1. Field of the Invention
The invention relates generally to the field of oil and gas production. More specifically, the present invention relates to a perforating system. Yet more specifically, the present invention relates to a perforating gun system capable of regulating wellbore fluid dynamics.
2. Description of Related Art
Perforating systems are used for the purpose, among others, of making hydraulic communication passages, called perforations, in wellbores drilled through earth formations so that predetermined zones of the earth formations can be hydraulically connected to the wellbore. Perforations are needed because wellbores are typically completed by coaxially inserting a pipe or casing into the wellbore. The casing is retained in the wellbore by pumping cement into the annular space between the wellbore and the casing. The cemented casing is provided in the wellbore for the specific purpose of hydraulically isolating from each other the various earth formations penetrated by the wellbore.
Perforating systems typically comprise one or more perforating guns strung together, these strings of guns can sometimes surpass a thousand feet of perforating length. In
Included with the perforating gun 6 are shaped charges 8 that typically include a housing, a liner, and a quantity of high explosive inserted between the liner and the housing. When the high explosive is detonated, the force of the detonation collapses the liner and ejects it from one end of the charge 8 at very high velocity in a pattern called a “jet” 12. The jet 12 perforates the casing and the cement and creates a perforation 10 that extends into the surrounding formation 2.
As shown in
The present disclosure discloses examples of a perforating system and a method of perforating. In an example embodiment a perforating system is made up of a perforating string with first and second spaced apart perforating guns. Shaped charges are provided in both guns and a zonal isolation system is included for regulating pressure in a wellbore. The zonal isolation system of this embodiment has axially spaced apart plates that project radially out from the perforating string. The plates define an annulus between the string and a borehole wall, where the annulus restricts fluid flow to cause a pressure drop in the fluid flowing across the plates and along the annular space between the perforating string and wall of the wellbore. This lowers pressure in a fluid flowing from a higher pressure producing zone so that it does not flow into a lower pressure producing zone. In an example embodiment, passages are formed through the plates. Optionally, the diameters of the plates can vary. The zonal isolation system may be disposed on one of the first or second perforating guns. In an example embodiment, the zonal isolation system is disposed between the first and second perforating guns. A sub may optionally be included that connects between the first and second perforating guns. In this example the zonal isolation system is disposed on the sub. In an example embodiment, the zonal isolation system is a first zonal isolation system, and a second zonal isolation system is included with the system.
Also disclosed herein is an alternate perforating system that has a perforating string with shaped charges. The perforating string has a stack of axially spaced apart plates projecting radially outward therefrom that define a restricted flow area between a portion of the perforating string and a wellbore wall. As such, when shaped charges in the perforating string are detonated and perforate formation zones adjacent the wellbore, if the formation zones are at different pressures, fluid communication between the respective formations is impeded by the plates. In an example embodiment, the perforating string includes perforating guns stacked end to end. Optionally, the plates direct fluid from one of the formations along a labyrinthine path for reducing pressure in the fluid. Passages may optionally be included that are formed axially through the plates. Further, the passages in adjacent plates may be offset from one another. Yet further optionally, the diameters of the plates can vary.
A method is described herein for dynamically isolating flow within a wellbore between a first subterranean formation zone and a second subterranean formation zone, where the zones are at different pressures. In an example the method includes inserting a downhole tool in a wellbore, where the downhole tool includes a pressure isolation system that has axially spaced apart plates that extend radially outward from an outer surface of the downhole tool. A restricted flow annulus is defined between the member and the wellbore. Connate fluid flow is induced from within the first and second subterranean formation zones and a dynamic pressure drop is created between the first and second subterranean formation zones by locating the restricted flow annulus between the first and second subterranean formation zones. Directing connate fluid from the higher pressure formation across the restricted flow annulus reduces pressure in the fluid to prevent the fluid from flowing into the lower pressure formation zone. In an example embodiment, the plates are configured to form a labyrinthine path for connate fluid flow along the downhole tool. Alternatively, the labyrinthine path is formed by providing passages through the plates and positioning the passages in each plate to be axially offset from passages in an adjacent plate. Yet further alternatively, the labyrinthine path is formed by varying the diameter of plates that are adjacent.
Some of the features and benefits of the present invention having been stated, others will become apparent as the description proceeds when taken in conjunction with the accompanying drawings, in which:
While the invention will be described in connection with the preferred embodiments, it will be understood that it is not intended to limit the invention to that embodiment. On the contrary, it is intended to cover all alternatives, modifications, and equivalents, as may be included within the spirit and scope of the invention as defined by the appended claims.
The method and system of the present disclosure will now be described more fully hereinafter with reference to the accompanying drawings in which embodiments are shown. The method and system of the present disclosure may be in many different forms and should not be construed as limited to the illustrated embodiments set forth herein; rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey its scope to those skilled in the art. Like numbers refer to like elements throughout.
It is to be further understood that the scope of the present disclosure is not limited to the exact details of construction, operation, exact materials, or embodiments shown and described, as modifications and equivalents will be apparent to one skilled in the art. In the drawings and specification, there have been disclosed illustrative embodiments and, although specific terms are employed, they are used in a generic and descriptive sense only and not for the purpose of limitation. Accordingly, the improvements herein described are therefore to be limited only by the scope of the appended claims.
With reference now to
An auger flight 28 is provided along the outer circumference of the perforating string 20. The auger flight 28 is a generally helical member that winds along on the outer circumference of the perforating string 20 along a portion of its length. As shown, the auger flight 28 is disposed primarily along the accumulator section 26 of the perforating string 20. Optionally the auger flight 28 may extend also along one or more of the perforating sections 22, 23 in addition to being along the accumulator section 26. It should be pointed out that the cross section of the auger flight 28 may take one of many different configurations. Typically the base of the auger flight 28 has a wider cross section where it attaches to the perforating string 20 and tapers to a narrower cross section at its outer edge. Other embodiments of the auger flight 28 include a shape where the base and the terminating end have substantially the same thickness with no tapering. However it is well within the scope of those skilled in the art to determine and produce an auger flight suitable for use.
A port 30 is provided on the accumulator section 26 that may be selectively opened or closed. When open, the port 30 provides fluid communication across the side walls of the perforating string 20. Optionally, a reservoir 30 (shown in dashed lines) can be provided within the perforating string 20 and in communication with the port 30. Opening/closing of the port 30 may selectively communicate fluid between the reservoir 30 and outside of the perforating string 20. The reservoir 32 can be disposed solely within the accumulator section 26 or one of the perforation sections 22, 23.
In one non-limiting example of operation, a perforating system 4 having an embodiment of the perforating string 20 herein described is lowered within a wellbore 1 to a predetermined depth wherein perforating operations are to be performed. Initiating detonation of shaped charges 24 shown provided with the perforating system 4 creates perforations 10 in the corresponding formation 2. As previously discussed, in an under-balanced situation, fluid in the higher pressure formation 2 will flow into the lower pressure wellbore 1 through the perforations 10. The ports 30 can be opened, simultaneously with initiation of the shape charges 24 or soon thereafter, so the reservoir 32 can act as a potential sink or accumulator for at least a portion of the formation fluid flowing into the wellbore 1 from the formation 2. The fluid flowing into the reservoir 32 is not limited to wellbore fluid but can also include all flowable matter resident in the wellbore 1, such as drilling mud, drilling fluid, as well as the producing fluid from the formation 2. Accordingly having the accumulator section 26 within the wellbore 1 after perforating provides an open space to absorb potential kinetic energy resulting from the pressure imbalance between the formation 2 and the wellbore 1.
Pressure imbalances between the formation 2 and the wellbore 1 may result from changes in the density of fluid in the wellbore, or by perforating into a formation 2 having a higher pressure than the wellbore 1. Flow into the wellbore 1 from the formation 2 may be induced by perforating into a formation 2 as well as introducing an accumulator within a wellbore 1 having wellbore fluid, wherein the confines of the accumulator are at a lower pressure than the wellbore fluid. Providing fluid communication between the confines of the accumulator and the wellbore 1 can also induce connate fluid flow from the formation 2 into the wellbore 1. As discussed in more detail below, the accumulator in combination with the auger flights can isolate the pressure of one subterranean zone from another.
With reference now to
The scope of the present disclosure is not limited to perforating systems, but as shown in
Optionally the present device may further allow pressure isolation between various subterranean zones Z1, Z2, Z3. For example, as shown in
Referring now to
Embodiments of the plates 81 of
Shown in a side perspective view in
The embodiments described herein, therefore, are well adapted to carry out the objects and attain the ends and advantages mentioned, as well as others inherent therein. While a presently preferred embodiment of an invention has been given for purposes of disclosure, numerous changes exist in the details of procedures for accomplishing the desired results. For example, instead of an auger flight extending partially between the outer surface of a downhole tool and the inner surface of a casing, other flow path restriction members may be employed. Examples of such members include coaxially disposed plates, plates having orifices therethrough, a partially extended packer, as well as any other member for retarding flow across the length of the tool. Further, the downhole conveyance means used for disposing the above described devices includes casing and drill pipe. These and other similar modifications will readily suggest themselves to those skilled in the art, and are intended to be encompassed within the spirit of the present invention disclosed herein and the scope of the appended claims.
This application is a continuation-in-part of and claims priority to and the benefit of co-pending U.S. application Ser. No. 11/602,107, filed November 20th, 2006, the full disclosure of which is hereby incorporated by reference herein in its entirety for all purposes.
Number | Date | Country | |
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Parent | 11602107 | Nov 2006 | US |
Child | 13159946 | US |