EP3464691B1 - Yarn forming element for a pre-spinning machine and pre-spinning machine equipped therewith - Google Patents
Yarn forming element for a pre-spinning machine and pre-spinning machine equipped therewith Download PDFInfo
- Publication number
- EP3464691B1 EP3464691B1 EP17723523.1A EP17723523A EP3464691B1 EP 3464691 B1 EP3464691 B1 EP 3464691B1 EP 17723523 A EP17723523 A EP 17723523A EP 3464691 B1 EP3464691 B1 EP 3464691B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- yarn
- forming element
- truncated cone
- roving
- fiber structure
- 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.)
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- 238000009987 spinning Methods 0.000 title description 22
- 239000000835 fiber Substances 0.000 claims description 71
- 230000007704 transition Effects 0.000 claims description 10
- 230000015572 biosynthetic process Effects 0.000 description 7
- 238000000034 method Methods 0.000 description 4
- 239000004753 textile Substances 0.000 description 3
- 238000010042 air jet spinning Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000007378 ring spinning Methods 0.000 description 2
- 238000004804 winding Methods 0.000 description 2
- 238000011109 contamination Methods 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 230000000284 resting effect Effects 0.000 description 1
- 239000013598 vector Substances 0.000 description 1
- 238000009941 weaving Methods 0.000 description 1
Images
Classifications
-
- D—TEXTILES; PAPER
- D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
- D01H—SPINNING OR TWISTING
- D01H1/00—Spinning or twisting machines in which the product is wound-up continuously
- D01H1/11—Spinning by false-twisting
- D01H1/115—Spinning by false-twisting using pneumatic means
-
- D—TEXTILES; PAPER
- D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
- D01H—SPINNING OR TWISTING
- D01H5/00—Drafting machines or arrangements ; Threading of roving into drafting machine
- D01H5/18—Drafting machines or arrangements without fallers or like pinned bars
- D01H5/70—Constructional features of drafting elements
- D01H5/72—Fibre-condensing guides
-
- D—TEXTILES; PAPER
- D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
- D01H—SPINNING OR TWISTING
- D01H7/00—Spinning or twisting arrangements
- D01H7/92—Spinning or twisting arrangements for imparting transient twist, i.e. false twist
Definitions
- the present invention relates to a yarn-forming element for a roving machine, with which roving can be produced from a fiber structure with the aid of compressed air, the yarn-forming element comprising an inlet opening for the fibers of the fiber structure, and the yarn-forming element having an outlet for the outlet of the roving machine during operation the fiber structure in the region of the inlet opening of the yarn formation element and has a discharge channel connecting the inlet opening and the outlet.
- a roving machine for producing a roving from a fiber structure with at least one spinning station having a whirlpool chamber with an inlet opening for the fiber structure and a yarn-forming element extending at least partially into the whirlpool chamber, and the spinning station having air nozzles directed into the whirlpool chamber via which air can be introduced into the vortex chamber in a predetermined direction of rotation in order to impart a rotation in said direction of rotation to the fiber structure fed via the inlet opening in the region of an inlet opening of the yarn-forming element.
- Roving machines with corresponding spinning positions are known in the prior art and are used to produce a roving from an elongated fiber structure.
- the outer fibers of the fiber structure are wound around the inner core fibers with the help of a turbulent air flow generated by the air nozzles inside the turbulence chamber in the area of the inlet opening of the yarn-forming element and thus form the core fibers that are decisive for the desired strength of the yarn.
- B. can be wound onto a sleeve.
- a spinning position of an air jet spinning machine for spinning a fiber structure to produce a yarn is known.
- the spinning position points a pair of delivery rollers and a spinneret, the spinneret having a yarn-forming element and a fiber-guiding element.
- the fiber guide element has a beginning facing the pair of delivery rollers and an end facing away from the pair of delivery rollers.
- the fiber structure is fed to the spinneret with the pair of delivery rollers and introduced into the spinneret through the fiber guide element, and then a yarn is formed from the fiber structure by the yarn-forming element.
- the spinning station has a turbulence chamber with an inlet opening for the fiber structure and a yarn-forming element that extends at least partially into the turbulence chamber.
- the term roving (other designation: Lunte) to understand a fiber structure, in which at least a part of the fibers around a inner core are wound.
- This type of yarn is characterized by the fact that, despite having a certain strength that is sufficient to transport the yarn to a subsequent textile machine, it is still capable of being drawn.
- the roving can thus using a default device, z. B. the drafting system, a textile machine processing the roving, for example a ring spinning machine, before it is finally spun into a conventional yarn.
- a fiber guide element is usually arranged, via which the fiber strand is guided into the spinneret and finally into the area of the yarn-forming element, with the yarn-forming elements generally being elongated structures with a internal discharge duct find use.
- the geometry of the yarn-forming element In addition to the geometry of the vortex chamber and the strength and alignment of the individual air flows formed by the air nozzles, the geometry of the yarn-forming element also plays a decisive role in the quality of the roving.
- the object of the present invention is therefore to propose a yarn-forming element and a roving machine equipped with it, which enables the production of a roving of particularly high quality.
- the yarn-forming element is characterized in that it comprises an end face surrounding the inlet orifice, which at least partially has the shape of a truncated cone, with the top surface of the truncated cone being arranged between the base of the truncated cone and the outlet of the yarn-forming element.
- the top surface of the truncated cone is understood to be the flat and circular surface of the truncated cone with the smaller radius and the base surface is understood to be the flat and circular surface of the truncated cone with the larger radius.
- a corresponding truncated cone is shown in Figure 3a .
- the yarn-forming element thus has an end face that is at least partially conical or funnel-shaped, with the funnel or cone or the above-mentioned truncated cone tapering in the direction of the outlet of the yarn-forming element.
- a shape is produced, for example, by countersinking.
- the angle between a generatrix of the truncated cone and its cone axis has a magnitude that is less than 90° and greater than 70°.
- the cone axis is the axis of rotation of the truncated cone.
- the generating line is a line that lies on the lateral surface of the truncated cone and is in a plane with the axis of the cone runs. Also in this context Figure 3a referenced, showing a corresponding truncated cone.
- the end face should therefore have the shape of a relatively flat truncated cone, the height of which should be only between 2% and 20% of the diameter of the base area. If a slub of the roving reaches the area of the end face, which is thicker than the inner diameter of the discharge channel, the slub area in the area of the end face of the yarn forming element or the frustoconical section gets caught and can thus be easily removed.
- the frustoconical area of the end face should merge directly into the discharge channel, so that the diameter or the cross-sectional shape of the discharge channel in this area corresponds to the diameter or the shape of the top surface of the truncated cone.
- the discharge channel has a longitudinal axis and the longitudinal axis and said cone axis run parallel or collinear to one another.
- the discharge duct is preferably rotationally symmetrical, in which case the longitudinal axis would correspond to the axis of rotation of the discharge duct.
- the stated mutual arrangement of the longitudinal axis and cone axis ensures that a plane resting on the end face of the yarn-forming element runs perpendicular to the longitudinal axis of the discharge channel, along which the roving moves in the direction of the outlet of the yarn-forming element.
- the discharge channel has an inner diameter in a region adjoining the inlet opening or the truncated cone, the amount of which is 4 mm to 12 mm, preferably 6 mm to 8 mm. If the specified diameter limits are observed, a particularly advantageous air flow occurs in the area of the inlet opening of the yarn-forming element, which causes only part of the outer fiber ends to be caught and wrapped around the actual fiber core with the desired strength. On the other hand, if the diameter is less than 4 mm, one gradually arrives in the range of the conventional Air spinning is known and results in a relatively strong yarn that is only partially suitable as a roving.
- the air pressure of the air supplied via the air nozzles must be significantly increased in order to ensure the necessary turbulent flow within the turbulence chamber, since part of the incoming air leaves the turbulence chamber via the inlet opening of the yarn-forming element without going to the contribute to vortex formation.
- a particularly advantageous roving can only be produced if the diameter deviates significantly from the values known from conventional air-jet spinning, which are between 0.5 and a maximum of 2.0 mm the centrally arranged core fibers are looped (thus providing the roving with a protective twist), with the proportion and strength of the wrapping fibers being only so high that the desired drafting of the roving is still possible in the course of the subsequent spinning process on a subsequent spinning machine.
- the yarn-forming element has a cylindrical wall with a cylindrical outer surface and a cylindrical inner surface delimiting the discharge channel in the area of the inlet opening, the inner surface and the outer surface running concentrically.
- the yarn-forming element therefore has at least one cylindrical section with a constant wall thickness in the area adjoining the end face.
- the entire end face of the yarn-forming element which connects the outer surface and the inner surface, has the shape of a truncated cone.
- the section of the yarn-forming element that has the inlet opening thus preferably has three surface sections, namely a surface section formed by the outer surface of the yarn-forming element, a surface section formed by the inner surface adjoining the inlet opening (and at least partially delimiting the discharge channel), and a surface section formed by the end face. which has the shape of a truncated cone.
- the transition area between the end face and the discharge channel and/or the transition between the end face and an outer surface of the yarn-forming element is not sharp-edged, but rounded.
- the radius of the rounded portions which should have a ring shape in a plan view of the end face of the yarn-forming element, should be between 0.1 mm and 2.0 mm.
- the yarn-forming element has a chamfer in the area of the end face, which also has the shape of a truncated cone.
- the bevel should preferably merge into the outer surface of the yarn-forming element and be spaced apart from the discharge channel by a frustoconical area on the end face of the yarn-forming element.
- the base of the truncated cone forming the bevel is arranged between the top surface of this truncated cone and the outlet of the yarn-forming element.
- the chamfer should thus form a truncated cone which is inverted with respect to the truncated cone described in claim 1.
- the base of the truncated cone adjoining the discharge channel corresponds to the top surface of the truncated cone formed by the chamfer.
- the two truncated cones therefore advantageously merge directly into one another.
- the bevel encloses an angle ⁇ with a longitudinal axis of the discharge channel, the amount of which is between 20° and 70°, preferably between 30° and 60°. Furthermore, in a longitudinal section of the yarn-forming element, the bevel should enclose an angle of between 70° and 90° with the further frustoconical region mentioned in claim 1. If the chamfer is arranged between the discharge channel and the further area of the end face of the yarn-forming element, which forms a truncated cone, the stated angle should be greater than 140° and smaller than 180°.
- the end face has at least one second frustoconical region in addition to a first frustoconical region, the second frusto-conical region surrounding the first frusto-conical region in a plan view of the end face of the yarn-forming element.
- the cylindrical end of the yarn-forming element which also includes the inlet opening, is first machined with a countersink in such a way that the area mentioned in claim 1, which has the shape of a truncated cone, is created and then the transition area is provided with an annular chamfer between the face of the yarn-forming element and the outer surface of the yarn-forming element.
- the second frustoconical area directly adjoins the first frustoconical area, with both frustoconical areas preferably running concentrically to one another. It is conceivable in this context that the base of the first frustoconical area forms the top surface of the second frustoconical area. Furthermore, it is advantageous if the diameter of the top surface of the first frustoconical area is smaller than the top surface of the second frustoconical area.
- the smallest angle between a generatrix of the first frustoconical area and a longitudinal axis of the discharge channel has a different, preferably smaller, amount (e.g. 50° to 80°) than the smallest angle between a generatrix of the second frustoconical region and said longitudinal axis of the flue (which should be greater than 70° and less than 90°).
- the yarn-forming element according to the invention is characterized in that at least a part, e.g. B. an annular region of an end face of the yarn-forming element, preferably the entire end face thereof, is inclined inwardly in the direction of the discharge channel in a longitudinal section of the yarn-forming element.
- the present invention relates to a roving machine for producing a roving from a fiber structure with at least one spinning station, the spinning station having a turbulence chamber with an inlet opening for the fiber structure and a yarn forming element extending at least partially into the vortex chamber.
- the spinning station also includes air nozzles directed into the whirl chamber, via which air can be introduced into the whirl chamber in a predetermined direction of rotation, in order to impart a rotation in said direction of rotation to the fiber structure fed via the inlet opening in the region of an inlet opening of the yarn-forming element.
- the yarn-forming element has an outlet for the outlet of the roving and a discharge channel connecting the inlet opening and the outlet, through which the roving passes before exiting via the outlet.
- the yarn-forming element is designed according to the previous or following description, with the individual features being able to be implemented in any combination, provided that this does not result in any contradictions.
- figure 1 shows a schematic view of a section of a roving machine.
- the roving machine can have a drafting system with several, each around a rotary axis 23 rotatable drafting system rollers 21 (only two of the six drafting system rollers 21 are provided with a reference number), the drafting system being supplied with a fiber structure 1, for example in the form of a doubled draw frame sliver, during the spinning operation.
- the roving frame shown comprises one or more spinning nozzles 22 arranged adjacent to one another, each with an internal turbulence chamber 15 (see FIG figure 2 ), in which the fiber structure 1 or at least some of the fibers of the fiber structure 1 is provided with a twist (the precise mode of operation of the spinneret 22 is described in more detail below).
- the roving machine can comprise a take-off device 24 with a plurality of interacting take-off rollers 31 and a winding device 25 downstream of the take-off rollers 31, with the aid of which the spinneret 22 can be fed via an outlet 4 (which at the same time is the outlet 4 of the, for example, in figure 2 closer shown discharge channel 5 forms) leaving roving 2 can be wound onto a sleeve 32 to form a coil, in which case a traversing element 20 can be used.
- the roving machine according to the invention does not necessarily have to have a drafting system, as is shown in figure 1 is shown.
- the take-off rollers 31 are also not absolutely necessary.
- the roving machine works according to an air spinning process.
- the fiber strand 1 is guided into the turbulence chamber 15 of the spinneret 22 via an inlet opening 16, in which a so-called fiber guide element is preferably arranged (see also figure 2 ).
- a so-called fiber guide element is preferably arranged (see also figure 2 ).
- Some of the fibers are pulled out of the fiber structure 1 at least a little and wound around the tip of a yarn-forming element 17 protruding into the eddy chamber 15 .
- the draw-off channel 5 should also have an inside diameter D, the amount of which is in the above-mentioned range.
- the roving 2 produced is a yarn with a relatively small proportion of twisted fibers, or a yarn in which the twisted fibers are wrapped relatively loosely around the inner core, so that the Roving 2 remains draftable.
- a subsequent textile machine e.g. a ring spinning machine
- a drafting system in order to be able to be further processed into a conventional yarn that can be processed into a fabric, for example on a weaving machine.
- the air nozzles 18 it should also be mentioned at this point, purely as a precaution, that they should generally be aligned in such a way that they jointly generate a rectified air flow with a uniform direction of rotation.
- the individual air nozzles 18 are preferably arranged rotationally symmetrically to one another.
- the inclination of the air nozzles 18 in relation to the longitudinal axis L of the discharge channel 5 can be selected within certain limits.
- the air nozzles 18 could run perpendicular to the longitudinal axis L mentioned (see in figure 2 air nozzle 18 shown on the left).
- the yarn-forming element 17 is characterized in that said end face, which is part of the wall 30 of the yarn-forming element 17, is inclined slightly inward.
- the yarn-forming element 17 comprises an end face 6 surrounding the inlet opening 3, which has the shape of a truncated cone 27 at least in sections, with the top surface 7 of the truncated cone 27 being arranged between the base 8 of the truncated cone 27 and the outlet 4 of the yarn-forming element 17.
- the top surface 7 is the circular surface with the smaller radius and the base surface 8 is the circular surface with the larger radius.
- the lateral surface 29 is the surface that connects the base surface 8 to the top surface 7 .
- the generatrices 28 are the lines that lie on the lateral surface 29 and run in a plane with the cone axis K, which in turn represents the axis of rotation of the truncated cone 27 .
- the yarn-forming element 17 according to the invention has an end face 6 which, at least in sections, has the above-mentioned truncated cone shape, with the Figure 3b Angle ⁇ shown between the longitudinal axis L of the discharge channel 5 and any surface line 28 of the truncated cone 27 has an amount that is greater than 70 ° and less than 90 °. Said area thus forms a relatively flat cone, which also has only a slight funnel effect.
- the frustoconical area preferably forms the entire end face 6 of the Yarn-forming element 17, which surrounds the inlet opening 3 and which connects the inner surface 19 of the yarn-forming element 17, which delimits the discharge channel 5, and an outer surface 10 of the same, which preferably runs concentrically with said inner surface 19 (at least in a first area adjoining the end face 6).
- a corresponding version is in Figure 3b shown.
- transition 11 between the end face 6 of the yarn-forming element 17 and the aforementioned outer surface 10 of the same is rounded ( Figures 4a and 4b ).
- transition area 9 between the end face 6 of the yarn-forming element 17 and the discharge channel 5 can also be rounded ( Figure 4b ).
- the Figures 5a and 5b show solutions in which the end face 6 of the yarn-forming element 17 comprises, in addition to the area mentioned having the shape of a truncated cone 27 , a further area which also has the shape of a truncated cone 27 .
- the end face 6 therefore preferably comprises a first frustoconical area 13 and a second frustoconical area 14.
- the angle ⁇ between a surface line 28 of the first frustoconical area 13 and the longitudinal axis L of the discharge channel 5 is greater than the angle ⁇ between a surface line 28 of the second frustoconical area 14 and the longitudinal axis L of the discharge channel 5 ( Figure 5b ).
- the opposite design can also be advantageous, as shown in Figure 5a is shown.
- the Figures 6a and 6b show that the end face 6 of the yarn-forming element 17 can also be partially formed by a chamfer 12, the angle ⁇ between a surface line 28 of the truncated cone 27, which is described by the chamfer 12, and the longitudinal axis L of the discharge channel 5 preferably in the already in the range mentioned in the general description.
- the chamfer 12 forms the second frustoconical region 14 described above.
- the shape of the outer surface 10 of the yarn-forming element 17 and/or the shape of the inner surface 19 of the yarn-forming element 17 may deviate from the shape of a cylinder and/or have gradations.
- FIG 8 A detail of a cross section through another spinneret 22.
- the spinneret 22 also includes one or more piecing air nozzles 33, via which (likewise) Compressed air can be introduced into the vortex chamber 15.
- the spinning nozzle 22 has special piecing air nozzles 33 which are fed with compressed air exclusively or together with the air nozzles 18 during a piecing process.
- the piecing process is the initial sequence of roving production, in which the fiber structure 1 is introduced into the previously empty eddy chamber 15 and twisted there to form a roving 2 .
- the roving section thus formed is taken over by a corresponding take-off device 24 after leaving the take-off channel 5 and is brought into contact with a rotating sleeve 32 while the supply and twisting of the fiber structure 1 continues.
- This is followed by normal operation of the spinneret 22 , in which further roving 2 is continuously produced from the supplied fiber structure 1 and drawn off from the spinneret 22 .
- the piecing air nozzles 33 should be inclined relative to the longitudinal axis L of the offtake duct 5 in order to be able to generate an air flow that extends at least a little way into the offtake duct 5 (the angle between the longitudinal axis L and a central axis of the piecing air nozzles 33 or their direction vectors should therefore deviate from 90°). This ultimately prevents air from flowing through the discharge channel 5 in the direction of its inlet opening 3 counter to the direction of movement of the roving 2 .
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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)
Description
Die vorliegende Erfindung betrifft ein Garnbildungselement für eine Vorspinnmaschine, mit der aus einem Faserverband mit Hilfe von Druckluft Vorgarn herstellbar ist, wobei das Garnbildungselement eine Einlassmündung für die Fasern des Faserverbands umfasst, und wobei das Garnbildungselement einen Auslass für den Austritt des beim Betrieb der Vorspinnmaschine aus dem Faserverband im Bereich der Einlassmündung des Garnbildungselements hergestellten Vorgarns und einen die Einlassöffnung und den Auslass verbindenden Abzugskanal aufweist.The present invention relates to a yarn-forming element for a roving machine, with which roving can be produced from a fiber structure with the aid of compressed air, the yarn-forming element comprising an inlet opening for the fibers of the fiber structure, and the yarn-forming element having an outlet for the outlet of the roving machine during operation the fiber structure in the region of the inlet opening of the yarn formation element and has a discharge channel connecting the inlet opening and the outlet.
Darüber hinaus wird eine Vorspinnmaschine zur Herstellung eines Vorgarns aus einem Faserverband mit wenigstens einer Spinnstelle vorgeschlagen, wobei die Spinnstelle eine Wirbelkammer mit einer Einlauföffnung für den Faserverband und ein sich zumindest teilweise in die Wirbelkammer erstreckendes Garnbildungselement aufweist, und wobei die Spinnstelle in die Wirbelkammer gerichtete Luftdüsen umfasst, über die Luft in einer vorgegebenen Drehrichtung in die Wirbelkammer einbringbar ist, um dem über die Einlauföffnung zugeführten Faserverband im Bereich einer Einlassmündung des Garnbildungselements eine Drehung in der genannten Drehrichtung zu erteilen.In addition, a roving machine for producing a roving from a fiber structure with at least one spinning station is proposed, the spinning station having a whirlpool chamber with an inlet opening for the fiber structure and a yarn-forming element extending at least partially into the whirlpool chamber, and the spinning station having air nozzles directed into the whirlpool chamber via which air can be introduced into the vortex chamber in a predetermined direction of rotation in order to impart a rotation in said direction of rotation to the fiber structure fed via the inlet opening in the region of an inlet opening of the yarn-forming element.
Vorspinnmaschinen mit entsprechenden Spinnstellen sind im Stand der Technik bekannt und dienen der Herstellung eines Vorgarns aus einem länglichen Faserverband. Die äußeren Fasern des Faserverbands werden hierbei mit Hilfe einer durch die Luftdüsen innerhalb der Wirbelkammer erzeugten Wirbelluftströmung im Bereich der Einlassmündung des Garnbildungselements um die innenliegenden Kernfasern gewunden und bilden hierdurch die für die gewünschte Festigkeit des Garns ausschlaggebenden Umwindefasern. Hierdurch entsteht ein Vorgarn mit einer echten Drehung, welches schließlich über einen Abzugskanal aus der Wirbelkammer abgeführt und z. B. auf eine Hülse aufgewickelt werden kann.Roving machines with corresponding spinning positions are known in the prior art and are used to produce a roving from an elongated fiber structure. The outer fibers of the fiber structure are wound around the inner core fibers with the help of a turbulent air flow generated by the air nozzles inside the turbulence chamber in the area of the inlet opening of the yarn-forming element and thus form the core fibers that are decisive for the desired strength of the yarn. This creates a roving with a real twist, which is finally discharged via a discharge channel from the vortex chamber and z. B. can be wound onto a sleeve.
Aus der
Aus der
Generell ist im Sinne der Erfindung unter dem Begriff Vorgarn (andere Bezeichnung:
Lunte) ein Faserverband zu verstehen, bei dem zumindest ein Teil der Fasern um einen innenliegenden Kern gewunden sind. Diese Art Garn zeichnet sich dadurch aus, dass sie trotz einer gewissen Festigkeit, die ausreicht, um das Garn zu einer nachfolgenden Textilmaschine zu transportieren, noch immer verzugsfähig ist. Das Vorgarn kann also mit Hilfe einer Verzugseinrichtung, z. B. dem Streckwerk, einer das Vorgarn verarbeitenden Textilmaschine, beispielsweise einer Ringspinnmaschine, verzogen werden, bevor es endgültig zu einem herkömmlichen Garn versponnen wird.In general, within the meaning of the invention, the term roving (other designation:
Lunte) to understand a fiber structure, in which at least a part of the fibers around a inner core are wound. This type of yarn is characterized by the fact that, despite having a certain strength that is sufficient to transport the yarn to a subsequent textile machine, it is still capable of being drawn. The roving can thus using a default device, z. B. the drafting system, a textile machine processing the roving, for example a ring spinning machine, before it is finally spun into a conventional yarn.
Im Bereich des Einlasses der Spinndüse der Spinnstelle, in der die Vorgarnherstellung erfolgt, ist in der Regel ein Faserführungselement angeordnet, über welches der Faserverband in die Spinndüse und schließlich in den Bereich des Garnbildungselements geführt wird, wobei als Garnbildungselemente in der Regel längliche Gebilde mit einem innenliegenden Abzugskanal Verwendung finden.In the area of the inlet of the spinneret of the spinning station in which the roving is produced, a fiber guide element is usually arranged, via which the fiber strand is guided into the spinneret and finally into the area of the yarn-forming element, with the yarn-forming elements generally being elongated structures with a internal discharge duct find use.
Im Bereich der die Einlassmündung umgebenden Stirnseite des Garnbildungselements wird Druckluft über die Luftdüsen in die Wirbelkammer eingebracht, so dass sich letztendlich durch die entsprechende Ausrichtung der Luftdüsen die genannte rotierende Wirbelluftströmung ergibt. Dies führt dazu, dass aus dem das Faserführungselement verlassenden Faserverband einzelne außenliegende Fasern abgetrennt bzw. ein Stück weit aus dem Faserverband herausgezogen und über die Stirnseite des Garnbildungselements umgeschlagen werden. Im weiteren Verlauf rotieren diese Fasern auf der Oberfläche des Garnbildungselements. In der Folge werden durch die Vorwärtsbewegung der innenliegenden Kernfasern des Faserverbandes die rotierenden Fasern um die Kernfasern gewunden und dadurch das Vorgarn gebildet.In the area of the end face of the yarn-forming element surrounding the inlet opening, compressed air is introduced into the turbulence chamber via the air nozzles, so that ultimately the named rotating turbulence air flow results from the appropriate alignment of the air nozzles. As a result, individual outer fibers are separated from the fiber structure leaving the fiber guide element or are pulled out of the fiber structure a little and folded over the end face of the yarn-forming element. As they progress, these fibers rotate on the surface of the yarn-forming element. As a result, the rotating fibers are wound around the core fibers by the forward movement of the inner core fibers of the fiber structure, thereby forming the roving.
Für die Qualität des Vorgarns spielt nun neben der Geometrie der Wirbelkammer und der Stärke und Ausrichtung der einzelnen, durch die Luftdüsen gebildeten, Luftströmungen, auch die Geometrie des Garnbildungselements eine entscheidende Rolle.In addition to the geometry of the vortex chamber and the strength and alignment of the individual air flows formed by the air nozzles, the geometry of the yarn-forming element also plays a decisive role in the quality of the roving.
Aufgabe der vorliegenden Erfindung ist es daher, ein Garnbildungselement und eine damit ausgerüstete Vorgarnmaschine vorzuschlagen, die die Herstellung eines Vorgarns mit besonders hoher Qualität ermöglicht.The object of the present invention is therefore to propose a yarn-forming element and a roving machine equipped with it, which enables the production of a roving of particularly high quality.
Die Aufgabe wird gelöst durch ein Garnbildungselement sowie eine Vorspinnmaschine mit den Merkmalen des unabhängigen Patentanspruchs.The object is achieved by a yarn forming element and a roving machine with the features of the independent patent claim.
Erfindungsgemäß zeichnet sich das Garnbildungselement nun dadurch aus, dass es eine die Einlassmündung umgebende Stirnseite umfasst, die zumindest abschnittsweise die Form eines Kegelstumpfs aufweist, wobei die Deckfläche des Kegelstumpfs zwischen der Grundfläche des Kegelstumpfs und dem Auslass des Garnbildungselements angeordnet ist. Wie üblich, wird auch im Rahmen der vorliegenden Erfindung unter der Deckfläche des Kegelstumpfs diejenige ebene und kreisrunde Fläche des Kegelstumpfs mit dem kleineren Radius und unter der Grundfläche diejenige ebene und kreisrunde Fläche des Kegelstumpfs mit dem größeren Radius verstanden. Dargestellt ist ein entsprechender Kegelstumpf in
Das Garnbildungselement besitzt also eine Stirnseite, die zumindest bereichsweise konus- bzw. trichterförmig ausgebildet ist, wobei sich der Trichter bzw. Konus bzw. der oben genannte Kegelstumpf in Richtung des Auslasses des Garnbildungselements verjüngt. Hergestellt wird eine derartige Form beispielsweise durch Senkbohren.The yarn-forming element thus has an end face that is at least partially conical or funnel-shaped, with the funnel or cone or the above-mentioned truncated cone tapering in the direction of the outlet of the yarn-forming element. Such a shape is produced, for example, by countersinking.
Durch die genannte Form des die Einlassmündung umgebenden Bereichs erhält man eine Stirnseite, die in einer Draufsicht den Abzugskanal ringförmig umgibt und die aufgrund der Trichterwirkung ein sanftes Einlaufen des Vorgarns in den Abzugskanal sicherstellt. Es hat sich gezeigt, dass die Bildung der oben genannten Umwindefasern hierdurch verbessert wird und die Qualität des Vorgarns, insbesondere dessen Gleichmäßigkeit, zunimmt.The stated shape of the area surrounding the inlet opening results in an end face which, in a top view, surrounds the discharge channel in a ring shape and which, due to the funnel effect, ensures that the roving enters the discharge channel gently. It has been shown that the formation of the above-mentioned twisted fibers is improved as a result and the quality of the roving, in particular its uniformity, increases.
Um nun zu verhindern, dass Dickstellen des Vorgarns (die z. B. durch Verunreinigungen des Faserverbands oder durch Bauchbinden des Vorgarns entstehen können) zu weit in den Abzugskanal gezogen werden, wird erfindungsgemäß vorgeschlagen, dass der Winkel zwischen einer Mantellinie des Kegelstumpfs und dessen Kegelachse einen Betrag aufweist, der kleiner als 90° und größer als 70° ist. Die Kegelachse ist hierbei die Rotationsachse des Kegelstumpfs. Bei der Mantellinie handelt es sich um eine Linie, die auf der Mantelfläche des Kegelstumpfs liegt und in einer Ebene mit der Kegelachse verläuft. Auch in diesem Zusammenhang wird auf
Mit anderen Worten sollte die Stirnseite also die Form eines relativ flachen Kegelstumpfs aufweisen, dessen Höhe lediglich zwischen 2 % und 20 % des Durchmessers der Grundfläche betragen sollte. Gelangt nun eine Dickstelle des Vorgarns in den Bereich der Stirnseite, die dicker ist als der Innendurchmesser des Abzugskanals, so bleibt die Dickstelle im Bereich der Stirnseite des Garnbildungselements bzw. des kegelstumpfförmigen Abschnitts hängen und kann somit leicht entfernt werden.In other words, the end face should therefore have the shape of a relatively flat truncated cone, the height of which should be only between 2% and 20% of the diameter of the base area. If a slub of the roving reaches the area of the end face, which is thicker than the inner diameter of the discharge channel, the slub area in the area of the end face of the yarn forming element or the frustoconical section gets caught and can thus be easily removed.
Im Übrigen sollte der kegelstumpfförmige Bereich der Stirnseite direkt in den Abzugskanal übergehen, so dass der Durchmesser bzw. die Querschnittsform des Abzugskanals in diesem Bereich dem Durchmesser bzw. der Form der Deckfläche des Kegelstumpfs entspricht.In addition, the frustoconical area of the end face should merge directly into the discharge channel, so that the diameter or the cross-sectional shape of the discharge channel in this area corresponds to the diameter or the shape of the top surface of the truncated cone.
Darüber hinaus bringt es Vorteile mit sich, wenn der Abzugskanal eine Längsachse aufweist und die Längsachse und die genannte Kegelachse parallel oder kolinear zueinander verlaufen. Der Abzugskanal ist vorzugsweise rotationssymmetrisch, wobei die Längsachse in diesem Fall der Rotationsachse des Abzugskanals entsprechen würde. Durch die genannte gegenseitige Anordnung von Längsachse und Kegelachse wird sichergestellt, dass eine auf der Stirnseite des Garnbildungselements aufliegende Ebene senkrecht zur Längsachse des Abzugskanals, entlang derer sich das Vorgarn in Richtung des Auslasses des Garnbildungselements bewegt, verläuft.In addition, there are advantages if the discharge channel has a longitudinal axis and the longitudinal axis and said cone axis run parallel or collinear to one another. The discharge duct is preferably rotationally symmetrical, in which case the longitudinal axis would correspond to the axis of rotation of the discharge duct. The stated mutual arrangement of the longitudinal axis and cone axis ensures that a plane resting on the end face of the yarn-forming element runs perpendicular to the longitudinal axis of the discharge channel, along which the roving moves in the direction of the outlet of the yarn-forming element.
Besondere Vorteile bringt es mit sich, wenn der Abzugskanal in einem sich an die Einlassmündung bzw. den Kegelstumpf anschließenden Bereich einen Innendurchmesser aufweist, dessen Betrag 4 mm bis 12 mm, vorzugsweise 6 mm bis 8 mm, beträgt. Bei Einhaltung der genannten Durchmessergrenzen entsteht eine besonders vorteilhafte Luftströmung im Bereich der Einlassmündung des Garnbildungselements, die bewirkt, dass lediglich ein Teil der äußeren Faserenden erfasst und mit der gewünschten Festigkeit um den eigentlichen Faserkern geschlungen werden. Liegt der Durchmesser hingegen unterhalb von 4 mm, so gelangt man allmählich in den Bereich, der vom herkömmlichen Luftspinnen bekannt ist und der in einem relativ festen Garn resultiert, das als Vorgarn nur bedingt geeignet ist. Wählt man hingegen einen Durchmesser von über 12 mm, so muss der Luftdruck der über die Luftdüsen zugeführten Luft signifikant erhöht werden, um die nötige Wirbelströmung innerhalb der Wirbelkammer sicherzustellen, da ein Teil der einströmenden Luft die Wirbelkammer über die Einlassmündung des Garnbildungselements verlässt, ohne zur Wirbelbildung beizutragen.There are particular advantages if the discharge channel has an inner diameter in a region adjoining the inlet opening or the truncated cone, the amount of which is 4 mm to 12 mm, preferably 6 mm to 8 mm. If the specified diameter limits are observed, a particularly advantageous air flow occurs in the area of the inlet opening of the yarn-forming element, which causes only part of the outer fiber ends to be caught and wrapped around the actual fiber core with the desired strength. On the other hand, if the diameter is less than 4 mm, one gradually arrives in the range of the conventional Air spinning is known and results in a relatively strong yarn that is only partially suitable as a roving. If, on the other hand, a diameter of more than 12 mm is selected, the air pressure of the air supplied via the air nozzles must be significantly increased in order to ensure the necessary turbulent flow within the turbulence chamber, since part of the incoming air leaves the turbulence chamber via the inlet opening of the yarn-forming element without going to the contribute to vortex formation.
Erst durch die signifikante Abweichung des Durchmessers von den vom herkömmlichen Luftspinnen bekannten Werten, die zwischen 0,5 und maximal 2,0 mm liegen, lässt sich jedoch ein besonders vorteilhaftes Vorgarn herstellen, das sich dadurch auszeichnet, dass ein Teil der Fasern als Umwindefasern um die mittig angeordneten Kernfasern geschlungen werden (und das Vorgarn damit mit einer Schutzdrehung versehen), wobei der Anteil und die Festigkeit der Umwindefasern nur so hoch ist, dass im Verlauf des anschließenden Spinnprozesses an einer nachfolgenden Spinnmaschine auch weiterhin der gewünschte Verzug des Vorgarns möglich ist.However, a particularly advantageous roving can only be produced if the diameter deviates significantly from the values known from conventional air-jet spinning, which are between 0.5 and a maximum of 2.0 mm the centrally arranged core fibers are looped (thus providing the roving with a protective twist), with the proportion and strength of the wrapping fibers being only so high that the desired drafting of the roving is still possible in the course of the subsequent spinning process on a subsequent spinning machine.
Ebenso ist es vorteilhaft, wenn das Garnbildungselement im Bereich der Einlassmündung eine zylindrische Wandung mit einer zylindrischen Außenfläche und einer zylindrischen, den Abzugskanal begrenzenden, Innenfläche aufweist, wobei die Innenfläche und die Außenfläche konzentrisch verlaufen. Das Garnbildungselement besitzt also in dem sich an die Stirnseite anschließenden Bereich zumindest einen zylindrischen Abschnitt mit konstanter Wanddicke.It is also advantageous if the yarn-forming element has a cylindrical wall with a cylindrical outer surface and a cylindrical inner surface delimiting the discharge channel in the area of the inlet opening, the inner surface and the outer surface running concentrically. The yarn-forming element therefore has at least one cylindrical section with a constant wall thickness in the area adjoining the end face.
Ebenso ist es von Vorteil, wenn die gesamte, die Außenfläche und die Innenfläche verbindende, Stirnseite des Garnbildungselements die Form eines Kegelstumpfs aufweist. Der die Einlassmündung aufweisende Abschnitt des Garnbildungselements besitzt somit vorzugsweise drei Flächenabschnitte, nämlich einen durch die Außenfläche des Garnbildungselements gebildeten Flächenabschnitt, einen durch die sich an die Einlassmündung anschließende (und den Abzugskanal zumindest teilweise begrenzenden) Innenfläche gebildeten Flächenabschnitt und einen durch die Stirnseite gebildeten Flächenabschnitt, der die Form eines Kegelstumpfs aufweist.It is also advantageous if the entire end face of the yarn-forming element, which connects the outer surface and the inner surface, has the shape of a truncated cone. The section of the yarn-forming element that has the inlet opening thus preferably has three surface sections, namely a surface section formed by the outer surface of the yarn-forming element, a surface section formed by the inner surface adjoining the inlet opening (and at least partially delimiting the discharge channel), and a surface section formed by the end face. which has the shape of a truncated cone.
Ebenso kann es Vorteile mit sich bringen, wenn der Übergangsbereich zwischen der Stirnseite und dem Abzugskanal und/oder der Übergang zwischen der Stirnseite und einer Außenfläche des Garnbildungselements nicht scharfkantig, sondern abgerundet ist. Der Radius der abgerundeten Abschnitte, die in einer Draufsicht auf die Stirnseite des Garnbildungselements eine Ringform aufweisen sollten, sollte zwischen 0,1 mm und 2,0 mm liegen. Hierdurch werden die Fasern des Faserverbands geringeren mechanischen Belastungen ausgesetzt als bei entsprechend scharfkantigen Übergängen.It can also bring advantages if the transition area between the end face and the discharge channel and/or the transition between the end face and an outer surface of the yarn-forming element is not sharp-edged, but rounded. The radius of the rounded portions, which should have a ring shape in a plan view of the end face of the yarn-forming element, should be between 0.1 mm and 2.0 mm. As a result, the fibers of the fiber structure are exposed to lower mechanical loads than in the case of correspondingly sharp-edged transitions.
Ebenso ist es vorteilhaft, wenn das Garnbildungselement im Bereich der Stirnseite eine Fase aufweist, welche ebenfalls die Form eines Kegelstumpfs aufweist. Die Fase sollte hierbei vorzugsweise in die Außenfläche des Garnbildungselements übergehen und durch einen kegelstumpfförmigen Bereich der Stirnseite des Garnbildungselements vom Abzugskanal beabstandet sein. Insbesondere ist es von Vorteil, wenn die Grundfläche des die Fase bildenden Kegelstumpfs zwischen der Deckfläche dieses Kegelstumpfs und dem Auslass des Garnbildungselements angeordnet ist. Die Fase sollte also einen Kegelstumpf bilden, der bezüglich des in Anspruch 1 beschriebenen Kegelstumpfs auf dem Kopf gestellt ist. Insbesondere ist es von Vorteil, wenn die Grundfläche des sich an den Abzugskanal anschließenden Kegelstumpfs der Deckfläche des durch die Fase gebildeten Kegelstumpfs entspricht. Beide Kegelstümpfe gehen also vorteilhafterweise direkt ineinander über.It is also advantageous if the yarn-forming element has a chamfer in the area of the end face, which also has the shape of a truncated cone. The bevel should preferably merge into the outer surface of the yarn-forming element and be spaced apart from the discharge channel by a frustoconical area on the end face of the yarn-forming element. In particular, it is advantageous if the base of the truncated cone forming the bevel is arranged between the top surface of this truncated cone and the outlet of the yarn-forming element. The chamfer should thus form a truncated cone which is inverted with respect to the truncated cone described in
Vorteilhaft ist es, wenn die Fase mit einer Längsachse des Abzugskanals einen Winkel β einschließt, dessen Betrag zwischen 20° und 70°, vorzugsweise zwischen 30° und 60°, liegt. Ferner sollte die Fase in einem Längsschnitt des Garnbildungselements mit dem weiteren, in Anspruch 1 genannten, kegelstumpfförmigen Bereich einen Winkel einschließen, der zwischen 70° und 90 liegt. Ist die Fase zwischen dem Abzugskanal und dem weiteren, einen Kegelstumpf bildenden, Bereich der Stirnseite des Garnbildungselements angeordnet, so sollte der genannte Winkel größer als 140° und kleiner als 180° sein.It is advantageous if the bevel encloses an angle β with a longitudinal axis of the discharge channel, the amount of which is between 20° and 70°, preferably between 30° and 60°. Furthermore, in a longitudinal section of the yarn-forming element, the bevel should enclose an angle of between 70° and 90° with the further frustoconical region mentioned in
Besondere Vorteile bringt es mit sich, wenn die Stirnseite neben einem ersten kegelstumpfförmigen Bereich zumindest einen zweiten kegelstumpfförmigen Bereich aufweist, wobei der zweite kegelstumpfförmige Bereich den ersten kegelstumpfförmigen Bereich in einer Draufsicht auf die Stirnseite des Garnbildungselements umgibt. Beispielsweise kann eine derartige Ausführungsform dadurch realisiert werden, dass das zylindrische Ende des Garnbildungselements, das auch die Einlassöffnung umfasst, zunächst mit einem Senkbohrer derart bearbeitet wird, dass der in Anspruch 1 genannte Bereich entsteht, der die Form eines Kegelstumpfs aufweist und dass anschließend der Übergangsbereich zwischen der Stirnseite des Garnbildungselements und der Außenfläche des Garnbildungselements mit einer ringförmigen Fase versehen wird.There are particular advantages if the end face has at least one second frustoconical region in addition to a first frustoconical region, the second frusto-conical region surrounding the first frusto-conical region in a plan view of the end face of the yarn-forming element. For example, such an embodiment can be realized in that the cylindrical end of the yarn-forming element, which also includes the inlet opening, is first machined with a countersink in such a way that the area mentioned in
Besonders vorteilhaft ist es, wenn sich der zweite kegelstumpfförmige Bereich direkt an den ersten kegelstumpfförmigen Bereich anschließt, wobei beide kegelstumpfförmigen Bereiche vorzugsweise konzentrisch zueinander verlaufen. Denkbar ist in diesem Zusammenhang, dass die Grundfläche des ersten kegelstumpfförmigen Bereichs die Deckfläche des zweiten kegelstumpfförmigen Bereichs bildet. Ferner ist es von Vorteil, wenn der Durchmesser der Deckfläche des ersten kegelstumpfförmigen Bereichs kleiner ist als die Deckfläche des zweiten kegelstumpfförmigen Bereichs.It is particularly advantageous if the second frustoconical area directly adjoins the first frustoconical area, with both frustoconical areas preferably running concentrically to one another. It is conceivable in this context that the base of the first frustoconical area forms the top surface of the second frustoconical area. Furthermore, it is advantageous if the diameter of the top surface of the first frustoconical area is smaller than the top surface of the second frustoconical area.
Vorteilhaft ist es zudem, wenn der kleinste Winkel zwischen einer Mantellinie des ersten kegelstumpfförmigen Bereichs und einer Längsachse des Abzugskanals einen anderen, vorzugsweise einen kleineren, Betrag (z. B. 50° bis 80°) aufweist, als der kleinste Winkel zwischen einer Mantellinie des zweiten kegelstumpfförmigen Bereichs und der genannten Längsachse des Abzugskanals (der größer als 70° und kleiner als 90° sein sollte).It is also advantageous if the smallest angle between a generatrix of the first frustoconical area and a longitudinal axis of the discharge channel has a different, preferably smaller, amount (e.g. 50° to 80°) than the smallest angle between a generatrix of the second frustoconical region and said longitudinal axis of the flue (which should be greater than 70° and less than 90°).
In jedem Fall zeichnet sich das erfindungsgemäße Garnbildungselement dadurch aus, dass zumindest ein Teil, z. B. ein ringförmiger Bereich einer Stirnseite des Garnbildungselements, vorzugsweise dessen gesamte Stirnseite, in einem Längsschnitt des Garnbildungselements nach innen in Richtung des Abzugskanals geneigt ist.In any case, the yarn-forming element according to the invention is characterized in that at least a part, e.g. B. an annular region of an end face of the yarn-forming element, preferably the entire end face thereof, is inclined inwardly in the direction of the discharge channel in a longitudinal section of the yarn-forming element.
Schließlich betrifft die vorliegende Erfindung eine Vorspinnmaschine zur Herstellung eines Vorgarns aus einem Faserverband mit wenigstens einer Spinnstelle, wobei die Spinnstelle eine Wirbelkammer mit einer Einlauföffnung für den Faserverband und ein sich zumindest teilweise in die Wirbelkammer erstreckendes Garnbildungselement aufweist. Die Spinnstelle umfasst darüber hinaus in die Wirbelkammer gerichtete Luftdüsen, über die Luft in einer vorgegebenen Drehrichtung in die Wirbelkammer einbringbar ist, um dem über die Einlauföffnung zugeführten Faserverband im Bereich einer Einlassmündung des Garnbildungselements eine Drehung in der genannten Drehrichtung zu erteilen. Hierdurch ist aus dem Faserverband ein Vorgarn mit den bereits beschriebenen Eigenschaften herstellbar. Um das Vorgarn schließlich auf eine Hülse aufwinden zu können, besitzt das Garnbildungselement einen Auslass für den Austritt des Vorgarns und einen die Einlassöffnung und den Auslass verbindenden Abzugskanal, den das Vorgarn vor dem Austritt über den Auslass passiert.Finally, the present invention relates to a roving machine for producing a roving from a fiber structure with at least one spinning station, the spinning station having a turbulence chamber with an inlet opening for the fiber structure and a yarn forming element extending at least partially into the vortex chamber. The spinning station also includes air nozzles directed into the whirl chamber, via which air can be introduced into the whirl chamber in a predetermined direction of rotation, in order to impart a rotation in said direction of rotation to the fiber structure fed via the inlet opening in the region of an inlet opening of the yarn-forming element. As a result, a roving with the properties already described can be produced from the fiber structure. In order to finally be able to wind the roving onto a sleeve, the yarn-forming element has an outlet for the outlet of the roving and a discharge channel connecting the inlet opening and the outlet, through which the roving passes before exiting via the outlet.
Erfindungsgemäß ist nun vorgesehen, dass das Garnbildungselement gemäß bisheriger bzw. nachfolgender Beschreibung ausgebildet ist, wobei die einzelnen Merkmale in beliebiger Kombination verwirklicht sein können, sofern sich hieraus keine Widersprüche ergeben.According to the invention, it is now provided that the yarn-forming element is designed according to the previous or following description, with the individual features being able to be implemented in any combination, provided that this does not result in any contradictions.
Weitere Vorteile der Erfindung sind in den nachfolgenden Ausführungsbeispielen beschrieben. Es zeigen, jeweils schematisch:
Figur 1- eine Vorspinnmaschine in der Seitenansicht,
Figur 2- einen Ausschnitt einer bekannten Spinndüse einer Vorspinnmaschine,
- Figur 3a
- einen Kegelstumpf,
- Figur 3b
- einen Ausschnitt eines erfindungsgemäßen Garnbildungselements im Längsschnitt,
- Figuren 4a bis 7b
- einen Ausschnitt weiterer Ausführungsformen erfindungsgemäßer Garnbildungselemente im Längsschnitt, und
Figur 8- einen Ausschnitt einer weiteren Spinndüse einer Vorspinnmaschine.
- figure 1
- a roving machine in side view,
- figure 2
- a section of a known spinneret of a roving machine,
- Figure 3a
- a truncated cone,
- Figure 3b
- a section of a yarn formation element according to the invention in longitudinal section,
- Figures 4a to 7b
- a detail of further embodiments of yarn formation elements according to the invention in longitudinal section, and
- figure 8
- a section of another spinneret of a roving frame.
Ferner umfasst die gezeigte Vorspinnmaschine eine oder mehrere benachbart zueinander angeordneten Spinndüsen 22 mit jeweils einer innenliegenden Wirbelkammer 15 (siehe
Darüber hinaus kann die Vorspinnmaschine eine Abzugseinrichtung 24 mit mehreren zusammenwirkenden Abzugswalzen 31 sowie eine den Abzugswalzen 31 nachgeschaltete Spulvorrichtung 25 umfassen, mit deren Hilfe das die Spinndüse 22 über einen Auslass 4 (der gleichzeitig den Auslass 4 des beispielsweise in
In jedem Fall arbeitet die erfindungsgemäße Vorspinnmaschine nach einem Luftspinnverfahren. Zur Bildung des Vorgarns 2 wird der Faserverband 1 über eine Einlauföffnung 16, in der vorzugsweise ein so genanntes Faserführungselement angeordnet ist, in die Wirbelkammer 15 der Spinndüse 22 geführt (siehe auch
Generell sei an dieser Stelle klargestellt, dass es sich bei dem hergestellten Vorgarn 2 um ein Garn mit einem relativ geringen Anteil an Umwindefasern, bzw. um ein Garn, bei dem die Umwindefasern relativ locker um den inneren Kern geschlungen sind, handelt, so dass das Vorgarn 2 verzugsfähig bleibt. Dies ist entscheidend, da das hergestellte Vorgarn 2 an einer nachfolgenden Textilmaschine (beispielsweise einer Ringspinnmaschine) nochmals mit Hilfe eines Streckwerks verzogen werden muss, um zu einem herkömmlichen Garn weiterverarbeitet werden zu können, das beispielsweise auf einer Webmaschine zu einem Stoff verarbeitet werden kann.In general, it should be made clear at this point that the roving 2 produced is a yarn with a relatively small proportion of twisted fibers, or a yarn in which the twisted fibers are wrapped relatively loosely around the inner core, so that the
Im Hinblick auf die Luftdüsen 18 sei an dieser Stelle zudem rein vorsorglich erwähnt, dass diese in der Regel so ausgerichtet sein sollten, dass sie gemeinsam eine gleichgerichtete Luftströmung mit einem einheitlichen Drehsinn erzeugen. Vorzugsweise sind die einzelnen Luftdüsen 18 hierbei rotationssymmetrisch zueinander angeordnet. Zudem sei darauf hingewiesen, dass die Neigung der Luftdüsen 18 bezogen auf die Längsachse L des Abzugskanals 5 in gewissen Grenzen gewählt werden kann. So könnten die Luftdüsen 18 beispielsweise senkrecht zur genannten Längsachse L verlaufen (siehe in
Während
Wie nun beispielsweise
Hinsichtlich der verwendeten Begrifflichkeiten im Zusammenhang mit dem Kegelstumpf 27 wird auf
Wie den einzelnen Ausführungsbeispielen gemäß den
Vorzugsweise bildet der kegelstumpfförmige Bereich die gesamte Stirnseite 6 des Garnbildungselements 17, die die Einlassmündung 3 umgibt und die die den Abzugskanal 5 begrenzende Innenfläche 19 des Garnbildungselements 17 und eine Außenfläche 10 desselben verbindet, die vorzugsweise konzentrisch zur genannten Innenfläche 19 verläuft (zumindest in einem ersten sich an die Stirnseite 6 anschließenden Bereich). Eine entsprechende Ausführung ist in
Ferner ist es denkbar, dass der Übergang 11 zwischen der Stirnseite 6 des Garnbildungselements 17 und der genannten Außenfläche 10 desselben abgerundet ist (
Die
Vorzugsweise ist der Winkel ε zwischen einer Mantellinie 28 des ersten kegelstumpfförmigen Bereichs 13 und der Längsachse L des Abzugskanals 5 größer als der Winkel δ zwischen einer Mantellinie 28 des zweiten kegelstumpfförmigen Bereichs 14 und der Längsachse L des Abzugskanals 5 (
Die
Des Weiteren ist den
Abschließend zeigt
Mit anderen Worten ist es also von Vorteil, wenn die Spinndüse 22 spezielle Anspinnluftdüsen 33 aufweist, die ausschließlich oder gemeinsam mit den Luftdüsen 18 während eines Anspinnvorgangs mit Druckluft beschickt werden. Bei dem Anspinnvorgang handelt es sich um die Anfangssequenz der Vorgarnherstellung, bei der der Faserverband 1 in die bis dahin leere Wirbelkammer 15 eingeführt und dort zu einem Vorgarn 2 verdreht wird. Der hierdurch gebildete Vorgarnabschnitt wird bei weiterhin andauernder Zufuhr und Verdrehung des Faserverbands 1 über eine entsprechende Abzugseinrichtung 24 nach Verlassen des Abzugskanals 5 übernommen und mit einer sich drehenden Hülse 32 in Kontakt gebracht. Im Anschluss daran erfolgt der Normalbetrieb der Spinndüse 22, bei der kontinuierlich weiteres Vorgarn 2 aus dem zugeführten Faserverband 1 hergestellt und aus der Spinndüse 22 abgezogen wird.In other words, it is advantageous if the spinning
Während es von Vorteil sein kann, während des Normalbetriebs nur die Luftdüsen 18 und während des Anspinnvorgangs ausschließlich die Anspinnluftdüsen 33 mit Druckluft zu beaufschlagen (beide sollten mit der Längsachse L des Abzugskanals 5 unterschiedliche Winkel einschließen), kann es ebenso Vorteile mit sich bringen, wenn die Anspinnluftdüsen 33 auch während des Normalbetriebs mit Druckluft beaufschlagt werden. Insbesondere sollten die Anspinnluftdüsen 33 hierbei gegenüber der Längsachse L des Abzugskanals 5 geneigt sein, um eine Luftströmung generieren zu können, die sich zumindest ein Stück weit in den Abzugskanal 5 erstreckt (der Winkel zwischen der Längsachse L und einer Mittelachse der Anspinnluftdüsen 33 bzw. deren Richtungsvektoren sollte also von 90° abweichen). Hierdurch wird schließlich verhindert, dass Luft entgegen der Bewegungsrichtung des Vorgarns 2 durch den Abzugskanal 5 in Richtung dessen Einlassmündung 3 strömt.While it can be advantageous to apply compressed air only to the
Die vorliegende Erfindung ist nicht auf die dargestellten und beschriebenen Ausführungsbeispiele beschränkt. Abwandlungen im Rahmen der Patentansprüche sind möglich.The present invention is not limited to the illustrated and described embodiments. Modifications within the scope of the patent claims are possible.
- 11
- Faserverbandfiber bandage
- 22
- Vorgarnroving
- 33
- Einlassmündung des GarnbildungselementsYarn forming element inlet mouth
- 44
- Auslass des GarnbildungselementsYarn forming element outlet
- 55
- Abzugskanalculvert
- 66
- Stirnseite des GarnbildungselementsFront side of the yarn formation element
- 77
- Deckfläche des KegelstumpfsTop surface of the truncated cone
- 88th
- Grundfläche des Kegelstumpfsbase of the truncated cone
- 99
- Übergangsbereich zwischen der Stirnseite des Garnbildungselements und dem AbzugskanalTransition area between the end face of the yarn formation element and the discharge channel
- 1010
- Außenfläche des GarnbildungselementsOuter surface of the yarn forming element
- 1111
- Übergang zwischen der Stirnseite des Garnbildungselements und der Außenfläche desselbenTransition between the face of the yarn-forming element and the outer surface of the same
- 1212
- Fasechamfer
- 1313
- erster kegelstumpfförmiger Bereichfirst frustoconical area
- 1414
- zweiter kegelstumpfförmiger Bereichsecond frustoconical area
- 1515
- Wirbelkammervortex chamber
- 1616
- Einlauföffnunginlet opening
- 1717
- Garnbildungselementyarn forming element
- 1818
- Luftdüseair nozzle
- 1919
- den Abzugskanal begrenzende Innenfläche des Garnbildungselementsinner surface of the yarn-forming element delimiting the drainage channel
- 2020
- Changierelementoscillating element
- 2121
- Streckwerkswalzedrafting roller
- 2222
- Spinndüsespinneret
- 2323
- Drehachse der StreckwerkswalzeAxis of rotation of the drafting system roller
- 2424
- Abzugseinrichtungtrigger device
- 2525
- Spulvorrichtungspooling device
- 2626
- Wirbelkammerwandungvortex chamber wall
- 2727
- Kegelstumpftruncated cone
- 2828
- Mantellinie des Kegelstumpfssurface line of the truncated cone
- 2929
- Mantelfläche des Kegelstumpfslateral surface of the truncated cone
- 3030
- Wandung des GarnbildungselementsWall of the yarn forming element
- 3131
- Abzugswalzepull-off roller
- 3232
- Hülsesleeve
- 3333
- Anspinnluftdüsepiecing air nozzle
- αa
- Winkel zwischen einer Mantellinie des Kegelstumpfs und dessen KegelachseAngle between a surface line of the truncated cone and its cone axis
- ββ
- Winkel zwischen der Fase und einer Längsachse des AbzugskanalsAngle between the chamfer and a longitudinal axis of the flue
- δδ
- Winkel zwischen einer Mantellinie des zweiten kegelstumpfförmigen Bereichs und der Längsachse des AbzugskanalsAngle between a generatrix of the second frustoconical portion and the longitudinal axis of the flue
- εε
- Winkel zwischen einer Mantellinie des ersten kegelstumpfförmigen Bereichs und einer Längsachse des AbzugskanalsAngle between a generatrix of the first frustoconical portion and a longitudinal axis of the flue
- DD
- Innendurchmesser des AbzugskanalsInside diameter of the flue
- LL
- Längsachse des AbzugskanalsLongitudinal axis of the culvert
- KK
- Kegelachsecone axis
Claims (10)
- A yarn-forming element (17) for a roving machine, with which a roving (2) can be produced from a fiber structure (1) with the help of compressed air,- wherein the yarn-forming element (17) comprises an intake opening (3) for fibers of the fiber structure (1), and- wherein the yarn-forming element (17) has an outlet (4) for the emergence of the roving (2) produced from the fiber structure (1) in the area of the intake opening (3) of the yarn-forming element (17) during operation of the roving machine and having a draw-off channel (5), which connects the intake opening (3) and the outlet (4),characterized in that
the yarn-forming element (17) comprises a front end (6), which surrounds the intake opening (3) and has a truncated cone shape (27) in at least some sections,- wherein the cover surface (7) of the truncated cone (27) is arranged between the base surface (8) of the truncated cone (27) and the outlet (4) of the yarn-forming element (17), and- wherein the angle (α) between a lateral line (28) of the truncated cone (27) and its cone axis (K) has a value less than 90° and greater than 70°. - The yarn-forming element (17) according to the preceding claims, characterized in that the draw-off channel (5) has a longitudinal axis (L), and the longitudinal axis (L) and the aforementioned cone axis (K) run parallel or colinear to one another.
- The yarn-forming element (17) according to any one of the preceding claims, characterized in that the draw-off channel (5) has an inside diameter (D) in an area adjacent to the intake opening (3), the amount being 4 mm to 12 mm, preferably 6 mm to 8 mm.
- The yarn-forming element (17) according to any one of the preceding claims, characterized in that the yarn-forming element (17) has a cylindrical wall (30) with a cylindrical outside surface (10) and a cylindrical inside surface (19) bordering the draw-off channel (5) in the area of the intake opening (3), wherein the inside surface (19) and the outside surface (10) run concentrically, and wherein the entire front end (6) of the yarn-forming element (17) connecting the outside surface (10) and the inside surface (19) has a truncated cone shape (27).
- The yarn-forming element (17) according to any one of the preceding claims, characterized in that the transition region (9) between the front end (6) and the draw-off channel (5) and/or the transition (11) between the front end (6) and an outside surface (10) of the yarn-forming element (17) is/are rounded.
- The yarn-forming element (17) according to any one of the preceding claims, characterized in that the yarn-forming element (17) has in the area of the front end (6) a chamfer (12), which is also in a truncated cone shape (27), wherein the base surface (8) of the truncated cone (27) forming the chamber (12) is arranged between the cover surface (7) of this truncated cone (27) and the outlet (4) of the yarn-forming element (17).
- The yarn-forming element (17) according to any one of the preceding claims, characterized in that the chamfer (12) forms an angle (β) with the longitudinal axis (L) of the draw-off channel (5), this angle amounting to between 20° and 70°, preferably between 30° and 60°.
- The yarn-forming element (17) according to any one of the preceding claims, characterized in that the front end (6) has at least one second truncated cone region (14) in addition to a first truncated cone region (13), wherein the second truncated cone region (14) surrounds the first truncated cone region (13) in a top view of the front end (6) of the yarn-forming element (17).
- The yarn-forming element (17) according to the preceding claim, characterized in that the second truncated cone region (14) is connected directly to the first truncated cone region (13) wherein both truncated cone regions preferably run concentrically to one another.
- A roving machine for producing a roving (2) from a fiber structure (1) having at least one spinneret,- wherein the spinneret has an eddy chamber (15) with an intake opening (16) for the fiber structure (1) and a yarn-forming element (17) extending at least partially into the eddy chamber (15), and- wherein the spinneret comprises air jets (18) directed into the eddy chamber (15), by means of which air can be introduced into the eddy chamber (15) in a predetermined direction of rotation in order to impart a twist in the aforementioned direction of rotation to the fiber structure (1) fed through the intake opening (16) in the region of an intake opening (3) of the yarn-forming element (17),characterized in that
the yarn-forming element (17) is designed according to any one of the preceding claims.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH00675/16A CH712489A1 (en) | 2016-05-26 | 2016-05-26 | Garnbildungselement for a roving and equipped therewith roving. |
PCT/IB2017/052586 WO2017203376A1 (en) | 2016-05-26 | 2017-05-04 | Twine forming element for a pre-spinning machine and pre-spinning machine equipped therewith |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3464691A1 EP3464691A1 (en) | 2019-04-10 |
EP3464691B1 true EP3464691B1 (en) | 2023-05-03 |
Family
ID=58707971
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP17723523.1A Active EP3464691B1 (en) | 2016-05-26 | 2017-05-04 | Yarn forming element for a pre-spinning machine and pre-spinning machine equipped therewith |
Country Status (6)
Country | Link |
---|---|
US (1) | US10900144B2 (en) |
EP (1) | EP3464691B1 (en) |
JP (1) | JP6972025B2 (en) |
CN (1) | CN109154110B (en) |
CH (1) | CH712489A1 (en) |
WO (1) | WO2017203376A1 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH712663A1 (en) * | 2016-07-14 | 2018-01-15 | Rieter Ag Maschf | Process for processing a strand-like fiber composite and roving machine. |
DE102020108257A1 (en) * | 2020-03-25 | 2021-09-30 | Saurer Spinning Solutions Gmbh & Co. Kg | Apparatus for separating fibers and spinning equipment comprising such a device |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102012108613A1 (en) * | 2012-09-14 | 2014-03-20 | Maschinenfabrik Rieter Ag | Spinning station of a roving machine |
Family Cites Families (23)
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US2852906A (en) * | 1951-12-14 | 1958-09-23 | Du Pont | Method and apparatus for producing bulky continuous filament yarn |
US2853906A (en) | 1956-06-07 | 1958-09-30 | Stanley J Pesta | Fixture for stripping metal ends from containers |
CH615467A5 (en) * | 1977-05-17 | 1980-01-31 | Toyo Boseki | Process and apparatus for the purely mechanical production of a staple-fibre yarn consisting of natural or synthetic fibres |
US4290378A (en) * | 1979-08-31 | 1981-09-22 | Monsanto Company | Twisted singles carpet yarn |
ATE20253T1 (en) | 1983-04-12 | 1986-06-15 | Rieter Ag Maschf | FALSE SPIN UNIT. |
JPS60259636A (en) * | 1984-06-04 | 1985-12-21 | Toyoda Autom Loom Works Ltd | Nozzle for spinning fasciated yarn |
IN166161B (en) * | 1985-06-07 | 1990-03-24 | Alan Nicholas Jacobsen | |
JPH01162829A (en) * | 1987-12-18 | 1989-06-27 | Mas Fab Rieter Ag | Air jet nozzle and method for forming rotary air layer at twisting part of said nozzle |
CS269174B1 (en) * | 1988-04-21 | 1990-04-11 | Havranek Zdenek | Spinning jet for yarn's pneumatic formation |
CH676725A5 (en) * | 1988-11-07 | 1991-02-28 | Rieter Ag Maschf | |
DE3927910A1 (en) * | 1989-08-24 | 1991-02-28 | Stahlecker Fritz | FALSE SWIRL NOZZLE FOR PNEUMATIC SPIRAL SPINNING |
JPH0469471U (en) * | 1990-10-26 | 1992-06-19 | ||
JPH0674530B2 (en) * | 1991-07-30 | 1994-09-21 | 村田機械株式会社 | Spinning equipment |
JPH0748673Y2 (en) * | 1992-02-19 | 1995-11-08 | 村田機械株式会社 | Spinning equipment |
JP3552618B2 (en) * | 1999-12-13 | 2004-08-11 | 村田機械株式会社 | Core yarn manufacturing method and apparatus |
DE60104160T3 (en) * | 2000-04-04 | 2012-03-15 | Murata Kikai K.K. | Hollow guide spindle in a vortex spinning machine and method of use |
US20020152739A1 (en) * | 2000-12-22 | 2002-10-24 | Maschinenfabrik Rieter Ag | Spinning device |
CN1200155C (en) * | 2002-07-10 | 2005-05-04 | 东华大学 | Complex twisting device for air-jet eddy-current spinning |
DE10255035A1 (en) * | 2002-11-19 | 2004-06-03 | Wilhelm Stahlecker Gmbh | Air vortex spinning unit for staple fibers includes contraction in annular air exit channel near yarn draw-off tube entry |
EP1621649B1 (en) * | 2004-07-28 | 2008-09-10 | FARE' S.p.A. | Apparatus and method for treating synthetic yarns |
DE102004052206A1 (en) * | 2004-10-19 | 2006-04-20 | Wilhelm Stahlecker Gmbh | Air-jet spinning device |
CN101476180B (en) * | 2009-01-23 | 2010-12-08 | 东华大学 | Self-twisting hollow ingot special for jet air vortex spinning |
US9290863B2 (en) * | 2013-02-13 | 2016-03-22 | Maschinenfabrik Rieter Ag | Spinning unit of an air-jet spinning machine |
-
2016
- 2016-05-26 CH CH00675/16A patent/CH712489A1/en not_active Application Discontinuation
-
2017
- 2017-05-04 EP EP17723523.1A patent/EP3464691B1/en active Active
- 2017-05-04 US US16/303,267 patent/US10900144B2/en active Active
- 2017-05-04 WO PCT/IB2017/052586 patent/WO2017203376A1/en unknown
- 2017-05-04 JP JP2018561497A patent/JP6972025B2/en active Active
- 2017-05-04 CN CN201780031625.6A patent/CN109154110B/en active Active
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
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DE102012108613A1 (en) * | 2012-09-14 | 2014-03-20 | Maschinenfabrik Rieter Ag | Spinning station of a roving machine |
Also Published As
Publication number | Publication date |
---|---|
US10900144B2 (en) | 2021-01-26 |
WO2017203376A1 (en) | 2017-11-30 |
CN109154110B (en) | 2021-06-18 |
US20190323151A1 (en) | 2019-10-24 |
JP2019519690A (en) | 2019-07-11 |
CH712489A1 (en) | 2017-11-30 |
CN109154110A (en) | 2019-01-04 |
JP6972025B2 (en) | 2021-11-24 |
EP3464691A1 (en) | 2019-04-10 |
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