US2456015A - Electrical conductor - Google Patents

Electrical conductor Download PDF

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Publication number
US2456015A
US2456015A US547590A US54759044A US2456015A US 2456015 A US2456015 A US 2456015A US 547590 A US547590 A US 547590A US 54759044 A US54759044 A US 54759044A US 2456015 A US2456015 A US 2456015A
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Prior art keywords
rope
conductor
core
strands
yarns
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US547590A
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Keith L Orser
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Columbian Rope Co
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Columbian Rope Co
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01BCABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
    • H01B7/00Insulated conductors or cables characterised by their form
    • H01B7/04Flexible cables, conductors, or cords, e.g. trailing cables
    • H01B7/043Flexible cables, conductors, or cords, e.g. trailing cables attached to flying objects, e.g. aircraft towline, cables connecting an aerodyne to the ground

Definitions

  • This invention relates to electrical conductors and particularly to a conductor for use in load sustaining structures such as ropes.
  • the primary object of the invention is to provide an electricalconductor unit, such as an insulated wire for telephone circuits which can be used in combination with load sustaining structures or ropes that are elongated when the load is imposed thereon.
  • Another object is to provide a load sustaining structure or rope which has a relatively high elongation and recovery factor with a protected, insulated electrical conductor or telephone line wire which will accommodate itself to the stretching and recovery of said structure.
  • a still further object is to provide an electrical conductor unit especially adapted for incorporation in a load carrying rope. said unit being a counterpart of any of the individual yarns of which the rope is made, so far as concerns the elongation factor inherent in said yarns.
  • ropes having a high elongation and recovery'iactor are,preierably used as tow lines in order to absorb sudden shocks or strains imposed thereon during the take-oil" as well as under various other circumstances. It is also usually the practice to provide for interphone communication between the occupants of the connected power plane and glider planes but considerable dimculty has been experienced in maintaining the line connections between the telephone instruments due to the stretching of the tow lines and the resulting variances in the distance between connected planes.
  • the telephone wires between two connected planes have been "draped or festooned along the tow line and taped or tied to the tow line at longitudinally spaced points so that the slack in the wires between each two points of attachment could compensate for the stretching of the tow line.
  • Rope made 01' nylon has generally been adopted for use as glider tow lines and as rope of this character has a very high elongation factor the loops formed in the testooned wire are quite large and render it diflicult to properly maintain the intercommunication system by reason of the fact that these suspended loops are irequently damaged, especially in the take-ofl oi thepianu and when the tow lines are dropped.
  • One particular form 01 damage to the communication lines is the destruction of their insulation covering which is quickly worn off by abrasion of the iestooned loops.
  • the invention seeks to provide a glider plane tow line provided with insulated telephone line wires that will fully compensate for elongation of the tow line and which. at the same time, will be fully protected against abrasion or other damage under all conditions of usage.
  • Fig. 2 is an enlarged view of one of the line wires
  • Fig. 3 is a detail view illustrating the preferred manner of splicing the present rope when made of nylon and used for towing glider planes.
  • each conductor unit or element is embedded in a strand of the rope, the rope being illustrated as consisting of three strands l0 although the invention is not limited to the use of any particular number of strands.
  • each strand is made of a plurality of spun yarns twisted. to-
  • the yarns will be assumed to be made oi. a multiplicity of nylon" threads or elements spun or twisted into yarns.
  • the direction in which the nylon is twisted in spinning the yarns and the directions in which the yarns are twisted into strands and the strands into ropes are so arranged as to produce a stable rope structure.
  • due to the high degree of stretchability or elongation of the nylon and the ability of the rope to elongate under tension by reason of the twist in its structural elements it has been impossible to satisfactorily combine an electrical conductor or telephone line wire with such a rope, as previously pointed out.
  • the present invention contemplates an electrical conductor unit which possesses substantially the same elongation and recovery factory as is possessed by the yarns of the rope in conjunction with which it is to be used.
  • an electrical conductor unit which possesses substantially the same elongation and recovery factory as is possessed by the yarns of the rope in conjunction with which it is to be used.
  • this conductor unit comprises a core ll around which the conductor wire I! is wrapped and an elastic covering l3 of non-conductive material for insulating the wire. Rubber insulation or other non-conductive material having the necessary elasticity can be used.
  • the core III is preferably made of a multiplicity of filaments of the same material as is used in the rope yarns, in this instance nylon, and these filaments are also preferably spun or twisted into a yarn which constitutes said core. This so-called core has the same degree of twist as the yarn composing the strands l0.
  • the conductor element I2 is composed of a plurality of small wires which are disposed parallel to each other spirally of the core II, asshown.
  • the conductor unit By reason of the parallel, spiral disposition of the several ends of the conductor wire i2 and the spiral arrangement of the nylon filaments of core H, the conductor unit as a whole, including the elastic insulation covering l3, has an elongation and recovery factor substantially corresponding to that of the individual yarns and of the rope itself.
  • this conductor unit is preferably associated with the rope by being incorporated in the strand at a point where it will not be exposed at the surface of the rope. Any point within the interior of the strand will prove entirely satisfactory although the nearer the center of the strands the conductor unit is located, the less the unit will have to elongate and straighten out when the rope is placed under tension and the strands and yarns elongate and tend to untwist.
  • the conductor unit can be located at the geometrical center of the strand, thus constituting a core or center for the strand.
  • the conductor is run into the strand as one of the core yarns, all of which, including the con ductor, are enclosed within and protected by the outer or cover yarns of the strand. This is en tirely feasable because.
  • the conductor unit has an elongation or stretching factor equal to the normal yarns of which the strand is formed and hence the conductor can be substituted, so to speak, for any one of the yarns, However, as indicated, it should be located beneath the surface of the strand so as to insure against it bein damaged by abrasion by surfaces against which the rope may contact. This renders the present rope construction highly adaptable for use as tow-lines for glider planes as there is little, if any, danger of the conductor wires breaking or of the unit as a whole being damaged so that inter-telephonic communication can be maintained between planes under all conditions with maximum efilciency.
  • Conductor units having a nylon core made of .050" diameter with five turns per inch of sixteen #34 wires have been found to give very satisfactory results under actual flying conditions but it will be appreciatedthatthe number of turns. per unit of length, used in wrapping the wire on the core may be varied as the elongation permitted the conductor wires will bear a more or less predetermined relationship to the elongation factor of the core and rope proper.
  • the number of turns, per inch, given the conductor wires may be varied accordingly, a smaller number of turns being required as the elongation factor decreases and a larger number of turns being used as the elongation factor increases. While it is preferred to make core ll of the conductor unit and strands ill of the rope of one and the same material, such practice need not be adhered to strictly so long as the materials used in these two elements possess substantially the same elongation factors. It will also be understood that the number of wires or the size of the wires used for conductor I2 may also be varied. Depending upon the electrical conductivity desired for conductor II, the number of wires can be varied with their size remaining constant or their number can remain constant and their size varied, or both.
  • the present rope made of nylon, with the conductor unit incorporated therein as described, has been used in numerous glider flights and for pur poses of connecting up the conductor wires in these actual flights, the construction illustrated in Fig. 3 has proven highly satisfactory.
  • the end of the tow line is run through a metallic U -shaped thimble H with a tape wrapping it interposed between the rope and thimble to protect against abrasion.
  • the rope is then spliced by inserting or "tucking each strand of the free end of the rope between strands of the rope at a point in advance of the thimble. Four of these tucks are made with eachstrand containing the conductor after which one-half of the yarns in the remaining free ends of the strands are cut off.
  • the conductor wire is then withheld at the exterior of the rope to form leads and the remaining half-portions oi' the strands, indicated at ill, are each inserted between the full strands twice to form what are termed two half-tucks in each one.
  • the unused portions of the half-strands are then cut off with the result that the spliced portion tapers more or less until its diameter substantially corresponds to the normal diameter of the rope.
  • nylon tow line for glider planes has been adopted for pur poses of disclosing the present invention as the latter has been developed in connection with the production of nylon rope but it will be understood that the invention is not limited to this particular type of rope or tow line except as expressly set forth in the appended claims.
  • a stranded rope structure each strand being composed of a plurality of spirally arranged load carrying elements of twisted filaments of stretchable non-metallic material, certain of said strands having an electrical conductor element embedded therein having a core constituted of twisted filaments forming one of said load carrying elements, electrical conducting wire arranged spirally around said core and an elastic non-conductive covering encasing said wire, the twisted filaments forming the core of said conductor elements having elongation and recovery characteristics substantially corresponding to the elongation and recovery characteristics of the twisted filaments forming other load carrying elements of the strands in which said conductor elements are embedded.
  • each strand being composed of a plurality of spirally arranged load carrying elements of twisted nylon filaments, cer tain of said strands having an electrical conductor element embedded therein having a core constituted of twisted nylon filaments forming one of said load carrying elements, electrical conducting wire arranged spirally around said core and an elastic non-conductive covering encasing said wire, the twisted nylon filaments forming the core of said conductor elements having elongationand recovery characteristics substantially correspending to the elongation and recovery characteristics of the twisted nylon filaments forming other load carrying elements 01' the strands in which said conductor elements are embedded.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Ropes Or Cables (AREA)

Description

K. L. ORSER ELECTRICAL CONDUCTOR Dec. 14, 1948.
Filed Aug. 1. 1944.
KEITH ,L. OR53F Patented Dec. 14, 1948 ELECTRICAL CONDUCTOR Keith L. Orser, Auburn, N. Y., assignor to Columbian Rope Company, Auburn. N. Y., a corporation of New York Application August 1, 1944, Serial No. 547,590
2 Claims. (01. 174-69) This invention relates to electrical conductors and particularly to a conductor for use in load sustaining structures such as ropes.
The primary object of the invention is to provide an electricalconductor unit, such as an insulated wire for telephone circuits which can be used in combination with load sustaining structures or ropes that are elongated when the load is imposed thereon.
Another object is to provide a load sustaining structure or rope which has a relatively high elongation and recovery factor with a protected, insulated electrical conductor or telephone line wire which will accommodate itself to the stretching and recovery of said structure.
A still further object is to provide an electrical conductor unit especially adapted for incorporation in a load carrying rope. said unit being a counterpart of any of the individual yarns of which the rope is made, so far as concerns the elongation factor inherent in said yarns.
For instance, in the use oi! glider planes towed by powered planes, ropes having a high elongation and recovery'iactor are,preierably used as tow lines in order to absorb sudden shocks or strains imposed thereon during the take-oil" as well as under various other circumstances. It is also usually the practice to provide for interphone communication between the occupants of the connected power plane and glider planes but considerable dimculty has been experienced in maintaining the line connections between the telephone instruments due to the stretching of the tow lines and the resulting variances in the distance between connected planes. Heretoifore, the telephone wires between two connected planes have been "draped or festooned along the tow line and taped or tied to the tow line at longitudinally spaced points so that the slack in the wires between each two points of attachment could compensate for the stretching of the tow line. Rope made 01' nylon has generally been adopted for use as glider tow lines and as rope of this character has a very high elongation factor the loops formed in the testooned wire are quite large and render it diflicult to properly maintain the intercommunication system by reason of the fact that these suspended loops are irequently damaged, especially in the take-ofl oi thepianu and when the tow lines are dropped.
2 One particular form 01 damage to the communication lines is the destruction of their insulation covering which is quickly worn off by abrasion of the iestooned loops. Specifically, therefore, the invention seeks to provide a glider plane tow line provided with insulated telephone line wires that will fully compensate for elongation of the tow line and which. at the same time, will be fully protected against abrasion or other damage under all conditions of usage.
In the accompanying drawing Figure 1 illustrates a short section of a stranded rope having a plurality of telephone line wires therein;
Fig. 2 is an enlarged view of one of the line wires; and
Fig. 3 is a detail view illustrating the preferred manner of splicing the present rope when made of nylon and used for towing glider planes.
In the embodiment of the invention each conductor unit or element is embedded in a strand of the rope, the rope being illustrated as consisting of three strands l0 although the invention is not limited to the use of any particular number of strands. In accordance with standard rope manufacturing practices each strand is made of a plurality of spun yarns twisted. to-
. gether in strand formation and, for purposes of this disclosure, the yarns will be assumed to be made oi. a multiplicity of nylon" threads or elements spun or twisted into yarns. Also, in accordance with the usual practices of rope manufacture, the direction in which the nylon is twisted in spinning the yarns and the directions in which the yarns are twisted into strands and the strands into ropes are so arranged as to produce a stable rope structure. However, due to the high degree of stretchability or elongation of the nylon and the ability of the rope to elongate under tension by reason of the twist in its structural elements, it has been impossible to satisfactorily combine an electrical conductor or telephone line wire with such a rope, as previously pointed out.
To overcome all the difllculties outlined above, the present invention contemplates an electrical conductor unit which possesses substantially the same elongation and recovery factory as is possessed by the yarns of the rope in conjunction with which it is to be used. In its preferred form,
which is illustrated in Fig. 2, this conductor unit comprises a core ll around which the conductor wire I! is wrapped and an elastic covering l3 of non-conductive material for insulating the wire. Rubber insulation or other non-conductive material having the necessary elasticity can be used. The core III is preferably made of a multiplicity of filaments of the same material as is used in the rope yarns, in this instance nylon, and these filaments are also preferably spun or twisted into a yarn which constitutes said core. This so-called core has the same degree of twist as the yarn composing the strands l0. Usually, the conductor element I2 is composed of a plurality of small wires which are disposed parallel to each other spirally of the core II, asshown. By reason of the parallel, spiral disposition of the several ends of the conductor wire i2 and the spiral arrangement of the nylon filaments of core H, the conductor unit as a whole, including the elastic insulation covering l3, has an elongation and recovery factor substantially corresponding to that of the individual yarns and of the rope itself. In accordance with the present invention, this conductor unit is preferably associated with the rope by being incorporated in the strand at a point where it will not be exposed at the surface of the rope. Any point within the interior of the strand will prove entirely satisfactory although the nearer the center of the strands the conductor unit is located, the less the unit will have to elongate and straighten out when the rope is placed under tension and the strands and yarns elongate and tend to untwist. In some instances the conductor unit can be located at the geometrical center of the strand, thus constituting a core or center for the strand. In other instances where no one yarn is located at the geometrical center, the conductor is run into the strand as one of the core yarns, all of which, including the con ductor, are enclosed within and protected by the outer or cover yarns of the strand. This is en tirely feasable because. as pointed out the conductor unit has an elongation or stretching factor equal to the normal yarns of which the strand is formed and hence the conductor can be substituted, so to speak, for any one of the yarns, However, as indicated, it should be located beneath the surface of the strand so as to insure against it bein damaged by abrasion by surfaces against which the rope may contact. This renders the present rope construction highly adaptable for use as tow-lines for glider planes as there is little, if any, danger of the conductor wires breaking or of the unit as a whole being damaged so that inter-telephonic communication can be maintained between planes under all conditions with maximum efilciency.
Conductor units having a nylon core made of .050" diameter with five turns per inch of sixteen #34 wires have been found to give very satisfactory results under actual flying conditions but it will be appreciatedthatthe number of turns. per unit of length, used in wrapping the wire on the core may be varied as the elongation permitted the conductor wires will bear a more or less predetermined relationship to the elongation factor of the core and rope proper. In other words, if the rope strands and core ll of the conductor are made of a material having an elongation factor different from that of nylon, the number of turns, per inch, given the conductor wires may be varied accordingly, a smaller number of turns being required as the elongation factor decreases and a larger number of turns being used as the elongation factor increases. While it is preferred to make core ll of the conductor unit and strands ill of the rope of one and the same material, such practice need not be adhered to strictly so long as the materials used in these two elements possess substantially the same elongation factors. It will also be understood that the number of wires or the size of the wires used for conductor I2 may also be varied. Depending upon the electrical conductivity desired for conductor II, the number of wires can be varied with their size remaining constant or their number can remain constant and their size varied, or both.
The present rope made of nylon, with the conductor unit incorporated therein as described, has been used in numerous glider flights and for pur poses of connecting up the conductor wires in these actual flights, the construction illustrated in Fig. 3 has proven highly satisfactory. The end of the tow line is run through a metallic U -shaped thimble H with a tape wrapping it interposed between the rope and thimble to protect against abrasion. The rope is then spliced by inserting or "tucking each strand of the free end of the rope between strands of the rope at a point in advance of the thimble. Four of these tucks are made with eachstrand containing the conductor after which one-half of the yarns in the remaining free ends of the strands are cut off. The conductor wire is then withheld at the exterior of the rope to form leads and the remaining half-portions oi' the strands, indicated at ill, are each inserted between the full strands twice to form what are termed two half-tucks in each one. The unused portions of the half-strands are then cut off with the result that the spliced portion tapers more or less until its diameter substantially corresponds to the normal diameter of the rope.
A more or less detailed description of nylon tow line for glider planes has been adopted for pur poses of disclosing the present invention as the latter has been developed in connection with the production of nylon rope but it will be understood that the invention is not limited to this particular type of rope or tow line except as expressly set forth in the appended claims.
What I claim is:
1. A stranded rope structure, each strand being composed of a plurality of spirally arranged load carrying elements of twisted filaments of stretchable non-metallic material, certain of said strands having an electrical conductor element embedded therein having a core constituted of twisted filaments forming one of said load carrying elements, electrical conducting wire arranged spirally around said core and an elastic non-conductive covering encasing said wire, the twisted filaments forming the core of said conductor elements having elongation and recovery characteristics substantially corresponding to the elongation and recovery characteristics of the twisted filaments forming other load carrying elements of the strands in which said conductor elements are embedded.
2. A stranded rope structure, each strand being composed of a plurality of spirally arranged load carrying elements of twisted nylon filaments, cer tain of said strands having an electrical conductor element embedded therein having a core constituted of twisted nylon filaments forming one of said load carrying elements, electrical conducting wire arranged spirally around said core and an elastic non-conductive covering encasing said wire, the twisted nylon filaments forming the core of said conductor elements having elongationand recovery characteristics substantially correspending to the elongation and recovery characteristics of the twisted nylon filaments forming other load carrying elements 01' the strands in which said conductor elements are embedded.
KEITH L. ORSER.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Name Date Verriil Oct. 28, 1890 Number Number Number
US547590A 1944-08-01 1944-08-01 Electrical conductor Expired - Lifetime US2456015A (en)

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Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2593427A (en) * 1945-01-23 1952-04-22 Us Sec War Counterpoise
US2751570A (en) * 1950-10-26 1956-06-19 Aircraft Marine Prod Inc Electrical connector
US2865978A (en) * 1954-08-26 1958-12-23 Bernard E Smith Elastic ropes and cables
DE1089025B (en) * 1951-01-23 1960-09-15 Pirelli General Cable Works Extensible rope with an insulated electrical wire
US3017493A (en) * 1960-01-22 1962-01-16 Pyrexon Ray Company Ltd Heated car seat
US3100240A (en) * 1956-07-17 1963-08-06 John W Schmidt Extensible electric conduit
US3217280A (en) * 1962-11-29 1965-11-09 Thermel Inc Heating element
US3275740A (en) * 1962-07-09 1966-09-27 Gen Electric High temperature insulation for electrical conductors
US3338046A (en) * 1965-12-29 1967-08-29 Cable Covers Ltd Looped wire rope or cable
US4116153A (en) * 1977-04-04 1978-09-26 The United States Of America As Represented By The Secretary Of The Navy Elastic electrically-conductive strain cable
EP0025223A1 (en) * 1979-09-07 1981-03-18 Gebrüder Kesel GmbH & Co. Climbing-rope with core
US4782196A (en) * 1983-11-30 1988-11-01 Maruichi Sangyo Kabushiki Kaisha Composite strand for transmitting electric or optical signals
US4975543A (en) * 1989-06-30 1990-12-04 Sanders Associates, Inc. Energy-absorbing towline with embedded electrical conductors and drogue deployment system including same
US20020177888A1 (en) * 2000-04-26 2002-11-28 Medtronic, Inc. Helix rotation by traction
US20110132660A1 (en) * 2007-10-19 2011-06-09 Geo. Gleistein & Sohn Gmbh Cable with electrical conductor included therein
US20190244724A1 (en) * 2018-02-06 2019-08-08 Intelligence Textile Technology Co., Ltd. Cable device
US20220018064A1 (en) * 2019-02-26 2022-01-20 Richardson Capex, LLC Rope Eye Splice and Systems, Apparatus & Methods for Forming an Eye in a Rope

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US439583A (en) * 1890-10-28 Method of splicing ropes and cables
US571539A (en) * 1896-11-17 Island
GB190811163A (en) * 1908-05-22 1909-03-04 Callenders Cable & Const Co Improvements in Submarine Signalling Cable
GB104401A (en) * 1916-03-17 1917-03-08 British Insulated & Helsby Cables Ltd Improvements in Electric Cables.
US1661102A (en) * 1924-02-28 1928-02-28 Driver Harris Co Ended cord and method of producing the same
US1839698A (en) * 1930-11-14 1932-01-05 John W Novotny Cable splice
US2002739A (en) * 1930-12-05 1935-05-28 Herkenberg Karl Extensible electric conductor
US2175389A (en) * 1934-05-16 1939-10-10 Siemens Ag Electrically conducting whale line
US2313234A (en) * 1940-09-14 1943-03-09 Gavitt Mfg Company Tinsel cord
US2348234A (en) * 1940-06-19 1944-05-09 Jr Richard F Warren Flexible composite rope

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US439583A (en) * 1890-10-28 Method of splicing ropes and cables
US571539A (en) * 1896-11-17 Island
GB190811163A (en) * 1908-05-22 1909-03-04 Callenders Cable & Const Co Improvements in Submarine Signalling Cable
GB104401A (en) * 1916-03-17 1917-03-08 British Insulated & Helsby Cables Ltd Improvements in Electric Cables.
US1661102A (en) * 1924-02-28 1928-02-28 Driver Harris Co Ended cord and method of producing the same
US1839698A (en) * 1930-11-14 1932-01-05 John W Novotny Cable splice
US2002739A (en) * 1930-12-05 1935-05-28 Herkenberg Karl Extensible electric conductor
US2175389A (en) * 1934-05-16 1939-10-10 Siemens Ag Electrically conducting whale line
US2348234A (en) * 1940-06-19 1944-05-09 Jr Richard F Warren Flexible composite rope
US2313234A (en) * 1940-09-14 1943-03-09 Gavitt Mfg Company Tinsel cord

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2593427A (en) * 1945-01-23 1952-04-22 Us Sec War Counterpoise
US2751570A (en) * 1950-10-26 1956-06-19 Aircraft Marine Prod Inc Electrical connector
DE1089025B (en) * 1951-01-23 1960-09-15 Pirelli General Cable Works Extensible rope with an insulated electrical wire
US2865978A (en) * 1954-08-26 1958-12-23 Bernard E Smith Elastic ropes and cables
US3100240A (en) * 1956-07-17 1963-08-06 John W Schmidt Extensible electric conduit
US3017493A (en) * 1960-01-22 1962-01-16 Pyrexon Ray Company Ltd Heated car seat
US3275740A (en) * 1962-07-09 1966-09-27 Gen Electric High temperature insulation for electrical conductors
US3217280A (en) * 1962-11-29 1965-11-09 Thermel Inc Heating element
US3338046A (en) * 1965-12-29 1967-08-29 Cable Covers Ltd Looped wire rope or cable
US4116153A (en) * 1977-04-04 1978-09-26 The United States Of America As Represented By The Secretary Of The Navy Elastic electrically-conductive strain cable
EP0025223A1 (en) * 1979-09-07 1981-03-18 Gebrüder Kesel GmbH & Co. Climbing-rope with core
US4782196A (en) * 1983-11-30 1988-11-01 Maruichi Sangyo Kabushiki Kaisha Composite strand for transmitting electric or optical signals
US4975543A (en) * 1989-06-30 1990-12-04 Sanders Associates, Inc. Energy-absorbing towline with embedded electrical conductors and drogue deployment system including same
US20020177888A1 (en) * 2000-04-26 2002-11-28 Medtronic, Inc. Helix rotation by traction
US7092764B2 (en) * 2000-04-26 2006-08-15 Medtronic, Inc. Helix rotation by traction
US20110132660A1 (en) * 2007-10-19 2011-06-09 Geo. Gleistein & Sohn Gmbh Cable with electrical conductor included therein
US9340924B2 (en) * 2007-10-19 2016-05-17 Helukabel Gmbh Cable with electrical conductor included therein
US20190244724A1 (en) * 2018-02-06 2019-08-08 Intelligence Textile Technology Co., Ltd. Cable device
US10818413B2 (en) * 2018-02-06 2020-10-27 Intelligence Textile Technology Co., Ltd. Cable device
US20220018064A1 (en) * 2019-02-26 2022-01-20 Richardson Capex, LLC Rope Eye Splice and Systems, Apparatus & Methods for Forming an Eye in a Rope

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