US3616123A - Helicoid laminate comprising several continuous tiered strips - Google Patents

Helicoid laminate comprising several continuous tiered strips Download PDF

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Publication number
US3616123A
US3616123A US701424A US3616123DA US3616123A US 3616123 A US3616123 A US 3616123A US 701424 A US701424 A US 701424A US 3616123D A US3616123D A US 3616123DA US 3616123 A US3616123 A US 3616123A
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Prior art keywords
strips
helicoid
strip
laminate
covering
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US701424A
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Harold J Reynolds Jr
George P Leistensnider
Angelo A Forte
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Johns Manville Corp
Johns Manville
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Johns Manville
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16LPIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L59/00Thermal insulation in general
    • F16L59/02Shape or form of insulating materials, with or without coverings integral with the insulating materials
    • F16L59/027Bands, cords, strips or the like for helically winding around a cylindrical object
    • 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
    • B29C53/00Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/02Bending or folding
    • B29C53/12Bending or folding helically, e.g. for making springs
    • 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
    • B29C63/00Lining or sheathing, i.e. applying preformed layers or sheathings of plastics; Apparatus therefor
    • B29C63/02Lining or sheathing, i.e. applying preformed layers or sheathings of plastics; Apparatus therefor using sheet or web-like material
    • B29C63/04Lining or sheathing, i.e. applying preformed layers or sheathings of plastics; Apparatus therefor using sheet or web-like material by folding, winding, bending or the like
    • B29C63/08Lining or sheathing, i.e. applying preformed layers or sheathings of plastics; Apparatus therefor using sheet or web-like material by folding, winding, bending or the like by winding helically
    • B29C63/10Lining or sheathing, i.e. applying preformed layers or sheathings of plastics; Apparatus therefor using sheet or web-like material by folding, winding, bending or the like by winding helically around tubular articles
    • B29C63/105Lining or sheathing, i.e. applying preformed layers or sheathings of plastics; Apparatus therefor using sheet or web-like material by folding, winding, bending or the like by winding helically around tubular articles continuously
    • 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
    • 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
    • B29C66/4329Joining 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 the joint lines being transversal but non-orthogonal with respect to the axis of said tubular articles, i.e. being oblique
    • 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
    • B29C66/49Internally supporting the, e.g. tubular, article 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
    • B29C66/80General 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
    • B29C66/834General aspects of machine operations or constructions and parts thereof characterised by the movement of the joining or pressing tools moving with the parts to be joined
    • B29C66/8341Roller, cylinder or drum types; Band or belt types; Ball types
    • B29C66/83411Roller, cylinder or drum types
    • B29C66/83413Roller, cylinder or drum types cooperating rollers, cylinders or drums
    • 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
    • B29C66/834General aspects of machine operations or constructions and parts thereof characterised by the movement of the joining or pressing tools moving with the parts to be joined
    • B29C66/8341Roller, cylinder or drum types; Band or belt types; Ball types
    • B29C66/83411Roller, cylinder or drum types
    • B29C66/83415Roller, cylinder or drum types the contact angle between said rollers, cylinders or drums and said parts to be joined being a non-zero angle
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16LPIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L11/00Hoses, i.e. flexible pipes
    • F16L11/24Hoses, i.e. flexible pipes wound from strips or bands
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16LPIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L58/00Protection of pipes or pipe fittings against corrosion or incrustation
    • F16L58/02Protection of pipes or pipe fittings against corrosion or incrustation by means of internal or external coatings
    • F16L58/16Protection of pipes or pipe fittings against corrosion or incrustation by means of internal or external coatings the coating being in the form of a bandage
    • 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
    • B29C65/1403Joining 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 characterised by the type of electromagnetic or particle radiation
    • B29C65/1412Infrared [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
    • 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
    • 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
    • B29K2021/00Use of unspecified rubbers as moulding material
    • 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
    • Y10S428/00Stock material or miscellaneous articles
    • Y10S428/92Fire or heat protection feature
    • 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
    • Y10S428/00Stock material or miscellaneous articles
    • Y10S428/92Fire or heat protection feature
    • Y10S428/921Fire or flameproofing
    • 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
    • Y10T156/00Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10Methods of surface bonding and/or assembly therefor
    • Y10T156/1002Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
    • Y10T156/1007Running or continuous length work
    • 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
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24752Laterally noncoextensive components
    • 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
    • Y10T428/249921Web or sheet containing structurally defined element or component
    • Y10T428/249922Embodying intertwined or helical component[s]

Definitions

  • the resulting helicoid product may be conformed to a mandrel and cured, vulcanized or otherwise treated to acquire a durable tubular helicoid form.
  • This technique is particularly useful in making helicoid coverings that may be repeatedly put on and removed from tubes, rods, wires and the like, as coverings, firesleeves, or insulation, for example.
  • the invention concerns a type of tubular covering that is flexible, fire-resistant and capable of repeated coiling and uncoiling installation and removal without damage about a tube, rod, wire, pipe, hose or the like to function as a firesleeve, packing, and the like.
  • Insulation materials in the form of ribbons or tapes which can be wrapped about a tubular conduct are known.
  • the time required to remove and reinstall such insulation coverings to permit inspection of the thermally protected conduit renders this type of product unsuitable for use where easy and frequent inspection of the conduit is required.
  • Some form of insulation covering having a relatively permanent shape and yet which may be readily applied and removed is in demand by the aircraft construction industry and by others.
  • coverings provided with fasteners such as zippers, hooks, buckles and the like have been investigated. All such removable insulation coverings, however, display poor flexibility when assembled upon a flexible hose and undergo fish mouthing on the compression side of a bend. Zippers and similar closure units which were attached to the insulation covering by machine stitching or the like tend to break loose at the stitch under tension when the enclosed flexible metal conduit is flexed. Also, covers using hooks, buckles and the like are difiicult to install.
  • the spiral wound product may be a self-supporting pipe or tube (U.S. Pat. No. 2,161,036) or may be a covering for a pipe to protect it against corrosion or for heat insulation purposes (U.S. Pat. No. 2,7l3,383).
  • a plurality of strips may be employed and formed in overlapped or staggered relationship between joints in the resulting tubular structure (U.S. Pat. No. 2,225,026).
  • complicated equipment may be used to get a tight telescoping interfitting of the helices by edge crimping (U.S. Pat. No. 2,759,521). a
  • a principal object of this invention is the provision of new forms of helicoid tubular products.
  • New helicoid coverings that may 'be used to protect and flameproof wire bundles, tubes, pipes or the like where ease of application of the coverings is important, such as in tight quarters or where repeated inspections of the enclosed conduit are required.
  • New forms of helicoid coverings that provide good protection to an encased tubular conduit at the junctions between separate coils of the helicoid structure.
  • Heat protection wraps that provide multiple layers of insulation over an encase conduit yet permit a good flexibility to be maintained throughout the entire assembly.
  • the operation comprises:
  • binder composition such as an elastomeric material
  • the strips are assembled in a tiered and staggered configuration with the edge of at least one strip being offset from the edge of at least one other strip;
  • said staggered configuration is cured into a helicoid integral structure having overlapping butt joints between strips of adjacent coils so that the structure is capable of being repeatedly coiled and uncoiled so that the insulation wrap may be repeatedly installed and removed from a tubular conduit without damage.
  • the inner face of the insulation wrap may be formed of material different from the remaining structure, e.g., an inner surfacing of ethylene-propylene rubber composition of low-corrosion properties to metal as compared with asbestos fibers and polychloroprene rubber used in forming the remaining portion of the insulation wrap.
  • the new helicoid products may be of a double-ply or a quad-ply construction, all of which employ the staggered or overlap edge arrangement which provides ship-lap joints between adjacent coils of the laminate in the helicoid product.
  • step d recovering from step d an uncured open helicoid laminate of said plurality of strips;
  • FIG. 1 is a flow sheet diagrammatically illustrating the materials and method steps employed in the formation of preferred new products of the invention
  • FIG. 2 is a side view, partially broken away and sectioned, of one form of a helicoid product of the invention having a tri ply structure;
  • FIG. 3 is a side view, partially broken away and sectioned, of another form of helicoid tubular covering of the invention.
  • FIG. 4 is a side view, partially broken away and sectioned, of a further embodiment of helicoid tubular covering of the invention.
  • FIG. 5 is a diagrammatic side view of apparatus used in the helicoid preforming step of the new methods
  • FIG. 6 is a perspective view of loose helicoid uncured preformed material as formed by the new processes
  • FIG. 7 is a fragmentary enlarged view of the structure of stepped driven rollers used in accordance with the invention to create the helicoid perform such as shown in FIG. 6.
  • FIG. 8 is an elevational view, partially in section, of another form of apparatus used in joining two strips of material being fed into opposing rolls in accordance with the invention.
  • FIG. 9 is a side view of the apparatus of FIG. 8 in which the laminate is wound on a tube.
  • the tri-ply form of insulation wrap 2 shown in FIG. 2, as applied to metal pipe 4, consists of three separate strips 6, 8 and 10 of asbestos cloth impregnated with an elastomeric material.
  • Inner strip 10 is offset to one side of the central strip 8 while the outer strip 6 is offset to the other side of the central strip 8. Consequently, there are ship-lap-type joints 12 between the adjacent coils 14a, 14b, 14c, etc., of the helicoid structure.
  • Each turn of the insulation wrap nests into the adjacent turn or coil in the manner of a bell-and-spigot joint. This arrangement provides excellent flexibility without fish-mouthing at bends and also gives uninterrupted protection to the encased conduit against external flame or heat.
  • straps or clamps 16 may be applied at opposite ends of the insulation wrap 2 or at any other appropriate position.
  • the insulation wrap 20 is of a bi-ply construction formed of an outer strip of elastomeric impregnated asbestos fiber cloth strip 22 and an inner strip 24. Strips 22 and 24 are laminated to one another along an interface 26 so that the two strips 22 and 24 form an integral unit. Theedge 28 of the strip 22 is offset from the edge 30 of the strip 24 in a staggered arrangement. Ship-lap joints are provided between adjacent coils of the laminate, with the joints in between coils of single strips being in a butt arrangement 32.
  • the insulation wrap 40 comprises an outer strip 42, a pair of central strips 44 and 46 and an innermost strip 48.
  • the central pair of strips are in full register with their longitudinal edges aligned thus creating the central section in the insulation wrap of this embodiment of double thickness.
  • the edge 50 of the outer strip 42 is offset to one side of the central ply while the edge 52 of the inner strip 48 is offset to the opposite side of the central ply.
  • the insulation wrap are fully overlapping at all points throughout the entire area of the wrap when installed upon the metal pipe or tubing 4.
  • FIG. 5 there is illustrated a preferred method of forming insulation wrap such astri-ply wrap (FIG. 2).
  • Separate reels 60, 62 and 64 of asbestos fiber cloth impregnated and covered with uncured, tacky, elastomeric material are mounted for free rotation upon supportingshafts 66, and 70.
  • Spring loaded retainers 67, 69 and 71 are used, the tensions of which may be adjusted to control the relative unrolling of strips 6, 8 and 10.
  • they In order to prevent sticking of t separate convolutions in the rolls of cloth strips, they have coverings of thin separator strips 72, 74 and 76 which are pulled from the respective strips 6, 8 and as they are unrolled and carried to the opposed driven rollers 78and 80.
  • the top roll 78- is carried on a driven shaft 82 and has a series of steps or faces 84, 88, 90 and a gear 92.
  • the roller 80 carried upon the driven shaft 94 is formed with a series of steps 96, 98, 100, 104 and a gearl06, the latter meshing with gear 92.
  • Face 90 is of the same diameter as face 84, while on roll 80, face 104 is of the same diameter as face. 96.
  • Face 90 and a portion of face 84' mate with steps 96 and a portion of step 104 of the roll 80 which serves to align and limit the two rolls 78,80 in operation when the rolls are biasedtoward eachpother under spring-loaded pressure by spring means (not shown).
  • Power is provided from a source (not shown) through themeshing gears (not drawn to scale) 92, I06.
  • step 100 is of smaller diameter than step 104, while step 98 is of smaller diameter than step 100.
  • Step 88 is equal in width to the upper strip 6'
  • step 100 is equal in width to one-half of strip 8
  • the widths of the three strips are preferably the same, so that if step 88 has a width x, step 100 has a width of x/2, and step 98 has a width ofx.
  • the relationship of the diameters of the two rolls 78, 80 is such that the smaller step 881s always larger than the diameter of step 98.
  • the step from the larger face 84, tothe smaller 88 is quite small, and the stepping down from step 104 to step 100 to step 98 is quite small.
  • the opening between the rolls 78 and 80 is exaggerated for purposes of clarity.
  • the diameter of steps 84, 90 compared to the diameter of steps 96, 104 is in the order of 1.6:], so that roughly the diameters of steps 88, 98 are in a similar ratio. This ratiocan be altered depending upon the degree of curvature desired to be applied to the formed laminate 6, 8 and 10.
  • Steps 88 and a portion of steps84 of roll 80 create the pressure to force opposing faces of the strips 6, 8 and 10 into contact with one another into a staggered arrangement as illustrated in FIG. 7 and cause the tacky faces of the strips which are in contact with one another to stick together.
  • the length of strip 8 Similarly, more of strip 8 is fed past the point of contact per unit time than of strip I8.
  • Unequal feeding from the rolls 68, 62, 64 is evidenced in that reel 68 is the first to unwind completely, reel 62 is the next to be unwound completely, and reel 61lis the last to unwind its material.
  • the relative rates of unwinding which in turn is usually indicative of the degree of curvature imparted to the laminate 6, 8, I8, is controlled by the relative tensions of retainers 67, 69 and 7 I, the diameter of roll 78 relative to the diameter of roll 80, the pressure loading on the two rolls 78, 88 and the speeds of rotation of the two rolls. Consequently, the laminated strips as they issue from the contacting rolls 78 and form an uncured open helicoid lamination 188. This open lamination is illustrated in more detail in FIGS. 5, 6.
  • FIGS. 8-9 two separate strips of impregnated materials, 'and 112, are fed from reels 116a, H241 to between two sets of opposed cylindrical rolls I18, I16 and I18, 120; reels 1I0a and 112a have joined thereto springs lI0b and 11211 which control the tension of unreeling.
  • the springtension of each is adjustable to control the relative rates of feed of strips I I0, 112.
  • FIG. 8 depicts the exit of the materials from, between the rolls.
  • the materials are in a stepped, overlapped relationship, in that a side end portion I22 of strip I10 mates with side end portion 124 of strip II2.
  • Roll H6 is larger in diameter relative to adjacent roll II6, and roll II8 is larger in diameter than adjacent roll 120.
  • Roll II6 is also larger in diameter than the larger roll I18.
  • Roll U4 is also larger in diameter than the diameter of :roll I26.
  • overlapped portions 122, 124 are under compression, and in addition, the free side end portions 126, 128 are also under compression.
  • the degree of compression is related to the spacings between the opposed rolls, the loading on the rolls, the tension of springs IItlb, 112b, and the relative thickness of the two strips of materials.
  • Strips I10 and I12 are fed in constant feed throughthe opposed rolls, being drawn through by the rate of rotation and relative diameters of the rolls. However, the rate of feed from reel 118a is greater than the rate from reel 1120.
  • the overlapped portions 122, 124 have a tendency to be drawn through linearly.
  • sidle portion 128 is either stretched, calendered to a greater degree than adjacent portion 124, or placed in tension relative to side end I26, or simply its strip is drawn through faster than adjacent stripl I2.
  • strip II2 appears to pass between opposed rolls II6 and 128 so that it is either in compression, or under slight tension but much less than the tension withinside end 126, or neither under tension nor compression.
  • the joined strips I18, I12 emitted from between the rolls incurvated to the right in FIG. 8 in a continuous arc.
  • reels IItla, II2a If the same amount of material is placed on reels IItla, II2a at the start of a forming operation, at the end of the cycle reel 110a will have unwound before reel Ill2a. This clearly indicates of course that although a constant feed from each separate reel is used, the rate of feed from one reel to the next is different.
  • the amount of material left on reel 112a when reel llItla is unwound is a function of the factors mentioned, that is, tension of springs lItIb, 1112b, temperature of the strips, the type of material used for the strips, the relative sizes of the rolls, and the loading on the rolls.
  • the laminate may be used as'is, or it may be wound on a mandrel or rod 130 (FIG. 9).
  • sidewall 118a of roll 118 acts as an end guide for strip 112
  • sidewall 116a of roll 116 acts as an end guide for strip 110.
  • This guide arrangement controls in precision the continuous overlap of the two strips 110, 112.
  • the laminate may be wound on a core so that a solid or continuous covering 112 is applied on the core, and a second continuous covering 1 10 is superimposed over the covering 112.
  • the tight abutment or tight helix arrangement may be a loose helix, so that spacings exist between adjacent strips 110 and adjacent strips 112. This, of course, depends upon the type of covering desired to be formed or the type of product desired to be produced.
  • the impregnant in the strips may thereafter be cured or hardened.
  • the resultant product is either a solid tube or a wrap or covering which can be wound and unwound.
  • heat is applied to cure or harden the impregnant, using techniques that are well known. If a polyester resin, for example, is the impregnant, fusion of the resins in the strips occurs so that a hard, unified product results.
  • the laminate veers to the right in arcuate form (FIG. 8).
  • An end of the laminate is applied to a rotating core 130 so that a helicoid wrap is formed directly adjacent the exit end of the opposed sets of rolls.
  • the individual strips 110, 112 are in abutment with adjacent strips. All helicoid strips (actually being one continuous strip) are in abutment with each other to provide a solid covering; all strips 110 are in abutment with each other to provide a solid covering over strip 112.
  • the coils of the complete laminate form ship-lap joints between each other.
  • the laminate on the core 130 may thereafter be subjected to heat to provide a cure or hardening of the impregnant.
  • the strips may be only amalgamated to each other to form the helicoid laminate or the impregnated may be fused throughout to form a solid tube upon removal of the core 130.
  • FIG. 1 An advantageous sequence of steps which may be used to produce new heat protective coverings of the invention is outlined in the flow diagram constituting FIG. 1.
  • a first stage of the operation is the provision of a plurality of separate strips of asbestos fiber cloth impregnated and covered with uncured, tacky, elastomeric or other binder material. Such strips could be obtained from a commercial source, but in a fully integrated operation, the attainment of such strips would advantageously begin by the coating and impregnating of woven fabric made from asbestos fibers with an elastomeric material composition, e.g., a solvent solution of the material known as coat cement.
  • an elastomeric material composition e.g., a solvent solution of the material known as coat cement.
  • Any suitable method of applying the elastomeric material coating may be employed, such as knife coating, roller coating, spraying, dipping and the like.
  • a preferred method is the so-called divine coating technique which results in a major portion of the coating material being retained on the surface of the cloth and only a minor amount of the coating penetrating into the interstices of the cloth.
  • Each of the separate strips which are to be plied together to form the lamination may be coated with the same elastomeric composition.
  • one or more surfaces of the strips may be coated with an elastomeric composition having very low corrosive characteristics.
  • a preferred form of the new insulation wraps may employ ethylene-propylene rubber compound (EPDM) to coat the surface of the insulation wrap and would be in contact with the metal pipe (e.g., the inner surface of strip 10 in FIG. 2).
  • EPDM ethylene-propylene rubber compound
  • the remaining surfaces of the strips would be coated with a polychloroprene composition.
  • the coating and impregnating operation will advantageously be accomplished using drying ovens or comparable equipment to evaporate solvents and other volatile material from the coating composition and leave the asbestos cloth impregnated and covered with an uncured, tacky, elastomeric coat. Normally, the resulting coated asbestos cloth will be rolled into a jumbo roll for subsequent processing. As this is accomplished, a release sheet of polyethylene film, holland cloth or comparable separator sheet will be applied to one sur' face of the coated asbestos cloth so that the cloth may be formed into rolls without convolutions adhering to each another.
  • the cloth is next slit into narrow widths, e.g., about 1 to 5 cms. These are then rolled into separate rolls of suitable diameter, e.g., 10 to 50 cms., for ease of handling in subsequent operations, such as reels 60 to 64 of FIG. 5.
  • the next stage of the operations is the helicoid preforming which has generally been described previously in connection with FIG. 5.
  • the operation involves bringing the separate strips of whatever desired number, advantageously between 2 to 4 separate strips, into generally parallel alignment, contacting opposed faces of the strips in a staggered, tiered arrangement with the edge of at least one strip being offset from the edge of at least one other strip.
  • staggered arrangements may take various forms, as illustrated in FIGS. 2 through 4.
  • With a two-ply construction such as in FIG. 3, little variation is possible except in the amount of overlapping at the edge between the separate strips.
  • equal overlap between the top and bottom strips relative to the central strip is advantageous.
  • a four-ply construction see FIG.
  • two central strips may be fully aligned with no overlap to provide a double-thickness central ply.
  • the strips are incurvated as described hereinbefore. As the strips contact under such conditions, the resulting laminated structure assumes an open loose helicoid form as illustrated in FIG. 6.
  • This loose helicoid product may be produced and handled in continuous length or suitable measured lengths may be cut from the product issued from forming rolls for handling in subsequent steps of the operation.
  • the helicoid preform is treated by dusting with release or antitack material to prevent exposed surfaces from sticking together or sticking to the mandrel in the subsequent operations.
  • Any suitable material known to the rubber-processing art as satisfactory dusting agent may be employed for this purpose including powdered mica, soapstone, chalk, calcium carbonate, or the like. Such dusting may be accomplished in wind tunnels, by spraying, in tumbling barrels or other suitable equipment.
  • the loosely coiled helicoid preform is wound upon a mandrel having a suitable outside diameter to form an inside diameter to the insulation wrap of approximate size to encase the tubing or conduit to be covered by the wrap.
  • Metal rods or pipes are advantageously used as mandrels. high-carbon steel or stainless steel being examples, although any other suitable materials including ceramics, glass, or the like, may be used for the mandrel.
  • Application of a release coat upon the surface of the mandrel prior to wrapping the helicoid preform is recommended in order to insure easy and clean removal of the finished product from the mandrel after the cure.
  • the curing step is performed using curing conditions as recommended by the manufacturer of the elastomeric material used in the initial coating stage of the operation. As is known to those associated with curing or vulcanizing of rubber of comparable curable elastomeric materials, such conditions may be varied. In some special cases, air curing at ambient temperature over substantial lengths of time may be used, e.g., with silicone elastomers. Normally, however, curing isaccomplished by heating the mandrel-wrapped product to an elevated temperature, e.g., ISO-250 C. for about I to 72 hours. Induction heating, infrared heating, or the like may be employed instead of themore common heating in electrical resistance or gas fired ovens. Where hollow mandrels are employed, heat exchange liquids may be circulated throughthe interior of the mandrel in order to provide all or part of the heat.
  • the cured helicoid lamination is removed from the mandrel and may be used for intended purposes without further treatment. Normally, however, the product will be trimmed at the edges toprovide sharp, neat product or may be cut to smaller lengths as required by the trade or special purchaser. Additionally, the subsequent handling may involve wrapping, packaging and the like.
  • EXAMPLE 1 This example illustrates the production of a three-ply construction insulation wrap having a low corrosion internal surface in various sizes.
  • a standard GR-M rubber cement consisting of about 85 percent volatile haloalkane solvent and 15 percent elastomeric mix was used as the principal elastomeric coating material for the production run.
  • the elastomeric mix in the cement was formed of rubber (100 parts), benzothiazyl disulfide (1 part), plasticizer (2 parts), stearic acid (0.5 parts), zinc oxide parts), magnesium carbonate (4 parts), antioxidant (2 parts), carbon black (5 parts) and hard clay (40 parts).
  • a standard plain weave cloth made of asbestos fiber yarn having a thickness of about 2.5 mm. was doctor-blade coated with the above coating cement at a rate of about 20 percent on each side based upon the weight of the cloth.
  • the coated cloth was dried in a hot air oven and polyethylene film wasapplied to one surface as a masking.
  • the cloth was slit into tapes of 2 cm. width and the tapes were wound into small rolls of about meters in length with the polyethylene masking between convolutions.
  • the same cloth was coated upon one side at the 20. percent rate with the GR-M cement and upon the other side at a percent rate with a similar standard coating cement used ElPDM rubber as the elastomer base rather than the GR-M rubber.
  • This different surfaced cloth was also slit into 2 cm. tapes and wound into 15 meter length rolls with a polyethylene film separator.
  • Two rolls of the first tape and one roll of the second tape were mounted on a helicoid preform machine of the type described hereinbefore. Before the tape from each roll was passed through the lamination rollers, the polyethylene masking strip was peeled from the tape.
  • the driven rollers of the machine were operated at about 35 r.p.m. and a helicoid preform of tri-ply construction was formed at a rate of about 2.5 meters per minute. As the preform emerged from the forming rolls, it was dusted with powdered mica.
  • the dusted preform was tightly wrapped upon a 5/16 in. OD. mandrel formed of Teflon" coated aluminum tubing on an arbor-type lathe maintaining about I to 2 mm. space at the joints while wrapping.
  • the mandrel wrapped material was then vulcanized in a circulating air oven for 1 hour at about C.
  • the vulcanized product was removed from the oven and cooled to ambient temperature, removed from the mandrel and end trimmed.
  • the resulting insulation wrap was installed upon black iron pipe and subjected to a standard heat transmission test in which the outer surface of the wrap is subjected to a flame maintained at a temperature of approximately l,I00 C. conducted for a period of 16 minutes while the temperature of the surface of the encased iron pipe was measured at 2-minute intervals. The mean temperature did not exceed 260 C.
  • the materials used for the continuous strips may be varied depending upon the helicoid product produced.
  • the materials may be paper, plastic, sponge rubbers, foamed plastics, glass fiber cloths, and metals. Materials of a fibrous or spongelike nature may utilize impregnants, which preferably are in a nonhardened or uncured stage when passing through the rolls.
  • impregnants which preferably are in a nonhardened or uncured stage when passing through the rolls.
  • the materials of the strips may be different, as for example, in wrapping electrical conduits a variety of insulation materials are desirable.
  • silicones, thermoplastic resins, thermosetting resins such as polyester, epoxy and phenols, may be used as impregnants for one or more of the strips.
  • Nonhardened or uncured impregnants are particularly useful in providing a good bond between the overlapping portions upon subsequent cure.
  • the elastomer of one strip may temporarily combine or fuse with the elastomer of the adjacent strip. Upon curing of the elastomer, the fusion is fixed to such an extent that the materials act as an original composite rather than joined strips. Curing or hardening may be effected by an air cure or by oven cure.
  • the material may be left on the core as a protective covering, as for example, as a wire insulation.
  • it may be removed from the core and cut in lengths or wound upon itself, such as in B-X cable.
  • the strip material is formed of asbestos fibers. Plain weave fabric of about 1-3 mm. thickness made of threads or yarns of asbestosfibers is particularly suitable. However, any other flexible webs such as nonwoven felts, knit fabrics or the like of good strength characteristics are contemplated for use a as the base for the strips in the laminated products. Use of asbestos fibers only in the webs is preferred, but inclusion of other heat-resistant fibers, e.g., glass fibers, in various amounts, e.g., up to 25 percent is contemplated as an altemative.
  • the three strips of material are preferred to be of equal widths.
  • the thicknesses and impregnants may vary, depending upon the materials used.
  • the temperatures of the individual strips are at ambient and the rolls are unheated. There may be a slight temperature rise above ambient at the rolls, depending upon the compression upon the materials. With metals and with certain impregnants, the rolls and/or the strips of material may be heated to improve the drawing effect or to assist in the hardening or cure of the impregnant.
  • the feed reels are in a general planar position on fixed bearings. This arrangement not only provides for ease in substituting a full reel for an empty one, but abo facilitates adjustments of the apparatus, such as the tensions on springs, without stopping the machine operation. Where the reels are wound around the core, as in wirewrapping apparatus, such simple adjustments cannot be made without stoppage. Moreover, with the reels rotating but fixed relative to each other, visual inspection is readily made of all portions of the apparatus in relative safety.
  • An important feature of the new heat-protective coverings is the overlap configuration provided along edges between separate coils or turns of the helicoid structures. This has been discovered to provide good flexibility without allowing fishmouthing at bends or creation of other openings when the encased conduit is bent or flexed.
  • the degree and nature of the overlapping can be varied by selection of sizes for individual tapes forming the laminations of the product, degree or edge overlap and the like. Simplicity of construction and manufacture, however, make it advantageous to use all tapes of equal width and to use an equal amount of edge overlap at each side of the product.
  • any suitable number of strips of elastomer coated cloth may be used to form the insulation covering. As indicated previously in describing a four-ply product, a plurality of strips may be manifolded to form a single step of the covering. This permits production of the new products to be varied for special end uses employing a minimum number of basic fabricating elements.
  • elastomers are available for use in forming the elastomeric coating compositions used in the new insulation coverings Elastomers having the highest degree of heat and oxidation resistance at a reasonable cost are advantageously used.
  • Polychloroprene and ethylene-propylene rubbers are preferred elastomers.
  • Silicone rubbers are another useful class of elastomers.
  • Elastomers of acrylic type polymers, e.g., 1-6 carbon atom alkyl esters of acrylic and methacrylic acids, chlorinated polyethylenes, and other elastomers of high-temperature resistance known to the art are contemplated for use in the invention. Mixtures of two or more elastomers may be employed.
  • the elastomeric coating compositions are prepared for coating of the flexible asbestos fiber webs according to industry-recognized procedures and formulations. Suitable compositions may contain from 5 to 50 percent solids and 50 to 95 solvents or dispersants, although other proportions may also be used in special cases. Solvent solutions or emulsions may be employed. Nonflammable solvents are preferred in forming the elastomeric solutions or so-called cements", e.g., haloalkane like tetrachloroethylene, dichlorotetrafluoroethane, carbon tetrachloride and the like.
  • cements e.g., haloalkane like tetrachloroethylene, dichlorotetrafluoroethane, carbon tetrachloride and the like.
  • the nonvolatile portion of the coating compositions in addition to an elastomer, will advantageously include antioxidants vulcanizing agents, fillers, pigments, plasticizers, accelerators and similar additives known to the rubber industry. Fillers are usually employed in amounts of to 60 parts filler per parts elastomer. The other additives advantageously amount to 0.01 to 10 percent, especially 0.5 to 5 percent, of
  • fillers which may be of the reinforcing type, as well as inert type, include magnesium carbonate, zinc oxide, carbon blacks, hard clays, calcium silicates, blanc fixe, whiting, talc, slate four, infusional earth and the like.
  • pigments examples include carbon black, iron oxide red and yellows, titanium dioxide and comparable inorganic pigments.
  • accelerators include mercaptobenzothiazole, benzothiazyl disulfide, metal dialkyl dithiocarbamates, alkylene thiuram tetrasulfides and the like.
  • antioxidants hydroquinone, monobenzyl ether, p-isopropoxy diphenylamine, phenylnaphthylamine, styrinated phenols, octylated diphenylamines and the like.
  • plasticizers and softeners examples include hydrocarbon oils, polyolefins, aromatic oils and the like.
  • vulcanizing agents include sulfur, tetra methylthiuramdisulfide, zinc oxide, magnesium oxide, organic peroxides and the like.
  • the elastomeric coating compositions are prepared and fonnulated according to commercial practice for rubber compounding and use. Future improvements in this art, therefore, should be adapted to continually upgrade products, basically designed in accordance with the invention, to give the highest possible values for all desirable qualities in the final product.
  • a helicoid laminate comprising:
  • adjacent helicoid portions of a strip are in a butt joint relationship with each other while adjacent portions of the laminate are in a ship-lap joint with respect to each other.
  • a helicoid laminate according to claim 1 in which at least two of said strips are silicone strips in contact with one another.
  • a helicoid flexible covering for tubular conduits to provide heat and flame protection to the conduit comprising:
  • said strips being joined in a staggered configuration with the edge of at least one strip being offset from the edge of at least one other strip; at least one of said joined strips being of unequal length with an adjacent strip thereby providing an incurvature in the joined strips forming a helicoid;
  • said staggered configuration being cured into the helicoid, integral structure, having ship-lap joints between adjacent coils, said structure being capable of being repeatedly coiled and uncoiled so the insulation wrap may be repeatedly installed and removed from a tubular conduit without damage.
  • a helicoid flexible covering as claimed in claim wherein the fibrous cloth is asbestos cloth and the bonding agent is an elastomeric material.
  • a helicoid flexible covering as claimed in claim 5 formed of three strips of equal width of asbestos cloth, the inner strip being offset to one side of the central strip and the outer strip being offset to the other side of the central strip.

Abstract

Helicoid products comprising several continuous tiered strips are made by superposing at least two continuous strips with their edges overlapped, incurvating the strips and durably adhering together the contacting faces of the strips. The resulting helicoid product may be conformed to a mandrel and cured, vulcanized or otherwise treated to acquire a durable tubular helicoid form. This technique is particularly useful in making helicoid coverings that may be repeatedly put on and removed from tubes, rods, wires and the like, as coverings, firesleeves, or insulation, for example.

Description

United States Patent Inventors Harold J. Reynolds, Jr.
Raritan; George P. Leistensnider, Somerville; Angelo A. Forte, Raritan, all of NJ. Appl. No. 701,424 Filed Jan. 29, 1968 Patented Oct. 26, 1971 Assignee Johns-Manville Corporation New York, N.Y.
HELICOID LAMINATE COMPRISING SEVERAL CONTINUOUS TIERED STRIPS 11] Claims, 9 Drawing Figs.
US. Cl 161/47, 138/129,138/130,138/131,138/144,138/150, 156/184,156/191,156/195,156/l99, 156/229,
Int. Cl F161 9/14, F16159/02 Field ofSearch 138/129-133,
References Cited UNITED STATES PATENTS 2,225,026 12/1940 Welsh 138/129 X 2,315,217 3/1943 Obiglio..... 156/192 X 2,468,589 4/1949 Cryoretal.... 138/133 X 2,676,127 4/1954 Hansen 138/129 X Primary Examiner-John T. Goolkasian Assistant Examiner-Joseph C. Gil Attorneys-John A. McKinney and Robert M. Krone ABSTRACT: Helicoid products comprising several continuous tiered strips are made by superposing at least two continuous strips with their edges overlapped, incurvating the strips and durably adhering together the contacting faces of the strips. The resulting helicoid product may be conformed to a mandrel and cured, vulcanized or otherwise treated to acquire a durable tubular helicoid form. This technique is particularly useful in making helicoid coverings that may be repeatedly put on and removed from tubes, rods, wires and the like, as coverings, firesleeves, or insulation, for example.
PATENTEDUCI 26 I97! 7 3,51 12 3 sum 2 F 4 F ,5. Flip 8 5 l2 4 INVENTORS,
HAROLD J RE Y/VOL/JS, JR. GEORGE P LEISTENS/V/OER ANGELO A FORTE ,4 MUM? BY am M; m. KW,
ATTORNEY) PATENTEnum 2s nan 3, 6 l 6, 123
sum 3 or a g 7! A 70 \V A v gym A 94 IN VENTORS /0 HAROLD J REYNOLDS, JR
---- GEORGEPLE/STENSN/DER ANGELO A. F0275 & jn fi mm? 7. M
ATTORNEYS PATENTEnnm 2s IBYI SHEET 0F 4 4. mc m7 mm ORNEYS HELICOID LAMINATE COMPRISING SEVERAL CONTINUOUS THEMED Sfi BACKGROUND OF THE INVENTION 1. Field ofthe Invention This invention relates to a method of forming several strips of material into a unified helicoid form, which can beused for novel covering materials or which upon hardening or curing of an impregnant can be formed into a novel type of conduit. In a specific way, the invention concerns a type of tubular covering that is flexible, fire-resistant and capable of repeated coiling and uncoiling installation and removal without damage about a tube, rod, wire, pipe, hose or the like to function as a firesleeve, packing, and the like.
There are numerous structures which require fluid conduits to be protected against heat and fire by some form of protective covering and yet the fluid conduits must be frequently inspected for possible damage, structural defects or the like while the protective covering is removed. Important examples of this are the hydraulic power-transmitting or fluid-conducting lines of aircraft. Such lines must be protected against fire or other adverse heat conditions, particularly in new highspeed jet aircraft but must be capable of being quickly and frequently inspected for possible structural defects. Flexible metal hose which is employed in such aircraft structures may, for example, be required to withstand an l,l C. flame on the surface for 15 minutes without exceeding a temperature of 260 C. on the inside. The flexible metal hose itself is incapable of providing such characteristics and it is necessary for it to be provided with some form of heat-protective covering, i.e., a fire sleeve.
Insulation materials in the form of ribbons or tapes which can be wrapped about a tubular conduct are known. However, the time required to remove and reinstall such insulation coverings to permit inspection of the thermally protected conduit renders this type of product unsuitable for use where easy and frequent inspection of the conduit is required. Some form of insulation covering having a relatively permanent shape and yet which may be readily applied and removed is in demand by the aircraft construction industry and by others.
Use of coverings provided with fasteners such as zippers, hooks, buckles and the like have been investigated. All such removable insulation coverings, however, display poor flexibility when assembled upon a flexible hose and undergo fish mouthing on the compression side of a bend. Zippers and similar closure units which were attached to the insulation covering by machine stitching or the like tend to break loose at the stitch under tension when the enclosed flexible metal conduit is flexed. Also, covers using hooks, buckles and the like are difiicult to install.
DESCRIPTION OF THE PRIOR ART Various techniques are known to make helical wrappings, coverings and conduits. For example, a single strip of material has been spirally wrapped on a conduit so as to be in continuous edge-abutting arrangement and provide an insulation covering for the conduit (US. Pat. No. 1,937,561). A modification of this basic concept involves use of a covering strip made to prevent sticking of the tape to the encased pipe or tube so that the tape may be unwound without damage (U.S. Pat. No. 2,353,494).
In addition to limp tapes having no form except the shape to which the tape is applied, it is also known to form insulation tape which is resiliently preformed in a spiral shape so that it can be handled more easily during installation upon or removal from a tubular conduit (U.S. Pat. No. 2,468,589). Such tape offers little or no heat protection at the abutting edges of the coils in the spiral shape.
In terms of prior practices which are not limited to insulation coverings, but generally concern helical products, the formation of structures from rubber, fabric and other materials in a permanent spiral shape or helicoid configuration has been practiced for many years, e.g., formation of piston packing (U.S. Pat. No. 143,705), pneumatic tire inner tubes (US. Pat. No. 1,428,382) and rubber tubing (U.S. Pat. No. 1,940,145). It is also common practice to make flexible hose, pipe or other conduits by spiral winding of layers of materials upon a forming mandrel or the like (U.S. Pat. Nos. 2,759,521; 2,913,011, and 3,252,483). Tubing may be formed by the helical winding of strips in combination with shaping wires or other metal inserts upon some form of helix-forming rolls (see U.S. Pat. No. 2,674,298 and 3,191,631).
It is, of course, well known to form tubing by the spiral winding of individual strips of material around a rod (U.S. Pat. No. 3,279,333). The spiral wound product may be a self-supporting pipe or tube (U.S. Pat. No. 2,161,036) or may be a covering for a pipe to protect it against corrosion or for heat insulation purposes (U.S. Pat. No. 2,7l3,383). In such operations, a plurality of strips may be employed and formed in overlapped or staggered relationship between joints in the resulting tubular structure (U.S. Pat. No. 2,225,026). Moreover, complicated equipment may be used to get a tight telescoping interfitting of the helices by edge crimping (U.S. Pat. No. 2,759,521). a
In view of the numerous prior developments as mentioned above, it is apparent many procedures are available for making coverings and other products by helical winding of strip materials. However, in the prior methods, there have been no provision for properly joining several strips of like or unlike materials so as to make a helicoid wrap or to make allowances in the joined strips so that a loose or tight helix can be formed. In the specific case of heat-protective wraps or coverings for metal tubes, pipes and other tubular conduits, moreover, there is a need for improved products that may be installed and removed repeatedly without disassembly of the conduit and without detriment to the conduit or covering.
OBJECTS A principal object of this invention is the provision of new forms of helicoid tubular products.
Further objects include the provision of:
1. New methods of forming helicoid heat protective coverings for conduits.
2. New forms of such coverings for tubular conduits that may be installed and removed repeatedly without disassem bly of the conduit and without detriment to the covering.
3. Such coverings of improved type having the further feature of being relatively noncorrosive to metal conduits to which the insulation may be appied.
4. New helicoid coverings that may 'be used to protect and flameproof wire bundles, tubes, pipes or the like where ease of application of the coverings is important, such as in tight quarters or where repeated inspections of the enclosed conduit are required.
5. Methods of making such new flame protection products from readily available materials with uncomplicated equipment and at relatively low cost.
6. New forms of helicoid coverings that provide good protection to an encased tubular conduit at the junctions between separate coils of the helicoid structure.
7. Heat protection wraps that provide multiple layers of insulation over an encase conduit yet permit a good flexibility to be maintained throughout the entire assembly.
8. New methods of joining two or more strips of like or unlike materials into a laminate, wherein allowances are provided for helicoid winding or wrapping of the laminate.
9. New methods of helically winding two or more strips of like or unlike materials into a loose or tight fitting helicoid arrangement, useful for a covering, or conduit or tube.
10. New forms of apparatus for creating helicoid tubular products for a plurality of continuous strips of binder-impregnated fibrous material or equivalent: material.
Other objects and further scope of applicability of the present invention will become apparent from the description given hereinafter; it should be understood, however, that the detailed description and specific examples, while indicating preferred embodiments of the invention, are given by way of illustration only, since various changes and modifications within the spirit and scope of the invention will become apparent to those skilled in the art from this description. It should also be understood the foregoing abstract of the disclosure is for the purpose of providing a nonlegal brief statement to serve as a searching-scanning tool for scientists, engineers and researchers and is not intended to limit the scope of the invention as disclosed herein nor is it intended it should be used in interpreting or in any way limiting the scope or fair meaning of the appended claims.
SUMMARY OF THE INVENTION The foregoing objects are accomplished in accordance with the invention by formation of helicoid products by superposing at least two continuous strips of material in a stepped, overlapping relationship, incurvating the superposed strips and durably adhering together the contacting faces of the strips. The incurvation of the strips may be attained by stretching or tensioning or unequal lengths of strips may be supplied to the superposing that creates the laminate. The emitted laminate thereby curves itself into a continuous helicoid form.
In the specific embodiment of this general technic in which helicoid heatand fire-protective wraps or coverings are formed, the operation comprises:
a. providing a plurality of strips of fibrous cloth;
b. the strips being impregnated with binder composition, such as an elastomeric material;
c. the strips are assembled in a tiered and staggered configuration with the edge of at least one strip being offset from the edge of at least one other strip; and
d. said staggered configuration is cured into a helicoid integral structure having overlapping butt joints between strips of adjacent coils so that the structure is capable of being repeatedly coiled and uncoiled so that the insulation wrap may be repeatedly installed and removed from a tubular conduit without damage.
In an exemplary form of the helicoid coverings, three strips of equal width of asbestos cloth are used, with one outer strip staggered to one side of the central strip and the other outer strip being staggered to the other side of the central strip. Advantageously, for situations where protection of an encased metal conduit against corrosion are important, the inner face of the insulation wrap may be formed of material different from the remaining structure, e.g., an inner surfacing of ethylene-propylene rubber composition of low-corrosion properties to metal as compared with asbestos fibers and polychloroprene rubber used in forming the remaining portion of the insulation wrap.
In other embodiments, the new helicoid products may be of a double-ply or a quad-ply construction, all of which employ the staggered or overlap edge arrangement which provides ship-lap joints between adjacent coils of the laminate in the helicoid product.
The success in forming helicoid products of this new type is in part due to the discovery that a helicoid configuration can be imparted to laminate strips of elastomer impregnated and coated fibrous cloth by a simple operation of imposing an arcuate configuration to the strips during their contact in the formation of an edge staggered lamination. This principle is employed in the method of forming the new insulation wraps which comprises:
a. providing a plurality of separate strips of fibrous cloth impregnated and covered with uncured, tacky elastomeric material;
b. bringing said separate strips into generally parallel alignment;
c. contacting opposed faces of the strips in a staggered arrangement with the edge of at least one strip being offset from the edge of at least one other strip;
d. imposing an arcuate configuration to the strips during said contacting;
e. recovering from step d an uncured open helicoid laminate of said plurality of strips;
f. treating the uncured lamination with a release agent;
g. winding the treated, uncured lamination about a mandrel in a tight helicoid configuration;
h. subjecting the mandrel wound lamination to necessary conditions to cure the elastomeric material contained therein; and
i. removing the cured helicoid lamination from the mandrel. It has been found that the imposition of an arcuate configuration is advantageously accomplished by passing the parallel aligned separate cloth strips in the uncured, tacky condition through opposed driven rollers which have lands or steps of different diameters which contact different strips or parts of the widths of different strips and drag these strips or parts forward at different angular velocities. The effect of this is to produce incurvation of the laminate which, in turn, causes it to assume an open or loose helicoid configuration. It is then relatively easy to wrap the uncured laminate into a tight spiral about a mandrel and to cure the product upon the mandrel so it acquires a tight permanent helicoid configuration which strongly reverts to a coiled condition when an attempt is made to uncoil the structure.
BRIEF DESCRIPTION OF THE DRAWINGS A further understanding of the new products, methods and apparatus of the invention may be had by reference to the accompanying drawings in which:
FIG. 1 is a flow sheet diagrammatically illustrating the materials and method steps employed in the formation of preferred new products of the invention;
FIG. 2 is a side view, partially broken away and sectioned, of one form of a helicoid product of the invention having a tri ply structure;
FIG. 3 is a side view, partially broken away and sectioned, of another form of helicoid tubular covering of the invention;
FIG. 4 is a side view, partially broken away and sectioned, of a further embodiment of helicoid tubular covering of the invention;
FIG. 5 is a diagrammatic side view of apparatus used in the helicoid preforming step of the new methods;
FIG. 6 is a perspective view of loose helicoid uncured preformed material as formed by the new processes;
FIG. 7 is a fragmentary enlarged view of the structure of stepped driven rollers used in accordance with the invention to create the helicoid perform such as shown in FIG. 6.
FIG. 8 is an elevational view, partially in section, of another form of apparatus used in joining two strips of material being fed into opposing rolls in accordance with the invention;
FIG. 9 is a side view of the apparatus of FIG. 8 in which the laminate is wound on a tube.
Referring in detail to the drawings, the tri-ply form of insulation wrap 2 shown in FIG. 2, as applied to metal pipe 4, consists of three separate strips 6, 8 and 10 of asbestos cloth impregnated with an elastomeric material. Inner strip 10 is offset to one side of the central strip 8 while the outer strip 6 is offset to the other side of the central strip 8. Consequently, there are ship-lap-type joints 12 between the adjacent coils 14a, 14b, 14c, etc., of the helicoid structure. Each turn of the insulation wrap nests into the adjacent turn or coil in the manner of a bell-and-spigot joint. This arrangement provides excellent flexibility without fish-mouthing at bends and also gives uninterrupted protection to the encased conduit against external flame or heat.
In order to hold the wrap 2 tightly upon the metal pipe 4 and prevent accidental movement or unwrapping, straps or clamps 16 may be applied at opposite ends of the insulation wrap 2 or at any other appropriate position.
In the embodiment shown in FIG. 3, the insulation wrap 20 is of a bi-ply construction formed of an outer strip of elastomeric impregnated asbestos fiber cloth strip 22 and an inner strip 24. Strips 22 and 24 are laminated to one another along an interface 26 so that the two strips 22 and 24 form an integral unit. Theedge 28 of the strip 22 is offset from the edge 30 of the strip 24 in a staggered arrangement. Ship-lap joints are provided between adjacent coils of the laminate, with the joints in between coils of single strips being in a butt arrangement 32.
In the form of insulation wrap shown in FIG. 4, which is of quad-ply construction, the insulation wrap 40 comprises an outer strip 42, a pair of central strips 44 and 46 and an innermost strip 48. The central pair of strips are in full register with their longitudinal edges aligned thus creating the central section in the insulation wrap of this embodiment of double thickness. The edge 50 of the outer strip 42 is offset to one side of the central ply while the edge 52 of the inner strip 48 is offset to the opposite side of the central ply. As a result, the
ship-lap joints 54 between adjacent coils 56a and 56b, etc., of
'the insulation wrap are fully overlapping at all points throughout the entire area of the wrap when installed upon the metal pipe or tubing 4.
Referring now to FIG. 5, there is illustrated a preferred method of forming insulation wrap such astri-ply wrap (FIG. 2).
Separate reels 60, 62 and 64 of asbestos fiber cloth impregnated and covered with uncured, tacky, elastomeric material are mounted for free rotation upon supportingshafts 66, and 70. Spring loaded retainers 67, 69 and 71are used, the tensions of which may be adjusted to control the relative unrolling of strips 6, 8 and 10. In order to prevent sticking of t separate convolutions in the rolls of cloth strips, they have coverings of thin separator strips 72, 74 and 76 which are pulled from the respective strips 6, 8 and as they are unrolled and carried to the opposed driven rollers 78and 80.
As seen in FIG. 7, the top roll 78-is carried on a driven shaft 82 and has a series of steps or faces 84, 88, 90 and a gear 92. Similarly, the roller 80 carried upon the driven shaft 94 is formed with a series of steps 96, 98, 100, 104 and a gearl06, the latter meshing with gear 92. Face 90is of the same diameter as face 84, while on roll 80, face 104 is of the same diameter as face. 96. Face 90 and a portion of face 84' mate with steps 96 and a portion of step 104 of the roll 80 which serves to align and limit the two rolls 78,80 in operation when the rolls are biasedtoward eachpother under spring-loaded pressure by spring means (not shown). Power is provided from a source (not shown) through themeshing gears (not drawn to scale) 92, I06.
In roll78, face 88 is of lesser diameter than faces'84, 903 Roll 80 has a three-step arrangement, in that step 100 is of smaller diameter than step 104, while step 98 is of smaller diameter than step 100.
Step 88 is equal in width to the upper strip 6', step 100 is equal in width to one-half of strip 8, and step 98-is equal in width to the width of strip 10. In a three-ply arrangement, the widths of the three strips are preferably the same, so that if step 88 has a width x, step 100 has a width of x/2, and step 98 has a width ofx.
The relationship of the diameters of the two rolls 78, 80 is such that the smaller step 881s always larger than the diameter of step 98. Actually, the step from the larger face 84, tothe smaller 88 is quite small, and the stepping down from step 104 to step 100 to step 98 is quite small. The opening between the rolls 78 and 80 is exaggerated for purposes of clarity. The diameter of steps 84, 90 compared to the diameter of steps 96, 104 is in the order of 1.6:], so that roughly the diameters of steps 88, 98 are in a similar ratio. This ratiocan be altered depending upon the degree of curvature desired to be applied to the formed laminate 6, 8 and 10.
Steps 88 and a portion of steps84 of roll 80 create the pressure to force opposing faces of the strips 6, 8 and 10 into contact with one another into a staggered arrangement as illustrated in FIG. 7 and cause the tacky faces of the strips which are in contact with one another to stick together. At the same 9 the length of strip 8. Similarly, more of strip 8 is fed past the point of contact per unit time than of strip I8. Unequal feeding from the rolls 68, 62, 64 is evidenced in that reel 68 is the first to unwind completely, reel 62 is the next to be unwound completely, and reel 61lis the last to unwind its material. The relative rates of unwinding which in turn is usually indicative of the degree of curvature imparted to the laminate 6, 8, I8, is controlled by the relative tensions of retainers 67, 69 and 7 I, the diameter of roll 78 relative to the diameter of roll 80, the pressure loading on the two rolls 78, 88 and the speeds of rotation of the two rolls. Consequently, the laminated strips as they issue from the contacting rolls 78 and form an uncured open helicoid lamination 188. This open lamination is illustrated in more detail in FIGS. 5, 6.
Referring to FIGS. 8 9, two separate strips of impregnated materials, 'and 112, are fed from reels 116a, H241 to between two sets of opposed cylindrical rolls I18, I16 and I18, 120; reels 1I0a and 112a have joined thereto springs lI0b and 11211 which control the tension of unreeling. The springtension of each is adjustable to control the relative rates of feed of strips I I0, 112. FIG. 8 depicts the exit of the materials from, between the rolls. The materials are in a stepped, overlapped relationship, in that a side end portion I22 of strip I10 mates with side end portion 124 of strip II2. Roll H6 is larger in diameter relative to adjacent roll II6, and roll II8 is larger in diameter than adjacent roll 120. Roll II6 is also larger in diameter than the larger roll I18. Roll U4 is also larger in diameter than the diameter of :roll I26.
In passing through the opposed rolls, overlapped portions 122, 124 are under compression, and in addition, the free side end portions 126, 128 are also under compression. The degree of compression is related to the spacings between the opposed rolls, the loading on the rolls, the tension of springs IItlb, 112b, and the relative thickness of the two strips of materials.
It is believed that the principles of incurvation of the joined strips are as follows. Strips I10 and I12 are fed in constant feed throughthe opposed rolls, being drawn through by the rate of rotation and relative diameters of the rolls. However, the rate of feed from reel 118a is greater than the rate from reel 1120. The overlapped portions 122, 124 have a tendency to be drawn through linearly. Since the diameter of roll IId is larger than the diameter of roll I20, side portion I28 has a tendency to be pulled'through faster :for example when the rate of rotation of roll II4 is greater than the rate of rotation of roll 120; Depending upon the type of material used for strip 1 10, the tension on springs 11812, 11212, and also strip temperature or the temperature of the rolls, sidle portion 128 is either stretched, calendered to a greater degree than adjacent portion 124, or placed in tension relative to side end I26, or simply its strip is drawn through faster than adjacent stripl I2.
Meanwhile, free side end portion 126 of strip II2 appears to pass between opposed rolls II6 and 128 so that it is either in compression, or under slight tension but much less than the tension withinside end 126, or neither under tension nor compression. The joined strips I18, I12 emitted from between the rolls incurvated to the right in FIG. 8 in a continuous arc.
If the same amount of material is placed on reels IItla, II2a at the start of a forming operation, at the end of the cycle reel 110a will have unwound before reel Ill2a. This clearly indicates of course that although a constant feed from each separate reel is used, the rate of feed from one reel to the next is different. The amount of material left on reel 112a when reel llItla is unwound is a function of the factors mentioned, that is, tension of springs lItIb, 1112b, temperature of the strips, the type of material used for the strips, the relative sizes of the rolls, and the loading on the rolls.
If a length of joined strips is cut off, it freely assumes the shape shown in FIG. 6, being that of a continuous, loose helicoid. The laminate may be used as'is, or it may be wound on a mandrel or rod 130 (FIG. 9). In FIG. 8, it is seen that sidewall 118a of roll 118 acts as an end guide for strip 112, while sidewall 116a of roll 116 acts as an end guide for strip 110. This guide arrangement controls in precision the continuous overlap of the two strips 110, 112. When the produced helicoid is wound on a mandrel 130 (FIG. 9), not only are the adjacent strips 110 of the laminate in abutment, but the adjacent strips 112 are also in abutment relative to each other. In addition, a joint between adjacent strips 112 (FIG. 3) is superimposed by a solid portion of superimposed strip 110 so that the laminate itself produces ship-lap joints between adjacent coils of the laminate.
The laminate may be wound on a core so that a solid or continuous covering 112 is applied on the core, and a second continuous covering 1 10 is superimposed over the covering 112.
If desired, the tight abutment or tight helix arrangement may be a loose helix, so that spacings exist between adjacent strips 110 and adjacent strips 112. This, of course, depends upon the type of covering desired to be formed or the type of product desired to be produced.
The impregnant in the strips may thereafter be cured or hardened. The resultant product is either a solid tube or a wrap or covering which can be wound and unwound. Generally, heat is applied to cure or harden the impregnant, using techniques that are well known. If a polyester resin, for example, is the impregnant, fusion of the resins in the strips occurs so that a hard, unified product results.
The laminate veers to the right in arcuate form (FIG. 8). An end of the laminate is applied to a rotating core 130 so that a helicoid wrap is formed directly adjacent the exit end of the opposed sets of rolls. On the core 130 the individual strips 110, 112 are in abutment with adjacent strips. All helicoid strips (actually being one continuous strip) are in abutment with each other to provide a solid covering; all strips 110 are in abutment with each other to provide a solid covering over strip 112. The coils of the complete laminate form ship-lap joints between each other.
The laminate on the core 130 may thereafter be subjected to heat to provide a cure or hardening of the impregnant. Depending upon the product desired to be produced, the strips may be only amalgamated to each other to form the helicoid laminate or the impregnated may be fused throughout to form a solid tube upon removal of the core 130.
DISCUSSION OF THE METHOD An advantageous sequence of steps which may be used to produce new heat protective coverings of the invention is outlined in the flow diagram constituting FIG. 1. A first stage of the operation is the provision of a plurality of separate strips of asbestos fiber cloth impregnated and covered with uncured, tacky, elastomeric or other binder material. Such strips could be obtained from a commercial source, but in a fully integrated operation, the attainment of such strips would advantageously begin by the coating and impregnating of woven fabric made from asbestos fibers with an elastomeric material composition, e.g., a solvent solution of the material known as coat cement. Any suitable method of applying the elastomeric material coating may be employed, such as knife coating, roller coating, spraying, dipping and the like. A preferred method is the so-called divine coating technique which results in a major portion of the coating material being retained on the surface of the cloth and only a minor amount of the coating penetrating into the interstices of the cloth.
Each of the separate strips which are to be plied together to form the lamination may be coated with the same elastomeric composition. However, in special cases, such as where maximum protection against corrosion of metal conduit by the insulation wrap at elevated temperatures is required, one or more surfaces of the strips may be coated with an elastomeric composition having very low corrosive characteristics. Thus, a preferred form of the new insulation wraps may employ ethylene-propylene rubber compound (EPDM) to coat the surface of the insulation wrap and would be in contact with the metal pipe (e.g., the inner surface of strip 10 in FIG. 2). In such a preferred tape, the remaining surfaces of the strips would be coated with a polychloroprene composition. Such a procedure is illustrated in FIG. 1 by a portion of the flow diagram which shows in dotted flow lines the optional different spreader coating step which can be employed where special surface coatings are used. In the procedure as illustrated in FIG. 1, one surface of a strip of asbestos cloth would be coated upon one side with elastomeric coat cement and on the other surface with a special surface coat.
The coating and impregnating operation will advantageously be accomplished using drying ovens or comparable equipment to evaporate solvents and other volatile material from the coating composition and leave the asbestos cloth impregnated and covered with an uncured, tacky, elastomeric coat. Normally, the resulting coated asbestos cloth will be rolled into a jumbo roll for subsequent processing. As this is accomplished, a release sheet of polyethylene film, holland cloth or comparable separator sheet will be applied to one sur' face of the coated asbestos cloth so that the cloth may be formed into rolls without convolutions adhering to each another.
The cloth is next slit into narrow widths, e.g., about 1 to 5 cms. These are then rolled into separate rolls of suitable diameter, e.g., 10 to 50 cms., for ease of handling in subsequent operations, such as reels 60 to 64 of FIG. 5.
The next stage of the operations is the helicoid preforming which has generally been described previously in connection with FIG. 5. Basically, the operation involves bringing the separate strips of whatever desired number, advantageously between 2 to 4 separate strips, into generally parallel alignment, contacting opposed faces of the strips in a staggered, tiered arrangement with the edge of at least one strip being offset from the edge of at least one other strip. Such staggered arrangements may take various forms, as illustrated in FIGS. 2 through 4. With a two-ply construction such as in FIG. 3, little variation is possible except in the amount of overlapping at the edge between the separate strips. Where the three-ply construction is employed, equal overlap between the top and bottom strips relative to the central strip (see FIG. 7) is advantageous. In a four-ply construction (see FIG. 4) two central strips may be fully aligned with no overlap to provide a double-thickness central ply. An alternative to this would be to use a three-ply construction with the asbestos cloth for the central portion being heavier in weight or of different woven construction than the strips for the two outer plies.
The strips are incurvated as described hereinbefore. As the strips contact under such conditions, the resulting laminated structure assumes an open loose helicoid form as illustrated in FIG. 6. This loose helicoid product may be produced and handled in continuous length or suitable measured lengths may be cut from the product issued from forming rolls for handling in subsequent steps of the operation.
Following the formation of the helicoid preform, it is treated by dusting with release or antitack material to prevent exposed surfaces from sticking together or sticking to the mandrel in the subsequent operations. Any suitable material known to the rubber-processing art as satisfactory dusting agent may be employed for this purpose including powdered mica, soapstone, chalk, calcium carbonate, or the like. Such dusting may be accomplished in wind tunnels, by spraying, in tumbling barrels or other suitable equipment.
Following the dusting, the loosely coiled helicoid preform is wound upon a mandrel having a suitable outside diameter to form an inside diameter to the insulation wrap of approximate size to encase the tubing or conduit to be covered by the wrap. Metal rods or pipes are advantageously used as mandrels. high-carbon steel or stainless steel being examples, although any other suitable materials including ceramics, glass, or the like, may be used for the mandrel. Application of a release coat upon the surface of the mandrel prior to wrapping the helicoid preform is recommended in order to insure easy and clean removal of the finished product from the mandrel after the cure.
The curing step is performed using curing conditions as recommended by the manufacturer of the elastomeric material used in the initial coating stage of the operation. As is known to those associated with curing or vulcanizing of rubber of comparable curable elastomeric materials, such conditions may be varied. In some special cases, air curing at ambient temperature over substantial lengths of time may be used, e.g., with silicone elastomers. Normally, however, curing isaccomplished by heating the mandrel-wrapped product to an elevated temperature, e.g., ISO-250 C. for about I to 72 hours. Induction heating, infrared heating, or the like may be employed instead of themore common heating in electrical resistance or gas fired ovens. Where hollow mandrels are employed, heat exchange liquids may be circulated throughthe interior of the mandrel in order to provide all or part of the heat.
Following the curing, the cured helicoid lamination is removed from the mandrel and may be used for intended purposes without further treatment. Normally, however, the product will be trimmed at the edges toprovide sharp, neat product or may be cut to smaller lengths as required by the trade or special purchaser. Additionally, the subsequent handling may involve wrapping, packaging and the like.
EXAMPLES The following details of operations in accordance with the invention and reported data illustrate the further principles and practice of the invention to those skilled in the art. In these examples and throughout the remaining specification and claims, all parts and percentages are by weight and all temperatures are in degrees centigrade unless otherwise specified.
EXAMPLE 1 This example illustrates the production of a three-ply construction insulation wrap having a low corrosion internal surface in various sizes.
A standard GR-M rubber cement consisting of about 85 percent volatile haloalkane solvent and 15 percent elastomeric mix was used as the principal elastomeric coating material for the production run. The elastomeric mix in the cement was formed of rubber (100 parts), benzothiazyl disulfide (1 part), plasticizer (2 parts), stearic acid (0.5 parts), zinc oxide parts), magnesium carbonate (4 parts), antioxidant (2 parts), carbon black (5 parts) and hard clay (40 parts).
A standard plain weave cloth made of asbestos fiber yarn having a thickness of about 2.5 mm. was doctor-blade coated with the above coating cement at a rate of about 20 percent on each side based upon the weight of the cloth. The coated cloth was dried in a hot air oven and polyethylene film wasapplied to one surface as a masking. The cloth was slit into tapes of 2 cm. width and the tapes were wound into small rolls of about meters in length with the polyethylene masking between convolutions.
In another operation, the same cloth was coated upon one side at the 20. percent rate with the GR-M cement and upon the other side at a percent rate with a similar standard coating cement used ElPDM rubber as the elastomer base rather than the GR-M rubber. This different surfaced cloth was also slit into 2 cm. tapes and wound into 15 meter length rolls with a polyethylene film separator.
Two rolls of the first tape and one roll of the second tape were mounted on a helicoid preform machine of the type described hereinbefore. Before the tape from each roll was passed through the lamination rollers, the polyethylene masking strip was peeled from the tape. The driven rollers of the machine were operated at about 35 r.p.m. and a helicoid preform of tri-ply construction was formed at a rate of about 2.5 meters per minute. As the preform emerged from the forming rolls, it was dusted with powdered mica.
The dusted preform was tightly wrapped upon a 5/16 in. OD. mandrel formed of Teflon" coated aluminum tubing on an arbor-type lathe maintaining about I to 2 mm. space at the joints while wrapping. The mandrel wrapped material was then vulcanized in a circulating air oven for 1 hour at about C. The vulcanized product was removed from the oven and cooled to ambient temperature, removed from the mandrel and end trimmed.
The resulting insulation wrap was installed upon black iron pipe and subjected to a standard heat transmission test in which the outer surface of the wrap is subjected to a flame maintained at a temperature of approximately l,I00 C. conducted for a period of 16 minutes while the temperature of the surface of the encased iron pipe was measured at 2-minute intervals. The mean temperature did not exceed 260 C.
In similar runs, preforms for larger size mandrels were formed on larger forming rolls and vulcanized on the requiredsize mandrels. In still further runs, even larger size insulation wraps were made using tapes of 2.5 cm. width rather than the 2 cm. size.
EXAMPLE 2.
The process of example l was repeated except that the smallamount of carbon black in the standard polychloroprene rubber cement was replaced with aluminum pigment. When the resulting product was subjected to the heat transmission test, satisfactory heat insulation properties were recorded. However, these properties were not as good as for the product of example 1, apparently due to the added conductivity through the metal particles.
In another run, perlite was substituted for the magnesium carbonate in the elastomeric coating composition of example I.
In a further run, titanium dioxide was substituted for the magnesium carbonate. The resulting insulation wraps using these alternate fillers exhibited acceptable heat insulation properties although they were inferior to the product of example 1.
DISCUSSION OF DETAILS The materials used for the continuous strips may be varied depending upon the helicoid product produced. The materials may be paper, plastic, sponge rubbers, foamed plastics, glass fiber cloths, and metals. Materials of a fibrous or spongelike nature may utilize impregnants, which preferably are in a nonhardened or uncured stage when passing through the rolls. Moreover, it is evident that the materials of the strips may be different, as for example, in wrapping electrical conduits a variety of insulation materials are desirable. In addition to elastomeric compounds, silicones, thermoplastic resins, thermosetting resins such as polyester, epoxy and phenols, may be used as impregnants for one or more of the strips. Nonhardened or uncured impregnants are particularly useful in providing a good bond between the overlapping portions upon subsequent cure. For example, the elastomer of one strip may temporarily combine or fuse with the elastomer of the adjacent strip. Upon curing of the elastomer, the fusion is fixed to such an extent that the materials act as an original composite rather than joined strips. Curing or hardening may be effected by an air cure or by oven cure.
After hardening or curing of the impregnant, the material may be left on the core as a protective covering, as for example, as a wire insulation. In another embodiment, it may be removed from the core and cut in lengths or wound upon itself, such as in B-X cable.
Where the helicoid product is a heat protective tubular covering in accordance with a preferred embodiment of the invention, the strip material is formed of asbestos fibers. Plain weave fabric of about 1-3 mm. thickness made of threads or yarns of asbestosfibers is particularly suitable. However, any other flexible webs such as nonwoven felts, knit fabrics or the like of good strength characteristics are contemplated for use a as the base for the strips in the laminated products. Use of asbestos fibers only in the webs is preferred, but inclusion of other heat-resistant fibers, e.g., glass fibers, in various amounts, e.g., up to 25 percent is contemplated as an altemative.
in order to obtain abutment of each layer in a three-ply system, the three strips of material are preferred to be of equal widths. However, the thicknesses and impregnants may vary, depending upon the materials used.
Normally, the temperatures of the individual strips are at ambient and the rolls are unheated. There may be a slight temperature rise above ambient at the rolls, depending upon the compression upon the materials. With metals and with certain impregnants, the rolls and/or the strips of material may be heated to improve the drawing effect or to assist in the hardening or cure of the impregnant.
One of the particular advantages of the invention from a production viewpoint is that the feed reels are in a general planar position on fixed bearings. This arrangement not only provides for ease in substituting a full reel for an empty one, but abo facilitates adjustments of the apparatus, such as the tensions on springs, without stopping the machine operation. Where the reels are wound around the core, as in wirewrapping apparatus, such simple adjustments cannot be made without stoppage. Moreover, with the reels rotating but fixed relative to each other, visual inspection is readily made of all portions of the apparatus in relative safety.
An important feature of the new heat-protective coverings is the overlap configuration provided along edges between separate coils or turns of the helicoid structures. This has been discovered to provide good flexibility without allowing fishmouthing at bends or creation of other openings when the encased conduit is bent or flexed. The degree and nature of the overlapping can be varied by selection of sizes for individual tapes forming the laminations of the product, degree or edge overlap and the like. Simplicity of construction and manufacture, however, make it advantageous to use all tapes of equal width and to use an equal amount of edge overlap at each side of the product.
Any suitable number of strips of elastomer coated cloth may be used to form the insulation covering. As indicated previously in describing a four-ply product, a plurality of strips may be manifolded to form a single step of the covering. This permits production of the new products to be varied for special end uses employing a minimum number of basic fabricating elements.
A wide variety of elastomers are available for use in forming the elastomeric coating compositions used in the new insulation coverings Elastomers having the highest degree of heat and oxidation resistance at a reasonable cost are advantageously used. Polychloroprene and ethylene-propylene rubbers are preferred elastomers. Silicone rubbers are another useful class of elastomers. Elastomers of acrylic type polymers, e.g., 1-6 carbon atom alkyl esters of acrylic and methacrylic acids, chlorinated polyethylenes, and other elastomers of high-temperature resistance known to the art are contemplated for use in the invention. Mixtures of two or more elastomers may be employed.
The elastomeric coating compositions are prepared for coating of the flexible asbestos fiber webs according to industry-recognized procedures and formulations. Suitable compositions may contain from 5 to 50 percent solids and 50 to 95 solvents or dispersants, although other proportions may also be used in special cases. Solvent solutions or emulsions may be employed. Nonflammable solvents are preferred in forming the elastomeric solutions or so-called cements", e.g., haloalkane like tetrachloroethylene, dichlorotetrafluoroethane, carbon tetrachloride and the like.
The nonvolatile portion of the coating compositions, in addition to an elastomer, will advantageously include antioxidants vulcanizing agents, fillers, pigments, plasticizers, accelerators and similar additives known to the rubber industry. Fillers are usually employed in amounts of to 60 parts filler per parts elastomer. The other additives advantageously amount to 0.01 to 10 percent, especially 0.5 to 5 percent, of
the elastomer content.
Examples of fillers, which may be of the reinforcing type, as well as inert type, include magnesium carbonate, zinc oxide, carbon blacks, hard clays, calcium silicates, blanc fixe, whiting, talc, slate four, infusional earth and the like.
Examples of pigments include carbon black, iron oxide red and yellows, titanium dioxide and comparable inorganic pigments.
Examples of accelerators include mercaptobenzothiazole, benzothiazyl disulfide, metal dialkyl dithiocarbamates, alkylene thiuram tetrasulfides and the like.
Examples of antioxidants hydroquinone, monobenzyl ether, p-isopropoxy diphenylamine, phenylnaphthylamine, styrinated phenols, octylated diphenylamines and the like.
Examples of plasticizers and softeners include hydrocarbon oils, polyolefins, aromatic oils and the like.
Examples of vulcanizing agents include sulfur, tetra methylthiuramdisulfide, zinc oxide, magnesium oxide, organic peroxides and the like.
In final analysis, the elastomeric coating compositions are prepared and fonnulated according to commercial practice for rubber compounding and use. Future improvements in this art, therefore, should be adapted to continually upgrade products, basically designed in accordance with the invention, to give the highest possible values for all desirable qualities in the final product.
The embodiments of the invention in which an exclusive property or right is claimed are defined as follows:
1. A helicoid laminate comprising:
a. two or more strips of material joined in overlapping relationship with each other along a longitudinal edge to provide a staggered and tiered arrangement;
b. the joined strips being bonded to each other to form a unified laminate;
c. the strips being coiled in a helicoid construction by an incurvation of the joined strips;
d. the incurvation of the joined strips being imposed therein by at least one strip being of unequal length with that of an adjacent joined strip; and
e. adjacent helicoid portions of a strip are in a butt joint relationship with each other while adjacent portions of the laminate are in a ship-lap joint with respect to each other.
2. A covering material as recited in claim 1 wherein adjacent coils of the laminate are not bonded to each other so that the helicoid laminate can be wound and unwound at will.
3. A covering material as recited in claim 1 wherein the adjacent coils of the laminate in the helicoid construction are bonded to each other at the ship-lap joint portions so that the helicoid laminate is a unified tubular product.
4. A helicoid laminate according to claim 1 in which at least two of said strips are silicone strips in contact with one another.
5. A helicoid flexible covering for tubular conduits to provide heat and flame protection to the conduit, comprising:
a. a plurality of strips of fibrous cloth;
b. a bonding agent impregnated into and covering said strips;
c. said strips being joined in a staggered configuration with the edge of at least one strip being offset from the edge of at least one other strip; at least one of said joined strips being of unequal length with an adjacent strip thereby providing an incurvature in the joined strips forming a helicoid;
e. said staggered configuration being cured into the helicoid, integral structure, having ship-lap joints between adjacent coils, said structure being capable of being repeatedly coiled and uncoiled so the insulation wrap may be repeatedly installed and removed from a tubular conduit without damage.
6. A helicoid flexible covering as claimed in claim wherein the fibrous cloth is asbestos cloth and the bonding agent is an elastomeric material.
7. A helicoid flexible covering as claimed in claim 5 formed of three strips of equal width of asbestos cloth, the inner strip being offset to one side of the central strip and the outer strip being offset to the other side of the central strip.
8. A helicoid insulation wrap as claimed in claim 7 wherein the elastomeric material covering the innermost face of said inner strip is an ethylene-propylene rubber composition and the remaining elastomeric material of the wrap is a termost strip being offset to the other side of the plied central strips.

Claims (9)

  1. 2. A covering material as recited in claim 1 wherein adjacent coils of the laminate are not bonded to each other so that the helicoid laminate can be wound and unwound at will.
  2. 3. A covering material as recited in claim 1 wherein the adjacent coils of the laminate in the helicoid construction are bonded to each other at the ship-lap joint portions so that the helicoid laminate is a unified tubular product.
  3. 4. A helicoid laminate according to claim 1 in which at least two of said strips are silicone strips in contact with one another.
  4. 5. A helicoid flexible covering for tubular conduits to provide heat and flame protection to the conduit, comprising: a. a plurality of strips of fibrous cloth; b. a bonding agent impregnated into and covering said strips; c. said strips being joined in a staggered configuration with the edge of at least one strip being offset from the edge of at least one other strip; d. at least one of said joined strips being of unequal length with an adjacent strip thereby providing an incurvature in the joined strips forming a helicoid; e. said staggered configuration being cured into the helicoid, integral structure, having ship-lap joints between adjacent coils, said structure being capable of being repeatedly coiled and uncoiled so the insulation wrap may be repeatedly installed and removed from a tubular conduit without damage.
  5. 6. A helicoid flexible covering as claimed in claim 5 wherein the fibrous cloth is asbestos cloth and the bonding agent is an elastomeric material.
  6. 7. A helicoid flexible covering as claimed in claim 5 formed of three strips of equal width of asbestos cloth, the inner strip being offset to one side of the central strip and the outer strip being offset to the other side of the central strip.
  7. 8. A helicoid insulation wrap as claimed in claim 7 wherein the elastomeric material covering the innermost face of said inner strip is an ethylene-propylene rubber composition and the remaining elastomeric material of the wrap is a polychloroprene rubber.
  8. 9. A helicoid insulation wrap as claimed in claim 5 formed of two strips of equal width of asbestos cloth.
  9. 10. A helicoid insulation wrap as claimed in claim 5 formed of four strips of equal width of asbestos cloth, the two central strips being plied in full edge-to-edge contact, the inner strip being offset to one side of said plied central strips and the outermost strip being offset to the other side of the plied central strips.
US701424A 1968-01-29 1968-01-29 Helicoid laminate comprising several continuous tiered strips Expired - Lifetime US3616123A (en)

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US3904467A (en) * 1971-10-26 1975-09-09 Goodrich Co B F Method of making curved resilient laminates
US3917898A (en) * 1971-10-22 1975-11-04 Showa Electric Wire & Cable Co Water-cooled cable
US3957085A (en) * 1970-05-21 1976-05-18 Dunlop Holdings Limited Flexible articles
US3959549A (en) * 1973-08-08 1976-05-25 Siemens Aktiengesellschaft Multi-layer insulation for deep-cooled cables
US3976526A (en) * 1974-09-16 1976-08-24 The Dow Chemical Company Preparation of curved composite panel containing a rigid foamed plastic
US4018962A (en) * 1975-04-09 1977-04-19 Pedlow J Watson Arc and fireproofing tape
US4104426A (en) * 1975-11-28 1978-08-01 Mcdonnell Douglas Corporation Production of muffler material
US4239064A (en) * 1979-01-15 1980-12-16 Richard Gilman Insulation tubes and process of making same
US4304268A (en) * 1979-01-15 1981-12-08 Richard Gilman Insulation tubes and process of making same
FR2501105A1 (en) * 1981-03-05 1982-09-10 Mannesmann Ag
US4421818A (en) * 1982-04-12 1983-12-20 The Procter & Gamble Company Articulated fabric formed by self-assembling fibers
US4441947A (en) * 1982-04-12 1984-04-10 The Procter & Gamble Company Articulated fabric formed by self-assembling fibers
EP0194137A2 (en) * 1985-03-06 1986-09-10 Raychem Limited Heat-recoverable article
US4675016A (en) * 1985-10-22 1987-06-23 Kimberly-Clark Corporation Method for adhering curved tensioned elastic strips to a gatherable base material and the article produced
EP0354756A2 (en) * 1988-08-08 1990-02-14 Bridgestone Corporation Take-up liner for uncured rubber members and method of producing the same
GB2239134A (en) * 1989-10-14 1991-06-19 Philips Nv Heat shield for a cable joint
US5222288A (en) * 1991-06-17 1993-06-29 Tru-Flex Metal Hose Corporation Method for forming a spiral-wound flexible piping
US5234518A (en) * 1991-10-03 1993-08-10 Fuji Corporation Felting coiled sleeve and method for preparing the same
US5336346A (en) * 1990-07-24 1994-08-09 O'neill, Inc. Method for forming an adhesively bonded seam between resiliently compressible fabric sheets
US5607529A (en) * 1995-02-15 1997-03-04 Adamczyk; Eric J. Insulated flexible air duct and the process for manufacturing the same
US5857497A (en) * 1985-08-05 1999-01-12 Wangner Systems Corporation Woven multilayer papermaking fabric having increased stability and permeability
US6048428A (en) * 1992-12-08 2000-04-11 Royal Ordnance Plc Pipe construction
WO2000066927A1 (en) * 1999-05-03 2000-11-09 Deepsea Flexibles, Inc. Composite tubular assembly and method of forming same
US6193824B1 (en) * 1995-06-02 2001-02-27 Siemens Aktiengesellschaft Method of installing an optical waveguide cable on a conductor of a high-voltage overhead line
US6199676B1 (en) 1999-04-06 2001-03-13 Air Cruisers Company Inflatable tubular structure with spiral seam
US6286557B1 (en) * 1998-03-12 2001-09-11 Spiral Guard Australia Pty. Ltd. Sheath
WO2002012775A1 (en) 2000-08-09 2002-02-14 Mandzsu Jozsef Sr Pipe insulating jackets and their manufacturing process
US6360780B1 (en) * 2000-08-30 2002-03-26 Owens Corning Fiberglas Technology, Inc. Liner for reinforcing a pipe and method of making the same
WO2002029307A1 (en) * 2000-10-06 2002-04-11 Mazzer Materie Plastiche Di Giacomo Ezio Mazzer & C. S.N.C. Protective sheath
US6375770B1 (en) 1990-07-24 2002-04-23 O'neill, Inc. Apparatus and method for forming an adhesively bonded seam between resiliently compressible fabric sheets
WO2002095281A1 (en) * 2001-05-23 2002-11-28 Nkt Flexibles I/S A method of manufacturing a reinforcement element for a flexible pipeline
US20030172981A1 (en) * 2002-03-15 2003-09-18 Smiths Group Plc Ducting
US6703091B1 (en) * 1999-04-16 2004-03-09 Roger H. Walker Structural lining system for pipes and method for applying same
US20040099324A1 (en) * 2002-11-27 2004-05-27 Wellstream, Inc. Flexible tubular member with sealed tape layer
US20050009652A1 (en) * 2003-07-07 2005-01-13 Ming-Hung Chen Spiral elastic protector
US20050045365A1 (en) * 2003-09-03 2005-03-03 Jan Bladh Cable
US20060249215A1 (en) * 2005-05-06 2006-11-09 Bryant Michael J Anti-collapse system and method of manufacture
US20060254807A1 (en) * 2005-05-12 2006-11-16 Stout Boyd J Insulating wrap
US20070228226A1 (en) * 2006-03-22 2007-10-04 Michael Taillon Adjustable spiral sleeve for protecting lines
US20100170629A1 (en) * 2009-01-08 2010-07-08 Chandra Sekar Methods for manufacturing a paint roller and component parts thereof
US20100282400A1 (en) * 2009-05-05 2010-11-11 Chandra Sekar Methods for manufacturing a paint roller and component parts thereof
US20140140809A1 (en) * 2012-11-20 2014-05-22 Rolls-Royce Plc Heat protection assembly
CN104044326A (en) * 2013-03-12 2014-09-17 Ems专利股份公司 Method for the continuous production of laminates made of fibre bands and use thereof
WO2016126647A1 (en) * 2015-02-04 2016-08-11 Bartell Machinery Systems, L.L.C. Multiple strip armoring system
US10322924B2 (en) * 2017-07-28 2019-06-18 Frizzie Corp. Low impact mobile and modular fuel delivery apparatus and kit
WO2020037353A1 (en) * 2018-08-23 2020-02-27 Peter Andrew John May A hose shroud
US11698161B2 (en) 2012-05-18 2023-07-11 Nelson Global Products, Inc. Breathable multi-component exhaust insulation system
US11806920B2 (en) 2012-09-28 2023-11-07 Nelson Global Products, Inc. Heat curable composite textile
US11867344B2 (en) * 2016-04-15 2024-01-09 Nelson Global Products, Inc. Composite insulation system
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US3957085A (en) * 1970-05-21 1976-05-18 Dunlop Holdings Limited Flexible articles
US3917898A (en) * 1971-10-22 1975-11-04 Showa Electric Wire & Cable Co Water-cooled cable
US3904467A (en) * 1971-10-26 1975-09-09 Goodrich Co B F Method of making curved resilient laminates
US3959549A (en) * 1973-08-08 1976-05-25 Siemens Aktiengesellschaft Multi-layer insulation for deep-cooled cables
US3976526A (en) * 1974-09-16 1976-08-24 The Dow Chemical Company Preparation of curved composite panel containing a rigid foamed plastic
US4018962A (en) * 1975-04-09 1977-04-19 Pedlow J Watson Arc and fireproofing tape
US4104426A (en) * 1975-11-28 1978-08-01 Mcdonnell Douglas Corporation Production of muffler material
US4239064A (en) * 1979-01-15 1980-12-16 Richard Gilman Insulation tubes and process of making same
US4304268A (en) * 1979-01-15 1981-12-08 Richard Gilman Insulation tubes and process of making same
FR2501105A1 (en) * 1981-03-05 1982-09-10 Mannesmann Ag
US4421818A (en) * 1982-04-12 1983-12-20 The Procter & Gamble Company Articulated fabric formed by self-assembling fibers
US4441947A (en) * 1982-04-12 1984-04-10 The Procter & Gamble Company Articulated fabric formed by self-assembling fibers
EP0194137A2 (en) * 1985-03-06 1986-09-10 Raychem Limited Heat-recoverable article
EP0194137A3 (en) * 1985-03-06 1989-01-25 Raychem Limited Heat-recoverable article
US5857497A (en) * 1985-08-05 1999-01-12 Wangner Systems Corporation Woven multilayer papermaking fabric having increased stability and permeability
US4675016A (en) * 1985-10-22 1987-06-23 Kimberly-Clark Corporation Method for adhering curved tensioned elastic strips to a gatherable base material and the article produced
EP0354756A2 (en) * 1988-08-08 1990-02-14 Bridgestone Corporation Take-up liner for uncured rubber members and method of producing the same
EP0354756A3 (en) * 1988-08-08 1991-09-25 Bridgestone Corporation Take-up liner for uncured rubber members and method of producing the same
GB2239134A (en) * 1989-10-14 1991-06-19 Philips Nv Heat shield for a cable joint
GB2239134B (en) * 1989-10-14 1994-03-30 Philips Nv Heat shield for a cable joint
US6375770B1 (en) 1990-07-24 2002-04-23 O'neill, Inc. Apparatus and method for forming an adhesively bonded seam between resiliently compressible fabric sheets
US5693177A (en) * 1990-07-24 1997-12-02 O'neill, Inc. Apparatus for forming an adhesively bonded seam between resiliently compressible fabric sheets
US5336346A (en) * 1990-07-24 1994-08-09 O'neill, Inc. Method for forming an adhesively bonded seam between resiliently compressible fabric sheets
US5222288A (en) * 1991-06-17 1993-06-29 Tru-Flex Metal Hose Corporation Method for forming a spiral-wound flexible piping
US5234518A (en) * 1991-10-03 1993-08-10 Fuji Corporation Felting coiled sleeve and method for preparing the same
US6048428A (en) * 1992-12-08 2000-04-11 Royal Ordnance Plc Pipe construction
US5607529A (en) * 1995-02-15 1997-03-04 Adamczyk; Eric J. Insulated flexible air duct and the process for manufacturing the same
US6193824B1 (en) * 1995-06-02 2001-02-27 Siemens Aktiengesellschaft Method of installing an optical waveguide cable on a conductor of a high-voltage overhead line
US6286557B1 (en) * 1998-03-12 2001-09-11 Spiral Guard Australia Pty. Ltd. Sheath
US6199676B1 (en) 1999-04-06 2001-03-13 Air Cruisers Company Inflatable tubular structure with spiral seam
US6703091B1 (en) * 1999-04-16 2004-03-09 Roger H. Walker Structural lining system for pipes and method for applying same
WO2000066927A1 (en) * 1999-05-03 2000-11-09 Deepsea Flexibles, Inc. Composite tubular assembly and method of forming same
US6491779B1 (en) 1999-05-03 2002-12-10 Deepsea Flexibles, Inc. Method of forming a composite tubular assembly
US6804942B2 (en) 1999-05-03 2004-10-19 Michael J. Bryant Composite tubular assembly and method of forming same
WO2002012775A1 (en) 2000-08-09 2002-02-14 Mandzsu Jozsef Sr Pipe insulating jackets and their manufacturing process
US6360780B1 (en) * 2000-08-30 2002-03-26 Owens Corning Fiberglas Technology, Inc. Liner for reinforcing a pipe and method of making the same
WO2002029307A1 (en) * 2000-10-06 2002-04-11 Mazzer Materie Plastiche Di Giacomo Ezio Mazzer & C. S.N.C. Protective sheath
US6734365B2 (en) 2000-10-06 2004-05-11 Mazzer Materie Plastiche Di Giacomo Ezio Mazzer & C. S.N.C. Protective sheath
US20070062633A1 (en) * 2001-05-23 2007-03-22 Nkt Research & Annovation A/S Method of manufacturing a reinforcement element for a flexible pipeline
WO2002095281A1 (en) * 2001-05-23 2002-11-28 Nkt Flexibles I/S A method of manufacturing a reinforcement element for a flexible pipeline
US8505587B2 (en) 2001-05-23 2013-08-13 National Oilwell Varco Denmark I/S Method of manufacturing a reinforcement element for a flexible pipeline
US20110067776A1 (en) * 2001-05-23 2011-03-24 Nkt Flexibles I/S Method of manufacturing a reinforcement element for a flexible pipeline
US20040185202A1 (en) * 2001-05-23 2004-09-23 Kristian Glejbol Method of manufacturing a reinforcement element for a flexible pipeline
US7842149B2 (en) 2001-05-23 2010-11-30 Nkt Flexibles I/S Method of manufacturing a reinforcement element for a flexible pipeline
US20030172981A1 (en) * 2002-03-15 2003-09-18 Smiths Group Plc Ducting
US6679296B2 (en) * 2002-03-15 2004-01-20 Smiths Group Plc Ducting
US20040099324A1 (en) * 2002-11-27 2004-05-27 Wellstream, Inc. Flexible tubular member with sealed tape layer
US6889715B2 (en) * 2002-11-27 2005-05-10 Wellstream International Limited Flexible tubular member with sealed tape layer
US20050009652A1 (en) * 2003-07-07 2005-01-13 Ming-Hung Chen Spiral elastic protector
US20050045365A1 (en) * 2003-09-03 2005-03-03 Jan Bladh Cable
US20060249215A1 (en) * 2005-05-06 2006-11-09 Bryant Michael J Anti-collapse system and method of manufacture
US7254933B2 (en) 2005-05-06 2007-08-14 Deepflex Inc. Anti-collapse system and method of manufacture
US20060254807A1 (en) * 2005-05-12 2006-11-16 Stout Boyd J Insulating wrap
US7521635B2 (en) * 2005-05-12 2009-04-21 Gazelle's Oilfield Services Ltd. Insulating wrap
US20070228226A1 (en) * 2006-03-22 2007-10-04 Michael Taillon Adjustable spiral sleeve for protecting lines
US7895716B2 (en) 2006-03-22 2011-03-01 Taimi R&D Inc. Adjustable spiral sleeve for protecting lines
US8142599B2 (en) 2009-01-08 2012-03-27 Chandra Sekar Methods for manufacturing a paint roller and component parts thereof
US20100170629A1 (en) * 2009-01-08 2010-07-08 Chandra Sekar Methods for manufacturing a paint roller and component parts thereof
US20100282400A1 (en) * 2009-05-05 2010-11-11 Chandra Sekar Methods for manufacturing a paint roller and component parts thereof
US11698161B2 (en) 2012-05-18 2023-07-11 Nelson Global Products, Inc. Breathable multi-component exhaust insulation system
US11806920B2 (en) 2012-09-28 2023-11-07 Nelson Global Products, Inc. Heat curable composite textile
US20140140809A1 (en) * 2012-11-20 2014-05-22 Rolls-Royce Plc Heat protection assembly
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