US3899991A - Weather resistant segmented fairing for a tow cable - Google Patents

Weather resistant segmented fairing for a tow cable Download PDF

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US3899991A
US3899991A US425434A US42543473A US3899991A US 3899991 A US3899991 A US 3899991A US 425434 A US425434 A US 425434A US 42543473 A US42543473 A US 42543473A US 3899991 A US3899991 A US 3899991A
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fairing
tow cable
sections
tow
cable
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US425434A
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Clarence K Chatten
Saul A Eller
Reece Folb
Arthur P Brisbane
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US Department of Navy
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US Department of Navy
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B21/00Tying-up; Shifting, towing, or pushing equipment; Anchoring
    • B63B21/56Towing or pushing equipment
    • B63B21/66Equipment specially adapted for towing underwater objects or vessels, e.g. fairings for tow-cables
    • B63B21/663Fairings

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  • ABSTRACT A weatherand ozone-resistant elastomeric fairing for a tow cable comprising a plurality of sections using butyl synthetic rubber (Buty1-O35) as the base polymer. Each section of the fairing is independently suspended and attached to the tow cable by fairing support rings and yokes by means of clips.
  • the material for the fairing sections is fabricated with Buty1-O35 as a base polymer and using different amounts of Elastopar, SAF black, zinc oxide, stearic acid, dioctyl sebacate, sulfur, methyl tuads, and captax to give the fairing sections weather resistant properties.
  • This invention relates to faired cables adapted for use in guiding both towed and self-propelled or maneuverable submerged devices and more particularly to a weather resistant segmented fairing for a tow cable for a variable depth sonar system and the like.
  • variable depth sonar is used to achieve sonar transducer at variable depths in water depending upon water conditions in order to achieve greater ranges of operation. Furthermore, quenching is eliminated and the sonar transducer can deliver much greater power to the water.
  • VDS variable depth sonar
  • towed variable depth sonar devices have been developed which may be towed behind a ship by means of a tow cable.
  • the tow cable provides a mechanical connection with the ship as well as electrical connections to the sonar transducers.
  • Such tow cables are normally circular in cross-section and they cause considerable turbulence when drawn through water, causing cable drag and consequent loss of depth of the VDS.
  • the weatherand ozone-resistant, segmented butyl rubber fairing for a tow cable of the present invention comprises a plurality of sectional pieces fabricated from Butyl035 as the base polymer and different amounts of Elastopar, SAF black, zinc oxide, stearic acid, dioctyl sebacate, sulfur, methyl tuads, and captax to give them ozoneand weather-resistant properties.
  • Butyl035 is a specific type of rubber. made by a number of manufacturers, wherein O35 refers to the specific amount of unsaturation for curing.
  • Each of the sectional pieces is hung from a yoke which is supported by a nylon thrust washer resting on a fairing support ring.
  • Each support ring is vulcanized to the tow cable.
  • the remainder of the fairing is held in proper position behind the tow cable by evenly spaced I rings or clips.
  • the yoke and the clips have sufficient clearance around the tow cable to allow the yoke and the entire length of the fairing to swivel freely around the tow cable. This ability of the fairing to swivel and hence to align itself helps the faired tow line to be nonkiting in service.
  • the rubber fairing sections are in the form of a streamlined shape, each section comprising an elastomeric section of a medium hardness leading edge and a soft trailing edge, a Dacron reinforced strength member, and an antichaffing ply.
  • One object of this invention is to have a faired cable for maintaining a VDS at a desired depth.
  • Another objectof this invention is to have a faired tow cable which is non-kiting in service.
  • Still another object of this invention is to have a segmented flexible fairing for a tow cable in short supported sections rather than of one continuous length to avoid bunching and buckling of the tow cable.
  • Still another object of this invention is to have a plurality of flexible fairing sections which are individually suspended and are not articulated to prevent contact.
  • Still another object of this invention is to have a plurality of fairing sections wherein each section is free to seek its own position in the free stream behind the tow cable.
  • Still another object of this invention is to make a segmented flexible fairing which is ozone-and weatherresistant.
  • Still another object of this invention is to have a plurality of flexible sectional fairing pieces wherein each section has leading and trailing edges made of butyl rubber compounds which are tail-light in sea water so that the fairing into which the compounds are vulcanized floats up behind the tow cable.
  • FIG. 1 is a perspective view of a tow cable having a segmented flexible fairing
  • FIG. 2 is a magnified view of a tow cable having a segmented fairing showing details of a yoke and a ring or clip used for securing a fairing section to the tow cable.
  • FIG. 10 shows a perspective view of a weather-and ozone-resistant segmented fairing.
  • a tow cable 12 has a plurality of fairing sections such as 14 attached to it.
  • Fairing section 14 comprises a streamlined fairing piece 16 having a relatively soft trailing edge 18 and a tough, medium hardness leading edge 20.
  • the trailing edge 18 has low specific gravity which is lower than that of sea water (i.e., less than L025), low shore durometer A hardness, low modulus at percent elongation, high tensile and high tear strength, low volume swell in water, good low temperature flexibility, and
  • Each fairing section is connected to tow cable 12 by means of a yoke 22 and a plurality of rings or clips such as 24 and 26. Each fairing section is independent of the motion of other fairing sections attached to the tow cable.
  • FIG. 2 shows attachment of a yoke such as shown in FIG. 1 by numeral 22 and a plurality of rings or clips, preferably evenly spaced on the tow cable, such as shown by numerals 24 and 26 in FIG. 1.
  • Cable 12 is shown in FIG. 2 by fathom lines.
  • Clip 26, its sleeves 28 and 30, screws 32 and 34, and corresponding nuts 36 and 38 are preferably made of No. 316 stainless steel. However, other similar materials may be substituted for stainless steel in the fabrication of these parts and the subsequent parts without deviating from the teachings of the subject invention.
  • Yoke 22 is supported on a nylon thrust washer resting on a fairing support ring 37.
  • the yoke is designed to straddle the support ring 37 in region 39.
  • the support ring 37 is preferably made of No. 18 gage, No. 316 stainless steel strip about 2 inches by inches, and is vulcanized to the tow cable by a Nitrile Rubber layer having composition as discussed be low.
  • a portion of the tow cable of width slightly greater than the width of the support ring is wire brushed; degreased by means of a solvent such as xylene or acetone; dried with cold air, painted with a phosphoric acid mixture (80 percent by volume) for about one minute, rinsed with water and dried with cold air thereafter.
  • the cleaned work area on the tow cable is then painted with a smooth coat of an adhesive such as Thixon P-4 or the like and allowed to dry for at least half an hour.
  • the uncured Nitrile Rubber is then slipped inside the pre-cleaned support ring and any rubber extending the surface of the support ring is removed.
  • the support ring with the rubber is then slipped over the already prepared section of the tow cable and squeezed thereon.
  • the tow cable and the support ring are then treated in a mold preheated to 307F and a pressure of 24,000 pounds is applied for minutes.
  • the excess rubber flashing is then removed and the seam of the support ring is carefully tack welded without burning a hole therein.
  • the weld is ground to match the surface of the support ring.
  • Yoke portion 40 of yoke 22 is attached to its insert 42 by two screws 44 and 46 which are preferably two No. 10-32 flat head screws passing through respective pairs of holes 48, 50 and 52, 54 provided with mating nuts which come flush with the yoke surfaces.
  • Yoke portion 40 is attached to the fairing piece 16' by means of screw 56, preferably a No.
  • Clip or ring 26 has its upper portion 58 mated with the tow cable 12 with its lower ears 60 and 62 in contact with opposite sides of the fairing section 64. Screws 32 and 34, together with the respective sleeves 28 and 30 and the respective nuts 36 and 38, are used to connect lower ears 60 and 62 of ring or clip 26 with fairing section 64.
  • Sleeve 28 is inserted through holes 66 and 68 in ring or clip 26 and screw 32 is passed through the sleeve 28 and is used together with nut 36 to fasten the ring or clip 26 to the fairing section 64.
  • FIG. 2 also shows a magnified view of yoke 22 to be attached to tow cable 12.
  • Yoke portion 40 of yoke 22 is placed in position over tow cable 12.
  • Insert 42 is attached to the fairing piece 16'.
  • Holes 48 and 50 in yoke portion 40 are lined up with the respective holes in insert 42, holes 52 and 54, and 74 and 76 in yoke portion 40 are lined with the respective holes in insert 42.
  • each fairing section has a yoke and insert section attaching the fairing section to the tow cable and a series of rings or clips, preferably evenly spaced, attaching the fairing section to the tow cable. There is enough clearance between the tow cable and the yoke and rings which enables the fairing to rotate about the tow cable freely.
  • the requirements for the material to be used for preparing various sections of the fairing are such that it will reduce galloping of the tow line, i.e., mechanical and hydromechanical characteristics of a tow line make the tow cable to be unstable like a telephone wire strumming in wind; kiting, i.e., the tow line experiencing side forces which bring about a sideway motion of the tow line; and buckling, i.e., instability resulting from the fact that stresses developing in the trailing edge are greater than stresses developing in leading edge if the material out of which a fairing section is made is of uniform density.
  • specific gravity of the material out of which trailing edge portion of each of the fairing sections is made should have specific gravity lower than that of sea water, i.e., 1.025, good weather-and ozone-resistant properties, low shore durometer A hardness, low modulus at percent elongation, high tensile and high tear strength, low volume swell in water and good low temperature flexibility.
  • a new material is developed, preferably using Butyl-035 as a base polymer and using a Super Abrasion Furnace black (i.e., SAF black) such as Philblack-E made by Phillips Petroleum, Rubber Chemical Division.
  • SAF black is used as a reinforcing agent to give the material tensile properties for reinforcement and its opacity prevents deterioration of the material by sunlight.
  • a peptizer such as Elastopar (i.e., 33.3 percent Ingredients Parts by weight Butyl-O35 100 Elastopar Philblack-E (SAF) Zinc Oxide Stearic Acid Dioctyl Scbacate Sulfur Methyl Tuuds Captax COMPOSITION OF LEADING EDGE OF FAIRING SECTIONS
  • the requirements for the medium hard leading edge compound are found to be low specific gravity, medium shore A durometer hardness, high modulus at 100 percent elongation, high ultimate tensile strength, high tear strength, low volume swell in water, good low temperature flexibility, and good weather resistance.
  • the composition of leading edge compound satisfying above-described properties is preferably found to have the following composition:
  • a segmented fairing blank is made of raw, i.e., uncured, pieces of the respective butyl-rubber compounds, a Dacron strength member along the leading edge and an antichaffing ply of nylon along the exterior portions of the leading edge.
  • the blank measures a certain length depending upon the length of the mold cavity and is roughly shaped to conform to the cavity.
  • the raw rubber blanks for fairing sections are so cut and arranged that the leading edge portion is preferably about one inch wide while the remaining trailing edge portion is preferably 4.5 inches wide.
  • the strength member is composed of preferably six or more plies of Dacron reinforcement for a total width of at least 0.25 inch.
  • Captax Z-Mercaptobenzo- .thiazole
  • sulfur is then added and the stock is cut and refined on the mill and is sheet-off to a thickness of 3/16 inch. Curing time is 10 minutes at 307F. The total mill-mixing time is about 25 minutes.
  • leading edge compound and trailing edge compound are made out of materials using Butyl- 035 as a base polymer and Nitrile Rubber for vulcanizing support rings to the tow cable is made using Hycar 1042 as the base polymer.
  • Fairing sections are attached to the tow cable using a yoke-insert arrangement and a series of clips or rings. Each fairing section is independent of the other fairing sections attached to the cable.
  • a tow cable having fairing sections attached thereto is free of galloping, kiting and buckling.
  • a towing system for a variable depth sonar comprising:
  • a substantially long tow cable means for securing a plurality of spaced fairing sections to said tow cable, said plurality of fairing sections having an axis of symmetry substantially normal to the longitudinal axis of said tow cable and having longitudinal axis substantially parallel to the longitudinal axis of said tow cable, each of said plurality of fairing sections having a leading edge and a trailing edge; a plurality of support rings vulcanized to said tow cable along the longitudinal axis thereof; a plurality of clips connected to said tow cable and to said plurality of fairing sections; and the trailing edge of each of said plurality of fairing sections being made from a first butyl rubber compound essentially of the following ingredients:
  • each of said plurality of fairing sections is made from a second butyl rubber compound essentially consisting of the following ingredients:

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Ropes Or Cables (AREA)

Abstract

A weather- and ozone-resistant elastomeric fairing for a tow cable comprising a plurality of sections using butyl synthetic rubber (Butyl-035) as the base polymer. Each section of the fairing is independently suspended and attached to the tow cable by fairing support rings and yokes by means of clips. The material for the fairing sections is fabricated with Butyl-035 as a base polymer and using different amounts of Elastopar, SAF black, zinc oxide, stearic acid, dioctyl sebacate, sulfur, methyl tuads, and captax to give the fairing sections weather resistant properties.

Description

United States Patent [191 Chatten et a1.
[ WEATHER RESISTANT SEGMENTED FAIRING FOR A TOW CABLE [75] Inventors: Clarence K. Chatten, Mesa, Ariz.;
Saul A. Eller, Whitestone, N.Y.; Reece Folb, Laytonville; Arthur P. Brisbane, Gaithersburg, both of Md.
[73] Assignee: The United States of America as represented by the Secretary of the Navy, Washington, DC.
[22] Filed: Dec. 17, 1973 21 Appl.No.:425,434
[52] U.S. CL... 114/235 F; 114/235 F [58] Field of Search 254/135 R, 190 R; 1 14/235 F [56] References Cited UNITED STATES PATENTS 3,224,406 12/1965 Clark 114/235 F 3,343,516 9/1967 Nichols et a1. 114/235 F 1 Aug. 19, 1975 3,407,777 10/1968 Anastasio ct a1. 114/235 F 3,443,020 5/1969 boshigian 114/235 F 3,467,047 9/1969 Chatten et a1 1 14/235 F Primary blraminer-R0bert J. Spar Assistant Examinerl(enneth Noland Attorney, Agent, or FirmRichard S. Sciascia; Arthur A. McGill; Prithyi C. Lall [5 7] ABSTRACT A weatherand ozone-resistant elastomeric fairing for a tow cable comprising a plurality of sections using butyl synthetic rubber (Buty1-O35) as the base polymer. Each section of the fairing is independently suspended and attached to the tow cable by fairing support rings and yokes by means of clips. The material for the fairing sections is fabricated with Buty1-O35 as a base polymer and using different amounts of Elastopar, SAF black, zinc oxide, stearic acid, dioctyl sebacate, sulfur, methyl tuads, and captax to give the fairing sections weather resistant properties.
2 Claims, 2 Drawing Figures WEATHER RESISTANT SEGMENTEI) FAIRING FOR A TOW CABLE STATEMENT OF GOVERNMENT INTEREST The invention described herein may be manufactured and used by or for the Government of the United States of America for governmental purposes without the payment of any royalties thereon or therefor.
BACKGROUND OF THE INVENTION This invention relates to faired cables adapted for use in guiding both towed and self-propelled or maneuverable submerged devices and more particularly to a weather resistant segmented fairing for a tow cable for a variable depth sonar system and the like.
A variable depth sonar is used to achieve sonar transducer at variable depths in water depending upon water conditions in order to achieve greater ranges of operation. Furthermore, quenching is eliminated and the sonar transducer can deliver much greater power to the water. In order to maintain the position of a variable depth sonar, hereinafter referred as VDS, at a preselected depth, towed variable depth sonar devices have been developed which may be towed behind a ship by means of a tow cable. The tow cable provides a mechanical connection with the ship as well as electrical connections to the sonar transducers. Such tow cables are normally circular in cross-section and they cause considerable turbulence when drawn through water, causing cable drag and consequent loss of depth of the VDS. One way to overcome this turbulence is to change the shape of the cable by attaching a fairing which streamlines the overall shape of the cable. Continuous fairings have been used for this purpose. However, if such tow cables are canted at an angle to the towing direction, a lateral thrust is developed which causes excessive motion of the towed VDS in the form of side-to-side oscillations or changes in depth of the VDS. Sectional plastic fairing which is streamlined has also been tried wherein individual pieces are held in proper position by aligner rods. However, in service, sectional plastic fairings are subject to column action, i.e., the towing forces cause the fairing sections to stack one against the other which prevents them to rotate freely around the tow cable and align themselves directly behind the tow cable. This column action causes the tow line to kite either to the port or starboard side and prevents the VDS from staying directly behind the ship as required by service conditions. In addition, the serviceability of the tow line has been poor due to frequent breakage of aligner rods and sectional plastic tail pieces, especially when the tow line is used at high sea states. Thus it is desirable to have a reliable tow cable which will maintain the VDS at desired depths without frequent breakdowns in the service.
SUMMARY OF THE INVENTION The weatherand ozone-resistant, segmented butyl rubber fairing for a tow cable of the present invention comprises a plurality of sectional pieces fabricated from Butyl035 as the base polymer and different amounts of Elastopar, SAF black, zinc oxide, stearic acid, dioctyl sebacate, sulfur, methyl tuads, and captax to give them ozoneand weather-resistant properties. It is to be noted that Butyl035 is a specific type of rubber. made by a number of manufacturers, wherein O35 refers to the specific amount of unsaturation for curing.
Each of the sectional pieces is hung from a yoke which is supported by a nylon thrust washer resting on a fairing support ring. Each support ring is vulcanized to the tow cable. The remainder of the fairing is held in proper position behind the tow cable by evenly spaced I rings or clips. The yoke and the clips have sufficient clearance around the tow cable to allow the yoke and the entire length of the fairing to swivel freely around the tow cable. This ability of the fairing to swivel and hence to align itself helps the faired tow line to be nonkiting in service. The rubber fairing sections are in the form of a streamlined shape, each section comprising an elastomeric section of a medium hardness leading edge and a soft trailing edge, a Dacron reinforced strength member, and an antichaffing ply.
One object of this invention is to have a faired cable for maintaining a VDS at a desired depth.
Another objectof this invention is to have a faired tow cable which is non-kiting in service.
Still another object of this invention is to have a segmented flexible fairing for a tow cable in short supported sections rather than of one continuous length to avoid bunching and buckling of the tow cable.
Still another object of this invention is to have a plurality of flexible fairing sections which are individually suspended and are not articulated to prevent contact.
Still another object of this invention is to have a plurality of fairing sections wherein each section is free to seek its own position in the free stream behind the tow cable.
Still another object of this invention is to make a segmented flexible fairing which is ozone-and weatherresistant.
Still another object of this invention is to have a plurality of flexible sectional fairing pieces wherein each section has leading and trailing edges made of butyl rubber compounds which are tail-light in sea water so that the fairing into which the compounds are vulcanized floats up behind the tow cable.
Other objects, advantages and novel features of the invention will become apparent from the following detailed description of the invention when considered in conjunction with the following drawings wherein:
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a perspective view of a tow cable having a segmented flexible fairing; and
FIG. 2 is a magnified view of a tow cable having a segmented fairing showing details of a yoke and a ring or clip used for securing a fairing section to the tow cable.
DESCRIPTION OF A PREFERRED EMBODIMENT Referring to the drawings wherein like reference characters designate identical or corresponding parts in -various figures, and more particularly to FIG. 1 thereof,
numeral 10 shows a perspective view of a weather-and ozone-resistant segmented fairing. A tow cable 12 has a plurality of fairing sections such as 14 attached to it. Fairing section 14 comprises a streamlined fairing piece 16 having a relatively soft trailing edge 18 and a tough, medium hardness leading edge 20. The trailing edge 18 has low specific gravity which is lower than that of sea water (i.e., less than L025), low shore durometer A hardness, low modulus at percent elongation, high tensile and high tear strength, low volume swell in water, good low temperature flexibility, and
good weather aging resistance. These requirements for the fairing sections reduce the buckling effect resulting from the cable catenary during towing and help to have the neutral axis of the fairing positioned so that the fairing tends to right itself on the cable. Leading edge 20 is of medium durometer hardness. Each fairing section is connected to tow cable 12 by means ofa yoke 22 and a plurality of rings or clips such as 24 and 26. Each fairing section is independent of the motion of other fairing sections attached to the tow cable.
FIG. 2 shows attachment of a yoke such as shown in FIG. 1 by numeral 22 and a plurality of rings or clips, preferably evenly spaced on the tow cable, such as shown by numerals 24 and 26 in FIG. 1. Cable 12 is shown in FIG. 2 by fathom lines. Clip 26, its sleeves 28 and 30, screws 32 and 34, and corresponding nuts 36 and 38 are preferably made of No. 316 stainless steel. However, other similar materials may be substituted for stainless steel in the fabrication of these parts and the subsequent parts without deviating from the teachings of the subject invention. Yoke 22 is supported on a nylon thrust washer resting on a fairing support ring 37. The yoke is designed to straddle the support ring 37 in region 39. The support ring 37 is preferably made of No. 18 gage, No. 316 stainless steel strip about 2 inches by inches, and is vulcanized to the tow cable by a Nitrile Rubber layer having composition as discussed be low.
For vulcanizing one of the support rings to the tow cable, a portion of the tow cable of width slightly greater than the width of the support ring is wire brushed; degreased by means of a solvent such as xylene or acetone; dried with cold air, painted with a phosphoric acid mixture (80 percent by volume) for about one minute, rinsed with water and dried with cold air thereafter. The cleaned work area on the tow cable is then painted with a smooth coat of an adhesive such as Thixon P-4 or the like and allowed to dry for at least half an hour. The uncured Nitrile Rubber is then slipped inside the pre-cleaned support ring and any rubber extending the surface of the support ring is removed. The support ring with the rubber is then slipped over the already prepared section of the tow cable and squeezed thereon. The tow cable and the support ring are then treated in a mold preheated to 307F and a pressure of 24,000 pounds is applied for minutes. The excess rubber flashing is then removed and the seam of the support ring is carefully tack welded without burning a hole therein. The weld is ground to match the surface of the support ring.
The support rings are positioned along the tow cable to ensure a nominal 4-inch clearance between the lower end of one fairing section and the upper end of the adjoining fairing section. Each support ring is tested to withstand a shear load of 1,000 pounds applied for a period of 1 minute. Yoke portion 40 of yoke 22 is attached to its insert 42 by two screws 44 and 46 which are preferably two No. 10-32 flat head screws passing through respective pairs of holes 48, 50 and 52, 54 provided with mating nuts which come flush with the yoke surfaces. Yoke portion 40 is attached to the fairing piece 16' by means of screw 56, preferably a No. %-24 flat head screw provided with a matching nut, so that there is adequate clearance between the fairing and the tow cable when the inner leading edge of the yoke is bearing against the tow cable. Clip or ring 26 has its upper portion 58 mated with the tow cable 12 with its lower ears 60 and 62 in contact with opposite sides of the fairing section 64. Screws 32 and 34, together with the respective sleeves 28 and 30 and the respective nuts 36 and 38, are used to connect lower ears 60 and 62 of ring or clip 26 with fairing section 64. Sleeve 28 is inserted through holes 66 and 68 in ring or clip 26 and screw 32 is passed through the sleeve 28 and is used together with nut 36 to fasten the ring or clip 26 to the fairing section 64. Likewise, sleeve 30 is inserted through holes 70 and 72 in ring or clip 26 and the fairing section 64. Screw 34 and nut 38 are then used to attach securely ring or clip 26 to fairing section 64. FIG. 2 also shows a magnified view of yoke 22 to be attached to tow cable 12. Yoke portion 40 of yoke 22 is placed in position over tow cable 12. Insert 42 is attached to the fairing piece 16'. Holes 48 and 50 in yoke portion 40 are lined up with the respective holes in insert 42, holes 52 and 54, and 74 and 76 in yoke portion 40 are lined with the respective holes in insert 42. Screws 44, 46, and 56 are used together with their matching nuts to tie fairing piece 16' to yoke portion 40 and tow cable 12. It should be noted that each fairing section has a yoke and insert section attaching the fairing section to the tow cable and a series of rings or clips, preferably evenly spaced, attaching the fairing section to the tow cable. There is enough clearance between the tow cable and the yoke and rings which enables the fairing to rotate about the tow cable freely.
COMPOSITION OF TRAILING EDGE or FAIRING SECTIONS The requirements for the material to be used for preparing various sections of the fairing are such that it will reduce galloping of the tow line, i.e., mechanical and hydromechanical characteristics of a tow line make the tow cable to be unstable like a telephone wire strumming in wind; kiting, i.e., the tow line experiencing side forces which bring about a sideway motion of the tow line; and buckling, i.e., instability resulting from the fact that stresses developing in the trailing edge are greater than stresses developing in leading edge if the material out of which a fairing section is made is of uniform density. In order to reduce galloping, kiting and buckling, it was considered essential to prepare a special type rubber material using Butyl-035 as a base polymer and preparing materials of different characteristics for trailing edge and leading edge of each of the fairing sections. Special nitrile rubber is also made for vulcanizing support rings to the tow cable.
As pointed out above, it is considered essential that specific gravity of the material out of which trailing edge portion of each of the fairing sections is made should have specific gravity lower than that of sea water, i.e., 1.025, good weather-and ozone-resistant properties, low shore durometer A hardness, low modulus at percent elongation, high tensile and high tear strength, low volume swell in water and good low temperature flexibility. In order to achieve these characteristics, a new material is developed, preferably using Butyl-035 as a base polymer and using a Super Abrasion Furnace black (i.e., SAF black) such as Philblack-E made by Phillips Petroleum, Rubber Chemical Division. SAF black is used as a reinforcing agent to give the material tensile properties for reinforcement and its opacity prevents deterioration of the material by sunlight. A peptizer such as Elastopar (i.e., 33.3 percent Ingredients Parts by weight Butyl-O35 100 Elastopar Philblack-E (SAF) Zinc Oxide Stearic Acid Dioctyl Scbacate Sulfur Methyl Tuuds Captax COMPOSITION OF LEADING EDGE OF FAIRING SECTIONS The requirements for the medium hard leading edge compound are found to be low specific gravity, medium shore A durometer hardness, high modulus at 100 percent elongation, high ultimate tensile strength, high tear strength, low volume swell in water, good low temperature flexibility, and good weather resistance. The composition of leading edge compound satisfying above-described properties is preferably found to have the following composition:
Ingredients Parts by weight Butyl-035 Elastopar Philblack-E (SAF) Zinc Oxide Stearic Acid Dioctyl Sebacate Sulfur Methyl Tuads Captax METHOD OF PREPARING FAIRING SECTIONS Both trailing edge compound and leading edge compound are formulated by allowing curing time to be seventy minutes at 307F. The following mixing procedure is developed for attaining trailing edge compound and leading edge compound having desirable properties.
1. Preheat Banbury type mixer to 300F.
2. Add Butyl polymer and masticate it for /2 minute.
3. Add Elastopar and mix for /2 minute.
4. Add half the amount of SAP black (Philblack-E) and halfthe amount of stearic acid and mix for 2 minutes.
5. Add remainder of SAP black and stearic acid and zinc oxide and mix for 2 minutes.
6. Remove mixed stock from Banbury type mixer and mill it on a cold rubber mill until homogeneous.
7. Add dioctyl sebacate, sulfur, methyl tuads and captax in the order listed and mill it until homogeneous.
8. Refine six times on a cold mill with tight rolls and batch off.
A segmented fairing blank is made of raw, i.e., uncured, pieces of the respective butyl-rubber compounds, a Dacron strength member along the leading edge and an antichaffing ply of nylon along the exterior portions of the leading edge. The blank measures a certain length depending upon the length of the mold cavity and is roughly shaped to conform to the cavity. The raw rubber blanks for fairing sections are so cut and arranged that the leading edge portion is preferably about one inch wide while the remaining trailing edge portion is preferably 4.5 inches wide. The strength member is composed of preferably six or more plies of Dacron reinforcement for a total width of at least 0.25 inch. It is positioned at and conforms to the leading edge of the fairing section and runs the entire length of the fairing section and is looped back on itself for 8 inches at each end to form an eye having a diameter of 9/16 inch. An antichaffing ply is attached over the leading edge and extends over both adjacent surfaces by about one inch and runs along the entire length of the fairing section. The entire raw length assembly is vulcanized in a mold under pressure of at least 600 per square inch (psi) mold surface area for minutes at 307F.
COMPOSITION AND FORMULATION OF NITRILE RUBBER Ingredients Parts by weight Hycar I042 Philblack-A (FEF) 60 Zinc Oxide 5 Stearic Acid 1 Maglite-D 4 DOTG 0.5 Captax l.5 Sulfur 2 The polymer is banded on the mill to form a rolling bank. Zinc oxide is added to about one-half the Philblack-A FEF, i.e., Fine Extrusion Furnace) and is millmixed into the polymer. Stearic acid, maglite-D, and DOTG (Di-Ortho-Tolyl-Guanidine) are then added to the remaining half of Philblack-A (FEF) and are millmixed into the polymer. Captax (Z-Mercaptobenzo- .thiazole) and sulfur are then added and the stock is cut and refined on the mill and is sheet-off to a thickness of 3/16 inch. Curing time is 10 minutes at 307F. The total mill-mixing time is about 25 minutes.
Briefly stated, leading edge compound and trailing edge compound are made out of materials using Butyl- 035 as a base polymer and Nitrile Rubber for vulcanizing support rings to the tow cable is made using Hycar 1042 as the base polymer. Fairing sections are attached to the tow cable using a yoke-insert arrangement and a series of clips or rings. Each fairing section is independent of the other fairing sections attached to the cable. A tow cable having fairing sections attached thereto is free of galloping, kiting and buckling.
Obviously many modifications and variations of the present invention are possible in the light of the above teachings. As an example, the compositions of leading edge compound and trailing edge compound of fairing sections may vary. Furthermore, the number and design of yoke-insert systems and clips may vary. It is therefore understood that within the scope of appended claims the invention may be practiced otherwise than as specifically described.
We claim: 1. A towing system for a variable depth sonar comprising:
a substantially long tow cable: means for securing a plurality of spaced fairing sections to said tow cable, said plurality of fairing sections having an axis of symmetry substantially normal to the longitudinal axis of said tow cable and having longitudinal axis substantially parallel to the longitudinal axis of said tow cable, each of said plurality of fairing sections having a leading edge and a trailing edge; a plurality of support rings vulcanized to said tow cable along the longitudinal axis thereof; a plurality of clips connected to said tow cable and to said plurality of fairing sections; and the trailing edge of each of said plurality of fairing sections being made from a first butyl rubber compound essentially of the following ingredients:
2. The towing system of claim 1 wherein said leading edge of each of said plurality of fairing sections is made from a second butyl rubber compound essentially consisting of the following ingredients:
Ingredients Parts by weight Butyl-035 Elastopar l Philblack-E (SAF) 65 Zinc Oxide Stearic Acid Dioctyl Sebacate l Sulfur Methyl Tuads Captax LIILII

Claims (2)

1. A TOWING SYSTEM FOR A VARIABLE DEPTH SONER COMPRISING
2. The towing system of claim 1 wherein said leading edge of each of said plurality of fairing sections is made from a second butyl rubber compound essentially consisting of the following ingredients:
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Cited By (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4027836A (en) * 1976-03-01 1977-06-07 Seibel Julia K Drag reducing fairing for landing gear
US4200999A (en) * 1978-05-30 1980-05-06 Deepsea Ventures, Inc. Pivotable means for decreasing drag effects on a generally cylindrical dredge pipe
JPS5929588A (en) * 1982-08-12 1984-02-16 Nec Corp Flow-straightening device for tow rope
FR2540822A1 (en) * 1983-02-14 1984-08-17 Gaspard Colette Anti-vibratory system for submerged cables
WO1985001261A1 (en) * 1983-09-13 1985-03-28 University Of Bath Fairing sections
US4756269A (en) * 1983-09-29 1988-07-12 Raytheon Company Cable fairing stacking ring
US6244204B1 (en) 1998-11-03 2001-06-12 Odim Holding Asa Fairing for a towed cable
US20050175415A1 (en) * 2001-10-19 2005-08-11 Mcmillan David W. Apparatus and methods for remote installation of devices for reducing drag and vortex induced vibration
US20060021560A1 (en) * 2004-05-02 2006-02-02 Mcmillan David W Tail fairing designed with features for fast installation and/or for suppression of vortices addition between fairings, apparatus incorporating such fairings, methods of making and using such fairings and apparatus, and methods of installing such fairings
US20060115335A1 (en) * 2004-11-03 2006-06-01 Allen Donald W Apparatus and method for retroactively installing sensors on marine elements
US20060177275A1 (en) * 2005-01-07 2006-08-10 Allen Donald W Vortex induced vibration optimizing system
US20060231008A1 (en) * 2005-04-11 2006-10-19 Donald Wayne Allen Systems and methods for reducing vibrations
US20060280559A1 (en) * 2005-05-24 2006-12-14 Allen Donald W Apparatus with strake elements and methods for installing strake elements
US20070003372A1 (en) * 2005-06-16 2007-01-04 Allen Donald W Systems and methods for reducing drag and/or vortex induced vibration
US20070104542A1 (en) * 2003-08-19 2007-05-10 Crp Group Limited Fairing for a riser
US20070125546A1 (en) * 2005-09-02 2007-06-07 Allen Donald W Strake systems and methods
US20070137956A1 (en) * 2003-08-27 2007-06-21 Stamps Frank B Dual spring rate damper
US20080166185A1 (en) * 2007-01-05 2008-07-10 Benton Frederick Baugh Method of installing fairings around vertical pipes
US20090242207A1 (en) * 2006-03-13 2009-10-01 Shell Internationale Research Maatschappij B.V. Strake systems and methods
US20100061809A1 (en) * 2006-11-22 2010-03-11 Shell Oil Company Systems and methods for reducing drag and/or vortex induced vibration
US20100098497A1 (en) * 2007-03-14 2010-04-22 Donald Wayne Allen Vortex induced vibration suppression systems and methods
US20100150662A1 (en) * 2007-02-15 2010-06-17 Donald Wayne Allen Vortex induced vibration suppression systems and methods
US9511825B1 (en) * 2011-01-05 2016-12-06 VIV Solutions LLC Apparatus for suppressing vortex-induced vibration of a structure with reduced coverage
US9534618B1 (en) * 2014-09-04 2017-01-03 VIV Solutions LLC Fairing bodies with multiple parts
US10344785B1 (en) 2017-01-03 2019-07-09 VIV Solutions LLC Multiple component fairing
US11427285B2 (en) * 2018-12-19 2022-08-30 Pgs Geophysical As Slit fairing for towed marine equipment

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US3224406A (en) * 1964-05-14 1965-12-21 United Aircraft Corp Underwater towing cable lift attachment
US3343516A (en) * 1966-08-31 1967-09-26 Donald A Nichols Minimum width towlines with stretchable electrical cable and improved clamping means
US3407777A (en) * 1967-04-25 1968-10-29 Navy Usa Fairing support ring
US3443020A (en) * 1967-11-22 1969-05-06 Uniroyal Inc Faired cable
US3467047A (en) * 1967-12-21 1969-09-16 Us Navy Minimum-width continuously faired towline

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US3224406A (en) * 1964-05-14 1965-12-21 United Aircraft Corp Underwater towing cable lift attachment
US3343516A (en) * 1966-08-31 1967-09-26 Donald A Nichols Minimum width towlines with stretchable electrical cable and improved clamping means
US3407777A (en) * 1967-04-25 1968-10-29 Navy Usa Fairing support ring
US3443020A (en) * 1967-11-22 1969-05-06 Uniroyal Inc Faired cable
US3467047A (en) * 1967-12-21 1969-09-16 Us Navy Minimum-width continuously faired towline

Cited By (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4027836A (en) * 1976-03-01 1977-06-07 Seibel Julia K Drag reducing fairing for landing gear
US4200999A (en) * 1978-05-30 1980-05-06 Deepsea Ventures, Inc. Pivotable means for decreasing drag effects on a generally cylindrical dredge pipe
JPS5929588A (en) * 1982-08-12 1984-02-16 Nec Corp Flow-straightening device for tow rope
FR2540822A1 (en) * 1983-02-14 1984-08-17 Gaspard Colette Anti-vibratory system for submerged cables
WO1985001261A1 (en) * 1983-09-13 1985-03-28 University Of Bath Fairing sections
US4836122A (en) * 1983-09-13 1989-06-06 University Of Bath Fairing sections
US4756269A (en) * 1983-09-29 1988-07-12 Raytheon Company Cable fairing stacking ring
US6244204B1 (en) 1998-11-03 2001-06-12 Odim Holding Asa Fairing for a towed cable
US20050175415A1 (en) * 2001-10-19 2005-08-11 Mcmillan David W. Apparatus and methods for remote installation of devices for reducing drag and vortex induced vibration
US7578038B2 (en) 2001-10-19 2009-08-25 Shell Oil Company Apparatus and methods for remote installation of devices for reducing drag and vortex induced vibration
US20070104542A1 (en) * 2003-08-19 2007-05-10 Crp Group Limited Fairing for a riser
US20070137956A1 (en) * 2003-08-27 2007-06-21 Stamps Frank B Dual spring rate damper
AU2005241044B2 (en) * 2004-05-02 2009-10-22 Shell Internationale Research Maatschappij B.V. Tail fairing designed with features for fast installation, apparatus incorporating such fairings, methods of making and using such fairings and apparatus, and methods of installing such fairings
US20060021560A1 (en) * 2004-05-02 2006-02-02 Mcmillan David W Tail fairing designed with features for fast installation and/or for suppression of vortices addition between fairings, apparatus incorporating such fairings, methods of making and using such fairings and apparatus, and methods of installing such fairings
US7398697B2 (en) 2004-11-03 2008-07-15 Shell Oil Company Apparatus and method for retroactively installing sensors on marine elements
US20060115335A1 (en) * 2004-11-03 2006-06-01 Allen Donald W Apparatus and method for retroactively installing sensors on marine elements
US20060177275A1 (en) * 2005-01-07 2006-08-10 Allen Donald W Vortex induced vibration optimizing system
US7316525B2 (en) 2005-01-07 2008-01-08 Shell Oil Company Vortex induced vibration optimizing system
US20090269143A1 (en) * 2005-01-07 2009-10-29 Donald Wayne Allen Vortex Induced Vibration Optimizing System
US20060231008A1 (en) * 2005-04-11 2006-10-19 Donald Wayne Allen Systems and methods for reducing vibrations
US7406923B2 (en) 2005-04-11 2008-08-05 Shell Oil Company Systems and methods for reducing vibrations
US20060280559A1 (en) * 2005-05-24 2006-12-14 Allen Donald W Apparatus with strake elements and methods for installing strake elements
US20070003372A1 (en) * 2005-06-16 2007-01-04 Allen Donald W Systems and methods for reducing drag and/or vortex induced vibration
US20070125546A1 (en) * 2005-09-02 2007-06-07 Allen Donald W Strake systems and methods
US20090242207A1 (en) * 2006-03-13 2009-10-01 Shell Internationale Research Maatschappij B.V. Strake systems and methods
US20100061809A1 (en) * 2006-11-22 2010-03-11 Shell Oil Company Systems and methods for reducing drag and/or vortex induced vibration
US20080166185A1 (en) * 2007-01-05 2008-07-10 Benton Frederick Baugh Method of installing fairings around vertical pipes
US8523492B2 (en) * 2007-01-05 2013-09-03 Benton Frederick Baugh Method of installing fairings around vertical pipes
US20100150662A1 (en) * 2007-02-15 2010-06-17 Donald Wayne Allen Vortex induced vibration suppression systems and methods
US20100098497A1 (en) * 2007-03-14 2010-04-22 Donald Wayne Allen Vortex induced vibration suppression systems and methods
US9511825B1 (en) * 2011-01-05 2016-12-06 VIV Solutions LLC Apparatus for suppressing vortex-induced vibration of a structure with reduced coverage
US9534618B1 (en) * 2014-09-04 2017-01-03 VIV Solutions LLC Fairing bodies with multiple parts
US10344785B1 (en) 2017-01-03 2019-07-09 VIV Solutions LLC Multiple component fairing
US11427285B2 (en) * 2018-12-19 2022-08-30 Pgs Geophysical As Slit fairing for towed marine equipment

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