The present invention relates to offshore oil and gas floating platforms, and to a system for tensioning a riser extending from a subsea wellhead to a floating platform. The system includes a plurality of hydraulic cylinders which control the vertical position of the riser and a mechanism to transfer riser torque to the hull.
Various types of tensioners have been devised for use in the oil and gas industry. U.S. Pat. No. 4,039,177 discloses a compensation mechanism with a passive damped pneumatic-hydraulic spring system. U.S. Pat. No. 4,799,827 discloses a modular riser tensioner, and U.S. Pat. No. 5,160,219 discloses a variable spring rate riser tensioner. U.S. Pat. No. 4,617,998 discloses a riser with a braking system. Other patents of interest includes U.S. Pat. Nos. 3,970,292, 4,004,532, 4,072,190, 4,215,950, 4,616,707, 4,721,053, 4,799,827, 4,828,230, 4,883,387, 4,883,388, 4,892,444, 5,020,942, 5,252,004, 5,283,552, 5,244,313, 5,551,803, 5,671,812, 5,846,028, 5,944,111, 6,045,296, 6,585,455, 7,112,011, 7,328,741, 7,329,070, and 7,632,044.
U.S. Pat. No. 4,787,778 discloses a riser tensioning system with three tensioners pivotally secured to a hollow surface of the production platform and to a tensioner ring. Publications of interest include U.S. 2005/0147473, U.S. 2006/0108121, U.S. 2006/0280560, U.S. 2007/0056739, U.S. 2007/0196182, U.S. 2008/0205992, and U.S. 2009/0145611.
The disadvantages of the prior art are overcome by the present invention, an improved riser tensioning system is hereinafter disclosed.
A riser tensioning system includes a tensioning ring 18 for secured engagement with the riser, a plurality of hydraulic cylinders 12 each extending between the tensioning ring and a folding platform, and a gimbal mechanism below the tensioning ring and acting between the platform and the riser to allow the riser axis to tilt relative to the platform. One or more torque transfer members or supports extend between the tensioning ring and the gimbal mechanism and allow axial movement of the tensioning ring and the riser with respect to the floating platform.
These and further features and advantages of the present invention will become apparent from the following detailed description, wherein reference is made to the figures in the accompanying drawings.
The tensioning system 10 includes a plurality of circumferentially spaced cylinders 12 each having a cylindrical axis 13 inclined relative to the system central axis 15. The lower end of each cylinder may be secured to the hull H, as discussed subsequently, while the rod end 14 is interconnected with the tensioning ring 18, which is conventionally in secured engagement with the riser R. More particularly, the rod end 14 of each cylinder 12 is connected to the load frame 16, which in turn is secured to the tensioning ring 18. One or more pressurized fluid hydraulic cylinders may be provided for extending and retracting each hydraulic cylinder 12. Those skilled in the art will appreciate that the tensioning system as shown in
As shown in
Referring now to
The system as disclosed herein uses gimbals for an angular offset between the riser and the platform, and prevents torsional loads from being directed through the hydraulic cylinders 12 while keeping the riser centralized within the wellbay. The hydraulic cylinders are preferably mounted at an angle relative to the riser as shown in the attached figures, so that the upper tensioning ring may be smaller in diameter to reduce the bending moment and allow the tensioning ring to pass through a conventional rotary table. Large diameter strakes or tie-back connectors may be passed through the system by simply detaching the upper end of the cylinders and pivoting each cylinder out of the way. Angled cylinders are inherently less stable, which increases the benefits of accommodating both the torsional loads and the lateral loads between the riser and the hull.
The use of a plurality of cylindrical rods effectively transmits the torsional loads from the tensioning ring through the gimbal and to the hull. These rods also transfer the lateral loads from the riser to the gimbal and then to the structure, and resist bending loads which could be significant if one of the hydraulic cylinders should fail. The torque transfer rods provide support and stabilization to the cylinder arrangement while allowing the cylinders to move with respect to the platform. In an alternative embodiment, a single support tubular is used surrounding the riser for transmitting torsional and lateral loads through the gimbal and to the hull while allowing axial movement between the riser and the gimbal.
Load frame 16 serves the purpose of mechanically connecting the rod end of each hydraulic cylinder with the tensioning ring, while also allowing for adjustment so that all the hydraulic cylinders, when activated, uniformly move the tensioning ring. The torque transfer tubular 44, serves the same purpose as the rods 22.
Although specific embodiments of the invention have been described herein in some detail, this has been done solely for the purposes of explaining the various aspects of the invention, and is not intended to limit the scope of the invention as defined in the claims which follow. Those skilled in the art will understand that the embodiment shown and described is exemplary, and various other substitutions, alterations and modifications, including but not limited to those design alternatives specifically discussed herein, may be made in the practice of the invention without departing from its scope.
This application is a U.S. National Stage Application of International Application No. PCT/US2011/033054 filed Apr. 19, 2011 and claims the priority of U.S. Provisional Application No. 61/235,998 filed on Apr. 20, 2010, the disclosures of which are incorporated herein by reference for all purposes in their entirety.
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/US2011/033054 | 4/19/2011 | WO | 00 | 11/19/2014 |
Publishing Document | Publishing Date | Country | Kind |
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WO2011/133552 | 10/27/2011 | WO | A |
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Number | Date | Country | |
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20150136412 A1 | May 2015 | US |
Number | Date | Country | |
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61325998 | Apr 2010 | US |