This application is a nationalization of and claims priority to PCT/GB2018/053038, filed on Oct. 19, 2018, which claims priority to GB1811787.9, filed Jul. 19, 2018, and GB1717308.9, filed Oct. 20, 2017, the disclosures of each of which are hereby incorporated by reference in their entirety.
The present invention is related to preventing Vortex Induced Vibration (VIV)—and reducing drag occurring on substantially cylindrical objects when they are positioned within a body of water and/or are operating within a water current flow such as in an offshore environment. Such cylindrical objects are typically:
In fluid dynamics, vortex-induced vibrations (VIV) are motions induced on bodies interacting with an external fluid flow, produced by—or the motion producing—periodical irregularities on this flow.
A classic example is the VIV of an underwater cylinder. A skilled person can very simply observe how this happens in basic terms by putting a cylinder into the water (such as water held in a swimming-pool or even a bucket) and moving it through the water in the direction perpendicular to its axis. Since real fluids always present some viscosity, the flow around the cylinder will be slowed down while in contact with its surface, forming the so-called boundary layer. At some point however, this boundary layer can separate from the body because of its excessive curvature. Vortices are then formed changing the pressure distribution along the surface. When the vortices are not formed symmetrically around the body (with respect to its mid-plane), different lift forces develop on each side of the body, thus leading to motion transverse to the flow. This motion changes the nature of the vortex formation in such a way as to lead to a limited motion amplitude (differently than from what would be expected in a typical case of resonance).
It is therefore important to reduce or minimise VIV on cylindrical objects when they are positioned within and operating in the water column typically between and possibly from the water surface to the seabed within a water current flow such as in an offshore environment.
Conventionally, it is known to attempt to reduce VIV in a number of ways. For example, Matrix Composites and Engineering of Henderson, Wash., 6166, Australia produce the MATRIX LGS™ system (which is described in PCT Patent Publication No WO2016/205900) and which comprises a cylindrical element placed around a cylindrical structure deployed in a body of water (such as a marine riser, umbilical, cable or pipeline) where the cylindrical element comprises a plurality of longitudinally extending raised body portions which are adapted to reduce VIV.
Also, Trelleborg of Houston, Tex. 77073, USA jointly with Diamond Offshore Drilling, Inc. of Houston, Tex. 77094-1810, USA produce a Helical Buoyancy system which is arranged to be placed around a cylindrical structure deployed in a body of water which requires buoyancy support (such as Marine Drilling Risers, Intervention Risers, Jumpers, Long Pipeline Spans, Production Risers, Umbilicals, Flow Lines and Power Cables) where the Helical Buoyancy system comprises a cylinder made up of two half shells formed from buoyant material and where the cylinder is placed around the structure to be supported in the body of water and where the cylinder comprises helical grooves formed on its outer surface along its length. Further details of the Helical Buoyancy System may be viewed in U.S. Pat. Nos. 8,443,896 B2 and 9,322,221 B2.
According to the present invention, there is provided a generally cylindrical element adapted for immersion in a body of water, the generally cylindrical element having an outer surface arranged, in use, to be in contact with the water, the outer surface comprising:—
Preferably, each of the repeating shapes within each row is identical. This has the advantage of maximising the number of shapes within each row.
Preferably, each row provided on the outer surface comprises identical repeating shapes to the shapes of each other row, such that all of the shapes provided on the outer surface are identical.
The shapes may be triangles, squares, rectangles or pentagons but most preferably the shapes are hexagonal. This provides the advantage of maximising the total number of shapes for a given surface area provided on the outer surface. Most preferably, the said given surface area comprises a hexagonal tessellation. This provides the further advantage that the hexagonal patterns produce a more favourable flow pattern which improves the VIV suppression efficiency; there are several reasons for this but one of the main or most important reasons is that the hexagonal patterns and surrounding groove arrangement provide a plurality of flow separation points whilst minimising drag on the generally cylindrical element.
Preferably, the majority of the outer surface and more preferably the entire outer surface of the generally cylindrical element comprises a hexagonal tessellation in which each three adjacent hexagons meet at each adjoining vertex and the rest of the hexagons repeat that arrangement across the whole outer surface of the generally cylindrical element.
Typically, the vertex between two adjacent sides of each shape, preferably each hexagon shape, comprises a radius and preferably not a sharp corner and more preferably, each vertex between each adjacent pair of sides of each hexagon shape comprises a radius between 5 mm and 250 mm and more preferably said radius is between 150 mm and 250 mm.
Typically, the arrangement of hexagons comprises rows of hexagons stacked with respect to one another, each row being separated from the next upper or lower row by an arrangement of grooves.
Additionally or alternatively, the arrangement of hexagons on the outer surface of the generally cylindrical element can be considered to be in the form of staggered columns equi-spaced around the circumference of the outer surface, where any one column closely fits with the next adjacent column (albeit which is staggered by half the height of a hexagon when compared with the first column) and so on for other columns circumscribing the generally cylindrical element.
The skilled person will understand that the outer surface having such a hexagonal tessellation provided thereon, where the hexagons project outwardly from the outer surface due to the groove arrangements, provide the great advantage of maximising the number of shapes within each row and/or column and/or over the whole of the outer surface and this therefore has the great advantage of providing the most efficient VIV and/or drag reduction possible to the generally cylindrical element.
Preferably, the generally cylindrical element is further adapted to be placed around a substantially cylindrical structure which in use is located in the body of water, where the cylindrical structure may be a riser, umbilical, jumper, long pipeline span, flow line, power cable or the like.
The generally cylindrical element may be a Distributed Buoyancy Module (DBM), Drill Riser Buoyancy (DRB) or may be in the form of a cylindrical shroud used as a VIV strake. When the cylindrical element is a Distributed Buoyancy Module (DBM) or a Drill Riser Buoyancy (DRB) it is typically provided in the form of multiple part shells such as two semi-circular shells or four quarter-circular shells which when brought together envelope the substantially cylindrical structure located in the body of water and which typically comprise buoyancy to aid floatation of the substantially cylindrical structure located in the body of water.
Typically, when the generally cylindrical element is a DRB, it further comprises stacking flats to permit individual shells to be stacked one on top of another.
Typically, when the generally cylindrical element is a DBM it further comprises strap and/or lifting holes to assist transportation of the DBM.
When the cylindrical element is in the form of a cylindrical shroud used as a VIV strake, it may be manufactured in halves (i.e. in two split semi-circumferential pieces of 180° each, which when brought together wrap around or envelop the cylindrical structure and form a generally cylindrical element). Alternatively, the cylindrical shroud may be manufactured in thirds (i.e. in three split circumferential pieces of 120° each, which when brought together wrap around the cylindrical structure and form a generally cylindrical element). Alternatively, when the cylindrical element is in the form of a cylindrical shroud used as a VIV strake, it may be C shaped in cross section and typically comprises a slit formed along the whole length at one side such that it can be slid over the entire length of the substantially cylindrical structure located in the body of water. When the cylindrical element is in the form of a cylindrical shroud used as a VIV strake, it typically comprises strap recesses and/or socket and spigot/bolt and nut arrangements on each end thereof and/or along the longitudinal length thereof (particularly when it is provided in a ⅓ or a half configuration as discussed above).
Alternatively, the generally cylindrical element may be formed integrally with the substantially cylindrical structure such as a subsea conduit, typically on the outer surface thereof. Optionally, the inner surface or throughbore of the generally cylindrical element is bonded directly to the outer surface of the subsea conduit. Optionally, a protective coating layer may be provided between the inner surface or throughbore of the generally cylindrical element and the outer surface of the subsea conduit typically in a co-axial manner and in this case, the protective coating layer is preferably bonded to the respective surface on each of its outer and inner surfaces.
Typically, ties or straps are provided to prevent the generally cylindrical element from accidental removal from around the substantially cylindrical structure located in the body of water.
Preferably, the said groove arrangements comprise a groove having a depth of profile=0.01 to 0.1 times the outer diameter (OD) of the generally cylindrical element and more preferably the said groove arrangements comprise a groove having a depth of profile=approximately 0.05 times the outer diameter (OD) of the generally cylindrical element.
Preferably, the said groove arrangements comprise a groove having a width of profile=0.04 to 0.3 times the outer diameter (OD) of the generally cylindrical element. More preferably the said groove arrangements comprise a groove having a width of profile=0.25 to 0.3 times the outer diameter (OD) of the generally cylindrical element.
The groove arrangement may comprise a groove having a square or rectangular shape.
The groove arrangement may more preferably comprise angled side faces which may be angled between 40 to 80 degrees to the radius of the generally cylindrical element. In this case, the angled side faces of the groove arrangement may be angled in the region of 60 degrees to the radius of the generally cylindrical element.
Alternatively, the profile of the groove arrangement may be a full round (i.e. semi-circular) where the diameter of the cut can be=0.03 to 0.15 times the outer diameter (OD) of the generally cylindrical element. More preferably the said groove arrangements comprise a groove having a diameter of the cut=0.07 to 0.09 times the outer diameter (OD) of the generally cylindrical element.
Typically, the groove arrangement for each row of shapes comprises an upper groove and a lower groove, where each of the upper and lower grooves encircles the full 360-degree circumference of the generally cylindrical element at that longitudinal cross section such that each of said grooves is continuous around the 360 degrees of the generally cylindrical element (i.e. it has no separate start or end point). This has the significant advantage over conventional helical grooves that the groove arrangements of the present invention do not require to be cut as deep as conventional helical grooves because they provide a much greater coverage of grooves than conventional helical grooves. Additionally, because there is no separate start or end point for the grooves, they provide a much smoother exit point for water leaving contact with the groove arrangement and thus the outer surface of the generally cylindrical element.
The said shapes may comprise corners with radius edges which may range from 5 mm-250 mm and more preferably in the range of 50 mm to 70 mm.
Preferably the groove arrangement provides at least one and preferably a plurality of separated paths to flow of water when navigating around the circumference of the generally cylindrical element such that water flowing around the outside circumference of the generally cylindrical element from one side to another (which would occur when the generally cylindrical element were substantially vertical within a body of water which is flowing past that generally cylindrical element) meets a number of flow separation points. Preferably, said flow separation points comprise corner points of the hexagon shapes, or alternatively the flow separation points may comprise a side portion of the hexagon shapes. Typically, water flowing along the flow path within the groove arrangement from one side of the generally cylindrical element to another will meet a flow separation point at which point it will be separated into a first flow path and a second flow path. Preferably, there are a number of flow separation points provided around the outer surface of the generally cylindrical element and which are preferably encountered by water flowing around 180 degrees of the generally cylindrical element. This flow separation characteristic, particularly provided by the arrangement of shapes being staggered when viewed along each row and/or along each column of hexagonal shapes provides significantly greater flow separation, which in turn greatly reduces the VIV, and this provides significant technical advantages to embodiments of the present invention. Preferably, the point of flow separation comprises a corner of a shape and optionally the point of flow separation is less than 90 degrees such that the water flowing in the groove arrangement is forced to change direction by less than 90 degrees in order to keep the coefficient of drag of the generally cylindrical element as low as possible. Optionally the point of flow separation may be 60 degrees such that the water flowing in the groove arrangement is forced to change direction by 60 degrees no matter which of the two paths the water takes around the hexagon shape and thus the coefficient of drag of the generally cylindrical element is kept as low as possible.
Preferably, the depth of the repeating shapes is substantially equal to the Radius of the corner at the edge of each shape.
Optionally, the width of the groove in the circumferential direction is substantially equal to the outermost radius of the element multiplied by 0.50 to 0.60. Further optionally, the width of groove in the diagonal direction is substantially equal to the outermost radius of the element multiplied by 0.55 to 0.60.
Preferably, the repeating shape angle comprises an equal sided and uniformly shaped hexagon, having the enclosed angle of each corner fixed at 120 degrees.
Preferably, the shape pattern comprises multiple rows of 3 fixed 120° enclosed angle hexagons equi-spaced per row around the circumference of the generally cylindrical element, optionally with the adjacent row comprising 3 similarly shaped hexagons but offset by half a pitch out of phase (i.e. 60°).
The accompanying drawings illustrate presently exemplary embodiments of the disclosure and together with the general description given above and the detailed description of the embodiments given below, serve to explain, by way of example, the principles of the disclosure.
In the description that follows, like parts are marked throughout the specification and drawings with the same reference numerals, respectively. The drawings are not necessarily to scale. Certain features of the invention may be shown exaggerated in scale or in somewhat schematic form and some details of conventional elements may not be shown in the interest of clarity and conciseness. The present invention is susceptible to embodiments of different forms. Specific embodiments of the present invention are shown in the drawings and herein will be described in detail, with the understanding that the present disclosure is to be considered an exemplification of the principles of the invention and is not intended to limit the invention to that illustrated and described herein. It is to be fully recognized that the different teachings of the embodiments discussed below may be employed separately or in any suitable combination to produce the desired results.
The various aspects of the present invention can be practiced alone or in combination with one or more of the other aspects, as will be appreciated by those skilled in the relevant arts. The various aspects of the invention can optionally be provided in combination with one or more of the optional features of the other aspects of the invention. Also, optional features described in relation to one embodiment can typically be combined alone or together with other features in different embodiments of the invention. Additionally, any feature disclosed in the specification can be combined alone or collectively with other features in the specification to form an invention.
Various embodiments and aspects of the invention will now be described in detail with reference to the accompanying figures. Still other aspects, features and advantages of the present invention are readily apparent from the entire description thereof, including the figures, which illustrates a number of exemplary embodiments and aspects and implementations. The invention is also capable of other and different embodiments and aspects, and its several details can be modified in various respects, all without departing from the scope of the present invention.
Any discussion of documents, acts, materials, devices, articles and the like is included in the specification solely for the purpose of providing a context for the present invention. It is not suggested or represented that any or all of these matters formed part of the prior art base or were common general knowledge in the field relevant to the present invention.
Accordingly, the drawings and descriptions are to be regarded as illustrative in nature and not as restrictive. Furthermore, the terminology and phraseology used herein is solely used for descriptive purposes and should not be construed as limiting in scope. Language such as “including”, “comprising”, “having”, “containing” or “involving” and variations thereof, is intended to be broad and encompass the subject matter listed thereafter, equivalents and additional subject matter not recited, and is not intended to exclude other additives, components, integers or steps. In this disclosure, whenever a composition, an element or a group of elements is preceded with the transitional phrase “comprising”, it is understood that we also contemplate the same composition, element or group of elements with transitional phrases “consisting essentially of”, “consisting”, “selected from the group of consisting of”, “including” or “is” preceding the recitation of the composition, element or group of elements and vice versa. In this disclosure, the words “typically” or “optionally” are to be understood as being intended to indicate optional or non-essential features of the invention which are present in certain examples but which can be omitted in others without departing from the scope of the invention.
All numerical values in this disclosure are understood as being modified by “about”. All singular forms of elements, or any other components described herein including (without limitations) components of the apparatus described herein are understood to include plural forms thereof and vice versa.
Embodiments of the present invention will now be described, by way of example only, with reference to the accompanying drawings, in which:—
In certain embodiments of the present invention, the generally cylindrical element 10 may be the actual (i.e. integral) outer surface of a substantially cylindrical structure (not shown) which in use is located in the body of water, where the substantially cylindrical structure may be a riser (not shown), umbilical, jumper, long pipeline span, flow line, power cable or the like. Alternatively and more preferably, the substantially cylindrical element 10 is a separate substantially tubular component to the said substantially cylindrical structure (not shown), wherein in use the substantially cylindrical element 10 is adapted to be placed around the said generally cylindrical structure such that the generally cylindrical structure is located within the throughbore 15 of the generally cylindrical element 10 such that the generally cylindrical element 10 envelops the section of the said generally cylindrical structure located within it and therefore acts like a sleeve to the generally cylindrical structure located within it.
Importantly, in all embodiments, the generally cylindrical element 10 is provided with an arrangement or pattern of repeating shapes 20 on its outer surface 11, as will be described in more detail subsequently and which acts to reduce the Vortex Induced Vibration (VIV) and/or drag acting upon the generally cylindrical element 10 (and therefore acts to reduce the VIV and/or drag on any substantially cylindrical structure located within the throughbore 15 of the generally cylindrical element 10).
The skilled person will understand that the combination of the shapes 20 and the arrangement of grooves 30 provided around the shapes 20 alter the way in which vortices (not shown) are formed as compared to a cylindrical structure that has a uniform (flat) outer surface 11. The skilled person will also realise that by providing the generally cylindrical element 10 having the said outer surface 11 will mean that additional (conventional) VIV strakes which would normally additionally be provided around some cylindrical structures or tubulars used subsea will not be required because the generally cylindrical element 10 will provide sufficient and possibly more than sufficient reduction of VIV and/or drag.
As shown in
In the embodiment as shown in
The skilled person should note that it is preferred that each vertex 22 between two adjacent sides of each hexagon shape 20 comprises a radius and not a sharp corner and more preferably, each vertex 22 between each adjacent pair of sides of each hexagon shape 20 comprises a radius between 5 mm and 250 mm and more preferably said radius is between 150 mm and 250 mm.
In the embodiment of the generally cylindrical element 10 as shown in
Additionally, the arrangement of hexagons 20 on the outer surface 11 of the generally cylindrical element 10 can be considered to be in the form of staggered columns 50 equi-spaced around the circumference of the outer surface 11, where the first column 50A shown in
The skilled person will understand that the outer surface 11 having such a hexagonal tessellation 21 provided on itself, where the hexagons 20 project outwardly from the outer surface 11 due to the groove arrangements 30, provide the great advantage of maximising the number of shapes 20 within each row 40 and/or column 50 and/or over the whole surface of the outer surface 11 and this therefore has the great advantage of providing the most efficient VIV and/or drag reduction possible to the generally cylindrical element 10.
The shapes 20 and the groove arrangements 30 may be formed on the outer surface 11 of the generally cylindrical element 10 by any suitable means such as moulding the generally cylindrical element 10 as an integral one-piece component with the groove arrangement 30 and hexagonal tessellation 21 provided thereon (and such a moulding operation could be a pumped, injected or roto-moulded operation). Alternatively, the generally cylindrical element 10 may start out as a homogeneous tubular and the groove arrangements 30 may be cut into the outer surface of the homogeneous tubular (not shown) in order to form the arrangement of shapes 20 and in particular the preferred arrangement of the hexagonal tessellation 21 provided on the outer surface 11. Other suitable manufacturing techniques could also be used. A less preferred manufacturing technique is having a homogeneous tubular and fixing by some suitable fixing means such as adhesive or screws etc. the shapes 20 to the outer surface 11 of the homogeneous tubular (not shown) in such a hexagonal tessellation 21 arrangement such that the groove arrangements 30 are provided by the resulting gaps or channels between the various fixed shapes 20.
The hexagonal tessellation 21 is very efficient at reducing the VIV and indeed it is designed to reduce the VIV by a minimum of 80% and also reduce the drag below 1.2 for Reynolds numbers ranging from 1.4e5 to 4.2e6.
The dimensions of the groove arrangements 30 are as follows:—
The skilled person will therefore understand that the hexagonal tessellation 21 (and therefore each row 40 and/or each column 50 within the hexagonal tessellation 21) encircles the full 360-degree circumference of the generally cylindrical element 10 and will further understand that each groove 30 at the upper and lower sides of each row 40 is continuous around the 360 degrees of the outer surface 11 such that it has no separate start or end point. This provides significant advantages in terms of VIV reduction and/or drag reduction because the groove arrangement 30 provides a much smoother exit point for water leaving contact with the outer surface 11 (when compared to a completely “smooth” outer surface).
The skilled person will also realise that, whilst the hexagonal tessellation 21 is the most preferred shape profile provided on the outer surface 11, other less preferred shapes 20 could also be used such as triangles, square, rectangles, pentagons or other suitable shapes. The more preferred suitable shapes are shapes having symmetry (and which are therefore capable of being closely fit together in a tessellation). It is also preferred that all of the shapes 20 within the tessellation 21 are identical to one another in order to increase the number of shapes 20 that can be fit or provided on the outer surface 11 and therefore whilst different shapes could be provided within separate rows 40, it is preferred that all of the shapes 20 within a tessellation are identical and it is most preferred that all of the shapes are hexagons 20 and therefore the tessellation is a hexagonal tessellation 21. It is further preferred that the groove arrangement 30 provides at least one and preferably a plurality of separated paths to flow of water when navigating around the circumference of the generally cylindrical element 10 such that water following around the outside circumference of the generally cylindrical element 10 from one side to another (which would occur when the generally cylindrical element 10 were substantially vertical within a body of water which is flowing past that generally cylindrical element 10) meets a number of flow separation points 23 in the form of the corner points 23 of the hexagon shapes 20. For example, water flowing along the flow path 25A within the groove arrangement 20 from left to right in
The generally cylindrical element 10 and the shapes 20 provided thereon are formed from any suitable material and the suitable material may be a material which is buoyant within water.
Alternative configurations of the surface tessellation are shown in
a show cylindrical element 210 having an outer surface 211 that comprises repeating hexagonal shapes 220, elongated along an axis that is offset from the longitudinal and the transverse axes of the element 210, with rounded points. Between the shapes 220 are grooves 230. The cylindrical element 210 has an upper end 212U and a lower end 212L as before. Water flowing around element 210 within the grooves 230 meets with at least one vertex 223 of the hexagonal shapes 220 and splits along different flow paths. Compared to the configuration of grooves 30 and shapes 20 illustrated in
b show cylindrical element 310 again having an outer surface 311 comprising elongated hexagonal repeating shapes 320 with rounded points, but the shapes 320 in this example are less elongated than those in
c show cylindrical element 410 having an outer surface 411 with repeating hexagonal shapes 420. The shapes 420 are again elongated along an axis that is offset from the longitudinal and transverse axes of the cylindrical element 410. However, in this example, the shapes 420 are elongated to a lesser degree than those shown in
d show cylindrical element 510 having an outer surface 511 comprising hexagonal shapes 520 in a repeating pattern across the surface 511. Grooves 530 space the shapes 520 from one another. In this example, the grooves 530 are wider than the grooves 30 shown in
e show cylindrical element 610 having an outer surface 611 comprising hexagonal shapes 620 that have been elongated along the longitudinal axis of the cylindrical element. The shapes 620 are arranged in a repeating pattern across the surface 611. Similarly, to
f show cylindrical element 710 having an outer surface 711 comprising hexagonal shapes 720 in a repeating patter across the surface 711. Grooves 730 space the shapes 720 from each other. The shapes 720 are elongated along the longitudinal axis of the cylindrical element 710 and relatively densely packed in comparison to the shapes 520, 620 illustrated in
The skilled person will understand that the various dimensions are liable to vary as per requirements of the particular application of use and will particularly vary dependent upon the inner radius 5201R of the cylindrical element 510 in question, but the various dimensions (e.g. the GDepth 520D, the Radius 520R, GCircumferential 530C and the GDiagonal 530D) are all preferably a relatively fixed ratio of the Inner Radius 5201R, as will be subsequently described in more detail. Simply put though, the greater the Inner Radius 5201R of the cylindrical element 510 in question, the greater the GDepth 520D but the relative proportions between the two are preferably substantially constant because the relative dimensions share come common feature ratios as will now be described. In all examples shown in
There are three main fields of application for the generally cylindrical element 10, these being:
Distributed Buoyancy Modules (DBM) 62—as Shown in
DBM's 62 are typically used at selected points on the outside of a conduit 64 such as a riser 64 which extends in a body of water between a surface vessel (not shown) or platform and a subsea structure (not shown), where the function of the DBM 62 is to provide the conduit 64 with buoyancy at a required location (for example to enable the conduit 64 to be installed in a “lazy wave” or “lazy S” configuration). The generally cylindrical element 10 may be secured by any suitable means such as clamping or straps to the outside of the DBM 62 but more preferably, the generally cylindrical element 10 is fully integral with the DBM 62 such that the outer surface 11 of the element 10 is the (integral) outer surface 11 of the DBM 62 and in this scenario, the DBM 62 is not an integral cylinder but instead is provided in the form of two half shells 62U; 62L which, when brought together, form a cylinder or sleeve around the outer surface of riser 64. The majority or all of the DBM 62 is formed from a buoyancy material). The generally cylindrical element in the form of the DBM 62 is provided with suitable strap recesses 66 and lifting holes 68 to facilitate transportation, installation and securing of the generally cylindrical element in the form of the DBM 62.
Drill Riser Buoyancy (DRB) 70—as Shown in
DRB modules 70 are typically fitted along the whole length of a riser 71 (which typically have an arrangement of conductors 72 provided around their outer circumference along their length—five are shown in
Cylindrical Shrouds Traditionally Used as VIV Strakes—First Embodiment Based Upon
Certain underwater conduit such as cables, flow lines, pipes and pipelines can conventionally be provided with subsea VIV suppression strakes which typically comprise radially extending helically arranged fins which act to reduce the VIV. Instead of providing such conventional fins, the generally cylindrical element 10 having the outer surface 11 as shown in
Cylindrical Shrouds Traditionally Used as VIV Strakes—Second Embodiment as Shown in
In an alternative embodiment to the C-shaped generally cylindrical element 10 of
The generally cylindrical element 100A of
The two part or pair of semi-circular shells 102a, 102b are typically formed of a relatively lightweight, relatively strong and non-brittle material such as polyurethane (PU) or the like. Additionally, buoyant material such as polystyrene (not shown) or other suitable material may be added to the inner surface of the throughbore of the generally cylindrical element 100A (such that the buoyancy material is in the annulus between the inner throughbore of the generally cylindrical element 100A and the outer surface of the conduit 110) if the operator requires to add buoyancy to the conduit 110.
Additional generally cylindrical elements 1008 identical to the first generally cylindrical element 100A can be provided adjacent each end of the first generally cylindrical element 100A and so on until the whole length or a sufficient length of the conduit 110 is entirely enveloped by the generally cylindrical element 100A; 1008 of
Each generally cylindrical element 100 is provided with a suitably shaped co-operating or mating surface provided on an outer end surface 109 at one end (which may be e.g. a lower in use end) and on an inner end surface 108 (which may be in use an uppermost end) at the other end. The mating surfaces may be suitably shaped co-operating surfaces such as radially acting tongue and groove arrangements or the like. During installation around the conduit 110, the second generally cylindrical element 1008 is placed around the conduit 110, with its upper end 108 having the inner mating surface lying in an overlapping manner with respect to the outer mating surface 109 of the lower most end of the first generally cylindrical element 100A, such that the respective radially acting tongue and groove arrangements mate with one another. This installation method is repeated down the length of the conduit 110 requiring VIV suppression by the generally cylindrical elements 100 and the respective radially acting tongue and groove arrangements prevent axial separation of adjacent generally cylindrical elements 100A; 1008.
Cylindrical Shrouds Traditionally Used as VIV Strakes—Third Embodiment as Shown in
However, the generally cylindrical element 120 of
In all other respects (including having an outer end surface 129 similar to the outer end surface 109 of
Cylindrical Shrouds Traditionally Used as VIV Strakes—Fourth Embodiment as Shown in
The generally cylindrical element 140 of
However, each of the two half shells 142 of the generally cylindrical element 140 of
This embodiment of generally cylindrical element 140 of
An operator will typically be able to retrofit the generally cylindrical element 140 of
This embodiment of generally cylindrical element 140 of
The generally cylindrical element 140 of
Any one of the embodiments 100, 120, 140 of generally cylindrical element could be picked by an operator to replace the existing subsea conduit protection system/buoyancy system as appropriate.
Cylindrical Shrouds Traditionally Used as VIV Strakes—Fifth Embodiment as Shown in
In a yet further alternative embodiment to the C-shaped generally cylindrical element 10 of
The generally cylindrical element 160 of
The inner surface 163 of the generally cylindrical element 160 of
The generally cylindrical element 160 of
Other applications of embodiments in accordance with the present invention are possible, where VIV reduction and/or drag reduction particularly within subsea environments is required, without departing from the scope of the invention.
Modifications and improvements may be made to the embodiments hereinbefore described without departing from the scope of the invention.
Number | Date | Country | Kind |
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1717308 | Oct 2017 | GB | national |
1811787 | Jul 2018 | GB | national |
Filing Document | Filing Date | Country | Kind |
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PCT/GB2018/053038 | 10/19/2018 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
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WO2019/077370 | 4/25/2019 | WO | A |
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Number | Date | Country | |
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20200248731 A1 | Aug 2020 | US |