Bearing system for turret on a vessel
09834282 · 2017-12-05
Assignee
Inventors
Cpc classification
F16C19/507
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B63B35/4413
PERFORMING OPERATIONS; TRANSPORTING
Y10T29/49679
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B63B22/021
PERFORMING OPERATIONS; TRANSPORTING
F16C2326/30
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C2326/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C27/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C2300/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F16C27/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B63B22/02
PERFORMING OPERATIONS; TRANSPORTING
B63B35/44
PERFORMING OPERATIONS; TRANSPORTING
B63B21/50
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A bearing system including a wheel assembly transmitting load to a damping assembly, wherein the wheel assembly is configured to rotate angularly relative to the damping assembly.
Claims
1. A bearing system configured to support rotation of a turret carried by a vessel, the rotation of the turret relative to said vessel being about a substantially vertical turret axis and the turret having a bearing surface, the bearing system comprising: a plurality of bearing assemblies, each of which comprising: a roller in contact with said turret bearing surface; a linkage system configured to transmit force from said bearing surface toward said roller into a supporting structure of said vessel; and a mounting system configured to mount said bearing assembly to said supporting structure, the mounting system including one or more wedge-shaped members shaped to position the bearing assembly with respect to the supporting structure and positioned to transmit force from said linkage system to said supporting structure.
2. The bearing system of claim 1, wherein the bearing assembly is a substantially prefabricated cartridge-type subassembly configured for installation and/or removal from said supporting structure.
3. The bearing system of claim 2, wherein said prefabricated subassembly is fastened to said supporting structure using no more than ten bolt fasteners.
4. The bearing system of claim 1, wherein said linkage system comprises a compression spring system configured to allow movement of said roller in a direction perpendicular to the bearing surface.
5. The bearing system of claim 4, wherein said linkage system is configured such that when the spring system is not compressed to a maximum position, force from the bearing surface towards the roller passes through the spring system into a spring end piece, and when the spring system is compressed to the maximum position, further force from the bearing surface towards the roller passes directly through the linkage system to said supporting structure without increasing a load on the spring end piece.
6. The bearing system of claim 4, wherein the linkage system comprises one or more linkage elements configured to allow freedom of movement of linkage elements in directions parallel to the turret bearing surface.
7. The bearing of claim 1, wherein said bearing surface faces downwards and said bearing assemblies are axial bearing assemblies.
8. The bearing system of claim 1, wherein said bearing surface is an outer annular rail secured about an outer circumference of said turret and said bearing assemblies are radial bearing assemblies.
9. The bearing system of claim 1, wherein said roller includes an outer roller surface configured to contact the bearing surface and said outer roller surface is curved in a direction parallel to a central rotating axis of the roller.
10. The bearing system of claim 1, wherein said mounting system comprises one or more slidably mating thread-free mounting elements configured to restrain movement of at least a front portion of said bearing assembly with respect to said supporting structure.
11. The bearing system of claim 10, wherein said slidably mating thread-free mounting elements include one or more tongue elements protruding from an outer housing of the bearing assembly that are configured to mate with one or more groove elements on said supporting structure.
12. The bearing system of claim 1, wherein said vessel is configured to receive hydrocarbons produced from subsea subterranean reservoirs.
13. The bearing system of claim 12, wherein the vessel is a floating production, storage and offloading vessel.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The subject disclosure is further described in the detailed description which follows, in reference to the noted plurality of drawings by way of non-limiting examples of embodiments of the subject disclosure, in which like reference numerals represent similar parts throughout the several views of the drawings, and wherein:
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DETAILED DESCRIPTION
(12) The particulars shown herein are by way of example and for purposes of illustrative discussion of the embodiments of the subject disclosure only, and are presented in the cause of providing what is believed to be the most useful and readily understood description of the principles and conceptual aspects of the subject disclosure. In this regard, no attempt is made to show structural details of the subject disclosure in more detail than is necessary for the fundamental understanding of the subject disclosure, the description taken with the drawings making apparent to those skilled in the art how the several forms of the subject disclosure may be embodied in practice. Further, like reference numbers and designations in the various drawings indicate like elements.
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(14) Vessel 112 can be exposed to substantial wind, current and wave influences. When harsh wind and wave impact occurs on vessel 112, the turret 110 is pressed against the radial turret bearings, which form part of the bearing system 120. In many designs a certain amount of radial flexibility on the bearing system 120 is highly beneficial to accommodate such movements along with the vessel's hog, sag and ovality/tolerances. Such radial flexibility ensures that the distribution of the radial loads is taken on many wheels, rather than overloaded on any one or two wheels.
(15) According to some embodiments, bearing system 120 includes a plurality of wheel bearing cartridges to support rotatable turret 110 on FPSO 112 that allow the FPSO 112 to weathervane 360° around vertical turret axis 114, as shown by the dotted arrows. Risers 130 and the anchor chains 132 are locked to the lower part of turret 110. According to some embodiments, rotating turret 110 is also used to supply umbilical 136 to subsea system 134 which can be, for example, a subsea pump and/or compressor.
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(18) As shown in
(19) A spring shaft 306 is placed behind the wheel and is also fixed on the top and bottom to the box 304. A first spherical bearing 307 and a rod end 308 are placed on the spring shaft 306. The first spherical bearing 307 is fixed vertically in the inner box 304 by two thin pipes 309. In this example, one of the pipes 309 is placed over the first spherical bearing 307 and the other is placed below bearing 307.
(20) According to some embodiments, the rod end 308 is fastened and/or threaded to a damping assembly via a spring rod 310. A second spherical bearing 311 is placed on the back end of the spring rod 310. The second spherical bearing 311 is fixed in a spring housing lid 312 and a cover 313. The cover 313 can be fastened to the spring housing lid 312, for example, by bolts 314. The spring housing lid 312 can be fastened to a spring housing 315 by bolts 316. According to some embodiments, the damping assembly 330 includes a number of disc springs 317 that are placed on the spring rod 310. The disc springs 317 can be arranged in any of a number of different ways on the spring rod 310 depending on the purpose as will be known by one skilled in the art. Alternatively, different disc types (e.g. differing in thickness, shape and/or material) can also be combined on the same rod assembly 310. The disc springs 317 and spring rod 310 can be designed to be preloaded or not, depending on the particular application. According to some alternative embodiments to disk springs 317, conventional compression springs, elastomers or different combinations of these three types can be used. According to some alternative embodiments, the damping system 330 might comprise a piston rod (instead of the spring rod 310) and use hydraulics to obtain and/or apply loads so to exert damping effect. The spring housing 315 is fastened to an outer housing 318 by, for example, bolts 319.
(21) In the example shown in
(22) According to some embodiments, the outer housing 318 has in front a tongue and groove interface to the ship structure to take vertical and side forces of the turret, as will be described in further detail, infra.
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(24) Referring to
(25) In the described embodiments, the horizontal load from the wheel/spring system is going via the outer housing 318 and then through a pair of wedge assemblies (422 and 420) into the cartridge support structure 116. This reduces the need for vertical fastening bolts. Furthermore, the few vertical fastening bolts that are used are not exposed to any large shear forces. The main wedges 420 have sloped interfaces 424 to the cartridge support structure 116, making it easy to make fine adjustments in the horizontal position of cartridge system 210, by moving the wedges 420 up or down.
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(32) After the rough position of bearing cartridge 210 on support structure 620 is made, the wedge assemblies are installed, according to some embodiments. According to some embodiments, the wedge assembly includes a wedge support 422, one or more shim plates 1037 (for larger adjustments), a main wedge 420, a bolt plate 1039, bolts 1040 and nuts 1041. The main wedges 420 have slotted (or oblong) boltholes and a slope interface surface which engages the rear edge of holes 950 of support structure 620. The radial placement of the cartridge 210 can be finely adjusted by moving the main wedges 420 up or down before the final tightening of all the fastening parts. Heavy radial (and lateral) loads onto the bearing cartridge 210 from the turret 110 in operation will mainly pass through the outer housing 318, then into the lower part of the wedge assemblies and then into the support structure 620 and deck/ship walls in surrounding vessel structure 116. In this way, the vertical bolts 630 do not take any large sheer forces.
(33) According to some embodiments, the described bearing system allows relatively rough internal tolerances and alignment features for the inner parts of the bearing cartridge. The cartridge can be pre-mounted and/or the spring system preloaded. The cartridge-type mounting in the vessel allows for quick and easy mounting and/or dismounting in the vessel. The design also allows for easy fine-tuning of the radial position of the bearings in the vessel. The radial forces are transferred from bearing cartridge to vessel via wedges, with no large shear forces placed on interface bolts. The tongue-and-groove-type interface between the ship structure and the front end of the bearing cartridge are configured to take vertical forces and lateral forces while using very few interface bolts. The system described is thus also configured for easy inspection and/or lubrication of the wheels and turret rail.
(34) While the subject disclosure is described through the above embodiments, it will be understood by those of ordinary skill in the art that modification to and variation of the illustrated embodiments may be made without departing from the inventive concepts herein disclosed. Moreover, while the preferred embodiments are described in connection with various illustrative structures, one skilled in the art will recognize that the system may be embodied using a variety of specific structures. Accordingly, the subject disclosure should not be viewed as limited except by the scope and spirit of the appended claims.