985-03-15 | 1986-07-10 | Barmag Barmer Maschinenfabrik Ag, 5630 Remscheid | Take-up machine |
| DE3614831A1 (en) * | 1985-05-10 | 1986-11-13 | Barmag Barmer Maschinenfabrik Ag, 5630 Remscheid | Winding machine |
| DE3703731A1 (en) * | 1986-02-25 | 1987-08-27 | Barmag Barmer Maschf | Winding machine with flier traverse |
| DE3826130A1 (en) * | 1987-08-05 | 1989-02-23 | Barmag Barmer Maschf | Method for stabilising the package end regions |
| DE3835873A1 (en) * | 1987-10-27 | 1989-05-11 | Barmag Barmer Maschf | Apparatus for the production of fancy yarn |
| US4991783A (en) * | 1987-12-30 | 1991-02-12 | Teijin Seiki Co., Ltd. | Yarn traversing method and an apparatus therefor |
| EP0612683B1 (en) * | 1992-08-19 | 1998-02-25 | Toray Engineering Co., Ltd. | Multi-thread take-up machine |
| DE9307746U1 (en) * | 1993-05-21 | 1993-08-05 | Neumag - Neumünstersche Maschinen- und Anlagenbau GmbH, 24536 Neumünster | Device for winding threads |
-
1995
- 1995-02-24 DE DE29503084U patent/DE29503084U1/en not_active Expired - Lifetime
- 1995-12-15 JP JP8525329A patent/JP2895242B2/en not_active Expired - Lifetime
- 1995-12-15 US US08/913,545 patent/US5887817A/en not_active Expired - Fee Related
- 1995-12-15 AT AT95942164T patent/ATE173231T1/en not_active IP Right Cessation
- 1995-12-15 EP EP95942164A patent/EP0810972B1/en not_active Expired - Lifetime
- 1995-12-15 WO PCT/EP1995/004962 patent/WO1996026149A1/en active IP Right Grant
- 1995-12-15 DE DE59504244T patent/DE59504244D1/en not_active Expired - Lifetime
- 1995-12-15 CN CN95197698A patent/CN1062237C/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| DE29503084U1 (en) | 1995-04-27 |
| EP0810972A1 (en) | 1997-12-10 |
| US5887817A (en) | 1999-03-30 |
| DE59504244D1 (en) | 1998-12-17 |
| CN1175238A (en) | 1998-03-04 |
| JPH10512224A (en) | 1998-11-24 |
| JP2895242B2 (en) | 1999-05-24 |
| WO1996026149A1 (en) | 1996-08-29 |
| CN1062237C (en) | 2001-02-21 |
| ATE173231T1 (en) | 1998-11-15 |
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