Roving-forming element for a roving machine as well as a roving machine equipped therewith

Abstract

A yarn-forming element is provided for a roving machine that produces a roving from a fiber structure using compressed air. The yarn-forming element includes an intake opening for fibers of the fiber structure, an outlet for emergence of the roving produced from the fiber structure, and a draw-off channel that connects the intake opening and the outlet. A front end surrounding the intake opening is formed as a first truncated cone in at least some sections thereof. The first truncated cone includes a larger base surface and a smaller opposite cover surface that is adjacent the draw-off channel. An angle () between a lateral line of the first truncated cone and an axis of the first truncated cone is less than 90 and greater than 70.

Claims

1. A roving-forming element for a roving machine for producing a roving from a fiber structure using compressed air, the roving-forming element comprising: an intake opening for fibers of the fiber structure; an outlet for emergence of the roving produced from the fiber structure; a draw-off channel that connects the intake opening and the outlet; a front end surrounding the intake opening, the front end formed as a first truncated cone in at least some sections thereof; the first truncated cone comprising a larger base surface and a smaller opposite cover surface adjacent the draw-off chapel; and wherein an angle () between a lateral line of the first truncated cone and an axis of the first truncated cone is less than 90 and greater than 70.

2. The roving-forming element according to claim 1, wherein the draw-off channel comprises a longitudinal axis that is or colinear with the axis of the cone.

3. The roving-forming element according to claim 1, the draw-off channel comprises an inside diameter in an area adjacent to the intake opening of 4 mm to 12 mm.

4. The roving-forming element according to claim 1, further comprising a cylindrical wall with a cylindrical outside surface and a concentric cylindrical inside surface bordering the draw-off channel in an area adjacent the intake opening, and wherein an entirety of the front end of the roving-forming element connecting the cylindrical outside surface and the cylindrical inside surface defines the first truncated cone.

5. The roving-forming element according to claim 1, further comprising a transition region between the front end and the draw-off channel and a transition region between the front end and an outside surface of the roving-forming element, wherein one or both of the transition regions are rounded.

6. The roving-forming element according to claim 1, further comprising a chamfer formed in the front end in the shape of a second truncated cone, the second truncated cone comprising a larger base surface adjacent an outside surface of the roving-forming element and an opposite smaller cover surface adjacent the base surface of the first truncated cone.

7. The roving-forming element according to claim 6, wherein the chamfer forms an angle () with a longitudinal axis of the draw-off channel of between 20 and 70.

8. The forming roving-forming element according to claim 1, further comprising a second trucated cone situated above the first truncated cone in a side view of the roving-forming element, the second truncated cone surrounding the first truncated cone in a top view of the yarn-forming element.

9. The roving-forming element according to claim 8, wherein the second truncated cone is connected directly to the first truncated cone, wherein the first and second truncated cones are concentric.

10. The roving-forming element according to claim 8, wherein a lateral line of the first truncated cone and a lateral line of the second truncated cone form a different respective angle (, ) with a longitudinal axis of the draw-off channel.

11. A roving machine for producing a roving from a fiber structure, comprising: at least one spinning device; the spinning device comprising an eddy chamber with an intake opening for the fiber structure and a roving-forming element extending at least partially into the eddy chamber; air jets directed into the eddy chamber, by means of which air is introduced into the eddy chamber in a predetermined direction of rotation in order to impart a twist to the fiber structure fed through the intake opening in a region of an intake opening of the roving-forming element; and wherein the roving-forming element is according to claim 4.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) Additional advantages of the invention are described in the following embodiments. Schematically in the drawings:

(2) FIG. 1 shows a roving machine in a side view;

(3) FIG. 2 shows a detail of a known spinning device of a roving machine;

(4) FIG. 3a shows a truncated cone;

(5) FIG. 3b shows a detail of a roving-forming element according to the invention in a longitudinal section;

(6) FIGS. 4a to 7b show details of additional embodiments of roving-forming elements according to the invention in longitudinal section; and

(7) FIG. 8 shows a detail of another spinning device of a roving machine.

DETAILED DESCRIPTION

(8) Reference will now be made to embodiments of the invention, one or more examples of which are shown in the drawings. Each embodiment is provided by way of explanation of the invention, and not as a limitation of the invention. For example features illustrated or described as part of one embodiment can be combined with another embodiment to yield still another embodiment. It is intended that the present invention include these and other modifications and variations to the embodiments described herein.

(9) FIG. 1 shows a schematic view of a detail of a roving machine. The roving machine may comprise, as needed, a drawing device having a plurality of drawing device rollers 21, each of which can rotate about an axis of rotation 23 (only two of the six drawing device rollers 21 are labeled with a reference numeral), wherein the drawing device is supplied with a fiber structure 1, for example, in the form of a doubled drawing sliver, during the spinning operation.

(10) Furthermore, the roving machine shown here has one or more spinning devices 22 arranged next to one another, each having an interior eddy chamber 15 (see FIG. 2), in which the fiber structure 1 and/or at least some of the fibers of the fiber structure 1 is/are provided with a twist (the exact mechanism of action of the spinning device 22 is described in greater detail below).

(11) In addition, the roving machine may have a draw-off device 24 with a plurality of cooperating draw-off rollers 31, as well as a bobbin device 25 downstream from the draw-off rollers 31, with the help of which the roving 2 leaving the spinning device 22 through an outlet 4 (which at the same time forms the outlet 4 of the draw-off channel 5, which is shown in greater detail in FIG. 2, for example) can be wound onto a sleeve 32 in order to form a bobbin, with the aid of a traversing element 20. The roving machine according to the invention need not necessarily have a drawing device, as illustrated in FIG. 1. The draw-off rollers 31 are not absolutely necessary.

(12) In any case, the roving machine according to the invention operates according to an air-spinning method. To form the roving 2, the fiber structure 1 is arranged over an intake opening 16, where a so-called fiber guide element is preferably guided into the eddy chamber 15 of the spinning device 22 (see also FIG. 2). It receives a twist there, i.e., at least some of the free fiber ends of the fiber structure 1 are picked up by an air current created by air jets 18 arranged accordingly in an eddy chamber wall 26 surrounding the eddy chamber 15. Some of the fibers here are pulled out of the fiber structure 1 at least some distance and wound around the tip of a roving-forming element 17 protruding into the eddy chamber 15. Due to the fact that the fiber structure 1 is drawn out of the eddy chamber 15 through a draw-off channel 5 arranged inside the roving-forming element 17 and through an intake opening 3 in the roving-forming element 17 arranged in the area of the front end 6 of the roving-forming element 17 pointing in the direction of the inlet opening 16, finally the free fiber ends are therefore also drawn in the direction of the intake opening 3 and are thereby wrapped as so-called winding fibers around the core fibers running centrallyresulting in a roving 2 having the desired twist. The draw-off channel 5 should also have an inside diameter D, the size of which is within the range given above.

(13) In general, it should be pointed out that the roving 2 produced here is a yarn with a relatively small amount of winding fibers or a yarn in which the winding fibers are wrapped relatively loosely around the inner core so that the roving 2 remains drawable. This is crucial because the roving 2 that is produced here must be drawn again with the help of a drawing device on a downstream textile machine (for example, a ring-spinning machine) in order to be suitable for further processing to form a traditional yarn, which can be processed on a weaving machine, for example, to form a fabric.

(14) With regard to the air jets 18, it should be pointed out here merely as a precautionary measure that the air jets should usually be oriented so that they jointly create an air flow directed in the same direction with a uniform direction of rotation. The individual air jets 18 here are preferably arranged in rotational symmetry to one another. Furthermore, it should be pointed out that the inclination of the air jets 18 can be selected within certain limits based on the longitudinal axis L of the draw-off channel 15. The air jets 18 may thus run, for example, at a right angle to the aforementioned longitudinal axis L (see the air jet 18 shown at the right of FIG. 2). A certain oblique position is of course also conceivable, so that the angle between a central axis of the air jet 18 (not shown) and the longitudinal axis L is different from 90 (see air jet 18 shown at the right of FIG. 2). In general, the inclination of all the air jets 18 should be the same. The diagram in FIG. 2 was selected only in order to show in principle that different inclinations of the air jets 18 are conceivable in general.

(15) Whereas FIG. 2 shows a known roving-forming element 17 with a front end 6 running at a right angle to the longitudinal axis L of the draw-off channel 5, FIGS. 3b to 7b show embodiments of roving-forming elements 17 according to the invention, wherein only the region of the front end 6 surrounding the intake opening 3 and a portion of the wall 30 of the roving-forming element 17 connected thereto are shown for reasons of simplicity.

(16) As shown in FIG. 3b, for example, the roving-forming element 17 according to the invention is characterized in that the aforementioned front end 6, which is part of the wall 30 of the roving-forming element 17, has a slight inward inclination. In other words, the roving-forming element 17 comprises a front end 6, which surrounds the intake opening 3 and is shaped like a truncated cone 27 in at least some sections, wherein the cover surface 7 of the truncated cone 27 is situated between the base surface 8 of the truncated cone 27 and the outlet 4 of the roving-forming element 17.

(17) With regard to the concepts used in conjunction with the truncated cone 27, reference is made to FIG. 3a, from which it can be seen that the cover surface 7 is the circular area having the smaller radius and the base surface 8 is the circular area having the larger radius. Finally, the lateral surface 29 is the area connecting the base surface 8 to the cover surface 7. The lateral lines 28 are the lines situated on the lateral surface 29 and running in a plane having the cone axis K, which in turn represents the axis of rotation of the truncated cone 27.

(18) As can be seen with the individual embodiments according to FIGS. 3b to 7b, the roving-forming element 17 according to the invention has a front end 6, which has the aforementioned truncated cone shape in at least some sections, wherein the angle between the longitudinal axis L of the draw-off channel 5 and any lateral line 28 on the truncated cone 27 (this angle is the only one shown in FIG. 3 for reasons of simplicity) has a value greater than 70 and less than 90. The aforementioned range thus forms a relatively shallow cone, which thus also has only a slight funnel effect.

(19) The region of the entire front end 6 of the roving-forming element 17, which surrounds the intake opening 3 and connects the inside face 19 of the roving-forming element 17 bordering the draw-off channel 5 and an outside surface 10 of same, which is preferably concentric with said inside surface 19 (at least in a first region connected to the front end 6). FIG. 3b shows a corresponding embodiment.

(20) Furthermore, it is conceivable for the transition 11 between the front end 6 of the roving-forming element 17 and the aforementioned outside surface 10 of same to be rounded (FIGS. 4a and 4b). Alternatively or additionally, the transitional area 9 between the front end 6 of the roving-forming element 17 and the draw-off channel 5 may be rounded (FIG. 4b).

(21) FIGS. 5a and 5b show approaches, in which the front end 6 of the roving-forming element 17 comprises another region in addition to the aforementioned truncated cone-shaped region 27, the additional region also being a truncated cone-shaped region 27. The front end 6 thus preferably comprises a first truncated cone-shaped region 13 and a second truncated cone-shaped region 14.

(22) The angle between a lateral line 28 on the first truncated cone region 13 and the longitudinal axis L of the draw-off channel 5 is preferably greater than the angle between a lateral line 28 of the second truncated cone region 14 and the longitudinal axis L of the draw-off channel 5 (FIG. 5b). However, for many cases, an embodiment of a different type may also be advantageous, such as that shown in FIG. 5a.

(23) FIGS. 6a and 6b show that the front end 6 of the roving-forming element 17 may also be formed in part by a chamfer 12, wherein the angle between a lateral line 28 on the truncated cone 27 which is described by the chamfer 12, and the longitudinal axis L of the draw-off channel 5 is preferably in the range already mentioned in the general description. The chamfer 12 in principle forms the second truncated cone region 14 described above.

(24) In addition, FIGS. 7a and 7b show that the shape of the outside surface 10 of the roving-forming element 17 and/or the shape of the inside surface 19 of the roving-forming element 17 may differ from the shape of a cylinder and/or may have step gradations.

(25) FIG. 8 shows details of a cross section through another spinning device 22. In addition to air jets 18, which serve to form the eddy current flow already described during normal operation and thus according to a spinning start process, the spinning device 22 also comprises one or more spinning start jets 33, by means of which compressed air can be introduced into the eddy chamber 15 during a spinning start process (also).

(26) In other words, it is thus advantageous if the spinning device 22 has special spinning start air jets 33, which are charged with compressed air exclusively or jointly with the air jets 18 during a spinning start process. The spinning start process is the initial sequence of roving production, in which the fiber structure 1 is introduced into the eddy chamber 15 which has been empty until then, and is twisted there to form a roving 2. The resulting roving section is transferred over a corresponding draw-off device 24 after leaving the draw-off channel 5 with continued feed and twisting of the fiber structure 1 and is brought in contact with a rotating sleeve 32. Following that, there is normal operation of the spinning device 22, in which the additional roving 2 is produced continuously from the fiber structure 1 supplied, and the roving is drawn off from the spinning device 22.

(27) It may be advantageous for only the air jets 18 to apply compressed air during normal operation and for only the spinning start air jets 33 to apply compressed air during the spinning start process (both should form different angles to the longitudinal axis L of the draw-off channel 5), but it may also be advantageous if the spinning start air jets 33 are also subjected to compressed air during normal operation. In particular, the spinning start air jets 33 should be inclined with respect to the longitudinal axis L of the draw-off channel 5 to be able to generate an air flow, which extends at least a distance into the draw-off channel 5 (the angle between the longitudinal axis L and the central axis of the spinning start air jets 33 and/or their directional vectors should thus be different from 90). This ultimately prevents air from flowing through the draw-off channel 5 in the direction of its intake opening 3 opposite the direction of movement of the roving 2.

(28) The present invention is not limited to the embodiment described and illustrated here. Modifications within the scope of the patent claims are also possible, as is any combination of the features described here, even if they are described and illustrated in different parts of the description and/or the claims or in different embodiments.

LIST OF REFERENCE NUMERALS

(29) 1 fiber structure 2 roving 3 intake opening of the roving-forming element 4 outlet of the roving-forming element 5 draw-off channel 6 front end of the roving-forming element 7 cover surface of the truncated cone 8 base surface of the truncated cone 9 transitional area between the front end of the roving-forming element and the draw-off channel 10 exterior surface of the roving-forming element 11 transition between the front end of the roving-forming element and the outside surface of same 12 chamfer 13 first truncated cone region 14 second truncated cone region 15 eddy chamber 16 intake opening 17 roving-forming element 18 air jet 19 inside face of the roving-forming element bordering the draw-off channel 20 traversing element 21 drawing device roller 22 spinning device 23 axis of rotation of the drawing device roller 24 draw-off device 25 bobbin device 26 eddy chamber wall 27 truncated cone 28 lateral line of the truncated cone 29 lateral surface of the truncated cone 30 wall of the roving-forming element 31 draw-off roller 32 sleeve 33 spinning start air jet angle between a lateral line of the truncated cone and its cone axis angle between the chamfer and a longitudinal axis of the draw-off channel angle between a lateral line of the second truncated cone region and the longitudinal axis of the draw-off channel angle between a lateral line of the first truncated cone region and the longitudinal axis of the draw-off channel D inside diameter of the draw-off channel L longitudinal axis of the draw-off channel K cone axis