US3109219A - Seam structure for fourdrinier type screen fabric and method of making same - Google Patents

Seam structure for fourdrinier type screen fabric and method of making same Download PDF

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US3109219A
US3109219A US118702A US11870261A US3109219A US 3109219 A US3109219 A US 3109219A US 118702 A US118702 A US 118702A US 11870261 A US11870261 A US 11870261A US 3109219 A US3109219 A US 3109219A
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warp
fabric
end portions
nylon
seam
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US118702A
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Bell John M De
Wesley S Larson
Kevin W Flynn
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Cheney Bigelow Wire Works Inc
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Cheney Bigelow Wire Works Inc
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    • 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
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/48Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
    • B29C65/50Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like
    • B29C65/5057Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like positioned between the surfaces 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
    • B29C66/05Particular design of joint configurations
    • B29C66/10Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/11Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
    • B29C66/112Single lapped joints
    • B29C66/1122Single lap to lap joints, i.e. overlap joints
    • 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
    • B29C66/40General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
    • B29C66/41Joining substantially flat articles ; Making flat seams in tubular or hollow articles
    • B29C66/43Joining a relatively small portion of the surface of said articles
    • B29C66/432Joining a relatively small portion of the surface of said articles for making tubular articles or closed loops, e.g. by joining several sheets ; for making hollow articles or hollow preforms
    • B29C66/4322Joining a relatively small portion of the surface of said articles for making tubular articles or closed loops, e.g. by joining several sheets ; for making hollow articles or hollow preforms by joining a single sheet to itself
    • 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
    • B29C66/40General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
    • B29C66/41Joining substantially flat articles ; Making flat seams in tubular or hollow articles
    • B29C66/43Joining a relatively small portion of the surface of said articles
    • B29C66/432Joining a relatively small portion of the surface of said articles for making tubular articles or closed loops, e.g. by joining several sheets ; for making hollow articles or hollow preforms
    • B29C66/4324Joining a relatively small portion of the surface of said articles for making tubular articles or closed loops, e.g. by joining several sheets ; for making hollow articles or hollow preforms for making closed loops, e.g. belts
    • 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
    • DTEXTILES; PAPER
    • D06TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06HMARKING, INSPECTING, SEAMING OR SEVERING TEXTILE MATERIALS
    • D06H5/00Seaming textile 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
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/48Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
    • B29C65/4805Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the type of adhesives
    • B29C65/481Non-reactive adhesives, e.g. physically hardening adhesives
    • B29C65/482Drying adhesives, e.g. solvent based adhesives
    • 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
    • B29C65/48Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
    • B29C65/4805Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the type of adhesives
    • B29C65/483Reactive adhesives, e.g. chemically curing adhesives
    • 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
    • B29C66/71General 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 composition of the plastics material of the parts to be joined
    • 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
    • B29L2031/733Fourdrinier belts
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S162/00Paper making and fiber liberation
    • Y10S162/904Paper making and fiber liberation with specified seam structure of papermaking belt
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/19Sheets or webs edge spliced or joined

Definitions

  • This invention relates to seam or joint structures, and method of making them, in fourdrinier type screen fabrics, in which the warp elements, at least, are formed of synthetic organic yarns or filaments, or of yarns or filaments containing synthetic organic material such as glass yarns or filaments coated with a synthetic organic material.
  • Fourdrinier type screen fabric is the type of fabric commonly used in paper making machines and is characterized by a relatively fine mesh, an ability to sustain constant movement under tension and flexure in the presence of water and to withstand frictional abrasion.
  • Fourdrinier type fabric has utility for many commercial purposes but finds its principal use in paper making machines, for which, and for other uses, the ends of a length of the screen fabric are seamed or joined together to form an endless belt. It is important that the seam be not only strong enough to sustain the tensile strain imposed thereon in the operation of the machine, but also, in the case of paper makingmachines, that it suificiently conform to the adjacent surfaces of the screen as not to materially affect or objectionably mar the appearance of the surface of the paper product made thereon. If correct drainage is lacking the paper cannot be stripped from the belt in an endless sheet.
  • a further object is to provide a scam, the transverse width of which may be controlled, and if found desirable or necessary, restricted to a width equal to or not substantially greater than, the transverse width of a weft element of the fabric hein'g spliced, the thickness of the seam being similarly subject to control and restriction to a thickness not substantially greater than the overall thickness of the fabric.
  • the above objectives of the invention are attained by forming a relatively narrow transversely extending body of a synthetic organic material of which lapped free end portions of the warp elements, extending from the edges of the fabric to be joined, are at least-an incorporate part, adhesively and/ or cohesively bonded together into a strain resisting unit, having a per-inch tensile strength in the direction of the warp adequately proportional to that of the per-inch strength of the warp assembly, for the use to which the seamed fabric is to be put.
  • FIG. 1 is a longitudinal sectional view, on a greatly enlarged non-exact scale, of the end portions of a length of fourdrinier type fabric, illustrating an initial step in the seaming procedure;
  • FIG. 2 is a view of the end portions, similar to FIG. 1 but showing the end portions prepared for the second step in the seaming procedure;
  • FIG. 3 is a similar view showing the third step
  • FIG. 4 is a fragmentary plan view on a greatly enlarged non-exact scale showing the relative position of the fabric elements in correspondence to that of FIG. 3;
  • FIGS. 5 to 7 are views showing succeeding steps in the seaming operation.
  • FIGS. 8 and 9 illustrate a modification in the procedure.
  • a length of the fourdrinier fabric of the type previously describcd is generally indicated at l, the'non-metallic Warp-filaments being indicated at 2 and the metal shoots or wefts elements at 3.
  • the end portions of the strip which are to be seamed together are annealed or heat treated to remove internal strains from and stabilize the warp material as found necessary.
  • the fabric ends are then trimmed to provide the needed end extension of the warp elements. For the assumed use of the fabric this is conveniently done by trimming along the terminal shoot wire as indicated at 4 and 5.
  • the terminal weft or shoot wires are then removed from each end of the strip leaving end portions 6 and '7 of the warp extending from the strip ends. As shown in FIG.
  • the extending end portions are brought into the general plane of the weft and, as indicated at 8 in FIGS. 2 and 4, are flattened or otherwise shaped at their extreme end portions by swaging or pressure, under heat if found desirable, and cleaned to remove any processing oils, dirt, or other foreign matter.
  • the end portions are then brought into lapped relation as shown in FIG. 4, the extent of overlap not materially exceeding the width of a shoot or weft element of the fabric.
  • the opposed warp elements are substantially aligned and the side edges of the flattened ends of adjacent warp elements are in substantial contact, but alignment of the opposed warp elements is not essential and the sides of the flattened end portions of the adjacent elements may lapeach other, the opposed warp ends in effect interdigitating.
  • the end portions of the strip are held in the position of FIGS. 3 and 4, in any suitable manner as by bars 9 and I 10 which clamp the end portions against a supporting surface, not shown.
  • solute embedding material will depend on the material of which the Warp filaments are formed and is either an effective adhesive there-for oris effectively compatible and miscible therewith to, respectively, elfect either a bonding adhesion between the surfaces of the lapped warp ends, or such superficial intermixing, by the solvent of the solution, as to create a union between the material of the warp ends and also a union of the warp ends and the solute material.
  • Nylon is one of the various synthetic organic materials commonly used for the warp filaments, and is below 3 referred to for one exemplary disclosure of the seaming structure and method of the invention.
  • the warp filaments 2 are formed of nylon, such as nylon 6, a nylon solvent such as phenol, preferably in the form of a solution of nylon in phenol (later more specifically described) is applied in a single or in successive coats to both sides of the fabric at the lapped area of the filament ends by use of a dip pen, or equivalent applicator, as indicated at 12, by stippling in FIG. 6 and in section in FIG. 5.
  • a nylon solvent such as phenol
  • the solution is preferably brought to a temperature of 350 F. and applied as above described. After each application the temperature of the seam area is raised to a temperature suificient to drive oil the solvent, preferably in the range of 350 F. to 375 F. After each of the first two applications pressure (about 5 pounds per lineal inch) may be applied over the seam area, in order to assure that the free end portions 6 and 7 are properly positioned and held in place to assure an adequate flow of the initial coating solution between and around the lapped filament end portions 6 and 7 which define the width of the seam.
  • Phenol softens the nylon of the filaments sufficiently to render it superficially miscible with the nylon of the adjacent coatings, so that the coatings bond to the filaments and to each other without a perceptible or elfective interface between them.
  • the increase of the tem perature following each application of the coating solution dries that coating to leave it in condition to similarly miscibly accept the succeeding coatings.
  • the warp ends 6 and 7 are integrally bonded together into a unitary body 12 with theresin cast from the coatings.
  • lengths of nylon ribbon 13 and 14, each about 4 to 7 mils thick and 15 mils wide are placed 1ongitudinally over and along the outer surfaces of the bonding body 12, as indicated in FIG. 5.
  • the ribbons 13 and 14 are softened with hot phenol (350 F), before being put in place, and the temperature of the seam area again raised to 350 F. to 375 F.
  • the resin of the end portions 6 and 7, the resin of the coating body 12 and of the ribbons 1314 is formed into a substantially homogeneous seam structure as indicated at 15 in FIG. 7.
  • the ribbons 13 and and 14 may be applied and heated in successive operations or may be simultaneously integrated into the seam structure by a single heating step following their application. Pressure may be employed in the integration of the ribbons if found desirable.
  • the 5% nylon content of the coating solution in the above example was nylon 6/ 10,. that is the polymerization product of hexamethylenediamine containing 6 carbon atoms, and sebacic acid containing carbon atoms, and the nylon ribbons used were formed of 6/6 nylon, that is it is the polymerization product of hexamethylenediamine containing 6 carbon atoms and adipic acid containing 6 carbon atoms.
  • Nylon 6 or nylon 11 may be used in place of the 6/6 and 6/10.
  • Alcohol soluble nylon copolymers may also be used. It will be understood that the percentage of solute material in the solution is not critical and while solutions of the order of 5% facilitate application in the manner above de scribed, percentages up to saturation may be used as found feasible.
  • the above procedure and materials provide a seam which conforms closely to the screen texture of the fabric.
  • the cross-sectional dimensions of the seam and its position with respect to the adjacent fabric elements closely approximate those of the weft elements so that no objectionable marking or marring of the paper made thereon results, and drainage through the screen is not materially impeded.
  • the transverse width of the seam may be increased by increasing the length of the free warp ends 6--7 and increasing the extent to which they are lapped, the transverse width of application of the embedding material and the width of the ribbon being correspondingly increased.
  • the embedding material may be such as makes a strong adhesive bond with the warp ends rather than a rniscible bond.
  • the embedding material may be a cyanoacrylate monomer polymerizing, preferably, at room temperature, with approximately 10% plasticizer, thickening agent and stabilizer; the material available under the trade name Eastman 910 being an example.
  • Such material may be applied in successive coats in the manner above described, the coats being allowed to cure under pressure as found necessary (about 5 pounds per lineal inch).
  • the monomer may be aluminum-filled (up to 10% by weight) with some increase in the strength of the bond, but aluminum powder accelerates the cure of the resin. Strips l3 and 14 of nylon may be pressed into bonding adherence to the final coating of the embedding adhesive. Any of the various commercially available adhesives which make a strong bond with nylon,
  • the warp elements are formed of polyester resin such as polyethylene terephthalate
  • the warp ends having been suitably shaped or flattened as in FIG. 2 and cleaned, may be lapped to the desired extent.
  • the bonding 12 may comprise one or more coatings of asuitable solvent such as m-chloro-aniline or phenol, preferably with about 5% polyethylene terephthalate in the solvent, successively applied at a temperature of 350- 420" F.
  • Ribbons 13 of polyethylene terephthalate V film may then be incorporated at opposite sides of the coating body 12.
  • Such ribbons may be coated with a polyester adhesive.
  • a 3 mil polyethylene terephthalate ribbon with 2 mil coating of 46971 Mylar adhesive by Du Pont may be employed.
  • FIGS. 8 and '9 may be employed prior to or after trimming the fabric as described but before removal of the end shoot.
  • the mesh'of the fabric for a short distance back of the fabric ends may be filled with 'ashown in FIGS. 3 and 4.
  • the forming of theseam structure may then be proceeded with as above described,
  • the space between the barriers 16 may be bridged with a mold plates, not shown, and the cavity formed by the barriers 15 and the plates filled with the bonding composition by injection or otherwise.
  • the barriers 16 are dissolved away by a suitable solvent or removed by manual stripping, air blasting, or other suitable procedure.
  • a seam comprisin lapped end portions of the Warp elements embedded in a body of synthetic organic material, said body extending transversely of the fabric between and parallel to weft elements of the fabric and bonding the embedded warp ends to each other and to said body, said body including a preformed strip of the warp material extending longitudinally thereof and incorporated therein.
  • a seam comprising flattened end portions of the warp positioned in lapping relation substantially in the plane of the weft and embedded in a body of synthetic organic material extending transversely of the fabric between, spaced from and parallel to the adjacent weft elements of the fabric and bonding the embedded warp ends to each other and to said body.
  • Warp elements being nylon and said body comprising one or more integrated coatings of nylon and preformed strips of nylon superposed on opposite sides of said body.
  • Warp elements being polyethylene terephathale and the body comprising superposed coatings of up to 5% polyethylene terephthalate in mchloro-aniline.
  • the method of seaming together warp edges of a fourdrinier screen fabric having a warp containing synthetic organic material which comprises, clearing the said edges of weft elements as needed to provide extending Warp end portions, at each edge, cleaning the extending warp end portions, bringing the extending warp end portions at said edges into lapped relation and applying a synthetic organic material to said lapped end portions to form an embedding body around the lapped end portions to bend said portions together and to said body.
  • the m thod of seaming together warp edges of a fourdrinier screen fabric having a warp containing synthetic organic material which comprises, clearing the said edges of weft elements as needed to provide extending Warp end portions, at each edge, cleaning the ends, bringing the extending Warp end portions at said edges into lapped relation, applying successive coatings of a synthetic organic material to said lapped end portions at opposite sides of the fabric, and applying preformed solvent-softened strips of the warp material over said coatings at opposite sides of the fabric.
  • the method of seaming together warp edges of a fourdrinier screen fabric, having a warp of nylon which comprises clearing the said edges of weft elements as needed to provide extending warp end portions at each edge, cleaning the ends, bringing the extending warp end portions at said edges into lapped relation, and applying to said lapped end portions at both sides of the fabric, successive coatings of a viscous solution of nylon, raising the temperature of the seam area following each coating operation to substantially drive off the solvent, applying slight pressure to at least the initial coating prior to the application of the successive coatings.
  • the method of seaming warp edges of a fourdrinier screen fabric, having a warp of nylon which comprises clearing the said edges of weft elements as needed to provide extending warp end portions at each edge, cleaning the ends, positioning the extending warp end portions in lapping relation substantially in the plane of the weft members, applying to the so-positioned extending warp end portions, atboth sides of the fabric, successive coatings of a 5% solution of nylon in phenol at a temperature of substantially 350 F., raising the temperature of the seam area, following each coating operation, to a temperature in the range 350 F. to 375 F.
  • the method of seaming warp edges of a fourdrinier screen Wabric, having a warp of nylon which comprises clearing the said edges of weft elements as needed to provide extending warp end portions at each edge, cleaning the ends, positioning the extending warp end portions in lapping relation substantially in the plane of the weft members, applying to the so-positioned extending warp end portions, at both sides of the fabric, successive coatings of a cyanoacrylate monomer, and curing the successive coats to form an embedding body around the lapped portions'of the extending Warp ends.
  • the method of seaming warp edges of a fourdrinier screen fabric, having a warp of nylon which comprises clearing the said edges of weft elements as needed to provide extending warp end portions at each edge, cleaning the ends, positioning the extending warp end portions in lapping relation substantially in the plane of the Weft members, applying to the so-positioned extending Warp end portions, at both sides of the fabric, successive coatings of a cyanoacrylate monomer polymerizing at room temperature, allowing the successive coats to cure under contact pressure, to form an embedding body around the lapped portions of the extending Warp ends and pressing a strip of nylon into bonding adherence with the embedding body.

Description

N 1963 J. M. DE BELL ETAL 3,109,219
SEAM STRUCTURE FOR FOURDRINIER TYPE SCREEN FABRIC AND METHOD OF MAKING SAME Filed June 21, 1961 I a Q a AKA INVENTORS JOHN M- DGBELL WESLEY LARSON and K5 VIN W- FL YNN av fwd- 72nd fiwfmmsys United States Patent 3,109,219 SEAM STRUCTURE FGR FGURDIER TYPE SCREEN FABRIC AND METHOD OF MAKING ARE John M. De Bell, Longrneadow, Mass, and Wesley Larson and Kevin W. Flynn, Hazardville, Conm, assignors, by mesne assignments, to Cheney Bigelow Wire Works, Inc, Sprinfield, Mass, a corporation of Deltaware Filed June 21, 1961, Ser. No. 11$,7ll2 22 Claims. (Cl. 2374) This invention relates to seam or joint structures, and method of making them, in fourdrinier type screen fabrics, in which the warp elements, at least, are formed of synthetic organic yarns or filaments, or of yarns or filaments containing synthetic organic material such as glass yarns or filaments coated with a synthetic organic material.
Fourdrinier type screen fabric, as the term is here used, is the type of fabric commonly used in paper making machines and is characterized by a relatively fine mesh, an ability to sustain constant movement under tension and flexure in the presence of water and to withstand frictional abrasion.
Fourdrinier type fabric has utility for many commercial purposes but finds its principal use in paper making machines, for which, and for other uses, the ends of a length of the screen fabric are seamed or joined together to form an endless belt. It is important that the seam be not only strong enough to sustain the tensile strain imposed thereon in the operation of the machine, but also, in the case of paper makingmachines, that it suificiently conform to the adjacent surfaces of the screen as not to materially affect or objectionably mar the appearance of the surface of the paper product made thereon. If correct drainage is lacking the paper cannot be stripped from the belt in an endless sheet.
While presently known splicing techniques are adequate for splicing all-metal foundrinier screen fabrics, such techniques are not applicable to a fourdrinier screen fabric having a warp of non-metallic yarns or filaments.
It is the broad object of the present invention to provide seam structures and methods of making them, applicable to fourdrinier type screen fabric, at least the warp elements of which are non-metallic and which contain a synthetic organic plastic.
' Stated in another way it is an object of the invention to provide a seam geometry broadly applicable to the above stated fourdrin-ier type screen fabrics.
A further object is to provide a scam, the transverse width of which may be controlled, and if found desirable or necessary, restricted to a width equal to or not substantially greater than, the transverse width of a weft element of the fabric hein'g spliced, the thickness of the seam being similarly subject to control and restriction to a thickness not substantially greater than the overall thickness of the fabric.
Other and further objects and advantages of the invention will be made apparent in the following specification and claims.
Broadly the above objectives of the invention are attained by forming a relatively narrow transversely extending body of a synthetic organic material of which lapped free end portions of the warp elements, extending from the edges of the fabric to be joined, are at least-an incorporate part, adhesively and/ or cohesively bonded together into a strain resisting unit, having a per-inch tensile strength in the direction of the warp adequately proportional to that of the per-inch strength of the warp assembly, for the use to which the seamed fabric is to be put.
The most exacting structural limitations are perhaps imice posed in the seaming of fourdrinier screen fabric to meet the requirements of its use in the manufacture of fine quality paper, and in the following illustrative disclosures it is assumed that the seamed fabric is to be used for that purpose, the Warp being of a synthetic organic material in the form of a monofilament, or a staple or multifilament yarn, and the weft, by way of illustration and not limitation, being metal wire.
In the accompanying drawings which diagrammatically disclose such an illustrative embodiment of the invention:
FIG. 1 is a longitudinal sectional view, on a greatly enlarged non-exact scale, of the end portions of a length of fourdrinier type fabric, illustrating an initial step in the seaming procedure;
FIG. 2 is a view of the end portions, similar to FIG. 1 but showing the end portions prepared for the second step in the seaming procedure;
FIG. 3 is a similar view showing the third step;
FIG. 4 is a fragmentary plan view on a greatly enlarged non-exact scale showing the relative position of the fabric elements in correspondence to that of FIG. 3;
FIGS. 5 to 7 are views showing succeeding steps in the seaming operation; and
FIGS. 8 and 9 illustrate a modification in the procedure.
Referring to FIG. 1 a length of the fourdrinier fabric of the type previously describcd is generally indicated at l, the'non-metallic Warp-filaments being indicated at 2 and the metal shoots or wefts elements at 3. As the initial step in the seaming procedure the end portions of the strip which are to be seamed together are annealed or heat treated to remove internal strains from and stabilize the warp material as found necessary. The fabric ends are then trimmed to provide the needed end extension of the warp elements. For the assumed use of the fabric this is conveniently done by trimming along the terminal shoot wire as indicated at 4 and 5. The terminal weft or shoot wires are then removed from each end of the strip leaving end portions 6 and '7 of the warp extending from the strip ends. As shown in FIG. 2 the extending end portions are brought into the general plane of the weft and, as indicated at 8 in FIGS. 2 and 4, are flattened or otherwise shaped at their extreme end portions by swaging or pressure, under heat if found desirable, and cleaned to remove any processing oils, dirt, or other foreign matter. The end portions are then brought into lapped relation as shown in FIG. 4, the extent of overlap not materially exceeding the width of a shoot or weft element of the fabric. Ideally and as shown the opposed warp elements are substantially aligned and the side edges of the flattened ends of adjacent warp elements are in substantial contact, but alignment of the opposed warp elements is not essential and the sides of the flattened end portions of the adjacent elements may lapeach other, the opposed warp ends in effect interdigitating. The end portions of the strip are held in the position of FIGS. 3 and 4, in any suitable manner as by bars 9 and I 10 which clamp the end portions against a supporting surface, not shown.
With the end portions so confined a suitable solvent or a plastic solution is applied to the ends 67. The solute embedding material will depend on the material of which the Warp filaments are formed and is either an effective adhesive there-for oris effectively compatible and miscible therewith to, respectively, elfect either a bonding adhesion between the surfaces of the lapped warp ends, or such superficial intermixing, by the solvent of the solution, as to create a union between the material of the warp ends and also a union of the warp ends and the solute material. I
Nylon is one of the various synthetic organic materials commonly used for the warp filaments, and is below 3 referred to for one exemplary disclosure of the seaming structure and method of the invention.
Assuming therefore that the warp filaments 2 are formed of nylon, such as nylon 6, a nylon solvent such as phenol, preferably in the form of a solution of nylon in phenol (later more specifically described) is applied in a single or in successive coats to both sides of the fabric at the lapped area of the filament ends by use of a dip pen, or equivalent applicator, as indicated at 12, by stippling in FIG. 6 and in section in FIG. 5. By way of example for a fourdrinier fabric of the order of 50 to 55 mesh, the warp filaments being .011 of an inch, and the shoot wires .0111 of an inch, in diameter, five coatings of a 5% solution of nylon in phenol has been found satisfactory. The solution is preferably brought to a temperature of 350 F. and applied as above described. After each application the temperature of the seam area is raised to a temperature suificient to drive oil the solvent, preferably in the range of 350 F. to 375 F. After each of the first two applications pressure (about 5 pounds per lineal inch) may be applied over the seam area, in order to assure that the free end portions 6 and 7 are properly positioned and held in place to assure an adequate flow of the initial coating solution between and around the lapped filament end portions 6 and 7 which define the width of the seam.
Phenol softens the nylon of the filaments sufficiently to render it superficially miscible with the nylon of the adjacent coatings, so that the coatings bond to the filaments and to each other without a perceptible or elfective interface between them. The increase of the tem perature following each application of the coating solution dries that coating to leave it in condition to similarly miscibly accept the succeeding coatings. Thus the warp ends 6 and 7 are integrally bonded together into a unitary body 12 with theresin cast from the coatings. Following the last coating operation, without drying the latter coatings, lengths of nylon ribbon 13 and 14, each about 4 to 7 mils thick and 15 mils wide, are placed 1ongitudinally over and along the outer surfaces of the bonding body 12, as indicated in FIG. 5. The ribbons 13 and 14 are softened with hot phenol (350 F), before being put in place, and the temperature of the seam area again raised to 350 F. to 375 F. Thus the resin of the end portions 6 and 7, the resin of the coating body 12 and of the ribbons 1314 is formed into a substantially homogeneous seam structure as indicated at 15 in FIG. 7. It will be understood that the ribbons 13 and and 14 may be applied and heated in successive operations or may be simultaneously integrated into the seam structure by a single heating step following their application. Pressure may be employed in the integration of the ribbons if found desirable.
In seaming the nylon-metal fabric of the above illustration the 5% nylon content of the coating solution in the above example was nylon 6/ 10,. that is the polymerization product of hexamethylenediamine containing 6 carbon atoms, and sebacic acid containing carbon atoms, and the nylon ribbons used were formed of 6/6 nylon, that is it is the polymerization product of hexamethylenediamine containing 6 carbon atoms and adipic acid containing 6 carbon atoms. Nylon 6 or nylon 11 may be used in place of the 6/6 and 6/10. Alcohol soluble nylon copolymers may also be used. It will be understood that the percentage of solute material in the solution is not critical and while solutions of the order of 5% facilitate application in the manner above de scribed, percentages up to saturation may be used as found feasible.
The above procedure and materials provide a seam which conforms closely to the screen texture of the fabric. The cross-sectional dimensions of the seam and its position with respect to the adjacent fabric elements closely approximate those of the weft elements so that no objectionable marking or marring of the paper made thereon results, and drainage through the screen is not materially impeded.
As will be apparent, where desired and where the use of the spliced screen permits, the transverse width of the seam may be increased by increasing the length of the free warp ends 6--7 and increasing the extent to which they are lapped, the transverse width of application of the embedding material and the width of the ribbon being correspondingly increased.
As above pointed out the embedding material may be such as makes a strong adhesive bond with the warp ends rather than a rniscible bond. For example, if the Warp comprises nylon, the embedding material may be a cyanoacrylate monomer polymerizing, preferably, at room temperature, with approximately 10% plasticizer, thickening agent and stabilizer; the material available under the trade name Eastman 910 being an example. Such material may be applied in successive coats in the manner above described, the coats being allowed to cure under pressure as found necessary (about 5 pounds per lineal inch). The monomer may be aluminum-filled (up to 10% by weight) with some increase in the strength of the bond, but aluminum powder accelerates the cure of the resin. Strips l3 and 14 of nylon may be pressed into bonding adherence to the final coating of the embedding adhesive. Any of the various commercially available adhesives which make a strong bond with nylon,
such as the phenolic butyral adhesives, exemplified by rial, it only being necessary to use solvents, and bonding agents which are appropriate for the resin of which the Warp elements are formed. For a further example, assuming the warp elements are formed of polyester resin such as polyethylene terephthalate, the warp ends, having been suitably shaped or flattened as in FIG. 2 and cleaned, may be lapped to the desired extent. In this example the bonding 12 may comprise one or more coatings of asuitable solvent such as m-chloro-aniline or phenol, preferably with about 5% polyethylene terephthalate in the solvent, successively applied at a temperature of 350- 420" F. to opposite sides of the lapped warp ends with the latter at approximately the same temperature and with pressure applied at that temperature for about three minutes, and the coatings cooled to room temperature under pressure. Ribbons 13 of polyethylene terephthalate V film may then be incorporated at opposite sides of the coating body 12. Such ribbons may be coated with a polyester adhesive. For example a 3 mil polyethylene terephthalate ribbon with 2 mil coating of 46971 Mylar adhesive by Du Pont may be employed.
In seaming heavier fabrics than that of the example above given or where for manufacturing conditions or other reasons ditliculty is encountered in maintaining the width of the seam within the desired width, additional steps shown in FIGS. 8 and '9 may be employed. Prior to or after trimming the fabric as described but before removal of the end shoot, the mesh'of the fabric for a short distance back of the fabric ends may be filled with 'ashown in FIGS. 3 and 4. The forming of theseam structure may then be proceeded with as above described,
or the space between the barriers 16 may be bridged with a mold plates, not shown, and the cavity formed by the barriers 15 and the plates filled with the bonding composition by injection or otherwise. In any event after the seaming structure has been formed the barriers 16 are dissolved away by a suitable solvent or removed by manual stripping, air blasting, or other suitable procedure.
What is claimed is:
1. In a fourdrinier screen fabric having a non-metallic warp containing synthetic organic material, a seam comprisin lapped end portions of the Warp elements embedded in a body of synthetic organic material, said body extending transversely of the fabric between and parallel to weft elements of the fabric and bonding the embedded warp ends to each other and to said body, said body including a preformed strip of the warp material extending longitudinally thereof and incorporated therein.
2. In a fourdrinier screen fabric having a non-metallic warp containing synthetic organic material, a seam comprising flattened end portions of the warp positioned in lapping relation substantially in the plane of the weft and embedded in a body of synthetic organic material extending transversely of the fabric between, spaced from and parallel to the adjacent weft elements of the fabric and bonding the embedded warp ends to each other and to said body.
3. A seam as in claim 2, the warp elements being nylon and said body comprising nylon.
4. A seam as in claim 2, the Warp elements being nylon and said body comprising one or more integrated coatings of nylon and preformed strips of nylon superposed on opposite sides of said body.
5. A seam as in claim 2, the warp elements being nylon and the body comprising one or more superposed coatings of polycyanoacrylate.
6. A seam as in claim 2, the warp elements being nylon and the body comprising one or more superposed coatings of polycyanoacrylate and preformed strips of nylon superposed on opposite sides of said body.
7. A seam as in claim 2 the warp elements and said body comprising a polyester resin.
8. A seam as in claim 2., the Warp elements being polyethylene terephathale and the body comprising superposed coatings of up to 5% polyethylene terephthalate in mchloro-aniline.
9. A seam as in claim 2, the warp elements being polyethylene terephthalate and the body comprising superposed coatings of up to 5% polyethylene terephthalate in m-chloro-aniline, and preformed strips of polyethylene terephthalate superposed on opposite sides of said body.
10. The method of seaming together warp edges of a fourdrinier screen fabric having a warp containing synthetic organic material which comprises, clearing the said edges of weft elements as needed to provide extending Warp end portions, at each edge, cleaning the extending warp end portions, bringing the extending warp end portions at said edges into lapped relation and applying a synthetic organic material to said lapped end portions to form an embedding body around the lapped end portions to bend said portions together and to said body.
11. The method of claim '10 in which said embedding body is formed by the application of successive coatings of a solution of embedding material to the lapped warp end portions at opposite sides of the fabric.
12. The method of seaming together warp edges of a fourdrinier screen fabric having a warp containing synthetic organic material which comprises clearing the said edges of weft elements as needed to provide extending warp end portions, at each edge, flattening the ends of said portions, cleaning the ends, bringing the opposed extending Warp end portions into substantial alignment at said edges and into lapped relation and applying a synthetic organic material to said lapped end portions to form an embedding body around the lapped end portions to bond said portions together and to said body.
13. The m thod of seaming together warp edges of a fourdrinier screen fabric having a warp containing synthetic organic material which comprises, clearing the said edges of weft elements as needed to provide extending Warp end portions, at each edge, cleaning the ends, bringing the extending Warp end portions at said edges into lapped relation, applying successive coatings of a synthetic organic material to said lapped end portions at opposite sides of the fabric, and applying preformed solvent-softened strips of the warp material over said coatings at opposite sides of the fabric.
14. The method of seaming together warp edges of a fourdrinier screen fabric, having a warp of nylon which comprises clearing the said edges of weft elements as needed to provide extending warp end portions at each edge, cleaning the ends, bringing the extending warp end portions at said edges into lapped relation, and applying to said lapped end portions at both sides of the fabric, successive coatings of a viscous solution of nylon, raising the temperature of the seam area following each coating operation to substantially drive off the solvent, applying slight pressure to at least the initial coating prior to the application of the successive coatings.
15. The method of seaming warp edges of a fourdrinier screen fabric, having a warp of nylon, which comprises clearing the said edges of weft elements as needed to provide extending warp end portions at each edge, cleaning the ends, positioning the extending warp end portions in lapping relation substantially in the plane of the weft members, applying to the so-positioned extending warp end portions, atboth sides of the fabric, successive coatings of a 5% solution of nylon in phenol at a temperature of substantially 350 F., raising the temperature of the seam area, following each coating operation, to a temperature in the range 350 F. to 375 F. to drive oft" the solvent, applying a pressure of approximately 5 pounds per lineal inch to at least the initial coating prior to the application of the successive coatings, and applying a strip, 4 to 7 mils thick and approximately 15 mils wide, of nylon softened with phenol at a temperature of 350 F., longitudinally over the coatings at each side of the fabric, and again raising the temperature of the seam area to a temperature in the range 350 F. to 375 F.
16. The method of seaming warp edges of a fourdrinier screen Wabric, having a warp of nylon, which comprises clearing the said edges of weft elements as needed to provide extending warp end portions at each edge, cleaning the ends, positioning the extending warp end portions in lapping relation substantially in the plane of the weft members, applying to the so-positioned extending warp end portions, at both sides of the fabric, successive coatings of a cyanoacrylate monomer, and curing the successive coats to form an embedding body around the lapped portions'of the extending Warp ends.
17. The method of claim 16 in which the eyanoacrylate monomer is filled, up to 10% by weight with finely divided aluminum.
18. The method of seaming warp edges of a fourdrinier screen fabric, having a warp of nylon, which comprises clearing the said edges of weft elements as needed to provide extending warp end portions at each edge, cleaning the ends, positioning the extending warp end portions in lapping relation substantially in the plane of the Weft members, applying to the so-positioned extending Warp end portions, at both sides of the fabric, successive coatings of a cyanoacrylate monomer polymerizing at room temperature, allowing the successive coats to cure under contact pressure, to form an embedding body around the lapped portions of the extending Warp ends and pressing a strip of nylon into bonding adherence with the embedding body.
19. The method of seaming warp edges of a fourdrinier screen fabric, having a warp of polyethylene terephthalate, which comprises clearing the said edges of weft elements as needed to provide extending warp end portions at each edge, cleaning said portions, positioning the extending warp end portions in lapping relation substantially in the plane of the weft members, heating the so-positioned extending warp end portions to' a temperature of approximately 350 F. to 420 F., applying successive coats of approximately polyethylene terephthalate in m-chloro-aniline heated to a temperature of approximately 350 F. to 420 F. to the so-positioned extending warp :end portions.
20. The method of seaming warp edges of a fourdrinier screen fabric, having a warp of polyethylene terephthalate, which comprises heat treating the fabric at, and for a substantial distance rearwardly from, the edges to be joined to stabilize the material of the warp, clearing said edges of weft elements as needed to provide warp end portions at each edge, flattening the ends of said portions, cleaning the said end portions, bringing the flattened end portions into lapped relation, heating the so-positioned warp end portions to a temperature of approximately 250 F., applying successive coats of hot phenol thereto, raising the temperature of said warp end portions to approximately 420 F. under pressure, permitting evaporation of the phenol, applying hot phenol to ribbons of polyethylene terephthalate and to the now cool warp end portions,-at each side of the fabric, and applying the said ribbons, successively one to each side of the fabric, over the warp end portions, under pressure and at a temperature approximating 420 F.
21. The method of seaming together warp edges of a fourdrinier screen fabric having a 'warp containing synthetic organic material which comprises trimming the edges along a weft element, filling the mesh of the fabric rearwardly of said weft element with a barrier material,
rial as needed to provide extending warp end portions extending from the remaining barrier material, bringing the so-extending wrap end portions into lapped relation, forming an embedding body of a synthetic organic material around the said lapped end portions between the adjacent edges of the barrier material to bond said Warp end portions together and thereafter cleaning the fabric of said barrier material.
22. The method of seaming together warp edges of a fonrdrinier screen fabric having a warp containing synthe'tic organic material which comprises trimming the edges along a weft element, filling the mesh of the fabric rearwardly of said weft element with a barrier material, clearing the said edges of Weft elements and barrier material as needed to provide extending warp end portions extending from the remaining barrier material, bringing the soextending warp end portions into lapped relation, filling the space between the adjacent edges of the barrier material with a material bonding the said warp end portions together and thereafter clearing the fabric of said barrier material.
References Cited in the tile of this patent UNITED STATES PATENTS 2,049,752 Steinhart Aug. 4, 1936 2,116,812 Webb May 10, 1938 2,117,222 Sinclair May 10, 1938 2,391,731 Miller et a1 Dec. 25, 1945 2,435,467 Spencer Feb. 3, 1948 2,903,021 Holden et a1 Sept. 8, 1959

Claims (1)

1. IN A FOURIDRINIER SCREEN FABRIC HAVING A NON-METALLIC WARP CONTAINING SYNTHETIC ORGANIC MATERIAL, A SEAM COMPRISING LAPPED END PORTIONS OF THE WARP ELEMENTS EMBEDDED IN A BODY OF SYNTHETIC ORGANIC MATERIAL, SAID BODY EXTENDING TRANSVERSELY OF THE FABRIC BETWEEN AND PARALLEL TO WEFT ELEMENTS OF THE FABRIC AND BONDING THE EMBEDDED WARP ENDS TO EACH OTHER AND TO SAID BODY, SAID BODY INCLUDING A PREFORMED STRIP OF THE WARP MATERIAL EXTENDING LONGITUDINALLY THEREOF AND INCORPORATED THEREIN.
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Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3238594A (en) * 1962-06-22 1966-03-08 Karl U Schuster Method of connecting the ends of screen fabrics for producing endless forming wires for paper machines
US3622415A (en) * 1967-12-22 1971-11-23 Lindsay Wire Weaving Co Papermaking fabric seam and method of making the same
US3704788A (en) * 1971-01-11 1972-12-05 Ecodyne Corp Sewage treatment system
US4119030A (en) * 1976-07-13 1978-10-10 Takaji Funahashi Endless printing belt for rotary rubber stamp
US4283184A (en) * 1979-04-30 1981-08-11 Winfred M. Berg, Inc. Non-metallic silent chain
US5571590A (en) * 1995-06-06 1996-11-05 Appleton Mills Methods of making papermaking felt and substrate
US5707496A (en) * 1991-01-23 1998-01-13 Asten, Inc. Papermakers fabric having a synthetic molding seam
US5731063A (en) * 1995-06-06 1998-03-24 Appleton Mills Papermaking felt and substrate
US20040154148A1 (en) * 2002-12-30 2004-08-12 Anders Nilsson Papermaker's and other industrial process fabric characteristics by calendering
US20080064281A1 (en) * 2006-09-08 2008-03-13 Frank Bez Band for a machine for producing web material, in particular paper, board or tissue, and process for the production of such a band
US20080289716A1 (en) * 2007-05-23 2008-11-27 CROOK Robert Low tensile creep belt

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2049752A (en) * 1934-03-21 1936-08-04 Steinhart Ferdinand Welding joint for wire cloth
US2117222A (en) * 1936-01-22 1938-05-10 Peter S Sinclair Dandy roll and cylinder mold and method of making same
US2116812A (en) * 1936-05-15 1938-05-10 Eastwood Nealley Corp Seam-wire and method for making wire-cloth seams
US2391731A (en) * 1943-05-17 1945-12-25 Minnesota Mining & Mfg Spliced abrasive belt, band, and the like
US2435467A (en) * 1946-12-11 1948-02-03 Firestone Tire & Rubber Co Splicing monofilament fabrics
US2903021A (en) * 1955-12-23 1959-09-08 F C Huyck & Sons Fourdrinier cloth

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2049752A (en) * 1934-03-21 1936-08-04 Steinhart Ferdinand Welding joint for wire cloth
US2117222A (en) * 1936-01-22 1938-05-10 Peter S Sinclair Dandy roll and cylinder mold and method of making same
US2116812A (en) * 1936-05-15 1938-05-10 Eastwood Nealley Corp Seam-wire and method for making wire-cloth seams
US2391731A (en) * 1943-05-17 1945-12-25 Minnesota Mining & Mfg Spliced abrasive belt, band, and the like
US2435467A (en) * 1946-12-11 1948-02-03 Firestone Tire & Rubber Co Splicing monofilament fabrics
US2903021A (en) * 1955-12-23 1959-09-08 F C Huyck & Sons Fourdrinier cloth

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3238594A (en) * 1962-06-22 1966-03-08 Karl U Schuster Method of connecting the ends of screen fabrics for producing endless forming wires for paper machines
US3622415A (en) * 1967-12-22 1971-11-23 Lindsay Wire Weaving Co Papermaking fabric seam and method of making the same
US3704788A (en) * 1971-01-11 1972-12-05 Ecodyne Corp Sewage treatment system
US4119030A (en) * 1976-07-13 1978-10-10 Takaji Funahashi Endless printing belt for rotary rubber stamp
US4283184A (en) * 1979-04-30 1981-08-11 Winfred M. Berg, Inc. Non-metallic silent chain
US5707496A (en) * 1991-01-23 1998-01-13 Asten, Inc. Papermakers fabric having a synthetic molding seam
US5571590A (en) * 1995-06-06 1996-11-05 Appleton Mills Methods of making papermaking felt and substrate
US5731063A (en) * 1995-06-06 1998-03-24 Appleton Mills Papermaking felt and substrate
US20040154148A1 (en) * 2002-12-30 2004-08-12 Anders Nilsson Papermaker's and other industrial process fabric characteristics by calendering
US7514030B2 (en) 2002-12-30 2009-04-07 Albany International Corp. Fabric characteristics by flat calendering
US20080064281A1 (en) * 2006-09-08 2008-03-13 Frank Bez Band for a machine for producing web material, in particular paper, board or tissue, and process for the production of such a band
US7918970B2 (en) * 2006-09-08 2011-04-05 Voith Patent Gmbh Band for a machine for producing web material, in particular paper, board or tissue, and process for the production of such a band
US20080289716A1 (en) * 2007-05-23 2008-11-27 CROOK Robert Low tensile creep belt
US7513277B2 (en) * 2007-05-23 2009-04-07 Voith Patent Gmbh Low tensile creep belt

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