Packing elements are used for securing production tubing inside of casing or a liner within a borehole, for example. Packing elements are also used to create separate zones within a borehole. A packing element is mounted to a rigid support body, and carried by a conveyance tubular (such as a production tubing string) downhole to a desired position. The packing element is then set within an annular space between the conveyance tubular and the outer tubing, casing, or open-hole diameter, and held in place by a packing element containment system. Conventional packing element containment systems may fail when exposed to prolonged high working pressures and large extrusion gaps.
A packing element containment system includes a support member extending from a first end to a second end. One of the first and second ends includes a support ring engagement section. A support ring is carried by the support ring engagement section of the support member. The support ring is configured and disposed to shift relative to the support member converting an axial movement of one of the support ring and the support member to a radial expansion of the support ring to provide one of a support to an anti-extrusion ring and containment for a packing element.
A method of containing a packing element includes shifting a support ring relative to a support member with an axial force, and transferring the axial force into a radial force through an outward expansion of the support ring.
Referring now to the drawings wherein like elements are numbered alike in the several Figures:
A resource extraction system, in accordance with an exemplary embodiment, is indicated generally at 2, in
In accordance with an exemplary embodiment, a packing element containment system 42 is provided on inner conduit 34 to provide support for packing element 38. In addition, packer 24 includes slip components, indicated at 44 and 46. Packer 24 is introduced downhole into bore 21 to a desired position in formation 22. Packing element 38 is activated to move against a casing 47 in formation 22 to create a zonal isolation. Of course, it should be understood, that packing element 38 may be moved into contact with a tubular (not shown) or an open hole diameter (also not shown). As will be detailed more fully below, an axial force is delivered to packer 24 through setting string 32 and eventually into an anti-extrusion ring 48 provided adjacent to packing element 38. Packing element containment system 42 translates the axial force to a radial expansion that limits or prevents extrusion of packing element 38 depending on the configuration. At this point, it should be understood that packing element 38 may take on a variety of forms and should not be considered to be limited to the particular packing element shown. It should be further understood that packing element 38 may be formed from a variety of materials and may be present in various quantities downhole.
As shown in
Support ring 62 includes a body portion 97 having an axial end 98. Body portion 97 also includes an outer surface portion 99 and an inner surface portion 100 that defines a first radial thickness. Inner surface portion 100 may be provided with a plurality of threads 102 that may engage with threads 93 on outer surface section 82 of support member 60. Support ring 62 also includes a deflection member 110 extending from body portion 97. Interaction between an angled surface 112 of anti-extrusion ring 48 and axial end 98 causes support ring 62 to move over support ring engagement section 80. Plurality of threads 102 move axially over threads 93 converting axial movement of support member 60 relative to support ring 62 into a radial expansion of support ring 62. As support ring 62 moves relative to support member 60, deflection member 110 begins to fold, as will be detailed below.
In accordance with an aspect of an exemplary embodiment, deflection member 110 extends from a first end portion 113, coupled to body portion 97, to a second, cantilevered, end portion 114 and includes a radially outer surface 116 and a radially inner surface 117 that defines a second radial thickness that is less than the first radial thickness. A passage (not separately labeled) extends through deflection member 110 and may be provided with a pin 122 that secures support ring 62 to support member 60. In the exemplary embodiment shown, radially outer surface 116 includes first and second annular grooves 124 and 125. Radially inner surface includes a third annular groove 126 that is arranged between first and second annular groves 124 and 125. Grooves 124-126 form a deformation or folding zone 130.
More specifically, relative axial movement of support member 60 and support ring 62 causes deflection member 110 to contact an abutment surface (not separately labeled) on body 68. Further relative axial movement causes deflection member 110 to bend or fold at annular grooves 124-126. The bending of deflection member 110 allows threads 102 on support ring 62 to shift relative to threads 93 on support member 60. As threads 102 travel axially along threads 93, support ring 62 expands radially outwardly, as shown in
Reference will now follow to
Support ring 138 includes a body portion 164 having an axial end 165. Body portion 164 further includes an outer surface portion 166 and an inner surface portion 167 that defines a first radial thickness. Inner surface portion 167 may be provided with a plurality of threads 169 that may engage with threads 162 on outer surface section 154 of support member 136. Support ring 138 also includes a deflection member 173 extending from body portion 164. In a manner similar to that described above, deflection member 173 folds or deflects when axial end 165 is forced against angled surface 112 of anti-extrusion ring 48.
In accordance with an aspect of an exemplary embodiment, deflection member 173 extends from a first end portion 176, coupled to body portion 164, to a second, cantilevered, end portion 177 and includes a radially outer surface 179 and a radially inner surface 180 that defines a second radial thickness that is less than the first radial thickness. A plurality of openings, one of which is indicated at 184 extends through deflection member 173. Openings 184 define a plurality of deformation members 186 that extends axially outwardly of body portion 164. In accordance with an aspect of the exemplary embodiment, deformation members 186 extend at an angle relative to an axial axis to allow for axial deformation of deflection member 173.
More specifically, relative axial movement of support member 136 and support ring 138 caused by an axial force applied by anti-extrusion ring 48 causes deflection member 173 to contact an abutment surface (not separately labeled) on body 143. Further relative axial movement causes deformation members 186 to bend. The bending of deformation members 186 allows threads 169 on support ring 138 to shift relative to threads 162 on support member 136. As threads 169 travel axially along threads 162, support ring 138 expands radially outwardly, as shown in
Reference will now follow to
Support ring 194 includes a body portion 217 having an axial end 218. Body portion 217 further includes outer surface portion 220 and an inner, angled surface portion 221 that defines a first radial thickness. Inner, angled surface portion 221 may compliment outer, angled surface section 207 of support member 192. Support ring 194 also includes a deflection member 224 extending from body portion 217. In a manner similar to that discussed above, deflection member 224 folds or deflects when axial end 218 is forced against angled surface 112 of anti-extrusion ring 48.
In accordance with an aspect of an exemplary embodiment, deflection member 224 extends from a first end portion 229, coupled to body portion 217, to a second, cantilevered, end portion 230 and includes a radially outer surface 232 and a radially inner surface 233 that defines a second radial thickness that is less than the first radial thickness. A snap member 235 is provided at second, cantilevered end portion 230. Snap member 235 snap-fittingly engages with annular groove 214 provided on body 197 to retain support ring 194 relative to support member 192. In accordance with an aspect of the exemplary embodiment, a plurality of slots, one of which is indicated at 239, extends from second, cantilevered end portion 230 toward first end portion 229. Slots 239 form a plurality of deflecting or deformation members 241.
Relative axial movement of support member 192 and support ring 194 resulting from an interaction between axial end 218 and anti-extrusion ring 48 causes snap member 235 to become unseated from annular groove 214, as shown in
At this point, it should be understood that the exemplary embodiments describe a packing element containment system that converts axial movement of a downhole tool to a radial expansion of a support ring to limit extrusion gap of a packing element. While shown on a packer, designed with slip-element-slip packing element employed permanently downhole, the exemplary embodiment may also be employed with retrievable and/or removable packing element systems. It can also be employed in additional packer configurations such as slip-element configuration in which all slips are located above the packing element, sometimes referred to as a “slips above” configuration or an element-slip design in which all slips are located below the packing element, sometimes referred to as the “slips below” configuration. Further, while shown as engaging an anti-extrusion ring, the support ring may also be configured to directly engage a packing element as shown in
While one or more embodiments have been shown and described, modifications and substitutions may be made thereto without departing from the spirit and scope of the invention. Accordingly, it is to be understood that the present invention has been described by way of illustrations and not limitation.
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Entry |
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International Search Report and Written Opinion of the International Searching Authority issued in related International Patent Application No. PCT/US15/46791 dated Oct. 19, 2015, 8 pages. |
Parker Hannifin Corporation, “Packing Elements: Custom Designed for the Most Challenging Applications”, 2014, 4 pages, retrieved at: http://www.parker.com/literature/Engineered%20Seals%20Division/ESD%20Packing%20Elements%205612.pdf dated Jul. 1, 2016. |
Number | Date | Country | |
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20160090813 A1 | Mar 2016 | US |