GB2140894A - Sealing ducts - Google Patents

Sealing ducts Download PDF

Info

Publication number
GB2140894A
GB2140894A GB08413015A GB8413015A GB2140894A GB 2140894 A GB2140894 A GB 2140894A GB 08413015 A GB08413015 A GB 08413015A GB 8413015 A GB8413015 A GB 8413015A GB 2140894 A GB2140894 A GB 2140894A
Authority
GB
United Kingdom
Prior art keywords
bag
duct
neck
support member
fabric
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
GB08413015A
Other versions
GB2140894B (en
GB8413015D0 (en
Inventor
Alec Reginald Carruthers
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.)
ALH Systems Ltd
Original Assignee
ALH Systems Ltd
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
Priority claimed from GB838315198A external-priority patent/GB8315198D0/en
Application filed by ALH Systems Ltd filed Critical ALH Systems Ltd
Priority to GB08413015A priority Critical patent/GB2140894B/en
Publication of GB8413015D0 publication Critical patent/GB8413015D0/en
Publication of GB2140894A publication Critical patent/GB2140894A/en
Application granted granted Critical
Publication of GB2140894B publication Critical patent/GB2140894B/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16LPIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L55/00Devices or appurtenances for use in, or in connection with, pipes or pipe systems
    • F16L55/10Means for stopping flow from or in pipes or hoses
    • F16L55/12Means for stopping flow from or in pipes or hoses by introducing into the pipe a member expandable in situ
    • F16L55/124Means for stopping flow from or in pipes or hoses by introducing into the pipe a member expandable in situ introduced radially into the pipe or hose
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16KVALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K7/00Diaphragm valves or cut-off apparatus, e.g. with a member deformed, but not moved bodily, to close the passage ; Pinch valves
    • F16K7/10Diaphragm valves or cut-off apparatus, e.g. with a member deformed, but not moved bodily, to close the passage ; Pinch valves with inflatable member

Abstract

In an iris-stop arrangement for stopping-off a duct 1 the secondary bag 20 has a contact length with the duct of at least 0.7 times its diameter. The apparatus is such that the point where the inflation neck 13 of the bag 20 meets the remainder of the bag can adopt a position not substantially in front of the secondary bag support member 10. Thus the bag 20 has improved functional grip on the duct 1, and does not suffer severe flexing at the neck 13 when it moves back to rest against the support member 10. Preferably the portion of the bag which contacts the duct in use is a single layer of fabric thick while the ends of the bag, which have to withstand the bag inflation pressure unsupported, are two layers thick. In this way the bag can have good performance characteristics while only needing a relatively small insertion hole 9 in the side of the duct. <IMAGE>

Description

SPECIFICATION Sealing ducts This invention relates to sealing ("stopping-off") ducts or pipes for example during repair or maintainance operations. The most common example of a duct or pipe on which this is done is a distribution duct for main gas supplies.
We are primarily concerned in this invention with the stopping-off of large ducts, say up to about 120 cm diameter, where the pressure to be resisted may be comparatively high, perhaps up to about 2 bar.
To stop-off systems which are working at that sort of pressure, primary sealing is achieved by a socalled iris-stop system. In this, an expansible disc is introduced into the duct through a hole in its wall and opened out to occupy most of its cross-section.
A so-called primary bag is introduced into the duct at the upstream side of the disc. Once it is positioned inside the duct it is inflated and thereby forms a seal across the duct. The end of the bag remote from its point of inflation is supported by the disc. This therefore both prevents sliding of the bag along the duct under the high pressure encountered and reduces the general stresses on the primary bag.
A secondary bag is introduced into the duct downstream of the primary bag. The secondary bag acts as a further seal for gas seeping past the first bag. It is also desirable for the secondary bag to act as a safety device, maintaining the seal on the duct if the primary bag fails. The secondary bags currently in use do not perform this back-up safety function very well. Because it is a back-up system the secondary bag has to be designed to meet pressure differentials greater than those which were withstood by the primary system and to meet them in conditions where there has been a sudden collapse of the primary bag, which can result in a substantial shock effect.Because it has to meet anticipated higher pressures it will itself have to be inflated to substantial pressures if it is to seal effectively and so it will, even while the primary bag is still acting, be subjected to considerable stress.
In order to provide some support for the secondary bag, a support member (usually a steel tube) is inserted into the duct through the same hole as is used for insertion of the bag. The support member is placed downstream of the bag. The bag is normally inflated through its downstream end, and the pipe carrying the inflation fluid normally runs from the hole in the duct to the inflation point on the bag through the support member. This support member is much less effective than the iris disc supporting the primary bag, but it is a much simpler structure and does not require a separate insertion hole in the duct, while providing at least a degree of support for the secondary bag. The inflation fluid is in practice always compressed air or another gas, nitrogen is often used.
We have identified one problem with existing secondary bags as a danger that dislodgement of the bag along the duct by shock or pressure may, if it goes over too great a distance, unduly stress the bag in the region of its inflation connection which is mechanically fixed in relation to the duct because the inflation pipe is held by the support tube.
In particular, the bag usually has a sleeve-like neck at this connection for egress of the mouth of an inflation bladder. The neck tends not to move, and as the remainder of bag moves the bag material may be flexed and bent back at the point where the neck joins the remainder of the bag. Accordingly in the present invention the length of the neck, the dimensions of the inflation pipe, the dimensions of the support member and their dispositions in use are such that if the bag moves until its downstream end presses against the support member, the point where the neck meets the remainder of the bag is not substantially upstream of the upstream side of the support member. In this way, the material cannot be bent back at this point when the bag slips, greatly reducing the risk of bag failure.If the support member is a tube, and the inflation pipe runs within the tube to the connection on the bag, then this condition can become that when the inflation pipe runs in contact with the inside of the support tube at its downstream side, the point where the neck meets the rest of the bag is not substantially upstream of the outside of the tube at its upstream side. Roughly speaking, this means that the length of the neck including its connector for the inflation pipe should be less than the diameter of the tube.
Although a support tube is currently used in practice, other support members are possible.
Another problem which we have identified is that it is not easy to provide the prior art bags with sufficient frictional grip against the duct, to avoid slippage. Accordingly we have increased the length to width ratio of the bag. In the prior art the length over which the inflated bag contacted the duct was about .5 of the bag diameter. According to the present invention the length is at least .7, preferably between .75 and 1.0, more preferably between .8 and .9 of the bag diameter. This increased length gives an increased contact area and therefore an increased frictional grip for a given contact pressure.
In practice very long bags are not highly advantageous. As the contact length to diameter ratio increases past 1 the bags become less practical, with 1.5 representing the practical limit in the present state of the art. The very long bags have a number of problems. First, the longer the bag the longer the section of duct which needs to be excavated, and the greater the spacing between the iris disc and the secondary support member. Second, it becomes difficult to arrange the uninflated bag correctly in the duct before inflation. Third, the longer bag takes longer to inflate and deflate, especially if it has a large diameter. Last, the preferred bag materials are available in fixed widths, currently of about 1 metre, and it may require more expensive tailoring to make long bags.
Usually a bag and to some degree it associated apparatus are designed to be used in blocking off a duct of a predetermined diameter against a fluid flow in the duct at a predetermined pressure. In order to grip the duct with sufficient force, we find that the pressure differential between the inflation fluid in the bag and the fluid in the pipe should be about 5 p.s.i. (about 1/3 bar). Therefore the bag should be inflated to a pressure of about 2 1/3 bar if it is to block a duct against a fluid flow at 2 bar.
However, since the bag is a secondary bag, it is not subjected to fluid pressure in the duct unless and until the primary system fails. Consequently the bag must be able to support the full differential pressure of 2 1/3 bar. This will be called the operating pressure in the following discussion.
Current safety requirements include that the bag should be able to withstand inflation to four times its operating pressure. Therefore the bag discussed above must be able to withstand 9 1/3 bar. If the bag is short, and has a small contact area, its frictional grip on the duct can be improved by inflating it to a higher pressure differential. However, in this case it becomes difficult to meet the safety requirements, as the maximum pressure to be withstood will increase by four times the increase the operating pressure. If the bag is made stronger, to meet this safety requirement then it will be bulkier when uninflated and thus require a bigger insertion hole in the side of the duct.
If a short bag is not inflated to a high pressure, but operated at a pressure giving reduced frictional grip on the duct, nothing adverse will happen for as long as the primary bag does not fail. If the primary bag fails, then the secondary bag is subjected to the full pressure of the fluid in the duct. It is also subjected initially to a shock. Further, the increase of applied pressure in the duct will tend to compress the inflation gas in the bag. At this moment the bag will tend to slip back, and also distort, pressing the downstream end against the support member. (This is the moment when the bag is stressed at the upstream end of the neck if it protrudes past the upstream side of the support member).All bags will tend to slip and distort at this moment, but if the bag's grip on the duct is insufficient it will move so farthatthe downstream end begins to wrap around the support member. This will pull away from the duct wall part of the duct-contacting surface of the bag. This surface consequently loses the support of the duct wall which it had previously enjoyed, and is therefore exposed to an increased risk of failure.
Once again, this can be counter-acted by strengthening the bag, but this will tend to increase its uninflated bulk.
The features of the present invention discussed above are aimed at reducing stress, so that the bag can operate satisfactory and meet the safety requirements without being disadvantageously bulky. Current conventional secondary bags are manufactured in double envelope form mainly because the outer skin acts as an anti-scuffing layer in the event of bag slip. In order to obtain double strength from the two layer construction the tailoring must be exact or one layer will experience greater stress than the other.
The general elongation of the nylon material is some 15% maximum and thus a small inner can be supported by the outer if sizing is not too far out. If, however, the inner is larger than the outer only the outer skin is stressed. If this fails then the inner skin of the same material will also fail.
As mentioned above, the part of the bag which is in contact with the duct is substantially relieved of stress by the duct. However, the end faces of the bag must be able to withstand the full operating pressure. Therefore we prefer to make the ends of the bag stronger than the duct-contacting portion, avoiding unnecessary bulk in the latter. In fact, the unsupported parts of the bag are not all stressed to the same degree. The tension in a surface restraining a given pressure depends on the radius of curvature of that surface, the smaller the radius the less the tension. If the bag has a generally cylindrical shape, then at the point where the bag surface leaves the duct wall the stress is relatively low. It is highest over the centre of the end faces. Thus it does not matter if the stronger end surfaces do not reach quite to the wall of the duct.
Preferably the secondary stopping-off bag is constructed as a hollow cylinder of fabric with end closures constructed of a double layer of fabric the warps of the respective layers in a given end closure being at an angle to each other, the end closure being secured to the cylinder by means of foldedover end flaps of the latter. The angle between the warps of the layers in the end closures is optimally 90 . The sleeve-like neck in one end closure of the bag for egress of the mouth of the inflation bladder is made as short as possible and preferably also of a double layer of fabric, each layer having end flaps to be folded over and be secured to the end closures.
The flaps radiate from the sleeve with end flaps originating from one layer of the neck being angularly offset from and overlapping the flaps originating from the other.
A seam of the cylinder is axial and is aligned to lie within the convergence of the warps of the layers of the end closures; furthermore when a gas connector is fitted to the neck it should be aligned generally with a continuation of the direction of the seam.
To minimise strength loss during stitching of the fabric it is desirable to use so-called "delta" needles, which have a rounded point and a triangular-section tip portion.
The invention also includes the method of making a secondary bag.
A particular embodiment of the invention, given by way of example, will now be described with reference to the accompanying drawings in which: Figure 1 shows the conventional layout of an iris-stop primary bag system and a secondary bag system in a duct, seen in cross-section; Figure 2 shows the secondary bag embodying the present invention in position in the duct; Figures 3a,3b,3c,3d and 3e show various stages in the formation of a neck piece of the present bag; Figure 4 shows an end closure of the bag; Figure 5shows the cylinder of the bag; Figure 6 shows an assembly stage; Figure 7 shows a further assembly stage; Figure 8 shows a completed assembly; Figure 9 shows a partial cross-section through the assembly as positioned in a duct; and Figure 10 is a similar cross-section but of a modified embodiment.
Referring first to Figure 1, a duct 1 of a mains gas pipe in which the gas flows from left to right is being temporarily stopped-off by a primary sealing bag 2 introduced by known means through a hole 3 formed in the wall of the duct. Downstream of the hole 3 a second hole 4 is formed, through which is introduced the support 5 of a spreadable iris-disc 6.
The bag 2 having been guided to lie downstream of its insertion position by a skid 7, can be inflated to occupy the duct with its base resting against the iris-disc 6. Downstream of the iris-disc a further hole 9 is formed and a secondary bag (which here is a conventional secondary bag 11) is introduced through it and positioned in the duct upstream of it.
A hollow support column 10 is also introduced through the hole 9 and positioned downstream of the secondary bag 11. The secondary bag is inflated through a gas connector 12 connected to a neck 13 of the bag. As can be seen the total length of the gas connector 12 and the neck 13 is greater than the cross-sectional width of the hollow column 10 so that when the bag 11 is inflated its rear end is substantially spaced out from the column. If, however, the primary bag were to fail the secondary bag might be forced back down the duct towards the position shown in dotted lines 11' at which it can be seen that its rear end closure is substantially flexed and stressed around the neck. The secondary bag 11 contacts the duct over a length which is about one half of the duct diameter.
Figure 2 shows a bag 20 embodying the invention in use. The column 10 may be identical but the total length of the connector 12' and neck 13' is not greater than the cross-sectional dimension of the column. Thus in a normal position shown in full lines the rear end of the bag 20 is supported by the column. This secondary bag 20 contacts the duct over a length which is at least 0.7 times the duct diameter, preferably between 0.8 and 0.9 times the duct diameter. As compared with the conventional bag 11 the increased contact length makes the bag 20 less likely to slip along the duct. Even if it is somewhat dislodged by sudden pressure, to the position 20', there is substantially less flexion and stress in the region of the neck (slight overlapping past the column 10 is possible but only beyond each side of the column).
The bag 20 embodying the invention is made up as follows.
A neck portion of the bag is made up as seen in Figure 3. Two parts 23 and 24 each having a plurality of tongues 25 and 26 at one of their edges are placed so that the tongues are in staggered relationship and are tacked together by a line of stitching 27, Figure 3a. They are then brought round as shown in Figure 3b and seamed along one edge as far as the line of the root of the tongues. This seam 28 results in the formation of the sleeve portion 29. This sleeve is pushed through a central aperture in a planar annulus 30 of fabric seen in Figure 3d and the tongues 25, 26 are turned outwardly from the sleeve to be radiated upon the face of the annulus 30 and are then stitched down onto that by a circular row of stitching 31. The placing of a cylindrical former inside the sleeve portion 29 as this is being done, is helpful.
In the final step of the formatioi the sleeve portion 29 is pulled through so that the hem is now inside it, Figure 3e.
The next step to be described is making end closures of the bag. Each end closure consists of two polygonal sheets of fabric of coincident outline laid upon each other so that the warp direction W1 of one of the sheets 32 lies at an angle which is preferably 90 to the warp direction W2 of the other sheet 31.
The two layers thus formed are stitched together along radial lines of stitching 33 into the corners of the polygon. In the end closure seen in Figure 4, which is that which is going to receive the neck assembly, both layers 31,32 have a central aperture 34 which is surrounded by a reinforcing annulus of fabric 35 which is stitched to the layers by a circle of stitching 36. In the end closure which is to form the other end of the bag (the one to be remote from the column 10) the fabric layers 31,32 are uninterrupted by any aperture.
After the two layers have been attached together in that way, the neck assembly is mounted on them by having the sleeve portion 29, in the condition seen in Figure 3e, inserted through the aperture 34 from that face of the end closure which is to be innermost in use. The annulus 35 on the interrupted end closure face is on the layer which is to be outermost in use.
The tongues 25, 26 are therefore entrapped between the reinforcing annulus 30 and the inner of the two layers of the end closure. The neck assembly is then stitched to the end closure by a ring of stitching 37, Figure 6, through to the reinforcing annulus 35.
Meanwhile, a hollow cylinder has been prepared from a rectangular blank of fabric 38 having at each major edge extensions which are to form flaps 39.
The ends of the blank are brought round together and are overlapped to form a seam 42 and are tacked together at 40, at their end portions only. The sleeve thus formed is next secured to the end closures. In a first step a continuous line of stitching 41 (Figure 6) is formed parallel to the polygonal edges of the end closure and along the line joining the roots of the end flaps 39 of the cylinder. It is important to note that the securing of the cylinder to the end closures is done in such a way that the seam 42 of the cylinder occurs within the angle between the two warps W1, W2. That is it could either be to the corner marked F or to the corner marked G in Figure 6, or perhaps between those corners. The same disposition of warps W1, W2 is followed when securing the other of the end closures.
In a second stage of securing of the end closures the end flaps 39 are folded over the end closure and are stitched down onto it by a line of stitching 43 parallel to the edges of the end flaps spaced slightly in from those edges. It is very important that the folded over end flaps 39 shall be at the same tension as the underlying layers 31, 32 of fabric of the end closure, so that all layers of fabric secured between the lines 41 and 43 of stitching are in equal tension and equally share any stresses to be experienced.
In a final stage of assembly the bag so formed is turned inside-out by eversion through the gap left along the seam 42 between the tackings 40 and its bladder is inserted into it through the same gap. The inflation neck of the bladder is brought out through the sleeve 29 which is now projecting outside the bag as a whole and is there united by means of standard fitments both with the sleeve and with a gas connector 44 having an inlet 45 which is at right angles to the axis of the bag in the sleeve. It is important that this inlet is orientated generally toward the seam 42 in the cylindrical sleeve, that is to be directed to within the angle formed between the warps W1 and W2 of the end closure.
Finally, the seam 42 is closed either by bonding or stitching. The dimensions of the bag are, of course, chosen in accordance with expected pressures in the duct and the diameter of the duct to be stopped-off and the dimension of the projecting neck and gas connector are selected in relation to the column 10 as has already been noted in connection with Figure 2.
The fabric used for most of the structural parts is a plain nylon fabric but for the reinforcing annuli such as 30,35 and also for one of the two parts 23, 24 polyurethane coated nylon is used. The stitching is found to involve least loss of strength if it is performed with round pointed "delta needles", that is to say needles of which at least the tip of the end portion is of triangular section.
Figure 9 shows the conformation of the bag in use, at the important region where it parts from the wall 1 of the duct. The construction is as previously described except that an additional row of stitching 46 is shown which may advantageously be applied.
This method of assembling the single bag 38 to the double end wall 31,32 is preferred because of its manufacturing advantage but it does leave a region where only a single layer of fabric is resisting, unsupported, the pressures in the bag. This single layer region can usually be tolerated, as the radius of curvature of the fabric is high here and so the stresses induced are relatively low.
An alternative method of construction is shown in Figure 10 where inner panel 31' is extended at the region 48 to underlie the bag 38 and is secured by a row of stitching 47. This has the advantage of doubling the fabric at the critical area but it is a much more complex method of fabrication.
It is possible for the bag to be inflated not with gas but with liquid, which is advantageous because of the incompressability of the liquid (leading to lower pressure stress in the free standing normal mode of the secondary bag before failure of the primary bag) and because of its high mass leading to high mechanical inertia of the bag.

Claims (10)

1. Apparatus for sealing a duct against directional fluid flow comprising a fluid-tight bag, an inflation pipe connected to the bag in use and a support member, the bag being placed inside a duct in use and inflated by the passage of fluid through the inflation pipe so as to press against the inside of the duct and seal the duct, the support member being fixed in use inside the duct and stationary with respect to the duct, adjacent the downstream (with respect to the direction of fluid flow in the duct being sealed against) end of the bag, the inflation pipe being connected to bag in use by a neck on the downstream end of the bag and running from the neck within or to one side of the support member, the length of the neck, the dimensions of the inflation pipe, the dimensions of the support member and their dispositions in use being such that when the downstream end of the bag is pressed against the support member the point where the neck meets the rest of the bag is not substantially upstream of the upstream side of the support member and the bag being so dimensioned that when it is inflated within the duct the axial length of the area of contact between the bag and the duct is at least .7 of the diameter of the bag.
2. Apparatus according to Claim 1 in which the support member is a tube, and the inflation pipe runs in use from the neck of the bag into the support tube and then within the support tube to the outside the duct, the length of the neck and dimensions of the inflation pipe and the support tube being such that if the inflation pipe runs in contact with the inside of the support tube at its downstream side, the point where the neck meets the rest of the bag is not substantially upstream of the outside of the support tube at its upstream side.
3. Apparatus according to Claim 1 or Claim 2 in which the said axial length of the area of contact is from .8 to .9 of the diameter of the bag.
4. Apparatus according to any one of the preceding claims in which the bag is constructed as a hollow cylinder of fabric with end closures constructed of a double layer of fabric, the warps of the respective layer of each end closure being at an angle to each other, the end closure being secured to the cylinder by means of folded-over end flaps of the cylinder.
5. Apparatus according to Claim 4 in which the angle between the warps of the respective layers of each end closure is substantially equal to 900.
6. Apparatus according to Claim 4 or Claim 5 in which one fabric layer of an end closure overlaps the cylinder.
7. Apparatus for sealing a duct substantially as described herein with reference to and as illustrated in the accompanying drawings.
8. A method of manufacturing a bag to form part of apparatus according to any one of the preceding claims, in which seams in the fabric are stitched using round pointed needles having a triangular section at least at the said round point.
9. A method of manufacturing a bag to form part of apparatus according to any one of Claims 1 to 7, the method being substantially as herein described with reference to and as illustrated in Figures 3 to 10 of the accompanying drawings.
10. A bag made by the method of Claim 8 or Claim 9.
GB08413015A 1983-06-02 1984-05-22 Sealing ducts Expired GB2140894B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB08413015A GB2140894B (en) 1983-06-02 1984-05-22 Sealing ducts

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB838315198A GB8315198D0 (en) 1983-06-02 1983-06-02 Sealing pipes
GB08413015A GB2140894B (en) 1983-06-02 1984-05-22 Sealing ducts

Publications (3)

Publication Number Publication Date
GB8413015D0 GB8413015D0 (en) 1984-06-27
GB2140894A true GB2140894A (en) 1984-12-05
GB2140894B GB2140894B (en) 1986-07-02

Family

ID=26286284

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08413015A Expired GB2140894B (en) 1983-06-02 1984-05-22 Sealing ducts

Country Status (1)

Country Link
GB (1) GB2140894B (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2200710A (en) * 1986-12-03 1988-08-10 Shorco Trench Systems Limited Inflatable expandable device
EP0335300A1 (en) * 1988-03-28 1989-10-04 Göbel, Gerd Inflatable plug to block holes and passages
EP0479302A1 (en) * 1990-10-05 1992-04-08 SION, Karl Closure device for sealing flow-passages
US5285806A (en) * 1992-12-30 1994-02-15 Public Service Company Of Colorado Method and apparatus for temporarily sealing off pipelines
EP0583819A1 (en) * 1992-08-19 1994-02-23 J. Van Beugen Beheer B.V. Device for closing the passage in a pipe
EP0676578A1 (en) * 1994-04-08 1995-10-11 Tigerholm Aktiebolag Blocking method for pipes
US5778919A (en) * 1993-12-30 1998-07-14 Custom Service Laboratories Of N.J., Inc. Pipeline flow stopper with dual shafts
WO2001016518A1 (en) * 1999-09-01 2001-03-08 Sarco Stopper Limited Inflatable stopper
WO2011055214A1 (en) * 2009-11-04 2011-05-12 Holcim Technology Ltd Duct plug inflatable safety device
JP2019086117A (en) * 2017-11-08 2019-06-06 クロダイト工業株式会社 Fluid shut-off air bag

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2200710A (en) * 1986-12-03 1988-08-10 Shorco Trench Systems Limited Inflatable expandable device
EP0335300A1 (en) * 1988-03-28 1989-10-04 Göbel, Gerd Inflatable plug to block holes and passages
EP0479302A1 (en) * 1990-10-05 1992-04-08 SION, Karl Closure device for sealing flow-passages
EP0583819A1 (en) * 1992-08-19 1994-02-23 J. Van Beugen Beheer B.V. Device for closing the passage in a pipe
US5285806A (en) * 1992-12-30 1994-02-15 Public Service Company Of Colorado Method and apparatus for temporarily sealing off pipelines
US5778919A (en) * 1993-12-30 1998-07-14 Custom Service Laboratories Of N.J., Inc. Pipeline flow stopper with dual shafts
EP0676578A1 (en) * 1994-04-08 1995-10-11 Tigerholm Aktiebolag Blocking method for pipes
US5524661A (en) * 1994-04-08 1996-06-11 Tigerholm Ab Method of blocking a pipe and device therefor
CN1052295C (en) * 1994-04-08 2000-05-10 蒂格霍尔姆股份公司 Blocking method for pipes
WO2001016518A1 (en) * 1999-09-01 2001-03-08 Sarco Stopper Limited Inflatable stopper
WO2011055214A1 (en) * 2009-11-04 2011-05-12 Holcim Technology Ltd Duct plug inflatable safety device
JP2019086117A (en) * 2017-11-08 2019-06-06 クロダイト工業株式会社 Fluid shut-off air bag

Also Published As

Publication number Publication date
GB2140894B (en) 1986-07-02
GB8413015D0 (en) 1984-06-27

Similar Documents

Publication Publication Date Title
US4627470A (en) Sealing ducts
US6142227A (en) Expandable retrievable bridge plug
GB2140894A (en) Sealing ducts
US4087306A (en) Turn-up or turn-over bladder for tire building machines
US10131092B1 (en) Material joint for an inflatable structure and method of constructing the same
EP0464121B1 (en) Improvements relating to the lining of pipelines or passageways
US4467836A (en) Flexible tube means, especially for an expansible valve
EP0058951A1 (en) Pneumatic cushion and manufacturing method therefor
US7066490B2 (en) Airbag device
HUT59472A (en) Device for repairing tubes, tunnels and similars
KR20010021847A (en) Single piece air bag with improved stress distribution
GB2028601A (en) Sealing closure members to substrates
US7467496B1 (en) Method for joining components of inflatable structures
US2989324A (en) Pressurized garments
US5031260A (en) Fluid-filled mattress construction
EP0583819B1 (en) Device for closing the passage in a pipe
CA1171004A (en) Inflatable plug for interiorly cylindrical conduits
US6432495B1 (en) Abrasion resistant air bag
US4029272A (en) Variable-geometry aircraft seal
CA2541204C (en) Flow control device, with assisted anchoring, insertable into a pipeline
CA1054447A (en) Stepped and angle-cut, pinch closure
JP3473781B2 (en) How to line branch pipes
GB2200710A (en) Inflatable expandable device
CN220540594U (en) Three-cabin plugging air bag
JPS6123754Y2 (en)

Legal Events

Date Code Title Description
732E Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977)
PE20 Patent expired after termination of 20 years

Effective date: 20040521