Information
-
Patent Grant
-
6566604
-
Patent Number
6,566,604
-
Date Filed
Monday, February 7, 200024 years ago
-
Date Issued
Tuesday, May 20, 200321 years ago
-
Inventors
-
Original Assignees
-
Examiners
- Reichard; Dean A.
- Mayo, III; William H.
Agents
- Wheatcraft; Allen
- Sheets; Eric J
-
CPC
-
US Classifications
Field of Search
US
- 174 120 R
- 174 110 R
- 174 103
- 174 113 R
- 174 47
- 174 116
- 174 1015
- 174 114 R
-
International Classifications
-
Abstract
A cable comprising a stress-bearing matrix extending substantially through the length of the cable; and a plurality of conducting elements extending substantially through the length of the cable, the plurality off the conducting elements being located within and spaced from one another by the stress-bearing matrix, wherein at least one of the plurality of conducting elements is in intimate contact with a low friction liner disposed about at least one of the plurality of conducting elements, and the at least one of the, conducting elements is longitudinally moveable relative to the stress-bearing matrix.
Description
FIELD OF THE INVENTION
This invention relates to cable and to the manufacture of cable. The invention has particular application in cable which is likely to be subject to flexing, radial compression and tensile and shear stresses. Embodiments of the invention are suited for use as ocean bottom cable (OBC).
BACKGROUND OF THE INVENTION
One method of surveying the geology of subsea strata involves laying long lengths (for example 50-60 km lengths) of sensing cable in a serpentine manner on the sea floor; the cable is generally known as ocean bottom cable (OBC). The cable will typically comprise a number of cable sections, for example a 57 km cable may comprise 150 cable sections each of 380 m length, each cable section carrying a number of sensors. Acoustic waves are created in the water above the cable, which waves are reflected at varying amplitudes and angles by the strata beneath the sea floor. The reflected waves are detected by the sensors and the resulting signal output is analyzed to produce a seismograph of the subsurface geology of the area. This method of geological surveying is perhaps most commonly used in identifying subsea hydrocarbon-bearing formations with potential for oil or gas production.
The OBC is laid on the sea floor using a vessel equipped with an arrangement for deploying and retrieving the cable, known as a “linear traction wrench” or “squirter”. Typically, the squirter comprises a plurality of pairs of driven wheels, often shod with vehicle tires, each pair defining a “nip” or “pinch point” for engaging a section of cable. The vessel will follow a serpentine path over the area of sea floor to be surveyed, with the squirter deploying the cable at a corresponding rate. Once the survey has been completed the squirter is operated to retrieve the cable.
Conventional OBC comprises a central reinforcing fiber core, a plurality of elongate components, typcially insulated conductors helically would around the core, an extruded sheath, possible further braided fiber reinforcement, and an outer abrasion resistant protective sheath or jacket. When a section of the OBC passes through the squirter or is subjected to flexing, compressive and longitudinal forces are quickly transferred to the components and may, in time, result in damage to the components. The components of the cable, for example the reinforcing braid, may also shift position within the cable upon flexing. When the cable is next subjected to longitudinal stress, the displaced component may be subject to damage.
As the cable is deployed and retrieved, particularly in deep water, the weight and drag on the cable suspended from the squirter is considerable. Accordingly, the squirter must apply significant compressive and longitudinal forces to the cable. These forces are of course first applied to the exterior of the cable and are then transferred radially inward through the components of the cable to the central core. This may place significant stresses on individual components, increasing the possibility of component failure. One recognized failure mechanism is termed “Z-kinking”, and involves a component being subject to longitudinal forces which stretch the component beyond its elastic limit or “yield point.” When the forces are removed, the elongated component retracts and is folded back on itself, thereby damaging the component. Furthermore, the different components of the cable may behave differently under stress. For example, the overlying extruded sheath or jacket is likely to have greater elasticity than the adjacent layer of helically wound conductors, which may lead to the jacket extending longitudinally relative to the conductor layer. Where such extensions occur rapidly over short sections of cable, as at the squirter during sudden starts or stops or due to pitching and yawing of the vessel, the longitudinally flexing jacket may damage underlying components. Also, such displacement prevents the effective transfer of shear forces from the jacket to the reinforcing core. The sheath will then bear substantially all of the tension applied to the cable by the squirter, possibly leading to premature failure of the jacket and cable. Where the jacket has been pressure extruded over the conductor layer, the jacket's inner profile corresponds to the rope-like surface of the helically wound conductors, such that longitudinal displacement of the jacket relative to the conductor layer may impart considerable localized abrasions and loads upon the conductors. To avoid damage caused by inefficient load transfers as described above, the longitudinal force applied to the cable jacket is typically distributed over longer sections of cable by adding squirter nips. The compressive forces applied at the squirter nips are typically increased, and elaborate controls are sometimes employed to avoid jerking.
In existing OBCs, it is common for voids to remain within the core of the cable. As a result, water pressure will often deform the cable as the atmospheric voids collapse and move within the cable, displacing individual elements within the cable and thus changing the electrical, optical, and/or mechanical characteristics of the elements or cable in general. Such displacements may increase rigidity in regions of the cable, for example, resulting in handling problems and increasing the likelihood of component damage when the cable is retrieved. Displaced air within the cable may also collect in pressurized pockets which breach the outer jacket on retrieval of the cable, allowing water to penetrate into the cable. To avoid problems associated with voids, cables have been filled with oil or other viscous materials with a view to flushing out any trapped air and filling any voids in the cable. Such methods, however, generally have other problems associated with them and are only partially effective. Complete air removal is difficult to achieve, particularly with higher viscosity materials, and lower viscosity fluids require special considerations for filling the cable and may reduce load transfers.
EP-A-O 193 780 discloses a submarine cable for optical fiber telecommunications. The cable has a core comprising armoring of antitorsional rope and a plurality of small tubes wound helically and in direct contact with the armoring. The small tubes loosely house the optical fibers and are filled with a practically incompressible fluid such as a petroleum jelly or a silicon grease.
It is among the objectives of embodiments of the present invention to provide an OBC which obviates or mitigates these difficulties.
It is a further objective of embodiments of the present invention to provide an improved cable containing a plurality of elements in which the elements are protected from stresses and forces applied to the cable.
SUMMARY OF THE INVENTION
According to the present invention there is provided a cable comprising: a stress-bearing matrix extending substantially through the length of the cable; and a plurality of conducting elements extending substantially through the length of the cable, the plurality of said conducting elements being located within and spaced from one another by said stress-bearing matrix, wherein at least one of the plurality of conducting elements is in intimate contact with a low friction liner disposed about the at least one of the plurality of conducting elements and the at least one of the conducting elements is longitudinally movable relative to the stress-bearing matrix.
In use, the provision of the low friction liner disposed about at least one of the conducting elements allows embodiments of the present invention to be designed such that loads are transferred to selected conducting elements at differing rates. This is particularly useful where the elements are fragile or susceptible to stress induced damage, for example optical fibers or small diameter electrical conductors. Further, the flexibility of the cable is improved as relatively inelastic elements, such as metallic conductors, may incur minimal loads over short lengths as the cable flexes. In contrast to the cable configuration disclosed in EP-A-0 193 780, in which optical fibers are loosely housed in tubes, the intimate contact between the conducting element and the liner of the present invention provides the cable with structural stability, that is the conducting element will not move laterally within the liner as the cable experiences stresses and strains; as noted above, displacing individual elements within a cable may change the electrical, optical, and/or mechanical characteristics of the elements or cable in general. Further, the elements and liners of the present invention are more compact, and thus a cable of a given diameter may accommodate a greater number of elements. In addition, locating a liner around an element in accordance with the present invention is likely to be easier, more reliable and thus less expensive than locating an element in a tube and completely filling the tube with a viscous incompressible fluid.
According to another aspect of the present invention there is provided a cable comprising a plurality of elongate conducting elements located within and spaced from one another by a stress-bearing matrix substantially throughout the length of the cable, the cable being non-rigid and bendable in multiple planes.
In use, when a longitudinal stress is applied to cables of embodiments of these aspects of the invention via the jacket of the cable, for example by a squirter arrangement for deploying or retrieving cable, shear forces applied to the outer surface of the jacket are transferred radially inwardly through the cable primarily the matrix. The presence of the matrix material between individual elements significantly reduces the amount of shear forces transferred radially inwardly of the cable via load-sensitive elements, and instead facilitates concentration of said forces on selected load bearing elements within the cable. In testing it has been found that longitudinal forces applied externally to cables in accordance with embodiments of the present invention will transfer to specified load bearing elements within the cable at a rate in excess of ten times that of longitudinal forces applied to a comparable conventional cable. Subsequently, lower longitudinal forces are transferred to selected sensitive elements and at a greatly reduced rate. In addition, the presence of the matrix material surrounding the individual elements allows for more even distributions of compressive forces. Where the cable is utilized as an ocean bottom cable (OBC), these features allow much higher loads to be applied over much shorter squirter lengths than those required for conventional ocean bottom cables.
Preferably, the cable is round. Preferably also, the elements are helically wound, and most preferably the elements are wound around a central axis of the cable.
Preferably also, a plurality of elements are located within respective low friction liners. The low friction liner may be formed of a friction-reducing material, such as expanded polytetrafluoroethylene (ePTFE), to facilitate sliding movement of the element. Other materials which may be used include ethylene-propylene copolymer (EPC), polyester, polyethylene, and fluorocarbon or silicon based materials. Utilizing a porous material, such as ePTFE, to form the liner also allows the matrix-forming material to penetrate into the porous structure to secure the liner to the matrix, thereby helping to maintain the structural integrity of the liner. The low friction liner material may be tape-wrapped around the element or may be in the form of an extruded tube.
Preferably also, the matrix fills substantially all of the space between the elements, and is preferably substantially incompressible. This is useful in applications in which the cable experiences high external pressures, for example where the cable serves as ocean bottom cable (OBC). This feature is also useful in minimizing the risk of damage or deformation of the cable on passing through a cable squirter or other arrangement defining a nip.
The elements may include one or more electrical conductors, one or more optical fibers, one or more force transmission members, and/or one or more fluid transmission conduits for conducting, for example, pressurized gases, hydraulic fluids, exhaust gases or cooling fluids. The electrical conductors may be of copper, silver, or aluminum or alloys/containing these materials.
The electrical conductors may be insulated by any suitable material, such as ePTFE, ethylene-propylene co-polymer (EPC), polyester-based materials such as MIL-ENE® obtainable from W L Gore & Associates, fluorinated ethylene-propylene copolymer (FEP), or polyvinylchloride (PVC).
Each conducting element may comprise a single member, or may comprise a plurality of members, for example a liner may accommodate a quad, that is the conducting element may comprise two pairs of electrical conductors
Preferably also, the cable includes load-bearing reinforcing elements. Typically, the cable will include a central load-bearing core, and may be provided with an outer sheathing of load-bearing elements. The load-bearing core and sheathing elements may be a synthetic or natural strength member and may comprise a fibrous material. The load-bearing core and sheathing elements may be of: aramid fiber, for example KEVLAR® fiber available from DuPont; stainless steel wire; polyamide fibers, such as nylon fibres; or ePTFE fibers such as RASTEX® fibers obtainable from W L Gore & Associates in Putzbrunn, Germany. These elements may be impregnated with materials which are bondable to the matrix material.l.
According to another aspect of the present invention there is provided a method of forming a non-rigid cable which is bendable in multiple planes, the method comprising setting a plurality of elongate elements in spaced relation within a sectable matrix-forming material, and permitting the material to set so that the elements are spaced from one another within the cable by a stress-bearing matrix substantially throughout the length of the cable.
Preferably, the cable is formed by a method including the following steps:
forming a core of said matrix-forming material;
laying elongate elements in circumferentially spaced relation on an outer surface of the core; and
applying matrix-forming material over the elements to form a sheath to cover the elements.
In one embodiment, the elongate elements are laid into the outer surface of the core before the core has set, such that the core surface deforms to accommodate the elements. The matrix forming material may then be applied to fill any remaining spaces between the elements. The core surface may be subject to heating to prevent the material from setting prior to application of the elements. Of course the method of handling the core will be selected for compatibility with the matrix-forming material setting mechanism.
In the preferred embodiment, at least some of the elongate elements are provided with sheaths of matrix-forming material which merge with the other elements of matrix-forming material during processing. This method facilitates accurate placement of the elongate elements within the matrix, particularly when the sum of the diameters of the sheathed elongate elements is equivalent to the circumference of the cable at the centers of the elongate elements.
In a further embodiment, a single stage extrusion process is utilized to form the matrix in a single step. This may be achieved by utilizing a multi-holed extruder tip and profiled die placed at the gathering point of a non-planetary cabler with a rotating take-up. Alternatively, the matrix is formed using a material which sets by means of a mechanism other than cooking, such as a two-part compound or a heat or UV-curable material.
Preferably also, the matrix-forming material is polyurethane, though of course any suitable material may be utilized, including thermoplastic rubber (TPR); polyester (PES); or polyolefins including polyethylene or polypropylene (PP). The core-forming material and sheath-forming materials are the same or similar and will bond to one another.
The modulus of the matrix-forming material may be selected to suit particular applications: a low modulus material would result in a more flexible cable but might not be suitable for use in cable experiencing high pressures and would not be well adapted to transfer load, whereas a higher modulus material would be less flexible but better adapted to withstand pressure and loads.
One or both of the core and the sheath may be extruded.
Preferably also, the matrix-forming material core is formed around a central load-bearing core. The provision of the stress-bearing matrix around the core allows forces applied externally to the cable, for example by a cable squirter, to be more evenly distributed around and effectively transferred to the load-bearing core.
As the elements are isolated from one another within the cable by the matrix, any forces applied or transferred to the elements result in the elements tending to move individually relative to the matrix, rather than as a single composite unit as in conventional cables. This has significant advantages where “takeouts” are provided in a cable, that is when an element, or a portion of an element, sometimes known as a “pig-tail”, is pulled out of the cable for connection to a device, sensor and the like mounted on the cable. In conventional ocean bottom cables, the tendency for the conductor layer to move longitudinally as a unit relative to overlying sheaths increases the risk of the pig-tail being sheared due to movement between the elements and the overlying sheaths. In the present invention, the tendency for such movement is substantially reduced, and as elements will tend to move individually within the cable any movement will follow the helical path of the respective element, substantially reducing the risk of shearing. One practical consequence of this is that the window which is cut in the cable sheath to form the take out may be relatively small in cables according to embodiments of the present invention, as described below.
In conventional cables, the window which is cut in the outer sheath or jacket is generally of the same dimensions as the pig-tail, thus a 7.5 cm pig-tail will result in a 7.5 cm window being cut in the cable sheath or jacket. This will result in the outer reinforcing fibers, typically KEVLAR braid, being cut through at a number of points, weakening the cable. In embodiments of the present invention, the provision of elements isolated and spaced apart by the matrix, and also the use of transparent sheathing, allows an operator to form a pig-tail by cutting or drilling two relatively small holes to intersect the selected element, cutting the element at one hole and then pulling the cut tail of the element through the other hole, It will normally be possible to cut the holes without damaging the outer reinforcing fibers and weakening the cables and to pull the element from the matrix without sustaining damage.
According to a further aspect of the invention there is provided a combination of a cable and a device comprising: a cable with an outer surface and having a stress-bearing matrix extending substantially through the length of the cable, a plurality of conducting elements each extending in a path substantially through the length of the cable and being located within and spaced from one another by said stress-bearing matrix, at least one hole being cut from the outer surface of the cable to a point within said stress-bearing matrix and intersecting the path of at least one of the plurality of conducting elements; wherein at least one of the plurality of conducting elements extends through said at least one hole and is connected to the device.
According to another aspect of the present invention there is provided a method of providing a take out in a cable comprising at least one elongate element extending along a path through the body of the cable and contained within a sheath, the method comprising:
cutting holes at two points in the sheath, the holes intersecting the path of the element;
cutting the element at one hole to form a tail; and
pulling the tail through the other hole.
Preferably, the element is movable relative to the body of the cable and is most preferably provided within a low-friction liner.
Preferably also, the overlying matrix material is selected to be transparent, such that the location of the element and any sensitive overlying elements (for example reinforcing fibers, adjacent elements and the like) within the body of the cable may be ascertained by visual inspection.
BRIEF DESCRIPTION OF THE DRAWINGS
These and other aspects of the present invention will now be described, by way of example, with reference to the accompanying drawings, in which:
FIG. 1
is a diagrammatic sectional view of a cable in accordance with an embodiment of the present invention;
FIG. 2
is a cut-away side view of a section of the cable of
FIG. 1
;
FIGS. 3
to
6
are diagrammatic sectional views of steps in a cable-forming process in accordance with an embodiment of the present invention;
FIG. 7
is a diagrammatic sectional view of a step in a cable-forming process in accordance with a preferred embodiment of the present invention;
FIGS. 8
to
10
are diagrammatic sectional views of steps in a cable-forming process in accordance with another embodiment of the present invention; and
FIG. 11
is a diagrammatic longitudinal sectional view of a combination of a cable and a sensor in accordance with an embodiment of another aspect of the present invention.
DETAILED DESCRIPTION OF THE DRAWINGS
Reference is first made to
FIGS. 1 and 2
of the drawings, which illustrate a cable
8
in accordance with an embodiment of the present invention. The cable
8
comprises an outer sheath or jacket
10
, a continuous load-bearing polyurethane matrix
12
extending throughout the length of the cable and within which are set: a load-bearing central aramid fiber core
14
; a plurality of helically wound elongate elements in the form of insulated conductors
16
; and outer aramid fiber reinforcement in the form of a braid
18
.
The insulated conductors
16
and the core
14
are separated by the matrix
12
, with the matrix extending between the insulated conductors
16
. The insulated conductors
16
are contained within liners
17
and are movable relative to the liners
17
.
Steps in forming at least the inner portion or the cable
10
are illustrated in
FIGS. 3 through 8
of the drawings. The load-bearing fibrous core
14
(
FIG. 3
) is passed through an extrusion die and a core
22
of matrix-forming material
25
extruded over the fibrous core
14
(FIG.
4
). On passing from the die, the core
22
is retained at an elevated temperature by appropriate heaters. The heated core
22
is then passed through a cabling station, where the insulated conductors
16
, In their liners
17
, are pressed into the hot outer surface of the core
22
. The outer surface of the core
22
deforms to accommodate the insulated conductors
16
to form core
26
(FIG.
5
). The core
26
is then passed through a further extrusion die, where a sheath of matrix-forming material
24
is extruded over the core
26
, the material
24
moving into the spaces between the insulated conductors
16
to bond with the core material
22
. The core material
22
and sheath material
24
are then permitted to set, in the process bonding to form the homogeneous matrix
12
and a core
28
(
FIG. 6
) Other layers of material, such as the outer fiber reinforcement
18
and/or overlying jackets
10
may subsequently be applied over the core
28
. The outer jackets
10
and the materials
24
which make up matrix
12
are of the same or similar materials which are bondable with one another, preferably polyurethane.
Reference is now made to
FIG. 7
of the drawings, which illustrates a step in an alternative, and preferred, method of forming the inner portion of a cable in accordance with the present invention. In this method, the heated core
122
is passed through a cabling station, where heated conductors
116
, provided with ePTFE liners
117
and thicker polyurethane sleeves
119
, are pressed into the soft outer surface of the core
122
. A sheath of matrix-forming material is subsequently extruded over the sheathed conductors
116
. The method is preferred as it facilitates location of the conductors
116
around the core
122
: the sum of the diameters of the sheathed conductors
116
is approximately equivalent to the desired circumference of the cable at the centers of the conductors.
In a further embodiment, a single stage extrusion may be utilized, to form the matrix
12
in a single step. This may be achieved by utilizing a multi-holed tip and profiled die placed at the gathering point of a non-planetary cabler with a rotating take-up.
In a still further embodiment the matrix is formed of a two-part polyurethane compound. The compound may be injected onto polyurethane-sheathed components at a cross-head located at the gathering point of a cabler. If required, a polyurethane binder may then be bound around the cable to hold the matrix-forming material in place while the polyurethane compound sets.
Reference is now made to
FIGS. 8
,
9
and
10
of the drawings, which illustrate steps in a cable-forming process in accordance with another embodiment of the present invention. In this example, the cable
208
comprises an outer jacket
210
, a stress-bearing polyurethane matrix
212
extending through the length of the cable and within which are retained: a load-bearing central aramid fiber core or strength member
214
; a plurality of conducting elements in the form of power and sensor quads
216
(that is each element contains two pairs of conductors); and outer braided aramid strength members
218
.
The quads
216
are contained within close-fitting low friction ePTFE liners
217
such that the quads
216
are longitudinally movable relative to the matrix
212
.
The Figures illustrate steps in the formation of the cable
208
,
FIG. 8
showing the cable construction after a star-shaped core
222
of polyurethane has been extruded onto the central strength member
214
, and the quads
216
laid in the grooves
223
defined in the surface of the core
222
. The grooves
223
may extend helically to facilitate bending of the cable, or may extend axially. An inner “jacket”
224
of polyurethane material is then pressure extruded over the core
222
and quads
216
to fill the grooves, as illustrated in
FIG. 9
, the core
222
and jacket
224
setting and bonding to form the substantially homogeneous matrix
212
. The braiding
218
is then applied and the outer jacket
210
extruded onto the matrix
212
, the finished cable being illustrated in FIG.
10
.
This embodiment provides improved component isolation, and the location of the components in the matrix
212
provides excellent load transfer from the outer jacket
210
to the central strength member
214
.
Reference is now made to
FIG. 11
of the drawings, which is a diagrammatic longitudinal sectional view of a combination of a cable and a sensor in accordance with an embodiment of another aspect of the present invention. The cable
308
is of similar construction to the cables described above, comprising a transparent polyurethane outer jacket
310
, a stress-bearing polyurethane matrix
312
, a central strength member
314
, a plurality of helically wound quads
316
, and outer reinforcing aramid braid
318
. The quads
316
are contained within close-fitting low friction ePTFE liners
317
such that the quads
316
are longitudinally movable relative to the matrix
312
.
One of the quads
316
is shown extending through the jacket
310
and braid
318
to connect to a device, in the form of a sensor
350
, mounted on the cable
308
. The illustrated arrangement is utilized for mounting sensors on OBC and the method of forming the “take out” to allow the formation of a connection between the cable
308
and the sensor
350
is described below.
As the jacket
310
is transparent, the quads
316
are visible within the cable
308
, allowing an operator to visually locate a required quad
316
; in the region where the sensor
350
is to be located on the cable
308
, the operator then identifies a point along the length of the required quad
316
where the overlying aramid braid
318
does not obstruct access to the quad
316
. Using a hot (around 250° C.) iron with a blunt tip, the operator then bores through the jacket
310
down to the quad
316
, taking care not to damage or expose any of the braid
318
. The exposed quad
316
is then hooked with a tool, care being taken not to nick neighboring components. The quad
316
is then pulled through the hole
352
formed in the jacket
310
and cut with suitable pair of cutters, ensuring that all components of the quad
316
are cut, including in this example, an aramid strength member and the low friction ePTFE binder
317
. The operator then visually locates a point along the quad
316
approximately 10 cm (four inches) from the cut point in the direction of the cable end connector in which the overlying braid
318
does not obstruct access to the quad
316
. Using the round shaft of the hot iron, the operator then burns a trough
354
in the jacket
310
parallel and above the quad
316
down to just above the aramid braid
318
, and then, with the blunt tip of the iron, bores through the outer jacket
310
down to the quad
316
. Any excess polyurethane is trimmed away, and the trough
354
tapered into the hole
356
, again care being taken not to damage or expose any of the braid
318
.
The loose end or tail of the quad
316
is then slowly pulled through the hole
356
. If the ePTFE binder
317
is damaged, the base of the exposed tail is taped with PTFE pipe tape. A short PTFE tube
358
is then slid over the quad
316
and inserted into the hole
356
. The polyurethane in the area around the base of the tube
358
is then heated with the side of the hot iron and polyurethane-based adhesive applied with a hot melt gun. The free end of the tube
358
is then laid in the trough
354
and adhesive applied from the hot melt gun over the top and sides of the tube
358
to secure the tube
358
to the cable
308
. The hot iron and hot melt gun are then utilised to patch the quad cut hole
352
.
The quad
316
is then terminated as described below (but which level of detail is not shown in the Figure). The quad strength member is tied to an anchor and the anchor attached to the cable with hot melt adhesive such that the strength member exits directly out of the tube
358
. A service loop is then constructed, by threading approximately 5 cm (two inches) of the quad
316
into the tube
358
such that it forms an S-bend inside the tube
358
, and sealing the end of the tube
358
with hot melt adhesive. The quad is then terminated, by slipping a boot seal over each of the individual quad wires and, with a connector locking ring in place, soldering each wire into an appropriate solder cup. Once the solder joints have been cleaned of flux, the boot seals are slid down over the solder cups.
Following cleaning of the area around the takeout, a mold is placed around the takeout and natural polyurethane
360
injected into the mold. On the polyurethane setting, the mold is removed and any excess polyurethane flash removed. The sensor
350
may then be connected to the quad
316
and secured to the cable
308
.
In contrast to existing takeouts, the cables of the present invention permit a takeout to be formed by only removing or forming two small holes on the cable jacket, and without damaging the reinforcing braid. Further, in the present invention, the holes may be resealed, unlike takeouts in existing cables in which a large cutout must be retained to accommodate the relative movement which occurs between the individual conductors and the outer cable jacket.
As will be apparent to those of skill in the art, the composition of the cables described above offer numerous advantages over the prior art cables, including: enhanced ability to transfer longitudinal or shear forces radially through the cable to the load bearing elements; increased resistance to radial compression, whether resulting from fluid pressure or mechanical pressure; absence of contact and abrasion between the elements; and greater isolation of the conductors from forces applied to the cable, thereby retaining flexibility throughout the cable. In addition, problems associated with the movement of component layers relative to overlying layers, such as those encountered in the construction of takeouts and as specifically discussed above, are obviated. The cable also remains flexible and bendable in multiple planes, facilitating handling and increasing the number of dynamic applications in which the cable may be utilized.
Although flexible, the matrix will not tend to deform to any great extent when subject to stress, particularly under longitudinal or shear stresses. Thus, the matrix may transfer forces applied to the exterior of the cables by a squirter to the load-bearing core without substantial deformation, mitigating disruption to the internal cable configuration and damage to the conductors.
It will be clear to those of skill in the art that the above-described embodiments are merely exemplary of the invention, and that various modifications and improvements may be made thereto, without departing from the scope of the present invention. For example, in other embodiments the elongate elements may include optical fibers, force transmission cables or fluid conduits and the liners may be omitted or modified such that there is a predetermined transfer of forces from the matrix to selected elongate elements, which may be useful in reinforcing the cable.
Claims
- 1. A combination of a cable and a device comprising:a cable with an outer surface and a length, said cable having a stress-bearing matrix extending substantially through said length of said cable; a plurality of conducting elements each extending in a path substantially through said length of said cable and being surrounded and spaced apart from one another by said stress-bearing matrix; at least one hole extending from said outer surface of said cable to a point within said stress-bearing matrix and intersecting said path of at least one of the plurality of conducting elements; and, a device attached to said cable; wherein said device is connected of at least one of said plurality or conducting elements through said at least one hole.
- 2. The combination of claim 1, wherein the device is a sensor.
- 3. The combination of claim 1, wherein said at least one of the plurality of conducting elements is in intimate contact with a low friction liner disposed about at least one of the plurality of conducting elements and the at least one of the conducting elements is longitudinally movable relative to the stress-bearing matrix.
- 4. The combination of claim 3, wherein said low friction liner is of expanded polytetrafluoroethylene (ePTFE).
- 5. The combination of claim 3, wherein said low friction liner is of a fluorocarbon material such as PTFE, FEP, or PFA; silicons; graphites; talcs; polyethylenes; polypropylenes; EPC; polyesters; or the like.
- 6. The combination of claim 3, wherein said liner is a crush-resistant tube.
- 7. The combination of claim 1, wherein the cable has a transparent sheath, such that the location of an element within the cable may be ascertained by visual inspection through the sheath.
- 8. The combination of claim 1, wherein the cable further comprises load-bearing reinforcing elements encompassing all of said conducting elements and extending through said stress-bearing matrix wherein said at least one hole passes between said reinforcing elements.
- 9. The combination of claim 8, wherein the reinforcing elements are fibrous.
- 10. The combination of claim 8, wherein said at least one of the plurality of reinforcing elements comprises a reinforcing element and an end of the reinforcing element is anchored to the outer surface of the cable.
- 11. A method of providing a take out in a cable comprising two or more elongate elements extending along a path through a body of the cable, wherein said elongate elements are surrounded and spaced apart from one another by a stress-bearing matrix, and contained within a sheath, the method comprising:cutting holes at two points in an outer circumference or the sheath through at least a portion of the stress-bearing matrix to an element intersecting the holes; and cutting the element at a first one of the holes to form a tall; and pulling the tail through a second of the holes.
Priority Claims (1)
Number |
Date |
Country |
Kind |
9804415 |
Mar 1998 |
GB |
|
PCT Information
Filing Document |
Filing Date |
Country |
Kind |
PCT/IB99/00450 |
|
WO |
00 |
Publishing Document |
Publishing Date |
Country |
Kind |
WO99/45549 |
9/10/1999 |
WO |
A |
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EP |
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Dec 1992 |
FR |
291625 |
Jun 1928 |
GB |
339104 |
Dec 1930 |
GB |
574753 |
Jan 1946 |
GB |
WO 8300564 |
Feb 1983 |
WO |