USRE30311E - Apparatus and method for externally testing conduit connections - Google Patents

Apparatus and method for externally testing conduit connections Download PDF

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Publication number
USRE30311E
USRE30311E US06/041,028 US4102879A USRE30311E US RE30311 E USRE30311 E US RE30311E US 4102879 A US4102879 A US 4102879A US RE30311 E USRE30311 E US RE30311E
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US
United States
Prior art keywords
ring
test
connection
fluid pressure
seal
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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.)
Expired - Lifetime
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US06/041,028
Inventor
Gervase M. Chaplin
Thomas W. Childers
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ExxonMobil Upstream Research Co
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Exxon Production Research Co
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Filing date
Publication date
Priority claimed from US05/652,969 external-priority patent/US4019371A/en
Priority to AU22577/77A priority Critical patent/AU501296B2/en
Priority to GB17546/77A priority patent/GB1558857A/en
Application filed by Exxon Production Research Co filed Critical Exxon Production Research Co
Priority to US06/041,028 priority patent/USRE30311E/en
Application granted granted Critical
Publication of USRE30311E publication Critical patent/USRE30311E/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M3/00Investigating fluid-tightness of structures
    • G01M3/02Investigating fluid-tightness of structures by using fluid or vacuum
    • G01M3/26Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors
    • G01M3/28Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors for pipes, cables or tubes; for pipe joints or seals; for valves ; for welds
    • G01M3/2853Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors for pipes, cables or tubes; for pipe joints or seals; for valves ; for welds for pipe joints or seals
    • G01M3/2861Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors for pipes, cables or tubes; for pipe joints or seals; for valves ; for welds for pipe joints or seals for pipe sections by testing its exterior surface
    • 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
    • F16L23/00Flanged joints
    • F16L23/16Flanged joints characterised by the sealing means
    • F16L23/167Flanged joints characterised by the sealing means in connection with the appearance or detection of leaks

Abstract

Apparatus and method are disclosed for externally testing flanged or hubbed connections used on fluid conducting conduits. A ring gasket fits between the faces of the connecting flanges or hubs to effect a fluid tight seal. A test ring also fits between the faces of the hub or flange connection in a manner so as to form a space between the test ring and the ring gasket. Seal means closes the space between the test ring and the faces of the flanges or hubs. The outside diameter of the test ring is confined within fastening means which secures the hubs or flanges together. Fluid under pressure, used to test the effectiveness of the ring gasket seal, is applied to the space between the ring gasket and the test ring seal means. The pressure in that space falls when the ring gasket is defective but remains constant if the ring gasket is sound. Following the test, fluid pressure is bled off the space between the ring gasket and the test ring seal means. The test fluid pressure is applied to and bled from such space through a pressure port or passageway formed in the test ring or in one of the flanges or hubs.

Description

BACKGROUND OF THE INVENTION
Flanged or hubbed connections which connect together conduits for carrying fluids are conventionally tested by applying internal pressure to the seal elements and checking for signs of external leaks. However, it is often inconvenient, costly and/or impossible to perform such a test immediately after the connection is made, as for example, following installation of a pipeline riser or a subsea tie-in or a connection to a multiported vessel in offshore oil and gas drilling and production operations. It is advantageous to know that the ring gasket constituting the seal element in the connection has been properly installed and a sound seal obtained as soon as the connection is made.
The present invention permits evaluation of a seal in a flanged or hubbed connection between fluid carrying conduits through the application of external pressure to the seal immediately after the connection is made.
BRIEF DESCRIPTION OF THE INVENTION
A connection between fluid conducting conduits includes a ring gasket fitted between the faces of the halves of the connection and a test ring also fitted between the faces of the halves of the connection and surrounding the ring gasket. Seal means close off the spaces between the faces of the halves of the connection and the test ring. An annular space is formed between the ring gasket and test ring seal means. The outside diameter of the test ring fits within the means securing the halves of the connection together. A port or passageway formed in the test ring or in one of the halves of the connection extends from the annular space to the exterior of the connection. The exterior end of the port is connected to a source of fluid pressure. The exterior end of the port may be connected to a nipple which, in turn, is connected to the source of fluid pressure. When the port is formed in the test ring the nipple may also serve as a handle for inserting the test ring into and removing the test ring from the connection. The test ring may be made integral with the ring gasket or may be glued to it or may be arranged completely separate from it.
In conducting a test of the ring gasket after the port is connected to the source of fluid pressure, fluid pressure is applied to the annular space through the port to test the ring gasket. After the test, the fluid pressure in the annular space is bled off and the fluid pressure source disconnected from the port.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 illustrates one embodiment of the invention in which a test ring, having a pressure port therethrough, is arranged in a flanged connection and O-rings are positioned on the test ring;
FIG. 2 is a view taken along lines 2--2 of FIG. 1;
FIG. 3 is a schematic illustration of a test apparatus assembly connected to the flanged connection of FIG. 1;
FIG. 4 is a view similar to FIG. 2 illustrating severance of a portion of the nipple and its protector sleeve and plugging of the nipple;
FIG. 5 illustrates another embodiment of the invention in which the test ring of FIG. 1 is arranged in a hubbed connection and O-rings are positioned on the hubs;
FIGS. 6 and 7 illustrate side and top views, respectively, partly in section, of the seal ring (gasket) and test ring of FIGS. 1 and 2 formed integrally;
FIGS. 8 and 9 illustrate side and top views, respectively, partly in section, of the seal ring (gasket) and test ring of FIGS. 1 and 2 formed by gluing the test ring to the gasket; and
FIG. 10 illustrates still another embodiment of the invention in which a test ring is arranged in a hubbed connection having a pressure port therethrough.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
Referring to FIGS. 1 and 2 there is shown a flanged connection or coupling 10 having halves thereof bolted together by a series of studs 11 on which nuts 12 have been threaded. These studs are arranged in a circular pattern as shown in FIG. 2. A gasket in the form of a metal seal ring 15 is positioned between the flange halves in circular grooves 16 formed in the faces of the flange halves. A metal test ring 20 is also positioned between the flange halves. Test ring 20 contains O- ring seals 21 and 22 arranged thereon to seal off the space between the flange halve faces and test ring 20 to form a closed annular space 19 between outer diameter 15' of seal ring 15 and O- rings 21 and 22. The outer diameter 25 of test ring 20 is sized to fit inside the bolts in a bolted flange (or inside the clamp on a clamped hub connection as indicated in FIG. 5). Test ring thickness is machined to match the standard separation between flanges (or hubs) after the bolts (or clamps) are fully tightened. Test ring 20 contains a pressure port 23 which opens into annulus 19. A nipple 24 (shown in FIG. 1 sealingly threaded into the test ring) provides an extension port 23' of pressure port 23. A protector sleeve 26 surrounds a portion of nipple 24. A tubing connector fitting 27 is attached to the outer end of nipple 24 which protrudes between flange bolts 11, as shown. Nipple 24, together with protector sleeve 26, may serve as a handle to insert and arrange test ring 20 in and remove it from the connection.
As illustrated in FIG. 3 fitting 27 is connected to a source of fluid under pressure 30 through a hose or conduit 31 in which is connected a valve 32 for controlling flow of pressure fluid through hose 31 and a pressure gauge 33 for measuring pressure in hose 31.
In the operation of the apparatus illustrated in FIGS. 1 and 2 ring gasket 15 and test ring 20 are installed between the faces of the flange halves 10, as shown, and the connection of the flange halves is made by tightening nuts 12 on studs 11. Fluid under pressure is introduced into extension port 23', port 23 and annulus 19 through hose 31 and open valve 32 from source 30 resulting in pressure buildup in annulus 19. Valve 32 is then closed trapping fluid pressure in annulus 19. If the seal formed by seal ring 15 is defective, fluid will leak from the annulus 19 and pressure in the annulus will fall and be so indicated on pressure gauge 33. However, if the seal is sound the pressure in the annulus will remain constant which also will be indicated on pressure gauge 33.
After the test has been completed fluid pressure in annulus 19 is bled off and hose 31 is disconnected. Nipple 24 may then be left intact to serve as a weep hole for long life leak monitoring or it may be cut off leaving the connection area uncluttered if that is desired.
As shown in FIG. 4 a further alternative is to seal the nipple. The test nipple 24 and sleeve 26 are severed at the point they protrude from the flanges and nipple 24 is welded shut at the outer edge of the nipple protector sleeve 26 as shown by plug 40. In that manner a backup resilient seal (the O-rings) is provided for the seal effected by seal ring 15.
In the event there is insufficient clearance between the flange or hub faces for the O-ring grooves and the pressure port, one or both of the O-rings may be installed in the flange or hub faces instead of in the test ring, as illustrated in FIG. 5, or the test port may be drilled through one of the flanges or hubs, as illustrated in FIG. 10. Referring to FIG. 5 there is shown a hubbed connection or coupling 45 having the halves thereof clamped together by clamp means 46. A double cone metal seal ring or gasket 47 seals off the connection. A metal test ring 48 is positioned between the faces of the hub halves. O- rings 49 and 50 are located in grooves formed in the faces of hub members 45 to seal off the space between those faces and test ring 48 to form an annular space 51 between gasket 47 and O- rings 49 and 50. The test ring is provided with a pressure port 52 which connects to annular space 51. A nipple 53 containing an extension port 52' is connected to test ring 48, as shown. Nipple 53 is protected by a sleeve 54 and is also provided with a connector fitting 54' which connects to a hose 31 in the same manner hose 31 is connected to connector fitting 27 as described with respect to FIGS. 1 and 2, above. The test operation is also the same as the test operation described with respect to those figures.
The seal ring may be manufactured integral with the test ring as illustrated in FIGS. 6 and 7. When so made the combined gasket or seal ring and test ring 55 contains a pressure port 56 in the test ring section 57 thereof, which is open to an annular space 59, formed by an undercut or recessed surface in member 55, located between the seal ring section 58 thereof and the O-ring seals, not shown. A nipple 60 contains a connection fitting 61 for hose 31 and an extension port 56' of port 56. Nipple 60 is connected to section 57 and is surrounded by a nipple protector 62 in the same manner as is described above with respect to the embodiment of FIGS. 1 and 2. The integral test ring is particularly useful in subsea operations for the test ring section acts as a centralizing ring for the seal ring section making the task of locating the seal ring in grooves 16 of flanges 10, for example, (see FIG. 1) extremely easy and minimizes the chances of damaging the seal ring. More specifically, the outside diameter of the test ring fits just inside the bolt circle of the flange connection. The inside diameter of the test ring is slightly (e.g. 1/16 inch) larger than the outside diameter of the seal ring or gasket to assure proper positioning of the gasket. Thus, when three or four bolts have been installed in the connection, the test ring and the gasket are inserted together between the flanges or hubs and pushed against the bolts. This action automatically positions the gasket. Subsequent bolts cannot be installed unless the gasket (and test ring) are in proper position. This arrangement is particularly useful for making underwater connections where visibility is poor.
Also, the seal ring may be attached to the test ring by gluing one to the other with a resilient compound such as a silicon rubber adhesive. Such structure is illustrated in FIGS. 8 and 9 where there is shown a seal ring 70 glued to a test ring 71 by adhesive material 72. Test ring 71 contains a port 73 which is connected to an annular space 74 formed by undercutting or recessing test ring 71 adjacent seal ring 70. As similarly disclosed in other Figures a nipple 75 provided with a pressure port extension 73' and surrounded by a protective sleeve 76 welded thereto is threaded to test ring 71, as shown, and is provided with a suitable connection fitting 77.
The test port may be drilled through one of the flanges or hubs instead of being provided in the test ring and the nipple "handle," when the latter is included. Referring to FIG. 10 there is shown a hubbed connection or coupling 80 having halves thereof clamped together by clamp means 81. A double cone metal seal ring or gasket 82 seals off the connection. A metal test ring 83 is positioned between the faces of the hub halves. O- rings 84 and 85 are located in grooves formed in the faces of members 80 to seal off the space between the hub halve faces and test ring 83 to form an annular space 86 between gasket 82 and O- rings 84 and 85. The upper half of the hub halves 80 contains a pressure port 87 which extends from annular space 86 to the exterior thereof and is connected to a conduit 88 (which may be a nipple such as member 76 of FIG. 8) which in turn is connected to a suitable source of fluid pressure 30 as illustrated in FIG. 3.
It should be clear that when the seal ring and test ring are manufactured integral as illustrated in FIGS. 6 and 7 or are attached to each other by an adhesive as illustrated in FIGS. 8 and 9 they may be used with either the hub type or flange type connection. Also, the seals may be formed on the test ring or on the flange or hub members whether the test ring is separate from the seal ring, attached to the seal ring or formed integral with the seal ring. In addition, the sealing members and other components while preferably made of metallic materials may be made of nonmetallic materials. Other variations and modifications of the invention described herein may be made without departing from the scope of the invention as defined in the appended claims.

Claims (1)

    Having fully described the method, apparatus, advantages and objects of our invention we claim: .[.1. Apparatus for testing a connection between fluid conducting conduits employing an external source of fluid pressure comprising:
  1. grooves..]. .[.15. A method for externally testing a connection between fluid conducting conduits comprising the steps of:
    installing ring seal means in said connection for sealing off and preventing leaks through said connection when said connection is made;
    installing a test ring seal in said connection surrounding said ring seal means to form a closed annulus between said test seal ring and said ring seal means;
    connecting a source of fluid pressure to passageway means which extends from said closed annulus to the exterior of said connection;
    applying fluid pressure to said passageway means;
    shutting off the source of fluid pressure; and
    then measuring the fluid pressure in said closed annulus..]. .[.16. A method as recited in claim 15 comprising releasing fluid pressure from said annulus..]. .[.17. A method for externally testing a connection between fluid conducting conduits, said connection including ring seal means for sealing off and preventing leaks through said connection when said connection is made comprising the steps of:
    installing a test ring seal in said connection surrounding said ring seal means to form a closed annulus between said test ring seal and said ring seal means, said test seal ring having a pressure port;
    connecting a source of fluid pressure to said pressure port;
    applying fluid pressure to said pressure port;
    shutting off the source of fluid pressure; and then measuring the fluid pressure in said annulus..]. .[.18. A method as recited in claim 17 comprising:
    releasing fluid pressure from said annulus..]. .[.19. A method as recited in claim 18 including the steps of: after releasing fluid pressure from said annulus, cutting off a test nipple, which contains a port connected to said pressure port and which extends beyond the outer rim of said connection, adjacent the outer rim of said connection and then welding shut said port in said test nipple..]. .Iadd. 20. Apparatus for use in testing a connection between fluid conductive conduits, said connection having two mateable flanges, each of which contains a circle of alignable bolt holes comprising:
    a seal ring for engaging the surface of and sealing off the spaces between said flanges to prevent flow of fluids into and from said conduits via said flange connection;
    a test ring having seal means for sealing off the spaces between said flange faces and said test ring, said test ring and said seal ring forming a one-piece unit;
    an annular space formed between said seal ring, said seal means on said test ring and said mateable flange faces; and
    a passageway for communicating test fluid under pressure to said annular space for testing the effectiveness of said seal ring and said seal means, said test ring having a greater diameter than said seal ring with the outside diameter of said test ring being about the same diameter as the inside diameter of said circle of bolt holes in said flanges. .Iaddend..Iadd. 21. Apparatus as recited in claim 20 including means connected to said passageway for measuring fluid pressure in said annular space. .Iaddend..Iadd. 22. Apparatus as recited in claim 21 including a circular groove formed in each flange for receiving said seal ring. .Iaddend. .Iadd. 23. Apparatus as recited in claim 22 including a nipple extending external of said connection and connected to said port means. .Iaddend..Iadd. 24. Apparatus as recited in claim 23 in which said seal means comprises O-rings for sealing off the spaces between said flanges. .Iaddend..Iadd. 25. Apparatus as recited in claim 24 in which said passageway extends through said test ring. .Iaddend..Iadd. 26. Apparatus as recited in claim 25 including a source of fluid pressure connected to said passageway for supplying fluid pressure to said annular space. .Iaddend..Iadd. 27. Apparatus as recited in claim 24 in which said passageway extends through one of said flanges. .Iaddend..Iadd. 28. Apparatus as recited in claim 27 including a source of fluid pressure connected to said passageway for supplying fluid pressure to said annular space. .Iaddend..Iadd. 29. A method for testing a connection between fluid conducting conduits, said connection including two matable flanges each having a circle of alignable bolt holes comprising the steps of:
    inserting at least one bolt through at least one set of aligned holes in said flanges;
    inserting test sealing apparatus between said flanges, said sealing apparatus including a seal ring for sealing off the spaces between said flanges to prevent flow of fluids into and from said conduits and a test ring, formed integral with said seal ring, for sealing off the spaces between said flanges, said test ring and said seal ring having an annular space therebetween, said test ring having a greater diameter than said seal ring with the outside diameter of said test ring being about the same diameter as the inside diameter of said circle of bolt holes in said flanges;
    manipulating said sealing apparatus, including pushing said sealing apparatus against said bolt, until the outside diameter of said test ring is positioned within the diameter of said circle of bolt holes;
    inserting bolts through said remaining sets of aligned bolt holes;
    securing said flanges together;
    applying fluid pressure to said annular space;
    shutting off said fluid pressure; and then measuring the fluid pressure in said annular space. .Iaddend..Iadd. 30. A method as recited in claim 29 including inserting several bolts through sets of aligned holes in said flanges prior to inserting said test sealing apparatus, the outside diameter of said test ring being positioned within the diameter of said bolt holes by pushing sail sealing apparatus against said several inserted bolts. .Iaddend..Iadd. 31. A method as recited in claim 30 comprising:
    releasing fluid pressure from said annular space. .Iaddend..Iadd. 32. A method as recited in claim 31 in which said fluid pressure is applied through a passageway extending through said test ring. .Iaddend. .Iadd. 33. A method as recited in claim 32 in which a nipple is connected to said passageway and including the steps of cutting off said nipple adjacent the outer rim of said connection after releasing pressure from said annular space and then welding said nipple closed. .Iaddend..Iadd. 34. A method as recited in claim 31 in which said fluid pressure is applied through a passageway in one of said flanges. .Iaddend..Iadd. 35. A method as recited in claim 34 in which a nipple is connected to said passageway and including the steps of cutting off said nipple adjacent the outer rim of said connection after releasing pressure from said annular space and then welding said nipple closed. .Iaddend.
US06/041,028 1976-01-28 1979-05-21 Apparatus and method for externally testing conduit connections Expired - Lifetime USRE30311E (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
AU22577/77A AU501296B2 (en) 1976-01-28 1977-02-23 Externally testing conduit connections
GB17546/77A GB1558857A (en) 1976-01-28 1977-04-27 Apparatus and method for extermally testing conduit connections
US06/041,028 USRE30311E (en) 1976-01-28 1979-05-21 Apparatus and method for externally testing conduit connections

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US05/652,969 US4019371A (en) 1976-01-28 1976-01-28 Apparatus and method for externally testing conduit connections
GB17546/77A GB1558857A (en) 1976-01-28 1977-04-27 Apparatus and method for extermally testing conduit connections
US06/041,028 USRE30311E (en) 1976-01-28 1979-05-21 Apparatus and method for externally testing conduit connections

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US05/652,969 Reissue US4019371A (en) 1976-01-28 1976-01-28 Apparatus and method for externally testing conduit connections

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AU (1) AU501296B2 (en)
GB (1) GB1558857A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4888979A (en) * 1989-02-15 1989-12-26 The United States Department Of Energy Leak detection aid
US6523394B2 (en) * 2001-04-18 2003-02-25 The United States Of America As Represented By The Secretary Of The Navy Leak test fixture
US20090188301A1 (en) * 2008-01-24 2009-07-30 Caterpillar Inc. Faceplate connection assembly and method
US20110108280A1 (en) * 2009-11-10 2011-05-12 Benton Frederick Baugh Method of testing a drilling riser connection

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GB2264760B (en) * 1992-02-19 1995-06-14 Seaboard Lloyd Ltd Seal
GB2270767B (en) * 1992-09-17 1995-11-01 Texaco Ltd Leak detection
US5839765A (en) * 1996-11-01 1998-11-24 Cooper Cameron Corporation Metal seal ring for tubular joint
NO314155B1 (en) 2001-03-08 2003-02-03 Ann Helen Hystad Device by pipe flanging
CN102435404B (en) * 2011-09-22 2013-11-06 航天材料及工艺研究所 Thermal vibration joint test device and method of flange sealing structure under complicated loaded conditions
GB2521340B (en) 2013-10-14 2017-10-04 Edwards Ltd Vacuum system pipe couplings
GB201408263D0 (en) * 2014-05-09 2014-06-25 Klinger Ltd Gasket assembly
USD753801S1 (en) 2014-08-11 2016-04-12 Klinger Ltd. Seal
CN104359635A (en) * 2014-11-24 2015-02-18 中国航空动力机械研究所 Multifunctional all-working-condition metal elastic sealing ring testing device
GB2538323B (en) * 2015-05-15 2017-11-01 Evenort Ltd Mechanical seal assembly
CN106066230A (en) * 2016-06-14 2016-11-02 沈阳飞机工业(集团)有限公司 A kind of multi-link ring flange exerciser and using method thereof
CN108644499B (en) * 2018-05-08 2020-05-15 蔡美珠 Dredging pipe leak-proof connecting device

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US2350867A (en) * 1939-05-09 1944-06-06 Cameron Iron Works Inc Sealing and testing well head connections
US2460238A (en) * 1944-09-18 1949-01-25 Oil Ct Tool Company Casing head
US2478628A (en) * 1947-01-27 1949-08-09 Shell Dev Testing casing heads
GB854189A (en) * 1957-01-29 1960-11-16 Commissariat Energie Atomique Improvements in or relating to joints for effecting the sealing of the connection between two piping elements
GB952755A (en) * 1959-10-28 1964-03-18 Gray Tool Co Improved coupling for fluid pressure duct

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Publication number Priority date Publication date Assignee Title
US2350867A (en) * 1939-05-09 1944-06-06 Cameron Iron Works Inc Sealing and testing well head connections
US2460238A (en) * 1944-09-18 1949-01-25 Oil Ct Tool Company Casing head
US2478628A (en) * 1947-01-27 1949-08-09 Shell Dev Testing casing heads
GB854189A (en) * 1957-01-29 1960-11-16 Commissariat Energie Atomique Improvements in or relating to joints for effecting the sealing of the connection between two piping elements
GB952755A (en) * 1959-10-28 1964-03-18 Gray Tool Co Improved coupling for fluid pressure duct

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4888979A (en) * 1989-02-15 1989-12-26 The United States Department Of Energy Leak detection aid
US6523394B2 (en) * 2001-04-18 2003-02-25 The United States Of America As Represented By The Secretary Of The Navy Leak test fixture
US20090188301A1 (en) * 2008-01-24 2009-07-30 Caterpillar Inc. Faceplate connection assembly and method
US7814778B2 (en) 2008-01-24 2010-10-19 Caterpillar Inc Faceplate connection assembly and method
US20110108280A1 (en) * 2009-11-10 2011-05-12 Benton Frederick Baugh Method of testing a drilling riser connection
US8272444B2 (en) * 2009-11-10 2012-09-25 Benton Frederick Baugh Method of testing a drilling riser connection

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Publication number Publication date
AU501296B2 (en) 1979-06-14
GB1558857A (en) 1980-01-09
AU2257777A (en) 1978-08-31

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