# Patent

## Title
Tubular anchoring system and method

## Abstract

A tool setting arrangement includes a mandrel, and a tool positionable at the mandrel. The tool includes, a cone, and at least one slip in operable communication with the cone configured to radially expand to set the tool when the slip is moved relative to the cone with at least a setting load. The at least one slip has a portion configured to engage with a feature of the mandrel such that movement of the mandrel relative to the cone causes the at least one slip to move relative to the cone, at least one of the portion and the feature is configured to release at a release load to disengage the mandrel from the tool. The release load is selected to be greater than the setting load.

## Background
CROSS REFERENCE TO RELATED APPLICATION
This application is a continuation-in-part application of U.S. patent application Ser. No. 13/358,307, filed Jan. 25, 2012, the entire contents of which are incorporated herein by reference.


BACKGROUND
Tubular systems, such as those used in the completion and carbon dioxide sequestration industries often employ anchors to positionally fix one tubular to another tubular. Although existing anchoring systems serve the function for which they are intended, the industry is always receptive to new systems and methods for anchoring tubulars.
BRIEF DESCRIPTION
Disclosed herein is a tool setting arrangement. The arrangement includes a mandrel, and a tool positionable at the mandrel. The tool includes, a cone, and at least one slip in operable communication with the cone configured to radially expand to set the tool when the slip is moved relative to the cone with at least a setting load. The at least one slip has a portion configured to engage with a feature of the mandrel such that movement of the mandrel relative to the cone causes the at least one slip to move relative to the cone, at least one of the portion and the feature is configured to release at a release load to disengage the mandrel from the tool. The release load is selected to be greater than the setting load.
Further disclosed herein is a method of setting a tool within a structure. The method includes running a tool disposed at a mandrel within a structure, loading a portion of at least one slip of the tool with a feature of the mandrel, moving the at least one slip relative to a cone, anchoring the tool with a setting load applied between the portion and the feature, releasing at least one of the portion and the feature with a release load applied between the portion and the feature, and disengaging the mandrel from the tool.



BRIEF DESCRIPTION OF THE DRAWINGS
The following descriptions should not be considered limiting in any way. With reference to the accompanying drawings, like elements are numbered alike:
FIG. 1 depicts a cross sectional view of a tubular anchoring system disclosed herein in a non-anchoring position;
FIG. 2 depicts a cross sectional view of the tubular anchoring system of FIG. 1 in an anchoring position;
FIG. 3 depicts a cross sectional view of an alternate tubular anchoring system disclosed herein in a non-anchoring position;
FIG. 4 depicts a cross sectional view of the tubular anchoring system of FIG. 3 in an anchoring position;
FIG. 5 depicts a cross sectional view of an alternate tubular anchoring system disclose herein;
FIG. 6 depicts a cross sectional view of yet another alternate tubular anchoring system disclosed herein
FIG. 7 depicts a cross sectional perspective view of a tool setting arrangement disclosed herein;
FIG. 8 depicts a magnified partial cross sectional view of the tool setting arrangement of FIG. 7;
FIG. 9 depicts a perspective view of slips employed in the tool setting arrangement of FIG. 7; and
FIG. 10 depicts a partial cross sectional view of an alternate embodiment of a tool setting arrangement disclosed herein.



DETAILED DESCRIPTION
A detailed description of one or more embodiments of the disclosed apparatus and method are presented herein by way of exemplification and not limitation with reference to the Figures.
Referring to FIGS. 1 and 2, a tubular anchoring system disclosed herein is illustrated at 10. The system 10, among other things includes, a frustoconical member 14, a sleeve 18, shown herein as a slip ring having a surface 22, a seal 26, having a surface 30, and a seat 34. The system is configured such that longitudinal movement of the frustoconical member 14 relative to the sleeve 18 and relative to the seal 26 cause the surfaces 22 and 30 of the sleeve 18 and seal 26 respectively to be radially altered. And, although in this embodiment the radial alterations are in radially outward directions, in alternate embodiments the radial alterations could be in other directions such as radially inward. The seat 34 is connected with the frustoconical member 14 such that movement of the seat 34 also causes movement of the frustoconical member 14. And the seat 34 has a land 36 that is sealingly engagable with a plug 38, shown herein as a ball (in FIG. 2 only), runnable thereagainst. Once the plug 38 is sealingly engaged with the seat 34 pressure can be built upstream thereof to perform work such as fracturing an earth formation or actuating a downhole tool, for example, when employed in a hydrocarbon recovery application.
The surface 22 of the sleeve 18 in this embodiment includes protrusions 42 that may be referred to as teeth, configured to bitingly engage with a wall 46 of a structure 50, within which the system 10 is employable, when the surface 22 is in a radially altered (i.e. expanded) configuration. This biting engagement serves to anchor the system 10 to the structure 50 to prevent relative movement therebetween. Although the structure 50 disclosed in this embodiment is a tubular, such as a liner or casing in a borehole, it could just as well be an open hole in an earth formation, for example.
In the embodiment illustrated in the FIGS. 1 and 2 the sleeve 18 includes a plurality of slots 54 that extend fully through walls 58 thereof that are distributed perimetrically about the sleeve 18 as well as longitudinally along the sleeve 18. The slots 54, in this embodiment, are configured such that a longitudinal dimension of each is greater than a dimension perpendicular to the longitudinal dimension. Webs 62 in the walls 58 extend between pairs of longitudinally adjacent slots 54. The foregoing structure permits the sleeve 18 to be radially altered by the frustoconical member 14 with less force than if the slots 54 did not exist. The webs 62 may be configured to rupture during radial alteration of the sleeve 18 to further facilitate radial alteration thereof.
The sleeve 18 also has a recess 66 formed in the walls 58 that are receptive to shoulders 70 on fingers 74 that are attached to the seat 34. Once the seat 34 has moved sufficiently relative to the sleeve 18 that the shoulders 70 are engaged in the recess 66 the seat 34 is prevented from moving in a reverse direction relative to the sleeve 18, thereby maintaining the frustoconical member 14 longitudinally overlapping with the sleeve 18. This overlapping assures that the radial expansion of the sleeve 18 is maintained even after forces that drove the frustoconical member 14 into the sleeve 14 are withdrawn. Additional embodiments are contemplated for maintaining relative position between the frustoconical member 14 and the sleeve 18 once they have become longitudinally overlapped including frictional engagement between the frustoconical member 14 and the sleeve 18, as well as wickers on one or both of the frustoconical member 14 and the sleeve 18 that engage with a surface of the other, for example.
A setting tool 78 (FIG. 1 only) can generate the loads needed to cause movement of the frustoconical member 14 relative to the sleeve 18. The setting tool 78 can have a mandrel 82 with a stop 86 attached to one end 90 by a force failing member 94, also referred to herein as a release member, shown herein as a plurality of shear screws. A plate 98 guidingly movable along the mandrel 82 (by means not shown herein) in a direction toward the stop 86 can longitudinally urge the frustoconical member 14 toward the sleeve 18. Loads to fail the force failing member 94 can be set to only occur after the sleeve 18 has been radially altered by the frustoconical member 14 a selected amount. After failure of the force failing member 94 the stop 86 may separate from the mandrel 82 thereby allowing the mandrel 82 and the plate 98 to be retrieved to surface, for example.
Movement of the frustoconical member 14 relative to the sleeve 18 causes the seal 26 to be longitudinally compressed, in this embodiment, between a shoulder 102, on a collar 103 movable with the frustoconical member 14, and a shoulder 106, on the seat 34. This compression is caused by another shoulder 104 on the collar 103 coming in contact with an end 105 of the frustoconical member 14. This longitudinal compression results in growth in a radial thickness of the seal 26. The frustoconical member 14 being positioned radially inwardly of the seal 26 prevents the seal 26 from reducing in dimension radially. Consequently, the surface 30 of the seal 26 must increase radially. An amount of this increase can be set to cause the surface 30 to contact the walls 46 of the structure 50 (FIG. 2 only) resulting in sealing engagement therewith between. As with the anchoring of the sleeve 18 with the walls 46, the seal 26 is maintained in sealing engagement with the walls 46 by the shoulders 70 of the fingers 74 being engaged with the recess 66 in the sleeve 18.
The tubular anchoring system 10 is configured such that the sleeve 18 is anchored (positionally fixed) to the structure 50 prior to the seal 26 sealingly engaging with the structure 50. This is controlled by the fact that the seal 26 is not longitudinally compressed between the end 105 of the sleeve 18 and the shoulder 102 until a significant portion of the sleeve 18 has been radially expanded over the frustoconical member 14 and into anchoring engagement with the structure 50. Positionally anchoring the tubular anchoring system 10 to the structure 50 prior to engaging the seal 26 with the structure has the advantage of preventing relative movement between the seal 26 and the structure 50 after the seal 26 has radially expanded. This sequence prevents damage to the seal 26 that could result if the seal 26 were allowed to move relative to the structure 50 after having been radially expanded. The land 36 of the seat 34 in this embodiment is positioned longitudinally upstream (as defined by fluid flow that urges the plug 38 against the seat 34) of the sleeve 18. Additionally in this embodiment the land 36 is positioned longitudinally upstream of the seal 26. This relative positioning allows forces generated by pressure against the plug 38 seated against the land 36 to further compress the seal 28 into sealing engagement with the structure 50.
The tubular anchoring system 10 is further configured to leave a through bore 107 with a minimum radial dimension 108 that is large in relation to a radial dimension 109 defined by a largest radial dimension of the system 10 when set within the structure 50. In fact the minimum radial dimension 108 is no less than about 70% of the radial dimension 109. Such a large ratio allows the anchoring system 10 to be deployed as a treatment plug, or a frac plug, for example, in a downhole application. In such an application pressure built against the plug 38 seated at the land 36 can be used to frac a formation that the structure is positioned within. Subsequent the fracing operation production through the through bore 107 could commence, after removal of the plug 38 via dissolution or pumping, for example, without the need of drilling or milling any of the components that define the tubular anchoring system 10.
Referring to FIGS. 3 and 4, an alternate embodiment of a tubular anchoring system disclosed herein is illustrated at 110. Similar to the system 10 the system 110 includes a frustoconical member 114, a sleeve 118 having a surface 122, a seal 126 having a surface 130 and a seat 134. A primary difference between the system 10 and the system 110 is how the extents of radial alteration of the surfaces 22 and 30 are controlled. In the system 10 an extent of radial alteration of the surface 22 is determined by a radial dimension of a frustoconical surface 140 on the frustoconical member 14. And the extent of radial alteration of the surface 30 is determined by an amount of longitudinal compression that the seal 26 undergoes.
In contrast, an amount of radial alteration that the surface 122 of the sleeve 118 undergoes is controlled by how far the frustoconical member 114 is forced into the sleeve 118. A frustoconical surface 144 on the frustoconical member 114 is wedgably engagable with a frustoconical surface 148 on the sleeve 118. As such, the further the frustoconical member 114 is moved relative to the sleeve 118 the greater the radial alteration of the sleeve 118. Similarly, the seal 126 is positioned radially of the frustoconical surface 144 and is longitudinally fixed relative to the sleeve 118 so the further the frustoconical member 114 moves relative to the sleeve 118 and the seal 126 the greater the radial alteration of the seal 126 and the surface 130. The foregoing structure allows an operator to determine the amount of radial alteration of the surfaces 122, 130 after the system 110 is positioned within a structure 150.
Optionally, the system 110 can include a collar 154 positioned radially between the seal 126 and the frustoconical member 114, such that radial dimensions of the collar 154 are also altered by the frustoconical member 114 in response to the movement relative thereto. The collar 154 can have a frustoconical surface 158 complementary to the frustoconical surface 144 such that substantially the full longitudinal extent of the collar 154 is simultaneously radially altered upon movement of the frustoconical member 114. The collar 154 may be made of a material that undergoes plastic deformation to maintain the seal 126 at an altered radial dimension even if the frustoconical surface 144 is later moved out of engagement with the frustoconical surface 158, thereby maintaining the seal 126 in sealing engagement with a wall 162 of the structure 150.
Other aspects of the system 110 are similar to those of the system 10 including, the land 36 on the seat 126 sealably engagable with the plug 38. And the slots 54 and the webs 62 in the walls 58 of the sleeve 118. As well as the recess 66 in the sleeve 118 receptive to shoulders 70 on the fingers 74. Additionally, the system 110 is settable with the setting tool 78 in a similar manner as the system 10 is settable with the setting tool 78.
Referring to FIG. 5 an alternate embodiment of a tubular anchoring system disclosed herein is illustrated at 210. The system 210 includes, a frustoconical member 214 having a first frustoconical portion 216 and a second frustoconical portion 220 that are tapered in opposing longitudinal directions to one another. Slips 224 are radially expandable in response to being moved longitudinally against the first frustoconical portion 216. Similarly, a seal 228 is radially expandable in response to being moved longitudinally against the second frustoconical portion 220. One way of moving the slips 224 and the seal 228 relative to the frustoconical portions 216, 220 is to longitudinally compress the complete assembly with a setting tool that is not shown herein, that could be similar to the setting tool 78. The system 210 also includes a seat 232 with a surface 236 that is tapered in this embodiment and is receptive to a plug (not shown) that can sealingly engage the surface 236.
The tubular anchoring system 210 is configured to seal to a structure 240 such as a liner, casing or open hole in an earth formation borehole, for example, as is employable in hydrocarbon recovery and carbon dioxide sequestration applications. The sealing and anchoring to the structure 240 allows pressure built against a plug seated thereat to build for treatment of the earth formation as is done during fracturing and acid treating, for example. Additionally, the seat 232 is positioned in the system 210 such that pressure applied against a plug seated on the seat 232 urges the seat 232 toward the slips 224 to thereby increase both sealing engagement of the seal 228 with the structure 240 and anchoring engagement of the slips 224 with the structure 240.
The tubular anchoring system 210 can be configured such that the slips 224 are anchored (positionally fixed) to the structure 240 prior to the seal 228 sealingly engaging with the structure 240, or such that the seal 228 is sealingly engaged with the structure 240 prior to the slips 224 anchoring to the structure 240. Controlling which of the seal 228 and the slips 224 engage with the structure first can be through material properties relationships or dimensional relationships between the components involved in the setting of the seal 228 in comparison to the components involved in the setting of the slips 224. Regardless of whether the slips 224 or the seal 228 engages the structure 240 first may be set in response to directions of portions of a setting tool that set the tubular anchoring system 210. Damage to the seal 228 can be minimized by reducing or eliminating relative movement between the seal 228 and the structure 50 after the seal 228 is engaged with the structure 240. In this embodiment, having the seal 228 engage with the structure 240 prior to having the slips 224 engage the structure 240 may achieve this goal. Conversely, in the embodiment of the tubular anchoring system 10, discussed above, having the sleeve 18 engage with the structure 50 before the seal 26 engages with the structure may achieve this goal.
The land 236 of the seat 232 in this embodiment is positioned longitudinally upstream (as defined by fluid flow that urges a plug against the seat 232) of the slips 224. Additionally in this embodiment the land 236 is positioned longitudinally upstream of the seal 228. This relative positioning allows forces generated by pressure against a plug seated against the land 236 to further urge the seal 228 into sealing engagement with the structure 240.
The seat 232 of the embodiment illustrated in the system 210 also includes a collar 244 that is positioned between the seal 228 and the second frustoconical portion 220. The collar 244 illustrated has a wall 248 whose thickness is tapered due to a radially inwardly facing frustoconical surface 252 thereon. The varied thickness of the wall 248 allows for thinner portions to deform more easily than thicker portions. This can be beneficial for at least two reasons. First, the thinner walled portion 249 needs to deform when the collar 244 is moved relative to the second frustoconical portion 220 in order for the seal 228 to be radially expanded into sealing engagement with the structure 240. And second, the thicker walled portion 250 needs to resist deformation due to pressure differential thereacross that is created when pressuring up against a plug seated at the seat 232 during treatment operations, for example. The taper angle of the frustoconical surface 252 may be selected to match a taper angle of the second frustoconical portion 220 to thereby allow the second frustoconical portion 220 to provide radial support to the collar 244 at least in the areas where they are in contact with one another.
Regardless of whether the taper angles match, the portion of the collar 244 that deforms conforms to the second frustoconical portion 220 sufficiently to be radially supported thereby. The taper angles may be in the range of 14 to 20 degrees to facilitate radial expansion of the collar 244 and to allow frictional forces between the collar 244 and the second frustoconical portion 220 to maintain positional relationships therebetween after removal of longitudinal forces that caused the movement therebetween. (The first frustoconical portion 216 may also have taper angles in the range of 14 to 20 degrees for the same reasons that the second frustoconical portion 220 does). Either or both of the frustoconical surface 252 and the second frustoconical portion 220 may include more than one taper angle as is illustrated herein on the second frustoconical portion 220 where a nose 256 has a larger taper angle than the surface 220 has further from the nose 256. Having multiple taper angles can provide operators with greater control over amounts of radial expansion of the collar 244 (and subsequently the seal 228) per unit of longitudinal movement between the collar 244 and the frustoconical member 214. The taper angles, in addition to other variables, also provide additional control over longitudinal forces needed to move the collar 244 relative to the frustoconical member 214. Such control can allow the system 210 to preferentially expand the collar 244 and the seal 228 to set the seal 228 prior to expanding and setting the slips 224. Such a sequence may be desirable since setting the slips 224 before the seal 228 would require the seal 228 to move along the structure 240 after engaging therewith, a condition that could damage the seal 228.
Referring to FIG. 6, another alternate embodiment of a tubular anchoring system disclosed herein is illustrated at 310. The system 310 includes a first frustoconical member 314, slips 318 positioned and configured to be radially expanded into anchoring engagement with a structure 322, illustrated herein as a wellbore in an earth formation 326, in response to be urged against a frustoconical surface 330 of the first frustoconical member 314. A collar 334 is radially expandable into sealing engagement with the structure 322 in response to be urged longitudinally relative to a second frustoconical member 338. And a seat 342 with a surface 346 sealingly receptive to a plug 350 (shown with dashed lines) runnable thereagainst. The seat 342 is displaced in a downstream direction (rightward in FIG. 6) from the collar 334 as defined by fluid that urges the plug 350 against the seat 342. This configuration and position of the surface 346 relative to the collar 334 aids in maintaining the collar 334 in a radially expanded configuration (after having been expanded), by minimizing radial forces on the collar 334 due to pressure differential across the seat 342 when plugged by a plug 350.
To clarify, if the surface 346 were positioned in a direction upstream of even a portion of the longitudinal extend of the collar 334 (which it is not) then pressure built across the plug 350 seated against the surface 346 would generate a pressure differential radially across the portion of the collar 334 positioned in a direction downstream of the surface 346. This pressure differential would be defined by a greater pressure radially outwardly of the collar 334 than radially inwardly of the collar 334, thereby creating radially inwardly forces on the collar 334. These radially inwardly forces, if large enough, could cause the collar 334 to deform radially inwardly potentially compromising the sealing integrity between the collar 334 and the structure 322 in the process. This condition is specifically avoided by the positioning of the surface 346 relative to the collar 334 of the instant invention.
Optionally, the tubular anchoring system 310 includes a seal 354 positioned radially of the collar 334 configured to facilitate sealing of the collar 334 to the structure 322 by being compressed radially therebetween when the collar 334 is radially expanded. The seal 354 may be fabricated of a polymer to enhance sealing of the seal 354 to both the collar 334 and the structure 322.
Referring to FIGS. 7 through 9, an embodiment of a tool setting arrangement disclosed herein is illustrated at 410. The arrangement 410 includes a tool 414 disposed on a mandrel 418 that is runnable within a structure 422 (FIG. 8 only), illustrated herein as a casing or drill string in a borehole in an earth formation such as a wellbore. The tool 414 in this embodiment is a treatment plug or frac plug that has slips 426 that move radially outwardly upon axial movement against a cone 430. The cone 430 includes the surface 346 that is sealingly engagable with the plug 350 (note: while the surface 346 is shown in FIGS. 6, 7 and 8, the plug 350 is only shown in FIG. 6) for use during treating or fracing operations, for example. The slips 426 are configured to bite into the structure 422 at a selected setting load to anchor the tool 414 to the structure 422. The tool 414 of this embodiment also has a seal 434 configured to radially expand to sealingly engage the structure 422 at loads less than the setting load. Axial loads are applied to a portion 438 of the slips 426 by a feature 442 of the mandrel 418. The portion 438 in this embodiment is a fin that protrudes radially inwardly from a balance of the slips 426, while the feature 442 is a pin that spans a slot 446 oriented substantially parallel to an axis of the mandrel 418. One or both of the portion 438 and the feature 442 are configured to release when a selected release load between the portion 438 and the feature 442 is reached. Upon such release the mandrel 18 disengages from the tool 414 and is free to be withdrawn from the tool 414 thereby leaving the tool 414 sealably anchored to the structure 422.
Referring to FIG. 9, depending upon the specific configuration of the portion 438 and the feature 442, release of the portion 438 or the feature 442 can be reversible. In the embodiment illustrated, however, the release is not reversible as one or both of the portion 438 and the feature 442 are sheared at the release load. Design parameters of the portion 438 and the feature 442 can be adjusted to control loads at which each is releasable. If the feature 442 releases at the release load then the features 442 are sheared and the portion 438 is left intact. The embodiment includes six of the slips 426 with each of the slips 426 having one of the portions 438. As such after release the six portions 438 remain intact thereby jointly forming a seat 450 having a radial dimension capable of catching a runnable member (not shown) such as a ball for example.
Alternately, an operator can selectively have the portions 438 release at the release load thereby leaving the features 442 intact. In such an embodiment the portions 438 are sheared off at a radial dimension at least equal to the outer radial dimension defined by the features 442. In this scenario the tool 414 can be configured to leave no radial dimension smaller than an inner radial surface 454 (FIGS. 7 and 8) of the cone 430 that defines a smallest radial dimension of the cone 430 and of the balance of the tool 414. Such a configuration may be desirable to allow for intervention therethrough while minimizing radial restrictions.
Referring to FIG. 10, an alternate embodiment of a tool setting arrangement disclosed herein is illustrated at 510. The arrangement 510 is similar to the arrangement 410 in many ways and elements common to both arrangements 410, 510 are identified with the same reference character and are not described again hereunder. The arrangement 510 includes a tool 514 disposed on a mandrel 518 that is runnable within a structure. The tool 514 in this embodiment is a treatment plug that has slips 526 that move radially outwardly upon axial movement against the cone 430. A portion 538 of the slips 526 have a ring 532 with release members 536, shown herein as pins or shear screws. The release members 536 protrude radially inwardly from the ring 532 that is positioned within a recess 540 of the slips 526 and engage with a feature 542 of the mandrel 518 that is a shoulder in this embodiment. The release members 536 shear at the release load thereby allowing the mandrel 518 to be withdrawn from the tool 514 leaving a minimum radial dimension through the tool 514 that is no smaller than that of the cone 430. Additionally, the ring 532 is maintained in the recess 540 of the slips 526 after removal of the mandrel 518. As such, by retaining a first portion 544 of the release members 536 in the ring 532 and a second portion 548 of the release members 536 in the feature 542, in this embodiment, no pieces of debris are generated during release that is not physically retained by the tool 514 or the mandrel 518.
The release members 536 can be retained by the tool 514 and the mandrel 518 in different ways. One way is to have the release members threadably engaged into the mandrel 518 through radial holes 552 formed in the ring and radially holes 556 formed in the slips 526. Set screws 560 could then hold the portions 548 to the ring 532 after release of the release members 536. Another way is to have portion 544 of the release members 536 threadably engaged to the ring 532 and have the portion 548 retained to the mandrel 518 by set screws 564. Alternate methods could also be employed to assure that the portions 544, 548 of the release members 536 are retained in at least one of the ring 532 and the mandrel 518.
While the invention has been described with reference to an exemplary embodiment or embodiments, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this invention, but that the invention will include all embodiments falling within the scope of the claims. Also, in the drawings and the description, there have been disclosed exemplary embodiments of the invention and, although specific terms may have been employed, they are unless otherwise stated used in a generic and descriptive sense only and not for purposes of limitation, the scope of the invention therefore not being so limited. Moreover, the use of the terms first, second, etc. do not denote any order or importance, but rather the terms first, second, etc. are used to distinguish one element from another. Furthermore, the use of the terms a, an, etc. do not denote a limitation of quantity, but rather denote the presence of at least one of the referenced item.

## Claims

1. A tool setting arrangement comprising:
a mandrel; and a tool positionable at the mandrel comprising:
a cone having a surface sealingly receptive to a plug run thereagainst;
and at least one slip in operable communication with the cone configured to radially expand to set the tool when moved relative to the cone with at least a setting load, the at least one slip having a fin configured to engage with a pin of the mandrel such that movement of the mandrel relative to the cone causes the at least one slip to move relative to the cone, at least one of the fin and the pin being configured to release at a release load to disengage the mandrel from the tool, the release load being greater than the setting load and wherein the at least one slip is a plurality of slips and the fins of each of the plurality of slips form a seat receptive to a runnable member after the mandrel has been disengaged from the tool.

2. The tool setting arrangement of claim 1, wherein mandrel and the tool are runnable within a structure and are settable to the structure.

3. The tool setting arrangement of claim 2, wherein the at least one slip anchors the tool to the structure when the tool is set.

4. The tool setting arrangement of claim 2, wherein the tool further includes a seal sealably engagable with the structure.

5. The tool setting arrangement of claim 4, wherein the seal radially expands into sealing engagement with the structure during setting of the tool.

6. The tool setting arrangement of claim 4, wherein the tool remains anchored to the structure after having been set and after the mandrel has been disengaged from the tool.

7. The tool setting arrangement of claim 4, wherein the tool remains sealed to the structure after having been set and after the mandrel has been disengaged from the tool.

8. The tool setting arrangement of claim 1, wherein one of the portion and the feature is sheared at the release load.

9. The tool setting arrangement of claim 1, wherein the seat defines a smallest radial dimension of the tool.

10. The tool setting arrangement of claim 1, wherein the tool provides radial clearance therethrough that is radially no smaller than a smallest radial dimension of the cone after the mandrel has disengaged from the tool.

11. The tool setting arrangement of claim 1, wherein no pieces of debris are generated during the release that are not physically retained by the tool or the mandrel.

12. A tool setting arrangement comprising:
a mandrel; and a tool positionable at the mandrel, the mandrel and the tool being runnable within a structure and settable to the structure, the tool including a seal radially expandable into sealing engagement with the structure during setting of the tool and wherein a load to sealingly engage the seal with the structure is less than the setting load comprising:
a cone having a surface sealingly receptive to a plug run thereagainst;
and at least one slip in operable communication with the cone configured to radially expand to set the tool when moved relative to the cone with at least a setting load, the at least one slip having a portion configured to engage with a feature of the mandrel such that movement of the mandrel relative to the cone causes the at least one slip to move relative to the cone, at least one of the portion and the feature being configured to release at a release load to disengage the mandrel from the tool, the release load being greater than the setting load.

13. A method of setting a tool as claimed in claim 12 within a structure comprising: running the tool disposed at the mandrel within a structure; loading the portion of the at least one slip of the tool with the feature of the mandrel;
moving the at least one slip relative to the cone;
anchoring the tool with the setting load applied between the portion and the feature;
releasing at least one of the portion and the feature with the release load applied between the portion and the feature;
disengaging the mandrel from the tool;
running a plug; and
sealing the plug against a surface on the cone.

14. The method of setting a tool within a structure of claim 13, further comprising shearing at least one of the portion and the feature.

15. The method of setting a tool within a structure of claim 14, further comprising retaining any pieces of the portion and the feature generated during the releasing with the tool or the mandrel.

16. The method of setting a tool within a structure of claim 13, further comprising defining a seating surface by the portion of the at least one slip engagable with a runnable member after disengaging the mandrel from the tool.

17. The method of setting a tool within a structure of claim 13, further comprising leaving a bore through the tool after disengagement of the mandrel from the tool that radially no smaller than a smallest radial dimension of the cone.