US20010000225A1 - Apparatus for reducing fastener bending stress in flanged connections - Google Patents
Apparatus for reducing fastener bending stress in flanged connections Download PDFInfo
- Publication number
- US20010000225A1 US20010000225A1 US09/729,746 US72974600A US2001000225A1 US 20010000225 A1 US20010000225 A1 US 20010000225A1 US 72974600 A US72974600 A US 72974600A US 2001000225 A1 US2001000225 A1 US 2001000225A1
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- United States
- Prior art keywords
- fastener
- retaining means
- flange
- bending stress
- face
- Prior art date
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- 238000005452 bending Methods 0.000 title claims abstract description 35
- 230000000295 complement effect Effects 0.000 claims description 5
- 230000036316 preload Effects 0.000 claims 18
- 230000004048 modification Effects 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 230000004075 alteration Effects 0.000 description 2
- 238000005553 drilling Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L23/00—Flanged joints
- F16L23/02—Flanged joints the flanges being connected by members tensioned axially
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L23/00—Flanged joints
- F16L23/02—Flanged joints the flanges being connected by members tensioned axially
- F16L23/036—Flanged joints the flanges being connected by members tensioned axially characterised by the tensioning members, e.g. specially adapted bolts or C-clamps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L23/00—Flanged joints
- F16L23/003—Auxiliary devices
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L23/00—Flanged joints
- F16L23/006—Attachments
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L23/00—Flanged joints
- F16L23/02—Flanged joints the flanges being connected by members tensioned axially
- F16L23/032—Flanged joints the flanges being connected by members tensioned axially characterised by the shape or composition of the flanges
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S411/00—Expanded, threaded, driven, headed, tool-deformed, or locked-threaded fastener
- Y10S411/916—Bolt having tension feature
Definitions
- This invention relates to a novel apparatus for reducing stresses due to bending in threaded fasteners, particularly bolts and cap screws, used in connecting flanged connections.
- flanged connections have a wide variety of industrial uses including connecting structural members that will be subjected to critical external loads and in sealing high pressure vessels.
- the flanges used in such applications must be maintained in face to face contact to ensure proper operation. This face to face contact is maintained by the plurality of threaded fasteners that are tightened to a high percentage of their yield strength to ensure this contact is maintained. It is well known in the art that such flanges bend in an axial or meridional direction during this tightening procedure.
- This meridional bending is transmitted to the threaded fasteners and is known to contribute significantly to the stress in the threaded fastener and reduces the amount of tightening to which the threaded fastener can be safely subjected. This in turn reduces the face to face contact between the flanges and therefore the load to which the flanged connection can be subjected.
- the present invention has particular applicability in the oil and gas industry where large diameter tubular members with flanged end connections, called “risers” or “riser joints”, are used.
- risers are used in offshore drilling and production operations and extend from the wellhead at the ocean floor to a surface vessel. These risers have typically been manufactured in fifty and eighty foot lengths.
- the flanged connection between adjacent riser joints must contain internal pressure along with enormous external loads due to environmental conditions. It is critical that these flanged connections, and the threaded fasteners holding them together, function flawlessly.
- These flanged connections and the threaded fasteners connecting them are the area to which the present invention most closely applies.
- the current invention uses a radially tapered surface that is machined into the backface of the flange, adjacent to the bolt or stud holes, to compensate for the axial or meridional direction bending that the flange undergoes during fastener tightening.
- the machined radially tapered surface ensures that as the flanges bend the threaded fastener remains straight and thereby minimizes the bending stress transmitted to the fastener.
- an all thread stud with a single nut is used in place of the bolt of the first embodiment.
- a radially tapered surface is machined into the backface of the upper flange adjacent each of the stud holes.
- the lower flange has a plurality of complementary holes threaded to receive the all thread stud.
- the machined radially tapered surface of the backface of the flange is in substantially face to face contact with the nut of the fastener and perpendicular to the axis of the fastener.
- an all thread stud with a pair of nuts is used in place of the fasteners of the previous embodiments.
- a radially tapered surface is machined into the backface of the upper and lower flanges adjacent each of the stud holes.
- the machined radially tapered surfaces of the backface of the flanges are in substantially face to face contact with the nuts of the fasteners and perpendicular to the axis of the fastener.
- a principal object of the present invention is to provide an apparatus to reduce the bending stress transmitted to threaded fasteners due to deflection of the flange.
- a final object of the present invention is to provide an apparatus for reducing the bending stress in threaded fasteners without requiring the use of special fasteners.
- FIG. 1 is an isometric view of a riser connector used in subsea oil and gas drilling operations with the backface of the flanges machined with a radially tapered surface.
- FIG. 2 is a sectional view of the first embodiment of the radially tapered surface bending stress reducing apparatus using a threaded bolt fastener with the riser connectors unloaded.
- FIG. 3 is a sectional view of the first embodiment of the radially tapered surface bending stress reducing apparatus using a threaded bolt fastener with the riser connectors loaded.
- FIG. 4 is a sectional view of the second embodiment of the radially tapered surface bending stress reducing apparatus using a threaded stud and single nut with the riser connectors unloaded.
- FIG. 5 is a sectional view of the second embodiment of the radially tapered surface bending stress reducing apparatus using a threaded stud and single nut with the riser connectors loaded.
- FIG. 6 is a sectional view of the third embodiment of the radially tapered surface bending stress reducing apparatus using a threaded stud and two nuts with the riser connectors unloaded.
- FIG. 7 is a sectional view of the third embodiment of the radially tapered surface bending stress reducing apparatus using a threaded stud and two nuts with the riser connectors loaded.
- riser connector 100 is shown in an isometric view.
- Riser connector 100 includes first or upper flange 102 and second or lower flange 104 .
- Upper flange 102 and lower flange 104 include butt weld preparations 106 and 108 , respectively, for attaching appropriate sized tubular members (not shown) as is well known in the art.
- Seal element 110 is disposed in the bores of upper flange 102 and lower flange 104 .
- a plurality of fastener holes 112 are spaced circumferentially around upper flange 102 and lower flange 104 with threaded fasteners 114 disposed therein.
- Upper flange 102 and lower flange 104 include raised faces 116 and 118 , respectively, that are held in face to face contact when threaded fasteners 114 are tightened to a specified torque value.
- the first embodiment of the present invention includes upper flange 102 and lower flange 104 with raised faces 116 and 118 , respectively.
- Fastener hole 112 in upper flange 102 receives threaded fastener 120 in close fitting relationship.
- Fastener hole 112 in lower flange 104 includes threads 122 to engage threads 124 of threaded fastener 120 .
- Upper flange 102 includes backface 126 with radially tapered surface 128 machined thereon.
- the radially tapered surface 128 is tapered radially as shown to define angle ⁇ between tapered surface 128 and the underside 130 of the head 132 of threaded fastener 120 .
- riser connector 200 includes upper flange 102 and lower flange 104 with raised faces 116 and 118 , respectively.
- Fastener hole 112 in upper flange 102 receives threaded stud 202 in close fitting relationship.
- Fastener hole 112 in lower flange 104 includes threads 122 to engage threads 204 of threaded stud 202 .
- Upper flange 102 includes backface 126 with radially tapered surface 128 machined thereon.
- the radially tapered surface 128 is tapered radially as shown to define angle ⁇ between tapered surface 128 and the underside 206 of nut 208 of threaded stud 202 .
- tapered surface 128 is in face to face contact with underside 206 of nut 208 of threaded stud 202 and perpendicular to the axis of the stud 202 . This tapered surface 128 minimizes the bending stress from meridional bending of upper flange 102 transmitted to threaded stud 202 . This reduction in bending stress on threaded stud 202 is a significant factor in increasing the fatigue life of threaded studs 202 .
- riser connector 300 includes upper flange 102 and lower flange 104 with raised faces 116 and 118 , respectively.
- Fastener hole 112 in upper flange 102 and lower flange 104 receives threaded stud 302 in close fitting relationship.
- Upper flange 102 and lower flange 104 include backfaces 304 and 306 , respectively, with radially tapered surfaces 308 and 310 machined thereon, respectively.
- Radially tapered surfaces 308 and 310 are tapered radially as shown to define angle ⁇ between radially tapered surfaces 308 and 310 and the underside 312 of nuts 314 of threaded stud 302 . After threaded stud 302 is initially installed, nuts 314 are tightened and the undersides 312 of nuts 314 contact tapered surfaces 308 and 310 at the outer edge and angle ⁇ as shown.
- Radially tapered surfaces 308 and 310 are in face to face contact with underside 312 of nuts 314 of threaded stud 302 and perpendicular to the axis of the stud 302 . These radially tapered surfaces 308 and 310 minimize the bending stress from meridional bending of upper flange 102 and lower flange 104 transmitted to threaded stud 302 . This reduction in bending stress on threaded stud 302 is a significant factor in increasing the fatigue life of threaded studs 302 . Although shown with both flanges having radially tapered surfaces, the present invention envisions and claims a construction with only one flange having the radially tapered surfaces machined therein.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Mutual Connection Of Rods And Tubes (AREA)
- Bolts, Nuts, And Washers (AREA)
- Measuring Fluid Pressure (AREA)
- Flanged Joints, Insulating Joints, And Other Joints (AREA)
- Bending Of Plates, Rods, And Pipes (AREA)
- Discharge Heating (AREA)
Abstract
An apparatus for reducing the bending stress imparted to threaded fasteners in flanged connections is disclosed. The apparatus includes a radially tapered surface machined in the backface of the flanges to coact with the head of the threaded fastener as the threaded fastener is tightened to a predetermined torque value. This coaction compensates for flange deflection as the threaded fastener is tightened.
Description
- 1. This is a divisional application of application Ser. No. 09/216,201 filed Dec. 18, 1998, hereby incorporated herein by reference.
- 2. 1. Field of the Invention
- 3. This invention relates to a novel apparatus for reducing stresses due to bending in threaded fasteners, particularly bolts and cap screws, used in connecting flanged connections. Such flanged connections have a wide variety of industrial uses including connecting structural members that will be subjected to critical external loads and in sealing high pressure vessels. The flanges used in such applications must be maintained in face to face contact to ensure proper operation. This face to face contact is maintained by the plurality of threaded fasteners that are tightened to a high percentage of their yield strength to ensure this contact is maintained. It is well known in the art that such flanges bend in an axial or meridional direction during this tightening procedure. This meridional bending is transmitted to the threaded fasteners and is known to contribute significantly to the stress in the threaded fastener and reduces the amount of tightening to which the threaded fastener can be safely subjected. This in turn reduces the face to face contact between the flanges and therefore the load to which the flanged connection can be subjected.
- 4. The present invention has particular applicability in the oil and gas industry where large diameter tubular members with flanged end connections, called “risers” or “riser joints”, are used. These risers are used in offshore drilling and production operations and extend from the wellhead at the ocean floor to a surface vessel. These risers have typically been manufactured in fifty and eighty foot lengths. During normal operation the flanged connection between adjacent riser joints must contain internal pressure along with enormous external loads due to environmental conditions. It is critical that these flanged connections, and the threaded fasteners holding them together, function flawlessly. These flanged connections and the threaded fasteners connecting them are the area to which the present invention most closely applies.
- 5. 2. Description of Related Art
- 6. An apparatus for stretching threaded fasteners is shown in U.S. Pat. No. 3,749,362 (O'Connor et al.) The apparatus shown by O'Connor et al. uses an external fastener stretcher threaded onto a bolt to apply an axial load to the bolt wherein the bolt's nut can then be tightened with minimal torque. Removal of the fastener stretcher allows the bolt and nut to retain the load induced in the bolt.
- 7. The current invention uses a radially tapered surface that is machined into the backface of the flange, adjacent to the bolt or stud holes, to compensate for the axial or meridional direction bending that the flange undergoes during fastener tightening. The machined radially tapered surface ensures that as the flanges bend the threaded fastener remains straight and thereby minimizes the bending stress transmitted to the fastener.
- 8. According to the present invention, in a first embodiment a radially tapered surface is machined into the backface of the upper flange adjacent each of the bolt holes. The lower flange has a plurality of complementary holes threaded to receive the bolt. As the bolt fastener is tightened to its predetermined value and the flange deflects, the head of the fastener remains vertical while the radially tapered surface moves downwardly. At maximum fastener torque and flange deflection, the machined radially tapered surface of the backface of the flange is in substantially face to face contact with the head of the fastener and perpendicular to the axis of the fastener.
- 9. In a second embodiment of the invention, an all thread stud with a single nut is used in place of the bolt of the first embodiment. A radially tapered surface is machined into the backface of the upper flange adjacent each of the stud holes. The lower flange has a plurality of complementary holes threaded to receive the all thread stud. As in the first embodiment, as the nut of the fastener is tightened to its predetermined value and the flange deflects, the head of the fastener remains vertical while the radially tapered surface moves downwardly. At maximum fastener torque and flange deflection, the machined radially tapered surface of the backface of the flange is in substantially face to face contact with the nut of the fastener and perpendicular to the axis of the fastener.
- 10. In a third embodiment of the invention, an all thread stud with a pair of nuts is used in place of the fasteners of the previous embodiments. A radially tapered surface is machined into the backface of the upper and lower flanges adjacent each of the stud holes. As in the previous embodiments, as the nuts of the fastener are tightened to their predetermined value and the flange deflects, the fastener remains vertical while the radially tapered surface moves downwardly. At maximum fastener torque and flange deflection, the machined radially tapered surfaces of the backface of the flanges are in substantially face to face contact with the nuts of the fasteners and perpendicular to the axis of the fastener.
- 11. A principal object of the present invention is to provide an apparatus to reduce the bending stress transmitted to threaded fasteners due to deflection of the flange.
- 12. Another object of the present invention is to provide an apparatus for increasing the fatigue life of threaded fasteners used in flanged connections.
- 13. A final object of the present invention is to provide an apparatus for reducing the bending stress in threaded fasteners without requiring the use of special fasteners.
- 14. These with other objects and advantages of the present invention are pointed out with specificness in the claims annexed hereto and form a part of this disclosure. A full and complete understanding of the invention may be had by reference to the accompanying drawings and description of the preferred embodiments.
- 15. These and other objects and advantages of the present invention are set forth below and further made clear by reference to the drawings, wherein:
- 16.FIG. 1 is an isometric view of a riser connector used in subsea oil and gas drilling operations with the backface of the flanges machined with a radially tapered surface.
- 17.FIG. 2 is a sectional view of the first embodiment of the radially tapered surface bending stress reducing apparatus using a threaded bolt fastener with the riser connectors unloaded.
- 18.FIG. 3 is a sectional view of the first embodiment of the radially tapered surface bending stress reducing apparatus using a threaded bolt fastener with the riser connectors loaded.
- 19.FIG. 4 is a sectional view of the second embodiment of the radially tapered surface bending stress reducing apparatus using a threaded stud and single nut with the riser connectors unloaded.
- 20.FIG. 5 is a sectional view of the second embodiment of the radially tapered surface bending stress reducing apparatus using a threaded stud and single nut with the riser connectors loaded.
- 21.FIG. 6 is a sectional view of the third embodiment of the radially tapered surface bending stress reducing apparatus using a threaded stud and two nuts with the riser connectors unloaded.
- 22.FIG. 7 is a sectional view of the third embodiment of the radially tapered surface bending stress reducing apparatus using a threaded stud and two nuts with the riser connectors loaded.
- 23. With reference to the drawings, and particularly to FIG. 1,
riser connector 100 is shown in an isometric view.Riser connector 100 includes first orupper flange 102 and second orlower flange 104.Upper flange 102 andlower flange 104 include 106 and 108, respectively, for attaching appropriate sized tubular members (not shown) as is well known in the art.butt weld preparations Seal element 110 is disposed in the bores ofupper flange 102 andlower flange 104. A plurality offastener holes 112 are spaced circumferentially aroundupper flange 102 andlower flange 104 with threadedfasteners 114 disposed therein.Upper flange 102 andlower flange 104 include raised faces 116 and 118, respectively, that are held in face to face contact when threadedfasteners 114 are tightened to a specified torque value. - 24. As best seen in FIG. 2, the first embodiment of the present invention includes
upper flange 102 andlower flange 104 with raised 116 and 118, respectively.faces Fastener hole 112 inupper flange 102 receives threadedfastener 120 in close fitting relationship.Fastener hole 112 inlower flange 104 includesthreads 122 to engagethreads 124 of threadedfastener 120.Upper flange 102 includesbackface 126 with radially taperedsurface 128 machined thereon. - 25. The radially tapered
surface 128 is tapered radially as shown to define angle θ between taperedsurface 128 and theunderside 130 of thehead 132 of threadedfastener 120. When threadedfastener 120 is initially installed and threaded intolower flange 104, theunderside 130 of thehead 132 of threadedfastener 120 contacts taperedsurface 128 at the outer edge and angle θ as shown. - 26. Referring to FIG. 3, when threaded
fastener 120 is fully tightened, theflange 102 has deflected downwardly by the angle θ. Radially taperedsurface 128 is in face to face contact withunderside 130 of thehead 132 of threadedfastener 120 and perpendicular to the axis of thefastener 120. This radially taperedsurface 128 minimizes the bending stress from meridional bending ofupper flange 102 transmitted to threadedfastener 120. This reduction in bending stress on threadedfastener 120 is a significant factor in increasing the fatigue life of threadedfasteners 120. - 27. A second embodiment of the present invention is shown in FIG. 4. Those items that are the same as in the first embodiment retain the same numeric designation. As in the first embodiment,
riser connector 200 includesupper flange 102 andlower flange 104 with raised 116 and 118, respectively.faces Fastener hole 112 inupper flange 102 receives threadedstud 202 in close fitting relationship.Fastener hole 112 inlower flange 104 includesthreads 122 to engagethreads 204 of threadedstud 202.Upper flange 102 includesbackface 126 with radially taperedsurface 128 machined thereon. - 28. The radially tapered
surface 128 is tapered radially as shown to define angle θ between taperedsurface 128 and theunderside 206 ofnut 208 of threadedstud 202. After threadedstud 202 is initially installed and threaded intolower flange 104,nut 208 is tightened and theunderside 206 ofnut 208 contacts taperedsurface 128 at the outer edge and angle θ as shown. - 29. As best seen in FIG. 5, when
nut 208 is fully tightened, theflange 102 has deflected downwardly by the angle θ.Tapered surface 128 is in face to face contact withunderside 206 ofnut 208 of threadedstud 202 and perpendicular to the axis of thestud 202. Thistapered surface 128 minimizes the bending stress from meridional bending ofupper flange 102 transmitted to threadedstud 202. This reduction in bending stress on threadedstud 202 is a significant factor in increasing the fatigue life of threadedstuds 202. - 30. A third embodiment of the present invention is shown in FIG. 6. Those items that are the same as in the first two embodiments retain the same numeric designation. As in the prior embodiments,
riser connector 300 includesupper flange 102 andlower flange 104 with raised 116 and 118, respectively.faces Fastener hole 112 inupper flange 102 andlower flange 104 receives threadedstud 302 in close fitting relationship.Upper flange 102 andlower flange 104 include 304 and 306, respectively, with radially taperedbackfaces 308 and 310 machined thereon, respectively.surfaces - 31. Radially
308 and 310 are tapered radially as shown to define angle θ between radially taperedtapered surfaces 308 and 310 and thesurfaces underside 312 ofnuts 314 of threadedstud 302. After threadedstud 302 is initially installed,nuts 314 are tightened and theundersides 312 ofnuts 314 contact tapered 308 and 310 at the outer edge and angle θ as shown.surfaces - 32. As best seen in FIG. 7, when
nuts 314 are fully tightened, the 102 and 104 are deflected by the angle θ. Radiallyflanges 308 and 310 are in face to face contact withtapered surfaces underside 312 ofnuts 314 of threadedstud 302 and perpendicular to the axis of thestud 302. These radially tapered 308 and 310 minimize the bending stress from meridional bending ofsurfaces upper flange 102 andlower flange 104 transmitted to threadedstud 302. This reduction in bending stress on threadedstud 302 is a significant factor in increasing the fatigue life of threadedstuds 302. Although shown with both flanges having radially tapered surfaces, the present invention envisions and claims a construction with only one flange having the radially tapered surfaces machined therein. - 33. My improved apparatus to reduce the bending stress transmitted to threaded fasteners due to flange deflection and the methods of its application will be readily understood from the foregoing description and it will be seen I have provided an improved apparatus requiring minimal modification to existing flanges to reduce the bending stresses transmitted to the threaded fasteners. Furthermore, while the invention has been shown and described with respect to certain preferred embodiments, it is obvious that equivalent alterations and modifications will occur to others skilled in the art upon the reading and understanding of the specification. The present invention includes all such equivalent alterations and modifications, and is limited only by the scope of the appended claims.
Claims (9)
1. A flanged connection fastener bending stress reduction apparatus, comprising:
first and second flanges in facing relationship, said first flange having a plurality of fastener holes therethrough, said second flange having a plurality of complementary fastener holes therein;
said first flange fastener holes having a radially tapered surface on the back face of said first flange;
a fastener extending through said first flange fastener holes;
said radially tapered surface of said first flange fastener holes configured to minimize bending stress on said fastener when said fastener is tensioned;
said fastener including first and second preload retaining means; and, said fastener first and second preload retaining means engaging said first and second flanges, respectively, whereby tensioning of said fastener preloads said fastener and maintains said first and second flanges in preloaded abutting relationship.
2. A flanged connection fastener bending stress reduction apparatus according to wherein:
claim 1
said first fastener preload retaining means includes a flanged end, said flanged end having an upper end configured to receive a wrenching means for tightening said fastener, said lower end of said flanged end of said first fastener preload retaining means having a flat face;
said second fastener preload retaining means includes a threaded end; and,
said second flange complementary holes are threaded to receive said second fastener preload retaining means threaded end.
3. A flanged connection fastener bending stress reduction apparatus according to wherein:
claim 2
tensioning of said fastener causes said radially tapered surface to engage said flat face of said lower end of said flanged end of said first fastener preload retaining means in face to face contact.
4. A flanged connection fastener bending stress reduction apparatus according to wherein:
claim 1
said first fastener preload retaining means includes a threaded end and a nut positioned thereon, said lower end of said nut having a flat face;
said second fastener preload retaining means includes a threaded end; and,
said second flange complementary holes are threaded to receive said second fastener preload retaining means threaded end.
5. A flanged connection fastener bending stress reduction apparatus according to wherein:
claim 4
tensioning of said fastener causes said radially tapered surface to engage said flat face of said nut of said first fastener preload retaining means in face to face contact.
6. A flanged connection fastener bending stress reduction apparatus according to wherein:
claim 1
said first fastener preload retaining means includes a threaded end and a nut positioned thereon, said lower end of said nut having a flat face; and,
said second fastener preload retaining means includes a threaded end and a nut positioned thereon.
7. A flanged connection fastener bending stress reduction apparatus according to wherein:
claim 6
tensioning of said fastener causes said radially tapered surface to engage said flat face of said nut of said first fastener preload retaining means in face to face contact.
8. A flanged connection fastener bending stress reduction apparatus according to wherein:
claim 1
said second flange fastener holes having a radially tapered surface on the back face of said second flange;
said first fastener preload retaining means includes a threaded end and a nut positioned thereon, said nut having a flat face; and,
said second fastener preload retaining means includes a threaded end and a nut positioned thereon, said nut having a flat face.
9. A flanged connection fastener bending stress reduction apparatus according to wherein:
claim 8
tensioning of said fastener causes said radially tapered surfaces to engage said flat faces of said nuts of said first and second fastener preload retaining means in face to face contact.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US09/729,746 US6361085B2 (en) | 1998-12-18 | 2000-12-05 | Apparatus for reducing fastener bending stress in flanged connections |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US09/216,201 US6176663B1 (en) | 1998-12-18 | 1998-12-18 | Apparatus for reducing fastener bending stress in flanged connections |
| US09/729,746 US6361085B2 (en) | 1998-12-18 | 2000-12-05 | Apparatus for reducing fastener bending stress in flanged connections |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US09/216,201 Division US6176663B1 (en) | 1998-12-18 | 1998-12-18 | Apparatus for reducing fastener bending stress in flanged connections |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| US20010000225A1 true US20010000225A1 (en) | 2001-04-12 |
| US6361085B2 US6361085B2 (en) | 2002-03-26 |
Family
ID=22806142
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US09/216,201 Expired - Lifetime US6176663B1 (en) | 1998-12-18 | 1998-12-18 | Apparatus for reducing fastener bending stress in flanged connections |
| US09/729,746 Expired - Lifetime US6361085B2 (en) | 1998-12-18 | 2000-12-05 | Apparatus for reducing fastener bending stress in flanged connections |
Family Applications Before (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US09/216,201 Expired - Lifetime US6176663B1 (en) | 1998-12-18 | 1998-12-18 | Apparatus for reducing fastener bending stress in flanged connections |
Country Status (5)
| Country | Link |
|---|---|
| US (2) | US6176663B1 (en) |
| BR (1) | BR9905896A (en) |
| GB (2) | GB2344866B (en) |
| NO (2) | NO334894B1 (en) |
| SG (1) | SG74170A1 (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2010107903A1 (en) * | 2009-03-18 | 2010-09-23 | Taper-Lok Corporation | Pipe connection having a reverse hub |
| CN104896225A (en) * | 2015-05-07 | 2015-09-09 | 胡和萍 | High-pressure petroleum transportation pipe connector |
| EP2971442A4 (en) * | 2013-03-15 | 2016-10-26 | Ameriforge Group Inc | RIGGING COLUMNS ASSEMBLIES |
| WO2017048422A1 (en) * | 2015-09-15 | 2017-03-23 | Cameron International Corporation | Marine riser system |
| US20190145366A1 (en) * | 2016-04-18 | 2019-05-16 | Continental Automotive Gmbh | Arrangement of Housing and a Flange |
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| FR2921144B1 (en) * | 2007-09-19 | 2009-12-18 | Snecma | PRE-STRESSED FLANGED CONNECTION DEVICE WITH FLANGES |
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- 1999-10-25 SG SG1999005287A patent/SG74170A1/en unknown
- 1999-12-15 NO NO19996204A patent/NO334894B1/en not_active IP Right Cessation
- 1999-12-16 BR BR9905896-0A patent/BR9905896A/en not_active IP Right Cessation
- 1999-12-16 GB GB9929648A patent/GB2344866B/en not_active Expired - Fee Related
-
2000
- 2000-12-05 US US09/729,746 patent/US6361085B2/en not_active Expired - Lifetime
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2001
- 2001-01-19 GB GBGB0101407.5A patent/GB0101407D0/en not_active Ceased
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| Publication number | Priority date | Publication date | Assignee | Title |
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| WO2010107903A1 (en) * | 2009-03-18 | 2010-09-23 | Taper-Lok Corporation | Pipe connection having a reverse hub |
| US20100237614A1 (en) * | 2009-03-18 | 2010-09-23 | Howard Erik M | Pipe Connection Having a Reverse Hub |
| US10041614B2 (en) | 2009-03-18 | 2018-08-07 | Taper-Lok Corporation | Pipe connection having a reverse hub |
| EP2971442A4 (en) * | 2013-03-15 | 2016-10-26 | Ameriforge Group Inc | RIGGING COLUMNS ASSEMBLIES |
| EP3492689A1 (en) * | 2013-03-15 | 2019-06-05 | Ameriforge Group Inc. | Drilling riser assemblies |
| CN104896225A (en) * | 2015-05-07 | 2015-09-09 | 胡和萍 | High-pressure petroleum transportation pipe connector |
| WO2017048422A1 (en) * | 2015-09-15 | 2017-03-23 | Cameron International Corporation | Marine riser system |
| US9702213B2 (en) | 2015-09-15 | 2017-07-11 | Cameron International Corporation | Marine riser system |
| US20190145366A1 (en) * | 2016-04-18 | 2019-05-16 | Continental Automotive Gmbh | Arrangement of Housing and a Flange |
| EP4435237A1 (en) * | 2023-03-20 | 2024-09-25 | RTX Corporation | Mounting assembly for coupling a first case section of a gas turbine engine to a second case section of the gas turbine engine and gas turbine engine |
| KR102740829B1 (en) * | 2024-02-19 | 2024-12-10 | 김영율 | Flange with improved weldability |
Also Published As
| Publication number | Publication date |
|---|---|
| US6361085B2 (en) | 2002-03-26 |
| US6176663B1 (en) | 2001-01-23 |
| NO339933B1 (en) | 2017-02-20 |
| BR9905896A (en) | 2000-08-22 |
| GB9929648D0 (en) | 2000-02-09 |
| NO996204D0 (en) | 1999-12-15 |
| NO334894B1 (en) | 2014-06-30 |
| GB2344866A (en) | 2000-06-21 |
| NO20111403L (en) | 2000-06-19 |
| SG74170A1 (en) | 2000-07-18 |
| GB2344866B (en) | 2001-02-07 |
| NO996204L (en) | 2000-06-19 |
| GB0101407D0 (en) | 2001-03-07 |
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