US20040185202A1 - Method of manufacturing a reinforcement element for a flexible pipeline - Google Patents

Method of manufacturing a reinforcement element for a flexible pipeline Download PDF

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Publication number
US20040185202A1
US20040185202A1 US10/478,948 US47894804A US2004185202A1 US 20040185202 A1 US20040185202 A1 US 20040185202A1 US 47894804 A US47894804 A US 47894804A US 2004185202 A1 US2004185202 A1 US 2004185202A1
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Prior art keywords
strength
imparting
layer
thermoplastic
layers
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US10/478,948
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English (en)
Inventor
Kristian Glejbol
Jakob Wedel-Heinen
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National Oilwell Varco Denmark IS
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Individual
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Assigned to NKT FLEXIBLES I/S reassignment NKT FLEXIBLES I/S ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: GLEJBOL, KRISTIAN, WEDEL-HEINEN, JAKOB
Publication of US20040185202A1 publication Critical patent/US20040185202A1/en
Priority to US11/545,164 priority Critical patent/US7842149B2/en
Priority to US12/910,944 priority patent/US8505587B2/en
Abandoned legal-status Critical Current

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    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00—Layered products comprising a layer of synthetic resin
    • B32B27/06—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B—PERFORMING OPERATIONS; TRANSPORTING
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    • B32B1/00—Layered products having a non-planar shape
    • B32B1/08—Tubular products
    • B—PERFORMING OPERATIONS; TRANSPORTING
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    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B15/08—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • B32B15/085—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin comprising polyolefins
    • B—PERFORMING OPERATIONS; TRANSPORTING
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    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B15/08—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • B32B15/092—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin comprising epoxy resins
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    • B32B15/18—Layered products comprising a layer of metal comprising iron or steel
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    • B32B27/30—Layered products comprising a layer of synthetic resin comprising vinyl (co)polymers; comprising acrylic (co)polymers
    • B32B27/304—Layered products comprising a layer of synthetic resin comprising vinyl (co)polymers; comprising acrylic (co)polymers comprising vinyl halide (co)polymers, e.g. PVC, PVDC, PVF, PVDF
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    • B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/14—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
    • B32B37/16—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers with all layers existing as coherent layers before laminating
    • B32B37/20—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers with all layers existing as coherent layers before laminating involving the assembly of continuous webs only
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    • B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L11/00—Hoses, i.e. flexible pipes
    • F16L11/04—Hoses, i.e. flexible pipes made of rubber or flexible plastics
    • F16L11/08—Hoses, i.e. flexible pipes made of rubber or flexible plastics with reinforcements embedded in the wall
    • F16L11/081—Hoses, i.e. flexible pipes made of rubber or flexible plastics with reinforcements embedded in the wall comprising one or more layers of a helically wound cord or wire
    • F16L11/083—Hoses, i.e. flexible pipes made of rubber or flexible plastics with reinforcements embedded in the wall comprising one or more layers of a helically wound cord or wire three or more layers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L11/00—Hoses, i.e. flexible pipes
    • F16L11/14—Hoses, i.e. flexible pipes made of rigid material, e.g. metal or hard plastics
    • F16L11/16—Hoses, i.e. flexible pipes made of rigid material, e.g. metal or hard plastics wound from profiled strips or bands
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/56—Winding and joining, e.g. winding spirally
    • B29C53/58—Winding and joining, e.g. winding spirally helically
    • B—PERFORMING OPERATIONS; TRANSPORTING
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    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/02—Synthetic macromolecular fibres
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    • B32B2262/10—Inorganic fibres
    • B32B2262/106—Carbon fibres, e.g. graphite fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
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    • B—PERFORMING OPERATIONS; TRANSPORTING
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    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2305/00—Condition, form or state of the layers or laminate
    • B32B2305/08—Reinforcements
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
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    • B32B2307/50—Properties of the layers or laminate having particular mechanical properties
    • B32B2307/54—Yield strength; Tensile strength
    • B—PERFORMING OPERATIONS; TRANSPORTING
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    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/50—Properties of the layers or laminate having particular mechanical properties
    • B32B2307/546—Flexural strength; Flexion stiffness
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    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
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    • Y10T428/1352—Polymer or resin containing [i.e., natural or synthetic]
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    • Y—GENERAL 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
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    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/31504—Composite [nonstructural laminate]

Definitions

  • the invention relates to a method of manufacturing a reinforcement element for a flexible pipeline, a reinforcement element for a flexible pipeline, and a precursor therefore.
  • Flexible pipes containing reinforcement elements are known e.g. from JP 3265781, FR 2764669 and WO 00/36324. Such pipes are typically used for the transport of oil and gas in deep waters or waters of varying depth.
  • An example is pipes which are used for the transport of hydrocarbon from a subsea installation to an installation at the surface of the sea.
  • pipes which are used for the transport of hydrocarbon from a subsea installation to an installation at the surface of the sea.
  • extremely high requirements are made with respect to the reinforcement, since the pipes are subjected to great static and dynamic mechanical loads along their axes. These loads originate partly from the external pressure application caused by varying external water pressures, partly tensile forces caused by the own weight of the pipe, and partly forces caused by the positive pressure by which the fluid flowing in the pipe affects the pipe.
  • This method ensures that while the glue hardens, the layers are only kept together by the wound tape, which is not capable of absorbing transverse stresses to any significant degree.
  • the effect of this is that the layers kept together can slide over each other to a certain degree, and the resulting reinforcement element can therefore be configured within certain limits while the glue has still not hardened. After hardening, further sliding of the layers over each other will no longer be possible, and the combined layers will therefore constitute a rigid reinforcement element.
  • the advantage of applying the reinforcement element as a plurality of layers on the pipe is that it is hereby possible to apply the elements without any significant mechanical residual stresses occurring in the finished elements.
  • a further drawback of the above method is that during manufacture and repair of reinforcement elements it will be extremely difficult to separate the individual layers from each other, which excludes repairs, splicing and terminations of the individual reinforcement elements in practice.
  • an objective of the invention is to provide a structure of rein- forcement elements for use in the manufacture of flexible pipelines which is not limited by the problems mentioned above.
  • the invention thus includes a method of manufacturing precursor for a reinforcement element for a flexible pipeline, including the step of applying a thermoplastic layer to the reinforcement element, which consists of at least one strength-imparting layer, on at least one face thereof.
  • One or more precursors may thereafter be laminated with each other and/or other strength-imparting layer or layers to form a final reinforcement element.
  • the reinforcement element and the strength-imparting layer(s) may e.g. be as described below.
  • the invention also relates to a method of manufacturing a reinforcement element for a flexible pipeline, wherein the reinforcement element comprises two or more strength-imparting layers, e.g. 3, 4, 5, or more such as up to about 10 or even 20 strength-imparting layers.
  • the method includes a step of applying a thermoplastic layer to at least one of the strength-imparting layers, on at least one face thereof, followed by a lamination with another strength-imparting non-thermoplastic layer.
  • the strength-imparting non-thermoplastic layer or layers may in one embodiment be as the fiber based tapes described in WO 0066927 which is hereby incorporated by reference.
  • the strength-imparting layers are in the form of tape shaped units having two major sides.
  • the strength-imparting layer may in principle be of any material such as metals and fiber reinforced polymers. Basically it is preferred that the strength-imparting layer is a non-thermoplastic layer not made from any thermoplastic polymer, but in one embodiment it may contain small amounts e.g. up to about 10% by weight of a thermoplastic polymer provided that this thermoplastic polymer has a lover t g value than the thermoplastic layer applied onto or in between the strength-imparting layers.
  • the strength-imparting layers are made from materials as disclosed in WO 0066927.
  • the strength-imparting layer or layers are in the form of a polymer reinforced with at least 20% by volume, such as 30% by volume of fibres or whiskers, such as carbon fibres or mineral fibres.
  • the fibres may be randomly distributed or they may be oriented.
  • the major part of the fibres has orientations along the length of the shaped strength-imparting layer or layers.
  • the length of the fibres may influence the strength of the strength-imparting layer.
  • the fibres are endless along the strength-imparting layer, wherein the term “endless” designates that the major part of the fibres extends along length above 10 cm, such as 100 cm in the direction along the length of the strength-imparting layer.
  • the strength-imparting layer or layers are in the form of a fully or partly metallic material.
  • thermoplastic layers are applied onto one of the major faces of at least half of the strength-imparting layers.
  • This application of thermoplastic material is in one embodiment carried out before the lamination process where further strength-imparting layer or layers are laminated.
  • this application of thermoplastic material is carried out during the lamination process so that thermoplastic material is applied onto one major surface of a first strength-imparting layer, a second strength-imparting layer is applied onto the thermoplastic layer, the free major surface of the second strength-imparting layer is coated with a thermoplastic material and so on.
  • the thermoplastic material should be sufficiently soft to be moldable and to be capable of adhering to the strength-imparting layers. Therefore it is desired to perform the coating and lamination processes at elevated temperature e.g. above 100° C., above 150° C. or even higher. In one embodiment the coating and lamination processes are carried out at temperatures above the thermoplastic t g +10° C. In another embodiment the coating and lamination processes are carried out at a temperature below 100° C. and the thermoplastic material has immediately before the application been heated to above the thermoplastic t g +10° C., such as above the thermoplastic t g +100° C.
  • thermoplastic material are in the form of a thermoplastic polymer reinforced with fibres or whiskers, e.g. at least 20% by volume, such as 30% by volume of.
  • the fibres or whiskers may e.g. be carbon fibres or mineral fibres.
  • the fibres in the thermoplasticmaterial layer applied onto or between adjacent layers of strength-imparting layers may be randomly distributed or they may be oriented.
  • the major part of the fibres has orientations perpendicular to the length of the shaped strength-imparting layer or layers.
  • the reinforcement element has at least two strength-imparting layers, and a thermoplastic material is applied to the adjoining faces of at least one of the two strength-imparting layers.
  • heat is supplied to the strength-imparting layers during the lamination process.
  • This method is particularly useful in situation where the strength-imparting layer or layers are of a material with a high heat conductivity such as a metal, e.g. steel, aluminum or composite materials comprising metal.
  • the reinforcement element has at least two or more such as a plurality of strength-imparting layers
  • the method includes the application of a thermoplastic material to the adjoining faces of at least one of the two strength-imparting layers.
  • thermoplastic material is cross-linked after the lamination step, whereby it changes its state from being thermoplastic to being thermosetting.
  • the method may in one embodiment comprise a step of applying an energy-dissipating layer to at least one of the outer surfaces of the reinforcement element.
  • energy caused by shock loads may be dissipated, which is important particularly if the flexible pipe is of the type to which is applied a reinforcement layer exposed freely to the surroundings, i.e. a pipe without protective sheath.
  • One or more energy-dissipating layers may further be be applied between strength-imparting layers.
  • An energy-dissipating layer means a layer having a shore hardness, which is lower than the shore hardness of the strength-imparting layers of the reinforcement-element.
  • the energy-dissipating layer has a shore hardness, which is at least 5%, such as at least 10 lower than the shore hardness of the strength-imparting layers of the reinforcement-element.
  • the energy-dissipating layer may in one embodiment be of a polymeric material such as an epoxy polymer.
  • the reinforcement element consists of a plurality of strength-imparting layers, and these layers are reeled on a reel, and prior to or during reeling, they are given a shape which approximately has the final curvature of the reinforcement layer.
  • the reinforcement element comprising a plurality of strength-imparting layers with a shape which approximately has the final curvature of the reinforcement layer, it is ensured that the tensile reinforcement layer is essentially tension-free after application to the flexible pipe.
  • the reinforcement element may be applied or be reeled for subsequent use.
  • the thermoplastic material is sufficiently soft to adapt to the form provided during the reeling so that the reinforcement element obtains a shape which includes a curvature.
  • the shape corresponds to the final curvature of the reinforcement element.
  • the method of the invention may include the step of applying the reinforcement element. In one embodiment the method therefore includes the steps of
  • thermoplastic polymer material e.g. in a thickness of about 100 ⁇ m, 200 ⁇ m or 300 ⁇ m, to the flat profiles
  • the reinforcement element is reeled onto a bobbin or similar strong device, and later it is unwound under the application of heat and applied onto a flexible pipe.
  • thermoplastic layer is applied immediately before the final application.
  • the thermoplastic layer may be applied either as a film, which is subsequently melted, or as a sprayed layer.
  • the invention also relates to a precursor for a reinforcement element for a flexible pipeline.
  • the precursor comprises a strength-imparting, preferably non-thermoplastic layer comprising two major faces, having on at least one of its major faces a layer of a thermoplastic material.
  • the strength-imparting non-thermoplastic layer and the thermoplastic layer may be as described above and furthermore the precursor may be provided according to the method described above.
  • a reinforcement element having the desired strength easily can be provided by selecting the number of strength-imparting layers in relation to the desired strength. Thereby mass production of the precursor for final production of different enforcement elements with different strengths is possible.
  • the invention relates to a reinforcement element for a flexible pipe-line.
  • the reinforcement element comprises two or more strength-imparting preferably non-thermoplastic superimposed layers.
  • the two or more strength-imparting superimposed layers are fixed to each other by intermediate layer or layers of thermoplastic material.
  • the strength-imparting layer and the thermoplastic layer may be as described above and furthermore the precursor may be provided according to the method described above.
  • the reinforcement element according to the invention is simple to manufacture, easy to handle under the application onto a flexible pipe, and further it is easy to repair.
  • FIG. 1 shows the structure of an ordinary flexible pipe with reinforcement layers
  • FIG. 2 schematically shows a small part of the structure of a reinforcement layer according to the invention
  • FIG. 3 schematically shows a subprocess in the application of a reinforcement layer using one or more strength-imparting layers according to the invention.
  • FIG. 1, 1 designates a flexible pipe, e.g. for the transport of fluids such as oil and gas between offshore installations and installations near oil wells on the sea bed.
  • the flexible pipe in FIG. 1 consists of a tight liner 3 on whose inner side a so-called carcass formed by wound steel profiles is provided.
  • the carcass protects the liner against collapse because of external compressive forces, which may e.g. occur because of hydrostatic pressures.
  • Two types of reinforcement layers are arranged externally on the liner, of which the layer 5 , 6 positioned closest to the liner is a compression reinforcement layer that consists of coupled profiles which may be of the Z-, C-, X- or K-type.
  • the compression reinforcement layer has arranged externally thereon a tension reinforcement layer which consists of helically wound profiles 7 , 8 which are wound almost symmetrically relative to the longitudinal axis of the pipe, e.g. at an angle of about 55°, and such that the layers 7 , 8 are wound oppositely to each other.
  • an outer jacket 9 which is tight in some cases, but not necessarily so, is applied externally to the tension reinforcement layer.
  • FIG. 2 shows a small section of the structure of a strength-imparting layer 10 according to the invention, which may e.g. be used for the tension reinforcment layer 7 or 8 in FIG. 1.
  • the layer 10 is composed as a laminate, where 12 and 14 designate layers which do not exhibit any considerable thermoplastic behaviour, such as e.g. steel tapes or profiles of a carbon/epoxy composite, while 11 , 13 and 15 designate a thermoplastic material.
  • thermoplastic material has the property that it may be present in both a melted and a solid phase, and that reversible switching between the phases is possible by control of the temperature.
  • the layer used as a reinforcement according to WO 00/66927 is a glue which maintains its rigidity after solidification.
  • the first is a laminate consisting of a strength-imparting layer and a thermoplastic layer.
  • a laminate consisting of a strength-imparting layer and a thermoplastic layer.
  • Such a structure will be suitable for combination with other laminates of the same type.
  • Another basic configuration may consist of a strength-imparting layer which may be provided with a thermoplastic layer on each side.
  • one of the two layers may be a ductile material which is suitable as an outer layer in a reinforcement which is to be capable of resisting external impacts, such as shocks or the like. This is important especially if the reinforcement layer is exposed freely to the surroundings.
  • the layer is thermoplastic according to the invention, it can be worked relatively easily. In other words, even reinforcement layers having many layers and thereby a great strength may be reeled in limited amounts, since heating during working causes the thermoplastic layer to become so soft as to allow the steel elements/profiles to move relatively to each other.
  • the reinforcement layers are to be used on a long pipe, it may be desired in the manufacture of it that the reinforcement elements are manufactured with a curvature comparable to the curvature which they will describe on the finished pipe. It is important to note that the innermost fibres in a reinforcement layer will describe a shorter distance than the outermost fibres. Thus, if a pipe has wound thereon a straight reinforcement element where the individual strength-imparting layers are locked relative to each other, the winding will therefore cause compressive stresses in the innermost fibres of the reinforcement element. If a reinforcement element according to the invention is wound where the strength-imparting layers are not locked relative to each other (e.g. because of heating), this will cause the layers to move relative to each other. This is in most situations acceptable for short lengths of reinforcement elements, but may be difficult for long lengths, since the practical handling of the accumulated length difference between the individual strength-imparting layers will result in a very difficult manufacturing process.
  • FIG. 3 schematically shows how a strength-imparting layer may be manufactured according to the invention, where 10 designates a strength-imparting layer which is shown to the right in the figure prior to the lamination process.
  • non-thermoplastic strength-imparting layers 20 a , 20 b , 20 c , 20 d , and 20 e are fed from reels (not shown) to reels 16 , 18 , where a thermoplastic material is applied from applicator means (not shown) to the non-thermoplastic strength-imparting layers 20 a , 20 b , 20 c , 20 d , and 20 e shortly before the compression.
  • These applicator means may consist of guides which apply a thermoplastic layer, e.g. in the form of a film, to the strength-imparting layers, or by direct application of molten material by means of small rolls having perforations for discharging thermoplastic material.
  • This example describes a freely hanging configuration where the depth of the pipe below the surface of the sea is a monotonically increasing function of the length. In this configuration, the hydrostatic pressure around the pipe therefore increases monotonically along the length of the pipe.
  • the liner is formed of PVDF and serves to create an effective diffusion barrier between the fluid transported in the pipe and the environment. To prevent unintentional cooling of the transported fluid, the liner has extruded externally thereon a layer of polypropylene whose purpose is to serve as a thermal barrier.
  • polypropylene is stated as an example here, numerous other materials and combinations of materials may be used. In particular combinations of materials where syntactic foam is included as a component are conceivably suitable in this application.
  • the interior of the liner is reinforced with a 12 mm thick reinforcement layer which is wound on profiles made of duplex steel.
  • the external reinforcement is composed of elements which each are made of thin layers of a carbon/epoxy composite bonded together by thermoplastic intermediate layers.
  • the manufacture of the reinforcement layers starts with a pultrusion process where a plurality of flat strength-imparting layers having the dimensions 0.5 ⁇ 12 mm are manufactured.
  • This pultrusion process comprises manufacture of elements having a fibre content of about 50% by volume. Characteristic of the resulting pultruded product is a high degree of fibre alignment, and this pultruded product therefore has an extremely great strength along the fibre direction.
  • After pultrusion of this strength-imparting layer it is drawn through a furnace, which ensures complete hardening of the epoxy. Immediately after the passage through the furnace, a solid 200 ⁇ m thick thermoplastic polyurethane film is applied.
  • the polyurethane layer fuses with the strength-imparting carbon/epoxy layer.
  • the strength-imparting layer with applied polyurethane is now reeled and stored.
  • reinforcement layers are now composed by applying eight strength-imparting layers to the pipe. Immediately prior to winding on the pipe, the eight strength-imparting layers are heated, causing the applied thermoplastic polyurethane to melt. Hereby, the eight layers fuse to a unit. Since this fusion takes place immediately prior to the application to the pipe, the polyurethane layer will be molten at the winding, but will harden immediately after the application to the pipe.
  • the applied element will essentially have a shape that ensures that there are no mechanical stresses.
  • the outer reinforcement is wound at angles of about +/ ⁇ 55° relative to the longitudinal axis of the pipe.
  • a stocking of aramide is woven over the outer reinforcement.
  • This stocking of aramide imparts a great abrasive strength to the pipe, while it is so open to mass transport as to allow a free or almost free transport of fluids to take place through it. Since the aramide stocking is exposed to sunlight, a further cover layer will be applied to pipe lengths which are exposed to UV radiation.
  • This stocking is woven in a manner such that it yields if the pipe is compressed. It is ensured hereby that the tensile reinforcement of the pipe can travel radially if the pipe is subjected to compression in the direction of the axis, whereby the compressive stresses in the reinforcement elements are kept at an acceptable level.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Textile Engineering (AREA)
  • Laminated Bodies (AREA)
  • Rigid Pipes And Flexible Pipes (AREA)
US10/478,948 2001-05-23 2002-05-23 Method of manufacturing a reinforcement element for a flexible pipeline Abandoned US20040185202A1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
US11/545,164 US7842149B2 (en) 2001-05-23 2006-10-10 Method of manufacturing a reinforcement element for a flexible pipeline
US12/910,944 US8505587B2 (en) 2001-05-23 2010-10-25 Method of manufacturing a reinforcement element for a flexible pipeline

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DKPA200100832 2001-05-23
DK200100832A DK200100832A (da) 2001-05-23 2001-05-23 Fremgangsmåde til fremstilling af et armeringselement til en fleksibel rørledning
PCT/DK2002/000355 WO2002095281A1 (en) 2001-05-23 2002-05-23 A method of manufacturing a reinforcement element for a flexible pipeline

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US11/545,164 Continuation US7842149B2 (en) 2001-05-23 2006-10-10 Method of manufacturing a reinforcement element for a flexible pipeline

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US20040185202A1 true US20040185202A1 (en) 2004-09-23

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US10/478,948 Abandoned US20040185202A1 (en) 2001-05-23 2002-05-23 Method of manufacturing a reinforcement element for a flexible pipeline
US11/545,164 Expired - Fee Related US7842149B2 (en) 2001-05-23 2006-10-10 Method of manufacturing a reinforcement element for a flexible pipeline
US12/910,944 Expired - Fee Related US8505587B2 (en) 2001-05-23 2010-10-25 Method of manufacturing a reinforcement element for a flexible pipeline

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US12/910,944 Expired - Fee Related US8505587B2 (en) 2001-05-23 2010-10-25 Method of manufacturing a reinforcement element for a flexible pipeline

Country Status (9)

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US (3) US20040185202A1 (de)
EP (1) EP1390659B1 (de)
AT (1) ATE294945T1 (de)
BR (1) BR0209921B1 (de)
CA (1) CA2446153C (de)
DE (1) DE60204012D1 (de)
DK (1) DK200100832A (de)
NO (1) NO336498B1 (de)
WO (1) WO2002095281A1 (de)

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US20140290784A1 (en) * 2011-05-13 2014-10-02 Deepflex Inc. Reinforcement laminate having an alignment feature
CN108773593A (zh) * 2018-05-29 2018-11-09 深圳市百事达卓越科技股份有限公司 自由赋形加强筋
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US9562633B2 (en) 2009-10-28 2017-02-07 National Oilwell Varco Denmark I/S Flexible pipe and a method of producing a flexible pipe
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WO2013135243A1 (en) 2012-03-13 2013-09-19 National Oilwell Varco Denmark I/S A reinforcement element for an unbonded flexible pipe
CA2869588A1 (en) 2012-04-12 2013-10-17 National Oilwell Varco Denmark I/S A method of producing an unbonded flexible pipe and an unbonded flexible pipe
BR112014030179B1 (pt) * 2012-06-06 2020-11-17 National Oilwell Varco Denmark I/S tubo de subida para transportar fluido entre uma instalação superior e uma instalação submarina
CN104583661A (zh) * 2012-06-15 2015-04-29 迪普弗莱克斯有限公司 具有整体抗挤出层的压力防护
DK177627B1 (en) * 2012-09-03 2013-12-16 Nat Oilwell Varco Denmark Is An unbonded flexible pipe
FR3008161B1 (fr) 2013-07-03 2015-09-04 Technip France Embout de connexion d'une conduite flexible avec un organe d'espacement, conduite flexible et procede associes
WO2015139708A1 (en) 2014-03-21 2015-09-24 National Oilwell Varco Denmark I/S A flexible pipe
FR3022320B1 (fr) * 2014-06-16 2016-07-29 Technip France Conduite tubulaire a bande de maintien composite
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EP3345750B1 (de) 2017-01-10 2019-05-22 Evonik Degussa GmbH Thermoplastisches compositrohr mit mehrschichtiger zwischenlage
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US20110067776A1 (en) * 2001-05-23 2011-03-24 Nkt Flexibles I/S 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
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Also Published As

Publication number Publication date
BR0209921B1 (pt) 2014-01-28
US7842149B2 (en) 2010-11-30
US8505587B2 (en) 2013-08-13
EP1390659A1 (de) 2004-02-25
WO2002095281A1 (en) 2002-11-28
NO20035184D0 (no) 2003-11-21
BR0209921A (pt) 2004-07-27
EP1390659B1 (de) 2005-05-04
NO336498B1 (no) 2015-09-07
CA2446153A1 (en) 2002-11-28
CA2446153C (en) 2009-07-21
US20110067776A1 (en) 2011-03-24
DE60204012D1 (de) 2005-06-09
US20070062633A1 (en) 2007-03-22
ATE294945T1 (de) 2005-05-15
DK200100832A (da) 2001-05-23
NO20035184L (no) 2003-11-21

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