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GB2250718A - Filament dispensing arrangement - Google Patents

Filament dispensing arrangement Download PDF

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Publication number
GB2250718A
GB2250718A GB8331480A GB8331480A GB2250718A GB 2250718 A GB2250718 A GB 2250718A GB 8331480 A GB8331480 A GB 8331480A GB 8331480 A GB8331480 A GB 8331480A GB 2250718 A GB2250718 A GB 2250718A
Authority
GB
United Kingdom
Prior art keywords
tubular element
filament
dispensing
fluid
flexible
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
GB8331480A
Other versions
GB2250718B (en
Inventor
Michael John Cahill
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BAE Systems PLC
Original Assignee
British Aerospace PLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by British Aerospace PLC filed Critical British Aerospace PLC
Publication of GB2250718A publication Critical patent/GB2250718A/en
Application granted granted Critical
Publication of GB2250718B publication Critical patent/GB2250718B/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65HHANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H51/00Forwarding filamentary material
    • B65H51/16Devices for entraining material by flow of liquids or gases, e.g. air-blast devices
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles
    • F41G7/20Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/30Command link guidance systems
    • F41G7/32Command link guidance systems for wire-guided missiles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/01Arrangements thereon for guidance or control
    • F42B15/04Arrangements thereon for guidance or control using wire, e.g. for guiding ground-to-ground rockets
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B19/00Marine torpedoes, e.g. launched by surface vessels or submarines; Sea mines having self-propulsion means
    • F42B19/01Steering control

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Electric Cable Installation (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

A filament dispensing arrangement, for example for dispensing filament from a submarine to a wire-guided torpedo, includes a flexible hose 5 through which a filament 4 is dispensed and fluid supply means 8 which cause fluid to flow through the hose 5 thus assisting passage of the filament through the hose and also allowing the stiffness of the hose to be controlled by suitable selection of fluid flow rate and size of orifice 6. <IMAGE>

Description

FILAMENT DISPENSING ARRAGEMENTS This invention relates to filament dispensing arrangements and in particular, but not exclusively, to arrangements for dispensing wire from a submersible vehicle.
Such arrangements may be used when dispensing wire from a submarine to a wire-guided torpedo or for dispensing a wire to a submersible vehicle for monitoring the condition of the submersed parts of an oil rig.
When a wire-guided torpedo is launched from a parent vehicle the torpedo and parent vehicle may move a combined distance from the launch location of many kilometres. Part of the guidance wire is stored in the torpedo and is dispensed rearwardly therefrom as the torpedo travels to its destination, the remainder of the wire being stored on the parent vessel near the launch tube for the torpedo and being dispensed as the parent vessel moves from the location at which the torpedo was launched.
After the torpedo is launched, the parent vessel may perform various manoeuvres, possibly heading in the opposite direction to that in which the torpedo is travelling. In dispensing the wire from the parent vessel it has been the practice to provide a hose fixed to the parent vessel and to allow the wire to be drawn through the hose to attempt to avoid fouling of the wire with the propulsion or steerage means of the parent vessel during such manoeuvres. This apparatus and method previously adopted suffer from the following disadvantages.
Friction between the wire and hose may become excessive thus requiring a strong and consequently bulky wire.
If fouling of the wire with the parent vessel is to be avoided, the hose must have a "stand-off" capability to dispense the wire away from the body of the vessel and this has previously been achieved by using a stiff hose; but this stiffness is a disadvantage when the torpedo is moving in a direction offset to the axis of the free end of the hose because the wire rubs heavily on the walls of the hose. The provision of a stiff hose to give a stand-off capability therefore may increase friction between the wire and the hose.
The invention seeks to overcome these disadvantages and to provide a dispensing arrangement in which the friction between the dispensed wire and the hose is reduced yet which still allows a stand-off capability.
According to one aspect of this invention, there is provided a dispensing arrangement for dispensing a filament, for example wire, which arrangement includes a flexible tubular element through which the filament may be drawn from an inlet end thereof to an outlet end thereof, and fluid supply means operable to cause fluid to flow through said tubular element, said fluid acting to assist passage of the filament through the tubular element.
This arrangement allows the friction load on the filament as it is drawn through the tubular element to be reduced. It is thought that this is caused by providing a hydrodynamic effect which reduces contact of the filament with the bore of the tubular element. Additionally, the fluid supply means causes and increased internal pressure acting in the tubular element, thereby stiffening it.
Preferably, the arrangement includes fluid supply control means arranged to control the flow of fluid through the tubular element thereby to allow the stiffness of the tubular element to be maintained at a predetermined degree.
In one arrangement, the fluid supply means comprise a pump delivering fluid to the inlet end of the tubular element. In this instance, the control means may include a by-pass circuit and associated valve means operable to allow the mass flow delivered to the tubular element to be varied to achieve the required degree of stiffness.
At its end remote from the fluid supply means, the tubular element may include orifice means of reduced internal cross-section as compared to that of said tubular element, said orifice means serving to maintain the internal pressure acting in the tubular element and also serving to at least reduce contact of the filament with the wall of the tubular element at that end region.
Preferably, said dispensing arrangement includes storage means adapted to store the filament and the tubular element each in a compact (e.g. coiled) condition.
Further orifice means may be provided within the tubular element at intervals along the length thereof each sized and located so as to produce a pre-determined pressure distribution along the length thereof, thereby to impart a selected stiffness characteristic to the tubular element.
In another aspect of this invention, there is provided a dispensing arrangement for dispensing an elongate flexible signal-carrying element from a water-based vehicle, said arrangement including storage means for storing said flexible element, a flexible tubular element attached at one end to said vehicle and through which said flexible element may be dispensed, and fluid supply means operable to cause fluid to flow through said tubular element thereby to assist passage of the filament through the tubular element.
The fluid is preferably water and a low drag additive may be mixed therewith.
Further aspects will become apparent from the following exemplary description of a filament dispensing arrangement with reference to the accompanying drawing which is a general schematic representation of a filament dispensing arrangement.
The filament dispensing arrangement illustrated is for use in dispensing a wire from a submarine to a torpedo to allow the torpedo to be guided under command signals sent from the submarine along the wire. The dispensing arrangement would be located in the in-board end region of the torpedo launch tube and is illustrated in a deployed condition.
Referring to the drawing, there is shown a torpedo launch tube 1 at the inboard end of which is situated a hollow storage drum 2 in which is housed a core-less bobbin 3 of wire 4. An elongate flexible hose 5 formed of hose reinforced by POTEE fibres or metal wires is attached to the inboard end of the drum 2 and passes through the drum thence out of the launch tube to trail from the submarine. In use the wire 4 is drawn through the hose 5, unravelling from the interior of bobbin 3. An orifice element 6 is provided at the end of the hose remote from its attachment to drum 5, having an internal diameter substantially less than the internal diameter of hose 5. The orifice element is preferably made of a low friction material such as Delrin (an acetal resin).At the inboard end of the drum 2 adjacent the hose 5 is provided an inlet port 7 supplied with fluid by pump 8 via pipe 9. The pump is fitted with a regulatable by-pass circuit 10 to allow the flow of fluid supplied to drum 2 and thence along hose 5 to be adjusted as required. The amount of fluid flow supplied to the drum 2, and the size of orifice element 6 are selected so that in one aspect the flow through the hose 5 is sufficient significantly to reduce friction between the hose 5 and wire 4 as the wire is dispensed and in another aspect so that the pressure within hose 5 is sufficient to impart to the hose sufficient stiffness to provide a stand-off capability.
The flow of fluid through the hose 5 may be increased or decreased to suit the velocity of wire dispensing required.
The orifice element 6 is an optional feature, but when present, serves both to regulate the internal pressure in the hose and also to hold the wire away from the wall of the hose. Other orifice elements or guides may be placed along the length of the hose to provide a predetermined pressure distribution thereby to generate a particular flexibility characteristic. The length of the hose is typically about 50m.
Prior to launch of a torpedo, the hose 5 may be coiled around the bobbin 3 and releasably attached by means of a shear pin or similar arrangement to the rear end of the torpedo. On launch of the torpedo, the hose 5 is drawn out to its full extent from the drum 2 whereupon it is released from the torpedo whereafter wire 4 is drawn through the hose assisted by fluid supplied by pump 8.
The fluid employed would be sea water with which a low-drag additive had been mixed.
The above described arrangement allows the use of a thinner wire, thus increasing the possible range of guidance and reducing the volume of wire that has to be employed.
In the arrangement, fluid is forced through the hose 5 to assist the passage of the wire through the hose by skin friction, whilst serving to lubricate the areas where contact would otherwise occur between wire and hose.

Claims (9)

1. A dispensing arrangement for dispensing a filament, which arrangement includes a flexible tubular element through which the filament may be drawn from an inlet end therof to an outlet end thereof and fluid supply means operable to cause fluid to flow through said tubular element, said fluid acting to assist passage of said filament through the tubular element.
2. An arrangement according to claim 1, which further includes fluid supply control means adapted to control the flow of fluid through the tubular element.
3. An arrangement according to claim 1 or claim 2, wherein the fluid supply means comprise a pump delivering fluid to the inlet end of the tubular element.
4. An arrangement according to any of the preceeding claims, wherein the outlet end of the tubular element includes orifice means of reduced internal cross-section as compared to that of the flexible tubular element, said orifice means serving to maintain the internal pressure acting in the tubular element and also serving to at least reduce contact of the filament with the internal wall of the tubular element adjacent said outlet end region.
5. A dispensing arrangement according to any of the preceeding claims, which further includes storage means adapted to store the filament and the tubular element each in a compact condition.
6. A dispensing arrangement according to claim 4, wherein further orifice are provided within the tubular element spaced along the length thereof, each sized so as to produce a predetermined pressure distribution along the length thereof thereby to impart a selected stiffness characteristic to the tubular element.
7. A dispensing arrangement for dispensing an elongate flexible signal-carrying element from a water-based vehicle, said arrangement including storage means for storing said flexible element, a flexible tubular element attached at one end to said vehicle and through which said flexible element - be dispensed, and fluid supply means operable to caul fluid to flow through said tubular element, ;thereby to assist passage of the filament throught the tubular element.
8. A dispensing arrangement according to claim 7, wherein said fluid comprises water with a low drag additive added thereto.
9. A dispensing arrangement substantially as hereinbefore described with reference to, and as illustrated in, the accompanying drawing.
9. A dispensing arrangement substantially as hereinbefore described with reference to, and as illustrated in, the accompanying drawing.
Amendments to the clans have been ffled as follows 5. A dispensing arrangement according to any of the preceding claims, which further includes storage means adapted to store the filament and the tubular element each in a compact condition.
6. A dispensing arrangement according to Claim 4.
wherein further orifices are provided within the tubular element spaced along the length thereof, each sized and located so as to produce a predetermined pressure distribution along the length thereof thereby to impart a selected stiffness characteristic to the tubular element.
7. A dispensing arrangement for dispensing an elongate flexible signal-carrying element from a water-based vehicle, said arrangement including storage means for storing said flexible element. a flexible tubular element attached at one end to said vehicle and through which said flexible element may be dispensed, and fluid supply means operable to cause fluid to flow through said tubular element, thereby to assist passage of the filament through the tubular element.
8. A dispensing arrangement according to Claim 7, wherein said fluid comprises water with a low drag additive mixed therewith.
GB8331480A 1982-11-27 1983-11-25 Filament dispensing arrangements Expired - Lifetime GB2250718B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8233869 1982-11-27

Publications (2)

Publication Number Publication Date
GB2250718A true GB2250718A (en) 1992-06-17
GB2250718B GB2250718B (en) 1992-10-21

Family

ID=10534570

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8331480A Expired - Lifetime GB2250718B (en) 1982-11-27 1983-11-25 Filament dispensing arrangements

Country Status (1)

Country Link
GB (1) GB2250718B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0794117A1 (en) * 1996-03-08 1997-09-10 AEROSPATIALE Société Nationale Industrielle Wire-controlled missile
EP1895263A1 (en) * 2006-09-01 2008-03-05 Whitehead Alenia Sistemi Subacquei S.p.A. Torpedo

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1146684A (en) * 1965-03-16 1969-03-26 Post Office Improvements in or relating to apparatus for use in bonding an elongated member to a surface
GB1214801A (en) * 1965-08-23 1970-12-02 Licentia Gmbh Flexible protective tube for the control wire of a torpedo
US3613619A (en) * 1969-12-05 1971-10-19 Us Navy Payout coil impregnated with conductive adhesive
US3703874A (en) * 1970-07-15 1972-11-28 Us Navy Flexible hose wire payout system
GB2007599A (en) * 1977-10-18 1979-05-23 Foerenade Fabriksverken Wire Guided Torpedo
GB2020789A (en) * 1978-04-12 1979-11-21 Messerschmitt Boelkow Blohm Stabilising missile flight

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1146684A (en) * 1965-03-16 1969-03-26 Post Office Improvements in or relating to apparatus for use in bonding an elongated member to a surface
GB1214801A (en) * 1965-08-23 1970-12-02 Licentia Gmbh Flexible protective tube for the control wire of a torpedo
US3613619A (en) * 1969-12-05 1971-10-19 Us Navy Payout coil impregnated with conductive adhesive
US3703874A (en) * 1970-07-15 1972-11-28 Us Navy Flexible hose wire payout system
GB2007599A (en) * 1977-10-18 1979-05-23 Foerenade Fabriksverken Wire Guided Torpedo
GB2020789A (en) * 1978-04-12 1979-11-21 Messerschmitt Boelkow Blohm Stabilising missile flight

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0794117A1 (en) * 1996-03-08 1997-09-10 AEROSPATIALE Société Nationale Industrielle Wire-controlled missile
FR2745786A1 (en) * 1996-03-08 1997-09-12 Aerospatiale FILOGUIDE FLYING MACHINE
EP1895263A1 (en) * 2006-09-01 2008-03-05 Whitehead Alenia Sistemi Subacquei S.p.A. Torpedo

Also Published As

Publication number Publication date
GB2250718B (en) 1992-10-21

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19930121