1. Field of Invention
The present invention relates to the field of cutting tools, particularly to a device and method to cut a control line downhole in a well.
2. Related Art
With the advent of intelligent completions, running multiple control lines downhole along completions equipment is common practice. Unfortunate occurrences sometimes require cutting the downhole tubing to retrieve the completion equipment. In those cases, the control lines can complicate the retrieval operations if the control lines are pulled apart above the tubing cut. Ideally, the control lines are cut below the tubing cut to recover as much of the control lines as possible and leave a clean “fish” downhole.
Prior systems use a “splice sub” in which the control lines are anchored above and below the tubing cutting target length. A tubing cutter such as an Explosive Jet Cutter (EJC) is run to target depth and detonated to cut the tubing. Excess impact from the EJC at least partially cuts the control lines. When the tubing is removed, the control lines, if not completed severed, break at the damaged area, leaving the remaining control line portions in the vicinity of the remaining tubing. The remaining tubing is more easily “fished” if it is clear of control line remnants.
The present invention provides for a cutting device and associated method to cut one or more downhole control lines such that the cut ends of the control lines will not interfere with subsequent fishing operations.
Referring to
In
Sleeve 14 is carried on the lower end of mandrel 12 and can move in both rotation and translation relative to mandrel 12 and base 22. The relative motion provides a cutting action. Base 22 and sleeve 14 have mating helical surfaces 28 and each has a longitudinal passageway through its respective sidewall to accommodate control line 19. Those passageways are initially aligned. Axial holes 31 in mandrel 12 and axial holes 33 in base 22 of
Lugs 18 are carried in slots 26 of sleeve 14 and placed in sliding engagement with the lower end of mandrel 12. Lugs 18 extend into a groove 29 in the inner surface of housing 16, linking sleeve 14 to housing 16 while permitting sleeve 14 to rotate relative to housing 16. A recess 35 in mandrel 12 allows lugs 18 to disengage from housing 16 upon sufficient displacement of sleeve 14.
In operation, a tubing cutter 34 such as an explosive jet cutter is placed in the vicinity of tubing cutting target 20. The cutter 34 is actuated to sever mandrel 12 somewhere along the length of target 20. Once mandrel 12 is severed, the upper portion of tubing 24 is pulled upward by the operator. Because housing 16 is attached to the upper portion of tubing 24, housing 16 is pulled upward as well. Since lugs 18 extend into groove 29 of housing 16, sleeve 14 is also pulled upward. Thus, housing 16 provides a mechanical link between the upper portion of tubing 24 (that has now been severed from the lower portion of tubing 24) and cutting sleeve 14 to generate the relative motion required for cutting control line 19.
Helical surfaces 28 between sleeve 14 and cutting base 22 cause sleeve 14 to rotate relative to base 22 when sleeve 14 is pulled upward. The rotational motion advances the cutting edge of sleeve 14 through control line 19, thereby cutting control line 19. With sufficient upward travel of cutting sleeve 14, lugs 18 encounter and retract into recess 35 in mandrel 12 to release housing 16.
Once housing 16 is released, the upper portion of tubing 24, along with housing 16 and the upper portion of (severed) mandrel 12 can all be removed from the well. The newly cut end of the upper portion of control line 19 is enclosed inside housing 16 during retrieval. The severed end of the lower portion of control line 19 left in the well is enclosed inside sleeve 14. The lower portion of tubing 24 remains in the well and the uppermost end of the severed lower portion of mandrel 12 is clear of control lines 19. Preferably the severed end of mandrel 12 is beveled to allow for easy overshoot. Additionally, the outside diameter of sleeve 14 is preferably small enough to be swallowed up (i.e., enclosed and captured), for example, by a burner mill. This allows for removal of the remaining portion of the completion assembly from the well.
Although only a few exemplary embodiments of this invention have been described in detail above, those skilled in the art will readily appreciate that many modifications are possible in the exemplary embodiments without materially departing from the novel teachings and advantages of this invention. Accordingly, all such modifications are intended to be included within the scope of this invention as defined in the following claims. In the claims, means-plus-function clauses are intended to cover the structures described herein as performing the recited function and not only structural equivalents, but also equivalent structures. Thus, although a nail and a screw may not be structural equivalents in that a nail employs a cylindrical surface to secure wooden parts together, whereas a screw employs a helical surface, in the environment of fastening wooden parts, a nail and a screw may be equivalent structures. It is the express intention of the applicant not to invoke 35 U.S.C. §112, paragraph 6 for any limitations of any of the claims herein, except for those in which the claim expressly uses the words “means for” together with an associated function.
This application claims the benefit of U.S. Provisional Application No. 60/486,834, filed Jul. 11, 2003.
Number | Name | Date | Kind |
---|---|---|---|
3926252 | Ribeyre et al. | Dec 1975 | A |
4160478 | Calhoun et al. | Jul 1979 | A |
4306622 | Armstrong | Dec 1981 | A |
4427059 | Olivier | Jan 1984 | A |
4825953 | Wong et al. | May 1989 | A |
4886115 | Leggett et al. | Dec 1989 | A |
5575331 | Terrell | Nov 1996 | A |
5720348 | Hisaw | Feb 1998 | A |
6116344 | Longbottom et al. | Sep 2000 | A |
6135206 | Gano et al. | Oct 2000 | A |
6789627 | Leismer | Sep 2004 | B1 |
6805197 | Brumley et al. | Oct 2004 | B1 |
20040251027 | Sonnier et al. | Dec 2004 | A1 |
20050006102 | Cho | Jan 2005 | A1 |
Number | Date | Country | |
---|---|---|---|
20050006102 A1 | Jan 2005 | US |
Number | Date | Country | |
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60486834 | Jul 2003 | US |