WO2024115883A1 - Pipe for transporting cryogenic fluids - Google Patents
Pipe for transporting cryogenic fluids Download PDFInfo
- Publication number
- WO2024115883A1 WO2024115883A1 PCT/GB2023/053039 GB2023053039W WO2024115883A1 WO 2024115883 A1 WO2024115883 A1 WO 2024115883A1 GB 2023053039 W GB2023053039 W GB 2023053039W WO 2024115883 A1 WO2024115883 A1 WO 2024115883A1
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- WO
- WIPO (PCT)
- Prior art keywords
- polymer composite
- layer
- tape
- longitudinal
- polymer
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Ceased
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Classifications
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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
- F16L9/00—Rigid pipes
- F16L9/16—Rigid pipes wound from sheets or strips, with or without reinforcement
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- 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
- B29C53/581—Winding and joining, e.g. winding spirally helically using sheets or strips consisting principally of plastics material
- B29C53/582—Winding and joining, e.g. winding spirally helically using sheets or strips consisting principally of plastics material comprising reinforcements, e.g. wires, threads
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- 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
- B29C53/36—Bending and joining, e.g. for making hollow articles
- B29C53/38—Bending and joining, e.g. for making hollow articles by bending sheets or strips at right angles to the longitudinal axis of the article being formed and joining the edges
- B29C53/48—Bending and joining, e.g. for making hollow articles by bending sheets or strips at right angles to the longitudinal axis of the article being formed and joining the edges for articles of indefinite length, i.e. bending a strip progressively
- B29C53/50—Bending and joining, e.g. for making hollow articles by bending sheets or strips at right angles to the longitudinal axis of the article being formed and joining the edges for articles of indefinite length, i.e. bending a strip progressively using internal forming surfaces, e.g. mandrels
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- 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
- B29C53/80—Component parts, details or accessories; Auxiliary operations
- B29C53/82—Cores or mandrels
- B29C53/821—Mandrels especially adapted for winding and joining
- B29C53/822—Single use mandrels, e.g. destructible, becoming part of the wound articles
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- 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
- B29C63/00—Lining or sheathing, i.e. applying preformed layers or sheathings of plastics; Apparatus therefor
- B29C63/02—Lining or sheathing, i.e. applying preformed layers or sheathings of plastics; Apparatus therefor using sheet or web-like material
- B29C63/04—Lining 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
- B29C63/06—Lining 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 around tubular articles
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D23/00—Producing tubular articles
- B29D23/001—Pipes; Pipe joints
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- 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
- B32B1/00—Layered products having a non-planar shape
- B32B1/08—Tubular products
-
- 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
- B32B5/00—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
- 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
- B32B5/024—Woven fabric
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- 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
- B32B5/00—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
- B32B5/22—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
- B32B5/262—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary characterised by one fibrous or filamentary layer being a woven fabric layer
- B32B5/263—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary characterised by one fibrous or filamentary layer being a woven fabric layer next to one or more woven fabric layers
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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
- F16L11/02—Hoses, i.e. flexible pipes made of fibres or threads, e.g. of textile
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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
- F16L9/00—Rigid pipes
- F16L9/17—Rigid pipes obtained by bending a sheet longitudinally and connecting the edges
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- 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
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/02—Composition of the impregnated, bonded or embedded layer
- B32B2260/021—Fibrous or filamentary layer
- B32B2260/023—Two or more layers
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- 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
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/04—Impregnation, embedding, or binder material
- B32B2260/046—Synthetic resin
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- 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
- 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
- B32B2262/0253—Polyolefin fibres
-
- 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
- B32B2307/00—Properties of the layers or laminate
- B32B2307/70—Other properties
- B32B2307/732—Dimensional properties
- B32B2307/737—Dimensions, e.g. volume or area
- B32B2307/7375—Linear, e.g. length, distance or width
- B32B2307/7376—Thickness
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- 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
- B32B2597/00—Tubular articles, e.g. hoses, pipes
Definitions
- the present invention relates to a polymer composite pipe, to the use of the polymer composite pipe for transporting cryogenic fluid and to a method of making the polymer composite pipe.
- a large amount of natural gas (mainly methane) is present in remote locations around the world. This gas is of significant value if it can be economically marketed. If the stored gas is reasonably close to the places where it is to be consumed and the terrain between the locations allows, then the gas is generally extracted and transported in gaseous form to those end locations. T ransportation is achieved via underwater and/or onshore pipelines. However, if gas is produced where it is not economically feasible or where it is not permitted to lay a pipeline, then other techniques to transport the gas need to be employed.
- a commonly used technique for transporting gas without a pipeline is to liquefy the gas at or near the production site and then to transfer the liquefied gas into a specially designed storage tank on a carrier, such as a ship.
- Liquefying the gas significantly reduces its volume and increases the mass of gas that can be stored and transported.
- the natural gas is cooled and condensed to a liquid state to produce liquefied natural gas (LNG).
- LNG is typically (but not always) stored and transported at substantially atmospheric pressure and at a temperature of about -162 ° C.
- an LNG carrier arrives at a destination, typically the LNG is unloaded into other storage tanks.
- a regassification processes is then performed, as needed, to convert the LNG back into gaseous form, after which it may be transported, for example via pipelines, to end locations to be used.
- LNG is an increasingly popular transportation method for supplying natural gas to major energy consuming countries.
- the piping used to transport liquefied gases, such as LNG or the liquefied components of air, must be capable of withstanding very low temperatures, typically below -150°C. At such temperatures, steels tend to crack, because they undergo a brittle-ductile transition which causes them to shatter, rather than deform.
- steel combined with 9% Nickel is used (commercialised as ‘Inconel’ or ‘Invar’), because it has a much lower brittle-ductile transition temperature, so remains ductile at the cryogenic temperatures in question.
- Polymer pipe for transporting cryogenic fluids is also known.
- WO 2016/102618 A1 describes a process for making a polymer composite pipe comprising wound layers of polymer composite tape.
- Composite polymer piping has a number of advantages over metal piping. These include the fact that it does not corrode; that it is flexible, so that it may, for example, be wound onto a spool for storage and transport, or easily accommodate bends; that it can be made in continuous lengths which may be several kilometres long avoiding the need for welds and that it may be relatively low in weight. ‘618 is concerned with ensuring that the wound polymer composite tapes provide an adequate barrier to the cryogenic fluids.
- the tapes are wound so as to overlap one another and ensure that the tape edges of the preceding tape layer are overlapped by the next tape layer.
- ‘618 explains that the tapes are wound directly onto a mandrel or that, alternatively, the tapes may be wound onto a tube liner. ‘618 suggests that the tube liner may comprise already consolidated tape layers. A mandrel or such layers of tape may be relatively rigid and inflexible at low temperatures. Moreover, the process to lay the tape layers and consolidate them to form a tube liner may be complex to perform.
- a polymer composite pipe having a longitudinal axis comprising: a. an internal layer having an exterior surface; b. a polymer composite pipe body disposed around and bonded to the exterior surface; wherein the internal layer is formed from a longitudinal sheet of polymer composite having a sheet width defined between a first longitudinal side edge and a second longitudinal side edge, the longitudinal sheet of polymer composite having been wrapped around the longitudinal axis, such that the internal layer has the form of a broken annular cylinder having a circumference which is greater than the sheet width, the internal layer comprising a longitudinally extending break defined between the first longitudinal side edge and the second longitudinal side edge.
- the polymer composite pipe body is bonded to the exterior surface by fusion.
- the internal layer provides a surface onto which the polymer composite pipe body may be disposed. If a layer, such as the internal layer is not provided, then it may be complex and challenging to make the pipe body, especially in the case in which the pipe body is made of layers of wound tape. In order to wind tape, a surface must be provided onto which it may be wound.
- WO 2016/102618 A1 discusses a steel mandrel for this purpose. A metal mandrel such as this may render the pipe stiff and inflexible. ‘618 suggests that, in some instances, the mandrel may be removed after manufacture of the pipe body. In order to wind tapes to a mandrel, the tapes must be attached to the mandrel and breaking that attachment to remove the mandrel afterwards may not be straightforward. ‘618 also suggests the possibility of using layers of already compacted tape as a liner, but the same technical challenge arises in making such a liner, because it must be manufactured over a mandrel which must then be removed.
- a polymer composite pipe having a longitudinal axis comprising: a. an internal layer having an exterior surface; b. a polymer composite pipe body disposed around and bonded to the exterior surface; wherein the internal layer is formed from a longitudinal sheet of polymer composite having a sheet width defined between a first longitudinal side edge and a second longitudinal side edge, the longitudinal sheet of polymer composite having been wrapped around the longitudinal axis, such that the first longitudinal side edge and the second longitudinal side edge are contiguous or overlap one another and the internal layer has the form of an annular cylinder.
- the polymer composite pipe body is bonded to the exterior surface by fusion.
- first longitudinal side edge and the second longitudinal side edge are contiguous, they may or may not be connected together. If the first longitudinal side edge is connected to the second longitudinal side edge, then the connection may be formed by any suitable method, such as by bonding. In one example, bonding may be by fusion.
- the annular cylinder may or may not be sealed in the region of overlap. If there is a seal, then the seal may be formed by any suitable method, such as by bonding. In one example, bonding may be by fusion.
- Both the first and second alternatives of the first aspect of the invention provide a polymer composite pipe body disposed over an internal layer formed of a longitudinal sheet of polymer composite which has been wrapped into a cylinder or broken cylinder.
- the internal layer is formed of a single, unitary material which is simple to make and is of a homogenous, unitary construction, with fewer joins than other alternatives, such as already consolidated tape layers.
- Making the internal layer in this way also allows the skilled person easily to specify the alignment of fibres embedded in the polymer composite of the internal layer. Selecting the fibre alignment may allow properties of the internal layer, such as the stiffness, to be tailored to different end-uses.
- the longitudinally extending break provided in the first alternative of the first aspect of the invention may enhance the flexibility of the composite polymer pipe.
- the internal layer is not intended to function as a barrier layer, so the presence of a break is acceptable.
- the internal layer has a thickness of 0.1-1 mm, or a thickness of 0.2-0.7mm.
- the polymer composite may comprise or consist of polymer fibres embedded in a polymer matrix, that is, both the longitudinal sheet of polymer composite and the polymer composite pipe body comprise or consist of polymer fibres embedded in a polymer matrix.
- the polymer fibres and the polymer matrix may comprise or consist of the same homopolymer, or one of them may comprise or consist of a copolymer thereof, or both of them may comprise or consist of a mixture of copolymer and homopolymer.
- the homopolymer and/or copolymer is a thermoplastic polymer.
- the polymer fibres and the polymer matrix comprise or consist of the same polyolefin homopolymer, or one of them may comprise or consist of a copolymer of the polyolefin, or both of them may comprise or consist of a mixture of the polyolefin homopolymer and a polyolefin copolymer.
- the polyolefin is polyethylene or polypropylene.
- the polymer fibres consist of polypropylene or a copolymer thereof or mixtures thereof and the polymer matrix consists of polypropylene or a copolymer thereof or mixtures thereof.
- the polymer fibres have a softening point which is higher than the softening point of the polymer matrix. This may ensure that, if heat is applied to the polymer composite, for example during a heat compaction process or during welding and fusion processes, the matrix softens or melts, but the fibres do not soften or melt.
- the person skilled in polymer technology is aware of pairs of polymers which allow such a tailored softening point difference to be achieved.
- the polymer fibres of the internal layer are aligned either parallel to the longitudinal axis or orthogonal to the longitudinal axis.
- the composite pipe body comprises layers of wound polymer composite tape.
- the pipe body comprises: a. a first layer of polymer composite tape wound over the internal layer, the first layer of polymer composite tape comprising a plurality of adjacent windings all applied at the same angle, being an angle in the range from
- a fourth layer of polymer composite tape wound over the third layer comprising a plurality of adjacent windings, all applied at the same angle as the windings of the third layer of polymer composite tape, the windings of the fourth layer of polymer composite tape being applied longitudinally offset with respect to the windings of the third layer of polymer composite tape, so as to overlap the interfaces of the adjacent windings in the third layer of polymer composite tape; wherein the longitudinal axis is defined to be 0°.
- These layers of wound polymer composite tape may provide the fluid containment barrier and the pressure boundary wall of the pipe.
- the longitudinal offset in b and d is 30-70% of the tape width and, in another example, the longitudinal offset in b and d is about 50% of the tape width.
- the pipe body may additionally comprise one or more further layer(s) of tape wound over the fourth layer, each tape layer being wound at an angle from ⁇ 15° to ⁇ 40°.
- additional layers may bestow axial and bending strength to the polymer composite pipe.
- the polymer composite pipe according to the invention may be manufactured in continuous long lengths, such as greater than 1000m, greater than 2000m or greater than 3000m.
- a composite polymer pipe of the first aspect of the invention for conveying a fluid, especially a liquid, having a temperature below -150°C is provided.
- a method of making a polymer composite pipe having a longitudinal axis comprising a polymer composite pipe body and an internal layer, the method comprising: a. Providing a longitudinal sheet of polymer composite having a sheet width defined between a first longitudinal side edge and a second longitudinal side edge; b. Wrapping the longitudinal sheet of polymer composite around the longitudinal axis to provide the internal layer in the form of a broken annular cylinder having a circumference which is greater than the sheet width, so that the internal layer comprises a longitudinally extending break defined between the first longitudinal side edge and the second longitudinal side edge, the internal layer having an exterior surface; c. Disposing the pipe body around the internal layer and bonding it to the exterior surface.
- a method of making a polymer composite pipe having a longitudinal axis comprising a polymer composite pipe body and an internal layer, the method comprising: a. Providing a longitudinal sheet of polymer composite having a sheet width defined between a first longitudinal side edge and a second longitudinal side edge; b. Wrapping the longitudinal sheet of polymer composite around the longitudinal axis, such that the first longitudinal side edge and the second longitudinal side edge are contiguous or overlap one another to provide the internal layer which has the form of an annular cylinder having an exterior surface; c. Disposing the pipe body around the internal layer and bonding it to the exterior surface.
- the method of the first or second alternatives of the third aspect of the invention provides a simpler process alternative to prior art processes.
- the internal layer is formed of a single longitudinal sheet of polymer composite which is bent into an annular cylinder or a broken annular cylinder around a mandrel. There is no need to remove the internal layer afterwards and the process for making it is simpler than a process for making an annular cylinder of already-compacted tape.
- wrapping the longitudinal sheet of polymer composite in b. is achieved by: i. conveying the longitudinal sheet of polymer composite in a direction of travel over rollers which bend the longitudinal sheet of polymer composite into a U-shaped preform; ii. passing the U-shaped preform through a cone-shaped funnel which is configured to wrap the U-shaped preform around a mandrel to provide the internal layer.
- the longitudinal sheet of polymer composite may additionally be heated sufficiently to render it compliant and reduce the degree of force needed to bend it into a U-shaped preform and wrap it around the mandrel.
- disposing the polymer composite pipe body around the internal layer in c. is achieved by winding one or more layer(s) of polymer composite tape around the internal layer formed in b.
- the one or more layer(s) of polymer composite tape are wound around the internal layer formed in b while it is still wrapped around the mandrel.
- the one or more layer(s) of polymer composite tape are wound around the internal layer formed in b after the internal layer has been conveyed beyond the mandrel in the direction of travel.
- the second alternative may be used if the internal layer is stiff enough and/or the tension in the tape is sufficiently low for the internal layer not to collapse when tape is wound onto the internal layer.
- the polymer composite tape is bonded to the exterior surface of the internal layer by fusion.
- heat may be provided in the form of a laser beam to fuse the tape of the composite material to exterior surface of the internal layer.
- a laser beam may be capable of providing very localized melting and fusion at one or both of the surfaces to-be-combined, thereby ensuring that the remainder of the composite is not significantly heated and that, for example, the fibres do not soften or melt.
- any second and further layer(s) of wound polymer composite tape are bonded to the preceding layer of wound polymer composite tape by fusion. More preferably, heat is provided in the form of a laser beam to fuse the tape of the composite material to the preceding layer of wound polymer composite tape. Laser fusion/welding may have the advantages discussed above.
- the method comprises: a. winding a first layer of polymer composite tape over the internal layer, the first layer of polymer composite tape comprising a plurality of adjacent windings all applied at the same angle, being an angle in the range from > +75° to ⁇ +90°; b. winding a second layer of polymer composite tape over the first layer, the second layer of polymer composite tape comprising a plurality of adjacent windings, all applied at the same angle as the windings of the first layer of polymer composite tape, the windings of the second layer being applied longitudinally offset with respect to the windings of the first layer, so as to overlap the interfaces of the adjacent windings in the first player of polymer composite tape; c.
- the third layer of polymer composite tape comprising a plurality of adjacent windings all applied at the same angle, being an angle in the range from > -75° to ⁇ -90°; d.
- the fourth layer of polymer composite tape comprising a plurality of adjacent windings, all applied at the same angle as the windings of the third layer of polymer composite tape, the windings of the fourth layer of polymer composite tape being applied longitudinally offset with respect to the windings of the third layer of polymer composite tape, so as to overlap the interfaces of the adjacent windings in the third layer of polymer composite tape; wherein the longitudinal axis is defined to be 0°.
- the longitudinal offset in b and d is 30-70% of the tape width and, in another example, the longitudinal offset in b and d is about 50% of the tape width.
- the method may additionally comprise winding one or more further layer(s) of tape wound over the fourth layer, each tape layer being wound at an angle from ⁇ 15° to ⁇ 40°.
- the method is configured as a continuous process, such that a continuous longitudinal sheet is conveyed in the processing direction, is continuously wrapped to form an internal layer in the form of an annular cylinder or a broken annular cylinder having an exterior surface and the pipe body is continuously disposed around and bonded to the exterior surface.
- the continuous process may allow polymer composite pipe to be manufactured in continuous long lengths, such as greater than 1000m, greater than 2000m or greater than 3000m.
- Figure 1 shows a schematic perspective view of an apparatus used in the method according to an example of the invention.
- Figure 2 shows a schematic perspective view of part of the apparatus used in the method according to an example of the invention.
- Figure 3 shows a further perspective view of part of the apparatus used in the method according to an example of the invention.
- Figure 4 shows an end elevation of the polymer composite pipe according to an example of the invention.
- FIG 5 shows detail ‘A’ of the polymer composite pipe of Figure 4.
- a polypropylene single polymer composite (SPC) sheet comprising:
- polypropylene copolymer matrix in the form of thin film sheets (thin film sheet) having a softening point which is 20°C lower than the melting point of the polypropylene homopolymer fibres.
- One or more woven sheets is encased between thin film sheets to form the SPC. If there is more than one woven sheet, then each woven sheet may be separated from the next woven sheet by a thin film sheet interposed between the woven sheets.
- an SPC sheet is prepared which comprises three woven sheet layers, each having a thickness of 0.15mm. Each woven sheet layer is separated from the next woven sheet layer by an intermediate layer of thin film sheet, so that there are two intermediate layers of thin film sheet in total. Each intermediate layer of thin film sheet has a thickness of 0.02mm. The combination is sandwiched between two “skin” layers of thin film sheet, each skin layer having a thickness of 0.04mm. There are thus seven layers in total, being two “skin” layers, three woven sheet layers and two intermediate layers.
- the seven sandwiched layers are hot-compacted into an SPC of 0.57mm thickness.
- the thin film layers soften or melt to form the matrix.
- Softening or melting of the polypropylene homopolymer fibres is avoided or minimized, by careful application of heat and because of the higher softening point of the homopolymer fibres.
- SPCs of the present type are strong and tough at cryogenic temperatures, they are flexible and relatively low cost to produce. Their good material properties are in part due to the good adhesion between the fibres and the matrix on account of their identical or very similar chemical properties. SPCs have the environmental advantage that they may be melted to recycle them.
- a 50.8mm (2 inch) internal diameter pipe is manufactured from the above-described SPC sheet in the following manner.
- pipes having other dimensions, such as 15.24cm (6 inch), 20.32cm (8 inch) or 25.4cm (10 inch) internal diameter, etc., could also be made in this way:
- Both an internal layer and polymer composite tape are cut to width from a longitudinal sheet of SPC.
- the polymer composite tape is cut to have a width of 18mm (and has a thickness of 0.57mm, as mentioned above).
- the internal layer, cut to a width of 159.51 mm, is additionally rolled to further compact it to a thickness of 0.4mm.
- the longitudinal sheet of SPC (1 ) is conveyed in a direction of travel (2) through a forming box (not shown) which heats the longitudinal sheet of SPC (1 ) to 50-70°C to make it more pliable.
- the fibres embedded in the longitudinal sheet of SPC are aligned parallel to the direction of travel (2) or are aligned at 90° to the direction of travel (2).
- the longitudinal sheet of SPC (1 ) is conveyed further in the direction of travel (2) over rollers (4) which bend it into a U- shaped preform (5).
- the forming box and rollers (4) are located in housing (3) in Figure 1. Housing (3) has been removed for the purposes of showing the internal workings in Figures 2 and 3.
- the U-shaped preform (5) is conveyed further in the direction of travel (2) through a cone-shaped funnel (6) and onto a static mandrel (8) to wrap it into an internal layer (7) in the form of a broken annular cylinder, such that the longitudinal break (11 ), shown in Figures 4 and 5, in the broken annular cylinder is 2mm wide.
- the windings of the first layer of SPC tape (10) are applied at an angle of about +85° to the longitudinal axis (the longitudinal axis is defined as 0°) and are fused to the internal layer (7) by laser welding using a laser welding device (not shown).
- the windings of the second layer of SPC tape (10) are applied over the first layer of SPC tape and the windings are applied at the same angle as the windings of the first layer, but the windings of the second layer of SPC tape (10) are applied longitudinally offset with respect to the windings of the first layer of SPC tape (10), so as to overlap the interfaces of the adjacent SPC tape (10) windings in the first layer.
- the windings of the second layer of SPC tape (10) are fused to the windings of the first layer of SPC tape (10) by laser welding using a laser welding device (not shown).
- the windings of the third layer of SPC tape (10) are applied at an angle of about -85° to the longitudinal axis and are fused to the windings of the second layer of SPC tape (10) by laser welding using a laser welding device (not shown).
- the windings of the fourth layer of SPC tape (10) are applied over the third layer of SPC tape (10) and the windings are applied at the same angle as the windings of the third layer, but the windings of the fourth layer of SPC tape (10) are applied longitudinally offset with respect to the windings of the third layer of SPC tape (10), so as to overlap the interfaces of the adjacent SPC tape (10) windings in the third layer.
- the windings of the fourth layer of SPC tape (10) are fused to the windings of the third layer of SPC tape (10) by laser welding using a laser welding device.
- the four layers (9) of windings at an angle of about +/-85 0 are essentially hoop windings which, together, form the pressure boundary wall.
- the windings of the fifth layer of SPC tape (10) are applied at an angle of +25° to the longitudinal axis and are fused to the fourth layer of SPC tape (10) by laser welding using a laser welding device (not shown).
- the windings of the sixth layer of SPC tape (10) are applied at an angle of - 25° to the longitudinal axis and are fused to the fifth layer of SPC tape (10) by laser welding using a laser welding device (not shown).
- the windings of the seventh layer of SPC tape (10) are applied at an angle of +25° to the longitudinal axis and are fused to the sixth layer of SPC tape (10) by laser welding using a laser welding device (not shown).
- the windings of the eighth layer of SPC tape (9) are applied at an angle of - 25° to the longitudinal axis and are fused to the seventh layer of SPC tape (10) by laser welding using a laser welding device (not shown).
- Layers 5-8 bestow axial and bending strength to the pipe.
- Figure 4 shows a cross-section of the finished polymer composite pipe and
- Figure 5 is a magnified detail ‘A’ from Figure 4.
- These figures show the internal layer (7) and the layers (9) of wound SPC tape (10).
- the longitudinal break (11 ) in the internal layer is also shown.
- a polymer composite pipe manufactured according to this example has an internal diameter of 50.8mm (2 inch) and a length of 2000m. It is suitable for conveying LNG and may be operated at a pressure of up to 19 Barg (Bar gauge) and a temperature from -196°C to +50°C, with -163°C being a typical operating temperature.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Rigid Pipes And Flexible Pipes (AREA)
- Laminated Bodies (AREA)
- Thermal Insulation (AREA)
Abstract
Description
Claims
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP23832787.8A EP4627248A1 (en) | 2022-12-01 | 2023-11-21 | Pipe for transporting cryogenic fluids |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2218112.7 | 2022-12-01 | ||
| GB2218112.7A GB2624936B (en) | 2022-12-01 | 2022-12-01 | Pipe for transporting cryogenic fluids |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2024115883A1 true WO2024115883A1 (en) | 2024-06-06 |
Family
ID=84926574
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/GB2023/053039 Ceased WO2024115883A1 (en) | 2022-12-01 | 2023-11-21 | Pipe for transporting cryogenic fluids |
Country Status (3)
| Country | Link |
|---|---|
| EP (1) | EP4627248A1 (en) |
| GB (2) | GB2624936B (en) |
| WO (1) | WO2024115883A1 (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2814313A (en) * | 1952-11-21 | 1957-11-26 | Cordo Chemical Corp | Manufacture of pipe |
| JPH04201547A (en) * | 1990-11-30 | 1992-07-22 | Sekisui Chem Co Ltd | Manufacture of fiber reinforced resin pipe |
| US20160053922A1 (en) * | 2012-06-04 | 2016-02-25 | Mohammad R. Ehsani | Endless on-site pipe manufacturing |
| WO2016102618A1 (en) | 2014-12-24 | 2016-06-30 | Shell Internationale Research Maatschappij B.V. | Process for manufacturing a tube or a vessel of composite material |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2564708B (en) * | 2017-07-21 | 2020-02-12 | Magma Global Ltd | Void volume measurement for a composite pipe |
-
2022
- 2022-12-01 GB GB2218112.7A patent/GB2624936B/en active Active
- 2022-12-01 GB GB2317570.6A patent/GB2624976B/en active Active
-
2023
- 2023-11-21 EP EP23832787.8A patent/EP4627248A1/en active Pending
- 2023-11-21 WO PCT/GB2023/053039 patent/WO2024115883A1/en not_active Ceased
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2814313A (en) * | 1952-11-21 | 1957-11-26 | Cordo Chemical Corp | Manufacture of pipe |
| JPH04201547A (en) * | 1990-11-30 | 1992-07-22 | Sekisui Chem Co Ltd | Manufacture of fiber reinforced resin pipe |
| US20160053922A1 (en) * | 2012-06-04 | 2016-02-25 | Mohammad R. Ehsani | Endless on-site pipe manufacturing |
| WO2016102618A1 (en) | 2014-12-24 | 2016-06-30 | Shell Internationale Research Maatschappij B.V. | Process for manufacturing a tube or a vessel of composite material |
Also Published As
| Publication number | Publication date |
|---|---|
| GB2624976B (en) | 2025-02-05 |
| GB202218112D0 (en) | 2023-01-18 |
| EP4627248A1 (en) | 2025-10-08 |
| GB2624936B (en) | 2025-02-12 |
| GB2624976A (en) | 2024-06-05 |
| GB2624936A (en) | 2024-06-05 |
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