Method for forming pressure-testable field joint between pre-insulated pipe sections, and piping system with pressure-testable field joint
20180017463 ยท 2018-01-18
Inventors
Cpc classification
F16L2201/30
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B29C65/3468
PERFORMING OPERATIONS; TRANSPORTING
B29C66/73921
PERFORMING OPERATIONS; TRANSPORTING
B29C65/8246
PERFORMING OPERATIONS; TRANSPORTING
International classification
G01M3/28
PHYSICS
B29C44/12
PERFORMING OPERATIONS; TRANSPORTING
F16L59/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B29C65/00
PERFORMING OPERATIONS; TRANSPORTING
B29C65/34
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A method for forming a field joint between pipe sections is provided, preferably for pre-insulated pipe sections containing a carrier pipe surrounded by insulation and an outer jacket. The carrier pipes are joined, and an air tube is positioned so that its first end is within the joint area, and its second end extends beyond the joint area. A sleeve is sealed over the joint area, joining the jackets, with the sleeve positioned to cover the first end but not the second end of the tube. Air is injected into the tube to pressurize the cavity within the jacket, and the tube bore is sealed to allow air pressure testing. If the testing shows no loss of air pressure, the bore of the tube is sealed permanently to complete the seal on the field joint. Also provided is a piping system having a field joint formed by this method.
Claims
1. A method for forming a field joint between adjacent pipe sections, each pipe section comprising an inner carrier pipe disposed inside an outer jacket with a space between the carrier pipe and the outer jacket, comprising: forming a carrier pipe joint between ends of the carrier pipe of each of the pipe sections; positioning an air tube so that a first end of the air tube is positioned within a joint area of the adjacent pipe sections, with a second end of the air tube positioned to extend beyond the joint area; placing a sleeve over the joint area so that the sleeve surrounds the joint area and extends beyond a gap between the respective outer jackets of the pipe sections, wherein the sleeve is positioned so that it covers the first end of the air tube and does not cover the second end of the air tube; sealing the sleeve to each of the respective outer jackets of the pipe sections such that a sealed jacket joint is formed between the respective jackets so as to form a sealed cavity inside the sealed jacket joint, wherein the first end of the air tube is sealingly enclosed within the sealed cavity, and the second end of the air tube remains outside the sealed cavity and exposed to an outside environment; injecting air into a bore of the air tube at the second end of the air tube to pressurize the sealed cavity; closing off the bore of the air tube to maintain the air pressure in the cavity; testing for loss of air pressure inside the cavity; and then permanently sealing off the bore of the air tube.
2. The method according to claim 1, wherein each of the pipe sections is a pre-insulated carrier pipe section, wherein the space between the inner carrier pipe and the outer jacket along the longitudinal axis of the pipe section contains an insulating layer.
3. The method according to claim 2, further comprising filling a gap between respective insulating layers of respective adjoining carrier pipe sections by adding insulation to the gap.
4. The method according to claim 3, wherein the insulation added to the gap is comprised of pre-formed insulation segments.
5. The method according to claim 2, wherein the sleeve is comprised of a heat-shrinkable material, and sealing the sleeve comprises applying heat to the sleeve.
6. The method according to claim 2, wherein sealing the sleeve comprises welding the sleeve to each of the respective outer jackets of the carrier pipe sections.
7. The method according to claim 2, wherein sealing the sleeve comprises applying a sealant band around a segment of each of the respective outer jackets of the carrier pipe sections to form a seal between the sleeve and each of the respective outer jackets.
8. The method according to claim 2, wherein testing for loss of air pressure inside the cavity results in detection of a leak of the cavity, and further comprising repairing the leak before permanently sealing the bore of the air tube.
9. A piping system comprising a field joint formed between adjacent pipe sections, each pipe section comprising an inner carrier pipe disposed inside an outer jacket with a space between the carrier pipe and the outer jacket, wherein the field joint is formed by: forming a carrier pipe joint between ends of the carrier pipe of each of the pipe sections; positioning an air tube so that a first end of the air tube is positioned within a joint area of the adjacent pipe sections, with a second end of the air tube positioned to extend beyond the joint area; placing a sleeve over the joint area so that the sleeve surrounds the joint area and extends beyond a gap between the respective outer jackets of the pipe sections, wherein the sleeve is positioned so that it covers the first end of the air tube and does not cover the second end of the air tube; sealing the sleeve to each of the respective outer jackets of the pipe sections such that a sealed jacket joint is formed between the respective jackets so as to form a sealed cavity inside the sealed jacket joint, wherein the first end of the air tube is sealingly enclosed within the sealed cavity, and the second end of the air tube remains outside the sealed cavity and exposed to an outside environment; injecting air into a bore of the air tube at the second end of the air tube to pressurize the sealed cavity; closing off the bore of the air tube to maintain the air pressure in the cavity; testing for loss of air pressure inside the cavity; and then permanently sealing off the bore of the air tube.
10. The piping system according to claim 9, wherein each of the pipe sections is a pre-insulated carrier pipe section, wherein the space between the inner carrier pipe and the outer jacket along the longitudinal axis of the pipe section contains an insulating layer.
11. The piping system according to claim 10, wherein forming the field joint further comprises filling a gap between respective insulating layers of respective adjoining carrier pipe sections by adding insulation to the gap.
12. The piping system according to claim 11, wherein the insulation added to the gap is comprised of pre-formed insulation segments.
13. The piping system according to claim 10, wherein the sleeve is comprised of a heat-shrinkable material, and sealing the sleeve comprises applying heat to the sleeve.
14. The piping system according to claim 10, wherein sealing the sleeve comprises welding the sleeve to each of the respective outer jackets of the carrier pipe sections.
15. The piping system according to claim 10, wherein sealing the sleeve comprises applying a sealant band around a segment of each of the respective outer jackets of the carrier pipe sections to form a seal between the sleeve and each of the respective outer jackets.
16. The piping system according to claim 10, wherein testing for loss of air pressure inside the cavity results in detection of a leak, and forming the field joint further comprises repairing the leak before permanently sealing the bore of the air tube.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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DETAILED DESCRIPTION OF THE INVENTION
[0022] Pre-insulated piping 1 used in the method of this invention is shown in the drawings.
[0023] In pre-insulated pipe sections, the carrier pipe 10 is surrounded along its length in the axial direction by a carrier pipe insulating layer 16, as shown in
[0024] The carrier pipe insulating layer 16 is surrounded along its length in the axial direction by an outer jacket 24, which serves as the outermost layer of the pre-insulated pipe section, as shown in
[0025]
[0026] As shown in
[0027] The sleeve 26 is formed of suitable thermoplastic material, preferably of polyethylene, more preferably of high density polyethylene (HDPE). The sleeve 26 optionally may be formed of the same material as the jacket 24 to which it will be affixed and sealed. The sleeve 26 may preferably be made in a specific size in diameter as well as other dimensions and then is heated and expanded. The expanded sleeve 26 is then of a size to be slid into its initial position surrounding the jacket 24 of one of the sections of pre-insulated pipe. Then, later in the process, after being centered over the field joint area 2 and heated again, by the nature of the heat-shrinkable material of which it is formed, the sleeve 26 will shrink back down to smaller dimensions to closely surround the joint area 2.
[0028] The sleeve 26 can alternatively be made of a wrap-around sheet material that is formed into a tubular shape and sealed, being sized to be slid into the initial position surrounding the jacket 24 of one of the sections of pre-insulated pipe. Then, later in the process, after being centered over the field joint area 2 and heated again, by the nature of the heat-shrinkable sheet material, the sleeve 26 will shrink back down to smaller dimensions to closely surround the joint area 2.
[0029] As shown in
[0030] Next, as shown in
[0031] There are several known ways of adding this insulation segment 28, including field mixing liquid foam and pouring it into a mold that surrounds the gap, or installing into this gap pre-formed sections of insulation shaped to fit around the carrier pipe 10.
[0032] After installation of the insulation segment 28, all surfaces of the jacket 24 that are to be bonded to the sleeve 26 are cleaned and wiped to assure good adherence between the jacket 24 and the sleeve 26. The cleaning can be performed with 24 grit abrasive cloth. The jacket surface in this area is then wiped to remove any debris on the portions of the surface of the jacket 24 to be bonded.
[0033]
[0034] As shown in
[0035] With the air tube 34 in the position as depicted in
[0036] Then, as shown in
[0037] Thereafter, as shown in
[0038] The sleeve 26 preferably is, as described previously, formed of a heat-shrinkable material so that the seal between the sleeve 26 and the jacket 24 can be formed by applying heat to the exterior surface of the sleeve 26 so that the entire circumference of the sleeve 26 shrinks down so that the sleeve 26 closely fits onto and fuses with the outer surface of the jacket 24. Thereby, the sealed jacket joint is formed.
[0039] As shown in
[0040] The formation of the fully sealed jacket joint 44 (see
[0041] Next, air-pressure testing is conducted to confirm that the seal of the sealed cavity inside the jacket joint 44 (depicted in
[0042] First the installer connects the connector 40, which can preferably be any standard air tube fitting that provides a positive seal under air pressure, to an air pump apparatus, schematically shown as reference numeral 48 in
[0043] The air pump 48, thus connected to the air tube 34 via the connector 40, is then used to pump air through the bore of the air tube 34 into the sealed cavity within the outer jacket 24. The air pump 48 can be a simple known air pumping device such as a hand air pump, or a standard air compressor such as those conventionally used for pumping air into automobile tires. Such an air compressor typically comprises an air pumping means as well as an air pressure detection means 42 and/or shut off valve 46 that can be connected to the connector 40 of the air tube 34. A benefit of this invention is that these sorts of low cost, easily obtainable, standard compressor devices can be used as the air pump 48 for checking for air leaks by the claimed method. The standard devices often provide as well means to conduct the pressure testing function, and the shut off function. The shut off valve 46, as well as the air pressure detection means 42, which may preferably be in the form of a pressure gauge can alternatively be separate devices from the air pump 48.
[0044] Using the air pump 48, an air pressure above atmospheric pressure, preferably about 5 or so pounds per square inch (PSI), is created inside the cavity within the sealed jacket joint 44, by using the air pump 48 connected to the connector 40 of the air tube 34 to pump air into the air tube 34 through its outer end 38, through the bore in the air tube 34, into the space in the joint area 2, through the first (inside) end 36 of the air tube 34, which is positioned inside the cavity, thus pressurizing the cavity or space. The installer then temporarily closes off the outer end 38 of the air tube by closing the shut off valve 46 to prevent escape of air through outer end 38, to maintain the pressurization within the cavity. The installer then checks for air leaks in the cavity, by conventional means such as, e.g., listening for sounds of escape of the pressurized air through small holes in the sealed jacket joint 44, or soaping the joint area 2 to expose air leaks revealed by the visual cue of soap bubbles forming on the surface of the sealed jacket joint 44 in the joint area 2. The installer can also check for a drop in air pressure in the space between the joined carrier pipe 10 and the joined outer jacket 44 by reading air pressure measurements provided by the air pressure level detection means (pressure gauge) 42, which is connected to the end 38 of the air tube 34. The installer optionally may use a combination of such conventional means of detecting a change in the air pressure in the sealed cavity. The method thus allows the installer to find air leaks using inexpensive and readily available standard equipment. The installer is then enabled to easily make repairs in the seals of the newly formed jacket joint 44 as needed, and then to easily re-check for air leaks again after the repairs have been completed.
[0045] No leaking or drops in pressure mean a complete seal has been achieved. After this successful air pressure test has been completed, the air tube is disconnected from the air pump 48, shut off valve 46, and pressure gauge 42. Then the portion of the air tube 34 that extends outside end of the jacket joint 44 is preferably shortened by cutting off a portion of the air tube 34. Preferably the remaining portion of the cut air tube 34 extends about 1 inch outside the end of the jacket joint 44, as shown in
[0046] The sealing of the bore results in a final air-tight and water-tight seal of the newly formed jacket joint 44 extending over the entire joint area 2. This yields a final air-tight and water-tight cavity in the joint area that contains insulation segment 28 and that is enclosed within the jacket joint 44 and surrounds the carrier pipe joint.
[0047] As shown in
[0048] Also disclosed is another embodiment of the invention depicted in
[0049] As shown in
[0050] After sealing the sleeve 26 to the jacket 24 as described in the discussion above with regard to
[0051] Then the bore of the air tube 34 is permanently sealed off from the outside environment, by injecting into the remaining outer end of the air tube 34 flux, solder, a high temperature mastic, thermoplastic, or other sealing material, or combinations thereof, suitable to permanently and fully plug up and seal off the bore of the air tube 34 from the external environment. Other means of closing the bore optionally may be used, such as welding shut or crimping the tube, or otherwise collapsing and closing the open bore of the tube. Thus, in this second embodiment, the sealing of the bore results in a final air-tight and water-tight seal of the newly formed jacket joint 44 extending over the entire joint area 2. This embodiment has the benefit of avoiding any damage to the seal formed between the jacket 24 and the sleeve 26.
[0052] Also disclosed is a field joint made between pre-insulated pipe sections as described herein and schematically represented in
[0053] While an exemplary embodiment incorporating the principles of the present invention has been disclosed hereinabove, the present invention is not limited to the disclosed embodiments. Instead, this application is intended to cover any variations, uses, or adaptations of the invention using its general principles. Further, this application is intended to cover such departures from the present disclosure as come within known or customary practice in the art to which this invention pertains and which fall within the limits of the appended claims.
[0054] The terminology used herein is for the purpose of describing particular illustrative embodiments only and is not intended to be limiting. As used herein, the singular forms a, an and the may be intended to include the plural forms as well, unless the context clearly indicates otherwise. The terms comprises, comprising, including, and having, are inclusive and therefore specify the presence of stated features, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, steps, operations, elements, components, and/or groups thereof. The method steps, processes, and operations described herein are not to be construed as necessarily requiring their performance in the particular order discussed or illustrated, unless specifically identified as an order of performance. It is also to be understood that additional or alternative steps may be employed.
[0055] When an element or layer is referred to as being on another element or layer, it may be directly on, engaged, connected or coupled to the other element or layer, or intervening elements or layers may be present. As used herein, the term and/or includes any and all combinations of one or more of the associated listed items. Although the terms first, second, third, etc. may be used herein to describe various elements, components, regions, layers and/or sections, these elements, components, regions, layers and/or sections should not be limited by these terms. These terms may be only used to distinguish one element, component, region, layer or section from another region, layer or section. Terms such as first, second, and other numerical terms when used herein do not imply a sequence or order unless clearly indicated by the context. Thus, a first element, component, region, layer or section discussed below could be termed a second element, component, region, layer or section without departing from the teachings of the example embodiments.
[0056] Spatially relative terms, such as inner, outer, beneath, below, lower, above, upper and the like, may be used herein for ease of description to describe one element or feature's relationship to another element(s) or feature(s) as illustrated in the figures. Spatially relative terms may be intended to encompass different orientations of the device in use or operation in addition to the orientation depicted in the figures.
REFERENCE NUMERAL LIST
[0057] pre-insulated piping 1 [0058] joint area 2 [0059] carrier pipe 10 [0060] pre-insulated pipe section ends 12, 14 [0061] insulating layer 16 [0062] sealant 22 [0063] outer jacket 24 [0064] outer jacket hole 25 [0065] sealant for outer jacket hole 25A [0066] sleeve 26 [0067] insulation segment 28 [0068] air tube 34 [0069] sealant section 35 over air tube [0070] first end 36 of air tube 34 [0071] second end 38 of air tube 34 [0072] coupling 40 of air tube 34 [0073] pressure gauge 42 [0074] outer jacket joint 44 [0075] shut off valve 46 [0076] air pump/test apparatus 48 [0077] secondary shrink-wrap covering 50