Riser methods and apparatuses

Information

  • Patent Grant
  • 10508506
  • Patent Number
    10,508,506
  • Date Filed
    Wednesday, October 5, 2016
    8 years ago
  • Date Issued
    Tuesday, December 17, 2019
    5 years ago
  • Inventors
    • Hisdal; Pal Magne
    • Hestenes; John
    • Midtun; Andre Kristiansen
    • Myking; John Olav
  • Original Assignees
  • Examiners
    • Buck; Matthew R
    • Lembo; Aaron L
    Agents
    • Thompson Hine LLP
Abstract
An apparatus including an external surface portion shaped so as to mate with a docking device, and two half-shells having internal surfaces of semi-circular cross section. The apparatus further includes a plurality of segments arranged inside the two half-shells and including teeth for gripping onto a shaft, and an installation tool operable to cause the two half-shells to close around the shaft, thereby securing the apparatus to the shaft.
Description
CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a national stage filing of International Application No. PCT/EP2016/073778 (Publication No. WO 2017/060291), filed on Oct. 5, 2016, which claims priority to GB Application 1517554.0, filed on Oct. 5, 2015. The entire contents of both of these applications are incorporated by reference herein.


The present invention relates to risers, and specifically methods of repair thereof and apparatuses used in the repair thereof.


BACKGROUND

There is increasing demand in the oil and gas industry to develop equipment and methods to enable subsea riser repair. Often, the aging risers to be repaired are disposed in deep water, making them inaccessible to divers. Furthermore, increasing restrictions on the use of divers is making riser repair, even in shallow water, increasingly challenging. Thus efforts are being made to develop techniques for deep water riser repair, utilizing apparatuses which can be hydraulically controlled from a remotely operated vehicle (ROV). The techniques must by design also be sensitive to the often fragile nature of the risers, as well as incorporating contingency measures in the event of a failed repair effort.


SUMMARY

In one embodiment, the invention is an apparatus including an external surface portion shaped so as to mate with a docking device, and two half-shells having internal surfaces of semi-circular cross section. The apparatus further includes a plurality of segments arranged inside the two half-shells and including teeth for gripping onto a shaft, and an installation tool operable to cause the two half-shells to close around the shaft, thereby securing the apparatus to the shaft.





BRIEF DESCRIPTION OF THE DRAWINGS

Some embodiments of the invention will now be described by way of example only and with reference to the accompanying drawings, in which:



FIG. 1 shows an alignment, installation and activation apparatus according to an embodiment of the invention;



FIG. 2 shows an alignment, installation and activation apparatus according to an embodiment of the invention;



FIG. 3 shows an alignment, installation and activation apparatus according to an embodiment of the invention;



FIG. 4 shows an alignment, installation and activation apparatus according to an embodiment of the invention;



FIG. 5 shows an alignment, installation and activation apparatus according to an embodiment of the invention;



FIG. 6 shows an alignment, installation and activation apparatus according to an embodiment of the invention;



FIG. 7 shows an alignment, installation and activation apparatus according to an embodiment of the invention;



FIG. 8 shows an alignment, installation and activation apparatus according to an embodiment of the invention;



FIG. 9 shows an alignment, installation and activation apparatus according to an embodiment of the invention;



FIG. 10 shows an alignment, installation and activation apparatus according to an embodiment of the invention;



FIG. 11 shows an alignment, installation and activation apparatus according to an embodiment of the invention;



FIG. 12 shows an alignment, installation and activation apparatus according to an embodiment of the invention;



FIG. 13 shows an alignment, installation and activation apparatus according to an embodiment of the invention;



FIG. 14 shows a gripper unit apparatus according to an embodiment of the invention;



FIG. 15 shows a gripper unit apparatus according to an embodiment of the invention;



FIG. 16 shows a gripper unit apparatus according to an embodiment of the invention;



FIG. 17 shows a gripper unit apparatus according to an embodiment of the invention;



FIG. 18 shows a gripper unit apparatus according to an embodiment of the invention;



FIG. 19 shows a gripper unit apparatus according to an embodiment of the invention;



FIG. 20 shows a gripper unit apparatus according to an embodiment of the invention;



FIG. 21 shows a gripper unit apparatus installation tool according to an embodiment of the invention;



FIG. 22 shows a gripper unit apparatus installation tool according to an embodiment of the invention;



FIG. 23 shows a method step according to an aspect of the invention;



FIG. 24 shows a method step according to an aspect of the invention;



FIG. 25 shows a method step according to an aspect of the invention;



FIG. 26 shows a method step according to an aspect of the invention;



FIG. 27 shows a method step according to an aspect of the invention;



FIG. 28 shows a method step according to an aspect of the invention;



FIG. 29 shows a method step according to an aspect of the invention;



FIG. 30 shows a method step according to an aspect of the invention;



FIG. 31 shows a method step according to an aspect of the invention;



FIG. 32 shows a method step according to an aspect of the invention;



FIG. 33 shows a method step according to an aspect of the invention;



FIG. 34 shows a method step according to an aspect of the invention;



FIG. 35 shows a method step according to an aspect of the invention;



FIG. 36 shows a method step according to an aspect of the invention;



FIG. 37 shows a method step according to an aspect of the invention;



FIG. 38 shows a method step according to an aspect of the invention; and



FIG. 39 shows a method step according to an aspect of the invention.





DETAILED DESCRIPTION

A gripper unit apparatus (GU); alignment, installation and activation (AIA) apparatus; and several methods of use thereof are described in detail below, by way of example, and with reference to the accompanying drawings.


Alignment installation and activation (AIA) apparatus:


According to an exemplary embodiment, the AIA apparatus 100, illustrated in FIG. 1, comprises the following principal components:

    • Grabber bars 101 and 101′ on each side of the frame;
    • ROV panel 102 with ROV valves, gauges and receptacles;
    • Docking plate 103 for holding component;
    • Cage assembly supporting docking plate 108;
    • Pull-in cylinders 104 and 104′;
    • Pitch cylinders 105 and 105′;
    • Rotation cylinder 106;
    • Hang off unit 107;
    • Docking cone 109.



FIGS. 2 and 3 are detailed view of the docking plate 103 and cage assembly 108 respectively. Aspects of the AIA frame are described further below, with respect to the procedure for landing a component on a riser.


Non-limiting example dimensions for the AIA apparatus depicted in FIGS. 4 to 13 are given in the table below:
















Dimension
Value




















L1
1420
mm



L2
1080
mm



L3
1200
mm



L4
1612
mm



L5
3644
mm



L6
2268
mm



L7
985
mm



L8
400
mm



L9
240
mm



L10
740
mm



L11
90
mm



L12
975
mm



L13
101
mm



L14
1027
mm



L15
1137
mm



L16
1021
mm



ø1
33.7
mm



L17
1167
mm



L18
372
mm



L19
312
mm



L20
2344
mm



L21
101
mm



L22
916
mm



L23
552
mm



L24
110
mm



L25
600
mm



ø2
120
mm



ø3
20
mm



ø4
50
mm










θ1
20°



θ2
20°



θ3
1.4° 



θ4
5.0° 











L26
741
mm










θ5
40°











L27
1851
mm



L28
469
mm










Gripper Unit (GU) Apparatus:


An exemplary embodiment of a gripper unit (GU) apparatus 200 is illustrated in FIGS. 14-20. The GU should be sufficiently light-weight to allow an ROV to carry it from a basket to the worksite without crane assistance.


As load is applied to the GU, the slips segments 201 move upwards and inwards relative to the body of the unit 204 and the teeth protrude slightly into the pipe surface 203. The ultimate capacity is limited by the shear strength across the number of teeth activated. The GU also comprises a cap 205 shaped so as to interface with the docking cone 109 of the AIA frame.


As the slips will not engage around the complete circumference of the pipe, this will ensure that all alignment reaction forces introduced into the pipe will be on the part of the pipe that is circumferentially supported by the slip segments. The initial activation of the slip teeth onto the pipe is by mechanical closing of the slip carrier. This is only required to hold the weight of the unit. Thereafter the slips are self-activating. The GU has slips with longitudinal as well as transverse teeth. The longitudinal teeth will determine the torsional capacity of the GU during the subsequent rotational alignment. Some torsional forces may be introduced by the flexible riser, but these are assumed to be low.


To eliminate the need to lock the GU onto the riser pipe while suspended from the crane, with associated risk of introducing vessel dynamic forces to the riser, a light weight unit that can be launched with the ROV is proposed. The weight of the concept unit is about 50 kg.


Certain aspects of the GU include:

    • Light weight: ROV handling only
    • Nearly full circumferential pipe support
    • Self-activating slips
    • Reaction forces taken over long length
    • Teeth profile qualified by DnV, no fatigue issues after gripping
    • Pull test to ensure initial activation
    • Positive disengagement of slips


The GU has slips with longitudinal as well as transverse teeth. The longitudinal teeth will determine the torsional capacity of the GU during the subsequent rotational alignment.


Springs 202 in the GU ensure that the slip segments will always be forced inwards (towards the pipe). The springs will always try to pull the GU body downwards relative to the slip segments. When the GU body is pulled downwards relative to the slip segments, the slip segments will be forced inwards towards the pipe. Thus the GU will at all times hold onto the pipe. In the event that the GU is subjected to a large upwards force, it might release from the pipe, but once the force is removed the GU will grip back onto the pipe due to the force provided by the springs. From a risk point of view this is a significant advantage as otherwise (i.e. without springs) the GU might fall off the pipe.


The hardened teeth bite into the pipe surface. The tooth profile from the DnV qualified clamps will be utilized. These have been checked against RP-F113 to ensure that the marks left on the pipe surface shall not initiate subsequent fatigue damage.


Non-limiting example dimensions for the GU apparatus depicted in FIGS. 14-20 are given in the table below:
















Dimension
Value









L29
605.5 mm  



L30
584.5 mm  



L31
154.5 mm  



L32
153 mm



L33
584 mm



L34
300 mm



L35
125 mm



L36
 70 mm



L37
53.8 mm 



θ6
30°



ø5
108 mm











FIG. 19 is a close-up view of the encircled region (labelled 250) in FIG. 17, where 206 is a spring lower shell; 207 is a spring support; 208 is a screw (e.g. M8×16); 209 is a torsion spring; and 210 is a screw (e.g. M6×40). FIG. 20 is a bottom view of the GU apparatus. FIGS. 21 and 22 show an installation tool 260 for installing the GU apparatus 200 on a riser, where 211 is a buoyancy aid; 212 is the installation tool frame; 213 is a 6-line hot stab; 214 is a flange with cylinders for activation; 215 is a left running tool gripper; and 216 is a right running tool gripper.


Other aspects of the GU apparatus as illustrated in FIG. 16 include: upper half shell 217; locking bolt 218; bottom half shell 219; and disc springs flange 220.


Outline of Procedure for Landing a Component on a Riser:


In the following, an exemplary method for landing and installing a component (e.g. a flange adaptor) on a riser is outlined. The main method steps are depicted, in sequence, in FIGS. 23 to 39. It should be noted that certain steps may be omitted. Furthermore, although the below steps are directed towards a riser which is supported by a riser tower, one skilled in the art will appreciate that the method is also applicable to a riser which is independently suspended.


0) Perform initial cutting of the riser pipe 301; secure the lower section of the riser pipe once cut in a cofferdam provided on the riser tower 302; cut the piggyback straps above the cutting point to allow the bottom end of the upper section of the riser pipe to be moved out from the riser tower; install a riser jacking tool 303 (RJT) on the riser tower, above the cut; jack the bottom end of the upper section of the riser pipe (hereafter referred to as the “riser pipe”) outwards from the riser rower; cut a 2 metre long section from the end of riser pipe; remove pipe coating; and prepare end of pipe.


1) Perform a pre-survey to determine the extent of the lean of the riser tower and identify the heading of a 3 metre long straight section at the bottom of the riser pipe. The readings from a hydro-acoustic position reference transponder and high-precision acoustic position transponder on the riser tower buoyancy tank and remotely operated vehicle should be sufficient for the accuracy required. If the heading identified is within +/−20 degrees error margin, the rotation in the gripper unit (GU) apparatus 200 can correct for it.


2) Perform initial testing of all systems on the deck of the vessel.


3) Launch from the vessel the tool basket containing the GU apparatus 200 and a subsea marker. Alternatively these may be launched with the ROV 304. It should be ensured that the buoyancy tank and dynamic risers are avoided to prevent damage thereto.


4) Mark a 12 o'clock position 1.25 m from the end of the riser pipe. Also mark ROV grabber exclusion zones. The RJT may be retracted slightly to allow the ROV to grab onto the riser tower and be in a more stable position when performing the marking. The distance from the riser pipe end has a tolerance of +/−50 mm that can be corrected using the pull-in cylinders on the AIA frame 100. The distance is measured from the riser pipe end with a prefabricated L-shaped piece of tubing with magnets attaching it to the pipe, while the mark is made with the ROV. The mark is made with a subsea ‘crayon’ type stick. The IKM Technique Subsea Marker (http://www.ikm.com) may be used, for example. Care should be taken to ensure that the lower 250 mm of the riser pipe, and the 250 mm just below the GU apparatus are not be damaged by the ROV 5-function manipulator, as these areas are the primary and contingency sealing areas for the flange adaptor 306.


5) Grip onto the allowed grabbing zone on the pipe with the left hand ROV 5-function ‘grabber’. Install and activate the GU apparatus 200 using the installation tool 260 operated by the ROV's 7-function manipulator, as depicted in FIGS. 23-27. The GU apparatus is installed with the open slot perpendicular to the pipe bending plane. The activation is by turning an ROV handle clockwise using the wrist rotate function. The pitch of the threaded connection that activates the slips should be selected to ensure sufficient grip based on an applied torque of 100 Nm, for example.


6) Perform vertical pull test on GU apparatus using the ROV. Pull between the left hand grabber and the right hand 7-function manipulators. The left hand grabber may be holding onto the riser pipe below if possible, or the RJT may be used to bring the riser pipe closer to the riser tower thereby allowing the ROV to grab onto another riser tower pipe. This verifies initial engagement of the GU apparatus towards the riser pipe, and starts weight setting the teeth into the riser pipe wall. The vertical pull test is limited by the force capacity of the 7-function manipulator, but is only required to prove initial activation to support the weight of the GU apparatus itself.


7) Check the elevation and heading of the installed GU apparatus. A vertical allowance for incorrect installation may be +/−50 mm as measured from the riser pipe end. Correct installation within this tolerance is deemed to be uncomplicated to achieve with a prefabricated L-shaped measuring tool.


8) Rig the AIA apparatus and connected flange adapter and flexible riser for deployment by the vessel crane. The in-water center of gravity may be calculated to allow a 45 degrees deployment angle with the GU apparatus docking unit aligned with the riser pipe axis. In addition, the AIA apparatus may have an adjustable lifting point, to allow adjustment on site for the correct suspended angle.


9) Deploy and lower the AIA frame and flexible riser to the working depth. The net resultant force from the flexible riser will depend on whether the other end of the flexible riser is suspended from a second crane or winch. The lifting points will be designed in accordance with DnV Offshore standards (available at: https://rules.dnvgl.com/servicedocuments/dnv).


10) Move the AIA apparatus towards the riser pipe between the RJT and the GU apparatus, in one case keeping the load (including the AIA apparatus) under active heave compensation, FIG. 28. The AIA apparatus docking slot for the riser pipe has guide plates to facilitate guiding onto the riser pipe.


11) Guide the AIA apparatus docking slot onto the riser pipe with the ROV and lower the AIA apparatus until the lift rigging 305 is fully slack, FIGS. 29-32. Disconnect the lift rigging, FIG. 33. The docking slot can slide up and down the riser pipe including the three layer polypropylene coating. The amount the docking slot can slide is limited by the distance between the RJT and the GU apparatus. The docking cone is pre-adjusted so that its axis is roughly aligned with the riser pipe axis at the moment of docking. When being lowered, the hydraulic pitch cylinder on the AIA apparatus may bypass the hydraulic fluid to an accumulator tank to reduce the bending moment introduced into the riser pipe when the crane is lowering the AIA apparatus, flange adapter and flexible riser to a position where the loads become suspended from the riser pipe. The GU apparatus centralizes the docking cone as well as guiding it into the correct axial and rotational position. Some torsional forces may be introduced by the flexible riser, but these are assumed to be low. Maximum allowable landing speed will be determined by considering bending stresses induced in the riser pipe and radial reaction point loads in pipe wall. The self-activation property of the GU apparatus will create radial loads circumferentially on the riser pipe. Installing the AIA apparatus at an angle reduces risk of induced loads from the crane onto the prepared riser pipe end.


12) Grab onto the ROV panel of the AIA apparatus and close the ‘float’ function valve, FIG. 33. The float function is the bypass to the accumulator from the pitch cylinder, introduced to reduce bending moments in the riser pipe during landing, as well as reducing the bending moments on the extended pull-in cylinders. The ROV panel is designed with a grabber bar on the left side to provide a fixed position for the ROV. The grabber bar is used with the ROV's left 5-function ‘grabber’ arm, and the stab insert and valve operations are carried out with the right hand 7-function manipulator.


13) Insert 3 hydraulic 6-line stabs into receptacles on the ROV panel on the AIA apparatus. FMC/Oceaneering stabs may be used. All stabs may be delivered with D-handle as well as ‘fishtail’ handle for parallel 3-finger jaw.


14) Operate the pitch cylinder to lift the flange adaptor 306 until it is axially aligned with the riser pipe, FIG. 33. The pitch cylinder may be designed to provide up to 20 degrees of pitch. The pitch cylinder may be sized so that it cannot provide enough force to overstress the riser pipe.


15) Using, for example a level indicator, check that a plane through the axis of the two pull in cylinders is at 90 degrees to the riser bending plane. The ROV panel may have a level gauge to assist the visual indication that the AIA apparatus is correctly aligned.


16) If the angle is offset, operate the rotate cylinder to achieve axial alignment.


17) Stab the, for example Gisma, electrical/signal connector to the AIA apparatus. Tronic connectors may also be used.


18) Increase the hydraulic pressure in the pull-in cylinders of the AIA apparatus until the AIA apparatus starts lifting, FIG. 34. Use visual feedback through dedicated camera and proximity sensors to confirm alignment. The AIA apparatus/flange adapter may have two cameras, 90 degrees offset with a sighting line along the connector axis. The cameras are used to provide visual verification of alignment to the operator. Furthermore, proximity sensors are installed on the flange adaptor to assist with alignment.


19) Check alignment just before entry of the riser pipe into the flange adaptor. Operate pitch, rotate, and pull-in cylinders to align.


20) Keep lifting the AIA frame using the pull-in cylinders until the riser pipe is fully bottomed out in the flange adaptor. Monitor sensor feedback can be used to monitor this part of the installation. The operator may operate the two pull-in cylinders independently from each other for fine alignment. The operator should continuously monitor the alignment by camera and pressure readings. The pressures should be kept low, only 2-5% above the necessary pressure to lift the suspended weight. If the pull-in stops, that is an indication of jamming and without increasing the pressure, the primary method to resolve it is to identify and lift only with the lowest (most extended) cylinder. The tilt and rotate function of the AIA apparatus can also be used for fine alignment at this stage. The two hydraulic circuits for the pull-in cylinders can also be operated in parallel after a certain engagement has been achieved, utilizing the flange adaptor's self-aligning capability. This may save a small amount of operation time. The cylinder interface to the AIA apparatus can be built with a small degree of flexibility, by rubber bushings or springs. This utilizes the self-alignment capability of the flange adaptor, and may reduce the number of jamming incidents and simplify the task for the operator.


21) Increase the holding pressure in the pull-in cylinders to hold the riser pipe firmly to the flange adapter abutment face. Upon activation of the flange adapter when the balls make initial contact with the surface of the riser pipe, the activation will tend to separate the end of the riser pipe from the abutment face. The pull-in cylinders are dimensioned to counteract that force.


22) Activate the flange adaptor. The 1500 bar pressure for the tensioners is achieved by integrating a hydraulic intensifier on the connector body. The sensors on the tool are linked up to the ROV skid, where the signal from each sensor is multiplexed onto an RS485 serial communication to the topside control unit. Visual indications provide backup for the sensors in the connector.


23) Perform a seal test. The seal test may be carried out with hydraulic oil. The volume to be tested is small and only a very small volume is required to increase the pressure to 350 bar. A very small volume would then be released to the sea upon completion of the seal test. A hydraulic intensifier may be used to provide the pressure for the seal test.


24) Disconnect the hydraulic stabs between the AIA apparatus and the flange adapter.


25) Cut or pull off the sensor cables between the AIA apparatus and the flange adaptor. For cutting, the ROV cable cutter may be used.


26) Unlock the locking-bolt with the ROV handle on the AIA apparatus, and extend the pull-in cylinders approximately 500 mm, FIG. 35. Ensure the AIA apparatus is fully undocked from the flange adaptor. Monitor separation between the docking cone and GU apparatus.


27) Using the pitch cylinders, start pitching the AIA apparatus out, away from the riser pipe, FIG. 36. When the flange adaptor and flexible riser have been disconnected from the AIA apparatus, the AIA apparatus can be tilted outwards by a larger angle without inducing a large amount of stress into the riser pipe. This creates sufficient clearance to recover the AIA apparatus without danger of impact with the flange adaptor.


28) If required, operate the rotate cylinder on the AIA frame back to neutral position to align the key-slots in the docking cone.


29) Operate the pitch cylinder until maximum distance between the AIA apparatus and the flange adaptor is achieved. Disconnect the ROV stabs. Note that an angle greater than 20 degrees can now be achieved as the weight of the flange adaptor and flexible riser has been removed from the AIA apparatus.


30) Lower the crane with a forerunner and hook onto a lift point of the AIA apparatus for recovery of the AIA apparatus back to the surface, FIG. 37. The center of gravity (COG) of the AIA apparatus will by this point have changed significantly, due to disconnection of the flange adaptor, hence a separate lift point may be used. The lift point is designed for ease of ROV hook connection


31) Lift the AIA apparatus clear of the GU apparatus.


32) By movement of the vessel and/or crane boom, move the AIA apparatus clear of the riser pipe by a safe distance. The AIA apparatus may also be guided with assistance from the ROV. What constitutes a safe distance may be dependent on weather and vessel station-keeping capability, as well as actual current.


33) Recover the AIA frame back to the vessel deck.


34) Deactivate and recover the GU apparatus to the tooling basket and subsequently recover to the vessel deck.



FIG. 39 shows the riser pipe with the installed flange adaptor 306 after completion of the method.


Although the invention has been described in terms of certain embodiments as set forth above, it should be understood that these embodiments are illustrative only and that the claims are not limited to those embodiments. Those skilled in the art will be able to make modifications and alternatives in view of the disclosure which are contemplated as falling within the scope of the appended claims. Each feature disclosed or illustrated in the present specification may be incorporated in the invention, whether alone or in any appropriate combination with any other feature disclosed or illustrated herein.

Claims
  • 1. A method of repairing a shaft, wherein the shaft is a subsea riser for use in the oil industry, the method comprising: cutting through the shaft at a pre-determined location, resulting in a first shaft section and a second shaft section;attaching a gripper unit apparatus onto the first shaft section;landing an alignment and installation apparatus onto said gripper unit apparatus, the alignment and installation apparatus carrying a component to be installed on the cut end of the first shaft section, wherein the component is a connector for connecting the first shaft section to a flexible pipe;pitching and rotating the alignment and installation apparatus to align an axis of the connector with the axis of the first shaft section;contracting the alignment and installation apparatus, thereby translating the connector substantially along the axis of the first shaft section until the cut end of the first shaft section is positioned on or within the connector; andactivating the connector to secure it onto the first shaft section, thereby enabling the communication of fluids between the flexible pipe and the first shaft section, wherein the gripper unit apparatus comprises teeth that are arranged to protrude slightly into the surface of a shaft and are arranged to attach the gripper unit apparatus to any position along part of a section of a shaft such that the gripper unit apparatus is not restricted to only attaching to an external flange or fixed connector on part of a section of a shaft.
  • 2. The method according to claim 1, wherein said step of landing the alignment and installation apparatus comprises: suspending the alignment and installation apparatus from a topside vessel, such that a portion of the apparatus designed to mate with the gripper unit apparatus is positioned substantially above the gripper unit apparatus;maneuvering the alignment and installation apparatus substantially along the axial direction of the first shaft section until said portion of the alignment and installation apparatus comes into contact with the gripper unit apparatus; andreleasing the alignment and installation apparatus from the topside vessel such that the alignment and installation apparatus becomes supported on the first shaft section by the gripper unit apparatus.
  • 3. The method according to claim 2, further comprising using a remotely operated vehicle to guide the alignment and installation apparatus whilst it is suspended from the topside vessel.
  • 4. The method according to claim 2, wherein the alignment and installation apparatus is configured such that it transmits substantially only axial loads to the first shaft section via the gripper unit apparatus when it is released from the topside vessel onto the gripper unit apparatus.
  • 5. The method according to claim 1, wherein the gripper unit apparatus comprises: a body comprising two half-shells having internal surfaces of semi-circular cross section;a plurality of segments arranged inside the two half-shells and comprising teeth for gripping onto the riser; anda cap provided on the body and shaped so as to interface with a docking device;wherein an installation tool operable by a ROV is arranged to cause the two half-shells to close around the riser, thereby securing the gripper unit apparatus to the riser; and wherein the alignment and installation apparatus comprises:a frame;an interface element for supporting said component, the interface element being removably attached to the frame;the docking device, wherein the docking device is configured to mate with the gripper unit apparatus provided on the riser, the docking device being movably attached to the frame; andone or more actuators for controlling the position of the frame relative to the riser when in use.
Priority Claims (1)
Number Date Country Kind
1517554 Oct 2015 GB national
PCT Information
Filing Document Filing Date Country Kind
PCT/EP2016/073778 10/5/2016 WO 00
Publishing Document Publishing Date Country Kind
WO2017/060291 4/13/2017 WO A
US Referenced Citations (57)
Number Name Date Kind
1929447 Remde Oct 1933 A
2775469 Brown Dec 1956 A
3724061 Schipper Apr 1973 A
4014180 Kelly Mar 1977 A
4103943 Curtin Aug 1978 A
4290632 Manchester, Jr. Sep 1981 A
4330143 Reneau May 1982 A
4445804 Abdallah May 1984 A
4490073 Lawson Dec 1984 A
4643614 Laursen Feb 1987 A
4832379 Smith May 1989 A
4848949 Castel Jul 1989 A
4906136 Norbom Mar 1990 A
5590913 Morris Jan 1997 A
6129391 Rakieski Oct 2000 A
6694684 Radke Feb 2004 B2
6830268 Krausz Dec 2004 B2
7086807 Mackinnon Aug 2006 B2
7455478 Matteucci Nov 2008 B2
7600569 Routeau Oct 2009 B2
8047278 Swietlik Nov 2011 B2
8162061 Maxwell Apr 2012 B2
8418766 Luppi Apr 2013 B2
8511387 Fraser Aug 2013 B2
8517634 Liso Aug 2013 B1
8528646 Stezycki Sep 2013 B2
8540031 Rimi Sep 2013 B2
9004818 Laborde et al. Apr 2015 B2
9080393 Wishahy Jul 2015 B2
9784062 Solis Oct 2017 B1
10260664 Richardson Apr 2019 B2
20040120779 Evans Jun 2004 A1
20060062638 Bergeron et al. Mar 2006 A1
20070044973 Fraser Mar 2007 A1
20070095524 Lesko May 2007 A1
20070140797 Armstrong Jun 2007 A1
20080205990 Bird Aug 2008 A1
20080245933 Stokes Oct 2008 A1
20080289829 Bergeron Nov 2008 A1
20090272855 Oram Nov 2009 A1
20090290939 Large Nov 2009 A1
20100059990 Avery Mar 2010 A1
20100186963 Butcher Jul 2010 A1
20120118580 Swanson May 2012 A1
20120133122 Hovik May 2012 A1
20120141212 Long Jun 2012 A1
20120145407 Varley et al. Jun 2012 A1
20120199358 Larsson Aug 2012 A1
20120261133 Stezycki Oct 2012 A1
20150176340 Bastesen Jun 2015 A1
20150354295 Routeau Dec 2015 A1
20150361770 Luppi Dec 2015 A1
20160039076 Voss Feb 2016 A1
20160258552 Larsson Sep 2016 A1
20170130871 Bastesen May 2017 A1
20180313166 Nijjar Nov 2018 A1
20190055822 Cargol, Jr. Feb 2019 A1
Foreign Referenced Citations (3)
Number Date Country
248508 Mar 1926 GB
2004090348 Oct 2004 WO
2013144601 Oct 2013 WO
Non-Patent Literature Citations (2)
Entry
PCT, International Search Report and Written Opinion of the International Searching Authority, International Application No. PCT/EP2016/073778, 17 pages, dated Mar. 21, 2017.
GB, Combined Search and Examination Report Under Section s17 and 18(3), GB Application No. 1517554.0, 7 pages, dated May 5, 2016.
Related Publications (1)
Number Date Country
20180313175 A1 Nov 2018 US