EP0659240A1 - Amortissement des vibrations dans une machine a bobiner les filaments - Google Patents

Amortissement des vibrations dans une machine a bobiner les filaments

Info

Publication number
EP0659240A1
EP0659240A1 EP94918263A EP94918263A EP0659240A1 EP 0659240 A1 EP0659240 A1 EP 0659240A1 EP 94918263 A EP94918263 A EP 94918263A EP 94918263 A EP94918263 A EP 94918263A EP 0659240 A1 EP0659240 A1 EP 0659240A1
Authority
EP
European Patent Office
Prior art keywords
damping
axis
casing
liquid
mandrel
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.)
Withdrawn
Application number
EP94918263A
Other languages
German (de)
English (en)
Inventor
Armin Wirz
Peter Busenhart
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Maschinenfabrik Rieter AG
Original Assignee
Maschinenfabrik Rieter AG
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Maschinenfabrik Rieter AG filed Critical Maschinenfabrik Rieter AG
Publication of EP0659240A1 publication Critical patent/EP0659240A1/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
    • F16F15/023—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using fluid means
    • F16F15/0237—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using fluid means involving squeeze-film damping
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H54/00—Winding, coiling, or depositing filamentary material
    • B65H54/70—Other constructional features of yarn-winding machines
    • D—TEXTILES; PAPER
    • D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
    • D01H—SPINNING OR TWISTING
    • D01H7/00—Spinning or twisting arrangements
    • D01H7/02—Spinning or twisting arrangements for imparting permanent twist
    • D01H7/04—Spindles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C27/00—Elastic or yielding bearings or bearing supports, for exclusively rotary movement
    • F16C27/04—Ball or roller bearings, e.g. with resilient rolling bodies
    • F16C27/045—Ball or roller bearings, e.g. with resilient rolling bodies with a fluid film, e.g. squeeze film damping
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C27/00—Elastic or yielding bearings or bearing supports, for exclusively rotary movement
    • F16C27/06—Elastic or yielding bearings or bearing supports, for exclusively rotary movement by means of parts of rubber or like materials
    • F16C27/066—Ball or roller bearings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H2601/00—Problem to be solved or advantage achieved
    • B65H2601/50—Diminishing, minimizing or reducing
    • B65H2601/52—Diminishing, minimizing or reducing entities relating to handling machine
    • B65H2601/524—Vibration
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H2701/00—Handled material; Storage means
    • B65H2701/30—Handled filamentary material
    • B65H2701/31—Textiles threads or artificial strands of filaments
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2340/00—Apparatus for treating textiles
    • F16C2340/18—Apparatus for spinning or twisting

Definitions

  • the invention is concerned with a damping means for damping vibrations which can arise in the operation of a fast rotating axis (e.g. a spool) in a fila machine.
  • a fast rotating axis e.g. a spool
  • Damping means for a fast rotating axis are described in US 4,669,893.
  • a special application of damping agents in drawing rolls for filament processing has been explained in US Pat. No. 5,159,166.
  • Damping for a winding machine is shown in DE-A-42 40 920.
  • a bobbin mandrel differs fundamentally from a stretching roller in that a relatively long, rotatable element is supported on the fly and, due to the formation of the bobbin during operation, must withstand a considerable increase in weight in the part which is supported on the fly.
  • the solution proposed therein aims to reduce the critical speed of the arrangement in such a way that it is clearly below the operating range. According to this proposal, an attempt is therefore made to influence the natural resonances of the arrangement.
  • Corresponding means have been shown in EP-A-234 844 (see in particular FIG. 8).
  • a spool also differs from a stretching roller in that the external diameter of the rotatable element plays a critical role in the overall arrangement.
  • the outer surface of the mandrel must namely take up bobbin sleeves, which are mostly standardized. Increasing the diameter (to increase the rigidity) reduces the amount a given thread that can be wound into a bobbin. Shortening the mandrel (for the same purpose) has a similar effect.
  • a further difference between a spool mandrel and a stretching roller is therefore that the mandrel cannot necessarily be redesigned to cope with higher speeds - rather, it has to be adapted to many conditions of practical use. If the area of application is expanded from a given mandrel (e.g. according to EP-A 217 276), the resonance range of the second critical speed is therefore reached very quickly.
  • this invention does not attempt to shift this resonance range by changing the construction, but to limit the vibrations by damping in such a way that no significant damage occurs as a result.
  • the invention provides damping for a fast-rotating axis (in particular a spool) in a spool machine, which comprises a centering means for centering the axis relative to a holder, a narrow annular space being formed, in which space damping means surrounding the axis is provided.
  • the centering means is preferably formed in such a way that it can also perform its function in the overhung part in the case of on-the-fly storage and significant weight changes (for example when a docking is formed). This function consists, in particular, of avoiding sagging from the part mounted on the fly or of keeping it within narrow limits.
  • the centering means enables vibrations of the rotating axis to be transmitted to the damping means.
  • the damping agent can comprise a liquid.
  • a liquid supply can be provided in order to make up for losses in operation.
  • a separate centering means can be provided.
  • spring elements can be provided to support a bearing for the axle against a casing.
  • the damping fluid could, however, be provided in a closed elastic container. In this case "l, the container can be used as centering.
  • FIG. 4 shows a longitudinal section through a holder for a coil mandrel according to FIG. 1 with a first damping means according to this invention
  • Fig. 7 is a schematic representation of an alternative solution according to the invention.
  • the mandrel shown in FIG. 1 comprises a bearing part indicated by 12 and a cantilever part indicated by 14.
  • the bearing part 12 comprises a fixed housing 16 which encloses the bearings 18 which determine an axis of rotation 20.
  • the rotatable structure of the mandrel comprises a single, integral (one-piece) load-bearing element, which consists of a first tubular part 22 in the cantilever part 14, and a second tubular part 24, which extends from the first part 22 into the bearing part 12 to be carried by the bearings inside.
  • the outer surface of the tubular part 22 is cylindrical and the diameter of the cross section is selected such that the mandrel can receive and carry coil sleeves indicated by dashed lines 26, 260.
  • These sleeves are usually specified by the end user of the machine. They should have a smooth inner surface so as to allow the sleeves to be slid on the cylindrical outer surface of part 22 and to allow the full thread packs formed thereon, indicated by dashed lines, to be doffed at 28.
  • FIG. 1 shows a mandrel which is designed to carry two spool sleeves in operation in order to wind two packs of two threads supplied.
  • the mandrel is overhung, and the coil sleeves are "plugged” by their movement axially along the mandrel.
  • the mandrel When the mandrel is ready for operation, it therefore carries an "inner” coil sleeve 26 (in the vicinity of the carrier of the mandrel) and an “outer” coil sleeve 260 (near the free end of the mandrel).
  • the invention is not restricted to use with two spool sleeves.
  • the hollow interior of the tubular part 22 defines a chamber 30 which extends axially almost the entire length of the part 22 and opens at the free end of the mandrel.
  • the chamber is closed in operation by a cap 32, which may be by any suitable means (not shown) is attached to the part 22.
  • Devices for fastening and centering each coil sleeve 26 with respect to the tubular part 22 are arranged within the chamber 32. These devices are only indicated schematically in block form in Fig. 2; Suitable designs of such devices are shown in EP-A-217 276.
  • the device comprises a plurality of sleeve-engaging elements 34 which pass through respective openings in the part 22. These openings are arranged uniformly around the axis 20. There are usually six or eight such openings with an equal number of sleeve-engaging elements.
  • the elements are radially movable between retracted positions, in which they do not interfere with the insertion and opening of the coil sleeves, and extended positions, in which they secure the respective coil sleeve with respect to the part 22.
  • each coil sleeve There are two sets of elements 34 for each coil sleeve.
  • the inner movement means being indicated at 36.
  • Each movement means is operated in order to move the elements 34 of the associated set from the retracted to the extended position and to enable the elements to return to the retracted position.
  • the movement means can be operated selectively by a current supply means, which is indicated generally at 38, and extends axially along the central part of the chamber 30.
  • the connection to the power supply means 38 can be established via a passage 40 which extends axially to the tubular part 24.
  • the correct axial position of the inner coil sleeve The tubular part 22 is replaced by an axial one Stop 42 ensures that abuts the inner end of the part 22.
  • the inner coil sleeve can be pushed along the part 22 up to the stop 42.
  • the correct position of the outer coil sleeve 260 is ensured by a positioning element 44, which protrudes through a suitable opening in part 22 after the inner coil sleeve 26 has been fitted. When moved to its extended position, element 44 acts a stop that limits the movement of outer sleeve 260 toward the inner end of part 22.
  • the arrangement is such that a gap 46 is left between the adjacent ends of the correctly positioned sleeves 26, 260.
  • a catching and separating element 48 can be moved into this gap after the sleeves have been attached.
  • the elements 44 and 48 are supported by a common support ring 50 within the tubular part 22. A suitable shape of the ring 50 will be described later in this description.
  • a ring 52 similar to ring 50 is provided adjacent to the outer end of outer sleeve 260.
  • the ring 52 carries only the thread catching and separating elements 54, since the outer sleeve is axially positioned by the element 44 at its inner end.
  • the components arranged within the tubular part 22 are assembled by inserting them through the open, free end of the tubular part, which is then closed by the cap 32.
  • FIG. 2 shows the bearing part 12 of the mandrel according to FIG. 1, but with additional details of a practical embodiment.
  • the support housing is indicated at 16 and the bearing at 18.
  • the part of the rotatable structure with the smaller diameter is indicated by 24 and the axial bore therein by 40.
  • a brake and drive unit 60 is attached to part 24 at its end remote from part 22. This unit is common and will not be described in detail here.
  • the unit also provides a coupling 62, by means of which the liquid pressure medium can be directed into the interior of the passage 40.
  • FIG. 3 shows further details of the connection area 56 in greater detail.
  • FIG. 3 shows that the inner end of the chamber 30 can be brought very close to the outer bearing 18.
  • a suitable taper is provided between the outer diameter of the part 22 (determined by the reference to the coil sleeves to be used) and the outer diameter of the part 24 (determined by the structure of the bearing part 12).
  • the stop 42 forms a projection on this taper and in this embodiment borders on a further projection 63, which makes it possible to provide a thread catch notch 64. In the event that any thread turn extends beyond the inner end of the inner bobbin tube 26, it is retained in this notch 64.
  • the outer end of the passage 40 is connected to an inner end of a tube 66 which extends axially along the central part of the chamber 30.
  • a coil mandrel according to FIGS. 1 to 3 represents a very robust and stable construction which can be carried out relatively free of unbalance problems.
  • resonance problems must be expected, which are related to the so-called critical speeds.
  • the invention provides a damping means which will now be explained with reference to the other figures.
  • FIG. 4 shows the two end parts of a spool holder similar to the holder explained in FIGS. 1 to 3.
  • the intermediate middle part of the holder has nothing to do with the present invention and is not shown or described again.
  • the end section 100 corresponds to the left end of the embodiment according to FIG. 2 and the end section 102 (FIG. 4) corresponds to the right end of the embodiment according to FIG. 2.
  • the casing is indicated in FIG. 4 with the reference number 160; This largely corresponds to the support housing 16 of FIG. 2, with changes being made in the end parts to adapt to the invention, which are explained below.
  • a cavity 162 is formed by an inwardly projecting flange 164.
  • the cavity 162 has a constant round cross section over most of its length from the flange 164 to the end of the casing 160, a groove 168 being milled into the cylindrical inner surface 170 of the cavity.
  • the cavity 162 accommodates a bearing unit, which among other things comprises the following elements (see also FIG. 5):
  • a bearing bush consisting of a carrier 172 and a ring 174 with an L-shaped cross section, b) a cover element 176,
  • the ring 174, the carrier 172 and the cover element 176 each have a cylindrical surface 180, 182, 184 which, after the bearing unit has been received, lies in the cavity 162, either in contact with or at a short distance from the aforementioned inner surface 170.
  • the cover element 176 also has an outwardly projecting flange 186 which is fastened to the end face 188 of the end part 100 by screws (not shown).
  • the ring 174 is also fastened to the carrier 172 with screws (not shown), so that by mounting the cover element 176 in contact with the end face 188, all parts of the bearing unit are positioned relative to the cavity 162.
  • Two grooves 190, 192 are milled into the surface 182 of the carrier 172.
  • One groove 190 ⁇ receives an O-ring 194 which, together with a second O-ring 196 received in the groove 168, forms a narrow, annular space (not identified by a reference number) between the surface 182 and the inner surface 170 axially limited.
  • the second groove 192 opens into this space and is connected to the end face 188 via bores 198, 200.
  • the bore 200 opens into a corresponding opening (not identified by a reference number) in the flange 186, which enables a connection to an oil supply means 202.
  • the latter means is in operation in connection with a source 204 of oil as a damping fluid which flows through the bores 200, 198 can be supplied into the annular space to form an oil film therein.
  • An oil film of approximately 0.1 to 0.2 mm thick (preferably 0.1 to 0.15 mm) has proven to be advantageous.
  • cover element 176 and the carrier 172 are connected to one another via the spring pins 179 in such a way that they are centered against one another (specifically on the axis of rotation 20), so that a small distance A (FIG. 5) between the opposite end faces of these parts is maintained. This creates an annular gap.
  • the spring pins 179 are pressed into respective bores in the cover element 176 and carrier 172.
  • Each bore in the carrier 172 has a part 206 (FIG. 5) which has a larger cross section than the spring pin received and opens onto the annular gap.
  • the pins can be made of steel.
  • the axle 24 is connected to drive elements, as was shown in FIG. 2. These elements are not shown in Fig. 4 since they have nothing to do with the invention.
  • the end section 102 is essentially the same as the end section 100 and the same reference numerals have been used, where possible, to identify the same parts. The construction of the end section 102 will therefore be largely clear without repeating the above description, so that only individual minor deviations will be dealt with.
  • the cover element 176A is in this case with provided with an attachment 177 which projects into the annular space at the end of the mandrel part 22. A thread that jumps over the projection 63 is caught on the attachment 177.
  • a sealing ring 208 is located between a cylindrical part 171 of the carrier 172A and the tapering of the mandrel part 22.
  • the oil supply 202A does not supply damping fluid via an opening in the flange 186 of the cover element 176A, but through a bore 203 directly in the sheath 160.
  • the winder is preferably provided with its own source 204 of damping fluid.
  • the pressure of a few bar in this source must be maintained for safety reasons.
  • Pressure or level monitoring (not shown) can be provided and connected to the machine control system, so that an alarm is generated or the machine is switched off when the monitoring reports a faulty state. It is not necessary in all circumstances to continuously connect the source 204 to the annular space.
  • the feed line 202 or 202A can be provided with a self-closing valve (not shown), so that the source can be disconnected after the "filling" of the room. In this case, the pressure monitor must be connected to the supply line 202, 202A instead of the source 204.
  • a normal "life" for the filled system can be determined so that the damping is periodically replenished during normal machine maintenance.
  • the shaft is indicated here by 300 and the bearings by 302.
  • the sheathing is indicated by 304.
  • a hollow ring 306 is provided between the bearing 302 and the casing 304, which was filled with damping liquid under high pressure and hermetically sealed.
  • the walls 308 and 310 are connected to the bearing and the casing.
  • Form walls 312 and 314 one spring element each, which centers the shaft 300 with respect to the casing, but enables vibrations to be transmitted to the damping fluid.
  • the resilient walls 308, 310 guide the bearing 302 concentrically with the axis of rotation 20.
  • the cross section of the ring 306 is "crimped" at one point and expanded at the diametrically opposite point. Accordingly, the damping liquid tries to flow in the circumferential direction from the area with relatively high pressure to the area with relatively low pressure. At least in the case of discontinuous vibrations (impacts), however, the pressure conditions inside the capsule 306 are subjected to constantly changing forces, so that the liquid offers resistance to the deflection.
  • the entire damping capsule 306 can be replaced after a predetermined service life.
  • the invention is not limited to the application in a supply for the coil mandrel. It can be used to deal with resonance problems in different areas of a winding machine, e.g. also in the suspension of a contact roller (see e.g. EP-A-94 483) or in the carrier of a traverse (see e.g. EP-A-272 458).
  • the invention enables not only an expansion of the area of application from the coil mandrel to a higher speed range, but also in lower speed ranges, where (without the damping) dangerous vibrations at the first critical speed would be expected.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Textile Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Winding Filamentary Materials (AREA)

Abstract

Une fixation de mandrin de bobine comporte deux ensembles paliers étant constitués chacun par un coussinet (182) et un couvercle (184) reliés par des goupilles élastiques (178). Le couvercle (184) permet de loger chaque ensemble palier dans une chambre (162) appropriée, des alésages (200) reliant l'espace séparant le coussinet de la face interne (170) de la chambre à une amenée d'huile (202, 204).
EP94918263A 1993-07-02 1994-06-24 Amortissement des vibrations dans une machine a bobiner les filaments Withdrawn EP0659240A1 (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
CH1992/93 1993-07-02
CH199293 1993-07-02
PCT/CH1994/000131 WO1995001516A1 (fr) 1993-07-02 1994-06-24 Amortissement des vibrations dans une machine a bobiner les filaments

Publications (1)

Publication Number Publication Date
EP0659240A1 true EP0659240A1 (fr) 1995-06-28

Family

ID=4223381

Family Applications (1)

Application Number Title Priority Date Filing Date
EP94918263A Withdrawn EP0659240A1 (fr) 1993-07-02 1994-06-24 Amortissement des vibrations dans une machine a bobiner les filaments

Country Status (4)

Country Link
US (1) US5649670A (fr)
EP (1) EP0659240A1 (fr)
JP (1) JPH08500889A (fr)
WO (1) WO1995001516A1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE202016000655U1 (de) * 2016-02-02 2017-05-03 Leybold Gmbh Lager-Dämpfungselement, Lageranordnung sowie Vakuumpumpe
CN108516414A (zh) * 2018-05-09 2018-09-11 苏州索布机器人有限公司 一种纺织滚筒放置架

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US2155919A (en) * 1937-08-04 1939-04-25 Timken Roller Bearing Co Shaft bearing mounting
GB1212600A (en) * 1967-04-21 1970-11-18 Mtu Muenchen Gmbh A bearing assembly
DE2242852A1 (de) * 1972-08-31 1974-03-14 Motoren Turbinen Union Vorrichtung zur weichen und elastischen lagerung hochtourig umlaufender wellen
JPS5142214B2 (fr) * 1972-12-16 1976-11-15
US4548366A (en) * 1982-05-17 1985-10-22 Rieter Machine Works, Ltd. Chuck drive system
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JPH028102Y2 (fr) * 1985-02-07 1990-02-27
GB8524303D0 (en) * 1985-10-02 1985-11-06 Rieter Ag Maschf Chuck structures
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DE3780188T3 (de) * 1986-02-20 2001-06-21 Toray Industries Spulmaschine.
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EP0272458B1 (fr) * 1986-12-02 1991-08-14 Maschinenfabrik Rieter Ag Dispositif de lancement
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FR2664620A1 (fr) * 1990-07-12 1992-01-17 Schlumberger Cie N Dispositif de montage des broches de continus a filer sur le banc porte-broches.
JP2505140B2 (ja) * 1991-12-05 1996-06-05 村田機械株式会社 紡糸巻取機
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Title
See references of WO9501516A1 *

Also Published As

Publication number Publication date
US5649670A (en) 1997-07-22
WO1995001516A1 (fr) 1995-01-12
JPH08500889A (ja) 1996-01-30

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