GB2048163A - Flexible Self-sealing Wall Member - Google Patents

Flexible Self-sealing Wall Member Download PDF

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Publication number
GB2048163A
GB2048163A GB7905023A GB7905023A GB2048163A GB 2048163 A GB2048163 A GB 2048163A GB 7905023 A GB7905023 A GB 7905023A GB 7905023 A GB7905023 A GB 7905023A GB 2048163 A GB2048163 A GB 2048163A
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GB
United Kingdom
Prior art keywords
wall member
elastomer
sheets
layers
wall
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
GB7905023A
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GB2048163B (en
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.)
Broadhurst J C Fletcher R A
Original Assignee
Broadhurst J C Fletcher R A
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 Broadhurst J C Fletcher R A filed Critical Broadhurst J C Fletcher R A
Priority to GB7905023A priority Critical patent/GB2048163B/en
Publication of GB2048163A publication Critical patent/GB2048163A/en
Application granted granted Critical
Publication of GB2048163B publication Critical patent/GB2048163B/en
Expired legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B25/00Layered products comprising a layer of natural or synthetic rubber
    • B32B25/04Layered products comprising a layer of natural or synthetic rubber comprising rubber as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B25/042Layered products comprising a layer of natural or synthetic rubber comprising rubber as the main or only constituent of a layer, which is next to another layer of the same or of a different material of natural rubber or synthetic rubber
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04Interconnection of layers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04Interconnection of layers
    • B32B7/12Interconnection of layers using interposed adhesives or interposed materials with bonding properties
    • B32B7/14Interconnection of layers using interposed adhesives or interposed materials with bonding properties applied in spaced arrangements, e.g. in stripes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60KARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
    • B60K15/00Arrangement in connection with fuel supply of combustion engines or other fuel consuming energy converters, e.g. fuel cells; Mounting or construction of fuel tanks
    • B60K15/03Fuel tanks
    • B60K15/03177Fuel tanks made of non-metallic material, e.g. plastics, or of a combination of non-metallic and metallic material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65DCONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D90/00Component parts, details or accessories for large containers
    • B65D90/02Wall construction
    • B65D90/04Linings
    • B65D90/046Flexible liners, e.g. loosely positioned in the container
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B38/00Ancillary operations in connection with laminating processes
    • B32B2038/0052Other operations not otherwise provided for
    • B32B2038/008Sewing, stitching
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2439/00Containers; Receptacles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60KARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
    • B60K15/00Arrangement in connection with fuel supply of combustion engines or other fuel consuming energy converters, e.g. fuel cells; Mounting or construction of fuel tanks
    • B60K15/03Fuel tanks
    • B60K2015/03328Arrangements or special measures related to fuel tanks or fuel handling
    • B60K2015/03407Arrangements or special measures related to fuel tanks or fuel handling to protect tanks against projectiles

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Transportation (AREA)
  • Laminated Bodies (AREA)

Abstract

Layers 22 to 25 of natural or synthetic rubber are held together at spaced points by lines of drop thread stitching 28 or by spots of adhesive so that the sheets are free to move across each other between the points of connection. The wall may also include a reinforcing fabric web 21, and an outside barrier layer 20 and inside barrier layer 26, both layers being impermeable to fuel held in a tank of which the wall member may form a part. The wall member is self- sealing when penetrated by a projectile because the rubber layers then undergo large dynamic elongations but rapidly recover to close up the holes formed, these holes generally being out of alignment. <IMAGE>

Description

SPECIFICATION Flexible Self-sealing Wall Member The present invention relates to flexible self-sealing wall members which can be used to make self-sealing containers such as tanks for liquid fuels and hydraulic fluids.
It is well known to make flexible-walled tanks for use as aircraft fuel tanks with walls of a synthetic elastomer reinforced with a textile fabric and for the purpose of sealing punctures in the tank walls to incorporate a layer of natural latex which swells when exposed to the fuel stored in the tank and thereby closes up any opening.
With such a construction it is however difficult to prevent fuel reaching the latex layer prematuraly and causing swelling before any puncture has occurred. Moreover, the properties of the latex are adversely affected by extremes of heat and cold which may be experienced by aircraft and tend to deteriorate with time, especially when exposed to extremes of temperature.
In accordance with the present invention there is provided a flexible self-sealing wall member incorporating two or more sheets of elastomer in surface contact with one another and joined together at spaced positions, wherein the sheets are free to move across each other between the positions at which they are joined.
In this construction it is no longer necessary for the sheets of elastomer to be swellable by contact with fuel. It is found, surprisingly, that when the layers are punctured, for example by a projectile, the openings in the individual layers close up rapidly and the small holes remaining are out.of register with one another so that no through passage remains for the fuel.
The achievement of these results requires a number of thin layers of elastomer with a high elasticity. An elongation of not less than 200% under static conditions at normal temperature and pressure is desirable. It has been found that under dynamic conditions, that is when a sheet is punctured by a projectile moving at high speed, an elongation of over 500% can occur without damage and there will be rapid recovery to close the puncture. With some high tensile silicone rubbers an elongation of 1000% has been observed under dynamic conditions.
The sheets of natural or synthetic elastomer are preferably joined by lines of drop-thread stitching to produce a quilted effect with the lines of stitching defining discrete areas of the well member within which the sheets of elastomer are free to undergo relative movement. Alternatively the sheets can be joined at spaced points, for example by spots of adhesive placed between the sheets.
The elastomers used may be natural or synthetic rubbers and good results have been obtained with nitrile, silicone, and epichlorhydrin rubbers as well as natural rubber. Each layer has a thickness preferably in the range 0.1 to 1.0 mm.
The wall member preferably includes other layers, in particular reinforcing layers of coated fabric to which the self-sealing elastomer layers are preferably only connected at spaced points to allow maximum freedom of movement to the elastomer layers.
The flexible self-sealing wall member of the invention can be incorporated in a container which may be used to hold hydraulic fluids or liquid fuels, for example a fuel tank for a vehicle or an aircraft. In the case of a fuel tank an outer casing or reinforced synthetic resin or other rigid non-metallic material is preferably provided.
The invention will now be described in more detail with the aid of examples illustrated in the accompanying drawings, in which: Fig. 1 is a cross-section of the wall of a fuel tank embodying the invention; Fig. 2 is a sketch illustrating the bonding in an alternative wall; Fig. 3 is a diagrammatic cross-section through an automobile fuel tank incorporating the wall member, and Fig. 4 is a cross-section similar to Fig. 1 of an alternative wall member construction for a fuel tank.
Referring to Fig. 1, the inside of the tank is at the top of the figure and the outside at the bottom.
On the outside of the tank is a layer 20 of synthetic barrier material which in this case is epichlorohydrin but may alternatively be a polysulphide or high nitrile rubber. The layer 20 is impermeable and is resistant to fuel and hydraulic fluids. Joined to the layer 20 is a reinforcing fabric web 21. The fabric forming the web 21 is a random textile fabric which is neither knitted nor woven but made of a random mass of continuous filaments. The filaments are of synthetic plastics material, and may for example be a mixture of nylon and polyester fibres or preferably all of nylon. A fabric having these characteristics is sold by l.C.I. Fibres Division under the trade name TERRAM 1000 but a different grade of the fabric is required for the present purpose.
On the other side of the fabric web 21 is a first layer 22 of silicone rubber, such as the material supplied by Dow Corning under the trade name SILASTIC 35. Second, third and fourth layers 23, 24 and 25 of the silicone rubber are shown as overlying the layer 22. Finally there is another layer 26 of synthetic barrier material similar to the layer 20, which forms the inside of the tank wall.
The four layers 22 to 25 of silicone rubber are formed separately and are held together either by lines of drop thread stitching 28, as shown in Fig. 1, to produce a quilted effect, or by spot joining.
Stitching, if it is used, extends at least through the layers 22 to 25 and preferably also through the fabric web 21, the synthetic barrier layers 20 and 25 then being adhesively bonded. Alternatively, the silicone rubber layers 22 to 25 can be adhesively bonded each to the adjacent layers by spots of adhesive conveniently in the pattern shown in Fig. 2, with the adhesive spots being at approximately half-inch (12.6 mm) centres. Other ways of joining the layers may be suitable, for example hot moulding to produce a homogeneous blend of material, or using fibrous or plastics rivets.
The silicone rubber layers are essentially solid layers, that is to say they do not have to be rendered porous. They are free between the joining points to move laterally against one another. We have found that with such a multilaminated construction, when the wall is punctured by a projectile, the rubber layers will deform sufficiently to reseal the wall even without the presence of fuel to cause the rubber to swell. This is indeed a surprising effect, but it means that the wall can be used with great effect in other situations than aircraft fuel tanks, and that a minimum of other reinforcing layers are required in the wall, The use of silicone rubber enables the self-sealing properties to be effective at low temperature, in one example down to -600C.
It may be possible to dispense with the fabric web 21, in which case the wall consists solely of multilaminations of silicone rubber between the layers of synthetic barrier material. In practice, however, it may be desirable to introduce additional woven or non-woven fabric layers at various positions in the wall structure, providing always that at least two layers of contacting silicone rubber are present, and preferably more, these not being joined over their whole surfaces but being free to move between joining points.
The layers 22 to 25 are described as being of a silicone rubber, though any high tensile synthetic or indeed natural latex having good elasticity can be used. Other types of elastomeric material may be found to be suitable.
If the layer 26 is formed of a synthetic elastomer such as epichlorohydrin, it may be desirable to add a further layer of impermeable film, such as TEFLON/FEP film, on the inner surface of the wall.
Alternatively. the barrier layer 26 can itself be formed of the TEFLON/FEP film. ("Teflon" is a Registered Trade Mark). The film is available from Du Pont de Nemours International S.A., Geneva, Switzerland.
In one example typical thicknesses for the various layers were: Synthetic elastomer 20, 26 each 30 thou. (0.75 mm) Fabric web 21 20 thou. (0.5 mm) Silicone rubber 20 to 25 each 12 thou. (0.3 mm) The total thickness is thus about 1 30 thou. (32. mm).
The sheet material described above and shown in Fig. 1 can be cut and formed into a fuel tank by butt joining the cut edges, either with an adhesive or by vulcanising. The individual layers could be joined separately but this is not necessary. An example of an automobile fuel tank incorporating such a structure is shown in Fig. 3. Here a generally rectangular inner tank 30 is formed of the wall material of Fig. 1 and has a spout 31. The inner tank is placed within an outer tank 32 which is formed of any suitable non-metallic material, preferably a plastics material reinforced with a non-woven glass fibre web or with a material sold under the trade name KELVAR by Fothergill and Harvey Limited of Littleborough, Lancashire.The outer tank 32 should not be made of metal, because if penetrated by a projectile this tends to cause either nonrecovering or permanent "petalling", thus preventing recovery of the inner wall. The outer tank can be made in two halves, joined in any convenient manner at 33.
The interior of the inner tank including the spout is 85% filled with a explosive suppressant material such as the material sold by I.C.I. under the trade name PROMEL. This can conveniently be used in the form of 60 mm. cubes. The spout 31 contains a gauze 34 which retains the explosive suppressant in the tank.
The inner tank is not attached to the outer tank, except at the top of the spout 31, which is covered by a filler cap 36 is conventional manner. A fuel outlet pipe (not shown) is joined to the inner tank by a flexible or rigid coupling. The tank is provided with a known helical type of fuel gauge 35 which is sealed through the walls of both the inner and outer tanks.
As well as being used to form the fuel tank itself, the material can advantageously be used to provide protection for the fuel pipeline from the tank to the engine. The pipeline itself should be made of a non-metallic material, such as glass reinforced plastics for example, and the self-sealing material is then wrapped and sealed around the pipeline to form a protective bag. If the bag is penetrated and the pipeline shattered, fuel will fill the bag, but the bag will seal and form a reservoir maintaining fuel flow between the tank and the engine.
In the wall construction of Fig. 4 there are again four thin sheets of silicone rubber 22, 23, 24 and 25, each sheet being about 20 thou. (0.5 mm) thick. On the inside is a reinforcing layer 37 and on the outside a reinforcing layer 38, both the layers 37 and 38 consisting of coated fabrics in which the fabric is nylon 66 and the coating is nitrile rubber. The layers 22 to 25 are bonded to each other and to the layers 37 and 38 by adhesive spots 39. The flexible wall member contructed in this way is assembled within a rigid shell 40 consisting of glass-fibre-reinforced synthetic resin board.
Upon penetration of the wall construction shown in Fig. 4 by a projectile fired from outside a hole is formed in the rigid shell 40 and the projectile passes through to the inside of the container but the perforation formed in the inner reinforcing layer 37 is too small to be visible and overall there is no leakage from the container. Similar results are obtained whether the sheets 22 to 25 are of silicone rubber, e.g. Dow Corning S35, or of nitrile or epichlorhydrin synthetic rubber or natural rubber.

Claims (13)

Claims
1. A flexible self-sealing wall member incorporating two or more sheets of elastomer in surface contact with one another and joined together at spaced positions in such a way that the sheets are free to move across each other between these positions.
2. A wall member as claimed in claim 1 in which the sheets of elastomer are swellable by the action of hydrocarbon fuels.
3. A wall member as claimed in claim 1 or 2 in which the sheets of elastomer are joined together at points of a regular array.
4. A wall member as claimed in claim 1 or 2 in which the sheets of elastomer are joined along lines defining discrete areas.
5. A wall member as claimed in claim 4 in which the joining is by stitching.
6. A wall member as claimed in any of the preceding claims in which the sheets of elastomer are sandwiched between inner and outer barrier layers.
7. A wall member as claimed in claim 6 in which the inner barrier layer comprises a sheet of synthetic elastomer and an impermeable film on the free surface.
8. A wall member as claimed in claim 6 or 7 in which a reinforcing fabric web is incorporated between the inner and outer layers.
9. A wall member as claimed in claim 8 in which the fabric web is a random textile fabric comprising continuous filaments of synthetic plastics material fused together in a random mass.
10. A wall member as claimed in claim 9 in which the sheets of elastomer are joined by stitching which also passes through the fabric.web.
11. A wall member as claimed in claim 6 in which the barrier layers are both layers of fabric coated with a synthetic elastomer.
12. A container comprising a wall member as claimed in any of the preceding claims.
13. A container as claimed in claim 12 having an outer wall of reinforced synthetic resin material.
GB7905023A 1977-11-16 1979-02-13 Flexible self-sealing wall member Expired GB2048163B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB7905023A GB2048163B (en) 1977-11-16 1979-02-13 Flexible self-sealing wall member

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB4773577 1977-11-16
GB7905023A GB2048163B (en) 1977-11-16 1979-02-13 Flexible self-sealing wall member

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GB2048163A true GB2048163A (en) 1980-12-10
GB2048163B GB2048163B (en) 1982-05-19

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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0106423A2 (en) * 1982-09-13 1984-04-25 Dow Corning Corporation Fluoroelastomer coated silicone rubber
GB2155873A (en) * 1984-03-17 1985-10-02 British Aerospace Liquid storage tanks
GB2243328A (en) * 1990-04-28 1991-10-30 Seabass Gas-impermeable laminate material
AU655796B2 (en) * 1991-02-21 1995-01-12 W. Stuart Crippen Containment integrity system for vessels for use in transportation of petroleum products
WO2002014097A2 (en) * 2000-08-11 2002-02-21 Visteon Global Technologies, Inc. Low hydrocarbon emission fuel tank with internal components
ES2253127A1 (en) * 2005-10-20 2006-05-16 Marketing Active Sport Markets, S.L. Fuel tank for vehicles
EP1858768A2 (en) * 2005-05-24 2007-11-28 High Impact Technology, L.L.C. Material-selectable, self-healing, anti-leak method for coating liquid container
US9370674B2 (en) 2011-12-05 2016-06-21 High Impact Technology, Llc Plural layer, plural-action protective coating for liquid fuel container

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0106423A2 (en) * 1982-09-13 1984-04-25 Dow Corning Corporation Fluoroelastomer coated silicone rubber
EP0106423A3 (en) * 1982-09-13 1985-04-24 Dow Corning Corporation Fluoroelastomer coated silicone rubber
GB2155873A (en) * 1984-03-17 1985-10-02 British Aerospace Liquid storage tanks
GB2243328A (en) * 1990-04-28 1991-10-30 Seabass Gas-impermeable laminate material
AU655796B2 (en) * 1991-02-21 1995-01-12 W. Stuart Crippen Containment integrity system for vessels for use in transportation of petroleum products
WO2002014097A2 (en) * 2000-08-11 2002-02-21 Visteon Global Technologies, Inc. Low hydrocarbon emission fuel tank with internal components
WO2002014097A3 (en) * 2000-08-11 2002-05-10 Visteon Global Tech Inc Low hydrocarbon emission fuel tank with internal components
EP1858768A2 (en) * 2005-05-24 2007-11-28 High Impact Technology, L.L.C. Material-selectable, self-healing, anti-leak method for coating liquid container
EP1858768A4 (en) * 2005-05-24 2012-11-21 High Impact Technology Llc Material-selectable, self-healing, anti-leak method for coating liquid container
ES2253127A1 (en) * 2005-10-20 2006-05-16 Marketing Active Sport Markets, S.L. Fuel tank for vehicles
US9370674B2 (en) 2011-12-05 2016-06-21 High Impact Technology, Llc Plural layer, plural-action protective coating for liquid fuel container

Also Published As

Publication number Publication date
GB2048163B (en) 1982-05-19

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Legal Events

Date Code Title Description
732 Registration of transactions, instruments or events in the register (sect. 32/1977)
PCNP Patent ceased through non-payment of renewal fee