AU2001287886A1

AU2001287886A1 - Lining ducts

Info

Publication number: AU2001287886A1
Application number: AU2001287886A
Authority: AU
Inventors: Matthew Richard Turner; Nicholas Leo Weatherby
Original assignee: NCC Danmark AS; Anglian Water Authority; Severn Trent Water Ltd; Euro Projects LTTC Ltd; Yorkshire Water Services Ltd
Current assignee: NCC Danmark AS; Anglian Water Authority; Severn Trent Water Ltd; Euro Projects LTTC Ltd; Yorkshire Water Services Ltd
Priority date: 2000-09-19
Filing date: 2001-09-19
Publication date: 2002-06-20
Anticipated expiration: 2021-09-19

Description

LINING DUCTS

This invention relates to apparatus and a method for lining ducts with fibre-reinforced thermoplastics composite -materials.

The term 'duct' as used herein includes pipes, tubes and conduits, whether for conveying fluids (for example, water mains pipes or sewers) or for other purposes .

The ducts used for gas and water supplies are often of cast iron, and failure due to corrosion is becoming an increasing problem as existing systems age. It is, for example, estimated that over half of all water mains in the UK have been in service for more than 40 years, and that 20% have been in service for more than 80 years. Sewer ducts, which are generally of brickwork or concrete, can also fail due to structural deterioration of the materials. It is generally cheaper and causes less disruption if such ducts are rehabilitated by lining rather than removed and replaced. Various different techniques for lining existing ducts are known, but there is a demand for more efficient rehabilitation techniques.

Thus, WO 98/26919 shows a method of lining a duct, using a flexible liner which includes a layer of composite material made of thermoplastics and reinforcing fibres. The liner is introduced into the duct, heated to cause the thermoplastics fibres to melt, and then pressure is applied to mix the molten plastic and reinforcing fibres intimately, and to press the liner into contact with the duct, where it cools and consolidates into a structural member. The heating and application of pressure is performed by a robotic device commonly known as a pig. The pig passes along the inside of the liner, opening it up. The pig has means for heating the liner, and consolidation means which press the heated liner against the duct, where it cools and consolidates. One problem in designing the pig is to ensure that it provides sufficiently uniform heating of the liner to ensure uniformity of the final structural liner member.

DE-A-39 04 524 shows a method of lining a duct using a liner made only of thermoplastics, in this case a non-cross-linked plastics. The liner is introduced into the duct and expanded radially until it comes into contact with the duct, whereupon it becomes rigid and self-supporting. Expansion is preferably performed mechanically, by a pig which rolls in the duct. The liner may be heated to assist expansion, for example by warm air, while there is an air gap between the liner and the duct. However, it is important that the softening temperature of the plastics is not reached. The liner is therefore heated essentially by conduction, as its construction from thermoplastics means that it is relatively easy to control its temperature.

We have found that heating by conduction is not suitable for a liner described in WO 98/26919, which includes a layer of composite material comprising thermoplastics and reinforcing fibres. The composite material has air pockets throughout its thickness, and so cannot be heated uniformly to the melting point of the thermoplastics by conduction.

According to a first aspect of the invention, apparatus for converting a flexible liner, including a layer of composite material comprising thermoplastics material and reinforcing fibres, into a structural member within a duct, comprises a front portion adapted to be inserted in the liner, a central portion having heating means on one side of the layer of composite material, and a rear portion having consolidation means for forcing the heated layer of composite material towards the duct for consolidation and cooling under pressure to form the structural member, characterised in that the heating means produces hot gas which is forced under pressure through the layer of composite material to heat the layer, and the central portion is constructed and arranged to provide an air gap on the opposite side of the layer of composite material while heating takes place.

Providing the air gap on the side (inside or outside) of the layer of composite material opposite the heating means assists in the uniform heating of the layer, as it will not be in contact with the duct or part of the apparatus which can adversely affect heating. The air gap is on the low pressure side of the layer to provide a well-defined exit path for the pressurised hot gas through the thickness of the composite layer. The pressure differential across the layer drives the hot gas through in a uniform manner. The hot gas replaces the air in the pockets in the layer of composite material, and it has been found that this is a major contributory factor in uniform heating of the layer, and therefore of the liner as a whole.

The hot gas may be directed from the air gap forwardly to provide preheating of the liner at the front portion.

The hot gas is preferably produced by heating a supply of compressed air. Unheated compressed air may then conveniently be used as the consolidation means forcing the heated layer of composite material into contact with the duct. The compressed air inflates a flexible bag means which acts on the layer of composite material. The flexible bag means may be attached to the central portion. Alternatively, it may be separate, and be expanded from the rear, unrolling as it does so. This has the advantage of reducing friction between the layer and the bag means .

Preferably the central portion has inner and outer members, one of the inner and outer members having the heating means and the other having support means for providing the air gap. Conveniently, the inner member has the heating means, so that the layer of composite material is heated from the inside, while the outer member provides the air gap between the outside of the composite material layer and the duct.

In one embodiment the outer member is annular, surrounding and spaced from the inner member, and the layer of composite material is supported between the inner and outer members. In another embodiment the outer member increases in diameter from the front portion to the rear portion, and the layer of composite material is guided on the outside of the outer member. The outer member is preferably frusto-conical. This has the advantage of opening up the liner gradually as it is heated.

In yet another embodiment the outer member comprises a support carriage surrounding and spaced from the inner member. The layer of composite material is again supported between the inner and outer members. The carriage conveniently has external wheels by which it rolls along inside the duct.

Alternatively, the outer member has the heating means, so that the layer of composite material is heated from the outside, and the inner member has the support means providing the air gap between the inside of the layer and the inner member. In this embodiment the outer member may comprise a carriage. The carriage may extend forwardly to surround all or part of the front portion as well .

The liner may include an outer thermoplastics layer between the duct and the layer of composite material. The apparatus is conveniently moved along the duct by being winched from its front portion. Compressed air and power for the heating means are supplied through lines attached to the apparatus. A mobile unit may conveniently generate the compressed air supply and the power, for example electricity, to operate the apparatus.

According to a second aspect of the invention, a method of lining a duct comprises : inserting into the duct a flexible liner including a layer of composite material comprising thermoplastics material and reinforcing fibres; producing hot gas on one side of the layer of composite material and forcing the hot gas under pressure through the layer of composite material while maintaining an air gap on the opposite side of the layer, to melt the thermoplastics material; applying pressure to the heated layer to force it towards the duct for consolidation; and allowing the liner to cool under pressure whilst in contact with the duct to harden the layer of composite material into a structural member.

Thus, maintaining the air gap on the side (inside or outside) of the layer opposite to that which is being heated assists in the uniform heating of the layer. The hot gas passes through the composite to the air gap, on the low pressure side of the composite layer, and replaces the air in the pockets of the layer, to heat it uniformly.

The hot gas may then be directed from the air gap to provide pre-heating of the liner.

The liner is preferably inserted into the duct in a collapsed configuration and is subsequently expanded. Subsequent to insertion of the liner into the duct, apparatus according to the first aspect of the invention may be passed through the liner to perform the method.

A third aspect relates to a combination of the apparatus and the liner to provide an efficient rehabilitation technique for lining existing ducts.

According to a third aspect of the invention, in a combination of apparatus and a flexible liner for forming a structural member to line a duct, the liner includes a layer of composite material comprising thermoplastics material and reinforcing fibres, and is adapted for insertion into the duct, and the apparatus has a front portion adapted to be inserted in the liner, a central portion having heating means on one side of the layer of composite material, and a rear portion having consolidation means for forcing the heated layer of composite material towards the duct for consolidation and cooling under pressure to form the structural member, characterised in that the heating means produces hot gas which is forced under pressure through the layer of composite material to heat the layer, the combination being so constructed and arranged that there is an air gap on the opposite side of the layer of composite material while heating takes place.

The apparatus may be in accordance with the first aspect of the invention. The liner preferably comprises the layer of composite material together with an outer layer of thermoplastics material. Any other suitable combination of apparatus and liner could also be used.

As with the first two aspects of invention, it is the provision of pressurised hot gas and the air gap that assists in the uniform heating of the layer of composite material, to improve the effectiveness of the process. The various aspects of the invention are illustrated, by way of example, in the accompanying drawings, in which:

Figure 1 shows in diagrammatic form the use of apparatus for lining a duct with a liner having a layer of composite material;

Figure 2 shows a longitudinal section through the apparatus of Figure 1 which has internal heating means for the liner;

Figure 3 shows a longitudinal section through a modified apparatus with external heating means for the liner;

Figure 4 shows a longitudinal section through a modified apparatus with internal heating means for the liner;

Figure 5 is similar to Figure 4, but shows a further modification; and

Figure 6 is similar to Figure 5, and shows modified consolidation means.

Figure 1 illustrates apparatus used for lining an underground duct, in this case a water mains pipe 1, with a liner 2 of fibre-reinforced composite material to form a structural member.

The liner 2 is initially flexible and includes an inner layer 3 of composite material comprising filaments of thermoplastic and filaments of reinforcing fibres, and an outer layer 4 of thermoplastics material. Each layer is formed as a tube. The preferred material for the inner layer 3 is one knitted, braided, woven (or otherwise matted together) from tows comprising substantially continuous filaments of a thermoplastic such as polypropylene and similarly continuous reinforcing fibres such as that available from Vetrotex International under the registered trade name TWINTEX. It is also possible to use shorter lengths of fibres connected together in any suitable way. For example, the short fibres may be matted together with a thermoplastic binder, stitched, needle punched or stapled. The inner layer 3 has air pockets between the filaments.

The apparatus comprises a robotic device 5 (commonly known as a pig) which is moved through a section of liner 2 previously inserted into the pipe 1. The device 5 has a front portion 6, a central portion 7 including heating means 8 and support means 9, and a rear portion 10 including consolidation means 11. The device 5 is pulled through the pipe 1 by a winch 12 operating a cable 13 attached to the front portion 6. The heating means 8 comprises an electrical element (or any other suitable heater) which heats compressed air, producing hot gas which is then applied to the inside of the layer 3 to melt the thermoplastic filaments. The support means 9 provide an air gap 14 on the outside of the inner layer 3 between the inner layer 3 and the outer layer 4. The electricity for the heating element 8 and the compressed air are supplied by a generator and compressor respectively formed into a mobile unit 15 which remains above ground, and is connected to the device by an umbilical 25 containing the electricity and air lines. The compressed air is also used for the consolidation means, which comprises a flexible bag 11 inflated by the compressed air, to press the heated inner layer 3 and the outer layer 4 against the internal wall of the pipe 1. On cooling, the liner 2 forms a structural member within the pipe 1. The mobile unit 15 also includes a programmable process control unit to control operation of the various parts. The apparatus shown will normally reline about 100m of pipe in a single run. Figure 2 shows the device 5 and the liner 2 in more detail. When the liner 2 is inserted in the pipe 1, it tends to fold up at the lowest point of the pipe. As the device 5 travels along, the outer layer 4 is first pressed against the pipe, followed by the inner layer 3.

The front portion 6 of the device 5 comprises a rounded nose 16 having an eye 17 to which the winch cable 13 is attached. Movement of the nose 16 opens up the inner layer 3. The heating element 8 is attached to the rear of the nose 16, and is of smaller diameter, so that a gap opens up between the heating element 8 and the inside of the inner layer 3. The hot gas (up to 180°C) produced by the heating element 8 is under pressure, and is forced through the inner layer 3, by the pressure differential across the inner layer 3, between the higher pressure inside surface and the lower pressure air gap 14 on the outside surface. The hot gas drives out the air in the air pockets, thus heating the layer 3 from the inside. The hot gas reaches the lower pressure air gap 14 on the outside of the inner layer 3. The air gap 14 is provided by the support means 9, which also serves to direct the gas forwardly over the nose 16. The gas, which is still warm, serves to pre-heat the inner and outer layers 3, 4.

The support means 9 comprises a tubular metal carriage 18 surrounding part of the nose 16 and the heating element 8, and arranged between the inner and outer layers. Wheels 19 are mounted around the circumference of the radially outer side of the carriage 18 to roll along in engagement with the pipe and the outer layer 4. The radially inner surface 20 of the carriage 18 is contoured. A forward rounded annular projection 21 fits into a corresponding contour of the nose 16, so that movement of the nose 16 also pulls the carriage 18 along. Further projections 22, 23, 24 are spaced along the heating element 8 to keep the inner layer 3 in the correct place. At the rear portion 10 the inflatable bag 11, which is for example of silicone rubber, is attached to the rear of the heating element 8. When filled with compressed air at a suitable pressure, the bag 11 forces the hot inner layer 3 against the outer layer 4 and the pipe 1 , to consolidate and cool it under pressure to form a structural member.

Thus, in use, the liner 2 is first inserted into the pipe 1, perhaps by winching. The device 5 is then inserted into the liner 2, ensuring that the inner layer 3 is between the nose 16 and the carriage 18, and that the outer layer 4 is radially outside the carriage 18. The device 5 is then operated by the control unit to supply compressed air to the heating element 8, to provide hot gas under pressure to heat the inner layer 3, and then to inflate the bag 11 , and operate the winch 12 to pull the device 5 along the pipe 1. The control unit controls the gas temperatures and air pressures, and the velocity of the device.

With the device 5 in an initial position the hot gas directed over the nose 16 preheats an initial portion of the liner 2 and urges the outer layer 4 against the pipe 1. The hot gas also heats the thermoplastics filaments of the inner layer 3 uniformly, because the pressure differential as a result of the air gap 14 drives the hot gas through the thickness of the layer 3, replacing the air in the air pockets with hot gas. The thermoplastics filaments therefore melt and the molten plastics surrounds the reinforcing fibres. The device moves along a predetermined length, whereupon the bag 11 is inflated to press the hot inner layer 3 and the warm outer layer 4 against the pipe 1. The molten plastics of the inner layer 3 mixes intimately with the reinforcing fibres, as part of the consolidation of the layers, which then cool and harden under pressure to form a structural member. While the bag 11 is consolidating the initial portion of the liner, the hot gas is heating the next portion, and so the process continues . The device provides an efficient way of lining the pipe. Figure 3 shows a modified device, and corresponding reference numerals have been applied to corresponding parts. Thus, the device 5 of Figure 3 has the same basic elements as that of Figure 2, but the heating element 8 is provided on the carriage 18, rather than being attached between the nose 16 and the bag 11. The inner layer 3 is therefore heated from the outside instead of the inside. The support means 9 is then formed by a member 26 attached between the nose 16 and the bag 11. The member 26 comprises longitudinal fins 27, so that the required air gap 14 is provided on the inside of the inner layer 3. The hot gas is directed forwardly through the nose 16 to pre-heat the inner layer 3. Otherwise the embodiment of Figure 3 operates in the same way as that of Figure 2.

Figure 4 shows a diagram of a modification of the embodiment of Figure 2, and corresponding reference numerals have been applied to corresponding parts. In Figure 4 the heating element 8 is again provided for the inside of the liner 2, and is attached between the nose 16, which is spherical, and the bag 11 (shown uninflated) . The support means 9, instead of being a carriage 18, comprises an annular member 30 surrounding the nose 16 and heating element 8, to guide the inner layer 3 and maintain the air gap 14 during heating. The annular member 30 has an enlarged forward end 31 round the spherical nose 16, and a tubular rearward end 32 round the heating element 8. The member 30 may have wheels or rollers (not shown) to reduce friction. Otherwise the construction and operation of the embodiment of Figure 4 are the same as those of Figure 2.

Figure 5 shows a modification of the embodiment of Figure 4. In Figure 5 the front portion 6 of the device comprises a toroidal end cap 33 with the eye 17 to which the winch cable 13 is attached. The heating element 8 extends between the end cap 33 and the bag 11. The support means 9 comprises a perforated frusto-conical member 34 also attached between the cap 33 and the bag 11. The diameter of the member 34 increases from front to rear, and the inner layer 3 is guided along the outer surface of it. It has been found that the member 34 forms a guide for the inner layer 3, ensuring that the air gap 14 is maintained between the inner layer 3 and the pipe 1 during heating. It also opens the inner layer 3 up gradually as it is heated, so that consolidation is more efficient. Otherwise the construction and operation of the embodiment of Figure 5 are the same as those of Figure 4.

Figure 6 shows a modification of the embodiment of Figure 5. In Figure 6 the front portion 6, and central portion with the heating element 8 and conical member 34 are similar to those of Figure 5, although the conical member 34 has a rear end cap 35. The rear portion 10, including the consolidation means 11 is modified, as it is not attached to the central portion 7. The consolidation means still has a flexible inflatable bag 36, but this is inflated from its rearward end, and caused to unroll against the liner 2 as the device 5 moves along. The rolling contact between the liner 2 and the bag 36 creates less friction than the sliding contact of Figures 2 to 5. It may therefore be possible for the device 5 of Figure 6 to move continuously rather than in indexed steps as in Figures 2 to 5.

Claims

1. Apparatus for converting a flexible liner (2) , including a layer (3) of composite material comprising thermoplastics material and reinforcing fibres, into a structural member within a duct (1) , comprises a front portion (6) adapted to be inserted in the liner (2), a central portion (7) having heating means (8) on one side of the layer (3) of composite material and a rear portion (10) having consolidation means (11) for forcing the heated layer (3) of composite material towards the duct (1) for consolidation and cooling under pressure to form the structural member, characterised in that the heating means (8) produces hot gas which is forced under pressure through the layer (3) of composite material to heat the layer, and the central portion (7) is constructed and arranged to provide an air gap (14) on the opposite side of the layer of composite material while heating takes place.

2. Apparatus according to claim 1, characterised in that the hot gas is directed from the air gap (14) forwardly to provide pre-heating of the liner (2) at the front portion (6) .

3. Apparatus according to claim 1 or claim 2, characterised in that the hot gas is produced by heating a supply of compressed air.

4. Apparatus according to any preceding claim, characterised in that compressed air is used as the consolidation means (11) .

5. Apparatus according to claim 4, characterised in that the consolidation means comprises a flexible bag means (11 , 36) inflatable by the compressed air.

6. Apparatus according to claim 5, characterised in that the flexible bag means (11) is attached to the central portion (7) .

7. Apparatus according to claim 5, characterised in that the flexible bag means (36) is separate from the central portion (7) and, in use, is expanded from the rear, unrolling as it does so.

8. Apparatus according to any preceding claim, characterised in that the central portion (7) has inner and outer members, one of the inner and outer members having the heating means (8) and the other having support means (9) for providing the air gap (14) .

9. Apparatus according to claim 8, characterised in that the inner member has the heating means (8), so that, in use, the layer (3) of composite material is heated from the inside, while the outer member (9) provides the air gap between the outside of the composite material layer (3) and the duct (1) .

10. Apparatus according to claim 8 or claim 9, characterised in that the outer member (30) is annular, surrounding and spaced from the inner member, and, in use, the layer (3) of composite material is supported between the inner and outer members (8, 30) .

11. Apparatus according to claim 8 or claim 9, characterised in that the outer member (34) increases in diameter from the front portion (6) to the rear portion (10) , and, in use, the layer (3) of composite material is guided on the outside of the outer member (34) .

12. Apparatus according to claim 11 , characterised in that the outer member (34) is frusto-conical.

13. Apparatus according to claim 8 or claim 9, characterised in that the outer member comprises a support carriage (18) surrounding and spaced from the inner member (8) .

14. Apparatus according to claim 13, characterised in that the carriage (18) has external wheels (19) by which it rolls along inside the duct.

15. Apparatus according to claim 13 or claim 14, characterised in that the carriage (18) extends forwardly to surround all or part of the front portion (6) .

16. Apparatus according to claim 8, characterised in that the outer member has the heating means (8), so that, in use, the layer (3) of composite material is heated from the outside, and the inner member has the support means (26) providing the air gap (14) between the inside of the layer and the inner member.

17. Apparatus according to any preceding claim, characterised in that the liner (2) includes outer thermoplastics layer (4) between the duct (1) and the layer (3) of composite material.

18. A method of lining a duct comprising: inserting into the duct (1) a flexible liner (2) including a layer (3) of composite material comprising thermoplastics material and reinforcing fibres; producing hot gas on one side of the layer (3) of composite material and forcing the hot gas under pressure through the layer (3) of composite material while maintaining an air gap (14) on the opposite side of the layer (3) , to melt the thermoplastics material; applying pressure to the heated layer (3) to force it towards the duct (1) for consolidation; and allowing the liner (2) to cool under pressure whilst in contact with the duct (1) to harden the layer (3) of composite material into a structural member.

19. A method according to claim 18, characterised in that the hot gas is directed from the air gap (14) to provide pre-heating of the liner (2) .

20. A method according to claim 18 , or claim 19, characterised in that the liner (2) is inserted into the duct (1) in a collapsed configuration and is subsequently expanded.

21. A method according to any of claims 18 to 20, characterised in that after insertion of the liner (2) into the duct (1) apparatus as defined in any of claims 1 to 17 is passed through the duct to perform the method.

22. A combination of apparatus and a flexible liner for forming a structural member to line a duct, in which the liner (2) includes a layer (3) of composite material comprising thermoplastics material and reinforcing fibres, and is adapted for insertion into the duct (1) , and the apparatus has a front portion (6) adapted to be inserted in the liner (2) , a central portion (7) having heating means (8) on one side of the layer (3) of composite material, and a rear portion (10) having consolidation means (11) for forcing the heated layer (3) of composite material towards the duct (1) for consolidation and cooling under pressure to form the structural member, characterised in that the heating means (8) produces hot gas which is forced under pressure through the layer (3) of composite material to heat the layer (3) , the combination being so constructed and arranged that there is an air gap on the opposite side of the layer of composite material while heating takes place.

23. A combination according to claim 22, characterised in that the apparatus is as defined in any one of claims 1 to 17.

24. A combination according to claim 22 or claim 23, characterised in that the liner (2) comprises the layer (3) of composite material together with an outer layer (4) of thermoplastics material.