WO2011154745A2 - Noyau d'enroulement de toile - Google Patents

Noyau d'enroulement de toile Download PDF

Info

Publication number
WO2011154745A2
WO2011154745A2 PCT/GB2011/051084 GB2011051084W WO2011154745A2 WO 2011154745 A2 WO2011154745 A2 WO 2011154745A2 GB 2011051084 W GB2011051084 W GB 2011051084W WO 2011154745 A2 WO2011154745 A2 WO 2011154745A2
Authority
WO
WIPO (PCT)
Prior art keywords
web
winding core
core according
fibres
filler
Prior art date
Application number
PCT/GB2011/051084
Other languages
English (en)
Other versions
WO2011154745A3 (fr
Inventor
Steven John Morgan
Original Assignee
Composite Core Technologies Ltd
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 Composite Core Technologies Ltd filed Critical Composite Core Technologies Ltd
Priority to EP11728653.4A priority Critical patent/EP2616375B1/fr
Publication of WO2011154745A2 publication Critical patent/WO2011154745A2/fr
Publication of WO2011154745A3 publication Critical patent/WO2011154745A3/fr

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H75/00—Storing webs, tapes, or filamentary material, e.g. on reels
    • B65H75/02—Cores, formers, supports, or holders for coiled, wound, or folded material, e.g. reels, spindles, bobbins, cop tubes, cans, mandrels or chucks
    • B65H75/04—Kinds or types
    • B65H75/08—Kinds or types of circular or polygonal cross-section
    • B65H75/10—Kinds or types of circular or polygonal cross-section without flanges, e.g. cop tubes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H75/00—Storing webs, tapes, or filamentary material, e.g. on reels
    • B65H75/02—Cores, formers, supports, or holders for coiled, wound, or folded material, e.g. reels, spindles, bobbins, cop tubes, cans, mandrels or chucks
    • B65H75/18—Constructional details
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H75/00—Storing webs, tapes, or filamentary material, e.g. on reels
    • B65H75/02—Cores, formers, supports, or holders for coiled, wound, or folded material, e.g. reels, spindles, bobbins, cop tubes, cans, mandrels or chucks
    • B65H75/18—Constructional details
    • B65H75/185—End caps, plugs or adapters
    • B65H75/187—Reinforcing end caps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H75/00—Storing webs, tapes, or filamentary material, e.g. on reels
    • B65H75/50—Methods of making reels, bobbins, cop tubes, or the like by working an unspecified material, or several materials
    • 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
    • B65H2701/50—Storage means for webs, tapes, or filamentary material
    • B65H2701/51—Cores or reels characterised by the material
    • B65H2701/512—Cores or reels characterised by the material moulded
    • B65H2701/5122—Plastics
    • 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
    • B65H2701/50—Storage means for webs, tapes, or filamentary material
    • B65H2701/51—Cores or reels characterised by the material
    • B65H2701/512—Cores or reels characterised by the material moulded
    • B65H2701/5126—Particles of fibres, e.g. lignocelluloses material
    • 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
    • B65H2701/50—Storage means for webs, tapes, or filamentary material
    • B65H2701/51—Cores or reels characterised by the material
    • B65H2701/513—Cores or reels characterised by the material assembled mainly from rigid elements of the same kind
    • B65H2701/5136—Moulded plastic elements
    • 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
    • B65H2701/50—Storage means for webs, tapes, or filamentary material
    • B65H2701/51—Cores or reels characterised by the material
    • B65H2701/515—Cores or reels characterised by the material assembled from parts made of different materials
    • 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
    • B65H2701/50—Storage means for webs, tapes, or filamentary material
    • B65H2701/51—Cores or reels characterised by the material
    • B65H2701/515—Cores or reels characterised by the material assembled from parts made of different materials
    • B65H2701/5152—End flanges and barrel of different material
    • B65H2701/51528—Plastic barrel

Definitions

  • This invention relates to a web-winding core. It has particular, but not exclusive, application to a web-winding core for use with a lightweight material, such as tissue paper.
  • those cores described above that are intended for use with newsprint have far greater strength, and are therefore heavier and more costly, than is necessary for use with a lightweight web. They are also not well-suited to production of cores with the larger diameters (150 mm or more) typically used for tissue. Excess weight of these cores mean that a core may weigh more than an equivalent cardboard core, which can cause manual handling issues..
  • An aim of this invention is to provide a web-winding core that is better optimised for use with a lightweight web material such as tissue paper, and which is no heavier than a cardboard core that it will replace.
  • the invention provides a web-winding core formed as a hollow cylindrical shell, the shell being a three-layered sandwich comprising inner and outer skins, between which is a filler to which the inner and outer skins are bonded.
  • the core can be sufficiently strong for use as a core for a lightweight web, and which is of a sufficiently low density that the core is not heavier than a conventional cardboard core.
  • a cardboard core has a typical density of 0.75xl0 3 - 0.85xl0 3 kgm 3 .
  • Embodiments of the present invention can typically save 10-15% of this. (A greater or lesser saving may be achieved while still gaining the advantage of the invention.)
  • the cores have the advantage over cardboard that they are resistant to damage from water, and so can be stored outside.
  • the inner and outer layers may be of similar construction and composition.
  • the inner and/or the outer skin may be formed from a reinforced composite material.
  • a preferred form of construction for the inner and outer skins comprises reinforcing fibres disposed within a matrix.
  • the reinforcing fibres may comprise one or more of organic, inorganic or metallic materials and may be applied as preformed fabrics, short fibre fabrics or continuous orientated fibres.
  • the fibres may be incorporated into a ballistic fabric. Fibres of aramid are particularly preferable for its resistance to cutting and abrasion. It is also highly desirable to make the core highly resistant to damage low-speed impacts. To this end, fibres of ultra-high molecular weight polyethylene are particularly suitable, because they have a high impact resistance, and resist adhesion from the matrix, which acts to disperse the energy of impact against the core.
  • the fibres may be dry or may be pre-impregnated with an appropriate uncured polymer.
  • the matrix is typically a thermoset or thermoplastic polymer compound that is capable of a high degree of elongation.
  • it may be a modified polyester resin which has a urethane acrylate additive.
  • the inner and/or outer layer may be formed from a natural material or plant origin, such as a hemp fibre.
  • the filler of the tube is formed from a cellular or foam material.
  • a high proportion of the core will be void space formed either by the use of cellular materials with entrapped air, or low density 3D woven fabrics. This achieves low overall density of the tube wall construction.
  • the filler may be formed from a low-density natural material, such as balsa or cork.
  • a wide range of alternative filler materials can be used, with an aim of achieving a density within the core of 0.3-0.6xl0 3 kgm
  • An example is foamed PET formed as a lightweight 3-dimensional core.
  • the filler is bonded to the inner and outer layers so that the filler transmits stresses between the inner and the outer layers. Where the inner and/or outer layer is a composite material, the filler may be partially or wholly impregnated with the matrix of the inner and/or outer layers to form a strong bond between them, by effectively unifying the three layers of the wall.
  • the resin system proposed for the core tubes is a high grade modified polyester resin which has a urethane acrylate additive to impart very good impact resistant properties to the tube. This has already been extensively trialled in the resin transfer moulding process and gives very good cycle times and product quality.
  • a ring of impact-resistant material e.g., metal, such as steel, or a plastic material such as urethane polymer, may be provided at an end portion of the core to resist damage to the core, for example as might occur though impact.
  • the ring will typically be bonded to one or both of the inner and the outer layers. Most preferably, the inner and outer diameters of the ring are substantially the same as the respective diameter of the core.
  • the core may include end portions in each of which there is a reinforcing structure that increases the hoop strength of the core.
  • the reinforcing structure may comprises a strengthening tape wound around the inner layer.
  • Figure 1 is a side view of an end portion of a web-winding core being an embodiment of the invention
  • Figure 2 is a cross-section along A-A in Figure 1;
  • Figure 3 is an end view of a mould that can be used in production of the embodiment of Figure 1;
  • Figure 4 is a cross-section along B-B in Figure 3;
  • Figure 5 is a cross-section of a web-winding core being a modification of the embodiment of Figure 1;
  • Figure 6 is a cross-section of a web-winding core being a second modification of the embodiment of Figure 1;
  • Figure 7 is an end view of the embodiment of Figure 6.
  • a core for winding a lightweight web is formed as a generally cylindrical hollow cylindrical tube that is rotationally symmetrical about a longitudinal axis X-X.
  • the outer diameter of the cylinder is typically in the range 150-510mm
  • the wall thickness of the tube is typically in the range 12-20mm.
  • the cylindrical tube is formed with three radially-spaced layers that are disposed coaxially around the axis X-X: an inner layer 12, an outer layer 14 and a low-density reinforcing filler 16 that fills the space between the inner layer 12 and the outer layer 14.
  • the inner and outer layers 12, 14 are bonded to the filler 16 to form a composite sandwich structure.
  • the thicknesses of the inner and outer layers of the wall are typically in the range 1.5-4 mm, and the thickness of the filler is typically in the range 8- 16 mm.
  • the filler 16 serves to link the inner and outer layers 12, 14 and will transmit stresses between the layers 12, 14 to provide a stable structure.
  • the inner and outer layers 12, 14 are formed from reinforcing fibres which are impregnated with, and embedded in, a matrix of thermoset or thermoplastic polymer compound.
  • the fibres are ultra-high molecular weight polyethylene
  • the matrix is a polyester resin which has a urethane acrylate additive
  • the filler is an expanded hexagonal segment PET foam core.
  • the sandwich core portion of the tube is formed from a cellular or foam material which is bonded between the inner and outer skins of the tube and may be partially or wholly impregnated with the polymer matrix compound.
  • a high proportion of the core will be void space formed either by the use of cellular materials with entrapped air, or low density 3D woven fabrics. This is key to achieving low overall density of the tube wall construction.
  • the filler is polyethylene terephthalate (PET) foam formed as flexibly interconnected hexagonal units.
  • the tube wall is formed in layers with internal and external skins containing a reinforcing medium, and a bonded sandwich core portion which is of low density material.
  • the sandwich core serves to link the two skins and will transmit stresses between the skins to provide a stable structure.
  • the skins are formed from reinforcing fibres which are impregnated with, and embedded in, a matrix of thermoset or thermoplastic polymer compound.
  • the reinforcing fibres may be of organic, inorganic or metallic materials and may be applied as preformed fabrics, short fibre fabrics or continuous orientated fibres.
  • the fibres may be dry or may be pre-impregnated with an appropriate uncured polymer as described.
  • This central cylinder 20 is mounted concentrically with an outer metal mould shell 22, with an annular space 24 between the central cylinder 20 and the outer mould shell 22 equal to the design wall-thickness of the finished core tube 10.
  • a highly polished finish is required on this central cylinder and it is treated with a release agent to ensure that the resin will not be able to adhere to the surface.
  • the external mould shell 22 is split along its longitudinal centreline at 30 into two identical half shells which are precisely located relative to each other to form an accurate hollow cylindrical mould shell equal in diameter to the outside diameter of the core tube 10 to be formed.
  • This external mould shell 22 is provided with stiffeners (not shown) to ensure good dimensional stability of the structure, to provide the close dimensional tolerances required in the finished core tube 10.
  • Sealing rings 32 are fitted to the central cylinder at a distance apart which is equal to the required length of the finished core tube 10.
  • the longitudinal seams of the outer mould shell also incorporate airtight seals which are essential to the correct functioning of the mould.
  • a number of resin entry ports 34 and air venting points 36 are incorporated into the outer mould shell 22 to ensure that liquid resin can be introduced into the annular space 24 between the inner cylinder 20 and the outer split mould shell 22, and that air can be vented from the space 24 as the mould is filled.
  • the air may be displaced naturally by the ingress of the resin or a small level of vacuum may be applied through the air vent ports 36 to improve the resin flow into the mould.
  • the inner cylinder 20 is prepared by wrapping a layer of dry fibre fabric onto the surface between the two pre-located sealing rings 32 which determine the overall length of the core tube 10.
  • a dry layer of the selected foam core medium is then applied to cover the inner glass fabric.
  • This foam may be applied in sheets which are thermally preformed or may be applied as a spirally-wound or convolute-wound strip, depending upon the material selected.
  • another layer of dry fibre fabric is applied over the entire surface.
  • the prepared inner cylinder 20 with the dry materials is then located within the lower half of the split external mould 22.
  • the upper half of the external mould 22 is then accurately located onto the lower half mould trapping the internal cylinder 20 and the dry fabric and foam layers into the closed mould space.
  • a resin metering and pumping unit prepares a pre-determined quantity of liquid polyester resin with the appropriate curing agents added, and then pumps this mixed resin into the mould through one or more of the ingress ports 34 on the outer mould surface. Air venting or vacuum may be used to promote the resin flow through the mould and resin is pumped into the mould until all the air is displaced and resin flows from the air venting port 36.
  • Elevated temperature can be advantageous as it will speed up the curing reaction of the resin. Elevated temperature can readily be applied by pumping hot water or oil through the central cylindrical 20 member or by incorporating heating elements within the wall of the mould during construction.
  • the outer mould may be unsealed and split open and the cylindrical inner mould 20 with the laminated core tube may be removed from the assembly.
  • the moulded core tube 10 is then drawn off the internal cylinder with a mechanical or hydraulic pulling device.
  • the finished tube should need minimal second operation works to make it ready for despatch.
  • the possible removal of flash lines along the mould split lines may be necessary.
  • Some applications of cores embodying the invention may favour a textured external and/or internal surface on the core tube. This may be formed directly using the mould itself Alternatively the required internal and external surface textures may be applied by wrapping peel ply or similar textured fabric onto the central cylindrical mould member prior to applying the inner structural fabric layers, and/or onto the outer surface of the external layers of structural fabrics. The texture of the fabric is thereby transferred to the surface of the core. Use of such fabric has an additional advantage, in that it prevents the formation of mould flash, which obviates any need to remove such flash from the moulded core. There is some risk of the core tube edges spalling in the event of severe impact - typically if accidentally dropped during handling operations.
  • a modification to the mould tooling has been incorporated within the initial design to permit a protective body 40 of tough material such as metal or urethane polymer to be bonded or moulded within to an end portion of the core tube 10 to enhance the impact resistance if required, as shown in Figure 5.
  • This may be done by routing a cylindrical groove in an end face of the filler, and forming the protective body 40 by moulding it in situ. The material of the protective body flows into the groove to retain the protective body 40 in place.
  • the groove may be formed with a dovetail shape, as shown in the lower half of Figure 5.
  • the protective body 40 has a cylindrical locating portion 42 that is a close fit between the inner and the outer layers 12, 14. An end portion of each of the inner and outer layers 12, 14 projects beyond the end of the filler 16 to accommodate the locating portion 42, which is bonded to them.
  • the protective body projects beyond the inner and outer layers 12, 14, and has an outer diameter that is substantially the same as that of the core tube 10.
  • the protective body 40 has an axial through bore that has a diameter that is substantially the same as the inner diameter of the core tube 10. This arrangement ensures that the core as a whole has a substantially uniform inner and outer diameter along its length.
  • An outer portion of the bore of the protective body, shown at 44, is chamfered to provide a lead-in to assist the insertion of handling apparatus into the bore of the core.
  • additional strengthening can be applied to resist bursting of end portions of the core tube 10.
  • the aim is to increase the hoop strength of the core tube 10 at a region close to each of its ends. This is achieved in the present embodiment by omitting the filler 16 from a region at the end of the core tube 10 approximately 50 mm in length.
  • the inner layer 12 is encircled by a strengthening band 44 to the same depth as the filler 16.
  • the strengthening band 44 is formed from unidirectional glass tape, which has high tensile strength along its length.
  • several slots 50 are formed into the annular end surface of the strengthening band 44 that is exposed at the end of the core tube 10.
  • an entry hole is formed of 9mm diameter and 12 mm depth at a radius of approximately 212 mm from the centre of the core tube 10.
  • the slot 50 is formed with a parallel cutter 6 or 7 mm in diameter, extending from the entry hole in an arc centred on the centre of the core tube 10.
  • the slot 50 is then expanded with a dovetail cutter.
  • the dovetail cutter enters the entry hole and moves along the previously formed slot.
  • the dovetail cutter expands the slot such that it is approximately 7 mm in with at the surface and 9 mm in the base.
  • the circumferential length of each slot is approximately 40 mm, and they are spaced apart by approximately 10 mm.

Landscapes

  • Laminated Bodies (AREA)
  • Storage Of Web-Like Or Filamentary Materials (AREA)

Abstract

L'invention concerne un noyau d'enroulement de toile formé d'une enveloppe cylindrique creuse, l'enveloppe étant composée d'un sandwich trois couches comprenant une peau intérieure et une peau supérieure fixées à une couche de remplissage entre elles. La couche de remplissage peut être un matériau léger naturel tel que du balsa ou du liège ou une mousse polymère artificielle. Les peaux intérieure et extérieure peuvent être constituées d'une résine renforcée. Le renforcement peut être en fibres naturelles ou artificielles.
PCT/GB2011/051084 2010-06-11 2011-06-10 Noyau d'enroulement de toile WO2011154745A2 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP11728653.4A EP2616375B1 (fr) 2010-06-11 2011-06-10 Noyau d'enroulement de toile

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB1009779.8A GB2481058A (en) 2010-06-11 2010-06-11 Three layered web-winding core
GB1009779.8 2010-06-11

Publications (2)

Publication Number Publication Date
WO2011154745A2 true WO2011154745A2 (fr) 2011-12-15
WO2011154745A3 WO2011154745A3 (fr) 2012-02-23

Family

ID=42471491

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/GB2011/051084 WO2011154745A2 (fr) 2010-06-11 2011-06-10 Noyau d'enroulement de toile

Country Status (3)

Country Link
EP (1) EP2616375B1 (fr)
GB (1) GB2481058A (fr)
WO (1) WO2011154745A2 (fr)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103130039A (zh) * 2013-02-19 2013-06-05 桐乡市德盛纸业有限公司 泥浆复合纸管及其制造方法
WO2015120387A1 (fr) * 2014-02-07 2015-08-13 Aep Industries Inc. Manchon cylindrique
US9731932B2 (en) 2014-02-07 2017-08-15 Berry Global Films, Llc Cylindrical sleeve
RU2661819C1 (ru) * 2014-12-19 2018-07-19 ЭсСиЭй ТИШЬЮ ФРАНС Разрываемый сердечник, рулон, содержащий такой сердечник, и способ изготовления такого разрываемого сердечника
EP3663247A1 (fr) * 2018-12-06 2020-06-10 Double E Company LLC Protecteur d'extrémité de noyau d'enroulement

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10843892B2 (en) * 2017-09-12 2020-11-24 Michael Van Deurse Winding core end protector

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3105828A1 (de) 1981-02-18 1982-09-02 Paul & Co Inh. K. Kunert & Söhne GmbH & Co, 8789 Wildflecken Papierhuelse als wickelkern fuer extrem duennes bahnfoermiges wickelgut
DE29612786U1 (de) 1996-07-24 1996-09-19 Voith Sulzer Papiermasch Gmbh Wickelkern für eine Wickelmaschine
DE202009017716U1 (de) 2009-12-22 2010-04-08 Paul Sauer Gmbh & Co. Walzenfabrik Kg Wickelhülse mit Beschichtung

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US3451639A (en) * 1966-07-12 1969-06-24 Dyson Kissner Corp Textile tube
CH478706A (it) * 1967-05-12 1969-09-30 Steffenini Francesco Corpo sopportatore per filati
US3666589A (en) * 1968-07-01 1972-05-30 Teledyne Inc Method for making industrial rolls
DE3733731A1 (de) * 1987-10-06 1989-04-27 Messerschmitt Boelkow Blohm Antriebswelle
DE8907321U1 (de) * 1989-06-15 1991-03-28 Chlupsa, Otto, 6070 Langen Rohr, insbesondere Umlenkwelle, Expansionswelle o.dgl.
JP2799788B2 (ja) * 1991-08-28 1998-09-21 富士写真フイルム株式会社 ロール状写真フイルムの巻取芯及び巻取体
LU88074A1 (fr) * 1992-02-24 1992-08-25 Kleykamp Stephen Mandrins anneles en plastique
JPH06239533A (ja) * 1993-02-12 1994-08-30 Tenryu Ind Co Ltd 巻取りコア
DE19507514C2 (de) * 1995-03-03 1997-09-25 Alcan Gmbh Metallene Wickelhülse
JPH09300488A (ja) * 1996-05-13 1997-11-25 Oji Kako Kk 二重紙管及びその製造方法
JP4158100B2 (ja) * 2002-07-04 2008-10-01 ゲイツ・ユニッタ・アジア株式会社 紡糸用スリーブ
DE102008025580A1 (de) * 2008-05-28 2009-12-03 Tesa Se Wickelkern für Klebebänder

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3105828A1 (de) 1981-02-18 1982-09-02 Paul & Co Inh. K. Kunert & Söhne GmbH & Co, 8789 Wildflecken Papierhuelse als wickelkern fuer extrem duennes bahnfoermiges wickelgut
DE29612786U1 (de) 1996-07-24 1996-09-19 Voith Sulzer Papiermasch Gmbh Wickelkern für eine Wickelmaschine
DE202009017716U1 (de) 2009-12-22 2010-04-08 Paul Sauer Gmbh & Co. Walzenfabrik Kg Wickelhülse mit Beschichtung

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103130039A (zh) * 2013-02-19 2013-06-05 桐乡市德盛纸业有限公司 泥浆复合纸管及其制造方法
CN103130039B (zh) * 2013-02-19 2016-12-28 桐乡市德盛纸业有限公司 泥浆复合纸管及其制造方法
WO2015120387A1 (fr) * 2014-02-07 2015-08-13 Aep Industries Inc. Manchon cylindrique
US9481536B2 (en) 2014-02-07 2016-11-01 Aep Industries Inc. Cylindrical sleeve
US9731932B2 (en) 2014-02-07 2017-08-15 Berry Global Films, Llc Cylindrical sleeve
US10087037B2 (en) 2014-02-07 2018-10-02 Berry Global Films, Llc Cylindrical sleeve
RU2661819C1 (ru) * 2014-12-19 2018-07-19 ЭсСиЭй ТИШЬЮ ФРАНС Разрываемый сердечник, рулон, содержащий такой сердечник, и способ изготовления такого разрываемого сердечника
EP3663247A1 (fr) * 2018-12-06 2020-06-10 Double E Company LLC Protecteur d'extrémité de noyau d'enroulement

Also Published As

Publication number Publication date
EP2616375B1 (fr) 2016-02-10
EP2616375A2 (fr) 2013-07-24
GB2481058A (en) 2011-12-14
GB201009779D0 (en) 2010-07-21
WO2011154745A3 (fr) 2012-02-23

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