The invention relates to a device and method for the end termination of a braided synthetic rope that is currently being used in the mooring of any or all offshore drilling, and production facilities, towing and other crane & rigging applications. Moreover the invention relates to a preferably alloy metal termination, or other suitably engineered material, of braided synthetic rope which will enhance the protection of mooring lines and other synthetic rope applications at the end fitting, will reduce installation times in turn reducing costs, and will utilize standard wire rope, and/or chain connectors. The device and method is intended to create a safe and efficient manner to connect objects in the mooring and rigging industry such as other synthetic mooring lines, tow lines, anchor chains, and wire ropes.
The offshore oil production industry, due to the increased demand from the marketplace for oil production, has constantly improved their technology and capabilities to explore and to drill in deeper waters. While ongoing upgrades are taking place on the current drilling fleets the weight increases that they are subjected to because of longer and heavier mooring lines, an alternative innovation solution had to be explored to address these issues. Braided synthetic ropes are being used much more often to replace the heavier more cumbersome steel wire rope thus requiring synthetic ropes to undergo many changes in design and use. The synthetic rope fittings have been large, heavy and cumbersome resulting in long installation times, increased labor hours, and safety concerns for employees. The braided synthetic rope socket of this invention helps to resolve many of these issues. The current method of terminating a synthetic rope with a metal connector requires sending the rope to specialized connector manufacturers for in-house mating of the rope to the specialized socket and is time consuming and expensive. The advantages of the inventive synthetic rope socket is that it can be installed in the field on a braided synthetic rope and fitted with any custom end connection required for terminating the synthetic rope. Due to the design of the braided synthetic rope socket of the present invention there are no sharp or mitered edges to cut or cause abrasions, all corners or edges are rounded to protect the integrity of the synthetic rope.
The inventive synthetic rope socket includes a braided rope tapered solid compression thimble and enclosing tapered socket with screw-on cap used for the end termination of braided synthetic ropes offering 100% efficiency of the tensile strength of the subject synthetic rope and ease of connections. With the design of this apparatus it will allow for quick and efficient field assembly. The design of the apparatus will allow for the connection of synthetic ropes to other devices such as chains, wire ropes, and even other synthetic ropes without the need for intermediate hardware designed for the protection of the synthetic rope. The apparatus also has the capabilities of being customized to fit any connection point with the removable screw-on cap.
It is an object of this invention to provide a device for the end termination of braided synthetic rope, comprising; a tapered solid compression thimble with a rope entry and exit end, a top end, a longitudinal exterior contoured groove with rounded surfaces for the synthetic rope, extending from the rope entry and exit end of the tapered solid compression thimble to the top end of the tapered solid compression thimble, and where the unique surface topography/shape of the tapered solid compression thimble can be described mathematically as a parametric surface with third-order Gaussian geometry; an enclosing thimble socket with a rope entry and exit end, a rope entry and exit end opening with rounded edges at the rope entry end for insertion of the braided synthetic rope and extension through the rope entry end to the rope entry end of the tapered solid compression thimble and folded back and placed in the contoured groove of the tapered solid compression thimble and spliced onto itself, a solid compression thimble entry end a solid compression thimble opening, an internal tapered thimble seat in the enclosing thimble socket to receive the tapered solid compression thimble, internal female threads in the tapered thimble seat at the solid compression thimble entry end with a locking screw mechanism; a screw-on cap having a thimble socket engagement end and a fitting end with external threads at the socket engagement end for threaded engagement with the internal threads in the tapered solid compression thimble seat at the solid compression thimble entry end of the enclosing thimble socket after the tapered solid compression thimble is seated in the enclosing thimble socket; and a socket fitting fixedly attached to the fitting end of the screw-on cap and secured with a locking screw mechanism.
It is also an object of this invention to provide a method for the end termination of braided synthetic rope comprising the steps of: inserting the end of a braided synthetic rope through an enclosing thimble socket with a rope entry and exit end, a rope entry end opening with rounded edges at the rope entry end, said enclosing thimble socket also having a solid compression thimble entry end, an internal tapered thimble seat to receive a tapered solid compression thimble with a longitudinal exterior contoured groove for the synthetic rope and a rope entry and exit end, and internal female threads in the tapered solid compression thimble seat at the solid compression thimble entry end; drawing the end of the braided synthetic rope inserted through the rope entry end opening of the enclosing thimble socket in sufficient length to wrap the braided synthetic rope over and around the tapered solid compression thimble in the contoured groove from the rope entry and exit end over a top end with rounded surfaces and splice onto itself, the unique shape of the tapered solid compression thimble can be described mathematically as a parametric surface with third-order Gaussian geometry designed to transfer the minimum amount of strain onto the braided synthetic rope; splicing the braided synthetic rope onto itself after being wrapped over and around the tapered solid compression thimble in the contoured groove; pulling the spliced synthetic rope to draw and seat the tapered solid compression thimble in the enclosing thimble socket through the solid compression thimble opening at the solid compression thimble entry end, and; at the solid compression thimble entry end of the enclosing thimble socket threading a screw-on cap with a fixed socket fitting, with external threads, and secured with a locking screw mechanism. As an additional step the spliced braided synthetic rope would be wrapped in an anti-chafe material.
It is also an object of this invention to provide a device for the end termination of braided synthetic rope further comprising a screw-on cap with an adjustable externally threaded extension rod to receive an internally threaded clevis jaw and pin end fitting positioned as desired on the extension rod with a lock nut.
It is also an object of this invention to provide a method for the end termination of braided synthetic rope further comprising a screw-on cap with an adjustable externally threaded extension rod to receive an internally threaded clevis jaw and pin end fitting positioned as desired on the extension rod with a lock nut.
For a further understanding of the nature, objects and advantages of the invention, reference should be had to the following detailed description, read in conjunction with the following drawings.
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An alternative embodiment of the tapered solid compression thimble 8 is depicted in
The morphology and structural support of the tapered solid compression thimble 8 differentiate the invention from traditional thimbles. A traditional thimble experiences both compression and tension forces since it supports the rope it is attached to and it is attached via fixtures that are placed through the open body of the thimble to whatever device or fixture that is supporting/providing a load. In contrast, the tapered solid compression thimble 8 of the inventive synthetic rope socket 1 experiences only compressive forces from (a) the downward pressure of the rope along the top of the tapered solid compression thimble 8 and (b) the upward pressure along its lower tapered side 10 from the supporting, enclosing thimble socket 4 where the tapered solid compression thimble 8 rests inside the supporting, enclosing thimble socket 4 on the internal tapered thimble seat 20 at the zone of contact 22.
The strength requirements for lifting accessories, such as shackles and wire rope termination sockets, are well researched, documented and regulated by various surveying societies and industry associations; prime examples commonly used in the mooring & rigging industries include ASME (American Society of Mechanical Engineers), ABS (American Bureau of Shipping), CE (“Conformité Européene”=“European Conformity”) and DNV-GE (“Det Norske Veritas-Germanischer Lloyd”). The metallic components are required to be stronger than the synthetic or metal rope they support. For example metallic terminations covered by the CE standards require conformity with their Machinery Directive 2006/42/EC, including section 4.1.2.5 “Lifting Accessories & their Components;” therein section (d) states “all metallic components . . . must have a working coefficient chosen in such a way to guarantee an adequate level of safety; this coefficient is, as a general rule, equal to 4;”
The strength of the inventive synthetic rope socket sized for a 1.125″-1.25″ synthetic rope has undergone structural finite element analysis with simulated rope tension and a safe working load of 35,000 lbs. in accordance with DNV 2.22 Lifting Appliance standard (June 2013).
In addition to a structural finite element analysis to predict the strength and safety factor of the inventive synthetic rope socket itself, the performance of synthetic rope (the efficacy or performance of the rope) was tested when used in the inventive synthetic rope socket. A prototype socket was tested using 1.0″ Plasma® 12 Strand rope from Cortland®. This type of rope is manufactured from High Modulus Polyethylene fiber (HMPE) and claimed by the manufacturer to be the highest strength synthetic rope available. Synthetic ropes are characterized by their Minimum Breaking Load (MBL) or Minimal Tensile Strength (MTS). MTS's are provided for both the unspliced and spliced rope. From the manufacturer's data sheet, the MTS for 1.0″ Spliced Plasma® 12 Strand is 110,000 lbs.; the MTS for unspliced 1.0″ Plasma® 12 Strand is 122,000 lbs.
A pull test apparatus was designed in accordance with industry practice and calibrated to ASTM-E-4 standards. Using the rope manufacturer's testing methodology, the 1.0″ Plasma® 12 Strand rope was pulled to 55% of the spliced MTS (0.55×110,000=60,500 lbs.) 10 times (ten cycles), allowed to “rest” or cool for 30 minutes and then the rope was pulled to a tension of 110,000 and held for 30 seconds. The tension on the rope was then increased until failure. The 1.0″ Plasma® 12 Strand rope failed at 128,400 lbs. Since this failure was over the 122,000 lbs. MTS of the unspliced rope, the inventive synthetic rope socket allowed the rope to perform well and fail above MTS for both spliced and unspliced rope. On this basis the inventive synthetic rope socket allows the rope to perform at 100% MTS or 100% efficient (based on the formula of Breaking Strength/MTS X100=% Efficiency).
In the present invention the ratio of the diameter D around which the braided synthetic rope 6 of diameter d is bent (D/d) is 1.25, while it is common practice with conventional thimbles to have a D/d of no less than 3. It is generally known that the lower the D/d ratio, the lower the strength/efficiency of the rope. However, the present invention used with HMPE rope and a D/d of 1.25 has tested to 100% MTS.
This application is a Continuation-in-part of application Ser. No. 16/174,990 (the ‘990 application’) filed Oct. 30, 2018, co-owned with the present invention. The '990 application is incorporated here by reference for all purposes, and with respect to all of which the present invention claims priority under United States Patent Law.
Number | Date | Country | |
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Parent | 16174990 | Oct 2018 | US |
Child | 15931475 | US |