US20070104542A1 - Fairing for a riser - Google Patents
Fairing for a riser Download PDFInfo
- Publication number
- US20070104542A1 US20070104542A1 US10/568,710 US56871004A US2007104542A1 US 20070104542 A1 US20070104542 A1 US 20070104542A1 US 56871004 A US56871004 A US 56871004A US 2007104542 A1 US2007104542 A1 US 2007104542A1
- Authority
- US
- United States
- Prior art keywords
- fairing
- cylindrical member
- collar
- riser
- fairing body
- 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.)
- Abandoned
Links
- 239000004033 plastic Substances 0.000 claims description 14
- 229920003023 plastic Polymers 0.000 claims description 14
- 239000000463 material Substances 0.000 claims description 12
- 238000000465 moulding Methods 0.000 claims description 9
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- 230000001050 lubricating effect Effects 0.000 claims description 4
- 239000002519 antifouling agent Substances 0.000 claims description 3
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- 230000003373 anti-fouling effect Effects 0.000 description 2
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- JPVYNHNXODAKFH-UHFFFAOYSA-N Cu2+ Chemical compound [Cu+2] JPVYNHNXODAKFH-UHFFFAOYSA-N 0.000 description 1
- 239000004677 Nylon Substances 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- 230000003466 anti-cipated effect Effects 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000003115 biocidal effect Effects 0.000 description 1
- 229910001431 copper ion Inorganic materials 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000002939 deleterious effect Effects 0.000 description 1
- 238000000605 extraction Methods 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 238000010348 incorporation Methods 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
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- 230000001681 protective effect Effects 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B21/00—Tying-up; Shifting, towing, or pushing equipment; Anchoring
- B63B21/56—Towing or pushing equipment
- B63B21/66—Equipment specially adapted for towing underwater objects or vessels, e.g. fairings for tow-cables
- B63B21/663—Fairings
-
- E—FIXED CONSTRUCTIONS
- E21—EARTH OR ROCK DRILLING; MINING
- E21B—EARTH OR ROCK DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
- E21B17/00—Drilling rods or pipes; Flexible drill strings; Kellies; Drill collars; Sucker rods; Cables; Casings; Tubings
- E21B17/01—Risers
-
- E—FIXED CONSTRUCTIONS
- E21—EARTH OR ROCK DRILLING; MINING
- E21B—EARTH OR ROCK DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
- E21B17/00—Drilling rods or pipes; Flexible drill strings; Kellies; Drill collars; Sucker rods; Cables; Casings; Tubings
- E21B17/01—Risers
- E21B17/012—Risers with buoyancy elements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15D—FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
- F15D1/00—Influencing flow of fluids
- F15D1/10—Influencing flow of fluids around bodies of solid material
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15D—FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
- F15D1/00—Influencing flow of fluids
- F15D1/10—Influencing flow of fluids around bodies of solid material
- F15D1/12—Influencing flow of fluids around bodies of solid material by influencing the boundary layer
-
- 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
- F16L1/00—Laying or reclaiming pipes; Repairing or joining pipes on or under water
- F16L1/12—Laying or reclaiming pipes on or under water
- F16L1/123—Devices for the protection of pipes under water
Definitions
- the present invention relates to a fairing for mounting upon a cylindrical underwater member such as a marine riser.
- the present invention has been developed for use in connection with marine risers used in offshore oil extraction, although it has potential applications in other situations in which a submersed, cylindrical member is exposed to water flow and must be protected from the effects thereof.
- VIV vortex induced vibration
- GB 1193750 describes a fairing device for a cable towed behind a ship.
- a “D” shaped channel to receive a cable 7 is formed along most of the length of the fairing between a flat front face of a body part and a “u” shaped metal strap bolted to it, so that the fairing surrounds and covers the cable.
- U.S. Pat. No. 5,722,340 discloses a fairing formed from two identical halves which are assembled together with a riser to form a teardrop shape surrounding and containing the riser.
- U.S. Pat. No. 4,078,605 depicts a fairing of teardrop shape having end walls with through-going openings to receive a riser. These openings are set well backward of the fairing's leading edge.
- U.S. Pat. No. 4,398,487 (Ortloff) concerns a fairing which defines an internal channel to receive a riser and has a relatively elaborate spring-loaded bearing arrangement through which it engages with the riser.
- U.S. Pat. No. 4474129 discloses a riser pipe fairing which splits into two halves along its plane of symmetry, the two halves being assembled around the riser during deployment and riding upon bearing assemblies formed as circular loops, which are slipped through slots in the fairing halves allowing the fairing to rotate relative to the bearing assemblies.
- the fairing disclosed in U.S. Pat. No. 6,067,922 is not a teardrop shape, but has a generally tubular portion with a planar flange projecting from it.
- the tube can be opened out to allow it to be placed around a riser and bolts through two halves of the flange secure it in position.
- GB 2334733 (Reading and Bates Development Co) discloses a fairing whose leading edge is formed by shaped “doors” having part-cylindrical portions which can be opened out to receive a riser and then closed around it to form a roughly cylindrical surrounding the riser.
- the present invention is intended to provide a novel and improved solution to the technical challenges.
- a fairing for mounting upon a cylindrical member for underwater deployment, the fairing comprising a fairing body which, viewed along its length, is substantially wedge-shaped, having a relatively broad front tapering to a relatively narrow trailing edge, and at least two collars which are both secured to the fairing body and are separated from each other along the length of the fairing body, the collars being positioned and aligned to receive the cylindrical member with the fairing body's front lying adjacent the cylindrical member and the axis of the cylindrical member lying along the length of the fairing body, thereby to pivotally mount the fairing body upon the cylindrical member such that it is able to rotate about the axis of the cylindrical member and so align itself with a water current, the fairing body and the cylindrical member together defining, when viewed along the length of the fairing, a teardrop shape having a leading edge formed, between the collars, by the cylindrical member.
- each collar is interposed between the firing body and the cylindrical member in use, providing clearance therebetween.
- Each collar is preferably shaped to form a respective bearing ring for receiving the cylindrical member.
- Each bearing ring preferably has a substantially circular interior surface.
- the bearing ring is split such that it can be opened out to allow the cylindrical member to be inserted into it laterally.
- An end portion of the collar may be initially free to allow the bearing ring to be opened out, means being provided to subsequently secure the free end of the collar to the fairing body to retain the fairing upon the cylindrical member.
- the collar comprises two bifurcated portions, one limb of each extending between the cylindrical member and the fairing body to provide clearance therebetween and the other limb of each being secured in use to the fairing body.
- the front of the fairing body may be shaped to complement the cylindrical member, its surface(s) lying upon a notional cylinder.
- a bearing surface of the collar which faces toward the cylindrical member and upon which the collar rides, comprises low friction material.
- the surface may be self lubricating.
- the collar comprises a plastics material with an admixture of a friction reducing agent.
- the collar comprises self lubricating material.
- the collar preferably comprises a plastics material with an admixture of an anti-fouling agent.
- fairing body and the collar are formed by separate plastics mouldings.
- the fairing body is preferably formed as a hollow plastics moulding whose interior communicates with the exterior to permit equalisation of pressure.
- a fairing for mounting upon a cylindrical member for underwater deployment, the fairing comprising a substantially wedge shaped fairing body which tapers from a front face of the body to its trailing edge, and at least one collar coupled to the fairing body and arranged to receive the cylindrical member and to mount the fairing upon the cylindrical member with the fairing body's front face adjacent the cylindrical member, the collar permitting the fairing to rotate about the cylindrical member and so to align itself with a water current.
- FIG. 1 is a perspective illustration of an assembly comprising a first fairing embodying the present invention mounted upon a marine riser;
- FIG. 2 is a side elevation of the same assembly
- FIG. 3 is a section through the assembly at station A-A;
- FIG. 4 is a section through the assembly at station B-B;
- FIG. 5 is a perspective illustration of a collar forming part of the fairing
- FIG. 6 is a section in a longitudinal plane through an assembly comprising a clamp and a fairing both embodying aspects of the present invention mounted upon a marine riser;
- FIG. 7 is a section through the same assembly in a transverse plane.
- FIG. 8 is a perspective illustration of a stage in the manufacture of a fairing body embodying the present invention.
- the fairing 2 illustrated in FIGS. 1 to 5 comprises (a) a fairing body 4 and (b) a plurality of collars 6 serving to rotatably couple the fairing body 4 to a cylindrical marine riser 8 .
- the fairing body 4 can be seen to be generally wedge shaped. Its front, lying adjacent the riser 8 , has a lateral dimension similar to that of the riser. In the illustrated embodiment this dimension is slightly smaller than the riser diameter. Moving toward its rear the fairing body tapers to a narrow trailing edge 10 . This shape is defmed by convergent walls 9 , 9 1 , which meet at the trailing edge.
- the front face 12 of the fairing body is shaped to conform to the adjacent surface of the riser, being part cylindrical and concave. The cross section which the assembly of riser and fairing presents to a current of water is best appreciated from FIG.
- each collar comprises a bearing ring 16 which is split at 18 to allow the riser 8 to be introduced laterally into the bearing ring.
- the collar is formed of a resiliently deformable material so that the ring can be opened out—that is, ends of the ring on either side of the split 18 can be drawn apart—to allow the riser to be introduced. In the present embodiment this deformation of the collar is facilitated by a reduced thickness region 20 which serves as a resilient hinge.
- the collar has a bifurcated section.
- One limb 26 , 28 leading from each bifurcation forms part of the bearing loop and in use lies between the fairing body and the riser (see FIG. 4 ) while the other limb 30 , 32 extends in a direction generally parallel to an adjacent face 34 , 36 of the fairing body and forms a mounting tab through which the collar is mounted to the fairing body.
- the fairing body has shallow recesses or pockets in which the mounting tabs are received, so that the tabs' outer surfaces are generally flush with the adjacent faces 34 , 36 of the fairing body (see FIG. 3 ).
- Attachment of the tabs to the fairing body is achieved using mechanical fasteners received by through-holes 38 , 40 in the tabs which align with holes in the fairing body.
- the fasteners shown in the drawings are formed as nuts and bolts 42 . In order to resist corrosion and minimise weight these may be formed of plastics.
- the fairing may be supplied to the end user with the tabs on one face 34 pre-attached so that to mount the fairing the user first inserts the riser into the collars and then secures the relevant tabs to the other face 36 .
- the fairing body is formed by a single plastics moulding. More specifically the illustrated item is manufactured by the well known technique of rotational moulding, so that it is hollow. Polythene is the preferred material for this component, which is advantageous due to its low specific gravity (similar to that of water), toughness and low cost.
- An opening 44 allows water to enter the fairing body to equalise internal and external pressures.
- the body could instead be formed as a solid polyurethane moulding.
- the collars are each formed by a single plastics moulding but for these the favoured material is nylon, which again has a specific gravity similar to that of water.
- the internal face 44 of the collar's bearing ring 16 serves as one half of a rotary bearing allowing the fairing to rotate about the riser's longitudinal axis and so to weathervane to face a current. Only the collar makes contact with the riser, its portion interposed between the fairing body and the riser serving to maintain clearance between these parts.
- the present inventor has recognised that it is highly desirable for this bearing surface to be (a) low friction and even “self lubricating” and (b) resistant to marine fouling. These properties can be promoted by incorporation of anti-fouling and friction reducing materials into the material of the collar.
- the plastics material of the collar contains an admixture of an anti-fouling composition which provides a controlled rate of release of copper ions, whose biocidal properties are well known, and also of silicon oil serving to reduce bearing friction.
- the internal part of the bearing on which the fairing is mounted may be provided by the riser itself. That is, the fairing may be mounted directly upon the riser (or on a cylindrical protective sheath conventionally provided around the riser). A number of such fairings would normally be placed adjacent one another in a string along the riser. To prevent the fairings from moving along the length of the riser, clamps are secured to it at intervals (typically a string of perhaps five fairings would be confined between a pair of clamps).
- the clamps may be of a type well known in the context having a pair of half cylindrical clamp shells secured to the riser by a tension band passed around the shells.
- FIGS. 6 and 7 An alternative arrangement can be understood from FIGS. 6 and 7 in which a clamp formed by two half cylindrical clamp shells 50 , 52 is secured to the riser, again labelled 8 in this drawing, by a tension band 54 received in a shallow annular recess in the exterior of a central flange 56 formed by the clamp shells from either side of which project reduced diameter spigot portions 58 upon which the collars 60 , 62 of respective fairings, arranged on opposite sides of the clamp, ride.
- the drawing is simplified in that remaining parts of the two fairings are omitted (they can be taken to be similarly formed to those of the previous embodiment). While only a single clamp is shown in the drawing, it is to be understood that in this arrangement a clamp is provided between each adjacent pair of fairings, so that the fairings'rotary bearings are in each case formed by a collar riding upon the clamp.
- the front face 12 of the fairing body can be omitted and that drag can thereby be reduced.
- the front edges of the walls 9 , 9 1 of the fairing body form its front surface, and may be shaped to conform to the adjacent cylindrical surface of the riser.
- FIG. 8 there is a single hollow moulding 70 is in the shape of two fairing bodies placed nose-to-nose. By dividing the moulding in the plane 72 and suitably machining/dressing the cut edges, two bodies are formed. Rotational moulding of the structure 70 is favoured. Shallow recesses 74 . 76 will receive the mounting tabs 30 , 30 of the collars.
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- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- General Life Sciences & Earth Sciences (AREA)
- Environmental & Geological Engineering (AREA)
- Geochemistry & Mineralogy (AREA)
- General Engineering & Computer Science (AREA)
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Abstract
A fairing is disclosed for mounting upon a cylindrical member which is deployed underwater. The fairing has a generally wedge shaped body 4 which tapers from front to rear. The body 4 is mounted upon the cylindrical member 8 through a collar 6, 6 1 in which the member is received. The fairing is thus mounted with its front face adjacent the cylindrical member so that the assembly of the fairing body and the member can together form a teardrop shape. The collar permits the fairing to weathervane, rotating about the cylindrical member, to align itself with a current.
Description
- The present invention relates to a fairing for mounting upon a cylindrical underwater member such as a marine riser.
- In fact the present invention has been developed for use in connection with marine risers used in offshore oil extraction, although it has potential applications in other situations in which a submersed, cylindrical member is exposed to water flow and must be protected from the effects thereof.
- Water currents impinging on marine risers create two particular problems. Firstly they create drag, i.e. a lateral loading upon the riser, producing undesirable bending stresses and potentially also increasing loads at the riser's point of suspension. Secondly they can create so-called vortex induced vibration (VIV). Vortices are found to be shed alternately from opposite sides of the riser and the effect can be to produce vibration which is potentially damaging, particularly if resonance effects cause the vibration's amplitude to build up.
- It is known to address both problems by placing around the riser a streamlined, teardrop shaped fairing which is free to pivot about the riser's axis and so to “weathervane”—that is, to align itself with the direction of the current. Searches have brought to light several such fairings in the patent literature.
- GB 1193750 describes a fairing device for a cable towed behind a ship. A “D” shaped channel to receive a cable 7 is formed along most of the length of the fairing between a flat front face of a body part and a “u” shaped metal strap bolted to it, so that the fairing surrounds and covers the cable.
- U.S. Pat. No. 5,722,340 (Sweetman) discloses a fairing formed from two identical halves which are assembled together with a riser to form a teardrop shape surrounding and containing the riser.
- U.S. Pat. No. 4,078,605 (Jones) depicts a fairing of teardrop shape having end walls with through-going openings to receive a riser. These openings are set well backward of the fairing's leading edge.
- U.S. Pat. No. 4,398,487 (Ortloff) concerns a fairing which defines an internal channel to receive a riser and has a relatively elaborate spring-loaded bearing arrangement through which it engages with the riser.
- U.S. Pat. No. 4474129 (Watkins et al) discloses a riser pipe fairing which splits into two halves along its plane of symmetry, the two halves being assembled around the riser during deployment and riding upon bearing assemblies formed as circular loops, which are slipped through slots in the fairing halves allowing the fairing to rotate relative to the bearing assemblies.
- The fairing disclosed in U.S. Pat. No. 6,067,922 (Denison et al) is not a teardrop shape, but has a generally tubular portion with a planar flange projecting from it. The tube can be opened out to allow it to be placed around a riser and bolts through two halves of the flange secure it in position.
- U.S. Pat. No. 4,171,674 (Hale) is another document concerned with a fairing formed from two halves for assembly around the riser.
- GB 2334733 (Reading and Bates Development Co) discloses a fairing whose leading edge is formed by shaped “doors” having part-cylindrical portions which can be opened out to receive a riser and then closed around it to form a roughly cylindrical surrounding the riser.
- A successful fairing must address several technical challenges:
- i. It should be capable of being straightforwardly fitted to the riser;
- ii. It must be capable of surviving the marine environment and of functioning without causing unacceptable damage to the riser.
- iii. It must be capable of reliably weathervaning, since if the fairing becomes fixed in a position transverse to the flow then its effect on both drag and VIV may be positively deleterious;
- iv. It should preferably be capable of straightforward and economical manufacture; and
- v. It is preferable to minimise drag.
- Looking at the above described prior art. complexity of construction is considered to be a problem of several of the fairings, adding to the difficulty and expense of manufacture. It is also regarded as undesirable that all of these fairings, since they surround the riser, inevitably add somewhat to the frontal area presented to the flow. Increased frontal area creates increased drag. There are also concerns about difficulty of deployment of some of the fairings, particularly where this involves assembly of multiple parts.
- The present invention is intended to provide a novel and improved solution to the technical challenges.
- In accordance with a first aspect of the present invention there is a fairing for mounting upon a cylindrical member for underwater deployment, the fairing comprising a fairing body which, viewed along its length, is substantially wedge-shaped, having a relatively broad front tapering to a relatively narrow trailing edge, and at least two collars which are both secured to the fairing body and are separated from each other along the length of the fairing body, the collars being positioned and aligned to receive the cylindrical member with the fairing body's front lying adjacent the cylindrical member and the axis of the cylindrical member lying along the length of the fairing body, thereby to pivotally mount the fairing body upon the cylindrical member such that it is able to rotate about the axis of the cylindrical member and so align itself with a water current, the fairing body and the cylindrical member together defining, when viewed along the length of the fairing, a teardrop shape having a leading edge formed, between the collars, by the cylindrical member.
- Preferably a portion of each collar is interposed between the firing body and the cylindrical member in use, providing clearance therebetween.
- Each collar is preferably shaped to form a respective bearing ring for receiving the cylindrical member. Each bearing ring preferably has a substantially circular interior surface.
- However in a preferred embodiment the bearing ring is split such that it can be opened out to allow the cylindrical member to be inserted into it laterally.
- An end portion of the collar may be initially free to allow the bearing ring to be opened out, means being provided to subsequently secure the free end of the collar to the fairing body to retain the fairing upon the cylindrical member.
- In a particularly preferred construction the collar comprises two bifurcated portions, one limb of each extending between the cylindrical member and the fairing body to provide clearance therebetween and the other limb of each being secured in use to the fairing body.
- The front of the fairing body may be shaped to complement the cylindrical member, its surface(s) lying upon a notional cylinder.
- Preferably a bearing surface of the collar, which faces toward the cylindrical member and upon which the collar rides, comprises low friction material. The surface may be self lubricating. It is particularly preferred that the collar comprises a plastics material with an admixture of a friction reducing agent.
- Preferably the collar comprises self lubricating material. The collar preferably comprises a plastics material with an admixture of an anti-fouling agent.
- It is particularly preferred that the fairing body and the collar are formed by separate plastics mouldings.
- The fairing body is preferably formed as a hollow plastics moulding whose interior communicates with the exterior to permit equalisation of pressure.
- In accordance with a second aspect of the present invention there is a fairing for mounting upon a cylindrical member for underwater deployment, the fairing comprising a substantially wedge shaped fairing body which tapers from a front face of the body to its trailing edge, and at least one collar coupled to the fairing body and arranged to receive the cylindrical member and to mount the fairing upon the cylindrical member with the fairing body's front face adjacent the cylindrical member, the collar permitting the fairing to rotate about the cylindrical member and so to align itself with a water current.
- 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 is a perspective illustration of an assembly comprising a first fairing embodying the present invention mounted upon a marine riser; -
FIG. 2 is a side elevation of the same assembly -
FIG. 3 is a section through the assembly at station A-A; -
FIG. 4 is a section through the assembly at station B-B; -
FIG. 5 is a perspective illustration of a collar forming part of the fairing; -
FIG. 6 is a section in a longitudinal plane through an assembly comprising a clamp and a fairing both embodying aspects of the present invention mounted upon a marine riser; and -
FIG. 7 is a section through the same assembly in a transverse plane; and -
FIG. 8 is a perspective illustration of a stage in the manufacture of a fairing body embodying the present invention. - The
fairing 2 illustrated in FIGS. 1 to 5 comprises (a) afairing body 4 and (b) a plurality ofcollars 6 serving to rotatably couple thefairing body 4 to a cylindricalmarine riser 8. - The
fairing body 4 can be seen to be generally wedge shaped. Its front, lying adjacent theriser 8, has a lateral dimension similar to that of the riser. In the illustrated embodiment this dimension is slightly smaller than the riser diameter. Moving toward its rear the fairing body tapers to anarrow trailing edge 10. This shape is defmed by 9, 9 1, which meet at the trailing edge. Theconvergent walls front face 12 of the fairing body is shaped to conform to the adjacent surface of the riser, being part cylindrical and concave. The cross section which the assembly of riser and fairing presents to a current of water is best appreciated fromFIG. 3 , where it can be seen that the assembly's leadingedge 14 is formed by the riser itself and that the whole assembly forms a streamlined teardrop shape. In a manner which will be wholly familiar to the skilled person, this shape tends to maintain laminar flow and serves both to reduce drag (i.e. lateral loading upon the riser due to the current) and to prevent or reduce VIV. - The illustrated embodiment has a pair of identically formed
6,6′ at opposite ends of the fairing body. Incollars FIG. 5 it can be seen that each collar comprises abearing ring 16 which is split at 18 to allow theriser 8 to be introduced laterally into the bearing ring. The collar is formed of a resiliently deformable material so that the ring can be opened out—that is, ends of the ring on either side of thesplit 18 can be drawn apart—to allow the riser to be introduced. In the present embodiment this deformation of the collar is facilitated by a reducedthickness region 20 which serves as a resilient hinge. At 22,24 the collar has a bifurcated section. One 26, 28 leading from each bifurcation forms part of the bearing loop and in use lies between the fairing body and the riser (seelimb FIG. 4 ) while the 30, 32 extends in a direction generally parallel to another limb 34, 36 of the fairing body and forms a mounting tab through which the collar is mounted to the fairing body.adjacent face - As seen in
FIG. 3 , the fairing body has shallow recesses or pockets in which the mounting tabs are received, so that the tabs' outer surfaces are generally flush with the adjacent faces 34, 36 of the fairing body (seeFIG. 3 ). Attachment of the tabs to the fairing body is achieved using mechanical fasteners received by through- 38, 40 in the tabs which align with holes in the fairing body. The fasteners shown in the drawings are formed as nuts andholes bolts 42. In order to resist corrosion and minimise weight these may be formed of plastics. - However it is anticipated that during refinement of the product some other form of plastics fastener such as a plastics rivet is likely to replace the nuts and bolts. The fairing may be supplied to the end user with the tabs on one
face 34 pre-attached so that to mount the fairing the user first inserts the riser into the collars and then secures the relevant tabs to theother face 36. - The fairing body is formed by a single plastics moulding. More specifically the illustrated item is manufactured by the well known technique of rotational moulding, so that it is hollow. Polythene is the preferred material for this component, which is advantageous due to its low specific gravity (similar to that of water), toughness and low cost. An
opening 44 allows water to enter the fairing body to equalise internal and external pressures. The body could instead be formed as a solid polyurethane moulding. The collars are each formed by a single plastics moulding but for these the favoured material is nylon, which again has a specific gravity similar to that of water. - It will be apparent that the
internal face 44 of the collar'sbearing ring 16 serves as one half of a rotary bearing allowing the fairing to rotate about the riser's longitudinal axis and so to weathervane to face a current. Only the collar makes contact with the riser, its portion interposed between the fairing body and the riser serving to maintain clearance between these parts. The present inventor has recognised that it is highly desirable for this bearing surface to be (a) low friction and even “self lubricating” and (b) resistant to marine fouling. These properties can be promoted by incorporation of anti-fouling and friction reducing materials into the material of the collar. In the illustrated embodiment the plastics material of the collar contains an admixture of an anti-fouling composition which provides a controlled rate of release of copper ions, whose biocidal properties are well known, and also of silicon oil serving to reduce bearing friction. - The internal part of the bearing on which the fairing is mounted may be provided by the riser itself. That is, the fairing may be mounted directly upon the riser (or on a cylindrical protective sheath conventionally provided around the riser). A number of such fairings would normally be placed adjacent one another in a string along the riser. To prevent the fairings from moving along the length of the riser, clamps are secured to it at intervals (typically a string of perhaps five fairings would be confined between a pair of clamps). The clamps may be of a type well known in the context having a pair of half cylindrical clamp shells secured to the riser by a tension band passed around the shells.
- An alternative arrangement can be understood from
FIGS. 6 and 7 in which a clamp formed by two half 50, 52 is secured to the riser, again labelled 8 in this drawing, by acylindrical clamp shells tension band 54 received in a shallow annular recess in the exterior of acentral flange 56 formed by the clamp shells from either side of which project reduceddiameter spigot portions 58 upon which the 60, 62 of respective fairings, arranged on opposite sides of the clamp, ride. The drawing is simplified in that remaining parts of the two fairings are omitted (they can be taken to be similarly formed to those of the previous embodiment). While only a single clamp is shown in the drawing, it is to be understood that in this arrangement a clamp is provided between each adjacent pair of fairings, so that the fairings'rotary bearings are in each case formed by a collar riding upon the clamp.collars - Trials have shown that the
front face 12 of the fairing body can be omitted and that drag can thereby be reduced. In this case the front edges of the 9, 9 1of the fairing body form its front surface, and may be shaped to conform to the adjacent cylindrical surface of the riser. A convenient way to manufacture this fairing body can be appreciated fromwalls FIG. 8 there is a singlehollow moulding 70 is in the shape of two fairing bodies placed nose-to-nose. By dividing the moulding in theplane 72 and suitably machining/dressing the cut edges, two bodies are formed. Rotational moulding of thestructure 70 is favoured. Shallow recesses 74.76 will receive the mounting 30, 30 of the collars.tabs
Claims (17)
1. A fairing for mounting upon a cylindrical member for underwater deployment, the fairing comprising a fairing body which, viewed along its length, is substantially wedge-shaped, having a relatively broad front tapering to a relatively narrow trailing edge, and at least two collars which are both secured to the fairing body and are separated from each other along the length of the fairing body, the collars being positioned and aligned to receive the cylindrical member with the fairing body's front lying adjacent the cylindrical member and the axis of the cylindrical member lying along the length of the fairing body, thereby to pivotally mount the fairing body upon the cylindrical member such that it is able to rotate about the axis of the cylindrical member and so align itself with a water current, the fairing body and the cylindrical member together defining, when viewed along the length of the fairing, a teardrop shape having a leading edge formed, between the collars, by the cylindrical member.
2. A fairing as claimed in claim 1 wherein a portion of each collar is interposed between the fairing body and the cylindrical member in use, providing clearance therebetween.
3. A fairing as claimed in claim 1 , wherein each collar forms a respective bearing ring for receiving the cylindrical member.
4. A fairing as claimed in claim 3 wherein each bearing ring has a substantially circular interior bearing surface.
5. A fairing as claimed in claim 3 wherein the bearing ring is split such that it can be opened out to allow the cylindrical member to be inserted into it laterally.
6. A fairing as claimed in claim 5 wherein at least an end portion of the collar is initially free to allow the bearing ring to be opened out and means are provided to subsequently secure the free end of the collar to the fairing body to retain the fairing upon the cylindrical member.
7. A fairing as claimed in claim 6 wherein means to secure the free end of the collar comprise a mechanical fastener.
8. A fairing as claimed in claim 1 wherein the collar comprises two bifurcated portions, one limb of each extending between the cylindrical member and the fairing body to provide clearance therebetween and the other limb of each being secured in use to the fairing body.
9. A fairing as claimed in claim 1 wherein the front of the fairing body is shaped to complement the cylindrical member, its surface(s) lying upon a notional cylinder.
10. A fairing as claimed in claim 1 wherein a bearing surface of the collar, which faces toward the cylindrical member and upon which the collar rides, comprises low friction material.
11. A fairing as claimed in claim 10 wherein the bearing surface comprises self lubricating material.
12. A fairing as claimed in claim 11 wherein the collar comprises a plastics material with an admixture of a friction reducing agent.
13. A fairing as claimed in claim 1 wherein the collar comprises an anti-fouling agent.
14. A fairing as claimed in claim 1 wherein the collar comprises a plastics material with an admixture of an anti-fouling agent.
15. A fairing as claimed in claim 1 wherein the fairing body and the collar are formed by separate plastics mouldings.
16. A fairing as claimed in claim 1 wherein the fairing body is a hollow plastics moulding whose interior communicates with the exterior to permit equalisation of pressure.
17. A fairing as claimed in claim 1 which is substantially neutrally buoyant.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GBGB0319438.8A GB0319438D0 (en) | 2003-08-19 | 2003-08-19 | Fairing |
| GB0319438.8 | 2003-08-19 | ||
| PCT/GB2004/003107 WO2005019595A1 (en) | 2003-08-19 | 2004-07-19 | Fairing for a riser |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20070104542A1 true US20070104542A1 (en) | 2007-05-10 |
Family
ID=28052749
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US10/568,710 Abandoned US20070104542A1 (en) | 2003-08-19 | 2004-07-19 | Fairing for a riser |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US20070104542A1 (en) |
| BR (1) | BRPI0413634A (en) |
| GB (2) | GB0319438D0 (en) |
| WO (1) | WO2005019595A1 (en) |
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| CN102943634A (en) * | 2012-11-16 | 2013-02-27 | 西南石油大学 | Free-rotation impeller device for inhibiting eddy induced vibration of marine riser |
| WO2012109355A3 (en) * | 2011-02-08 | 2013-04-04 | VIV Solutions LLC | Vortex-induced vibration suppression device and mating collar system |
| CN103437717A (en) * | 2013-09-16 | 2013-12-11 | 西南石油大学 | Rotatable pentagonal impeller type vortex-induced vibration inhibiting device and method |
| WO2015088997A1 (en) * | 2013-12-09 | 2015-06-18 | Westerngeco Llc | Foul release material for use with fairings |
| US9080610B1 (en) * | 2010-10-21 | 2015-07-14 | VIV Solutions LLC | Vortex suppression fairings |
| US9273752B1 (en) * | 2013-11-04 | 2016-03-01 | Hutchinson Aerospace & Industry, Inc. | Vibration isolator device for vehicle fairings |
| US20160298790A1 (en) * | 2015-04-07 | 2016-10-13 | Ensco International Incorporated | Riser deflection mitigation |
| US9511825B1 (en) * | 2011-01-05 | 2016-12-06 | VIV Solutions LLC | Apparatus for suppressing vortex-induced vibration of a structure with reduced coverage |
| US9534618B1 (en) * | 2014-09-04 | 2017-01-03 | VIV Solutions LLC | Fairing bodies with multiple parts |
| US9546523B1 (en) * | 2014-06-06 | 2017-01-17 | VIV Solutions LLC | Collars for multiple tubulars |
| US9567745B2 (en) * | 2014-12-04 | 2017-02-14 | Siemens Aktiengesellschaft | Strake for a wind turbine tower |
| US9677688B1 (en) * | 2015-06-02 | 2017-06-13 | VIV Solutions LLC | Fairing having an offset opening |
| US9702482B1 (en) * | 2015-06-23 | 2017-07-11 | VIV Solutions LLC | Two-piece U-shaped fairing |
| US10107048B2 (en) * | 2016-09-29 | 2018-10-23 | Ensco International Incorporated | Weathervaning riser joint |
| US10344785B1 (en) | 2017-01-03 | 2019-07-09 | VIV Solutions LLC | Multiple component fairing |
| US20200141517A1 (en) * | 2017-06-15 | 2020-05-07 | Bluemarine Offshore Yard Service B.V. | Viv suppression strake assembly |
| US10669785B1 (en) * | 2017-08-30 | 2020-06-02 | VIV Solutions LLC | VIV suppression devices with buoyancy modules |
| CN111613352A (en) * | 2020-06-04 | 2020-09-01 | 中国核动力研究设计院 | Vortex-induced vibration suppression device for cylindrical structure |
| US10890272B1 (en) | 2019-08-30 | 2021-01-12 | VIV Solutions LLC | U-shaped fairing with hinged blocks |
| CN113652952A (en) * | 2021-08-26 | 2021-11-16 | 深圳市鑫神科技开发有限公司 | Vortex elimination method and vortex elimination device |
| CN116398511A (en) * | 2023-01-10 | 2023-07-07 | 武汉理工大学 | A vortex-induced vibration suppression device |
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|---|---|---|---|---|
| US20060021560A1 (en) * | 2004-05-02 | 2006-02-02 | Mcmillan David W | Tail fairing designed with features for fast installation and/or for suppression of vortices addition between fairings, apparatus incorporating such fairings, methods of making and using such fairings and apparatus, and methods of installing such fairings |
| NO327944B1 (en) | 2006-03-15 | 2009-10-26 | Sinvent As | A finding for reducing water current-induced stress on a marine riser |
| GB0608431D0 (en) * | 2006-04-28 | 2006-06-07 | Balmoral Group | Device |
| US7337742B1 (en) * | 2006-08-09 | 2008-03-04 | Viv Suppression, Inc. | Twin fin fairing |
| GB2442003A (en) * | 2006-09-21 | 2008-03-26 | Trelleborg Crp Ltd | Fairing for a marine riser |
| GB2445751B (en) | 2007-01-17 | 2009-02-25 | Trelleborg Crp Ltd | Fairing |
| EP2373054B1 (en) | 2010-03-09 | 2016-08-17 | Deutsche Telekom AG | Playback into a mobile target sound area using virtual loudspeakers |
| GB201014182D0 (en) * | 2010-08-25 | 2010-10-06 | Luffrum Simon | Method and apparatus for riser performance optimisation |
| CN102071883A (en) * | 2010-12-03 | 2011-05-25 | 上海交通大学 | Underwater stand pipe vortex induced vibration inhibiter adopting rotatable cowling |
| GB2498808B (en) * | 2012-01-30 | 2015-05-13 | Acergy France SAS | Stoppers for structures attached to hybrid riser towers |
| CN110630446B (en) * | 2018-08-31 | 2020-11-03 | 北京金风科创风电设备有限公司 | Envelope, wind generating set and tower drum structure |
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| GB2192015B (en) * | 1986-06-25 | 1990-03-21 | Secr Defence | A towed cable fairing |
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- 2003-08-19 GB GBGB0319438.8A patent/GB0319438D0/en not_active Ceased
-
2004
- 2004-07-19 GB GB0603040A patent/GB2421751B/en not_active Expired - Fee Related
- 2004-07-19 BR BRPI0413634-9A patent/BRPI0413634A/en not_active IP Right Cessation
- 2004-07-19 US US10/568,710 patent/US20070104542A1/en not_active Abandoned
- 2004-07-19 WO PCT/GB2004/003107 patent/WO2005019595A1/en not_active Ceased
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| US3899991A (en) * | 1973-12-17 | 1975-08-19 | Us Navy | Weather resistant segmented fairing for a tow cable |
| US4078605A (en) * | 1977-02-25 | 1978-03-14 | Cameron Iron Works, Inc. | Riser pipe string |
| US4700651A (en) * | 1983-01-18 | 1987-10-20 | Fathom Oceanology Limited | Fairing for tow-cables |
| US5467728A (en) * | 1994-06-22 | 1995-11-21 | The United States Of America As Represented By The Secretary Of The Navy | Retractable bow diving plane for a submarine |
| US6347911B1 (en) * | 1996-06-11 | 2002-02-19 | Slickbar Products Corp. | Vortex shedding strake wraps for submerged pilings and pipes |
| US5722340A (en) * | 1996-12-11 | 1998-03-03 | Mobil Oil Corporation | Fairing for marine risers |
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Cited By (27)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9080610B1 (en) * | 2010-10-21 | 2015-07-14 | VIV Solutions LLC | Vortex suppression fairings |
| US9511825B1 (en) * | 2011-01-05 | 2016-12-06 | VIV Solutions LLC | Apparatus for suppressing vortex-induced vibration of a structure with reduced coverage |
| WO2012109355A3 (en) * | 2011-02-08 | 2013-04-04 | VIV Solutions LLC | Vortex-induced vibration suppression device and mating collar system |
| US8727667B2 (en) | 2011-02-08 | 2014-05-20 | VIV Solutions LLC | Vortex-induced vibration suppression device and mating collar system |
| US9151308B2 (en) | 2011-02-08 | 2015-10-06 | VIV Solutions LLC | Vortex-induced vibration suppression device and mating collar system |
| CN102943634A (en) * | 2012-11-16 | 2013-02-27 | 西南石油大学 | Free-rotation impeller device for inhibiting eddy induced vibration of marine riser |
| CN103437717A (en) * | 2013-09-16 | 2013-12-11 | 西南石油大学 | Rotatable pentagonal impeller type vortex-induced vibration inhibiting device and method |
| US9273752B1 (en) * | 2013-11-04 | 2016-03-01 | Hutchinson Aerospace & Industry, Inc. | Vibration isolator device for vehicle fairings |
| WO2015088997A1 (en) * | 2013-12-09 | 2015-06-18 | Westerngeco Llc | Foul release material for use with fairings |
| US9546523B1 (en) * | 2014-06-06 | 2017-01-17 | VIV Solutions LLC | Collars for multiple tubulars |
| US9534618B1 (en) * | 2014-09-04 | 2017-01-03 | VIV Solutions LLC | Fairing bodies with multiple parts |
| US9567745B2 (en) * | 2014-12-04 | 2017-02-14 | Siemens Aktiengesellschaft | Strake for a wind turbine tower |
| US9759350B2 (en) * | 2015-04-07 | 2017-09-12 | Ensco International Incorporated | Riser deflection mitigation |
| US20160298790A1 (en) * | 2015-04-07 | 2016-10-13 | Ensco International Incorporated | Riser deflection mitigation |
| US9677688B1 (en) * | 2015-06-02 | 2017-06-13 | VIV Solutions LLC | Fairing having an offset opening |
| US9702482B1 (en) * | 2015-06-23 | 2017-07-11 | VIV Solutions LLC | Two-piece U-shaped fairing |
| US10513888B2 (en) * | 2016-09-29 | 2019-12-24 | Ensco International Incorporated | Weathervaning riser joint |
| US10107048B2 (en) * | 2016-09-29 | 2018-10-23 | Ensco International Incorporated | Weathervaning riser joint |
| US20190085643A1 (en) * | 2016-09-29 | 2019-03-21 | Ensco International Incorporated | Weathervaning riser joint |
| US10344785B1 (en) | 2017-01-03 | 2019-07-09 | VIV Solutions LLC | Multiple component fairing |
| US20200141517A1 (en) * | 2017-06-15 | 2020-05-07 | Bluemarine Offshore Yard Service B.V. | Viv suppression strake assembly |
| US10774949B2 (en) * | 2017-06-15 | 2020-09-15 | Bluemarine Offshore Yard Service B.V. | VIV suppression strake assembly |
| US10669785B1 (en) * | 2017-08-30 | 2020-06-02 | VIV Solutions LLC | VIV suppression devices with buoyancy modules |
| US10890272B1 (en) | 2019-08-30 | 2021-01-12 | VIV Solutions LLC | U-shaped fairing with hinged blocks |
| CN111613352A (en) * | 2020-06-04 | 2020-09-01 | 中国核动力研究设计院 | Vortex-induced vibration suppression device for cylindrical structure |
| CN113652952A (en) * | 2021-08-26 | 2021-11-16 | 深圳市鑫神科技开发有限公司 | Vortex elimination method and vortex elimination device |
| CN116398511A (en) * | 2023-01-10 | 2023-07-07 | 武汉理工大学 | A vortex-induced vibration suppression device |
Also Published As
| Publication number | Publication date |
|---|---|
| GB2421751B (en) | 2007-08-22 |
| GB0603040D0 (en) | 2006-03-29 |
| BRPI0413634A (en) | 2006-10-17 |
| WO2005019595A1 (en) | 2005-03-03 |
| GB0319438D0 (en) | 2003-09-17 |
| GB2421751A (en) | 2006-07-05 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AS | Assignment |
Owner name: TRELLEBORG CRP LIMITED, UNITED KINGDOM Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:SOMERVILLE, DAVID MICHAEL RUTHVEN;GIBSON, ROBERT;REEL/FRAME:018598/0238 Effective date: 20061101 |
|
| STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO PAY ISSUE FEE |