This application is based on U.S. Provisional Patent Application No. 60/465,092, which was filed on Apr. 23, 2003.
The present invention is directed to a turret mooring system which comprises a turret that is rotatably supported in the moon pool of a vessel by at least an upper bearing assembly. More particularly, the invention is directed to a bearing support assembly which isolates the upper bearing assembly from deflections of the vessel.
Turret mooring systems are commonly used to anchor a vessel to the sea floor. Internal turret mooring systems typically comprise a turret which is rotatably supported in a moon pool that is formed in the hull of the vessel between the bow and the stern. The turret is often supported by both an upper bearing assembly which is connected between the upper end of the turret and the top of the moon pool and a lower bearing assembly which is connected between the lower end of the turret and the bottom of the moon pool. The upper bearing assembly typically comprises a combination axial and radial bearing which is capable of transmitting both the vertical and horizontal mooring loads from the turret to the vessel. The lower bearing assembly usually comprises a radial bearing which transmits only the horizontal mooring loads from the turret to the vessel.
A vessel in the open sea is often affected by waves and swells which can cause the vessel to hog and sag. As the vessel hogs and sags, the normally circular cross section of the moon pool deflects into alternating oval configurations. Since the vessel reacts somewhat like a beam in bending, these deflections are greatest at the top of the moon pool, which is normally where the upper bearing assembly is connected. In addition, turret mooring systems are typically designed to provide a clearance between the lower bearing assembly and the turret. As a result, the horizontal mooring loads will cause the turret to pivot about a horizontal axis located near the upper bearing assembly. Unless means are provided to isolate the upper bearing assembly from the deflections of the moon pool and the pivoting of the turret, these displacements may damage the upper bearing assembly and interfere with the operation of the turret mooring system.
In certain prior art turret mooring systems, bearing support assemblies comprising elastomeric or steel springs have been employed to isolate the upper bearing assembly from the deflections of the moon pool and to allow the turret to pivot about a horizontal axis. However, these bearing support assemblies contain many parts, require frequent maintenance and are expensive.
In accordance with the present invention, these and other disadvantages in the prior art are overcome by providing a bearing support assembly for a turret mooring system which comprises a turret that is rotatably supported in a moon pool of a vessel by an upper bearing assembly which is secured to an upper portion of the turret. The bearing support assembly comprises an upper ring which is connected to the upper bearing assembly, a lower ring which is connected to the moon pool, and a number of support beams which extend between the upper and lower rings. Furthermore, the lower ring is located near the vertical center of the moon pool where the deflections due to hogging and sagging of the vessel are minimal. In addition, the support beams are preferably designed to deflect slightly and thereby allow the turret to pivot about a horizontal axis located near the upper bearing assembly.
Since the lower ring of the upper bearing support assembly is located near the vertical center of the vessel, only minimal deflections of the vessel will be transmitted to the upper bearing assembly through the support beams. In addition, because the support beams will deflect and allow the turret to pivot, the pivoting of the turret will not adversely affect the upper bearing assembly. Thus, the upper bearing support assembly of the present invention provides an effective means to isolate the upper bearing assembly from both the deflections of the vessel and the pivoting of the turret.
These and other objects and advantages of the present invention will be made apparent from the following detailed description, with reference to the accompanying drawings.
Referring to
The turret 16 is rotatably supported in the moon pool 18 by an upper bearing assembly 32 and, when the buoy 22 is attached to the turret, a lower bearing assembly 34. In this manner, the vessel 14 is allowed to weathervane around the turret 16 while still being firmly anchored to the sea floor. The upper bearing assembly 32 ideally comprises a combination thrust and radial bearing, such as a conventional three-row roller bearing, which supports the weight of the turret 16 and the mooring chains 24 and accommodates the horizontal and vertical mooring loads acting between the turret and the hull 20. The lower bearing assembly 34, in contrast, preferably comprises a radial bearing which accommodates only the horizontal loads acting between the buoy 22 and the hull 20. If desired, the turret mooring system 12 may also include a number of bumper pads 36, which may be comprised of, for example, rubber or polyethylene, to cushion the lower portion of the turret 16 from the hull 20 prior to connecting the buoy 22 to the turret.
In accordance with the present invention, the upper bearing assembly 32 is supported on the bearing support assembly 10. Referring to
In the illustrated embodiment of the invention, the upper ring 38 is secured to the upper portion of the turret 16 and the support beams 42 are sufficiently long to allow the lower ring 40 to be secured to the hull 20 near the vertical center of the vessel 14. At this position, the deflections of the lower ring 40 caused by hogging and sagging of the vessel 14 will be significantly reduced compared with the deflections the lower ring would experience if it were secured to the hull 20 closer to the upper ring 38. As a result, the upper ring 38 will also experience reduced deflections, and the upper bearing assembly 32 will therefore remain generally circular. Thus, it may be seen that the bearing support assembly tends to isolate the upper bearing assembly 32 from the distortions of the moon pool 18 which are caused by hogging and sagging of the vessel 14.
The length, number and cross sectional configuration of the support beams 42 will depend on the size of the turret 16 and the anticipated vertical mooring loads that will be transmitted through the upper bearing assembly 32. In addition, the length and cross sectional configuration of the support beams 42 are selected so that they will deflect slightly to allow the turret 16 to pivot about a horizontal axis located near the upper bearing assembly 32 when the turret is subjected to horizontal mooring loads. In an exemplary embodiment of the invention, for example, the support beams 42 may each be constructed of twelve-inch diameter carbon steel tubing and have a length of approximately twenty feet, and a total of twenty four such support beams may be evenly distributed around the bearing support assembly 10.
Referring still to
If as shown in
The lower ring 40 preferably comprises a circular reaction ring 58 and a number of lower ribs 60, each of which is secured to the reaction ring and to the lower end of a corresponding support beam 42. The reaction ring 58 is supported on a conventional moon pool support ring 62 which is attached to the moon pool 18 near the vertical center of the vessel 14. In addition, the bearing support assembly 10 ideally includes a number of radial and axial jack screws 64 and 66, respectively, which are operatively engaged between the hull 20 and/or the support ring 62 on the one hand and the reaction ring 58 on the other hand, to provide a means for aligning the axis of rotation of the upper bearing assembly 32 with the axis of rotation of the lower bearing assembly 34. Once the axes of rotation are properly aligned, the interface between the support ring 62 and the reaction ring 58 may be filled with grout and these two components secured together with, for example, a number of bolts 68 to prevent the separation of the bearing support assembly 10 from the moon pool 18 due to uplift of the turret 16.
In operation of the bearing support assembly 10, the vertical and horizontal mooring loads acting on the turret 16 are transmitted through the upper bearing assembly 32 to the upper ring 38. From the upper ring 38, the mooring loads are transmitted through the support beams 42 to the lower ring 40, and from the lower ring 40 to the hull 20 of the vessel 14. In addition, due to the clearance between the turret 16 and the lower bearing assembly 34, the horizontal mooring loads will cause the turret to pivot about a horizontal axis located near the upper bearing assembly 32. The resulting bending force will be transmitted through the upper bearing assembly 32 to the support beams 42, which will deflect slightly to allow the turret 16 to pivot.
Since the vessel 14 reacts somewhat like a beam in bending, the deflections of the normally circular shape of the moon pool 18 caused by hogging and sagging of the vessel 14 will be minimized near the vertical center of the hull 20. Thus, by mounting the lower ring 40 near the vertical center of the hull 20, the deflections of the lower ring due to hogging and sagging of the vessel 14 will also be minimized. As a result, the upper ring 38 and, thus, the upper bearing assembly 32 will remain relatively circular during operation. In addition, due to the particular construction of the support beams 42, they will deflect slightly to accommodate the pivoting of the turret 16 caused by the horizontal mooring loads and thereby prevent the upper bearing assembly 32 from becoming damaged. Therefore, the bearing support assembly 10 effectively isolates the upper bearing assembly 32 from both the deflections of the vessel 14 and the pivoting of the turret 16.
It should be recognized that, while the present invention has been described in relation to the preferred embodiments thereof, those skilled in the art may develop a wide variation of structural and operational details without departing from the principles of the invention. Therefore, the present application should be construed to cover all equivalents falling within the true scope and spirit of the invention.
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Number | Date | Country | |
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Number | Date | Country | |
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60465092 | Apr 2003 | US |