THREAD CATCHING AND WINDING SYSTEM

Abstract: In a winder for synthetic filament, a chuck, upon which packages of filament are formed in use, has a filament catching and severing ring located beside a chuck region on which a bobbin tube is secured during a winding operation. In use, a filament is moved axially of the chuck first into the catching/severing ring and then on­ to the adjacent tube. Guide means for moving the fila­ ment is operated to increase the speed of axial move­ ment of the filament as soon as it has been caught by the catching ring.

Description: The present invention relates to a system for catching and winding a thread to form a reserve winding in winding a thread package on a bobbin tube. The term "thread" refers particularly, but not exclusively, to threads of synthetic plastics filament in mono-filamentary or multi-filamentary form. The invention is designed particularly, but not exclusively, for use in winding machines for winding packages of relatively high denier (titer) thread, and especially to automatic, so-called wasteless, winders for this purpose. Automatic winders for synthetic filament threads are now very well known in the relevant art, and will not be described herein in detail. One example of a so-called "revolver", machine of this type is described and illustrated in the US-A-4298171, although many alternative designs for this kind of machine are also known. An automatic winding machine operating on a different principle (different "machine geometry") is illustrated and described in EP-A-.73930. Still further machine designs have been proposed from time to time for automatic winding machines. Common to all such designs is a plurality of chucks (or "spindles") individually rotatable about their respective longitudinal chuck axes. Each chuck is adapted to receive one or more bobbin tubes and has means for securing received bobbin tubes to the chuck structure for rotation therewith about the chuck axis. Thread is delivered to the winder continuously. When a delivered thread has been wound into a completed package on one chuck, it is transferred to another chuck on which winding of a new package starts, the thread being severed between the two chucks. Whether the winder is designed with a plurality of chucks as an automatic (wasteless) winder, or with a single chuck, it is common practice to form a "reserve winding" on a bobbin tube after the thread has been caught in a changeover operation but before winding of the package itself begins. The reserve winding is formed on a region of the tube outside (but near) the region on which the package itself is formed. In a system in which the thread end is released by the catching device after completion of winding of the package, it is also known to "overwind" the reserve winding (US-A-3920193, column 6 lines 22 to 35) in order to retain it firmly on place when the package has been removed from the winder. Otherwise, there is a risk that the loose thread end will gradually unwind during subsequent handling and transport. The resultant loose "tail" of thread can catch on machine parts during processing and/or tangle with other threads, leading to severe processing problems. The known arrangements for forming overwound thread reserves are rather complex (both mechanically and from a control point of view). The present invention provides a relatively simple arrangement which can be easily integrated into thread catching and winding systems in general, as will be shown by the subsequent description of one embodiment of such a system. The invention provides in one aspect a method of forming an overwound thread reserve comprising the step of moving a thread guide carrier in a first direction against an abutment and permitting the carrier to recoil and thereby cause a return movement of the thread guide after striking said abutment. In a second aspect, the invention provides (in common with US-A-3920193) an apparatus for making an overwound thread reserve comprising a thread guide, a movable member movable in a predetermined direction and connected to the thread guide to cause the thread guide to form a reserve winding, an abutment for limiting movement of said movable member and means for moving the movable member against the abutment characterised in that said means for moving the movable member and said abutment are arranged so that the impact of said movable member on the abutment causes recoil of the movable member and hence a return movement of the thread guide thereby generating overwinding of the said reserve winding. By way of example, one embodiment of the invention will now be described with reference to the accompanying drawings, in which; Fig. 1 is a longitudinal section through part only of a chuck structure for use in an automatic winding machine for example of the type shown in the Patents referred to in the introduction of this specification, Fig. 2 A is a diagram showing the outline part of a chuck structure in accordance with Fig. 1, Fig. 2 B is a representation of the "winding angle" of a thread relative to the illustrated chuck portion during a changeover operation, and Fig. 2 C is an oscilloscope trace representing movement of a thread guide axially of the chuck, Fig. 3 is a diagrammatic representation of a portion of a winding machine including a chuck structure in accordance with Fig. 1, and Fig. 3 A shows a detail of Fig. 3 drawn to a larger scale, Figs. 4 A and 4 B together show a longitudinal section through a pneumatic piston and cylinder unit incorporated in the winder of Fig. 3. Fig. 1 shows portions of a chuck 10 for a filament winding machine, for example of the type disclosed in European published Patent Application No. 73930. As disclosed in that Patent Application, the chuck is mounted cantilever-fashion projecting forwardly from a headstock which would be disposed to the left of the chuck portion illustrated in Fig. 1. Chuck 10 is mounted in the headstock so as to enable the chuck to rotate in use about its own longitudinal chuck axis 12. The right hand portion (Fig. 1A) of Fig. 1 shows the outboard end of the chuck 10, whereas the left hand portion (Fig. 1B) shows an intermediate portion of the same chuck. As will be described below, chuck 10 is adapted to enable winding of a plurality of threads simultaneously into a corresponding plurality of thread packages spaced axially along the chuck. The main structural element of the chuck 10 is a longitudinally extending, tubular support 14. Within hollow support 14 there are arranged pneumatic operating devices for chuck elements which will be further described below. These pneumatic operating devices are conventional, and accordingly they have not been illustrated in the figures, and will not be described in any further detail. Tube 14 has a plurality of outwardly projecting lands 16 A, 16 B which support a plurality of sleeves 18 concentric with the tube 14 and axially slidable thereon. The number of sleeves 18 corresponds to the number of packages to be formed on the chuck. For convenience of description, it will be assumed that only one such sleeve 18 is illustrated in Fig. 1; the outboard end of the sleeve is seen in Fig. 1A and the inboard end in Fig. 1B. The other sleeves 18 are the same as that actually illustrated in Fig. 1, and the associated elements (which will now be described) are also the same. Adjacent each land 16 the tube 14 has an annular camming ring 20A, 20B respectively. In its end portion near ring 20 A, sleeve 18 has a plurality of elongated slots 22, only two of which can be seen in Fig. 1A. Each slot extends longitudinally of the sleeve and the slots are equiangularly spaced around the axis 12. Each slot receives and retains in use a respective camming element which is conventional and has been omitted for clarity of illustration in Fig. 1. The radially inner portion of the camming element has a surface designed to ride on the camming ring 20A as sleeve 18 is moved axially to the left as viewed in Fig. 1, thereby forcing the camming element radially outwardly relative to this sleeve. This enables the "head portions" (i.e. the radially outward portions) of the camming elements to project into and retain a bobbin tube 26 (dotted lines) which has been placed on the chuck ready for a winding operation. In its end portion near ring 20B, sleeve 18 has a second plurality of similar slots 28, only two of which can be seen in Fig. 1B, and similar camming elements are disposed in these slots for cooperation with the ring 20B as sleeve 18 is moved axially in the chuck structure. Each tube 26 is therefore held by two rings of camming elements 24 adjacent the inboard and outboard ends respectively of the tube. Axial movement of sleeve 18 in the chuck structure is caused by the pneumatically operated devices (referred to above) within the hollow tube 14. A connecting pin 30 extends from these devices through a slot 32 in the tube 14 to engage with sleeve 18, so that movement of pin 30 axially of the chuck causes corresponding axial movement of sleeve 18. As already referred to above, movement of sleeve 18 to the left as viewed in Fig. 1 causes the camming elements to be moved radially outwardly to engage and retain tube 26, and movement of sleeve 18 to the right as viewed in Fig. 1 will permit the head portions of camming elements to retract within the circumference of sleeve 18, thereby releasing tube 26 (and a thread package carried thereon) for removal from the chuck. By way of example, retention of the outboard bobbin tube 26 has been described in detail above. An end portion 34 of the adjacent bobbin tube is indicated in Fig. 1B. It will be understood that the retention of this tube is effected in the same manner, and this statement applies to any other tubes carried by the chuck 10. At its outboard end, chuck 10 is closed by a cap 36 secured to tube 14 by screws 38. The inboard end of cap 36 is formed as a ring element 46 which cooperates with a ring element 40, mounted on the tube 14, to form a thread catching and severing structure in accordance with US-Patent No. 4106711. Full details of the thread catching and severing ring can be obtained from US-Patent specification 4106711. It is sufficient to mention here that ring element 40 has axially projecting teeth 42 (only one of which can be seen in Fig. 1A) and the inboard end of element 46 is formed with a guide surface 44 for guiding a thread underneath the teeth 42. Under each tooth 42 there is a radially movable clamping pin 45 which moves outwardly under centrifugal force when chuck 10 is rotating at its normal operating speed to engage the underside of its respective tooth and thereby form a clamp for a thread end severed on the tooth. There is a respective thread catching and severing ring for each bobbin tube carried by the chuck 10 in use. The ring for tube 34 can be seen in Fig. 1B and this ring again comprises a ring element 40 identical to the element 40 in Fig. 1A. In each inboard ring, the counterpart to ring element 40 is provided by a second annular ring element 46 secured to tube 14 by screws 48. In Fig. 1B, the clamping pin has been shown in its radially outward (operating) position, whereas in Fig. 1A the clamping pin has been shown in its radially inward (release) position. Fig. 3 again shows the chuck 10 viewed this time in elevation from the front thereof. Chuck 10 is assumed to be in driving relationship with a friction drive roller 50. Roller 50 is mounted in the headstock (not shown) already described above, and is rotatable about its own longitudinal axis (not indicated) parallel to the axis 12 (Fig. 1). The arrangement is essentially as disclosed in European Patent Application No. 73930. Threads, such as thread 52 indicated in Fig. 3, delivered to the winding machine pass first around friction roller 50 before being transferred to respective packages forming on chuck 10. Threads 52 are wound around chuck 10 by reason of the rotation of the latter about its axis 12, caused by its driving contact with friction driver 50. In order to produce the required build for each package forming on chuck 10, each thread is contacted during a winding operation, upstream from the friction roll 50, by the thread guide element 54 of a conventional traverse mechanism 56. This arrangement is very well known in the art, and it will not be described in detail here. During a changeover operation, in which the thread leading to a completed package on an "outgoing" chuck is guided onto an "incoming" chuck in order to start forming a new package thereon, each thread is pushed out of contact with traverse mechanism 56 by a pneumatically operated piston and cylinder unit 58 just upstream from the traverse mechanism. This arrangement has already been described and illustrated in the US-Patent No. 3920193. The piston of the unit 58 pushes each thread into contact with a bar 60 disposed on the side of the thread path opposite the traverse mechanism. The threads are engaged in respective notches 62 (Fig. 3A). Bar 60 is reciprocable axially of roller 50 and chuck 10 by means of a piston and cylinder unit diagrammatically indicated at 64 in Fig. 3, one suitable embodiment which will be described later in this specification in connection with Fig. 4. The basic operation of guide bar 60 has already been disclosed in US-Patent 3920193. Thus, at completion of a winding operation on an outgoing chuck, bar 60 is first held stationary in a predetermined starting position and the threads are forced into the respective notches 62 by piston and cylinder unit 58. The threads therefore no longer traverse axially of their respective packages, but form an accumulation of windings at predetermined locations on the outer circumference of their respective packages. Taking the outboard thread 52 by way of example, the predetermined location is such that the length of thread extending between friction roller 50 and the outgoing package engages the cylindrical surface of the end cap 36 on incoming chuck 10. The inboard threads engage the cylindrical surfaces on their respective associated ring elements 46 (Fig. 1). Bar 60 is now drawn axially of roller 50 and chuck 10 from the above described starting position inboard towards the non-illustrated headstock. Each thread is therefore drawn to the left as viewed in Fig. 1 from the cylindrical receiving surface on ring element 46 onto the respective guide surface 44 (Fig. 1A) by means of which the thread is directed underneath the teeth 42 of the associated ring element 40 (Fig. 1A and 1B). By this means, the thread is clamped and severed as described in US-Patent No. 4106711, so that the threads are now each secured to the "incoming" chuck 10 and have been separated from the packages on the "outgoing" chuck (not illustrated). As described in US-Patent No. 3920193, continued axial movement of the bar 16 in the same direction will draw the clamped thread onto the associated bobbin tube 26, 34 etc., whereafter thread reserve windings can be formed (for example as disclosed in US-Patent No. 3920193) and the threads can eventually be returned to the traverse mechanism 56 to enable normal package winding to start. A desirable mode of movement of the thread during the changeover operation can be seen from Fig. 2. The lowermost portion (Fig. 2A) of Fig. 2 represents a detail of the outboard ring structure shown in Fig. 1A, but drawn to a larger scale. Due to the larger scale, it can be seen that end cap 36 is provided with a shallow recess 43 just to the right of the guide surface 44. The trough of this recess 43 provides a predetermined starting position for the thread when it rests on the end cap 36 prior to movement into the catching ring. In the starting position the thread lies in a plane normal to the axis 12 (Fig. 1) as indicated by the dotted line extending through the trough of recess 43 in Fig. 2. It will be recalled that in this starting condition the thread extends from the friction roller 50 (Fig. 3) over the end cap 36 to the outgoing package into which it is still being wound because of the rotational inertia of that package which has not yet been braked to a standstill. When bar 60 begins to move axially of chuck 10 the thread will move out of the plane at right angles to the axis 12 and will begin to slide on the end cap 36 to adopt an angle α (Fig. 2B) with respect to the plane through the trough of recess 43. Angle α is dependent upon the speed of axial movement of the corresponding notch 62 in bar 60. As will be explained further below, Fig. 2B has been grossly simplified for purposes of illustration of the principle only. According to this principle, bar 60 is moved with a constant axial speed throughout the phase A (Fig. 2B) during which the thread is moved into the clamp provided between one of the clamping pins 45 and the corresponding tooth 42. For the present, the corresponding angle α can be assumed to be correspondingly constant. As soon as the thread has been caught by the clamp 46, 42, the speed of bar 60 is increased to a higher level which is maintained constant throughout the phase B (Fig. 2) while the thread is moved from the clamping point onto the bobbin tube 26. The corresponding winding angle is indicated at β in Fig. 2B, and it is an essential feature of this invention that angle β is greater than angle α. In the phase C only partly illustrated in Fig. 2, a transfer tail winding is formed on the bobbin tube. Thereafter the thread passes into the traverse region in which the main package structure is built up. Phase C will not be described in any significant detail in this specification, since the principles involved have already adequately explained in US-Patent No. 392 0193. However, in relation to the illustrated portion of phase C, the piston and cylinder unit illustrated in figure provides a convenient and elegant means of obtaining the effect represented in Fig. 2B. In interpreting Fig. 2B, it must be borne in mind that the diagram does not represent the thread itself but only an approximated "winding angle" of the thread relative to a plane normal to the chuck axis. In Fig. 2B, the relevant angles have been grossly exaggerated for ease of illustration of the principles involved. These angles are in any event not directly observable and must be derived by calculations involving approximations as further explained below. Angle α must be maintained below a certain maximum value dependent upon the design of the thread catching ring structure. If this maximum value is exceeded, there is a risk that the thread will "bridge" the ring structure and will not be caught, so that the changeover operation is a failure. In practical terms, this means that there is a certain maximum permissible speed for the axial movement of the bar 60 during the phase A. During this phase A, bar 60 is functioning in the same way as a traverse mechanism and the "winding angle" α can be assessed in the same way as the winding angle induced by a traverse mechanism, i.e. by reference to the relation between the speed of the traverse guide notch 62 axially of the chuck and the linear speed of the thread delivered to the package. Based on this calculation, an angle α of up to about 1° is normally permissible, but the preferred range for angle α is 0.5 to 0.8°. The requirements for angle β are the opposite of those for angle α. With a steeper angle β the thread presents a better "profile" to the catching means usually provided on the bobbin tube end, e.g. in the form of a notch in that tube end. Angle β is preferably made as high as possible, the practical limit being determined by the practical possibilities to accelerate the masses associated with the movement of the bar 60. A minimum angle β of 2° is desirable, and the preferred region for angle β with the currently available means for moving the path 60 lies in range over 3°. For the reasons quoted in US-Patent No. 3920193, the winding angle in the transfer tail phase C as the thread passes into the traverse zone similar to the angle β. In Fig. 2 an "overwound" thread reserve is produced in the phase C by reversing the direction of winding in this phase, thereby fixing the thread tail released by the clamp 46, 42 at the completion of the winding operation. Fig. 2C represents an oscillograph trace illustrating the movement of the bar 60 in a winder according to the invention. The horizontal axis of this trace represents distance travelled by one of the notches in the bar and the vertical axis represents time. The scale of the horizontal axis of this trace is different from that of the other portions of Fig. 2, but the phases of movement of the path corresponding to phases A, B and C are clearly recognisable. As would be expected, it is not possible to achieve absolutely constant velocity within the various phases, and sudden changes of velocity between phases. Over the phase A, beginning at the origin of the curve and leading towards the "knee" in the curve, the average velocity is approximately 0.16 m/sec.; with a delivered speed of the thread of 3000 m/min., this gives a calculated angle α of 0.18°. The speed represented by a tangent at the knee in the curve, is 0.42 m/sec., giving a calculated angle of 0.48° at the join between the phases A and B. The average speed in phase B has been measured in the range 0.5 to 2.5 m/sec., giving an angle β of 1.7 to 2.8.°, again calculated at a delivered linear thread speed of 3000 m/min. Using this system it has been possible to reduce the percentage of rejected thread reserves, due to failure of the thread to climb onto the bobbin tube. Fig. 4 illustrates a pneumatically operated piston and cylinder unit suitable for use as unit 64 in the arrangement illustrated diagrammatically in Fig. 3. The upper half (Fig. 4A) of Fig. 4 represents the left hand portion of the piston and cylinder unit and the lower half (Fig. 4B) of the same figure represents the right hand portion of the same piston and cylinder unit, the portions being joined at the line I in these figures. The portions can be considered separately, since they perform quite separate functions, their common chamber 66 being used as a common pressure reservoir for both portions. The lefthand portion (64 A- Fig. 4A) of unit 64 controls and operates the bar 60 during the phases A and B, and this portion will be described first. Portion 64A comprises the common pressure reservoir chamber 66, defined by cylinder portion 68, and an auxiliary chamber 70 within cylinder portion 72. Cylinder portions 68 and 72 are joined by a bulkhead 74 having a central opening 76. When opening 76 is closed, as will be described below, the bulkhead and the closure for opening 76 together isolate chamber 70 from pressure reservoir 66. As soon as the closure is removed from opening 76, chamber 70 is subjected to the pressure in reservoir 66. Chamber 70 contains a piston 78 having a piston rod 80 extending through the block 82 defining the left hand end of chamber 70 and the left hand end of unit 64. Piston rod 80 is operatively connected to guide bar 60. The unit is illustrated in the starting condition, in which the thread passes through the plane of the recess 43 (Fig. 2) and lies in the plane normal to the chuck axis 12. In this condition, piston 78 engages bulkhead 74. In this condition, an extension 84 formed integral with piston 78 projects through the opening 76 into chamber 66. A seal 86 provided in the bulkhead 74 engages extension 84 so that the latter forms an effective closure for the opening 76 as referred to above. Chamber 66 can be pressurized and vented via an opening 88 (Fig. 4B) in cylinder portion 68. Chamber 70 can be pressurized and vented via the passages 90, 92 formed in end block 82 (Fig. 4A). These passages are joined by an auxiliary chamber 94 containing a valve element 96, preferably a rapid vent valve. When the passage 90 is pressurized, valve element 96 is forced to the upper end of chamber 94, (as viewed in Fig. 4A) and the pressure applied to passage 90 is communicated via chamber 94 and passage 92 to the chamber 70. If chamber 66 is vented at this stage, piston 78 is forced into the illustrated condition engaging bulkhead 74. If sub-atmospheric pressure appears at passage 90, valve element 96 is drawn rapidly downwardly (as viewed in Fig. 4A) along auxiliary chamber 94 into the illustrated condition, in which the upper portion of chamber 94, passage 92 and the chamber 70 are vented directly to atmosphere. This venting effect is produced in order to start the leftward movement of the thread as viewed in Fig. 2 B - before this triggering operation, the vent in block 82 is held closed and the chamber 70 is pressurized. Chamber 66 is also pressurized, but since the pressure in this chamber acts only on the surface area presented by the axial face of the extension 84, it is relatively easy for the pressure in chamber 70, acting upon the full axial face of the piston 78, to hold the piston 78 against the bulkhead 74 until vent valve 96 is opened. When valve 96 is opened the forces produced by the pressure in chamber 66 urge piston 78 towards the left in chamber 70 at a speed dependent upon the pressure in chamber 66 and the effective surface area of the extension 84. This represents phase A. Chamber 70 remains isolated from the pressure in chamber 66 until the extension 84 clears the bulkhead 74, and free the opening 76 for communication of fluid pressure between these chambers. Piston 78 is then subjected to the full pressure available in reservoir 66 on the full cross-sectional area of cylinder portion 70. The movement of piston 78 towards the left is accelerated very rapidly and piston 78 is driven against the plug 82 defining the lefthand end of chamber 70. This represents phase B referred to above and extends into phase C as seen in Fig. 2. The recoil from this substantial blow produces the return movement indicated in the illustrated portion of phase C. A ring 98 of resiliently compressible material is secured on the plug 82 within the chamber 70 surrounding the piston rod 80. This acts as a shock absorber absorbing some of the impact of the piston 78 on the plug 82. The resilience of the material of ring 98 is such that the ring can force piston 78 back against the pressure provided from reservoir 66 after the initial impact has been absorbed. This assists the recoil return movement referred to above and thus helps to produce the "overwound" transfer tail referred to above. As can be seen on the oscillograph trace, by adaptation of the characteristic of the material of ring 98, a degree of oscillation can be induced in phase C so that a "double overwinding" is induced. Fig. 4B illustrates an arrangement very similar in principle to that shown in Fig. 4A, and it is believed that a very brief description of this arrangement will suffice. In Fig. 4B, chamber 200 corresponds to chamber 70 in Fig. 4A; bulkhead 202 corresponds to bulkhead 74; piston 204 and piston rod 206 correspond to piston 78 and piston rod 80 respectively; extension 208 corresponds to extension 84 and plug 210 corresponds to plug 82. This arrangement produces the final phase shown in Fig. 2C; the extension 208 can therefore be made substantially shorter than the extension 84, since it is not required to produce a long phase, similar to the phase A, as an introduction to the final phase. The short extension 208 serves merely to seal with the bulkhead 202. The invention is not limited to details of the embodiment illustrated in and described with reference to the drawings. In particular, the arrangement shown in Fig.3 has been given by way of example only, to show the comcrete application of the principles to a specific winding machine. However, it is not necessary that the change in thread movement be induced by a thread guide system such as that shown in Fig. 3. Although the invention is expected to have its most useful application in automatic winders enabling wasteless operation, the simple diagrammatical illustration in Fig. 3 indicates that this also is not an essential feature. The invention can equally be applied to winders having only a single chuck where an interruption of winding is essential between successive winding operations in order to enable removal of the completed packages from the single chuck and substitution of fresh bobbin tubes therefor. Furthermore, the invention is not limited to the friction drive system shown in Fig. 3: alternative drive systems in which the chuck is driven directly by its own drive motor are well known in the winding art and the invention is equally applicable to them. Where a friction drive system is used, it is not essential to use the so-called "print friction" arrangement shown in Fig. 3 in which the thread is passed around the friction roller 50 before being transferred to the package. Alternative systems in which the thread is transferred to the package without first contacting the friction roller are known and the invention is applicable to them. The time intervals represented by phases A and B in Fig. 2B, and the speeds of movement represented by the oscillograph trace, can be controlled within limits by selection of the length and cross sectional area of the extension 84, the pressure in reservoir 66, the cross sectional area of chamber 70 and the length of that chamber. Final setting of the system to produce the optimum effect can be obtained by adjusting the position of the unit 64 at the mountings (not shown) securing it to the machine. It is not essential to eliminate entirely windings formed on the chuck (as opposed to the bobbin tube). A relatively short tail formed of such loosened windings, for example of approximately the same axial length as the bobbin tube itself, generally produces no problems. Attempts to eliminate such short tails will usually simply lead to unduly costly measures in controlling the system. The invention is not limited to use with a chuck in which the thread catching and cutting structure is permanently recessed "below" the outer peripheral surface of the chuck. Chucks have already been proposed in which catching and cutting devices are mounted for radial movement relative to the chuck between radially inner positions (when the chuck is stationary and a doffing operation is carried out) and radially outer positions (when the chuck is rotating and a changeover operation is to be effected) - see US Patent 4155512. The guide illustrated in Fig. 3A has been designed to move all threads of a given winding position simultaneously. This is not essential. For example, where settings are extremely critical, it may be desirable to provide individual guides for each of the threads at the position.

Claims: A method of forming an overwound thread reserve comprising the step of moving a thread guide carrier in a first direction against an abutment and permitting the carrier to recoil and thereby cause a return movement of the thread guide after striking said abutment. An apparatus for making an overwound thread reserve by a method as claimed in claim 1 comprising a thread guide (60), a movable member (78, 80) movable in a predetermined direction and connected to the thread guide (60) to cause the thread guide to form a reserve winding, an abutment (82, 98) for limiting movement of said movable member (78, 80) and means (66, 72) for moving the movable member (78, 80) against the abutment (82, 98) characterised in that said means (66, 72) for moving the movable member (78, 80) and said abutment (82, 98) are arranged so that the impact of said movable member (78, 80) on the abutment (82, 98) causes recoil of the movable member (78, 80) and hence a return movement of the thread guide (60) thereby generating overwinding of the said reserve winding. An apparatus as claimed in claim 2 characterised in that said abutment (82, 98) includes a resilient damping means (98) engageable by said movable member (78, 80)

Inventors: FLUEELI, ADOLF, OSWALD, HEINZ, SCHEFER, KURT, Flüeli, Adolf
Applicants: MASCHINENFABRIK RIETER AG
Application year: 1986
Main classification: B65H54
IPC codes: B65H54, B65H65, D01D7