WO2000075546A1 - Buoyant composite material - Google Patents

Buoyant composite material Download PDF

Info

Publication number
WO2000075546A1
WO2000075546A1 PCT/GB2000/002130 GB0002130W WO0075546A1 WO 2000075546 A1 WO2000075546 A1 WO 2000075546A1 GB 0002130 W GB0002130 W GB 0002130W WO 0075546 A1 WO0075546 A1 WO 0075546A1
Authority
WO
WIPO (PCT)
Prior art keywords
composite material
tubular members
moulded composite
matrix
moulded
Prior art date
Application number
PCT/GB2000/002130
Other languages
French (fr)
Inventor
Andrew Charles Ratcliffe Tyrer
Original Assignee
Crp Group Limited
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority claimed from GBGB9913131.0A external-priority patent/GB9913131D0/en
Application filed by Crp Group Limited filed Critical Crp Group Limited
Priority to AU52323/00A priority Critical patent/AU5232300A/en
Publication of WO2000075546A1 publication Critical patent/WO2000075546A1/en

Links

Classifications

    • 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
    • F16L11/04Hoses, i.e. flexible pipes made of rubber or flexible plastics
    • F16L11/12Hoses, i.e. flexible pipes made of rubber or flexible plastics with arrangements for particular purposes, e.g. specially profiled, with protecting layer, heated, electrically conducting
    • F16L11/133Hoses, i.e. flexible pipes made of rubber or flexible plastics with arrangements for particular purposes, e.g. specially profiled, with protecting layer, heated, electrically conducting buoyant
    • 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
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/58Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising fillers only, e.g. particles, powder, beads, flakes, spheres
    • B29C70/66Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising fillers only, e.g. particles, powder, beads, flakes, spheres the filler comprising hollow constituents, e.g. syntactic foam
    • 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
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/68Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
    • B29C70/681Component parts, details or accessories; Auxiliary operations
    • B29C70/682Preformed parts characterised by their structure, e.g. form
    • 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
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/68Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
    • B29C70/685Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks by laminating inserts between two plastic films or plates
    • B29C70/687Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks by laminating inserts between two plastic films or plates the inserts being oriented, e.g. nets or meshes
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08JWORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J9/00Working-up of macromolecular substances to porous or cellular articles or materials; After-treatment thereof
    • C08J9/32Working-up of macromolecular substances to porous or cellular articles or materials; After-treatment thereof from compositions containing microballoons, e.g. syntactic foams
    • EFIXED CONSTRUCTIONS
    • E21EARTH DRILLING; MINING
    • E21BEARTH DRILLING, e.g. DEEP DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
    • E21B17/00Drilling rods or pipes; Flexible drill strings; Kellies; Drill collars; Sucker rods; Cables; Casings; Tubings
    • E21B17/01Risers
    • E21B17/012Risers with buoyancy elements
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/60Multitubular or multicompartmented articles, e.g. honeycomb
    • B29L2031/601Multi-tubular articles, i.e. composed of a plurality of tubes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/706Buoys

Definitions

  • the present invention relates to composite materials which are moulded and
  • buoyant and also to buoyancy modules and insulating jackets comprising such
  • Fig. 1 illustrates the structure of a composite material well known for certain
  • spherical beads 2 known to those skilled in the art as macrospheres, set in a moulded
  • the matrix 4 of syntactic foam is of low density, being formed
  • thermosetting plastics typically polyester or epoxy.
  • the macrospheres are of a
  • the syntactic foam matrix itself comprises thermosetting plastics with thermosetting plastics with thermosetting plastics with thermosetting plastics with thermosetting plastics with thermosetting plastics with thermosetting plastics with thermosetting plastics with thermosetting plastics with thermosetting plastics with thermosetting plastics with thermosetting plastics with thermosetting plastics with thermosetting plastics with thermosetting plastics with thermosetting plastics with thermosetting plastics with thermosetting plastics with thermosetting plastics with thermosetting plastics with thermosetting plastics with thermosetting plastics with
  • the macrospheres can be manufactured by tumbling the expanded
  • polystyrene spheres 6 in a thermosetting plastics resin to coat them and so form the
  • macrospheres are formed by ultrasonically welding together two injection moulded
  • plastics hemispheres or by epoxy bonding two forged aluminium hemispheres are plastics hemispheres or by epoxy bonding two forged aluminium hemispheres.
  • Diameters can be in excess of 30 centimetres. It is also known to use macrospheres of mixed diameter to improve their packing factor.
  • thermosetting material has proved highly effective in use. While the thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting thermosetting
  • buoyancy elements One example of the material's use is in subsea oil extraction.
  • buoyancy modules require support along their length and this is typically provided by buoyancy modules
  • the matrix material is typically relatively
  • thermosetting plastics of the matrix since excess heat can create problems during the moulding process and can damage the macrospheres. This heating can
  • a further object of the present invention is to provide an improved buoyancy
  • composite material having positive buoyancy in water and comprising a matrix comprising plastics within which is disposed a plurality of elongate, substantially
  • the plastics material of the matrix is preferably a thermosetting plastics.
  • Polyester or epoxy are suitable, as are
  • vinyl ester in particular epoxy vinyl ester
  • phenolic phenolic
  • Polyurethane may be used.
  • Thermoplastics may alternatively be used.
  • the matrix should be such as to be crushed.
  • the matrix should be stiff enough to serve this function.
  • the stiffness of the matrix can be specified in terms of its Uniaxial
  • the matrix should comprise
  • UCM should have UCM not less than 300 Mpa.
  • UCMs as high as 2500MPa can be
  • the matrix material may itself be less dense than water. Currently preferred
  • thermosetting matrix material
  • tubular members can reinforce the material in a
  • buoyancy modules as used on sub-sea risers, can contain tubular members oriented
  • tubular members may be even more closely packed if, in accordance with
  • the material comprises first tubular members
  • first tubular members having a first lateral dimension and second tubular members having a second lateral
  • the packing of the tubular members can be still further increased by forming
  • polygonal cross section eg quadrilateral (which may be square or rectangular), triangular or hexagonal, such that the members can tessellate.
  • the material may further comprise macrospheres. These can be disposed in
  • Lateral dimensions of the tubular members are preferably macroscopic.
  • Lateral dimensions of substantially 5 mm and greater are preferred, and lateral
  • range of lateral dimensions is from 20 to 60 mm.
  • Walls of the tubular members are typically in the range 1 - 5 mm. in
  • Ends of the tubular members are preferably provided with closure means for
  • the end caps also help to withstand hydrostatic pressure in use.
  • means may comprise caps shaped to mate with respective tubular member ends.
  • the tubular members may comprise metal walls.
  • metal walls For example, aluminium
  • composite material forms the tubular
  • Fibre reinforced plastic is a suitable material. A pultruded or
  • extruded fibre reinforced plastic tube is especially suitable.
  • the currently preferred embodiments utilise filament wound tubes. It is particularly preferred that the walls
  • Glass fibres may be used but carbon fibres are particularly preferred.
  • tubular members to the surrounding matrix material.
  • tubular member exterior may be adapted to
  • aluminium, or other, tubes may be first blasted clean and then externally primed to form the bond.
  • the tubular members are preferably shaped to improve their crush resistance.
  • tubular members' cross section should vary along
  • the matrix material comprises syntactic foam.
  • the tubular members may be filled with gas - typically air.
  • gas - typically air
  • Aluminium paint could be given an insulative coating, eg a reflective coating. Aluminium paint
  • tubular members could be used for this purpose. It is especially preferred that the tubular members be closely packed. They
  • module or float comprising material according to the first aspect of the present
  • the float may be for attachment to a riser. Alternatively it may be a float for
  • ROV Remotely Operated Vehicle
  • float may alternatively take the form of an underwater buoy.
  • insulation module or jacket comprising material according to the first aspect of the
  • Such a jacket may be shaped and adapted to be arranged around a subsea oil
  • the present invention serves to provide to the relatively warm interior and the cooler exterior.
  • the module is maintained in more intimate contact with the pipeline, improving its performance.
  • tubular members are preferably aligned with a longitudinal axis of the item.
  • tubular members preferably each extend along substantially the full length of the
  • tubular members may extend along only part of the length of
  • the item and be of various lengths such that tubular member ends are misaligned
  • Fig. 1 illustrates the structure of a known buoyancy composite material in
  • Fig. 2 illustrates the structure of a material according to the present invention
  • Fig. 3 is a side view of a tube used in an embodiment of the present invention.
  • Fig. 4 is a perspective view of a riser buoyancy module according to the
  • the material illustrated in Fig. 2 comprises a matrix 20 of syntactic foam in
  • tubes serve as density reducing elements. Axes of the tubes are mutually parallel.
  • the lateral positioning of the tubes is not, in the illustrated embodiment, according to a uniform pattern.
  • the tubes are straight.
  • the tubes are also hollow.
  • the tubes may be at least partially
  • the material may comprise tubes of two or more types. For instance,
  • the packing factor of the tubes may be
  • tubes 22 with their ends closed are placed in a mould with their longitudinal axes
  • thermosetting plastics resin thermosetting plastics resin
  • FIG. 3 illustrates in isolation an alternative form of tube 30 to be used in the
  • the tube being of filament
  • resulting tube can be removed from the mandrel and is both light and stiff.
  • the process makes it
  • the wall thickness typically varies between 1 and 5
  • the desired variation in wall thickness could be achieved by using fibres of
  • a tape e.g. a metal tape
  • the tape could again be overwound with fibres.
  • the necessary shape may be imprinted on the tube exterior, eg
  • plastics resin can be any material.
  • plastics resin can flow into the region around the tube end.
  • a buoyancy module for attachment to a riser of the type
  • the module comprising
  • buoyancy elements 40 formed from composite
  • shaped mouldings may have tubes oriented in two or more different directions in

Abstract

A moulded composite material is disclosed which comprises a set of elongate tubular members 22 arranged substantially parallel to each other within a surrounding matrix 20 which comprises plastics, and most preferably syntactic foam. The matrix material is excluded from the interior of the tubular members, e.g. by provision of end caps 34 on the tubular member ends, and the resulting material is buoyant. The tubular members can be particularly closely packed to minimise density of the material and contribute strength to the material. Applications of the material include buoyancy modules, particularly for pipes and risers used subsea.

Description

DESCRIPTION
BUOYANT C0MPOSTE MATERIAL
The present invention relates to composite materials which are moulded and
buoyant, and also to buoyancy modules and insulating jackets comprising such
materials.
Fig. 1 illustrates the structure of a composite material well known for certain
maritime applications and comprising a large number of macroscopically sized
spherical beads 2, known to those skilled in the art as macrospheres, set in a moulded
matrix 4 of syntactic foam. The macrospheres 2 are of low density, being formed
with an expanded polystyrene core 6 surrounded by a harder shell 8 formed of
thermosetting plastics - typically polyester or epoxy. The macrospheres are of a
generally regular size in the illustrated material although in the cross section seen in
FigJ the exposed parts of the macrospheres vary in diameter due to the random bead
positioning. The syntactic foam matrix itself comprises thermosetting plastics with
an admixture of microspheres - hollow glass spheres too small to be seen in the
drawing.
The macrospheres can be manufactured by tumbling the expanded
polystyrene spheres 6 in a thermosetting plastics resin to coat them and so form the
shell 8, but this proves a troublesome process in practice. Alternative known
macrospheres are formed by ultrasonically welding together two injection moulded
plastics hemispheres or by epoxy bonding two forged aluminium hemispheres.
Diameters can be in excess of 30 centimetres. It is also known to use macrospheres of mixed diameter to improve their packing factor.
The material has proved highly effective in use. While the thermosetting
plastics is relatively dense, the inclusion of macrospheres and microspheres results
in a low overall density and hence good buoyancy. The material is thus suitable for
buoyancy elements. One example of the material's use is in subsea oil extraction.
Risers through which oil is conducted upward from a subsea well head to a rig
require support along their length and this is typically provided by buoyancy modules
formed by two generally "C" sectioned members formed of the material in question
and positioned to surround the riser. Means such as a tension band around the "C"
members secure them to the riser and a clamp engaging with the riser itself may be
provided to prevent motion of the buoyancy modules along the riser. The risers in
question may be of flexible type or may be of more rigid metal construction.
Despite the success of the above described material there are commercial and
technical incentives to improve upon it.
It is desirable, particularly where the material is used in a buoyancy element,
to minimise density and so maximise buoyancy for a given volume. Clearly it is
therefore desirable to increase the volume of the low density macroscopic elements -
in the known material, the macrospheres 2 - relative to that of the more dense matrix
material 4. Such decrease in the relative proportion of the matrix material is also
desirable in order to reduce costs (the matrix material is typically relatively
expensive) and to reduce the amount of heat given off during the exothermic curing
of the thermosetting plastics of the matrix, since excess heat can create problems during the moulding process and can damage the macrospheres. This heating can
undesirably limit the dimensions of items to be moulded, there being in effect a
critical size above which heating effects become unacceptable.
Unfortunately an upper limit on the proportion of the material which can be
taken up by the macrospheres of the known material is imposed by their mode of
packing.
Furthermore, any decrease in material density must be achieved while
maintaining acceptable mechanical properties - resistance to crushing, creep,
breakage etc. Indeed it is desirable to improve upon the resistance to breakage of the
known composite material since existing buoyancy modules made from the material
can on occasion break if mishandled.
It is an object of the present invention to provide an improved buoyant
composite material. Additionally or alternatively it is desired to provide a buoyant
composite material which can achieve lower density than the known composite
materials while maintaining required material properties such as resistance to
structural failure.
A further object of the present invention is to provide an improved buoyancy
module. Additionally or alternatively it is desired to provide a buoyancy module of
increased buoyancy (for a given volume) which nonetheless has required material
properties such as resistance to structural failure.
In accordance with a first aspect of the present invention, there is a moulded
composite material having positive buoyancy in water and comprising a matrix comprising plastics within which is disposed a plurality of elongate, substantially
mutually parallel, tubular members, the matrix material being excluded from the
interiors of the tubular members.
The plastics material of the matrix is preferably a thermosetting plastics.
Mouldable resins are particularly preferred. Polyester or epoxy are suitable, as are
vinyl ester (in particular epoxy vinyl ester) and phenolic. Polyurethane may be used.
Thermoplastics may alternatively be used.
The material's properties, and in particular its capacity to withstand
hydrostatic pressure without structural damage, result from a combination of the
properties of the tubular members and the matrix. Structural damage could in
particular occur if excessive pressure is placed on the tubular members, causing one
or more to be crushed. It is especially preferred that the matrix should be such as to
contribute resistance to crashing of the tubular members by hydrostatic pressure. In
paraticular it is preferred that the matrix should be stiff enough to serve this function.
Thus the entire compressive force due to immersion need not be borne by the tubular
members.
The stiffness of the matrix can be specified in terms of its Uniaxial
Compressive Modulus (UCM). It is preferred that the matrix should comprise
material having UCM not less than 150 Mpa. Still more preferably the material
should have UCM not less than 300 Mpa. UCMs as high as 2500MPa can be
achieved using plastics materials and may prove useful for deep water applications,
although materials with UCM in the region of 1200 Mpa are considered suitable for systems usable at 6000m depth.
The matrix material may itself be less dense than water. Currently preferred
materials have densities in the range 0.3 to 0.7gm./cc.
Whereas the known macrospheres, even when closely packed, can take up
approximately 55-60% of the volume of the known material previously described, the
elongate tubular members utilised in the material according to the present invention
can be packed to take up 70% volume or more. This allows a considerable reduction
in the relative volume of the matrix material and so in density, cost and in heat given
off on curing of thermosetting matrix material.
These advantages can be achieved while maintaining acceptable mechanical
properties of the material, since the tubular members can reinforce the material in a
manner not possible with macrospheres. Resistance of the material to breakage can
be particularly great along the tubular member's axes. Hence for example elongate
buoyancy modules, as used on sub-sea risers, can contain tubular members oriented
along their length, resulting in a module which is highly resistant to breakage.
The tubular members may be even more closely packed if, in accordance with
a preferred aspect of the invention, the material comprises first tubular members
having a first lateral dimension and second tubular members having a second lateral
dimension smaller than the first, the second tubular members being disposed in
interstices between the first tubular members.
The packing of the tubular members can be still further increased by forming
them to have a polygonal cross section, eg quadrilateral (which may be square or rectangular), triangular or hexagonal, such that the members can tessellate.
A further advantage of the material according to the invention is that the
tubular members can straightforwardly be made resistant to heat effects which can
damage macrospheres during moulding of an item.
The material may further comprise macrospheres. These can be disposed in
spaces around the tubular members and/or can be disposed in other re-entrant features
of the moulding, further reducing density.
Lateral dimensions of the tubular members are preferably macroscopic.
Lateral dimensions of substantially 5 mm and greater are preferred, and lateral
dimensions as large as 100mm. are considered suitable, but the currently favoured
range of lateral dimensions is from 20 to 60 mm.
Walls of the tubular members are typically in the range 1 - 5 mm. in
thickness.
Ends of the tubular members are preferably provided with closure means for
excluding matrix material from the tubular member interiors during the moulding
process. The end caps also help to withstand hydrostatic pressure in use. The closure
means may comprise caps shaped to mate with respective tubular member ends.
The tubular members may comprise metal walls. For example, aluminium
or titanium tubing may be used.
However in the preferred embodiment, composite material forms the tubular
member walls. Fibre reinforced plastic is a suitable material. A pultruded or
extruded fibre reinforced plastic tube is especially suitable. The currently preferred embodiments utilise filament wound tubes. It is particularly preferred that the walls
comprise helically or circumferentially wound fibres to improve crush resistance.
Glass fibres may be used but carbon fibres are particularly preferred.
Mechanical properties of the material may be improved by providing the
exteriors of the tubular members with shaped features which securely couple the
tubular members to the surrounding matrix material. For example a
circumferentially ribbed exterior prevents motion of the tubular member through the
matrix. Alternatively or additionally the tubular member exterior may be adapted to
bond to the matrix material. For example aluminium, or other, tubes may be first blasted clean and then externally primed to form the bond.
The tubular members are preferably shaped to improve their crush resistance.
In particular it is preferred that the tubular members' cross section should vary along
their lengths such as to increase the members' crush resistance. This may be by
ribbing or convolution of the walls of the members.
It is especially preferred that the matrix material comprises syntactic foam.
The tubular members may be filled with gas - typically air. However
according to a preferred embodiment of the present invention, the tubular members
are at least partly evacuated. In this way a material with low thermal conductivity
can be produced which is suitable for items such as insulating jackets for use subsea.
To further improve insulation properties, interior surfaces of the tubular members
could be given an insulative coating, eg a reflective coating. Aluminium paint
could be used for this purpose. It is especially preferred that the tubular members be closely packed. They
may be disposed one in contact with another or may be slightly mutually separated.
According to a second aspect of the present invention there is a buoyancy
module or float comprising material according to the first aspect of the present
invention.
The float may be for attachment to a riser. Alternatively it may be a float for
use in a submersible vehicle, for example a Remotely Operated Vehicle (ROV). The
float may alternatively take the form of an underwater buoy.
According to a third aspect of the present invention there is a thermal
insulation module or jacket comprising material according to the first aspect of the
present invention.
Such a jacket may be shaped and adapted to be arranged around a subsea oil
conduit and so to reduce loss of heat to surrounding water. Such jackets, formed
from other materials, are well known and help to prevent oil, following extraction,
from being cooled by the surrounding water to a temperature at which hydrate
formation - build up of waxy deposits - takes place causing the conduit to become
partially or wholly blocked.
Known insulating jackets comprising syntactic foam are subject to
deformation due to temperature variations, particularly due to the difference between
the relatively warm interior and the cooler exterior. The present invention serves to
reduce bending or other deformation since the tubular members resist bending
moments. Hence the module is maintained in more intimate contact with the pipeline, improving its performance.
In items formed from the material according to the present invention, the
tubular members are preferably aligned with a longitudinal axis of the item. The
tubular members preferably each extend along substantially the full length of the
item. Alternatively the tubular members may extend along only part of the length of
the item and be of various lengths such that tubular member ends are misaligned
with each other. In this way it is possible to avoid creating zones of weakness in the
material.
Specific embodiments of the present invention will now be described, by way
of example only, with reference to the accompanying drawings, in which: -
Fig. 1 illustrates the structure of a known buoyancy composite material in
perspective;
Fig. 2 illustrates the structure of a material according to the present invention
in perspective;
Fig. 3 is a side view of a tube used in an embodiment of the present invention;
and
Fig. 4 is a perspective view of a riser buoyancy module according to the
present invention.
The material illustrated in Fig. 2 comprises a matrix 20 of syntactic foam in
which are set circular tubes 22, formed in the Fig. 2 embodiment of aluminium. The
tubes serve as density reducing elements. Axes of the tubes are mutually parallel.
The lateral positioning of the tubes is not, in the illustrated embodiment, according to a uniform pattern. The tubes are straight. The tubes are also hollow.
Ends of the tubes are closed by shaped caps (not seen in Fig. 2) inserted into
the tube ends prior to the moulding process. In this way syntactic foam is excluded
from the tube interiors during moulding and the tubes are thus empty - that is to say
they contain only air. In other embodiments, the tubes may be at least partially
evacuated. The tubes are, in the completed moulding, sealed against ingress of water
which could otherwise enter the material due to hydrostatic pressure on immersion.
While the tubes of the illustrated embodiment are all of the same diameter and
construction, the material may comprise tubes of two or more types. For instance,
by utilising tubes of two different diameters the packing factor of the tubes may be
increased. It may be arranged that the tubes lying toward the surface of an item are
more robust that those lying toward the item's centre, making possible a reduction
in density without unacceptable impairment of the item's strength, crush resistance,
etc.
In the preferred method of moulding items from the material in question, the
tubes 22 with their ends closed are placed in a mould with their longitudinal axes
parallel (or at least substantially parallel). Syntactic foam resin (or other
thermosetting plastics resin) is then introduced to the mould and allowed to set.
In an alternative mode of construction, it is arranged that the tubes are slightly
mutually separated so that the resin can enter space between the tubes to improve the
strength of the material. For example, small spacers could be placed around the
tubes, at intervals along their length, to slightly separate the tubes during moulding. Fig. 3 illustrates in isolation an alternative form of tube 30 to be used in the
composite material according to the present invention, the tube being of filament
wound type. Manufacture of this tube involves in a known manner coating of glass
fibres or other filamentary material with plastics resin followed by winding of the
fibres onto a mandrel, the mandrel being rotated and the fibre being made to traverse
the mandrel to provide helical winding. After setting of the plastics resin, the
resulting tube can be removed from the mandrel and is both light and stiff. The
process allows properties of the tube - such as wall thickness- to be adjusted straight
forwardly in order to tailor the properties of the composite material to a particular
application. While the wall may be of uniform thickness, the process makes it
straight forward to create a tube wall whose thickness varies along the length of the
tube. The exterior of the illustrated tube can be seen at 32 to undulate along the tube
length due to the arrangement of its fibre windings. While dimensions are adjustable
to suit the particular application the wall thickness typically varies between 1 and 5
mm. It has been found that a tube having wall thickness which varies along the tube
length can have a greater crush resistance for a given weight than an equivalent tube
having uniform wall thickness. Relatively thick annuli along the tube length greatly
increase crush resistance while relatively thin intervening portions of the tube
minimise weight.
The desired variation in wall thickness could be achieved by using fibres of
two different thicknesses in fabrication of the tube, eg by winding relatively thick
fibres - say 2 mm in fhickness-onto the mandrel, then winding over relatively thin fibres - say 20 or 30 microns in thickness. Alternatively a tape, e.g. a metal tape
could be wound onto the mandrel to provide a desired contour for the tube exterior.
The tape could again be overwound with fibres.
Alternatively the necessary shape may be imprinted on the tube exterior, eg
by winding tape on the exterior before the resin of the tube has set.
An advantage of tubes whose exterior profile is shaped along the tube length
is that during the process of moulding the composite material, plastics resin can
penetrate spaces left between adjacent tubes, thereby minimising "dry" portions of
the moulding which the resin does not reach.
Resistance to crushing of the tube is of particular importance for items to be
used at depth, since hydrostatic pressure tends to crush such items and could cause
tubes of inadequate strength to collapse, with the danger of serious structural damage
to the item.
Seen in Fig. 3 is an end cap 34 which closes the end of the tube 30 during the
process of moulding the composite material, the end cap being shaped at 36 to
engage with the tube end and having a domed outer portion 38 which can rest against
the interior wall of the mould during moulding, ensuring by virtue of its domed shape
that plastics resin can flow into the region around the tube end.
Illustrated in Fig. 4 is a buoyancy module for attachment to a riser of the type
used in conducting crude oil away from a sub-sea wellhead, the module comprising
two elongate, generally "C" shaped buoyancy elements 40 (formed from composite
material according to the present invention) which can be secured together by tension straps 42 to form an internal cylindrical cavity 44 to receive the riser.
As can be seen in cutaway portion 46, the tubes of the composite material
extend axially of the elements thereby maximising their strength and resistance to
breaking.
While the tubes in the illustrated buoyancy module are all parallel, differently
shaped mouldings may have tubes oriented in two or more different directions in
different regions of the moulding, as necessary to accommodate features of the
moulding or to maximise strength.
The above described embodiments are, as will be apparent to the skilled
reader, merely illustrative of the range of possibilities arising from the present
invention as defined in the appended claims.

Claims

1. A moulded composite material having positive buoyancy in water and
comprising a matrix which comprises plastics and within which is disposed a
plurality of elongate, substantially mutually parallel tubular members, the matrix
material being excluded from the interiors of the tubular members.
2. A moulded composite material as claimed in claim 1 wherein the matrix
is such as to contribute resistance to crushing of the tubular members by hydrostatic
pressure.
3. A moulded composite material as claimed in claim 1 or claim 2 wherein
the matrix comprises plastics material having Uniaxial Compressive Modulus not
less than 150 Mpa.
4. A moulded composite material as claimed in any preceding claim wherein
the tubular members are closely packed.
5. A moulded composite material as claimed in any preceding claim
comprising tubular members having a lateral dimension which is substantially 5 mm
or greater.
6. A moulded composite material as claimed in any preceding claim
comprising tubular members whose lateral dimensions are between substantially 20
mm and substantially 60 mm.
7. A moulded composite material as claimed in any preceding claim wherein
the matrix comprises thermosetting plastics.
8. A moulded composite material as claimed in any preceding claim wherein
the matrix comprises syntactic foam.
9. A moulded composite material as claimed in any preceding claim wherein
macrospheres are incorporated within the plastics material of the matrix.
10. A moulded composite material as claimed in any preceding claim
wherein the tubular members are circular in cross section.
11. A moulded composite material as claimed in any of claims 1 to 9 wherein
the cross sections of the tubular members are polygonal and are such that the tubular
members can tessellate, the tubular members being arranged such that they tessellate.
12. A moulded composite material as claimed in any preceding claim
wherein the tubular members comprise walls formed of composite material.
13. A moulded composite material as claimed in any preceding claim
wherein the tubular members comprise walls formed of fibre reinforced plastics
material.
14. A moulded composite material as claimed in any preceding claim
wherein the tubular members comprise pultruded or extruded tubes.
15. A moulded composite material as claimed in any of claims 12 to 15
wherein the tubular members have walls comprising generally helically or
circumferentially wound reinforcing fibres.
16. A moulded composite material as claimed in any preceding claim
comprising first tubular members having a first lateral dimension and second tubular
members having a lateral dimension smaller than the first such that the second tubular members are disposed in interstices between the first tubular members.
17. A moulded composite material as claimed in any preceding claim in
which the tubular members are provided with closure means for excluding matrix
material from the tubular member interiors during the moulding process.
18. A moulded composite material as claimed in claim 17 wherein the
closure means are formed as end caps shaped to mate with respective tubular member
ends.
19. A moulded composite material as claimed in any preceding claim
wherein exteriors of the tubular members are provided with shaped features which
securely couple the tubular members to the surrounding matrix.
20. A moulded composite material as claimed in claim 19 wherein the shaped
features comprise helical or circumferential ribbing.
21. A moulded composite material as claimed in claim 18 wherein the tubular
member exteriors are adapted to bond to the matrix.
22. A moulded composite material as claimed in claim 21 wherein the tubular
member exteriors are textured to aid bonding to the matrix.
23. A moulded composite material as claimed in any preceding claim
wherein the tubular members are provided with respective spacers projecting from
the tubular members radially and thereby separating each of the tubular members
from its neighbours.
24. A buoyancy module, float or underwater buoy moulded from composite
material as claimed in any preceding claim.
25. A buoyancy module for coupling to a pipe or riser, the module being
moulded from composite material as claimed in any of claims 1 to 23.
26. A buoyancy module as claimed in claim 25 comprising a pair of
buoyancy bodies which are generally "C" shaped in cross section and adapted to be
secured around the pipe or riser .
27. A thermal insulation module or jacket comprising material as claimed in
any of claims 1 to 23.
28. A thermal insulation module or jacket as claimed in claim 37, shaped and
adapted to be arranged around a subsea oil conduit and so to reduce loss of heat to
surrounding water.
29. A moulded composite material having positive buoyancy in water
substantially as herein described with reference to, and as illustrated in,
accompanying Figs. 2 to 4.
30. A buoyancy module substantially as herein described with reference to,
and as illustrated in, accompanying Fig. 4.
PCT/GB2000/002130 1999-06-08 2000-06-02 Buoyant composite material WO2000075546A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU52323/00A AU5232300A (en) 1999-06-08 2000-06-02 Buoyant composite material

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
GB9913131.0 1999-06-08
GBGB9913131.0A GB9913131D0 (en) 1999-06-08 1999-06-08 Composite material
GB9922175A GB2350819A (en) 1999-06-08 1999-09-21 Composite buoyant material for forming floats
GB9922175.6 1999-09-21

Publications (1)

Publication Number Publication Date
WO2000075546A1 true WO2000075546A1 (en) 2000-12-14

Family

ID=26315640

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/GB2000/002130 WO2000075546A1 (en) 1999-06-08 2000-06-02 Buoyant composite material

Country Status (2)

Country Link
AU (1) AU5232300A (en)
WO (1) WO2000075546A1 (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2002095278A1 (en) * 2001-05-18 2002-11-28 Crp Group Limited Protection of underwater elongate members
WO2006076486A2 (en) 2005-01-14 2006-07-20 Shell Internationale Research Maatschappij B.V. System and methods to install subsea structures
EP1942051A2 (en) 2007-01-02 2008-07-09 In novo d.o.o. Depth buoy for maritime applications and process for making it
CN104494797A (en) * 2014-11-25 2015-04-08 苏州九鼎珍珠棉有限公司 Buoyancy stick based on foam materials
US10030094B2 (en) 2008-07-10 2018-07-24 Huntsman International Llc Polyisocyanurate-based syntactic coating for offshore applications
WO2019077370A1 (en) * 2017-10-20 2019-04-25 Balmoral Comtec Limited A cylindrical element profiled to reduce vortex induced vibration (viv) and/or drag
WO2020194064A2 (en) 2019-03-25 2020-10-01 Acergy France SAS Pressure-resistant buoys
CN112936915A (en) * 2021-04-13 2021-06-11 中国铁塔股份有限公司黑龙江省分公司 Reinforced composite material processing system

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1361215A (en) * 1971-06-09 1974-07-24 Yokohama Rubber Co Ltd Floatable hose and a method of making the same
US3989067A (en) * 1974-12-11 1976-11-02 The Gates Rubber Company Buoyant hose
US4000759A (en) * 1974-12-11 1977-01-04 The Gates Rubber Company Hose
FR2669342A1 (en) * 1990-11-20 1992-05-22 Inst Francais Du Petrole Composition of heat-curable resins which are employed in the manufacture of syntactic foams
GB2299975A (en) * 1995-04-18 1996-10-23 Kvaerner Earl & Wright Removable Buoyancy

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1361215A (en) * 1971-06-09 1974-07-24 Yokohama Rubber Co Ltd Floatable hose and a method of making the same
US3989067A (en) * 1974-12-11 1976-11-02 The Gates Rubber Company Buoyant hose
US4000759A (en) * 1974-12-11 1977-01-04 The Gates Rubber Company Hose
FR2669342A1 (en) * 1990-11-20 1992-05-22 Inst Francais Du Petrole Composition of heat-curable resins which are employed in the manufacture of syntactic foams
GB2299975A (en) * 1995-04-18 1996-10-23 Kvaerner Earl & Wright Removable Buoyancy

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2002095278A1 (en) * 2001-05-18 2002-11-28 Crp Group Limited Protection of underwater elongate members
WO2006076486A2 (en) 2005-01-14 2006-07-20 Shell Internationale Research Maatschappij B.V. System and methods to install subsea structures
US7195530B2 (en) 2005-01-14 2007-03-27 Shell Oil Company System and methods to install subsea structures
EP1942051A2 (en) 2007-01-02 2008-07-09 In novo d.o.o. Depth buoy for maritime applications and process for making it
US10030094B2 (en) 2008-07-10 2018-07-24 Huntsman International Llc Polyisocyanurate-based syntactic coating for offshore applications
CN104494797A (en) * 2014-11-25 2015-04-08 苏州九鼎珍珠棉有限公司 Buoyancy stick based on foam materials
WO2019077370A1 (en) * 2017-10-20 2019-04-25 Balmoral Comtec Limited A cylindrical element profiled to reduce vortex induced vibration (viv) and/or drag
US10962035B2 (en) 2017-10-20 2021-03-30 Balmoral Comtec Limited Cylindrical element profiled to reduce vortex induced vibration (VIV) and/or drag
WO2020194064A2 (en) 2019-03-25 2020-10-01 Acergy France SAS Pressure-resistant buoys
CN112936915A (en) * 2021-04-13 2021-06-11 中国铁塔股份有限公司黑龙江省分公司 Reinforced composite material processing system
CN112936915B (en) * 2021-04-13 2021-09-03 中国铁塔股份有限公司黑龙江省分公司 Reinforced composite material processing system

Also Published As

Publication number Publication date
AU5232300A (en) 2000-12-28

Similar Documents

Publication Publication Date Title
US6663453B2 (en) Buoyancy control systems for tubes
RU2679689C1 (en) High-pressure composite vessel and method of manufacturing high-pressure composite vessel
US10228083B2 (en) Flexible pipe including thermal insulation
US5795102A (en) Marine and submarine apparatus
JP2722237B2 (en) Tubular body containing composite layers with different elastic moduli
JP2805327B2 (en) FIBER REINFORCED COMPOSITE RESIN BAR AND MANUFACTURING METHOD THEREOF
CA2651578C (en) Improvements relating to hose
EP2513540B1 (en) Flexible pipe including carcass layer
US5830400A (en) Method of manufacturing a hollow structure for storing pressurized fluids
MXPA05011885A (en) Load-bearing, lightweight, and compact insulation system.
WO2002075203A1 (en) Insulating cladding, method of using same on elongate member of a pipe
WO2000075546A1 (en) Buoyant composite material
EP2079573B1 (en) Reinforced composite polyethylene pipe and a method of manufacturing same
BR122019018157B1 (en) FLEXIBLE TUBE BODY, FLEXIBLE AND JUMPER TUBE, ASCENDING TUBE (RISER) OR FLOWLINE (FLOWLINE), METHOD OF MANUFACTURING THE REFERRED FLEXIBLE TUBE BODY, METHOD TO PREVENT OR DELAY SUBMINE FLUIN REFRIGERATION TUBE
WO1993012370A2 (en) Improvements relating to pipeline insulation and anticorrosion protection
EP0521582A1 (en) Insulated flowline system
GB2350819A (en) Composite buoyant material for forming floats
CA2141808C (en) Improvements in marine and submarine apparatus
US20080233332A1 (en) Thermal Insulation Material
US20130251957A1 (en) Ultra low density syntactic foam buoyancy module
AU2014274507B2 (en) Flexible pipe including thermal insulation
CA1326215C (en) Insulated pipe apparatus
KR20110112815A (en) Heat accumulator

Legal Events

Date Code Title Description
AK Designated states

Kind code of ref document: A1

Designated state(s): AE AG AL AM AT AU AZ BA BB BG BR BY CA CH CN CR CU CZ DE DK DM DZ EE ES FI GB GD GE GH GM HR HU ID IL IN IS JP KE KG KP KR KZ LC LK LR LS LT LU LV MA MD MG MK MN MW MX MZ NO NZ PL PT RO RU SD SE SG SI SK SL TJ TM TR TT TZ UA UG US UZ VN YU ZA ZW

AL Designated countries for regional patents

Kind code of ref document: A1

Designated state(s): GH GM KE LS MW MZ SD SL SZ TZ UG ZW AM AZ BY KG KZ MD RU TJ TM AT BE CH CY DE DK ES FI FR GB GR IE IT LU MC NL PT SE BF BJ CF CG CI CM GA GN GW ML MR NE SN TD TG

121 Ep: the epo has been informed by wipo that ep was designated in this application
DFPE Request for preliminary examination filed prior to expiration of 19th month from priority date (pct application filed before 20040101)
REG Reference to national code

Ref country code: DE

Ref legal event code: 8642

122 Ep: pct application non-entry in european phase
NENP Non-entry into the national phase

Ref country code: JP