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EP2578730B1 - Thread creation element for a spinning position of an air jet spinning machine with a twist stop element - Google Patents

Thread creation element for a spinning position of an air jet spinning machine with a twist stop element Download PDF

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Publication number
EP2578730B1
EP2578730B1 EP12186910.1A EP12186910A EP2578730B1 EP 2578730 B1 EP2578730 B1 EP 2578730B1 EP 12186910 A EP12186910 A EP 12186910A EP 2578730 B1 EP2578730 B1 EP 2578730B1
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EP
European Patent Office
Prior art keywords
yarn
forming element
twist
previous
channel
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.)
Not-in-force
Application number
EP12186910.1A
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German (de)
French (fr)
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EP2578730A3 (en
EP2578730A2 (en
Inventor
Gerd Stahlecker
Gernot SCHÄFFLER
Markus Kübler
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Maschinenfabrik Rieter AG
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Maschinenfabrik Rieter AG
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Publication date
Application filed by Maschinenfabrik Rieter AG filed Critical Maschinenfabrik Rieter AG
Publication of EP2578730A2 publication Critical patent/EP2578730A2/en
Publication of EP2578730A3 publication Critical patent/EP2578730A3/en
Application granted granted Critical
Publication of EP2578730B1 publication Critical patent/EP2578730B1/en
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Classifications

    • DTEXTILES; PAPER
    • D01NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
    • D01HSPINNING OR TWISTING
    • D01H1/00Spinning or twisting machines in which the product is wound-up continuously
    • D01H1/11Spinning by false-twisting
    • D01H1/115Spinning by false-twisting using pneumatic means

Definitions

  • the present invention relates to a yarn-forming element for a spinning station of an air-spinning machine, wherein the yarn-forming element has an inlet opening on one end side as well as a discharge channel for a yarn beginning in the region of the inlet opening and extending along a longitudinal axis within the yarn formation element.
  • Yarn-forming elements are known from the prior art and are placed in the air-spinning machine in a so-called vortex chamber.
  • a vortex chamber Into the vortex chamber is introduced, usually with the help of a delivery roller pair, a stretched or evened fiber material via a yarn guide element and exposed to a tangential vortex air flow. Finally, this air flow causes the outer fiber ends of the fiber material in the region of the inlet opening of the yarn-forming element to wind around the non-twisted core fibers and permanently enclose them.
  • the yarn produced in this way is finally withdrawn via the discharge channel from the spinning station and wound, for example, on a spool.
  • the diameter of the inlet opening is usually chosen to be very small. That's what they call WO 2006/017 948 A1 For example, an inlet opening diameter of 0.8 mm to 1.2 mm.
  • the object of the invention is to avoid the mentioned disadvantages of the prior art.
  • the yarn-forming element has at least one swirl-stop element which at least partially narrows the cross-section of the take-off channel within the take-off channel.
  • an element or a profiling of the withdrawal channel bounding inner wall of the Garnsentelements is present, which protrudes into the discharge channel and thus provides a contact surface for the produced and withdrawn via the discharge duct yarn available.
  • the extraction channel thus does not have exclusively the known from the prior art form of a cylindrical or frusto-conical bore.
  • spin stop elements in the form of indentations, elevations, bulges, folds or other profilings, which cause the inner wall of the discharge channel has a shape that deviates from the shape of a cylinder or truncated cone.
  • the twist stop elements constitute an obstacle which counteracts false-wire formation, in particular of the core fibers. If these begin to rotate in the region of the inlet opening and with them the subsequent yarn, the yarn inevitably assumes a somewhat curved, ie deviating from a straight line, longitudinal extent. in this connection it comes in contact with the inner wall and thus also the spin stop element. Finally, the friction present between the yarn and the twist stop element effectively prevents the formation or continuation of the rotation and thus the formation of a false twisting wire. As a result, the yarn passes through the trigger channel without significant false rotation.
  • the inner wall of the exhaust duct in the region of the swirl stop element in a cross section running perpendicular to the longitudinal axis assumes a course which deviates from the course of a circle extending concentrically to the longitudinal axis.
  • the Garnticianselement has a plurality of spin stop elements, which are formed by elevations of the inner wall is particularly advantageous.
  • the elevations may be designed knob-shaped, wedge-shaped, rectilinear or curved and cause the inner wall has a surface structure that differs from a smooth wall.
  • the inner wall could also have a relatively large roughness (> RA 0.5), so that the inner wall has a plurality of roughness-causing elevations.
  • the spin stop element or elements can be arranged directly in the region of the withdrawal channel which adjoins the inlet opening.
  • a certain Distance between inlet opening and swirl stop element (s) wherein the distance, for example, an amount of 1 mm to 20 mm, preferably 1 mm to 10 mm, may have.
  • the swirl stop element is formed by a web which extends axially to the longitudinal axis of the discharge channel and extends in the radial direction with respect to the longitudinal axis in the discharge channel.
  • the individual teeth form the twist stop elements, which extend from an imaginary circular inner wall radially into the interior of the discharge channel.
  • the webs may have a flat or even a pointed or bevelled surface on their projecting into the interior of the discharge duct side.
  • the radial extent of the webs is also advantageously 0.1 mm to 2 mm.
  • the amount of said extension can also be selected as a function of the inlet opening diameter. For example, a radial extent, the amount of which corresponds to 1/10 to 1/3 of the inlet opening diameter would be advantageous.
  • the yarn-forming element has a plurality of twist-stop elements in the form of webs which are distributed uniformly over the inner wall in the circumferential direction of the inner wall. This creates a particularly effective rotation obstacle for the yarn produced, wherein the number of webs advantageously between 2 and 6.
  • the radial extension of the webs can in this case vary between the individual webs or be constant throughout.
  • the axial (with respect to the longitudinal axis of the discharge channel) expansion of the webs for example, between 1 mm and 30 mm, preferably between 10 mm and 20 mm.
  • the webs may generally have bevels at both ends or be stepped from the arranged between the web portions of the inner wall of the discharge channel.
  • the withdrawal channel has two sections which merge into one another into a transition region and have two inner diameter sections which deviate from one another, wherein the spin stop element is arranged in the transition region.
  • the yarn has only a small lateral support, since the contact with the inner wall is partially lost by the widening inner diameter of the discharge channel.
  • the twist stop elements may be arranged exclusively in the transition region or extending from this in or against the spinning direction in the axial direction of the discharge channel.
  • the discharge channel has two in a transition region merging into each other and two divergent inner diameter having portions, wherein the spin stop element, preferably exclusively, in the region of the portion with the larger inner diameter is arranged.
  • the spin stop element preferably exclusively, in the region of the portion with the larger inner diameter is arranged.
  • the spin stop element is used in the form of an insert in the yarn formation element.
  • the spin stop element may be made of a different material than the yarn formation element.
  • the production of an insert from a production point of view is easier than the formation of corresponding twist stop elements within the flue.
  • the insert may have a substantially cylindrical outer contour, so that it can be inserted into a corresponding bore of the Garn avoirselements and finally form a portion of the discharge channel.
  • the insert may have on its outer side bulges or indentations, which may cooperate with corresponding counterpart portions of the bore, thereby ensuring an anti-rotation of the insert relative to the Garn avoirselement.
  • the spin stop element is detachably connected to the yarn formation element.
  • the air spinning machine can be quickly adapted to the fiber material to be spun, in which the existing insert is exchanged for a matched to the new fiber material use when changing the fiber material.
  • the twist stop element can be screwed into a corresponding bore of the yarn formation element, clipped or otherwise connected positively or non-positively with this. If no detachable connection is necessary, it is also possible to glue the components mentioned.
  • spin stop elements are arranged in the longitudinal direction of the discharge channel, which are preferably spaced from each other by a spacer arranged therebetween.
  • a spacer arranged therebetween.
  • each spaced-apart spin stop elements are present in this case, wherein the individual spin stop elements and / or spacers in turn in the form of inserts may be present.
  • the respective swirl stop elements may be constructed, for example, in the manner of a sprocket, wherein the individual, preferably rounded teeth extend radially into the interior of the discharge channel.
  • the spacer is sleeve-shaped.
  • the spacer or spacers may, for example, have the shape of a hollow cylinder, so that they have a circular abutment surface for each adjacent swirl stop element.
  • the twist stop elements have a cylindrical outer contour, they can be inserted into a central bore of the Garn Strukturselements, wherein preferably a spacer is placed between each two twist stop elements.
  • the at least two twist stop elements delimit a passage opening for the yarn, which are arranged offset to one another with respect to the longitudinal axis in the radial direction.
  • the twist stop elements cause in this case a (with respect to the longitudinal axis) radial deflection of the yarn within the discharge channel and can be designed as mutually rotated arranged, having an identical shape inserts.
  • the passage openings themselves may in turn have a circular, oval, lenticular or even angular cross section.
  • the spin stop element and the yarn formation element are integrally formed.
  • the twist stop elements can be created, for example, characterized in that adjacent portions of the inner wall of the flue are subsequently removed.
  • the spin stop element has at least one rounded surface section. This avoids damage to the yarn, which should consciously come into contact with the twist stop element (s) in order to avoid the formation of a false twisting wire.
  • the yarn-forming element is designed as a spinning tip for a hollow spindle of an air-spinning machine consisting at least of spinning tip and spindle body.
  • the spinning tip in this case has a longitudinal extent of a few centimeters and is connected to the spindle body before the start of the air spinning machine.
  • Such a design allows a simple and quick replacement of the spinning tip, without having to replace the entire hollow spindle.
  • the yarn-forming element can also have a longer longitudinal extent and act as a hollow spindle of the air-spinning machine without connection to other components.
  • FIG. 1 shows a partially sectioned side view of a spinning station 14 of an air-spinning machine according to the prior art.
  • the spinning station 14 comprises a fiber guiding element 15, through which the fiber material 16 to be spun and usually present as a drawn sliver passes into the so-called swirl chamber 17 of the spinning station 14, in which finally the actual spinning process takes place.
  • the stretching takes usually a the fiber guide element 15 upstream drafting, from which the stretched sliver is withdrawn by means of a pair of withdrawal rollers.
  • the sliver is preferably detected by acting as a pair of delivery rollers 18 pair of rollers, which should be arranged as directly as possible subsequent to the fiber guide element 15 in order to avoid false warping.
  • the fiber material 16 After the fiber material 16 has passed the fiber guide element 15 via its guide channel 19, it passes into the effective range of several, usually tangentially into the swirl chamber 17 spinneret 20. If these are acted upon during the spinning operation via corresponding supply lines 21 with an overpressure, the result is a Vortex air flow, which flows around the upper region of Garn Strukturselements 1. If the outwardly protruding fiber ends are detected by this air flow, the result is finally the desired rotation of the outer fibers (binding fibers) around the untwisted core fibers and, as a result, the desired yarn 22, which finally passes through the inlet opening 2 and the adjoining exhaust duct 4 out of the Vortex chamber 17 can be deducted.
  • FIG. 2 it comes through the effect of the torque described to a yarn course, which has one or more bends with respect to the longitudinal axis 3.
  • the yarn 22 thus touches the inner wall 5 of the discharge channel 4 usually at several points and sweeps along the inner circumference, which eventually creates the unwanted false twisted wire.
  • the yarn-forming element 1 has at least one twist-stop element 6 arranged inside the withdrawal channel 4 and at least partially narrowing the cross-section of the withdrawal channel 4.
  • the operation of the or the twist stop elements 6 and possible embodiments can be the FIGS. 3 to 7 remove.
  • twist stop elements 6 in the example shown consist of a plurality of uniformly distributed over a region of the inner wall 5 of the discharge channel 4 elevations 7, the z. B. may be formed knob-shaped. It is also conceivable to achieve the aforementioned elevations 7 by choosing a sufficiently high roughness of the inner wall 5.
  • the twist stop element 6 comprises in shown four with respect to the longitudinal axis 3 of the discharge channel 4 radially inwardly projecting webs 8, wherein the number of webs 8 may vary.
  • the webs 8 are arranged uniformly distributed over the circumference of the discharge channel 4.
  • they are integrally formed with the Garn Strukturselement 1, whereby a separation into separate items would be possible.
  • the webs 8 now form the said obstacle to the migration of the yarn bends along the inner wall 5 during operation of the air-spinning machine, so that the formation of a false-twisting wire can be reliably prevented.
  • the webs 8 are arranged in the transition region 9 between the two sections of the discharge channel 4 having a different inner diameter.
  • the webs 8 extend from the transition region 9 in the axial direction of the discharge channel 4.
  • the length of the webs 8 is variable and can be several centimeters.
  • the webs 8 may be interrupted by gaps.
  • twist stop elements 6 shown here are distinguished by the fact that they have not been produced in one piece with the yarn formation element 1, but rather have been produced as a separate insert 10.
  • the inserts 10 can, for example, separated by the sleeve-shaped spacers 11, pushed from below into the central bore of Garn Strukturselements 1 and fixed accordingly.
  • FIG. 6 Spin stop elements 6 with web-shaped extensions shows the twist stop elements 6 according to FIG. 7 crescent-shaped and limit with the central bore of Garn Strukturselements 1 a lens-shaped through hole 12.
  • the twist stop elements 6 in FIG. 7 also have rounded surface portions 13 to prevent damage to the yarn 22 during the deflection.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Textile Engineering (AREA)
  • Spinning Or Twisting Of Yarns (AREA)
  • Yarns And Mechanical Finishing Of Yarns Or Ropes (AREA)
  • Spinning Methods And Devices For Manufacturing Artificial Fibers (AREA)

Description

Die vorliegende Erfindung betrifft ein Garnbildungselement für eine Spinnstelle einer Luftspinnmaschine, wobei das Garnbildungselement an einer Stirnseite eine Einlassöffnung sowie einen im Bereich der Einlassöffnung beginnenden und sich innerhalb des Garnbildungselements entlang einer Längsachse erstreckenden Abzugskanal für ein Garn aufweist.The present invention relates to a yarn-forming element for a spinning station of an air-spinning machine, wherein the yarn-forming element has an inlet opening on one end side as well as a discharge channel for a yarn beginning in the region of the inlet opening and extending along a longitudinal axis within the yarn formation element.

Gattungsgemäß Garnbildungselemente sind aus dem Stand der Technik bekannt und werden in der Luftspinnmaschine in einer so genannten Wirbelkammer platziert. In die Wirbelkammer wird, meist mit Hilfe eines Lieferwalzenpaars, eine verstrecktres bzw. vergleichmäßigtes Fasermaterial über ein Garnführungselement eingeführt und einer tangentialen Wirbelluftströmung ausgesetzt. Diese Luftströmung bewirkt schließlich, dass sich die äußeren Faserenden des Fasermaterials im Bereich der Einlassöffnung des Garnbildungselements um die nicht gedrehten Kernfasern winden und dieses dauerhaft umschließen. Das auf diese Weise erzeugte Garn wird schließlich über den Abzugskanal aus der Spinnstelle abgezogen und beispielsweise auf eine Spule aufgewickelt.Yarn-forming elements are known from the prior art and are placed in the air-spinning machine in a so-called vortex chamber. Into the vortex chamber is introduced, usually with the help of a delivery roller pair, a stretched or evened fiber material via a yarn guide element and exposed to a tangential vortex air flow. Finally, this air flow causes the outer fiber ends of the fiber material in the region of the inlet opening of the yarn-forming element to wind around the non-twisted core fibers and permanently enclose them. The yarn produced in this way is finally withdrawn via the discharge channel from the spinning station and wound, for example, on a spool.

Um eine Übertragung des von der Luftströmung auf die äußeren Fasern ausgeübten Drehmoments (der Lufteintrag erfolgt tangential zur Einlassöffnung) auf die ungedrehten Kernfasern möglichst zu vermeiden, wird der Durchmesser der Einlassöffnung meist sehr gering gewählt. So nennt die WO 2006/017 948 A1 beispielsweise einen Einlassöffnungsdurchmesser von 0,8 mm bis 1,2 mm.In order to avoid transmission of the torque exerted by the air flow on the outer fibers (the air is introduced tangentially to the inlet opening) as far as possible on the untwisted core fibers, the diameter of the inlet opening is usually chosen to be very small. That's what they call WO 2006/017 948 A1 For example, an inlet opening diameter of 0.8 mm to 1.2 mm.

DE-A-3714213 zeigt einen weiteren Stand der Technik. DE-A-3714213 shows another prior art.

Auch in diesem Fallzeiist jedoch eine - wenn auch geringe - Drehmomentübertragung von den Umwindefasern auf die Kernfasern nicht auszuschließen. Hierdurch kann es schließlich zu einer so genannten Falschdrahtbildung der Kernfasern und damit auch des gesamten Garns kommen. Da der Falschdraht jedoch drehmomentsbedingt die selbe Drehrichtung aufweist wie die Umwindefasern, kommt es beim Auflösen des Falschdrahts zu einer Rückdrehung der Fasern und damit zu einer gewissen Lockerung des Faserverbands bzw. einem Festigkeitsverlust des produzierten Garns.Even in this case, however, a - albeit small - torque transmission from the Umwindefasern on the core fibers can not be excluded. This can eventually lead to a so-called false-wire formation of the Core fibers and thus the entire yarn come. However, since the false-twisted wire has the same direction of rotation as the binder fibers due to the torque, a reverse rotation of the fibers occurs during the dissolution of the false-twisted wire and thus a certain loosening of the fiber dressing or a loss of strength of the produced yarn.

Aufgabe der Erfindung ist es, die genannten Nachteile des Stands der Technik zu vermeiden.The object of the invention is to avoid the mentioned disadvantages of the prior art.

Die Aufgabe wird gelöst durch ein Garnbildungselement mit den Merkmalen des Patentanspruchs 1.The object is achieved by a yarn formation element having the features of patent claim 1.

Erfindungsgemäß wird vorgeschlagen, dass das Garnbildungselement innerhalb des Abzugskanals wenigstens ein den Querschnitt des Abzugskanals zumindest partiell verengendes Drallstoppelement aufweist. Mit anderen Worten ist ein Element bzw. eine Profilierung der den Abzugskanal begrenzenden Innenwandung des Garnbildungselements vorhanden, das in den Abzugskanal ragt und damit eine Kontaktfläche für das produzierte und über den Abzugskanal abgezogene Garn zur Verfügung stellt. Der Abzugskanal weist somit nicht ausschließlich die aus dem Stand der Technik bekannte Form einer zylindrischen oder kegelstumpfförmigen Bohrung auf. Vielmehr besitzt er ein oder mehrere Drallstoppelemente in Form von Einbuchtungen, Erhebungen, Ausbuchtungen, Abkantungen oder sonstigen Profilierungen, die dazu führen, dass die Innenwandung des Abzugskanals eine Form aufweist, die von der Form eines Zylinders oder Kegelstumpfes abweicht.According to the invention, it is proposed that the yarn-forming element has at least one swirl-stop element which at least partially narrows the cross-section of the take-off channel within the take-off channel. In other words, an element or a profiling of the withdrawal channel bounding inner wall of the Garnbildelements is present, which protrudes into the discharge channel and thus provides a contact surface for the produced and withdrawn via the discharge duct yarn available. The extraction channel thus does not have exclusively the known from the prior art form of a cylindrical or frusto-conical bore. Rather, it has one or more spin stop elements in the form of indentations, elevations, bulges, folds or other profilings, which cause the inner wall of the discharge channel has a shape that deviates from the shape of a cylinder or truncated cone.

Die Drallstoppelemente stellen schließlich, anders als eine zylindrische oder kegelstumpfförmige Innenwandung, ein Hindernis dar, das einer Falschdrahtbildung insbesondere der Kernfasern entgegenwirkt. Beginnen sich diese nämlich im Bereich der Einlassöffnung und mit ihnen das nachfolgende Garn zu drehen, so nimmt das Garn zwangsläufig eine etwas gebogene, d. h. von einer geraden Linie abweichende, Längsausdehnung an. Hierbei kommt es mit der Innenwandung und damit auch dem Drallstoppelement in Kontakt. Die zwischen Garn und Drallstoppelement vorhandene Reibung verhindert schließlich effizient die Bildung bzw. Fortsetzung der Drehung und damit die Bildung eines Falschdrahts. Im Ergebnis durchläuft das Garn den Abzugskanal ohne signifikante Falschdrehung.Finally, unlike a cylindrical or frusto-conical inner wall, the twist stop elements constitute an obstacle which counteracts false-wire formation, in particular of the core fibers. If these begin to rotate in the region of the inlet opening and with them the subsequent yarn, the yarn inevitably assumes a somewhat curved, ie deviating from a straight line, longitudinal extent. in this connection it comes in contact with the inner wall and thus also the spin stop element. Finally, the friction present between the yarn and the twist stop element effectively prevents the formation or continuation of the rotation and thus the formation of a false twisting wire. As a result, the yarn passes through the trigger channel without significant false rotation.

In diesem Zusammenhang nimmt die Innenwandung des Abzugskanals im Bereich des Drallstoppelements in einem senkrecht zur Längsachse verlaufenden Querschnitt einen Verlauf ein, der vom Verlauf eines zur Längsachse konzentrisch verlaufenden Kreises abweicht. In jedem Fall weist der Abzugskanal im Bereich des oder der Drallstoppelemente eine Kontur auf, die von der Kontur einer zylindrischen oder kegelstumpfförmigen Bohrung abweicht. Dabei ist nicht ausgeschlossen, dass ein gewisser Umfangsabschnitt des Abzugskanals im Bereich der Drallstoppelemente einen kreisbogenförmigen Verlauf einnimmt. Dazwischen befinden sich jedoch eine oder mehrere Auskragungen, die ausgehend von einer gedachten Kreisform radial ins Innere des Abzugskanals ragen und damit ein Hindernis für die Ausbreitung eines Garnballons (sich bei der Falschdrahtbildung um eine Mittelachse des Abzugskanals bewegender und mit der Innenwandung in Kontakt kommender Abschnitt des Garns) darstellen.In this context, the inner wall of the exhaust duct in the region of the swirl stop element in a cross section running perpendicular to the longitudinal axis assumes a course which deviates from the course of a circle extending concentrically to the longitudinal axis. In any case, the discharge channel in the region of the or the swirl stop elements on a contour which differs from the contour of a cylindrical or frusto-conical bore. It is not excluded that a certain peripheral portion of the take-off channel in the area of the twist stop elements takes a circular arc course. In between, however, are one or more projections, which protrude from an imaginary circular shape radially into the interior of the flue and thus an obstacle to the propagation of a yarn balloon (in the false twisting around a central axis of the flue and moving to the inner wall in contact coming section of the Yarns).

Besonders vorteilhaft ist es, wenn das Garnbildungselement eine Vielzahl von Drallstoppelementen aufweist, die durch Erhebungen der Innenwandung gebildet werden. Die Erhebungen können dabei noppenförmig, keilförmig, geradlinig oder gebogen gestaltet sein und bewirken, dass die Innenwandung eine Oberflächenstruktur aufweist, die von einer glatten Wand abweicht. Beispielsweise könnte die Innenwandung auch eine verhältnismäßig große Rauhigkeit (> RA 0,5) aufweisen, so dass die Innenwandung eine Vielzahl von die Rauhigkeit bewirkenden Erhebungen aufweist. Generell sei an dieser Stelle zudem darauf hingewiesen, dass das oder die Drallstoppelemente unmittelbar in dem Bereich des Abzugskanals angeordnet sein können, der sich an die Einlassöffnung anschließt. Denkbar ist auch ein gewisser Abstand zwischen Einlassöffnung und Drallstoppelement(en), wobei der Abstand beispielsweise einen Betrag von 1 mm bis 20 mm, vorzugsweise 1 mm bis 10 mm, aufweisen kann.It when the Garnbildungselement has a plurality of spin stop elements, which are formed by elevations of the inner wall is particularly advantageous. The elevations may be designed knob-shaped, wedge-shaped, rectilinear or curved and cause the inner wall has a surface structure that differs from a smooth wall. For example, the inner wall could also have a relatively large roughness (> RA 0.5), so that the inner wall has a plurality of roughness-causing elevations. In general, it should also be pointed out at this point that the spin stop element or elements can be arranged directly in the region of the withdrawal channel which adjoins the inlet opening. Also conceivable is a certain Distance between inlet opening and swirl stop element (s), wherein the distance, for example, an amount of 1 mm to 20 mm, preferably 1 mm to 10 mm, may have.

Auch ist es äußert vorteilhaft, wenn das Drallstoppelement durch einen Steg gebildet wird, der axial zur Längsachse des Abzugskanals verläuft und sich in bezüglich der Längsachse radialer Richtung in den Abzugskanal erstreckt. In einem Querschnitt des Abzugskanals im Bereich des oder der Drallstauelemente entsteht auf diese Weise eine Art Zahnkranz mit nach innen gerichteten Zähnen, wobei die einzelnen Zähne die Drallstoppelemente bilden, die sich ausgehend von einer gedachten kreisförmigen Innenwandung radial ins Innere des Abzugskanals erstrecken. Die Ausbildung eines bei der Falschdrahtbildung vorzufindenden Garnballons und damit auch die Falschdrahtbildung selbst wird somit verhindert, da ein Schwingen bzw. Drehen des leicht gebogenen Garns um eine Mittelachse des Abzugskanals nicht mehr möglich ist. Die Stege können auf ihrer ins Innere des Abzugskanals ragenden Seite eine flächige oder aber auch eine spitze bzw. abgeschrägte Oberfläche aufweisen. Die radiale Erstreckung der Stege beträgt zudem vorteilhafterweise 0,1 mm bis 2 mm. Alternativ kann der Betrag der genannten Erstreckung auch in Abhängigkeit des Einlassöffnungsdurchmessers gewählt werden. Beispielsweise wäre eine radiale Erstreckung von Vorteil, deren Betrag 1/10 bis 1/3 des Einlassöffnungsdurchmessers entspricht.Also, it is extremely advantageous if the swirl stop element is formed by a web which extends axially to the longitudinal axis of the discharge channel and extends in the radial direction with respect to the longitudinal axis in the discharge channel. In a cross-section of the discharge channel in the region of the swirl or the baffles created in this way a kind of sprocket with inwardly directed teeth, the individual teeth form the twist stop elements, which extend from an imaginary circular inner wall radially into the interior of the discharge channel. The formation of a yarn balloon to be found in the false-twist formation, and thus also false-twisting itself, is thus prevented since it is no longer possible to swing or slightly turn the slightly curved yarn about a central axis of the discharge channel. The webs may have a flat or even a pointed or bevelled surface on their projecting into the interior of the discharge duct side. The radial extent of the webs is also advantageously 0.1 mm to 2 mm. Alternatively, the amount of said extension can also be selected as a function of the inlet opening diameter. For example, a radial extent, the amount of which corresponds to 1/10 to 1/3 of the inlet opening diameter would be advantageous.

Des Weiteren ist es vorteilhaft, wenn das Garnbildungselement mehrere Drallstoppelemente in Form von Stegen aufweist, die in Umfangsrichtung der Innenwandung gleichmäßig über die Innenwandung verteilt angeordnet sind. Hierdurch entsteht ein besonders wirksames Dreh-Hindernis für das produzierte Garn, wobei die Anzahl der Stege vorteilhafterweise zwischen 2 und 6 liegt. Die radiale Erstreckung der Stege kann hierbei zwischen den einzelnen Stegen schwanken oder aber durchgehend konstant sein. Die axiale (bezüglich der Längsachse des Abzugskanals) Ausdehnung der Stege beträgt beispielsweise zwischen 1 mm und 30 mm, vorzugsweise zwischen 10 mm und 20 mm. Ferner können die Stege generell an ihren beiden Enden Schrägen aufweisen oder sich stufenförmig von den zwischen den Stegen angeordneten Abschnitten der Innenwandung des Abzugskanals abheben.Furthermore, it is advantageous if the yarn-forming element has a plurality of twist-stop elements in the form of webs which are distributed uniformly over the inner wall in the circumferential direction of the inner wall. This creates a particularly effective rotation obstacle for the yarn produced, wherein the number of webs advantageously between 2 and 6. The radial extension of the webs can in this case vary between the individual webs or be constant throughout. The axial (with respect to the longitudinal axis of the discharge channel) expansion of the webs, for example, between 1 mm and 30 mm, preferably between 10 mm and 20 mm. Furthermore, the webs may generally have bevels at both ends or be stepped from the arranged between the web portions of the inner wall of the discharge channel.

Besondere Vorteile bringt es mit sich, wenn der Abzugskanal zwei in einen Übergangsbereich ineinander übergehende und zwei voneinander abweichende Innendurchmesser aufweisende Abschnitte aufweist, wobei das Drallstoppelement im Übergangsbereich angeordnet ist. Besonders in dem genannten Bereich hat das Garn nur einen geringen Seitenhalt, da der Kontakt mit der Innenwandung durch den sich erweiternden Innendurchmesser des Abzugskanals teilweise verloren geht. Wird nun ein Drehmoment auf das Garn ausgeübt, so kann es zu einer Falschdrahtbildung kommen, der jedoch erfindungemäß durch die Anordnung eines oder mehrerer Drallstoppelemente entgegengewirkt werden kann. Die Drallstoppelemente können ausschließlich im Übergangsbereich angeordnet sein oder sich ausgehend von diesem in oder entgegen der Spinnrichtung in axialer Richtung des Abzugskanals erstrecken.It has particular advantages when the withdrawal channel has two sections which merge into one another into a transition region and have two inner diameter sections which deviate from one another, wherein the spin stop element is arranged in the transition region. Especially in the above range, the yarn has only a small lateral support, since the contact with the inner wall is partially lost by the widening inner diameter of the discharge channel. Now, if a torque is exerted on the yarn, it can lead to false-wire formation, which, however, can be counteracted erfindungemäß by the arrangement of one or more twist stop elements. The twist stop elements may be arranged exclusively in the transition region or extending from this in or against the spinning direction in the axial direction of the discharge channel.

Ebenso bringt es Vorteile mit sich, wenn der Abzugskanal zwei in einen Übergangsbereich ineinander übergehende und zwei voneinander abweichende Innendurchmesser aufweisende Abschnitte aufweist, wobei das Drallstoppelement, vorzugsweise ausschließlich, im Bereich des Abschnitts mit dem größeren Innendurchmesser angeordnet ist. Wie oben bereits erwähnt, besteht besonders im Bereich mit dem größeren Innendurchmesser die Gefahr, dass das Garn einen leicht gebogenen Verlauf annimmt und durch Einwirkung eines von den Umwindefasern übertragenen Drehmoments in einer Kreisbahn zu schwingen beginnt (d. h. das Garn beschreibt die Außenkontur eines Ballons). Werden nun das oder die Drallstoppelemente speziell in diesem Bereich angeordnet, so wird ein Hindernis zur Verfügung gestellt, an dem das Garn beim Versuch, den genannten Ballon auszubilden, anstößt. Eine Drehung und damit die Bildung des unerwünschten Falschdrahts wird dadurch verhindert.Likewise, it brings advantages when the discharge channel has two in a transition region merging into each other and two divergent inner diameter having portions, wherein the spin stop element, preferably exclusively, in the region of the portion with the larger inner diameter is arranged. As already mentioned above, especially in the region with the larger inner diameter there is a risk that the yarn will take on a slightly curved course and begin to oscillate in a circular path by the action of a torque transmitted by the binder fibers (ie the yarn describes the outer contour of a balloon). Now, if the spin stop element (s) is specifically arranged in this area, an obstacle is provided at which the yarn abuts when trying to form said balloon. A rotation and thus the formation of the unwanted false wire is prevented.

Auch ist es äußert vorteilhaft, wenn das Drallstoppelement in Form eines Einsatzes in das Garnbildungselement eingesetzt ist. In diesem Fall kann das Drallstoppelement aus einem anderen Material bestehen als das Garnbildungselement. Zudem ist die Fertigung eines Einsatzes aus fertigungstechnischer Sicht einfacher als die Formung entsprechender Drallstoppelemente innerhalb des Abzugskanals. Der Einsatz kann eine im Wesentlichen zylindrische Außenkontur aufweisen, so dass er in eine entsprechende Bohrung des Garnbildungselements eingesetzt und schließlich einen Bereich des Abzugskanals bilden kann. Ferner kann der Einsatz auf seiner Außenseite Auswölbungen oder Einbuchtungen aufweisen, die mit entsprechenden Gegenabschnitten der Bohrung zusammenwirken können, um hierdurch eine Verdrehsicherung des Einsatzes gegenüber dem Garnbildungselement zu gewährleisten.It is also extremely advantageous if the spin stop element is used in the form of an insert in the yarn formation element. In this case, the spin stop element may be made of a different material than the yarn formation element. In addition, the production of an insert from a production point of view is easier than the formation of corresponding twist stop elements within the flue. The insert may have a substantially cylindrical outer contour, so that it can be inserted into a corresponding bore of the Garnbildungselements and finally form a portion of the discharge channel. Further, the insert may have on its outer side bulges or indentations, which may cooperate with corresponding counterpart portions of the bore, thereby ensuring an anti-rotation of the insert relative to the Garnbildungselement.

Ebenso ist es vorteilhaft, wenn das Drallstoppelement lösbar mit dem Garnbildungselement verbunden ist. Hierdurch ist ein einfacher Austausch desselben, beispielsweise nach einem Verschleiß, möglich. Ebenso kann die Luftspinnmaschine schnell auf das zu verspinnende Fasermaterial angepasst werden, in dem beim Wechsel des Fasermaterials auch der vorhandene Einsatz gegen einen auf das neue Fasermaterial abgestimmten Einsatz ausgetauscht wird. Das Drallstoppelement kann in eine entsprechende Bohrung des Garnbildungselements eingeschraubt, eingeklipst oder auf andere Weise kraft- oder formschlüssig mit diesem verbunden sein. Ist keine lösbare Verbindung nötig, so ist auch ein Verkleben der genannten Bauteile möglich.It is likewise advantageous if the spin stop element is detachably connected to the yarn formation element. As a result, a simple exchange of the same, for example, after a wear, possible. Likewise, the air spinning machine can be quickly adapted to the fiber material to be spun, in which the existing insert is exchanged for a matched to the new fiber material use when changing the fiber material. The twist stop element can be screwed into a corresponding bore of the yarn formation element, clipped or otherwise connected positively or non-positively with this. If no detachable connection is necessary, it is also possible to glue the components mentioned.

Auch ist es von Vorteil, wenn in Längsrichtung des Abzugskanals wenigstens zwei Drallstoppelemente angeordnet sind, die vorzugsweise durch einen dazwischen angeordneten Abstandshalter voneinander beabstandet sind. Innerhalb des Abstandskanals sind in diesem Fall mehrere, jeweils voneinander beabstandete Drallstoppelemente vorhanden, wobei die einzelnen Drallstoppelemente und/oder Abstandshalter wiederum in Form von Einsätzen vorliegen können. Die jeweiligen Drallstoppelemente können beispielsweise nach Art eines Zahnkranzes aufgebaut sein, wobei sich die einzelnen, vorzugsweise abgerundeten Zähne radial ins Innere des Abzugskanals erstrecken.It is also advantageous if at least two spin stop elements are arranged in the longitudinal direction of the discharge channel, which are preferably spaced from each other by a spacer arranged therebetween. Within the distance channel a plurality of, each spaced-apart spin stop elements are present in this case, wherein the individual spin stop elements and / or spacers in turn in the form of inserts may be present. The respective swirl stop elements may be constructed, for example, in the manner of a sprocket, wherein the individual, preferably rounded teeth extend radially into the interior of the discharge channel.

Des Weiteren ist es vorteilhaft, wenn der Abstandhalter hülsenförmig ausgebildet ist. Der oder die Abstandhalter können beispielsweise die Form eines Hohlzylinders aufweisen, so dass sie eine kreisrunde Anlagefläche für jeweils ein benachbartes Drallstoppelement besitzen. Wenn auch die Drallstoppelemente eine zylindrische Außenkontur aufweisen, so können diese in eine mittige Bohrung des Garnbildungselements eingeschoben werden, wobei vorzugsweise zwischen jeweils zwei Drallstoppelementen ein Abstandshalter platziert wird.Furthermore, it is advantageous if the spacer is sleeve-shaped. The spacer or spacers may, for example, have the shape of a hollow cylinder, so that they have a circular abutment surface for each adjacent swirl stop element. Although the twist stop elements have a cylindrical outer contour, they can be inserted into a central bore of the Garnbildungselements, wherein preferably a spacer is placed between each two twist stop elements.

Vorteile bringt es zudem mit sich, wenn die wenigstens zwei Drallstoppelemente eine Durchgangsöffnung für das Garn begrenzen, die bezüglich der Längsachse in radialer Richtung zueinander versetzt angeordnet sind. Die Drallstoppelemente bewirken in diesem Fall eine (bezüglich der Längsachse) radiale Umlenkung des Garns innerhalb des Abzugskanals und können als zueinander verdreht angeordnete, eine identische Form aufweisende Einsätze ausgebildet sein. Die Durchgangsöffnungen selbst können wiederum einen kreisrunden, ovalen, linsenförmigen oder auch kantigen Querschnitt aufweisen.It also brings advantages when the at least two twist stop elements delimit a passage opening for the yarn, which are arranged offset to one another with respect to the longitudinal axis in the radial direction. The twist stop elements cause in this case a (with respect to the longitudinal axis) radial deflection of the yarn within the discharge channel and can be designed as mutually rotated arranged, having an identical shape inserts. The passage openings themselves may in turn have a circular, oval, lenticular or even angular cross section.

Des Weiteren ist es vorteilhaft, wenn das Drallstoppelement und das Garnbildungselement einteilig ausgebildet sind. In diesem Fall kann auf eine nachträgliche Verbindung der jeweiligen Einzelteile verzichtet werden, wobei die Drallstoppelemente beispielsweise dadurch erstellt werden können, dass benachbarte Abschnitte der Innenwandung des Abzugskanals nachträglich entfernt werden.Furthermore, it is advantageous if the spin stop element and the yarn formation element are integrally formed. In this case, can be dispensed with a subsequent connection of the respective items, wherein the twist stop elements can be created, for example, characterized in that adjacent portions of the inner wall of the flue are subsequently removed.

Besondere Vorteile bringt es mit sich, wenn das Drallstoppelement zumindest einen abgerundeten Oberflächenabschnitt aufweist. Hierdurch lässt sich eine Beschädigung des Garns vermeiden, welches bewusst mit dem oder den Drallstoppelement(en) in Berührung kommen soll, um die Ausbildung eines Falschdrahts zu vermeiden.Particular advantages arise when the spin stop element has at least one rounded surface section. This avoids damage to the yarn, which should consciously come into contact with the twist stop element (s) in order to avoid the formation of a false twisting wire.

Vorteile bringt es zudem mit sich, wenn das Garnbildungselement als Spinnspitze für eine zumindest aus Spinnspitze und Spindelkörper bestehende Hohlspindel einer Luftspinnmaschine ausgebildet ist. Die Spinnspitze hat in diesem Fall eine Längserstreckung von wenigen Zentimetern und wird vor der Inbetriebnahme der Luftspinnmaschine mit dem Spindelkörper verbunden. Eine derartige Konstruktion erlaubt einen einfachen und schnellen Austausch der Spinnspitze, ohne die gesamte Hohlspindel austauschen zu müssen. Alternativ kann das Garnbildungselement jedoch auch eine längere Längsausdehnung aufweisen und ohne Verbindung mit weiteren Bauteilen als Hohlspindel der Luftspinnmaschine fungieren.It also brings advantages when the yarn-forming element is designed as a spinning tip for a hollow spindle of an air-spinning machine consisting at least of spinning tip and spindle body. The spinning tip in this case has a longitudinal extent of a few centimeters and is connected to the spindle body before the start of the air spinning machine. Such a design allows a simple and quick replacement of the spinning tip, without having to replace the entire hollow spindle. Alternatively, however, the yarn-forming element can also have a longer longitudinal extent and act as a hollow spindle of the air-spinning machine without connection to other components.

Die vorstehend erläuterten und/oder in den Unteransprüchen wiedergegebenen vorteilhaften Aus- und Weiterbildungen der Erfindung können dabei - außer z. B. in den Fällen eindeutiger Abhängigkeiten oder unvereinbarer Alternativen - einzeln oder aber auch in beliebiger Kombination miteinander zur Anwendung kommen.The above-explained and / or reproduced in the subclaims advantageous embodiments and refinements of the invention can - in addition to z. B. in cases of clear dependencies or incompatible alternatives - individually or in any combination with each other.

Weitere Vorteile der Erfindung sind in den nachfolgenden Ausführungsbeispielen beschrieben. Es zeigt:

Figur 1
eine teilweise geschnittene Seitenansicht einer Spinnstelle gemäß dem Stand der Technik während des Spinnprozesses,
Figur 2
einen Längsschnitt einer Spitze eines bekannten Garnbildungselements,
Figur 3
einen Längsschnitt einer Spitze eines erfindungsgemäßen Garnbildungselements,
Figur 4
einen Längsschnitt sowie einen Querschnitt entlang der Linie A-A' der Spitze eines erfindungsgemäßen Garnbildungselements,
Figur 5
einen Längsschnitt sowie einen Querschnitt entlang der Linie B-B' der Spitze eines weiteren erfindungsgemäßen Garnbildungselements,
Figur 6
einen Längsschnitt sowie einen Querschnitt entlang der Linie C-C' der Spitze eines weiteren erfindungsgemäßen Garnbildungselements,
Figur 7
einen Längsschnitt sowie einen Querschnitt entlang der Linie D-D' der Spitze eines weiteren erfindungsgemäßen Garnbildungselements,
Further advantages of the invention are described in the following exemplary embodiments. It shows:
FIG. 1
a partially sectioned side view of a spinning station according to the prior art during the spinning process,
FIG. 2
a longitudinal section of a tip of a known Garnbildungselements,
FIG. 3
a longitudinal section of a tip of a yarn formation element according to the invention,
FIG. 4
a longitudinal section and a cross section along the line AA 'of the tip of a yarn formation element according to the invention,
FIG. 5
a longitudinal section and a cross section along the line BB 'of the tip of another yarn formation element according to the invention,
FIG. 6
a longitudinal section and a cross section along the line CC 'of the tip of another yarn formation element according to the invention,
FIG. 7
a longitudinal section and a cross section along the line DD 'of the tip of another yarn formation element according to the invention,

Figur 1 zeigt eine teilweise geschnittene Seitenansicht einer Spinnstelle 14 einer Luftspinnmaschine gemäß dem Stand der Technik. Die Spinnstelle 14 umfasst ein Faserführungselement 15, durch welches das zu verspinnende und meist als verstrecktes Faserband vorliegende Fasermaterial 16 in die so genannte Wirbelkammer 17 der Spinnstelle 14 gelangt, in der schließlich der eigentliche Spinnprozess stattfindet. Die Verstreckung übernimmt in der Regel ein dem Faserführungselement 15 vorgeschaltetes Streckwerk, aus dem das verstreckte Faserband mit Hilfe eines Abzugswalzenpaars abgezogen wird. Anschließend wird das Faserband vorzugsweise von einem als Lieferwalzenpaar 18 wirkenden Walzenpaar erfasst, welches möglichst unmittelbar im Anschluss an das Faserführungselement 15 angeordnet sein sollte, um Fehlverzüge zu vermeiden. FIG. 1 shows a partially sectioned side view of a spinning station 14 of an air-spinning machine according to the prior art. The spinning station 14 comprises a fiber guiding element 15, through which the fiber material 16 to be spun and usually present as a drawn sliver passes into the so-called swirl chamber 17 of the spinning station 14, in which finally the actual spinning process takes place. The stretching takes usually a the fiber guide element 15 upstream drafting, from which the stretched sliver is withdrawn by means of a pair of withdrawal rollers. Subsequently, the sliver is preferably detected by acting as a pair of delivery rollers 18 pair of rollers, which should be arranged as directly as possible subsequent to the fiber guide element 15 in order to avoid false warping.

Nachdem das Fasermaterial 16 das Faserführungselement 15 über dessen Führungskanal 19 passiert hat, gelangt es in den Wirkbereich mehrerer, in der Regel tangential in die Wirbelkammer 17 mündender Spinndüsen 20. Werden diese während des Spinnbetriebs über entsprechende Versorgungsleitungen 21 mit einem Überdruck beaufschlagt, so entsteht eine Wirbelluftströmung, die den oberen Bereich des Garnbildungselements 1 umströmt. Werden die nach außen abstehenden Faserenden von dieser Luftströmung erfasst, so entsteht schließlich die gewünschte Drehung der außen liegenden Fasern (Umwindefasern) um die ungedrehten Kernfasern und im Ergebnis das gewünschte Garn 22, welches schließlich über die Einlassöffnung 2 und den daran anschließenden Abzugskanal 4 aus der Wirbelkammer 17 abgezogen werden kann.After the fiber material 16 has passed the fiber guide element 15 via its guide channel 19, it passes into the effective range of several, usually tangentially into the swirl chamber 17 spinneret 20. If these are acted upon during the spinning operation via corresponding supply lines 21 with an overpressure, the result is a Vortex air flow, which flows around the upper region of Garnbildungselements 1. If the outwardly protruding fiber ends are detected by this air flow, the result is finally the desired rotation of the outer fibers (binding fibers) around the untwisted core fibers and, as a result, the desired yarn 22, which finally passes through the inlet opening 2 and the adjoining exhaust duct 4 out of the Vortex chamber 17 can be deducted.

Durch die durch die Spinndüsen 20 induzierte Luftströmung wirkt auf die außen liegenden, so genannten Umwindefasern ein Drehmoment, das schließlich für die Garnbildung verantwortlich ist. Gleichzeitig wird dieses Drehmoment jedoch auch auf die innenliegenden Kernfasern übertragen, die prinzipiell ungedreht bleiben sollen. Dieses Drehmoment kann im ungünstigen Fall dazu führen, dass auch die Kernfasern in Rotation versetzt werden, so dass sich auch das im Abzugskanal 4 befindliche Garn 22 zu drehen beginnt. Diese Drehung kann sich jedoch nicht unbegrenzt fortpflanzen, da im Anschluss an den Abzugskanal 4 ein Abzugsorgen (z. B. in Form eines Abzugswalzenpaars) angeordnet ist, welches das Garn 22 klemmend fördert. Im Ergebnis entsteht im Bereich nach der Einlassöffnung 2 ein so genannter Falschdraht, d. h. eine Drehung des Garns 22, die sich im Laufe seines Weitertransports wieder auflöst. Hierdurch kommt es jedoch letztendlich zu einer Lockerung der Umwindefasern und zu einer Verschlechterung der Garnfestigkeit.As a result of the air flow induced by the spinnerets 20, a torque which is ultimately responsible for the yarn formation acts on the outer, so-called binding fibers. At the same time, however, this torque is also transmitted to the inner core fibers, which in principle should remain untwisted. In the worst case, this torque can lead to the core fibers also being set in rotation, so that the yarn 22 located in the draw-off channel 4 also begins to rotate. However, this rotation can not propagate indefinitely, since a withdrawal gate (eg in the form of a pair of withdrawal rollers) is arranged following the withdrawal channel 4, which conveys the yarn 22 in a clamping manner. As a result, in the area after the inlet opening 2, a so-called false-twisted wire is created, ie. H. a rotation of the yarn 22, which dissolves again in the course of its further transport. However, this ultimately leads to a loosening of the Umwindefasern and to a deterioration of the yarn strength.

Wie Figur 2 zu entnehmen ist, kommt es durch die Wirkung des beschriebenen Drehmoments zu einem Garnverlauf, der gegenüber der Längsachse 3 eine oder mehrere Biegungen aufweist. Das Garn 22 berührt also die Innenwandung 5 des Abzugskanals 4 an meist mehreren Stellen und streicht an dessen Innenumfang entlang, wobei schließlich der nicht gewünschte Falschdraht entsteht.As FIG. 2 can be seen, it comes through the effect of the torque described to a yarn course, which has one or more bends with respect to the longitudinal axis 3. The yarn 22 thus touches the inner wall 5 of the discharge channel 4 usually at several points and sweeps along the inner circumference, which eventually creates the unwanted false twisted wire.

Um die Bildung des genannten Falschdrahts zu vermeiden, wird nun erfindungsgemäß vorgeschlagen, dass das Garnbildungselement 1 wenigstens ein innerhalb des Abzugskanals 4 angeordnetes und den Querschnitt des Abzugskanals 4 zumindest partiell verengendes Drallstoppelement 6 aufweist. Die Funktionsweise des oder der Drallstoppelemente 6 sowie mögliche Ausführungsformen lassen sich den Figuren 3 bis 7 entnehmen.In order to avoid the formation of said false-twist wire, it is now proposed according to the invention that the yarn-forming element 1 has at least one twist-stop element 6 arranged inside the withdrawal channel 4 and at least partially narrowing the cross-section of the withdrawal channel 4. The operation of the or the twist stop elements 6 and possible embodiments can be the FIGS. 3 to 7 remove.

Eine beispielhafte Gestaltung erfindungsgemäßer Drallstoppelemente 6 zeigt Figur 3. Die Drallstoppelemente 6 bestehen im gezeigten Beispiel aus einer Vielzahl von über einen Bereich der Innenwandung 5 des Abzugskanals 4 gleichmäßig verteilter Erhebungen 7, die z. B. noppenförmig ausgebildet sein können. Denkbar ist ebenso, die genannten Erhebungen 7 durch die Wahl einer ausreichend hohen Rauhigkeit der Innenwandung 5 zu erzielen.An exemplary design of twist stop elements 6 according to the invention FIG. 3 , The twist stop elements 6 in the example shown consist of a plurality of uniformly distributed over a region of the inner wall 5 of the discharge channel 4 elevations 7, the z. B. may be formed knob-shaped. It is also conceivable to achieve the aforementioned elevations 7 by choosing a sufficiently high roughness of the inner wall 5.

Wird nun ein Drehmoment auf die Kernfasern übertragen, so bilden sich die in Figur 2 gezeigten Biegungen des Garns 22, d. h. das Garn 22 kommt im Bereich der Einlassöffnung 2 mit den Drallstoppelementen 6 in Form der Erhebungen 7 in Kontakt. Da die Erhebungen 7 einer Bewegung des Garns 22 in Umfangsrichtung der Innenwandung 5 entgegenwirken (schließlich stellen die Erhebungen 7 ein Hindernis dar, das vom Garn 22 ständig überstrichen werden müsste), ist auch die Ausbildung eines Falschdrahts behindert. Die Drallstoppelemente 6 erzeugen somit eine Anlagefläche, über die das auf die Kernfasern übertragene Drehmoment aufgefangen werden kann. Eine Falschdrahterzeugung wird verhindert, das Garn 22 besitzt eine gegenüber dem Stand der Technik verbesserte Festigkeit.Now, if a torque is transferred to the core fibers, then the form in FIG. 2 shown bends of the yarn 22, ie the yarn 22 comes in the region of the inlet opening 2 with the twist stop elements 6 in the form of the elevations 7 in contact. Since the elevations 7 counteract a movement of the yarn 22 in the circumferential direction of the inner wall 5 (finally, the elevations 7 are an obstacle that would have to be constantly swept over by the yarn 22), the formation of a false twisting wire is also hindered. The twist stop elements 6 thus generate a contact surface over which the torque transmitted to the core fibers can be absorbed. False-wire production is prevented, the yarn 22 has improved strength over the prior art.

Eine weitere Möglichkeit, das erfindungsgemäße Drallstoppelement 6 konstruktiv zu verwirklichen, zeigt Figur 4. Das Drallstoppelement 6 umfasst im gezeigten Beispiel vier bezüglich der Längsachse 3 des Abzugskanals 4 radial nach innen ragende Stege 8, wobei die Anzahl der Stege 8 variieren kann. Wie in Kombination mit der (nicht denselben Maßstab aufweisenden) Schnittansicht gemäß der Linie A-A' zu erkennen ist, sind die Stege 8 gleichmäßig über den Umfang des Abzugskanals 4 verteilt angeordnet. Zudem sind sie einteilig mit dem Garnbildungselement 1 ausgebildet, wobei auch eine Trennung in separate Einzelteile möglich wäre. Die Stege 8 bilden nun im Betrieb der Luftspinnmaschine das genannten Hindernis für die Wanderung der Garnbiegungen entlang der Innenwandung 5, so dass die Bildung eines Falschdrahts zuverlässig verhindert werden kann.Another way to realize the spin stop element 6 according to the invention constructively shows FIG. 4 , The twist stop element 6 comprises in shown four with respect to the longitudinal axis 3 of the discharge channel 4 radially inwardly projecting webs 8, wherein the number of webs 8 may vary. As can be seen in combination with the (not having the same scale) sectional view along the line AA ', the webs 8 are arranged uniformly distributed over the circumference of the discharge channel 4. In addition, they are integrally formed with the Garnbildungselement 1, whereby a separation into separate items would be possible. The webs 8 now form the said obstacle to the migration of the yarn bends along the inner wall 5 during operation of the air-spinning machine, so that the formation of a false-twisting wire can be reliably prevented.

Schließlich sind die Stege 8 im Übergangsbereich 9 zwischen den beiden einen unterschiedlichen Innendurchmesser aufweisenden Abschnitten des Abzugskanals 4 angeordnet. Selbstverständlich wäre auch eine Platzierung oder Erstreckung in den Bereich davor oder danach denkbar.Finally, the webs 8 are arranged in the transition region 9 between the two sections of the discharge channel 4 having a different inner diameter. Of course, a placement or extension in the area before or after conceivable.

Eine entsprechende Anordnung zeigt Figur 5. Hier erstrecken sich die Stege 8 ausgehend vom Übergangsbereich 9 in axialer Richtung des Abzugskanals 4. Die Länge der Stege 8 ist dabei variabel und kann mehrere Zentimeter betragen. Auch können die Stege 8 von Zwischenräumen unterbrochen sein.A corresponding arrangement shows FIG. 5 , Here, the webs 8 extend from the transition region 9 in the axial direction of the discharge channel 4. The length of the webs 8 is variable and can be several centimeters. Also, the webs 8 may be interrupted by gaps.

Schließlich sind den Figuren 6 und 7 zwei weitere vorteilhafte Weiterbildungen der Erfindung zu entnehmen. Im Gegensatz zu den bisher beschriebenen Varianten zeichnen sich die hierin gezeigten Drallstoppelemente 6 dadurch aus, dass sie mit dem Garnbildungselement 1 nicht einteilig hergestellt, sondern vielmehr als separater Einsatz 10 gefertigt wurden. Die Einsätze 10 können, beispielsweise getrennt durch die gezeigten hülsenförmigen Abstandshalter 11, von unten in die mittige Bohrung des Garnbildungselements 1 geschoben und entsprechend fixiert werden.Finally, the FIGS. 6 and 7 two further advantageous developments of the invention can be seen. In contrast to the variants described so far, the twist stop elements 6 shown here are distinguished by the fact that they have not been produced in one piece with the yarn formation element 1, but rather have been produced as a separate insert 10. The inserts 10 can, for example, separated by the sleeve-shaped spacers 11, pushed from below into the central bore of Garnbildungselements 1 and fixed accordingly.

Während Figur 6 Drallstoppelemente 6 mit stegförmigen Fortsätzen zeigt, sind die Drallstoppelemente 6 gemäß Figur 7 halbmondförmig ausgebildet und begrenzen mit der mittigen Bohrung des Garnbildungselements 1 eine linsenförmige Durchgangsöffnung 12. Durch den Versatz der beiden gezeigten Durchgangsöffnungen 12 durchläuft das Garn 22 schließlich einen ZickZack-Kurs, der die Bildung eines Falschdrahts zuverlässig verhindert. Die Drallstoppelemente 6 in Figur 7 weisen zudem abgerundete Oberflächenabschnitte 13 auf, um eine Beschädigung des Garns 22 während der Umlenkung zu vermeiden.While FIG. 6 Spin stop elements 6 with web-shaped extensions shows the twist stop elements 6 according to FIG. 7 crescent-shaped and limit with the central bore of Garnbildungselements 1 a lens-shaped through hole 12. By the offset of the two through holes 12 shown, the yarn 22 finally passes through a zigzag course, which reliably prevents the formation of a false twisting wire. The twist stop elements 6 in FIG. 7 also have rounded surface portions 13 to prevent damage to the yarn 22 during the deflection.

Im Übrigen ist die Erfindung nicht auf die dargestellten Ausführungsbeispiele beschränkt. Vielmehr sind sämtliche Kombinationen der beschriebenen Einzelmerkmale, wie sie in den Ansprüchen, der Beschreibung sowie den Figuren gezeigt oder beschrieben sind und soweit eine entsprechende Kombination technisch möglich bzw. sinnvoll erscheint, Gegenstand der Erfindung.Incidentally, the invention is not limited to the illustrated embodiments. Rather, all combinations of the individual features described, as shown or described in the claims, the description and the figures and as far as a corresponding combination is technically possible or seems reasonable, the subject of the invention.

BezugszeichenlisteLIST OF REFERENCE NUMBERS

11
GarnbildungselementGarnbildungselement
22
Einlassöffnunginlet port
33
Längsachselongitudinal axis
44
Abzugskanalculvert
55
Innenwandunginner wall
66
DrallstoppelementTwist stop element
77
Erhebungsurvey
88th
Stegweb
99
ÜbergangsbereichTransition area
1010
Einsatzcommitment
1111
Abstandshalterspacer
1212
DurchgangsöffnungThrough opening
1313
Oberflächenabschnittsurface section
1414
Spinnstellespinning unit
1515
FaserführungselementFiber guide element
1616
Fasermaterialfiber material
1717
Wirbelkammerswirl chamber
1818
LieferwalzenpaarPair of delivery rollers
1919
Führungskanalguide channel
2020
Spinndüsespinneret
2121
Versorgungsleitungsupply line
2222
Garnyarn

Claims (15)

  1. A yarn-forming element for a spinning station of an airjet spinning machine, wherein the yarn-forming element (1) comprises on one front side an inlet opening (2) as well as a draw-off channel (4) for a yarn which begins in the area of the inlet opening (2) and extends within the yarn-forming element (1) along a longitudinal axis (3), and wherein the yarn-forming element (1) comprises within the draw-off channel (4) at least one twist stop element (6) which at least partially narrows the cross-section of the draw-off channel (4), characterized in that the draw-off channel (4) comprises a contour in the area of the twist-stop element, or elements, which contour deviates from the contour of a cylindrical or truncated cone-shaped borehole.
  2. A yarn-forming element according to the previous claim, characterized in that an inner wall (5) of the draw-off channel (4) in the area of the twist-stop element (6) takes a course in a cross section extending perpendicular to the longitudinal axis (3), which deviates from the course of a circle extending concentrically to the longitudinal axis (3).
  3. A yarn-forming element according to any one or more of the previous claims, characterized in that the yarn-forming element (1) comprises a number of twist-stop elements (6), which are formed by raised areas (7) of the inner wall (5).
  4. A yarn-forming element according to any one or more of the previous claims characterized in that the twist-stop element (6) is formed by a bar (8), which extends axially to the longitudinal axis (3) of the draw-off channel (4) and extends into the draw-off channel (4) in radial direction in relation to the longitudinal axis (3).
  5. A yarn-forming element according to one or more of the previous claims, characterized in that the yarn-forming element (1) comprises a number of twist-stop elements (6) in the form of bars (8), which are arranged in circumferential direction of the inner wall (5) and preferably are uniformly distributed over the inner wall (5).
  6. A yarn-forming element according to any one or more of the previous claims, characterized in that the draw-off channel (4) comprises two sections merging into one another in a transition area (9) and two sections having different inner diameters, wherein the twist-stop element (6) is arranged in the transition area (9).
  7. A yarn-forming element according to any one or more of the previous claims, characterized in that the draw-off channel (4) comprises two sections merging into one another in a transition area (9) and two sections having different inner diameters, wherein the twist-stop element (6) is arranged in the area of the section having the larger inner diameter.
  8. A yarn-forming element according to any one or more of the previous claims, characterized in that the twist-stop element (6) is applied in the yarn-forming element (1) in the form of an insert (10).
  9. A yarn-forming element according to any one or more of the previous claims, characterized in that the twist-stop element (6) is joined to the yarn-forming element (1) in a detachable way.
  10. A yarn-forming element according to any one or more of the previous claims, characterized in that at least two twist-stop elements (6) are arranged in longitudinal direction of the draw-off channel (4), said twist-stop elements (6) preferably being placed at a distance to one another by means of a distance piece (11) arranged between them.
  11. A yarn-forming element according to any one or more of the previous claims, characterized in that the distance piece (11) is tube-shaped in design.
  12. A yarn-forming element according to any one or more of the claims 10 and 11, characterized in that the at least two twist-stop elements (6) border a through-opening (12) for the yarn, said openings (12) being arranged offset to one another in radial direction in relation to the longitudinal axis (3).
  13. A yarn-forming element according to any one or more of the previous claims, characterized in that the twist-stop element (6) and the yarn-forming element (1) are designed as one piece.
  14. A yarn-forming element according to any one or more of the previous claims, characterized in that the twist-stop element (6) comprises at least one rounded surface section (13).
  15. A yarn-forming element according to any one or more of the previous claims, characterized in that the yarn-forming element (1) is designed as a spinning tip for a hollow spindle of an airjet spinning machine consisting of at least a spinning tip and a spindle body.
EP12186910.1A 2011-10-07 2012-10-02 Thread creation element for a spinning position of an air jet spinning machine with a twist stop element Not-in-force EP2578730B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE201110054302 DE102011054302A1 (en) 2011-10-07 2011-10-07 Garnbildungselement for a spinning station of an air spinning machine with a twist stop element

Publications (3)

Publication Number Publication Date
EP2578730A2 EP2578730A2 (en) 2013-04-10
EP2578730A3 EP2578730A3 (en) 2015-04-08
EP2578730B1 true EP2578730B1 (en) 2016-07-06

Family

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EP12186910.1A Not-in-force EP2578730B1 (en) 2011-10-07 2012-10-02 Thread creation element for a spinning position of an air jet spinning machine with a twist stop element

Country Status (3)

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EP (1) EP2578730B1 (en)
CN (1) CN103031626B (en)
DE (1) DE102011054302A1 (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH708620A1 (en) * 2013-09-30 2015-03-31 Rieter Ag Maschf Fiber guide element for a spinning nozzle of an air spinning machine and thus equipped spinning station.
CN104568427A (en) * 2014-11-18 2015-04-29 中国航空动力机械研究所 Conical gear shaft twisting-stopping simulation structure device and application

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DE3824283C1 (en) * 1988-07-16 1989-10-26 Schubert & Salzer Maschinenfabrik Ag, 8070 Ingolstadt, De
JPH07126923A (en) * 1993-11-04 1995-05-16 Koyo Seiko Co Ltd Spindle apparatus for spinning machine
DE29907512U1 (en) * 1999-04-28 2000-08-31 Hamel Ag, Arbon Hollow spindle, in particular for the production of elastic winding yarns
JP2001146647A (en) * 1999-11-22 2001-05-29 Murata Mach Ltd Spinning apparatus
CN100467685C (en) * 2001-05-18 2009-03-11 村田机械株式会社 Spinning appuratus and method and hollow guide shaft member for spinning
EP1375709B1 (en) * 2002-06-21 2014-08-06 Maschinenfabrik Rieter Ag Piecing method for, or piecing of, spinning stations in Air vortex spinning machines
DE10261011A1 (en) * 2002-12-17 2004-07-08 Wilhelm Stahlecker Gmbh Device for producing a spun thread
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CN1882728B (en) * 2003-09-12 2010-09-01 里特机械公司 Drawing frame-roving frame combination for the production of rove and method for producing rove from the fiber group
DE102004013828B4 (en) * 2004-03-15 2007-03-15 Wilhelm Stahlecker Gmbh Garnabzugsdüse for an open-end rotor spinning device
CN101006214B (en) 2004-08-20 2010-05-12 里特机械公司 Spindle having an injector channel and method for piecing up the yarn end in an air jet spinning machine
DE102008006379A1 (en) * 2008-01-29 2009-07-30 Oerlikon Textile Gmbh & Co. Kg Air-jet spinning device for use in production of yarn, has cladding gap downstream to plane, in which air flow initially withdrawing from nozzles impinges housing part surface, where gap width suddenly increases and is in specific range
CN101294319B (en) * 2008-05-26 2010-06-02 东华大学 Spinning apparatus with air injection whirling current for lowering fibre
CN101476180B (en) * 2009-01-23 2010-12-08 东华大学 Self-twisting hollow ingot special for jet air vortex spinning

Also Published As

Publication number Publication date
EP2578730A3 (en) 2015-04-08
DE102011054302A1 (en) 2013-04-11
CN103031626A (en) 2013-04-10
EP2578730A2 (en) 2013-04-10
CN103031626B (en) 2016-01-20

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