CA2419449A1 - Method for lining a pipe or main - Google Patents
Method for lining a pipe or main Download PDFInfo
- Publication number
- CA2419449A1 CA2419449A1 CA002419449A CA2419449A CA2419449A1 CA 2419449 A1 CA2419449 A1 CA 2419449A1 CA 002419449 A CA002419449 A CA 002419449A CA 2419449 A CA2419449 A CA 2419449A CA 2419449 A1 CA2419449 A1 CA 2419449A1
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- CA
- Canada
- Prior art keywords
- pipe
- main
- liner
- liner pipe
- grooves
- 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.)
- Abandoned
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L55/00—Devices or appurtenances for use in, or in connection with, pipes or pipe systems
- F16L55/16—Devices for covering leaks in pipes or hoses, e.g. hose-menders
- F16L55/162—Devices for covering leaks in pipes or hoses, e.g. hose-menders from inside the pipe
- F16L55/165—Devices for covering leaks in pipes or hoses, e.g. hose-menders from inside the pipe a pipe or flexible liner being inserted in the damaged section
- F16L55/1652—Devices for covering leaks in pipes or hoses, e.g. hose-menders from inside the pipe a pipe or flexible liner being inserted in the damaged section the flexible liner being pulled into the damaged section
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
- Application Of Or Painting With Fluid Materials (AREA)
Abstract
The present invention relates to lining a pipe or main (40) and is particularly directed to the lining of underground gas, water mains or seer pipes. The invention discloses a method comprising providing a liner pipe (20) wit means (81,84) to convey fluid along its outside surface; providing a pipe or main to be lined with a vent (80) to enable fluid to pass through a wall of the pipe or main and passing the liner pipe through the pipe or main to line the pipe or main such that at least a portion of the means to convey fluid along the outside surface of the liner pipe is in fluid communication with the vent in the pipe or main.
Description
METHOD FOR LINTNG A PIPE OR MAIN
The present invention relates to a method for lining a pipe or main and is particularly directed to the lining of underground gas or water mains or sewer pipes.
A method for lining a pipe or main is known comprising providing a length of synthetic-resin liner pipe of external diameter substantially equal to or greater than the internal diameter of the pipe or main to be lined. The liner pipe is mechanically deformed to reduce its external diameter to less than the. internal diameter of the pipe or main to be lined, generally by pulling the liner pipe through a die. The liner pipe of reduced diameter is then caused to enter the pipe or main to be lined. This method is known by the registered trade mark 'swagelining'. Examples of this method are described in GB 2186340, GB 2218370, GB 2218484, GB 2218485, GB 2218486, GB 2218487, GB 2218488, GB 2218489, GB 2221741, GB 2242850, GB 2257767, GB 2257768 and GB 2288216.
However, the liner pipe may become at least slightly porous, especially when the lined pipe or main conveys high pressure fluid. Some conveyed fluid may pass through the wall of the liner to between the liner and the pipe or main. When the flow of fluid through the lined pipe is stopped or interrupted reducing the pressure within the liner, the CONFIRMATION COPY
The present invention relates to a method for lining a pipe or main and is particularly directed to the lining of underground gas or water mains or sewer pipes.
A method for lining a pipe or main is known comprising providing a length of synthetic-resin liner pipe of external diameter substantially equal to or greater than the internal diameter of the pipe or main to be lined. The liner pipe is mechanically deformed to reduce its external diameter to less than the. internal diameter of the pipe or main to be lined, generally by pulling the liner pipe through a die. The liner pipe of reduced diameter is then caused to enter the pipe or main to be lined. This method is known by the registered trade mark 'swagelining'. Examples of this method are described in GB 2186340, GB 2218370, GB 2218484, GB 2218485, GB 2218486, GB 2218487, GB 2218488, GB 2218489, GB 2221741, GB 2242850, GB 2257767, GB 2257768 and GB 2288216.
However, the liner pipe may become at least slightly porous, especially when the lined pipe or main conveys high pressure fluid. Some conveyed fluid may pass through the wall of the liner to between the liner and the pipe or main. When the flow of fluid through the lined pipe is stopped or interrupted reducing the pressure within the liner, the CONFIRMATION COPY
2 pressure of the fluid between the liner and the pipe or main may cause the liner pipe to collapse.
According to the present invention the liner pipe is provided with means to convey fluid along the length of its outside surface and a vent is provided in fluid communication with the means to convey fluid along the outside surface of the liner pipe.
The present invention enables fluid trapped between the liner and the pipe or main to be expelled through the vent preventing collapse of the liner when fluid flow is stopped or interrupted. The vent may be provided with a one way valve. The means to convey fluid along the outside surface of the liner pipe may comprise one or more grooves along the length of the liner pipe. The grooves or ridges may form one or more longitudinal passages along the length. of the outside surface of the liner pipe. If there are more than one longitudinal passages along the length of the liner pipe they may be interconnected at one or more points along their length. The groove may be arranged spirally around the liner pipe or a plurality of passages may be provided in an array around the liner pipe. The means for conveying fluid along the outside surface of the liner pipe may comprise one
According to the present invention the liner pipe is provided with means to convey fluid along the length of its outside surface and a vent is provided in fluid communication with the means to convey fluid along the outside surface of the liner pipe.
The present invention enables fluid trapped between the liner and the pipe or main to be expelled through the vent preventing collapse of the liner when fluid flow is stopped or interrupted. The vent may be provided with a one way valve. The means to convey fluid along the outside surface of the liner pipe may comprise one or more grooves along the length of the liner pipe. The grooves or ridges may form one or more longitudinal passages along the length. of the outside surface of the liner pipe. If there are more than one longitudinal passages along the length of the liner pipe they may be interconnected at one or more points along their length. The groove may be arranged spirally around the liner pipe or a plurality of passages may be provided in an array around the liner pipe. The means for conveying fluid along the outside surface of the liner pipe may comprise one
3 or more conduits provided with means for fluid to enter or leave the conduits.
Before causing the liner to enter the pipe or main the liner may be heated to assist the reduction of its diameter.
However, the liner need not be heated and may be used to line the pipe or main in normal atmospheric or 'cold' conditions.
An example of the present invention will now be particularly described with reference to the drawings in which:
Figure 1 is a plan view of a rig suitable to preheat and reduce the external diameter of a length of liner pipe, Figure 2 is a more detailed cross-section of the front end of the rig in use, Figures 3 to 9 show in schematic form a typical sequence of operations in the lining of a section of an existing main and Figures 10 and 11 are longitudinal sections through one form of device for closing the ends of the liner pipe so that it can be expanded by pressurisation, Figure 10 showing the situation before expansion and Figure 11 the situation after expansion.
Before causing the liner to enter the pipe or main the liner may be heated to assist the reduction of its diameter.
However, the liner need not be heated and may be used to line the pipe or main in normal atmospheric or 'cold' conditions.
An example of the present invention will now be particularly described with reference to the drawings in which:
Figure 1 is a plan view of a rig suitable to preheat and reduce the external diameter of a length of liner pipe, Figure 2 is a more detailed cross-section of the front end of the rig in use, Figures 3 to 9 show in schematic form a typical sequence of operations in the lining of a section of an existing main and Figures 10 and 11 are longitudinal sections through one form of device for closing the ends of the liner pipe so that it can be expanded by pressurisation, Figure 10 showing the situation before expansion and Figure 11 the situation after expansion.
4 Referring to Figure 1 the rig 1 comprises a heater tube 2 which in use is supported above ground on a support frame 3 (see also Figures 5 and 6). The tube 2 has a rear end 4 to receive a liner pipe for preheating on passage through the tube 2 and a front end 5 adapted to reduce the external diameter of the preheated liner pipe.
Extending parallel to the heater tube 2 is a smaller diameter tube 6 serving to provide hot gas for preheating a liner pipe within the heater tube 2.
The tube 6 is closed at a rear end 7 by an apertured plate ~8 through the aperture of which extends a gas supply pipe 9 for supplying gas to a gas fired burner 10 located within the tube 6. The tube 6 is provided with an air-take 11 at a point adjacent to the plate 8 to supply air for combustion of the gas within the burner 10.
Hot gas supplied by the burner 10 travels forwardly in the direction of the arrows to. an elongated chamber 12 forming the front end of the tube 8. The chamber 12 terminates in a distributor 13 which has a rectangular outlet 14 communicating with a similar shaped rectangular slot in the wall of the heater tube 2. In this way the hot gas is caused to renter the heater tube 2 from the chamber 12 radially at a point adjacent to its front end 5 taking the direction of the arrows. Once inside the tube 2, the gas travels rearwardly in the direction of the arrows.
Some of the hot gas then leaves the tube 2 by way of an exhaust pipe 15 located adjacent to the rear end 4 of the tube 2. The remaining majority of the hot gas re-enters the tube 6 by way of a radial tube 16 connecting the tubes 2 and 6 at a point adjacent to their rear ends.
The chamber l2 is provided with a circulating fan 17 to cause the circulation of the gas within the assembly to be accelerated.
Referring to Figures 1 and 2 the front end of~the tube 2 is formed by two swaging dies 18 and 19 serving in use to reduce the external diameter of the liner pipe 20 being drawn therethrough.
A first die 18 is located within the tube 2 and is held within a die holder 21 secured to the internal wall of the tube 2. The first die 18 has a forwardly tapering entry section 22 leading to a circular exit section 23. The tapering entry section 22 serves to provide the initial and major proportion of the reduction in the external diameter of the preheated liner pipe 20 as shown in Figure 2.
The second die 19 is located beyond the end of the tube 2 and is bolted to a circular flange 24 welded to the outer surface of the tube 2. The second die has a forwardly tapering aperture 25 serving to provide a final and minor proportion of the reduction in the external diameter of the preheated liner pipe 20.
In use, the preheated liner pipe 20 is drawn sequentially through the dies 18 and 19 by means of the cable 26 of the winch (shown in Figure 4). To achieve this the leading end of the liner pipe 20 is formed in the shape of a cone 28 by cutting the end of the liner pipe 20 into suitably triangular portions 29, folding the portions 29 to form the cone 28 and then welding adjacent portions 29 together. These portions 29 are formed with holes to receive the ends of bolts 30 and gaps 31 are Left between the portions 29 so that when the cone 28 has been formed the inside of the cone 28 can be accessed manually to place nuts 32 on the ends of the bolts 30. Next a steel cone 33 matching the tip of the pipe cone 28 is placed over the tip as shown in Figure 2, the steel cone 33 having holes to correspond with those in the pipe cone 28, and the cones 28 and 33 are bolted together by the nuts and bolts 30 and 32.
The steel cane 33 has an eye 34 which is in use as shown in Figure 2 connected to the cable 26 of the winch.
The internal diameter of the wall of tube 2 is greater than the external diameter of the liner pipe 20 so that an annular space 35 is formed between the outer wall of the liner pipe 20 and the inner wall of the tube 2. In use, this space 35 when the liner pipe 20 is within the tube 2 is enclosed at one end by the internal die 18 and at the other end by an apertured plate 36 attached to the rear end 4 of the tube 2, the wall of the aperture 37 in the plate 36 forming a close fit with the external wall of the liner pipe 20. Thus, the hot gas entering the tube 2 from the distributor 13 is caused to flow within the enclosed annular space 35 to heat the external wall of the liner pipe 20.
Referring to Figures 3 to 9, in the first stage of the lining process (Figure 3) the section 40 of the main 41 to be lined has ends 42, 43 isolated from adjacent portions 44, 45 ~of the main 41. This is done by digging excavations 46, 47 at two distant points in the main 41 and then removing pieces from the main 41 to expose the ends 42, 43 of the section 40, In the next stage of the process (Figure 4) a motorised winch 48 is mounted at ground level adj acent to the end 42 of the main section 40. A stiff rod 49 is then pushed along the main section 40 from the end 42 to the end 43. That end 50 of the rod 49 nearest the winch 48 is connected to the winch cable 26 after the cable 26 has been fed through guide rolls 51 mounted on the floor of the excavation 46. The rod 49 is then pushed completely through the main section 40 so that the cable 26 eventually emerges from the end 43 of the section 40. The cable 26 is then detached from the rod 49 and is fed through the reducing rig 1 as shown in Figure 5.
The cable 26 is then attached to the leading end of the pipe liner 20 in the manner previously described with reference to Figure 2. Sections of the pipe liner 20 are fed successively to a butt-welding machine 60 located upstream of the reducing rig 1. The machine 60 enables adj oining ends of the pipe liner sections 20 to be butt welded together to form a continuous length. The machine 60 may have facilities for removing both internal and external weld beads from the pipe liner which ideally is of polyethylene. The outside surface of the pipe liner 20 is provided with grooves along its length to enable fluid to pass along the length of the pipe liner 20 between the pipe liner 20 and the main section 40 when fitted.
The motor of the winch 48 is then actuated to draw the cable 26 towards the end 43 of the main section 40 as shown in Figure 6. This causes the liner pipe 20 to enter the heater 2 through which hot gas is circulating. The liner pipe 20 is then preheated by the gas in the manner previously described to a temperature of about 100°C and the preheated pipe 20 is then drawn through the dies to effect a reduction in the external diameter of the pipe 20 to an extent permitting the reduced diameter pipe 61 to enter the end 43 of the main section 40 by way of guide rolls 62 mounted on the floor of the excavation 47.
The reduced diameter pipe 61 is then drawn as a continuous length along the main section 40 to and out of the far end 42 as shown in figure 7. The reduction in diameter of the liner pipe 20 may be of the order of 30 or more.
Once the liner pipe 20 has reached and extended beyond the far end 42 of the main section 40, the winch cable 26 is disconnected from the eye 34 on the steel cone 33. ~ The steel cone 33 is then removed from the pipe cone 38 thus leaving the liner pipe 20 with ends 62 and 63 lying exposed beyond the ends 42, 43 of the main section 40.
The liner pipe 20 may be left to expand into contact with the internal wall of the main section 40.
However, in this example both ends of the pipe 20 are closed by closures 64 and air is injected into one end of the pipe 20 by mews of a compressor 65 mounted at ground level adjacent to the end 63 of the main section 40 as shown in Figure 8. The air is injected at super atmospheric pressure e.g. 2 to 67 bar for an extended period say 24 hours. This causes the liner pipe 20 to expand into contact with the internal wall of the main section 40 as shown in Figure 9.
A suitable closure 64 for the liner pipe 20 is shown in Figures 10 and 11. The closure 64 comprises a tubular sleeve 66 for receiving one end of the liner pipe 20 and a cap 67 for attachment to the sleeve 66.
The cap 67 has a cylindrical portion 68 having an outwardly flanged open end 69 for connection to a similar outwardly flanged end 70 on the sleeve 66 by means of several nut and bolt assemblies 72 (only two shown). The cap 67 has one end closed by a plate 72 which has a valve 73 which is adapted when open to connect the interior of the closure 64 to a compressor or like device for supplying air under pressure to the closure 64. Alternatively the valve 73 can be closed when the closure 64 is serving as a seal for preventing the escape of air from one end of the liner pipe 20 when air is being injected at the other end.
Located in two circumferential grooves 74 on the inner surface 75 of the sleeve 66 are two O-ring seals 76 which are arranged tc~ engage the outer surface 77 of the liner pipe 20 when an end of the pipe is located within the sleeve 66.
These seals 76 form a seal outer surface 77 between of the the liner pipe 20 and the inner surface 75 the sleeve of 66 and permit movement of the liner pipe withinthe sleeve since the liner pipe 20 expands radially and contracts longitudinally as pressure is applied the to interior of the liner pipe 20.
In use, both the exposed ends of the liner pipe 20 are closed with a closure device 64. The sleeve 66 may have a recessed end portion 78 to fit over the spigot end of the main section 40 as shown in Figures 10 and 11. Each closure 64 is supported against the internal walls of the excavation by means of struts 79 extending outwardly from the cap 67 to prevent its being blown off during pressurisation of the closure 64. One of the closure devices 64 is connected to the compressor 65 by means of the valve 73 which is opened..
The valve 73 of the other closure device is closed. Air is then supplied by the compressor to pressusrise the liner pipe 20. After use, the closure devices 64 are removed and the ends of the liner pipe 20 are connected up to the adjacent portions 44 and 45 of the main 41 by conventional means.
The pressurisation of the liner pipe may form part of a standard pressure test to test the soundness of the liner pipe.
A vent 80 is provided in the wall of the main section 40 as shown in Figures 10 and 11. In this example the vent 80 also passes through the end position 78 of sleeve 66, but the vent 80 could be positioned at a portion of the main section 40 which is clear, of the sleeve 66 to avoid having to pass through sleeve 66. Grooves 81 are are provided in the outside wall of liner pipeline 20 such that when the main section 40 is lined with the liner pipe 20, the vent 80 is in fluid communication with grooves 81 to enable gas which may for example have passed through the slightly porous liner 20 to escape from the region between the liner pipe 20 and the main section 40. The vent 80 is provided with a valve 82 to enable fluid to escape. The longitudinal grooves 81 are provided with one or more transverse grooves 84 to interconnect them and enable trapped fluid to reach the vent 80.
This means to convey fluid along the outside surface of the liner pipe 20 may not necessarily be as described above. For example there may be provided one or more grooves arranged spirally around the outside surface of the liner pipe 20 or an array of grooves arranged around the outside surface of the liner pipe 20, with the grooves in fluid communication with the vent 80. Alternatively, instead of grooves there may be pro~rided one or more conduits arranged between the outside surface of the liner pipe 20 and the inside surface of main section 40 with means for fluid to enter or leave the conduits such as a number of holes, with the conduits being in fluid communication with the vent 80.
Many alterations may be made to the example described above whilst still falling within the scope of the invention. For example the liner pipe 20 need not be heated before~being passed through the dies but could simply be pulled through at its normal or ambient temperature.
Extending parallel to the heater tube 2 is a smaller diameter tube 6 serving to provide hot gas for preheating a liner pipe within the heater tube 2.
The tube 6 is closed at a rear end 7 by an apertured plate ~8 through the aperture of which extends a gas supply pipe 9 for supplying gas to a gas fired burner 10 located within the tube 6. The tube 6 is provided with an air-take 11 at a point adjacent to the plate 8 to supply air for combustion of the gas within the burner 10.
Hot gas supplied by the burner 10 travels forwardly in the direction of the arrows to. an elongated chamber 12 forming the front end of the tube 8. The chamber 12 terminates in a distributor 13 which has a rectangular outlet 14 communicating with a similar shaped rectangular slot in the wall of the heater tube 2. In this way the hot gas is caused to renter the heater tube 2 from the chamber 12 radially at a point adjacent to its front end 5 taking the direction of the arrows. Once inside the tube 2, the gas travels rearwardly in the direction of the arrows.
Some of the hot gas then leaves the tube 2 by way of an exhaust pipe 15 located adjacent to the rear end 4 of the tube 2. The remaining majority of the hot gas re-enters the tube 6 by way of a radial tube 16 connecting the tubes 2 and 6 at a point adjacent to their rear ends.
The chamber l2 is provided with a circulating fan 17 to cause the circulation of the gas within the assembly to be accelerated.
Referring to Figures 1 and 2 the front end of~the tube 2 is formed by two swaging dies 18 and 19 serving in use to reduce the external diameter of the liner pipe 20 being drawn therethrough.
A first die 18 is located within the tube 2 and is held within a die holder 21 secured to the internal wall of the tube 2. The first die 18 has a forwardly tapering entry section 22 leading to a circular exit section 23. The tapering entry section 22 serves to provide the initial and major proportion of the reduction in the external diameter of the preheated liner pipe 20 as shown in Figure 2.
The second die 19 is located beyond the end of the tube 2 and is bolted to a circular flange 24 welded to the outer surface of the tube 2. The second die has a forwardly tapering aperture 25 serving to provide a final and minor proportion of the reduction in the external diameter of the preheated liner pipe 20.
In use, the preheated liner pipe 20 is drawn sequentially through the dies 18 and 19 by means of the cable 26 of the winch (shown in Figure 4). To achieve this the leading end of the liner pipe 20 is formed in the shape of a cone 28 by cutting the end of the liner pipe 20 into suitably triangular portions 29, folding the portions 29 to form the cone 28 and then welding adjacent portions 29 together. These portions 29 are formed with holes to receive the ends of bolts 30 and gaps 31 are Left between the portions 29 so that when the cone 28 has been formed the inside of the cone 28 can be accessed manually to place nuts 32 on the ends of the bolts 30. Next a steel cone 33 matching the tip of the pipe cone 28 is placed over the tip as shown in Figure 2, the steel cone 33 having holes to correspond with those in the pipe cone 28, and the cones 28 and 33 are bolted together by the nuts and bolts 30 and 32.
The steel cane 33 has an eye 34 which is in use as shown in Figure 2 connected to the cable 26 of the winch.
The internal diameter of the wall of tube 2 is greater than the external diameter of the liner pipe 20 so that an annular space 35 is formed between the outer wall of the liner pipe 20 and the inner wall of the tube 2. In use, this space 35 when the liner pipe 20 is within the tube 2 is enclosed at one end by the internal die 18 and at the other end by an apertured plate 36 attached to the rear end 4 of the tube 2, the wall of the aperture 37 in the plate 36 forming a close fit with the external wall of the liner pipe 20. Thus, the hot gas entering the tube 2 from the distributor 13 is caused to flow within the enclosed annular space 35 to heat the external wall of the liner pipe 20.
Referring to Figures 3 to 9, in the first stage of the lining process (Figure 3) the section 40 of the main 41 to be lined has ends 42, 43 isolated from adjacent portions 44, 45 ~of the main 41. This is done by digging excavations 46, 47 at two distant points in the main 41 and then removing pieces from the main 41 to expose the ends 42, 43 of the section 40, In the next stage of the process (Figure 4) a motorised winch 48 is mounted at ground level adj acent to the end 42 of the main section 40. A stiff rod 49 is then pushed along the main section 40 from the end 42 to the end 43. That end 50 of the rod 49 nearest the winch 48 is connected to the winch cable 26 after the cable 26 has been fed through guide rolls 51 mounted on the floor of the excavation 46. The rod 49 is then pushed completely through the main section 40 so that the cable 26 eventually emerges from the end 43 of the section 40. The cable 26 is then detached from the rod 49 and is fed through the reducing rig 1 as shown in Figure 5.
The cable 26 is then attached to the leading end of the pipe liner 20 in the manner previously described with reference to Figure 2. Sections of the pipe liner 20 are fed successively to a butt-welding machine 60 located upstream of the reducing rig 1. The machine 60 enables adj oining ends of the pipe liner sections 20 to be butt welded together to form a continuous length. The machine 60 may have facilities for removing both internal and external weld beads from the pipe liner which ideally is of polyethylene. The outside surface of the pipe liner 20 is provided with grooves along its length to enable fluid to pass along the length of the pipe liner 20 between the pipe liner 20 and the main section 40 when fitted.
The motor of the winch 48 is then actuated to draw the cable 26 towards the end 43 of the main section 40 as shown in Figure 6. This causes the liner pipe 20 to enter the heater 2 through which hot gas is circulating. The liner pipe 20 is then preheated by the gas in the manner previously described to a temperature of about 100°C and the preheated pipe 20 is then drawn through the dies to effect a reduction in the external diameter of the pipe 20 to an extent permitting the reduced diameter pipe 61 to enter the end 43 of the main section 40 by way of guide rolls 62 mounted on the floor of the excavation 47.
The reduced diameter pipe 61 is then drawn as a continuous length along the main section 40 to and out of the far end 42 as shown in figure 7. The reduction in diameter of the liner pipe 20 may be of the order of 30 or more.
Once the liner pipe 20 has reached and extended beyond the far end 42 of the main section 40, the winch cable 26 is disconnected from the eye 34 on the steel cone 33. ~ The steel cone 33 is then removed from the pipe cone 38 thus leaving the liner pipe 20 with ends 62 and 63 lying exposed beyond the ends 42, 43 of the main section 40.
The liner pipe 20 may be left to expand into contact with the internal wall of the main section 40.
However, in this example both ends of the pipe 20 are closed by closures 64 and air is injected into one end of the pipe 20 by mews of a compressor 65 mounted at ground level adjacent to the end 63 of the main section 40 as shown in Figure 8. The air is injected at super atmospheric pressure e.g. 2 to 67 bar for an extended period say 24 hours. This causes the liner pipe 20 to expand into contact with the internal wall of the main section 40 as shown in Figure 9.
A suitable closure 64 for the liner pipe 20 is shown in Figures 10 and 11. The closure 64 comprises a tubular sleeve 66 for receiving one end of the liner pipe 20 and a cap 67 for attachment to the sleeve 66.
The cap 67 has a cylindrical portion 68 having an outwardly flanged open end 69 for connection to a similar outwardly flanged end 70 on the sleeve 66 by means of several nut and bolt assemblies 72 (only two shown). The cap 67 has one end closed by a plate 72 which has a valve 73 which is adapted when open to connect the interior of the closure 64 to a compressor or like device for supplying air under pressure to the closure 64. Alternatively the valve 73 can be closed when the closure 64 is serving as a seal for preventing the escape of air from one end of the liner pipe 20 when air is being injected at the other end.
Located in two circumferential grooves 74 on the inner surface 75 of the sleeve 66 are two O-ring seals 76 which are arranged tc~ engage the outer surface 77 of the liner pipe 20 when an end of the pipe is located within the sleeve 66.
These seals 76 form a seal outer surface 77 between of the the liner pipe 20 and the inner surface 75 the sleeve of 66 and permit movement of the liner pipe withinthe sleeve since the liner pipe 20 expands radially and contracts longitudinally as pressure is applied the to interior of the liner pipe 20.
In use, both the exposed ends of the liner pipe 20 are closed with a closure device 64. The sleeve 66 may have a recessed end portion 78 to fit over the spigot end of the main section 40 as shown in Figures 10 and 11. Each closure 64 is supported against the internal walls of the excavation by means of struts 79 extending outwardly from the cap 67 to prevent its being blown off during pressurisation of the closure 64. One of the closure devices 64 is connected to the compressor 65 by means of the valve 73 which is opened..
The valve 73 of the other closure device is closed. Air is then supplied by the compressor to pressusrise the liner pipe 20. After use, the closure devices 64 are removed and the ends of the liner pipe 20 are connected up to the adjacent portions 44 and 45 of the main 41 by conventional means.
The pressurisation of the liner pipe may form part of a standard pressure test to test the soundness of the liner pipe.
A vent 80 is provided in the wall of the main section 40 as shown in Figures 10 and 11. In this example the vent 80 also passes through the end position 78 of sleeve 66, but the vent 80 could be positioned at a portion of the main section 40 which is clear, of the sleeve 66 to avoid having to pass through sleeve 66. Grooves 81 are are provided in the outside wall of liner pipeline 20 such that when the main section 40 is lined with the liner pipe 20, the vent 80 is in fluid communication with grooves 81 to enable gas which may for example have passed through the slightly porous liner 20 to escape from the region between the liner pipe 20 and the main section 40. The vent 80 is provided with a valve 82 to enable fluid to escape. The longitudinal grooves 81 are provided with one or more transverse grooves 84 to interconnect them and enable trapped fluid to reach the vent 80.
This means to convey fluid along the outside surface of the liner pipe 20 may not necessarily be as described above. For example there may be provided one or more grooves arranged spirally around the outside surface of the liner pipe 20 or an array of grooves arranged around the outside surface of the liner pipe 20, with the grooves in fluid communication with the vent 80. Alternatively, instead of grooves there may be pro~rided one or more conduits arranged between the outside surface of the liner pipe 20 and the inside surface of main section 40 with means for fluid to enter or leave the conduits such as a number of holes, with the conduits being in fluid communication with the vent 80.
Many alterations may be made to the example described above whilst still falling within the scope of the invention. For example the liner pipe 20 need not be heated before~being passed through the dies but could simply be pulled through at its normal or ambient temperature.
Claims (17)
1. A method for lining a pipe or main, the method comprising providing a liner pipe with means to convey fluid along its outside surface;
providing a pipe or main to be lined with a vent to enable fluid to pass through a wall of the pipe or main and passing the liner pipe through the pipe or main to line the pipe or main such that at least a portion of the means to convey fluid along the outside surface of the liner pipe is in fluid communication with the vent in the pipe or main.
providing a pipe or main to be lined with a vent to enable fluid to pass through a wall of the pipe or main and passing the liner pipe through the pipe or main to line the pipe or main such that at least a portion of the means to convey fluid along the outside surface of the liner pipe is in fluid communication with the vent in the pipe or main.
2. A method according to claim 1, wherein the liner pipe is passed through the pipe or main to line the pipe or main by first being passed through a die to reduce its external diameter to less than the internal diameter of the pipe or main to be lined.
3. A method according to claim 1 or claim 2, wherein the means to convey fluid along the outside of the liner pipe is one or more grooves in the outside surface of the liner pipe.
4. A method according to claim 3, wherein the groove or grooves extend in the axial direction of the liner pipe.
5. A method according to claim 4, wherein one or more grooves are also provided to extend in a direction transverse to the grooves in the axial direction,
6. A method according to claim 5, wherein the one ar more grooves in the axial direction are in fluid communication with the grooves in the transverse direction.
7. A method according to claim 3, wherein the one or more grooves extend spirally around the axis of the liner pipe.
8. A method according to claim 1 or claim 2, wherein the means to convey fluid along the outside surface of the liner pipe comprises one or more ridges.
9. A method according to claim 1 or claim 2, wherein the means to convey fluid along the outside surface of the liner pipe comprises one or more conduits provided with means for fluid to enter the conduits.
10. A method according to claim 9, wherein the conduits are arranged in the axial direction of the liner pipe and the means for fluid to enter the conduits comprises one or more holes in the walls of the conduits.
11. A liner pipe for use in lining a surrounding pipe or main, the liner pipe comprising means to convey fluid along its outside surface when installed within a surrounding pipe or main with a vent in the surrounding pipe or main.
22. A liner pipe according to claim 11, wherein the means to convey fluid along the outside surface of the liner pipe is one or more grooves in the outside surface of the liner pipe.
13. A liner pipe according to claim 12, wherein the grooves are arranged axially along the length of the liner pipe.
14. A pipe or main lined with a liner pipe according to the method of claim 1.
15. A method of lining a pipe or main substantially as described herein with reference to the accompanying drawings.
16. A liner pipe substantially as described herein with reference to the accompanying drawings.
17. A lined pipe or main substantially as described herein with reference to the accompanying drawings.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB0020011.3 | 2000-08-15 | ||
| GB0020011A GB0020011D0 (en) | 2000-08-15 | 2000-08-15 | Method for lining a pipe or main |
| PCT/GB2001/003598 WO2002014731A1 (en) | 2000-08-15 | 2001-08-13 | Method for lining a pipe or main |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA2419449A1 true CA2419449A1 (en) | 2002-02-21 |
Family
ID=9897602
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA002419449A Abandoned CA2419449A1 (en) | 2000-08-15 | 2001-08-13 | Method for lining a pipe or main |
Country Status (6)
| Country | Link |
|---|---|
| EP (1) | EP1311782A1 (en) |
| AR (1) | AR030450A1 (en) |
| AU (1) | AU2001276562A1 (en) |
| CA (1) | CA2419449A1 (en) |
| GB (2) | GB0020011D0 (en) |
| WO (1) | WO2002014731A1 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB0203638D0 (en) * | 2002-02-15 | 2002-04-03 | Lattice Intellectual Property | Method for lining a pipe or main |
Family Cites Families (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3506039A (en) * | 1967-11-09 | 1970-04-14 | Dow Chemical Co | Venting of lined pipe |
| DE2915838A1 (en) * | 1979-04-17 | 1980-10-23 | Mannesmann Ag | Double-wall exhaust pipe - has one pipe wall longitudinally ribbed providing axial grooves between them, with pipes tightly fitting together |
| AT389580B (en) * | 1981-11-16 | 1989-12-27 | Eternit Werke Hatschek L | PIPELINE SYSTEM, IN PARTICULAR MULTI-CHANNEL PIPELINE SYSTEM, AND METHOD FOR THE PRODUCTION THEREOF |
| DE3767499D1 (en) | 1986-02-10 | 1991-02-28 | British Gas Plc | METHOD FOR COATING PIPES OR LINES. |
| GB2218484B (en) | 1988-05-09 | 1992-02-12 | British Gas Plc | Pipelines |
| GB2218488B (en) | 1988-05-09 | 1992-10-21 | British Gas Plc | Pipelines. |
| GB2221741B (en) | 1988-08-11 | 1992-02-12 | British Gas Plc | Pipelining and liner pipe swaging dies |
| GB2218487B (en) | 1988-05-09 | 1992-07-29 | British Gas Plc | Pipelines. |
| GB2218370B (en) | 1988-05-09 | 1992-07-22 | British Gas Plc | Pipelining and liner pipe swaging dies. |
| GB2218486B (en) | 1988-05-09 | 1993-02-03 | British Gas Plc | Piplines. |
| GB2218485B (en) | 1988-05-09 | 1992-02-12 | British Gas Plc | Pipelines |
| GB2218489B (en) | 1988-05-09 | 1992-05-13 | British Gas Plc | Pipeline liner pipes and liner pipe swaging dies |
| GB8925104D0 (en) | 1989-11-07 | 1989-12-28 | British Gas Plc | Cutting apparatus |
| US5072622A (en) * | 1990-06-04 | 1991-12-17 | Roach Max J | Pipeline monitoring and leak containment system and apparatus therefor |
| NL9100403A (en) * | 1991-03-06 | 1992-10-01 | Wavin Bv | METHOD AND APPARATUS FOR INSTALLING AN INNER TUBE IN AN EXISTING PIPE WITH THE USE OF VENTILATORS AND WITH AN INNER TUBE CONTAINING THERMOPLASTIC ARTICLES INCLUDED HEREIN. |
| AU3066792A (en) * | 1991-11-05 | 1993-06-07 | Markel Corporation | Fuel system conduit and method of making same |
| NL9201566A (en) * | 1992-09-09 | 1994-04-05 | Wavin Bv | Method for arranging an inner pipe in an existing pipeline, using venting means and a radial seal with insert sleeve, as well as a pipeline of this nature |
| NL9201620A (en) * | 1992-09-18 | 1994-04-18 | Wavin Bv | Method and device for arranging an inner tube in an existing pipeline with a continuous supply of heat, and a pipeline thus obtained. |
| EP1105668A4 (en) * | 1998-07-28 | 2005-11-23 | Safety Liner Systems Llc | Enhancement of profiled tubular lining systems by channel augmentation |
-
2000
- 2000-08-15 GB GB0020011A patent/GB0020011D0/en not_active Ceased
-
2001
- 2001-08-13 AU AU2001276562A patent/AU2001276562A1/en not_active Abandoned
- 2001-08-13 CA CA002419449A patent/CA2419449A1/en not_active Abandoned
- 2001-08-13 EP EP01954218A patent/EP1311782A1/en not_active Withdrawn
- 2001-08-13 WO PCT/GB2001/003598 patent/WO2002014731A1/en not_active Application Discontinuation
- 2001-08-14 GB GB0119567A patent/GB2367601A/en not_active Withdrawn
- 2001-08-14 AR ARP010103879A patent/AR030450A1/en unknown
Also Published As
| Publication number | Publication date |
|---|---|
| GB0119567D0 (en) | 2001-10-03 |
| EP1311782A1 (en) | 2003-05-21 |
| GB2367601A (en) | 2002-04-10 |
| WO2002014731A1 (en) | 2002-02-21 |
| GB0020011D0 (en) | 2000-10-04 |
| AU2001276562A1 (en) | 2002-02-25 |
| AR030450A1 (en) | 2003-08-20 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request | ||
| FZDE | Discontinued |