CA2552009C - Forming fabric for use in a paper machine, and method and apparatus for manufacturing such a forming fabric - Google Patents

Forming fabric for use in a paper machine, and method and apparatus for manufacturing such a forming fabric Download PDF

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Publication number
CA2552009C
CA2552009C CA002552009A CA2552009A CA2552009C CA 2552009 C CA2552009 C CA 2552009C CA 002552009 A CA002552009 A CA 002552009A CA 2552009 A CA2552009 A CA 2552009A CA 2552009 C CA2552009 C CA 2552009C
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Prior art keywords
yarns
forming fabric
laser
another
fused
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Application number
CA002552009A
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French (fr)
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CA2552009A1 (en
Inventor
Walter Best
Christian Molls
Paul Wales
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Heimbach GmbH and Co KG
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Heimbach GmbH and Co KG
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Publication of CA2552009A1 publication Critical patent/CA2552009A1/en
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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/729Textile or other fibrous material made from plastics
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/14Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
    • B29C65/16Laser beams
    • B29C65/1629Laser beams characterised by the way of heating the interface
    • B29C65/1654Laser beams characterised by the way of heating the interface scanning at least one of the parts to be joined
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/344Stretching or tensioning the joint area during joining
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/69General aspects of joining filaments 
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/73General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/739General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/7392General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic
    • B29C66/73921General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic characterised by the materials of both parts being thermoplastics
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/80General aspects of machine operations or constructions and parts thereof
    • B29C66/83General aspects of machine operations or constructions and parts thereof characterised by the movement of the joining or pressing tools
    • B29C66/836Moving relative to and tangentially to the parts to be joined, e.g. transversely to the displacement of the parts to be joined, e.g. using a X-Y table
    • DTEXTILES; PAPER
    • D21PAPER-MAKING; PRODUCTION OF CELLULOSE
    • D21FPAPER-MAKING MACHINES; METHODS OF PRODUCING PAPER THEREON
    • D21F1/00Wet end of machines for making continuous webs of paper
    • D21F1/0027Screen-cloths
    • DTEXTILES; PAPER
    • D21PAPER-MAKING; PRODUCTION OF CELLULOSE
    • D21FPAPER-MAKING MACHINES; METHODS OF PRODUCING PAPER THEREON
    • D21F1/00Wet end of machines for making continuous webs of paper
    • D21F1/0027Screen-cloths
    • D21F1/0054Seams thereof
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C35/00Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
    • B29C35/02Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
    • B29C35/08Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation
    • B29C35/0805Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation using electromagnetic radiation
    • B29C2035/0822Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation using electromagnetic radiation using IR radiation
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/14Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
    • B29C65/16Laser beams
    • B29C65/1603Laser beams characterised by the type of electromagnetic radiation
    • B29C65/1612Infrared [IR] radiation, e.g. by infrared lasers
    • B29C65/1616Near infrared radiation [NIR], e.g. by YAG lasers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/14Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
    • B29C65/16Laser beams
    • B29C65/1677Laser beams making use of an absorber or impact modifier
    • B29C65/1683Laser beams making use of an absorber or impact modifier coated on the article
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/721Fibre-reinforced materials
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/73General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/739General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/7392General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2101/00Use of unspecified macromolecular compounds as moulding material
    • B29K2101/12Thermoplastic materials
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2313/00Use of textile products or fabrics as reinforcement
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/14Filters

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Toxicology (AREA)
  • Health & Medical Sciences (AREA)
  • Electromagnetism (AREA)
  • Optics & Photonics (AREA)
  • Textile Engineering (AREA)
  • Treatment Of Fiber Materials (AREA)
  • Paper (AREA)
  • Chemical Or Physical Treatment Of Fibers (AREA)
  • Filtering Materials (AREA)
  • Making Paper Articles (AREA)
  • Yarns And Mechanical Finishing Of Yarns Or Ropes (AREA)

Abstract

The present invention relates to a forming fabric, for use in the sheet-forming section of a paper machine, having or consisting of a textile planar structure which consists of longitudinal and transverse yarns and in which, in order to enhance inherent stability, crossing yarns are engaged into one another at crossing points and in which yarns additionally are fused to one another, wherein the planar structure comprises intersecting first and second yarns, wherein only some of the longitudinal and/or transverse yarns are first yarns, the first yarns having the property that they absorb laser energy and can be brought, by absorbed laser energy, to melting temperature at least at the surface, and that the second yarns absorb less laser energy than the first yarns or none at all and that first and second yarns are fused to one another at at least some of their crossing points. An advantage consists in the fact that the dimensional stability can be individually adapted to particular requirements by correspondingly varying the number of first yarns as well as the number of intersection points at which welding or fusing is performed.

Description

Forming fabric for use in a paper machine, and method and apparatus for manufacturing such a forming fabric The invention relates to a forming fabric, for use in the sheet-forming section of a paper machine, having or comprising a textile planar structure in which intersecting yarns are engaged into one another at intersection points and in which, in order to enhance inherent stability, yarns are fused to one another at intersection points. The invention further relates to a method for manufacturing such forming fabrics, in which method a textile planar structure is manufactured from yarns that intersect one another and are engaged into one another at intersection points, and in which yarns are then fused to one another at intersection points by heating to melting temperature. Lastly, the invention also refers to an apparatus for manufacturing a forming fabric of this kind.

Forming fabrics are long, wide belts that circulate in the first part of a paper machine, called the sheet-forming section, forming a flat upper run. At the beginning of the upper run, the previously prepared fiber pulp is applied onto the forming fabric and dewatered through the forming fabric, so that a paper web still having a high liquid content is gradually formed. In subsequent sections of the paper machine, the paper web is further dewatered mechanically and thermally.

Single- or multiple-ply woven fabrics are generally used as forming fabrics. A woven fabric (or even a knitted fabric) obtains its inherent stability or diagonal stability from the fact that intersecting yarns are engaged into one another, forming a weave pattern. Particularly in the context of large stresses such as those that occur in a paper machine, the inherent stability of the textile planar '70233-146 structure is not sufficient to ensure stable and problem-free circulation of the forming fabric through the sheet-forming section. Additional measures have therefore been taken in order to improve the dimensional stability, in particular the diagonal stiffness, of such textile planar structures.

One of these measures consists in adhesively bonding the yarns to one another at the intersection points, by the fact that the fabric structure is equipped with adhesive polymers. This method is cost-intensive because the dispersion must be applied very evenly, and because drying consumes a great deal of time and energy.
Permeability is furthermore considerably decreased, which has a negative effect on the sheet-forming process. A
further disadvantage is the fact that the adhesion at all intersection points resulting from this method causes a stiffening that is often not desired.

US 5,888,915 A proposes, in order to improve the dimensional stability of such textile planar structures, to use bicomponent yarns in which the melting temperature of the outer casing is lower than that of the core. A woven or knitted fabric or yarn layer equipped with bicomponent yarns of this kind is then heated, in a continuous furnace, to a temperature that is above the melting temperature of the outer casing of the bicomponent yarns, but below the melting temperature of the core of those yarns, so that the casing melts and a fused or adhesive bond to other yarns is produced in this fashion at the intersection points.

Forming fabrics having good dimensional stability can be manufactured using this method. Manufacture is costly, however, since the bicomponent yarns are expensive, and heating of the entire forming fabric in a continuous furnace is energy-intensive.

Also known are forming fabrics having or comprising a textile planar structure that is formed from a yarn layer in which the yarns are not engaged with one another, i.e. not woven or interlinked with one another.
Instead, transverse yarns that extend parallel to and at a distance from one another are laid onto a layer of longitudinal yarns that are likewise parallel to and at a distance from one another, and the longitudinal yarns are then joined to the transverse ones. Only thereby does the yarn layer acquire inherent stability. Joining can occur according to the method according to US 5,888,915 A, using bicomponent yarns.

The disadvantages of the aforementioned method are eliminated by a method that is evident from EP 1 359 251 Al.
In this method, the longitudinal and transverse yarns are fused to one another at intersection points as a consequence of a heating to melting temperature that is confined to those intersection points. The heating can be applied in single-point fashion by means of high-frequency, inductive, and/or laser energy. As an alternative thereto, however, the energy can also be applied in planar fashion if the intersection points are first equipped with an additive that promotes absorption of the energy and that concentrates energy uptake at the intersection points despite the planar application, so that only those points are heated to melting temperature and consequently fused to one another. When a laser is used, the additive should be a light-absorbing dye, e.g. black dye, or a photoactive substance. The additive can be applied between the yarns or onto the yarns. It is also proposed instead to add the additive to the yarn material during the extrusion operation.
It is an aspect of the invention to manufacture a forming fabric of the kind cited initially more economically, preferably without producing structural changes. A further object is to make available a method suitable for manufacture, and an apparatus therefor.

The invention relates to a forming fabric, for use in the sheet-forming section of a paper machine, having or consisting of a textile planar structure which consists of longitudinal and transverse yarns and in which, in order to enhance inherent stability, crossing yarns are engaged into one another at crossing points and in which yarns additionally are fused to one another, wherein the planar structure comprises intersecting first and second yarns, wherein only some of the longitudinal and/or transverse yarns are first yarns, the first yarns having the property that they absorb laser energy and can be brought, by absorbed laser energy, to melting temperature at least at the surface, and that the second yarns absorb less laser energy than the first yarns or none at all and that first and second yarns are fused to one another at at least some of their crossing points.

The invention also relates to a method for manufacturing a forming fabric for use in the sheet-forming section of a paper machine, in which method a textile planar structure is manufactured from longitudinal and transverse yarns that cross one another and are engaged into one another, and in which yarns are fused to one another at crossing points by heating to melting temperature, wherein first and second yarns are used in the manufacture of the planar structure, in which context the first yarns can absorb laser energy and for the second yarns yarns are used that absorb less laser energy than the first yarns or none at all, and that only some of the longitudinal and/or '70233-146 transverse yarns are first yarns and that first and second yarns are fused by means of laser energy at at least some of their crossing points.

According to the present invention, there is a 5 forming fabric in which the planar structure comprises intersecting first and second yarns, the first yarns having the property that they absorb laser energy and can be brought, by absorbed laser energy, to melting temperature at least at the surface; and in which first and second yarns are fused to one another at at least some of their intersection points. For many situations it is sufficient if only some of the first and second yarns are welded to one another, and those only at some of their intersection points.

The basic idea of the invention is therefore to use for some of the yarns, in the context of a forming fabric, particular yarns which are distinguished by the fact that they absorb laser light. In this fashion, the textile planar structure can be additionally stabilized by the fact that the first yarns are heated by means of a laser to melting temperature, and at at least some of the intersection points (if not at all) a fused join is thus produced with the second yarns, which absorb only little or no laser light. This manner of producing the fused join is substantially less time-consuming and energy-intensive than the known methods, especially since the first yarns themselves require little additional cost. A further advantage consists in the fact that the dimensional stability can be individually adapted to particular requirements by correspondingly varying the number of first yarns as well as the number of intersection points at which welding or fusing is performed. This is because in many cases, a forming fabric that is too stiff and therefore insufficiently adaptable is also disadvantageous.

In an embodiment of the invention, provision is made for the yarns otherwise not to be joined to one another, i.e. for no further join to exist beyond the mutual engagement of the yarns and their single-point welding at intersection points.

To allow the first yarns to absorb the laser light, they can contain an additive that imparts the ability to absorb laser light. Examples of such additives are near-infrared-active (NIR-active) substances that absorb, for example, in the region of the wavelengths 808 nm, 940 nm, 980 nm, or 1064 nm. Suitable for this are, for example, carbon or colorless additives such as Gentex's Clearweld or BASF's Lumogen IR. The additive preferably extends over the entire length of the first yarns and is evenly distributed over the length and cross section. The additive can be incorporated into the first yarns and/or applied onto the surface of the first yarns and/or introduced at the intersection points between the first and second yarns. If the additive is incorporated, the proportions by weight should be approximately 0.10% to 2.5%.

In a further embodiment of the invention, provision is made for the first yarns to be bicomponent yarns, only one of the two components containing the additive. The bicomponent yarns should preferably comprise a core and a casing surrounding it, the additive then being contained only in the casing.

Planar structures suitable according to the present invention are those in which intersecting yarns are engaged with one another, as is the case, for example, with woven and knitted fabrics. The planar structure should preferably comprise longitudinal and transverse yarns, in which context the first yarns can extend only in the longitudinal direction, only in the transverse direction, or in both directions. Depending on the dimensional stability requirements, only some of the longitudinal and/or transverse yarns can then also be embodied as first yarns.
The first yarns should preferably be part of the weave of the yarns in the planar structure, i.e. should not have been additionally introduced into the existing woven fabric, knitted fabric, etc., in order not to disrupt the desired yarn distribution and structure. It is definitely useful if the first yarns are distributed in the planar structure in a consistently regular pattern.

The first yarns are, if possible, advantageously engaged into the planar structure in such a way that they do not reach as far as the paper side of the forming fabric.
If the planar structure is embodied with multiple plies, the first yarns should be engaged only in an internally located ply and/or a roller-side ply.

Possible materials for the yarns are any type of thermoplastic material that is suitable for the respective application, i.e. that permanently withstands the respective ambient conditions in the paper machine. For cost reasons, at least the first yarns, but better yet all the yarns, can be embodied as single-component yarns that can additionally be fiber-reinforced; i.e. individual yarns, or all the yarns, can contain a fiber reinforcement.

Forming fabrics have a finite length, with ends joinable via a seam. In the region of the two ends, i.e. in the seam region, first yarns should be present that extend in the transverse direction and are welded to second yarns extending in the longitudinal direction. In order to achieve particularly high strength there, the first yarns should be present in a higher concentration in the seam region than in the remaining region of the forming fabric, and the first and second fabrics should be welded to one another at as many intersection points as possible. The longitudinal yarns inserted in correctly woven fashion into the respectively opposite end during the stitching process are then fused to the first yarns. This creates the possibility of shortening the seam region without thereby impairing the strength of the seam. In this fashion the seam region can be reduced from a usual extension of, for example, 100 mm in the longitudinal direction to, for example, 60 mm, i.e. the seam region can be shortened by 20-60% in the machine direction.

A laser beam that has a power output of 20 to 200 W, preferably 50 to 150 W, should be used for welding.

The second object is achieved, according to the invention, by a method in which first and second yarns are used in the manufacture of the planar structure, in which context the first yarns can absorb laser energy; and in which first and second yarns are fused by means of laser energy at at least some of their intersection points or at all their intersection points.

Welding of the first and second yarns at the intersection points can occur in a consistently regular pattern, but also in stochastically distributed fashion.
The possibility exists of guiding the laser over the forming fabric in parallel longitudinal tracks, the laser and forming fabric being moved relative to one another in the longitudinal direction of the forming fabric by the fact that either the laser is moved two-dimensionally over the forming fabric stretched in stationary fashion, or the forming fabric is moved along in the longitudinal direction below the laser, in which context the laser can additionally be displaced laterally. As an alternative thereto, the possibility exists of guiding the laser over the forming fabric in parallel transverse tracks along a transverse yarn. For this, the forming fabric can be alternately moved and then stopped, so that the laser is guided along every transverse yarn, or even every second, every third, or every tenth transverse yarn.

A further possibility is that of guiding the laser over the forming fabric in a diagonal direction, the anqle bctwccn the diaqonal direction and the transverse dirPnticn being selected so that the first and second yarns are fused to one another at as many intersection points as possible.
The laser can follow the weave ridges of the fabric weave.
The distances between the laser tracks can be selected, in the longitudinal direction, depending on the desired embodiment. Regardless thereof, it is not excluded for the laser to be guided over the forming fabric in spiral tracks.
Provision is also made according to the invention for the laser to be controlled in such a way that it is displaced to those intersection points of first and second yarns designated for joining. For joining, the laser first shines through the second yarn before striking the first yarn. The concentration of the additive in the first yarns, and the energy of the laser, should be correlated in such a way that the first yarns are melted only at the surface facing toward the laser, so that there is only a slight negative effect on the structure and shape of the yarns.

The third part of the object is achieved, according to the present invention, by an apparatus that comprises a tensioning device with which the forming fabric, rendered endless, is stretchable; and such that a laser 5 device having at least one laser head is associated with the tensioning device in such a way that at least one laser beam is directable onto the forming fabric in the stretched state; and that the tensioning device and laser device are embodied in such a way that a relative motion is producible 10 between the forming fabric and laser beam. With the aid of this apparatus, first and second yarns can be welded to one another by means of the at least one laser head.

Particularly suitable as a tensioning device are two spaced-apart tensioning rollers with which a longitudinal tension is impartable to the forming fabric pulled onto the tensioning rollers, for example by the fact that the spacing of the tensioning rollers is modifiable.
At least one of the tensioning rollers should be connected to a drive motor in such a way that a forming fabric pulled onto the tensioning rollers can be caused to circulate continuously or in steps, in which context the drive motor can also be embodied reversibly.

According to a further feature of the invention, provision is made for the at least one laser head to be movably guided transversely with respect to the forming fabric pulled onto the tensioning device, and preferably over the entire width of the tensioning device. As an alternative thereto, but preferably in combination therewith, the at least one laser head should also be movably guided longitudinally with respect to the forming fabric pulled onto the tensioning device. This can usefully be done in such a way that the at least one laser head is supported on a guide rail that extends transversely with respect to the forming fabric and is displaceable in the longitudinal direction of the forming fabric, the forming fabric being in each case pulled onto the tensioning device.

In order to allow the relative motions between laser beam and forming fabric, as proposed in accordance with the method according to the present invention, to proceed automatically, a programmable control device should be provided for controlling the tensioning device and laser device and their motors for moving, for example, the tensioning rollers and/or the laser head. This control device can additionally be combined with a sensor that is mounted on the laser device and serves to sense yarns of the forming fabric that differ from the other yarns of the forming fabric in terms of a property that can be sensed by the sensor. The sensor can be, for example, an optoelectronic sensor (photocell) if the first yarns of the forming fabric according to the present invention have a different color and/or a different brightness from the second yarns. It is also possible, however, to use a sensor that responds to the presence of the additive in the first yarns that imparts the ability to absorb laser light. In conjunction with the control device, the sensor allows the first yarns to be located, and allows the laser to be moved to the locations designated for welding.

The invention is illustrated in more detail in the drawing, with reference to an exemplifying embodiment. The drawing shows, in an oblique view, an apparatus for partial manufacture of forming fabric 2 according to the present invention.

Forming fabric 2 was previously woven in a finite length, and its ends were then stitched to one another so that an endless structure was produced. Forming fabric 2 was then stretched between two rollers 3, 4 arranged at a distance from one another, one of the rollers being movably guided in such a way that forming fabric 2 acquires a specific longitudinal tension. At least one of rollers 3, 4 is driven clockwise in motorized fashion. Upon activation of the drive system, forming fabric 2 is moved at a predetermined speed in the direction of arrow A, while rollers 3, 4 execute a rotary motion in the direction of arrow B, C. It is understood that rollers 3, 4 are supported in an apparatus frame (not depicted in further detail) in which the drive system is also housed.
Forming fabric 2 was manufactured in a finite length, and was converted into the endless form shown by way of a seam joining the ends. Formi.ng fahrin 2 is madP of a woven fabric that, in this embodiment, comprises longitudinal yarns (labeled 5 by way of example) extending in the machine direction (arrow A) and transverse yarns (labeled 6 by way of example) extending perpendicular thereto. Longitudinal and transverse yarns 5, 6 are produced from a thermoplastic that is usual for use in forming fabrics, and constitute second yarns for purposes of the present description. Longitudinal and transverse yarns 5, 6 are engaged into one another in accordance with a specific weave pattern.

Extending between each two transverse yarns 6 .constituting second yarns is a respective further transverse yarn (labeled 7 by way of example) that is emphasized in the drawing. Transverse yarns 7 are engaged into longitudinal yarns 5 and are part of the weave pattern. They constitute first yarns for purposes of the present description. They contain an additive that makes them capable of absorbing laser energy, so that they can be brought to melting temperature with the aid of a laser beam.
A laser apparatus 8 is arranged above the plane of rollers 3, 4. Laser apparatus 8 has longitudinal rails 9, (depicted only in shortened fashion here) that extend, parallel to one another, parallel to the plane of rollers 3, 5 4 and above them, and are immovably joined to the apparatus frame. Longitudinal rails 9, 10 have a spacing that is larger than the width of forming fabrics 2 that are to be processed in apparatus 1.

Mounted displaceably in the directions of double 10 arrow D on longitudinal rails 9, 10 is a transverse rail 11.
It extends perpendicular to longitudinal rails 9, 10 and thus parallel to the axes of rollers 3, 4. Mounted on transverse rail 11 via an arm 12 is a laser 13, which can be displaced back and forth on transverse rail 11 in the directions of double arrow E. It can furthermore be pivoted about the longitudinal axis of transverse rail 11 in the directions of double arrow F. The movement of transverse rail 11 relative to longitudinal rails 9, 10, and the movement of laser head 13 relative to transverse rail 11, are brought about by means of motors (not depicted here in further detail).

Apparatus 1 comprises a programmable control device (likewise not depicted here in further detail), similar to a CNC controller, with which the individual motors for moving laser head 13 and rollers 3, 4 can be controlled, and laser head 13 can be activated. In the example shown, laser head 13 is moved only in the transverse direction via transverse rail 11. Rollers 3, 4 are halted when a first transverse yarn 7 comes to rest below laser head 13. Laser head 13 is then guided along transverse yarn 7 over the width of forming fabric 2, and activated at the positions designated for welding. As a result of the laser energy, transverse yarn 7 heats up at the surface to melting temperature, with the consequence that it fuses to longitudinal yarns 5 at intersection points 14, so that a welded join is produced there after cooling.

Claims (35)

CLAIMS:
1. A forming fabric, for use in the sheet-forming section of a paper machine, having or consisting of a textile planar structure which consists of longitudinal and transverse yarns and in which, in order to enhance inherent stability, crossing yarns are engaged into one another at crossing points and in which yarns additionally are fused to one another, wherein the planar structure comprises intersecting first and second yarns, wherein only some of the longitudinal and/or transverse yarns are first yarns, the first yarns having the property that they absorb laser energy and can be brought, by absorbed laser energy, to melting temperature at least at the surface, and that the second yarns absorb less laser energy than the first yarns or none at all and that first and second yarns are fused to one another at at least some of their crossing points.
2. The forming fabric according to Claim 1, wherein the first and second yarns are fused to one another at all their crossing points.
3. The forming fabric according to Claim 1 or 2, wherein the yarns are otherwise not joined to one another.
4. The forming fabric according to any one of Claims 1 to 3, wherein the first yarns contain an additive that imparts the ability to absorb laser light.
5. The forming fabric according to Claim 4, wherein the additive is an NIR-active substance or an NIR-light-absorbing substance.
6. The forming fabric according to Claim 4 or 5, wherein the additive is incorporated into the first yarns and/or applied onto the surface of the first yarns and/or introduced at the intersection points between the first and second yarns.
7. The forming fabric according to any one of Claims 5 to 6, wherein the first yarns are bicomponent yarns, only one of the two components containing the additive.
8. The forming fabric according to Claim 7, wherein the bicomponent yarns comprise a core and a casing surrounding it, the additive being contained only in the casing.
9. The forming fabric according to any one of Claims 1 to 8, wherein the first yarns are part of the weave of the yarns in the planar structure.
10. The forming fabric according to any one of Claims 1 to 9, wherein the first yarns are distributed in the planar structure in a consistently regular pattern.
11. The forming fabric according to any one of Claims 1 to 10, wherein the planar structure is embodied with multiple plies; and the first yarns are engaged only in an internally located ply and/or a roller-side ply, wherein the first yarns do not reach as far as the paper side of the forming fabric.
12. The forming fabric according to any one of Claims 1 to 11, wherein the yarns are at least partially fiber-reinforced.
13. The forming fabric according to any one of Claims 1 to 12, wherein the forming fabric has a finite length with ends joinable via a seam, transverse yarns that are embodied as first yarns being present in the region of both ends.
14. The forming fabric according to Claim 13, wherein the forming fabric comprises longitudinal yarns that extend into the region of the ends and that in the region of the ends are fused to first yarns that extend in the transverse direction.
15. A method for manufacturing a forming fabric for use in the sheet-forming section of a paper machine, in which method a textile planar structure is manufactured from longitudinal and transverse yarns that cross one another and are engaged into one another, and in which yarns are fused to one another at crossing points by heating to melting temperature, wherein first and second yarns are used in the manufacture of the planar structure, in which context the first yarns can absorb laser energy and for the second yarns yarns are used that absorb less laser energy than the first yarns or none at all, and that only some of the longitudinal and/or transverse yarns are first yarns and that first and second yarns are fused by means of laser energy at at least some of their crossing points.
16. The method according to Claim 15, wherein the first and second yarns are fused to one another at all their crossing points.
17. The method according to Claim 15 or 16, wherein the yarns are otherwise not joined to one another.
18. The method according to any one of Claims 15 to 17, wherein first yarns are used that contain an additive that imparts the ability to absorb laser light.
19. The method according to Claim 18, wherein the additive and the wavelength of the laser are coordinated with one another.
20. The method according to any one of Claims 15 to 19, wherein the first yarns are engaged into the planar structure in such a way that they are part of the weave pattern.
21. The method according to any one of Claims 15 to 20, wherein the first yarns are distributed in the planar structure in a consistently regular pattern.
22. The method according to any one of Claims 15 to 21, wherein a multiple-ply planar structure is manufactured, and the first yarns are engaged only in an internally located ply and/or a roller-side ply, wherein the first yarns do not reach as far as the paper side of the forming fabric.
23. The method according to any one of Claims 15 to 22, wherein yarns made of a thermoplastic material are used.
24. The method according to any one of Claims 15 to 23, wherein yarns that are fiber-reinforced are used.
25. The method according to any one of Claims 15 to 24, wherein a laser beam that has a power output of 20 to 200 W, is used.
26. The method according to claim 25, wherein the power output is 50 to 150 W.
27. The method according to any one of Claims 15 to 26, wherein the laser for fusing the first and second yarns is guided over the forming fabric in parallel longitudinal tracks, the laser and forming fabric being moved relative to one another in the longitudinal direction of the forming fabric.
28. The method according to any one of Claims 15 to 27, wherein the laser for fusing the first and second yarns is guided over the forming fabric in parallel transverse tracks.
29. The method according to any one of Claims 15 to 26, wherein the laser for fusing the first and second threads is guided over the forming fabric in a diagonal direction.
30. The method according to Claim 3, wherein the angle between the diagonal direction and the transverse direction is selected so that the first and second yarns are fused to one another at as many crossing points as possible.
31. The method according to Claim 29 or 30, wherein the laser follows the weave ridges of the fabric weave.
32. The method according to any one of Claims 15 to 26, wherein the laser is guided over the forming fabric in spiral tracks.
33. The method according to any one of Claims 15 to 32, wherein the forming fabric is manufactured in finite fashion forming ends, and the forming fabric comprises longitudinal yarns that extend into the region of the ends and in the region of the ends are fused to first yarns that extend in the transverse direction.
34. The method according to Claim 33, wherein in the region of the ends, the first yarns are fused to the longitudinal yarns at all crossing points.
35. The method according to any one of Claims 15 to 34, wherein the laser is controlled in such a way that at the crossing points of first and second yarns, it first shines through the second yarn.
CA002552009A 2005-08-04 2006-07-13 Forming fabric for use in a paper machine, and method and apparatus for manufacturing such a forming fabric Active CA2552009C (en)

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ATE378461T1 (en) 2007-11-15
BRPI0603075B1 (en) 2016-09-27
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BRPI0603075A (en) 2008-03-18
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US20070028997A1 (en) 2007-02-08
CN1908297A (en) 2007-02-07

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