Background of the Invention
This invention relates to devices for leak testing of piping or tubing, and more particularly to a device for isolating an interior section of pipe or tubing to define a test section which can be subjected to pressure for the purpose of ascertaining the integrity of the section from the standpoint of leak tightness.
There are numerous instances in which sections of pipe or tubing are joined together and it is desired to check the connection to determine whether any leakage could occur. Among the fields in which such tubing is employed and in which fluid-tight interconnections between adjacent sections are desired is the oil and gas well drilling field. In that field, as the well bore is being drilled, various sections of tubing or pipe are lowered into the bore hole and connected to each other as the bore hole is drilled deeper. The pipe sections define a casing to prevent inward collapse of the bore hole and to permit withdrawal of the drilling fluids and debris, as well as to permit insertion and withdrawal of the drill head.
A number of devices have been developed in order to permit isolation of the piping section adjacent to a connection in order to define a restricted area within which a pressure test fluid can be introduced. Typically, such tools involve an elongated carrier member on which are positioned spaced packing rings which are expandable radially outwardly to contact the inner surfaces of the pipe on either side of the connection. The carriers on which the packing rings are positioned include passageways to permit the transmission of high pressure fluids from a pressure source to the space between the rings so that when the latter are expanded outwardly to define the axial limits of a test section, an enclosed volume is provided which includes the area to be tested as one surface thereof. Thus a pressurizable volume is provided to permit detection from the exterior of the pipe of any leakage which might take place at the area being tested.
Although a number of the prior art devices operate in a generally satisfactory manner, the slenderness and consequent flexibility of such devices results in high bending loads on the various tool sections during handling and use. A number of the prior art devices are prone to premature breakage or weakening because of stress cracks resulting from such loading conditions, and also from the high test pressures to which the devices are subjected, which can range from 5000 psi. to about 20,000 psi. It is therefore desirable to provide a pipe testing tool which is capable of quick and positive operation, and which can withstand high loading conditions to facilitate testing under high pressures while also being capable of withstanding the flexing loads to which such devices are oftentimes subjected in use.
Summary of the Invention
It is an object of the present invention to provide a pipe testing tool which is of simplified construction and which provides maximum interchangeability of the several parts thereof.
It is another object of the present invention to provide a pipe testing tool in which the various portions are so connected that they are capable of withstanding significant pressure and mechanical loadings so that failure of the tools is minimized.
Briefly stated, in accordance with one aspect of the present invention, a pipe connection testing tool is provided which includes a cylindrical mandrel having a through bore to define an interior fluid passageway therein. Two such mandrels are interconnected by a union through a hub member which is carried by each of the mandrels. Positioned about the outer periphery of the mandrel is a sleeve which is capable of axial sliding movement relative thereto, and a plurality of spaced resilient sealing rings radially expandable upon application of axial compressive force. The sealing rings have rigid metallic drift rings positioned therebetween. A transverse passageway extends from the interior passageway in the mandrel to a shoulder formed in the cylinder sleeve, one end of which abuts one of the drift rings. When pressurized fluid is introduced into the inner bore of the mandrel the fluid causes the cylinder to act against the sealing rings and drift rings in an axial direction relative to the tool, thereby causing the sealing rings to compress axially, which causes their peripheral surfaces to move radially outwardly against the inner surface of the pipe or tubing to provide a fluid-tight seal therebetween. The space between the upper and lower sealing ring assemblies defines an annular test chamber which encompasses the pipe joint connection. When subjected to pressure the pressure is confined to the area of interest, and the pressure absence of the pressurizing fluid externally of the test section is observed to verify the integrity of the pipe connection at the test section.
Brief Description of the Drawings
FIG. 1 is a side view of a pipe testing tool according to the present invention positioned within a pair of interconnected pipe sections to permit pressure testing of the joint therebetween.
FIG. 2 is an enlarged cross-sectional view of the lower mandrel of a testing tool in accordance with the present invention.
FIG. 3 is an enlarged cross-sectional view similar to FIG. 2 but showing the upper mandrel of a testing tool in accordance with the present invention.
FIG. 4 is a cross-sectional view taken along the line 4--4 of FIG. 2.
FIG. 5 is a cross-sectional view taken along the line 5--5 of FIG. 2.
FIG. 6 is a cross-sectional view taken along the line 6--6 of FIG. 3.
Description of the Preferred Embodiments
Referring now to the drawings and in particular to FIG. 1 thereof, there is shown a portion of a well casing 10 including a junction defined by the ends of a first pipe section 12 and a second pipe section 14. Each pipe section includes an externally threaded end and the two pipe sections are interconnected by an internally threaded union 16 which is in threaded engagement therewith.
Positioned within the interior of casing 10 is a pipe testing tool 18 in accordance with the present invention. Tool 18 includes a lower cylindrical mandrel 20 and an upper cylindrical mandrel 22 coaxial therewith and connected thereto by means of an intermediate cylindrical spacer tube 24, which includes internal threads at each end thereof to permit a threaded connection with the respective mandrels. The lowermost end of lower mandrel 20, the end opposite spacer tube 24, includes a guide plug member 26 which has a rounded end to facilitate insertion of the tool into a pipe section. Connected to the upper end of upper mandrel 22, the end opposite spacer tube 24, is a lifting cable 30 to allow the tool to be raised and lowered in order to permit it to be placed in the desired position within casing 10. Also connected to the upper end of upper mandrel 22 is a fluid conduit 34 to permit communication between the interior of tool 18 and a source of pressurized fluid (not shown), which can be water, a gas, or a combination of gases.
The interior construction and interconnection of the several parts of lower mandrel 20 is illustrated in cross section in FIG. 2. As there shown, mandrel 20 is a generally tubular member and has a through bore 36 extending axially therethrough and includes means at one end for securing the guide plug 26, which also serves to close the lower portion of bore 36. Guide plug 26 can be threaded as shown and can include an internally recessed area within which a resilient O-ring 40 can be positioned for sealing purposes. The opposite end of mandrel 20 includes a coaxial, reduced diameter piston surface 42 which terminates in an outwardly extending shoulder 44 at one end thereof and in an external thread 46 at the outer end thereof. Thread 46 is preferably an Acme thread, for example a 1.000-8 Acme-3G thread, for increased strength and in order to minimize the stress concentration sites which frequently exist when a thread having a V-type cross section, such as a 1.000-8UNC-2A, is utilized. A radially directed conduit 48 is provided between thread 46 and shoulder 44 to permit communication between through bore 36 and piston surface 42. Conduit 48 is spaced axially inwardly from the end of thread 46 and is preferably no closer thereto than two conduit diameters in order to minimize stress concentrations at the thread root and thereby reduce the propensity for failure at that position, which was frequently experienced when using prior art devices wherein the radial conduit was adjacent the thread end and the thread was a V-type thread.
Positioned between shoulder 44 and guide plug 26 at the lower end of mandrel 20 is a pair of opposed parallel flats 50 formed on the outer surface of mandrel 20 to facilitate the interconnection of the several parts of the assembly by providing surfaces on which a wrench or other suitable turning tool can be applied to permit engagement of threads 46 with a suitable connecting member.
A generally tubular hub member 52 is threadedly secured to the upper end of mandrel 20, opposite the end which carries plug 26, and also has a through bore 54 therein which is in axial alignment with through bore 36 in mandrel 20. Hub 52 also has a transverse threaded passageway 56 which extends radially from through bore 54 to the exterior of hub member 52. As shown, passageway 56 in hub member 52 is closed by means of a plug 58. As on mandrel 20, hub member 52 also includes a pair of opposed parallel flats 60 formed in the outer surface to facilitate interconnection. Adjacent flats 60 is an enlarged diameter portion 62 which defines an external abutment 64 at the interconnection with a reduced diameter piston surface 66. Piston surface 66 is a highly polished finished surface which includes a pair of axially spaced peripheral recesses 68 adapted to receive sealing rings, such as O-rings (not shown). As shown, piston surface 66 does not extend beyond conduit 48.
Hub member 52 includes an enlarged inner bore 65 which is concentric with through bore 54 and which is positioned inwardly of piston surface 66. Bore 65 includes an internal Acme thread 67 which engages thread 46 on mandrel 20. Thread 67 extends only partially along bore 65 and commences at a point spaced inwardly of the end of hub 52 to provide a smooth cylindrical surface which overlies a portion of piston surface 42 of mandrel 20. Bore 65 extends inwardly to an end relief groove 69 which terminates in an inner transverse wall 71 to provide an abutment for the end of mandrel 20. End relief groove 69 is positioned intermediate the ends of enlarged diameter portion 62 and the relative sizes thereof are such that the minimum hub wall thickness therebetween is greater than the minimum hub wall thickness between piston surface 66 and thread 67 to minimize fracture failure caused by bending loads.
Slidably positioned on the outer periphery of piston surface 42 of mandrel 20 is a cylindrical sleeve 70 which is of a stepped configuration having a first cylinder 72 adapted to slidably overlie the periphery of piston surface 42 and having an overlapping cylindrical extension in the form of a second cylinder 74 and which overlies piston surface 66 on hub 52. Positioned about the outer periphery of first cylinder 72 is a plurality of spaced annular sealing rings 76 with a plurality of intermediate spaced annular drift rings 78 positioned coaxially with the sealing rings and adjacent the respective ends thereof. Sealing rings 76 are formed from a resilient material, which can be natural or synthetic rubber, plastics, elastomers, or the like. Drift rings 78 are relatively inflexible, preferably rigid, metallic materials, so that any axial deflection in the assembly of sealing rings and drift rings is reflected solely in sealing rings 76 and not in drift rings 78.
Also positioned around piston surface 42 is a sleeve-like escape chamber 80 which abuts the side of the lowermost sealing ring and which has an inner wall 82 spaced from piston surface 42 to define an annular space within which first cylinder 72 is received. One or more radial apertures 84 extends from the annular space in order to permit escape of air when first cylinder 72 is moved axially toward plug 26.
The length of second cylinder 74 of sleeve 70 is such that when the uppermost end thereof is touching abutment 64, an annular space 86 (see FIG. 4) is provided between the lower end of hub 52 and an interior land 87 of sleeve 70 and is in communication with the radially extending conduit 48.
Upper mandrel 22 is of the same construction as lower mandrel 20 and like numerals identify like parts. However, instead of plug 58 as in lower mandrel 20, hub 52 of upper mandrel 22 includes a flow constriction in radially extending passageway 56. The constriction can be in the form of a plug 88 having an aperture 90 therein, the aperture preferably having a cross-sectional area substantially smaller than that of through bore 54 in hub 52.
Spacer tube 24, providing the interconnection between the respective hubs of upper mandrel 22 and lower mandrel 20, can be of any axial length desired, depending upon whether a single pipe connection joint is to be tested or whether a plurality of the same are to be tested, or even whether an entire pipe section between joints is to be tested for some particular reason. Tube 24 is a hollow cylinder having internal threads at each end adapted to engage the external threads on hubs 52. Again, an Acme thread is preferred for improved resistance to failure caused by stress concentrations.
The material from which the mandrels and hubs are preferably made is a high strength nickel-cobalt-chromium-molybdenum super-alloy designated MP35N, rather than the 4340HT and 4140HT still previously used. That super-alloy was found to provide the mechanical properties of extremely high yield strength, adequate elongation, and high fatigue resistance necessary to minimize failure of the parts subjected to tensile loading and fatigue cycling. Sleeves 70 can be made from 17-4-PH stainless steel; drift rings 78 can be made from 304 stainless steel; and plug 26 can be made from cold-rolled carbon steel.
The assembly of the testing tool is accomplished by interconnecting lower mandrel 20, as it is shown in FIG. 2, with spacer tube 24 by threading the latter thereto at hub 52, and thereafter, corresponding hub 52 of upper mandrel 22 is threadedly interconnected with the opposite end of spacer tube 24. Fluid conduit 34 is then connected to a suitable fitting (not shown) at the upper end of upper mandrel 22.
In use, assembled tool 18 is lowered into casing 10 by means of cable 30 to a point where the respective sealing rings of the upper and lower mandrels are on opposite sides of a joint, as illustrated in FIG. 1. A pressurized fluid is introduced to the interior of the tool through fluid connection 34 and through bores 36, 54 and acts through conduits 48 to cause the respective sleeves 70 to move in opposite directions relative to each other, toward the respective sealing rings 76, causing compression of the sealing rings radially outward expansion thereof into sealing engagement with the interior surface of casing 10.
Because the area of aperture 90 in hub member 52 associated with upper mandrel 22 is less than that of through bores 36 and 54 in the respective mandrels and hubs, the initial flow of fluid is confined to the mandrels and serves to force sleeves 80 axially against their associated sealing rings. When the latter have been expanded into tight engagement with the interior surface of the pipe, the pressure within the tool increases to the point where flow of pressurizing fluid occurs through aperture 90 and enters the annular space which is defined between the upper and lower sealing ring assemblies. Once a steady-state condition has been achieved, the pressure within the annular chamber can be monitored and any decay in pressure, which would indicate a fluid leak at the connection, would be reflected at the source of pressurized fluid and would signal the operator that repair of the joint assembly was necessary. Similarly, if desired, external indications of leakage can be provided and any of a number of sensing arrangements can be used to sense such leakage at the exterior of the connection joint.
While particular embodiments of the present invention have been illustrated and described, it will be apparent to those skilled in the art that various changes and modifications can be made without departing from the spirit and scope of the present invention, and it is intended to encompass in the appended claims all such changes and modifications which fall within the scope of the present invention.