The preferred embodiment of the present invention, contemplating a selectively deployable (i.e., retractable) reaction frame for self-elevating platforms utilizing cantilever beams, is described below with reference to the Figures. The utilization and deployment process of the present invention, as utilized in conjunction with a drilling unit, is also illustrated and discussed in detail, herein.
Referring to
As shown, in the retracted position 24, the reaction length of each of the frames is pivoted so that the length of each frame is situated adjacent to the transom, providing a storage position requiring minimal space.
A minimum distance “D” is kept between the jack up vessel 1 and the platform 4, this proximity is required for the cantilever and drill floor to reach out an adequate distance to the drilling template 6, once the platform is elevated above the platform deck 5. As shown, the reaction frames 7, 7′, being situated in their retracted position, allows the jack up vessel 1 to be positioned within the minimum distance “D” required.
Continuing with
The cantilever 15, formed by first 2 and second 2′ longitudinally aligned beams, supporting drill floor 3 are shown stowed, ready to be deployed, and the broken lines show the outline of the cantilever 15 and drill floor 3 at working position where the arrow 25 shown within indicates the deployment movement direction.
In this traditional scenario, (i.e., without the added support of the reaction frames 7, 7′ of present invention), the cantilever beams 2, 2′ transmit the load to the jack up vessel 1, predominantly at points R1 and R2. R1 has a hold down H/D effort where the cantilever beam is pushing upward under load. R2 has a push up effort where the cantilever beams are bearing down under load. Accordingly, R1 & R2 generates a force couple that counteracts the overturning moment of the cantilever beam 2, 2′.
Continuing with
Those support points R3, R3′ project significantly outward of the transom, ideally, for example, approximately one third 35 of the cantilever beam working envelope 34, so as to increase the distance between the reaction points, as well as to generate a more effective force couple, so as to sustain the overturning moment of the cantilever beam 2. As earlier indicated, partial load reaction can be obtained by designing the reaction frames (i.e., auxiliary structure) to share the cantilever beam loading, once a certain, level of deflection has being reached. Partial reaction can be computed for any given support arrangement, where the relation between deflection and load is proportional.
The present invention thereby provides an innovative support arrangement unlike any prior art on a self elevating drilling unit, and defines the basics of the present invention.
The drilling template 6 comprises many ports for well to be drilled through, the shaded ports show the boundary where the cantilever 15 can drill with full rated load under conventional support arrangement (without the use of the reaction frame of the present invention), beyond this limit the rating is reduced.
Once again, an important feature of the present invention is that the reaction frames 7, 7′ are stowable into a compact storage position allowing the vessel to be positioned within the minimum distance D (for example, 5-10 feet, depending upon soil conditions and operator skills) and be raised to the appropriate position for extending of the cantilever above the drilling template 6. (as shown in the above discussed
Further, as shown in
After modification, with the auxiliary stern reaction frames, as shown on 5B, the full load rating can be maintain nearly the entire drilling envelope, 90 percent, and the extremities are reduced to 76 percent only.
As shown in
The upper 41 mount and lower 41′ mounts pivotally engage the upper and lower base supports 50, 50′ via pivot pins 45, 45′, respectively, so as to allow the reaction frame to be pivotally 49, 49′ supported by the vessel. It is noted that the pivot pins 45, 45′ are not designed to support the reaction frame when in use (i.e., the pivot pins in the present configuration are not configured to support added load); rather, the pivot pins are intended for use during storage and deployment, i.e., for pivoted each reaction frame to and from the storage position, as well as retaining each reaction frame in a storage position, adjacent to the transom or other location on the vessel or structure
Formed through the upper mount 41 of the reaction frame and the primary base support 50 on the vessel are bores 51, 51′, respectively, said bores formed in a fashion such that, when the reaction frame RF is pivotally 49′ positioned at its deployed position relative to the transom (as shown in
Because of the incidence of the reaction frame with the bearing surfaces, the load pins are not particularly envisioned for use as a pivot, but rather to place the configuration into a load bearing configuration. Furthermore, to suit specific needs, the load pins may be engineered to have a profile other than cylindrical so as to resist pivoting.
When mounted in the deployed configuration, above, the lower base support 50′ receives loads from the reaction frame transmitted via two forces; the horizontal load 56 and the vertical 57 load, which are met with horizontal 58 and vertical 59 reaction efforts from the hull via bearing surfaces 60, 54. Likewise, the upper base support 50 receives loads from the reaction frame transmitted via two forces, the horizontal 56′ load and the vertical 57′ load, which are met with horizontal 58′ and vertical 59′ reaction efforts from the hull via the installed 48 pivot pin 52 and upper base support 50. The framework is thereby designed to transmit the reaction forces back to the main deck, cantilever support bulkheads, inner bottom and bottom structure.
An attribute or appendage 55 associated with the lower base support 50′ is shown as well, and depending on the loading, this appendage also can be used to transmit some of the vertical load by providing vertical support to the lower mount 41′ at bearing surface 54.
In the preferred embodiment of the present invention, the pivot points are auxiliary and are positioned off center and separate from the load pin, for space conservation, as well as to provide a better incidence between the 2 bearing surfaces at the bottom, where the pivot point is offset from the 2 bearing surfaces (similar to a hinge mechanism).
As earlier indicated, the second end 44′ of the reaction frame is provided with support surface 29. The support surface may include a raised engagement portion 46 which may be formed into the body, or may comprise a separate component, which may be adjustable as to height (i.e., vertically 38 adjustable via threaded engagement 37, for example) or location on the upper edge 43, the support surface formed to engage the underside of the cantilever beam(s), or otherwise engage and support the cantilever structure.
The engagement portion 46 may comprise a bearing surface of, for example, bronze, to provide low friction and corrosion resistance. The engagement portion (also may be referenced as a load pad) ideally will be adjustable to account for cantilever beam deflection under its own weight. A tapered bearing housing mounted on a slope may be provided for this purpose, which bearing housing may be selectively lockable at different positions to adjust the cantilever beam underside.
While the preferred embodiment of the auxiliary support structure of the present invention is shown as pivotal from a stowed to a deployed position, this pivotal operation is shown only as an example, and is not intended to be limiting. For example, other auxiliary support structures may also work in suitable fashion to accomplish the goals of the present invention which could comprise, for example, quick mount units engaging mounting brackets on the transom or other portion of the vessel which may be mounted prior to deploying the cantilever beam, and removed after retracting the cantilever beam, as required.
Further, mechanical devices may be utilized to position the reaction frames, adjust the raised engagement portion 46, or to install or remove the load pins into the system, as required.
The invention embodiments herein described are done so in detail for exemplary purposes only, and may be subject to many different variations in design, structure, application and operation methodology. Thus, the detailed disclosures therein should be interpreted in an illustrative, exemplary manner, and not in a limited sense.