US20060278393A1

US20060278393A1 - Method and apparatus for completing lateral channels from an existing oil or gas well

Info

Publication number: US20060278393A1
Application number: US11/507,145
Authority: US
Inventors: John Hunt; Henry Mazorow
Original assignee: Horizontal Expansion Tech LLC
Current assignee: Horizontal Expansion Tech LLC
Priority date: 2004-05-06
Filing date: 2006-08-21
Publication date: 2006-12-14

Abstract

A method and apparatus for completing a lateral channel from an existing oil or gas well includes a well perforating tool for perforating a well casing at a preselected depth, and a lateral alignment tool for directing a flexible hose and blaster nozzle through a previously made perforation in the casing to complete the lateral channel. The disclosed apparatus also is effective to provide an expanded groove within the earth strata beyond the well casing. The apparatus eliminates the need to maintain the precise alignment of a downhole “shoe” in order to direct the flexible hose and blaster nozzle through a previously made perforation through the well casing.

Description

CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a continuation-in-part of U.S. application Ser. No. 11/121,622 filed May 4, 2005, which claims the benefit of U.S. Provisional Application No. 60/568,492 filed May 6, 2004, and U.S. Provisional Application No. 60/573,013 filed May 20, 2004, the disclosures of all of which are incorporated herein by reference.

BACKGROUND OF THE INVENTION

1. Field of the Invention
The invention relates to methods and apparatus for completing lateral channels from existing oil or gas wells. More particularly, it relates to improved methods and apparatus for penetrating the well casing of an existing well at a given depth, and completing one or more laterals at that depth.
2. Description of Related Art
Oil and gas are produced from wells drilled from the earth surface into a hydrocarbon “payzone.” Once a well is drilled, it essentially is a hole in the earth extending from the earth surface downward several hundred or thousand feet into or adjacent a hydrocarbon payzone. The thus drilled hole generally is not very stable because, among other things, its earthen walls are highly subject to erosion or shifting over time, whether due to the flow of hydrocarbons to the surface, or other natural causes such as water erosion from rain or flooding. This is especially of concern considering many oil and gas wells stay online for several or tens of years, or longer.
To impart stability to a drilled well, it is conventional to encase the well bore with a casing material, typically made from steel. The steel well casing essentially is a cylindrical-walled pipe having an OD somewhat smaller than the ID of the well bore drilled from the earth surface. The well casing is placed down in the well bore, typically in discrete sections which are secured or otherwise joined together as is known in the art. Once the well casing is in place centrally within the earthen well bore, it is conventional to fill in the thus-defined annular space between the well casing and the well bore with cement.
The resulting construction is an oil or gas well consisting of a cement-encased steel pipe extending from the earth surface down into a hydrocarbon payzone from which hydrocarbons (oil and/or gas) can be extracted and delivered to the surface via conventional techniques. This steel pipe, also called the well casing, defines an inner bore or passageway for the delivery of hydrocarbons to the surface. The described construction has proven useful for decades to produce oil or gas from hydrocarbon payzones located at, or which empty into, the base (bottom end) of the well casing. However, once these payzones dry up, either the well must be abandoned or it must be treated in order to make it productive and profitable once again.
There are several conventional treatment techniques for revitalizing an otherwise unproductive well. Two of the most common are referred to as acidizing and fracturizing. Both of these techniques are designed to increase the adjacent formation's porosity by producing channels in the formation allowing hydrocarbons to flow more easily into the perforated well bore, thereby increasing the well's production and its value. However, the success of these operations is highly speculative and both are very expensive and require dedicated heavy equipment and a large crew.
A more efficient technique for stimulating a diminished production well is to drill a hole through the well casing at a depth below the earth surface, and then to bore a lateral channel through the predrilled hole into an adjacent payzone using a high pressure water jet nozzle (blaster nozzle). Various techniques and apparatus for boring lateral channels downhole are known in the art, for example as described in U.S. Pat. Nos. 6,530,439, 6,578,636, 6,668,948, and 6,263,984, the contents of all of which are incorporated herein by reference. Generally, an elbow or “shoe” is used downhole to redirect a cutting tool fed from the surface along a radial or lateral path at a depth at which a lateral channel is to be completed. The cutting tool is directed laterally against the well casing to cut or drill a small hole through the casing and the cement encasement beyond, and is then withdrawn to make way for a separate blaster nozzle and associated high pressure water hose that must be snaked through the previously drilled hole. This technique, which is simple to describe, in practice can be difficult to perform, with uncertain or irreproducible results.
For one thing, often it is difficult and sometimes even impossible to determine with certainty that a hole actually has been cut through the casing and the cement encasement. Also, even assuming a successfully cut hole, it can be extremely difficult to ensure accurate alignment of the elbow or downhole shoe in order to direct the blaster nozzle through the previously cut hole. For example, the shoe may be jerked or moved during withdrawal of the cutting tool or insertion of the blaster nozzle. In addition, it is extraordinarily difficult, if not impossible in most cases to realign the shoe with a previously cut hole if the shoe alignment is accidentally shifted, or if it must be shifted (e.g. to drill another hole) subsequent to drilling the hole in the casing but prior to feeding the blaster nozzle through the hole. Often it is impossible to know at the surface if the alignment of the shoe with the previously drilled hole has been disturbed and needs readjustment.
There is a need in the art for a method of perforating the well casing (and annular cement encasement) at depth within an existing oil or gas well, wherein the precise alignment of a downhole tool need not be exactly maintained to ensure a subsequently introduced boring tool, such as a high pressure blaster nozzle, can be directed through the previously made perforation to bore a lateral channel or channels therefrom.

SUMMARY OF THE INVENTION

A well perforating tool is provided. The tool has a substantially cylindrical body having a proximal end and a distal end and defining a circumferential wall of the perforating tool. The perforating tool has a longitudinal axis and includes an axial blind bore open to the proximal end of the perforating tool, which defines an axial flow passage within the perforating tool. A hole is provided through the distal end of the tool. This hole has a lateral dimensions smaller than the diameter of the blind bore. At least one lateral port is located in the circumferential wall of the perforating tool. The lateral port provides fluid communication between the axial flow passage and a position exterior of the perforating tool. The lateral port is adapted to accommodate a jet of high pressure cutting fluid for perforating a well casing.
An apparatus is provided, which includes a lateral channel alignment tool having a substantially elongate basic body having a longitudinal axis, a lateral alignment member pivotally attached to the basic body, and a biasing mechanism effective to bias the lateral alignment member in an angled or laterally engaged position relative to the basic body. The basic body has a longitudinal passage therethrough that is radially offset relative to the longitudinal axis of the basic body and adapted to accommodate a hose therein. The lateral alignment member includes a first portion that extends generally lengthwise, a terminal portion that extends at an angle relative to the lengthwise direction of the first portion, and an elbow-shaped passage provided within the lateral alignment member. The elbow-shaped passage extends through the respective first and terminal portions of the lateral alignment member from an entrance located in the first portion to an exit located in the terminal portion. The entrance of the elbow-shaped passage is located adjacent a distal end of the longitudinal passage in the basic body and is adapted to receive a blaster nozzle and associated hose therefrom. A hose is received within both the longitudinal passage and the elbow-shaped passage. The hose includes a first hose section, a second hose section, and a thruster coupling including a thruster port, wherein the first hose section and the second hose section are operatively connected by the thruster coupling. The thruster port is actuable based on fluid pressure in the hose.
A method of completing a lateral channel from an existing oil or gas well having a well casing is also provided. The method includes the steps of: providing a well perforating tool having a substantially elongate body defining a circumferential wall of the perforating tool, the perforating tool having a longitudinal axis and an axial blind bore open to a proximal end of the perforating tool, wherein the blind bore defines an axial flow passage within the perforating tool, at least one lateral port being located in the circumferential wall of the perforating tool, the lateral port providing fluid communication between the axial flow passage and a position exterior of the perforating tool; suspending the well perforating tool at a selected depth in the existing well; and pumping a fluid at high pressure through the axial flow passage such that a jet of said high pressure fluid shoots out from the lateral port, wherein the jet perforates the well casing and cuts away a portion of earth strata beyond the well casing.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 a is a side view of a well perforating tool;
FIG. 1 b is a side view of a further embodiment of a well perforating tool;
FIG. 2 is an end view of the well perforating tool of FIG. 1 a;
FIG. 3 a is a side perspective view of the well perforating tool of FIG. 1 a;
FIG. 3 b is a side perspective view of the well perforating tool of FIG. 1 b;
FIG. 4 a is a side view of a lateral channel alignment tool, with the lateral alignment member pivoted in an extended position;
FIG. 4 b is a side view as in FIG. 4 a, but with the lateral alignment member pivoted in a laterally engaged position;
FIG. 5 is a front perspective view of the lateral channel alignment tool of FIG. 4;
FIG. 6 is a schematic view showing the well perforating tool of FIG. 1 a lowered into the well casing of an existing oil or gas well at an early stage of a well perforating operation.
FIG. 7 is a schematic view as in FIG. 6, but at a later stage of the well perforating operation;
FIG. 7 a is a schematic view showing the same stage of the boring operation as FIG. 7, but according to a further preferred embodiment where the well perforating tool is operated to cut a circular groove in the earth strata beyond the well casing, in addition to perforating the well casing and the cement encasement surrounding the well.
FIG. 8 is a schematic view showing the lateral channel alignment tool of FIG. 4 lowered into the well casing of an existing well after a well perforating operation, shown at an early stage of a lateral channel boring operation;
FIG. 9 is a schematic view as in FIG. 8, but at a later stage of the lateral channel boring operation;
FIG. 9 a is a schematic view showing the same stage of the boring operation as FIG. 9, but according to the embodiment illustrated in FIG. 7 a where a circular groove is cut in the earth strata during the well perforating operation;
FIG. 9 b is a schematic view as in FIG. 9 a, except illustrating a further embodiment wherein an extensible hose guide member 260 is used;
FIG. 10 is a schematic view as in FIG. 9 but at a still later stage of the lateral channel boring operation;
FIG. 11 is a side view of a thruster coupling according to an aspect the invention;
FIG. 12 is a cross-sectional view of the thruster coupling taken along line 12-12 in FIG. 11;
FIG. 13 is a longitudinal cross-sectional view of the thruster coupling taken along line 13-13 in FIG. 12;
FIG. 14 is a perspective view of a flexible hose having thruster couplings;
FIG. 15 a is a perspective view of a blaster nozzle;
FIG. 15 b is an alternate perspective view of a blaster nozzle;
FIG. 16 is a perspective view of a flexible hose having thruster ports provided directly in the sidewall according to an embodiment of the invention;
FIG. 17 is a side view of a thruster coupling having adjustable thruster ports according to an embodiment of the invention;
FIG. 17 a is a side view as in FIG. 17, schematically illustrating an embodiment wherein pressure-relief or check valves are provided in the thruster ports, which have a characteristic cracking pressure and will permit the flow of cutting fluid therethrough once the fluid pressure within the hose has reached or exceeded each respective valve's cracking pressure.
FIG. 18 is a cross-sectional view of the thruster coupling taken along line 18-18 in FIG. 17;
FIG. 19 is a close-up view of an adjustable thruster port indicated at broken circle 19 in FIG. 17;
FIG. 20 is a side view of a lateral channel alignment tool similar to that shown in FIG. 4 a, except that it includes an extensible hose guide member located at the distal end of the terminal portion 206 of the lateral channel alignment tool 200; and
FIG. 21 is a close-up perspective view of the hose guide member shown in FIG. 20.

DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS OF INVENTION

As used herein, when a range such as 5 to 25 (or 5-25) is given, this means preferably at least 5 and, separately and independently, preferably not more than 25. Also as used herein, when referring to a tool used downhole in a well, such as the perforating tool 100, the lateral channel alignment tool 200, or the flexible hose assembly 10 described below, the proximal end of the tool is the end nearest the earth surface when being used, and the distal end of the tool is the end farthest from the earth surface when being used; i.e. the distal end is the end inserted first into the well. Also as used herein, a bore (such as a through bore or a blind bore) need not be made, necessarily, by drilling. It can be formed by any suitable method or means for the removal of material, for example, by drilling or cutting, or by casting or molding an object to have a bore.
Referring to FIGS. 1-5, a well perforating tool 100 (FIGS. 1-3) and a lateral channel alignment tool 200 (FIGS. 4-5) are provided. When used together according to methods described herein, these tools are useful to reproducibly complete lateral channels from an existing oil or gas well at a desired depth, without having to maintain the precise alignment of any downhole equipment between a well perforating operation and a subsequent lateral channel boring operation. First the structure of each of these tools is described. Following is a description of methods for completing lateral channels from an existing well, for example using a flexible hose assembly as described herein.
Referring first to FIGS. 1-3, the well perforating tool 100 has a substantially cylindrical body having a longitudinal axis 101, preferably made from steel or stainless steel, most preferably from 4140 steel. The perforating tool 100 has an axial blind bore 110 open to, preferably drilled from, the proximal end 107 of the tool 100, preferably extending substantially the entire length of the tool 100, but not through the distal end 108. The blind bore 110 defines an axial flow passage 115 within the perforating tool 100 to accommodate a high pressure abrasive cutting fluid as described below. Less preferably, the bore 110 can be a through bore drilled through the distal end 108 of the perforating tool 100, though this will have a substantially negative effect on the pressure of the cutting fluid used to perforate the well casing as will become evident below. In the embodiment illustrated in FIG. 1 a, the blind bore 110 is closed at the distal end 108 of the perforating tool 100; i.e. there is no fluid communication between the interior of that bore 110 and the exterior of the tool adjacent the distal end 108. In an alternate and preferred embodiment illustrated in FIG. 1 b, there is a small hole 109 provided through the distal end 108 of the tool 100. By ‘small’ here, it is meant that the hole 109 has smaller lateral dimensions (e.g. a smaller diameter) than the diameter of the blind bore 110. Preferably, a chamfered edge 111 is provided about the perimeter of the hole 109 at the interior surface of the distal end 108 of the tool 100. The chamfered edge 111 serves as a seat for a flow plug during operation of the perforating tool 100 as will be later described.
The perforating tool 100 preferably is machined at its proximal end 107 adjacent the opening for blind bore 110, to accommodate or be mated to the end of a length of upset tubing 500 as is known in the art. The exact means for attaching the upset tubing 500 to the proximal end of the perforating tool 100 are not critical, and can employ any known or conventional means for attaching upset tubing to downhole drilling equipment, which means are well known by those skilled in the art, so long as the following conditions are taken into consideration. First, the means employed should provide fluid tightness between the tubing 500 and the tool 100 at high internal fluid pressure, preferably at least 2500, preferably at least 3000, preferably at least 3500, preferably at least 4000, preferably at least 4500, preferably at least 5000, preferably at least 6000, preferably at least 8000, preferably at least 10,000, psi. By fluid tightness, it is not intended or implied that there cannot be any fluid leaking out of the tubing-perforating tool juncture or through the attachment means at the above fluid pressures, or even that substantial fluid cannot leak out; only that the fluid pressure in the axial flow passage 115 is not thereby diminished by more than about 40, preferably 30, preferably 20, preferably 10, preferably 5, percent. Second, the means for attaching the upset tubing 500 to the perforating tool 100 should be able to withstand rotational or torsional stresses downhole, e.g. at a depth of 50-5000 feet or more, based on rotating the upset tubing at the surface at a rate of about 10-500, more preferably 15-100 RPMs. This is because, as will be further described, the perforating tool 100 is caused to rotate downhole by rotating the upset tubing at the surface. Exemplary attachment means include threaded connections, snap-type or locking connections that are or may be sealed using gaskets, O-rings, and the like.
Preferably, the distal end 108 of the perforating tool 100 is chamfered to promote smooth insertion into and passage through the well casing. Optionally, the proximal end 107 can be chamfered as well to promote smooth retraction and withdrawal of the perforating tool 100 from the well casing following a well perforating operation.
The perforating tool 100 has at least one, and preferably has a plurality of lateral ports 120 located in the circumferential wall of the tool 100. Preferably, each port 120 is provided with an abrasion resistant insert 125 that has a port hole provided or drilled therethrough, and which is inserted and accommodated within an aperture drilled or punched substantially radially through the circumferential wall of the perforating tool 100. The lateral ports 120 provide fluid communication between the axial flow passage 115 and a position exterior the perforating tool 100, and are passageways for jets of the high pressure abrasive cutting fluid used to perforate the well casing as will be further described. The inserts 125 are resistant to abrasion or erosion from the cutting fluid which is the reason they are used. The ports 120 can be provided by first inserting solid inserts 125 made from carbide or other resistant material into predrilled apertures in the circumferential wall of the tool 100, and then drilling port holes through the inserts. Alternatively, the inserts 125 can have the port holes predrilled therein prior to being inserted in the apertures of the perforating tool 100 wall.
Preferably, the abrasion resistant inserts 125 are made from carbide material, most preferably from tungsten carbide. Less preferably, the abrasion resistant inserts 125 can be made from another suitable or conventional abrasion resistant material that is effective to withstand the high pressure abrasive cutting fluid that will be jetted through the ports 120, with little or substantially no erosion of the inserts 125 following 2, 3, 4, 5, 6, 7, 8, 9 or 10, well perforating operations (described below). However, it should be understood the inserts 125 (even those made from tungsten carbide) eventually will erode from the abrasive cutting fluid to the point that either the inserts 125 or the entire perforating tool 100 should be replaced.
The lateral ports 120 are of minor diameter compared to the diameter of the perforating tool 100, preferably not more than 20 or 15 percent the OD of the perforating tool, most preferably not more than 12, 10, 8, 6 or 5, percent the OD of the perforating tool.
In operation, the perforating tool 100 is rotated downhole via the upset tubing 500 from the surface, and the high pressure abrasive cutting fluid is pumped through the axial flow passage 115 and jetted out the lateral ports 120 to perforate the well casing at the desired depth. Therefore, it is desired the tool 100 be designed to be substantially balanced during a perforating operation. By balanced, it is meant that when the tool 100 is rotated within the well casing as high pressure cutting fluid is jetted out from the lateral ports 120, the perforating tool 100 rotates uniformly about its longitudinal axis without being thrust against the surrounding well casing. To achieve such a balanced design, preferably the plurality of ports 120 are provided 1) having substantially equal diameters and spaced circumferentially apart from one another according to the following relation when viewed along the longitudinal axis 101 of the perforating tool 100:
circumferential spacing of ports =2π radians/(number of ports)
resulting in a circumferential spacing of π radians for 2 ports, 2π/3 radians for 3 ports, π/2 radians for 4 ports, etc.; and 2) such that each port 120 is radially aligned with the perforating tool 100 so that a centerline 121 of each port 120 intersects the longitudinal axis 101 of the perforating tool 100.
When the ports 120 are provided as described in the preceding paragraph, the sum of the lateral thrust vectors resulting from the cutting fluid jetting out the ports 120 is substantially zero. Thus, the principal net force acting on the perforating tool 100 during a perforating operation is the rotational force or torque supplied via the upset tubing from the surface, and substantially no net lateral thrust or force moments act on the tool 100 as a result of the fluid jetting from lateral ports 120. Therefore, the perforating tool 100 is permitted to rotate freely within the well casing based on the torque supplied from the upset tubing 500, without substantially binding or seizing against the well casing as it is rotated.
Also, it is preferred that lateral ports 120 are provided spaced longitudinally of the perforating tool 100 in the circumferential wall thereof, in order to provide a perforation or groove 425 (FIG. 7) in the well casing 400 of sufficient width to accommodate a terminal portion 206 of the lateral channel alignment tool 200 (discussed below). It is noted that a net moment may result due to the longitudinal spacing of the ports 120 along the length of the perforating tool 100, which moment would tend to cause the tool 100 to rotate about an axis perpendicular to its longitudinal axis 101. However, such a moment is countered by the upset tubing 500 which extends from the surface generally along the longitudinal axis 101, and is rigidly connected to the perforating tool 100. Conversely, the upset tubing 500 is relatively ineffective to prevent lateral movement of the perforating tool 100 downhole, which is why it is desired the ports 120 be provided so the lateral force vectors from jetting fluid balance out.
The well perforating tool 100 can be supplied in a multitude of dimensions depending on the diameter of the well casing that is to be perforated. Generally, it is preferred the perforating tool 100 be provided such that its OD is slightly smaller than the ID of the well casing so the tool 100 slides readily down into the well casing until the desired depth has been reached. For example, for standard 4⅛″ well casing, the perforating tool 100 can have an OD of 3¾″ to 4 1/16″, and more preferably about 3⅞″ to about 4 1/32″. It will be understood the OD of the perforating tool 100 is provided to effect smooth rotation thereof within the well casing during a well perforation operation. From the present disclosure, a person of ordinary skill in the art can, without undue experimentation, make a perforating tool 100 having appropriate dimensions to suit the particular well casing in a particular well.
Referring now to FIGS. 4 a, 4 b, and 5, the lateral channel alignment tool 200 has a substantially elongate basic body 202 of generally cylindrical shape having a proximal end 207 and a distal end 208, and a lateral alignment member 204 pivotally attached to the basic body 202 at or adjacent the distal end 208 via a fulcrum or pivot joint 240. The basic body 202 preferably is made from a round steel billet. The body 202 has a longitudinal through bore 220 drilled therethrough, which defines a longitudinal passage 225 adapted to accommodate a blaster nozzle and associated high pressure hose (later described). The basic body 202 preferably is further machined at its proximal end 207 to accommodate or be mated to the end of a length of upset tubing (not shown) as is known in the art. As seen in FIG. 4 a, the machined opening 212 adjacent the proximal end 207 preferably includes a mating portion 213 for mating the upset tubing, and a neck potion 214 to provide a smooth transition and fluid communication between the mating portion 213 and the through bore 220.
Most preferably, the through bore 220, and therefore the longitudinal passage 225, is radially offset relative to the longitudinal axis 201 of the body 202. Typically, the longitudinal passage 225 has a smaller diameter than the mating portion 213 because the blaster nozzle and hose that must be accommodated by the passage 225 are of smaller diameter than the upset tubing that must be accommodated by the mating portion 213—typically 2⅜″ to 2⅞″ diameter. Therefore, the machined mating portion 213 is provided more centrally (though not necessarily concentrically) in the proximal end 207 of the basic body 202 to accommodate its larger diameter. In this construction, as seen in FIG. 4 a, the neck portion 214 is provided as a reducing portion in order to provide a smooth transition between the larger diameter of the more centrally aligned mating portion 213 and the smaller diameter of the radially offset through bore 220. The through bore 220 (longitudinal passage 225) is radially offset in order to accommodate larger diameter high pressure hose, and consequently greater drilling fluid flow rates, for boring a lateral channel into the earth's strata than has heretofore been possible or practical in the art as will be described.
The lateral alignment member 204 is pivotally attached to the basic body 202 at or adjacent the distal end 208 via fulcrum or pivot joint 240. The lateral alignment member 204 has a generally elbow shape, including a major or first portion 205 that extends generally lengthwise, and a terminal portion 206 that extends transversely on or at an angle relative to the lengthwise direction of the first portion 205. An elbow-shaped passage 230 is provided within the lateral alignment member 204, extending through the respective first and terminal portions 205 and 206 thereof, from an entrance located adjacent the pivot joint 240 along a substantially arcuate path to an exit located in the terminal portion 206. The entrance of the elbow-shaped passage 230 is located adjacent the distal end of the longitudinal passage 225 in the basic body 202, and is adapted to receive a blaster nozzle and associated high pressure hose therefrom. Thus received, the elbow-shaped passage 230 is adapted to direct the blaster nozzle and hose out the exit located in the terminal portion 206 and out into the earth strata to complete a lateral channel boring operation in the adjacent formation (described below). As seen in FIG. 4 a, the diameter of the elbow shaped passage 230 (including its entrance) can be larger than that of the longitudinal passage 225, so long as the two passages are arranged so that the blaster nozzle and higher pressure hose can be delivered from the latter to the former when fed down through the alignment tool 200.
The lateral alignment member 204 preferably is machined from A-2 or D-2 tool steel, and is machined in two mirror-image or clamshell halves via conventional techniques to provide the above-described construction. When made as clamshell halves, the two halves are fastened to one another, e.g., using socket head cap screws. The member 204 preferably is heat treated to acquire a hardness of 55-65 RC.
The alignment tool 200 includes a biasing mechanism effective to bias the lateral alignment member 204 in an angled or laterally engaged position relative to the basic body 202 as shown in FIG. 4 b. In the illustrated embodiment, the biasing mechanism is a pneumatic or hydraulic compression cylinder 250 attached to first and second tensioning brackets 252 and 254 located respectively on the basic body 202 and lateral alignment member 204. Compression cylinders generally are well known in the art, and the particular compression cylinder used (e.g. N₂, air, other gas, hydraulic, etc.) is not critical so long as it has the tendency to pull the brackets 252 and 254 closer together and thus bias the member 204 in the laterally engaged position shown in FIG. 4 b. The first and second tensioning brackets 252 and 254 preferably are located on the respective body 202 and member 204 such that they extend generally in the same radial direction (when viewed along an end of the basic body 202—arrow A in FIG. 4 a) as the transversely extending terminal portion 206 of the member 204. The pivot joint or fulcrum 240 between the body 202 and member 204 is arranged such that the lateral alignment member 204 pivots along an arc located in a plane with the first and second tensioning brackets 252 and 254. When a compression cylinder 250 is used as the biasing mechanism, preferably the basic body 202 has a cylinder pocket 251 provided or machined therein to accommodate the cylinder 250 within the overall geometric dimensions of the body 202, thereby facilitating unobstructed insertion of the entire assembly downhole.
With the construction described in the preceding paragraph, when the lateral channel alignment tool 200 is provided downhole within a well casing, the compression cylinder 250 urges or forces the terminal portion 206 of the lateral alignment member 204 (and correspondingly the exit of the elbow-shaped passage 230) toward an engaged position in a lateral direction radially outward relative to the longitudinal axis of the basic body 202 and against the well casing. (FIG. 4 b shows the alignment tool 200 in the engaged position). Alternatively, other suitable biasing mechanisms can be used to achieve this effect, for example a torsion spring located at or coupled to the pivot joint 240, spring clips, helical spring or elastic band connected to the brackets 252 and 254, or any other suitable or conventional means. In order to insert the tool 200 into the well casing, the lateral alignment member 204 is forced into an extended position against the action of the biasing mechanism (compression cylinder 250), shown in FIG. 4 a, such that the basic body 202 and member 204 are substantially longitudinally aligned to facilitate insertion of the tool 200. Once in the well casing, the external force holding the member 204 in the extended position is removed, and the terminal portion 206 is forced against the well casing by operation of the compression cylinder 250.
Methods for completing lateral channels from an existing well will now be described.
Referring first to FIG. 6, a conventional cement and steel encased oil or gas well is depicted schematically, having a steel well casing 400, an annular cement encasement 450, and showing the earth strata (oil bearing formation) 475 beyond. First, the well perforating tool 100 is connected to the distal end of a length of upset tubing 500 via suitable attachment means as previously described. The perforating tool 100 is lowered into the well casing 400 via the upset tubing 500 to a depth at which it is desired to perforate the casing and complete a lateral channel into the adjacent formation 475. The perforating tool 100 is suspended at the desired depth at the end of the upset tubing 500. On the surface, the upset tubing is connected to a high pressure abrasive cutting fluid source (not shown), capable of supplying high pressure cutting fluid at a pressure of 1000-10,000 psi, preferably 2000-8000 psi, more preferably about 2500 to 5000 psi. A suitable or conventional swivel tool as known in the art (also not shown) is coupled to the proximal end of the upset tubing 500 extending out from the well casing at the earth surface. The swivel tool is engaged, and supplies torque to the upset tubing 500, which in turn supplies torque to the perforating tool 100 downhole to rotate the tool 100. The swivel tool is operated to achieve a rotational velocity for the perforating tool 100 of 5-500, preferably 10-250, preferably 15-200, preferably 15-150, RPMs. Alternatively to a swivel tool at the surface, torque can be supplied to rotate the perforating tool 100 from a downhole motor as known in the art.
The high pressure cutting fluid source is engaged, and pumps abrasive cutting fluid through the upset tubing 500, and into the axial flow passage 115 of the tool 100, such that the cutting fluid is caused to jet out from the lateral ports 120 under high pressure and impinge against the well casing 400, preferably at 2500-5000 psi. The abrasive cutting fluid can be any known or conventional cutting fluid suitable to abrade and perforate the well casing 400.
As the tool 100 rotates and jets of the high pressure abrasive cutting fluid impinge on the well casing 400, the jets continually abrade and degrade the well casing 400 about its entire circumference along a 360° path. The tool 100 continues to rotate, and the cutting fluid is continuously pumped for a period of time, preferably 5-60, more preferably about 10-40 or 10-30 minutes, depending on the material and the integrity of the well casing 400, until ultimately the casing 400 and the cement encasement 450 surrounding the casing 400 have been worn away about the entire 360° circumference thereof. The results are a substantially severed well casing 400 and cement encasement 450 (see FIG. 7), yielding a circular perforation or groove 425 in the casing 400 and cement encasement 450 at the depth at which the perforating operation was performed. It is noted the upper portions of the now-severed well casing 400 and cement encasement 450 generally will not fall, thus closing the newly made groove 425, because these will remain suspended, held up by the surrounding earth. However, for relatively newer wells where the earth has not yet sufficiently bound to the encasement to prevent collapse, or otherwise for grooves 425 made at great depths, it is desirable to place one or a plurality of support members 430 in the groove 425 to support the upper portions of the severed casing 400 and cement encasement 450 to prevent collapse.
Alternatively, the circular perforation or groove 425 can be provided by the following, alternative method. Once the perforating tool 100 has been lowered to the appropriate depth at which it is desired to provide the groove 425, the abrasive cutting fluid is pumped into the axial flow passage 115, causing jets from the lateral ports 120 as before to impinge against the well casing 400. In this method, the well perforating tool 100 is alternately extended and withdrawn (i.e. translated alternately upward and downward) a certain distance corresponding to the desired overall height of the finished groove 425, such that the impinging jets against the well casing 400 cut a vertical slot through the casing 400. Once the vertical slot has been completed, the perforating tool 100 is rotated within the well casing incrementally such that the lateral port(s) 120 is/are aligned with a portion of the casing immediately adjacent the previously cut vertical slot. Then the jetting and alternate vertical translating steps are repeated to cut a subsequent vertical slot in the well casing, that is located circumferentially adjacent the prior-cut vertical slot, such that the vertical slots together define a substantially continuous opening through the casing. This operation is repeated ultimately until a substantially continuous circular perforation or groove is provided in the casing. In this embodiment, only one lateral port 120 may be necessary in the circumferential wall of the perforating tool 100 because the height of the groove 425 is provided based on the upward/downward translation of the tool 100. However, it may be desirable to provide multiple ports 120 at the same longitudinal elevation but at a different circumferential location, such as 180° offset, in order to improve cutting efficiency or time to produce the groove 425.
In a further alternative method, the circular perforation or groove 425 can be provided by simultaneously rotating, and translating alternately upward and downward, the well perforating tool 100 as the jets of the high pressure abrasive cutting fluid emerge from the ports 120 and impinge on the well casing 400. During this operation, the jets continually abrade and degrade the well casing 400 about its entire circumference along a 360° path based on the rotation of the perforating tool 100. At the same time, a groove 425 having a desired overall height is provided based on the upward/downward translation of the perforating tool 100 as it is rotated.
Regardless of the particular method of operation of the cutting tool 100 to perforate the well casing, the high pressure abrasive cutting fluid is forced out the ports 120 based on the pressure of that fluid being delivered to the flow passage 115 (defined by blind bore 110). During operation, the distal end 108 of the cutting tool 100 is closed to the flow of cutting fluid in order to ensure maximum fluid pressure through the ports 120. In the embodiment of FIG. 1 a, this is achieved by the distal end 108 being a solid, imperforate wall. In the embodiment of FIG. 1 b, a plug member 112 is provided to close the hole 109 during operation of the perforating tool 100. In the embodiment where the hole 109 is circular and has a chamfered edge 111 located at its interior circumference, the plug member 112 can be a ball bearing, such as a steel ball bearing, whose diameter is selected to be received and seated against the chamfered edge 111, thereby closing off the hole 109. By ‘closing off,’ ‘closed off’ and other cognates thereof, it is not meant that the plug member must provide a completely fluid-tight seal to completely prevent fluid from passing through the hole 109. Rather, the plug member simply closes the hole 109 to a sufficient extent to retain a substantial proportion of the cutting fluid pressure delivered to the axial flow passage 1 15, (preferably at least 50%, more preferably at least 60%, 70%, 80%, 90% or 95%, of initial fluid pressure), for delivery through the lateral port(s) 120, so that substantial pressure is not lost to flow through the hole 109 during operation of the perforating tool 100. No particular retention means are necessary to hold the plug member 112 in place, as it will be held in place, preferably seated against chamfered edge 111, by the fluid pressure of the cutting fluid during operation.
Once a particular cutting operation is complete (e.g. to perforate well casing at a selected depth), the cutting tool 100 can be cleaned out by flushing water or some other cleaning fluid in a ‘reverse flow’ direction through the cutting tool 100. This can be achieved by pumping a fluid (e.g. water) into the well casing 400 from the surface, in the annular space defined between the casing wall and the outer surface of the upset tubing 500. The pressure of this fluid presses upward against the plug member 112 as it flows through the distal end 108 from the bottom surface thereof, and flows upward through the flow passage 115, ultimately through the upset tubing 500 to exit at the surface. Such a reverse flow flushing step is desirable to clean out residual sand, grit or other abrasive particles or particulates that are present in the cutting fluid used to perforate the well casing. From time to time, some of these solids can or may settle in the flow passage 115, thereby restricting flow of the cutting fluid or perhaps blocking flow through the ports 120 altogether. A high-pressure reverse-flow flush as described here can be used to clean out the cutting tool 100, particularly to drive any settled or deposited solids upward and out of the system through the upset tubing 500 to exit at the surface. Once the flushing operation is complete, the water from the annular space in the well casing 400 can be drained, the plug member 112 re-set to close off the hole 109, and cutting operations restarted. Preferably, the plug member 112 is a ball bearing as mentioned above, whose diameter (and that of the corresponding chamfered edge 111) relative to the interior diameter of the blind bore 110 is sufficiently large that it will self-seat against the chamfered edge 111 by gravity. It should be noted it may not be necessary to pump the reverse-flow flushing fluid with sufficient pressure to eject the plug member 112 at the surface, though that may be desired to achieve adequate flushing of settled solids. If the plug member 112 is ejected, then it or another one can be replaced by simply dropping it through the upset tubing 500 from the surface, and it will re-seat against the chamfered edge 111 by gravity.
The foregoing flushing step will be desirable in the event the perforating tool should become clogged with settled solids during a perforating operation. Using the flushing method, the perforating tool 100 can be cleaned downhole and in place without moving it from the correct depth to complete the pending perforation. It is therefore made unnecessary to withdraw it for cleaning and then to attempt its re-alignment with the started perforation, which may be difficult. Alternatively, if it is desired to complete multiple casing perforations at different depths, one can conduct a flushing operation in between successive perforations, instead of withdrawing the perforating tool 100 each time to clean it before conducting the next perforating operation at a different depth.
Returning to drilling methods, once the circular perforation or groove 425 has been completed, or multiple of them at selected depths as the case may be, the perforating tool 100 is withdrawn from the well casing and the lateral channel alignment tool 200 is lowered in its place. As shown in FIG. 8, the alignment tool 200 is attached to the end of upset tubing (not shown) and lowered into the well casing 400 where the well perforating operation was previously performed. To insert the alignment tool 200 into the well casing, first the lateral alignment member 204 is pivoted in the extended position against the action of the biasing mechanism (compression cylinder 250) via an external force. Next, the tool 200 is inserted into the well casing and the external force is removed, so that the basic body 202 is substantially slidably disposed in the well casing 400 and the lateral alignment member 204 is biased such that the terminal portion 206 is forced up against the casing 400 at a position generally below the basic body 202.
With the terminal portion 206 forced against the well casing 400, the alignment tool 200 is pushed downward via the upset tubing from the surface, until the terminal portion 206 arrives at the previously made groove 425 in the casing 400 and the cement encasement 450. As the alignment tool 200 continues downward, due to the biasing of the lateral alignment member 204 the terminal portion 206 is caused to move laterally, and ultimately to lock into place in a laterally engaged position (FIG. 4 b) within the groove 425 adjacent the severed upper and lower portions of the casing and cement encasement. (See FIG. 9) Thus the lateral alignment member 204, and hence the alignment tool 200, automatically locks into place on reaching the groove 425, and the exit of the elbow-shaped passage 230 is now provided adjacent, preferably substantially up against, the earth formation 475 located laterally of the severed casing.
With the lateral alignment member 204 in this position, a blaster nozzle 300 is fed down through the upset tubing at the end of a length of high pressure hose 310, such as coil tubing or macaroni tubing as known in the art. On reaching the basic body 202, the blaster nozzle 300 is fed through the machined opening 212 adjacent the proximal end 207 of the basic body 202, into and through the longitudinal passage 225, into the entrance of the elbow-shaped passage 230, and through that passage 230 to the exit thereof located in the terminal portion 206, which is positioned and oriented laterally against the earth formation in which a lateral channel is to be completed.
Next, high pressure drilling fluid is pumped through the high pressure hose 310, down to the blaster nozzle 300 at the end thereof, so that the blaster nozzle 300 can bore a lateral channel 350 from the existing well adjacent the location where the well casing and cement encasement previously were severed (See FIG. 10). Nozzle blaster operations using high pressure fluid, such as water with or without abrasive component additives at pressures ranging from 2000-25,000 psi, generally are known in the art, and are described, e.g., in the aforementioned U.S. patents which have been incorporated herein. Generally, any suitable blaster nozzle and/or high pressure hose can be used so long as the blaster nozzle and hose can negotiate the longitudinal passage 225 and the elbow-shaped passage 230 of the lateral channel alignment tool 200. High pressure hose 310 is fed continuously from the surface until a lateral channel 350 of desired length has been completed, at which point the hose 310 is withdrawn at least to a sufficient extent to withdraw the blaster nozzle 300 from the newly bored lateral channel 350 in the earth strata. If it is desired to complete more than one lateral channel at the same depth, then the alignment tool 200 simply is rotated from the previously completed lateral channel and the process is repeated for a second lateral channel, and a third, and so on. It will be evident one can complete multiple lateral channels at a given depth without having to repeat a well perforating operation.
To remove the alignment tool 200, it is simply withdrawn in a conventional manner. The curved transition surface 290 between the first and terminal portions 205 and 206 acts as a cammed surface essentially forcing the alignment member 204 back into the extended position so that it can be withdrawn from the well casing. Alternatively, if it is desired to feed the alignment tool 200 deeper than the groove 425, for example down to a deeper groove 425 cut in the same well to complete additional lateral channels at a greater depth, the biasing mechanism can be provided such that it can be actuated to retain the member 204 in the extended position until the terminal portion 206 has exceeded the depth of the first groove. Then the biasing mechanism is de-actuated and once again is effective to bias the member 204, and terminal portion 206, against the well casing so it will automatically lock into place when the next-deeper groove in the casing 400 is reached. Servos and other actuating mechanisms and methods generally are known in the art. For example, when a gas or hydraulic compression cylinder 250 is used, gas or hydraulic pressure can be supplied or withdrawn via a hydraulic fluid line or gas manifold based on actuation signals from an operator. The implementation of such methods is within the skill of a person having ordinary skill in the art, and will not be described further here.
In a further preferred embodiment, the perforating tool 100 is used and operated similarly as described above to perforate the well casing 400 and to provide the circumferential groove 425 in the cement encasement 450. In this embodiment, however, the perforating tool 100 continues to operate so that the jets of cutting fluid emitted from the lateral ports 120 in the cutting tool 100 are directed at and cut away strata material beyond the cement encasement 450, to provide a circumferential groove 426 cut out of the earth strata. This mode of operation is illustrate with respect to FIGS. 7 a and 9 a. As is seen in these figures, the result of this procedure is to provide a circumferential groove 425/426 whose horizontal expanse (diameter) is substantially increased compared to when only the groove 425 in the cement encasement 450 is provided (FIG. 7 a). An advantage to this embodiment is that it will accommodate even larger-diameter high-pressure hose for boring a lateral channel from the original well bore (encased by casing 400), than if only the groove 425 is provided (described more fully below). This is because the terminal portion 206 of the lateral channel alignment tool 200 is permitted to extend even further horizontally than before, into the newly-formed groove 426 in the strata (FIG. 9 a). Consequently, a larger lateral alignment member 204, having a larger elbow-shaped passage 230 that has an outside bend (shown as the right-most broken line for passage 230 in FIG. 4 a) with a greater radius of curvature R₁, able to accommodate a larger-diameter hose, can be used.
In a further embodiment illustrated in FIG. 20, the lateral channel alignment tool 200 includes an extensible hose guide member 260 that is designed to extend or telescope from the distal end of the terminal portion 206 to help guide the high-pressure hose into engagement with the strata. As seen more clearly in FIG. 21, the hose guide member 260 is preferably provided as a series of guide sections 262, each having a horizontal and two opposing vertical plate portions that cooperate to provide a substantially U-shaped cross-section. The guide sections 262 can be made from a sheet of material (such as metal) that can be bent to provide the respective horizontal and vertical plate portions in a U-shaped configuration. Each guide section 262 is joined to the adjacent guide section(s) 262 via a pivot joint 264, which can be a simple hinge. A locking lip or flange 266 is provided extending forward from the underside of the horizontal plate portion of each guide section 262. The flange 266 has an upper surface that extends substantially parallel to the bottom face of horizontal plate portion to which it is attached. This flange 266 prevents the successive (next-forward) horizontal plate portion of the next successive guide section 262 a from pivoting below the plane of the horizontal plate portion of the instant guide section 262 b (see FIG. 21). Thus, when fully extended, all of the guide sections 262 cooperate to provide a substantially U-shaped guide passageway 208 to guide and support a high-pressure hose exiting the elbow-shaped passage 230 at the terminal portion 206 of the lateral alignment member 204. The vertically extending plate portions are not attached to adjacent ones on adjacent guide portions 262. When the guide member 260 (including its discrete guide portions 262) is retracted within the lateral alignment member 204, the vertical plate portions on adjacent guide portions 262 are able to deflect so that the guide portions 262 can pivot relative to one another for storage within a receiving compartment (for example within the elbow-shaped passage 230) that has a curved or elbow shape in order to accommodate the overall shape of the member 204. The guide member 260 can be actuated (extended and retracted) using suitable or conventional means, including through use of a small servo motor as known in the art. Alternatively, it can be spring-loaded so that it is biased into an extended position via a conventional spring mechanism, with a wire line connected to the proximal end and threaded up to the surface through the upset tubing 500. To extend the guide member 260, tension in the wire line can be relaxed, thus permitting extension of the guide member 260 by action of the spring that biases it in an extended position. When it is desired to retract the guide member 260, tension can be applied to the wire line to retract the guide member 260 back into the lateral alignment member 204, against the biasing action of the spring mechanism that is used. The disclosed hose guide member 260 may be useful if, for example, a groove is cut in the earth strata beyond the casing to a diameter too large for the terminal portion of the member 204 to reach in a fully engaged position. In this event, the hose guide member 260 can be extended or telescoped horizontally outward, toward the base of the groove cut in the strata, to help guide the flexible hose into contact with the strata at an appropriate location along a horizontal or lateral path, as seen in FIG. 9 b.
The disclosed tools and methods provide several advantages over conventional lateral drilling systems and techniques. One such advantage is that it is not necessary to maintain any downhole equipment at the exact depth and in precise alignment with a previously cut small hole through the well casing in order to align the blaster nozzle with the previously cut hole. With the apparatus herein described, once the well perforating operation has been completed and the well casing has been severed or perforated as described above, the alignment tool 200 is inserted downhole into the well casing and automatically locks into place once it reaches the previously made well perforation. Furthermore, because the well is severed/perforated substantially about its entire circumference, a lateral channel boring operation can be performed in any compass direction radially outward from the well casing and it is not necessary to maintain the precise compass alignment of the alignment tool 200. In addition, once a lateral channel has been bored in one compass direction, the blaster nozzle and hose can be withdrawn into the alignment member 204, the tool 200 can be rotated to another compass direction, and an additional drilling operation or operations can be performed at the same depth in different compass directions without having to drill additional holes or repeat a well perforating operation in the well casing.
A further advantage, described briefly above, is that a larger diameter high pressure hose and blaster nozzle can be used for boring a lateral channel in the earth strata from an existing oil or gas well than previously was possible with conventional equipment in a well having the same diameter. This is because, conventionally, the downhole “shoe” for redirecting the blaster nozzle and associated high pressure hose incorporated a longitudinal channel for receiving the blaster nozzle and high pressure hose that was substantially centrally aligned along the longitudinal axis of the well casing. Conversely, as can be see in FIG. 4 a, the longitudinal passage 225 and the longitudinal portion of the elbow-shaped passage 230 are radially offset from the longitudinal axis 201. In this construction, the radius of curvature R₁(FIG. 4 a) for the pathway of the high pressure hose is substantially increased compared to the case when the longitudinal passage is provided centered on the longitudinal axis. As a result, larger diameter high pressure hose can be employed to bore lateral channels into the earth strata, because the high pressure hose does not need to bend as tightly to be redirected in a lateral direction, so the binding that otherwise would occur from tightly bending a larger diameter hose is avoided. Simply off-setting the longitudinal passage 225 (and consequently offsetting or providing a relatively large inlet of the elbow-shaped passage 230), in conjunction with providing the groove 425 in the cement encasement 450 as described above, enables larger-diameter hose to be used than conventionally for reasons already described. However, as also described above, further providing a groove 426 in the strata beyond the encasement 450 enables even larger-diameter hose to be used, because now the radius of curvature for the outside bend of elbow-shaped passage 230 can be increased even more. The length of the lateral alignment member 204 may need to increase in order that the radius of curvature, R₁, can increase sufficiently so that the high-pressure hose will be directed along a substantially horizontal course on exiting the elbow-shaped passage 230, despite further horizontal penetration of the terminal portion 206 of the lateral alignment member 204.
One advantage of larger diameter high pressure hose is that higher volume flowrates of drilling fluid can be accommodated in the hose. This is particularly useful when a portion of the drilling fluid is used to provide forward thrust to the hose and the blaster nozzle via thrusters provided in the hose (described below), because high pressure jets of the fluid can exit the thrusters to thrust the blaster nozzle forward without substantially sacrificing the flow rate and pressure of the drilling fluid in the blaster nozzle used to bore the lateral channel.
In one embodiment, the high pressure hose includes or is provided as a flexible hose assembly comprising a flexible hose with thrusters and a blaster nozzle coupled to and in fluid communication with the terminal end of the hose. With reference to FIG. 14, there is shown generally a flexible hose assembly 10 for completing a lateral channel in a general direction indicated by the arrow B, which preferably comprises a blaster nozzle 300 and a high pressure hose 310. High pressure hose 310 includes a plurality of flexible hose sections 22, a pair of pressure fittings 23 attached to the ends of each hose section 22, and a plurality of thruster couplings 12, each of which joins a pair of adjacent pressure fittings 23. Hose assembly 10 comprises a blaster nozzle 300 at its distal end and is connected to a source (not shown) of high pressure drilling fluid, preferably an aqueous drilling fluid, preferably water, less preferably some other liquid, at its proximal end. Couplings 12 are spaced at least, or not more than, 5, 10, 20, 30, 40, 50, 60, 70, 80, 90 or 100 feet apart from each other in hose 310. The total hose length is preferably at least or not more than 100 or 200 or 400 or 600 or 700 or 800 or 900 or 1000 or 1200 or 1400 or 1600 or 1800 or 2000 feet. Hose sections 22 are preferably flexible hydraulic hose known in the art, comprising a steel braided rubber-TEFLON (polytetrafluoroethylene) mesh, preferably rated to withstand at least 5,000, preferably at least 10,000, preferably at least 15,000, psi water pressure. High pressure drilling fluid is preferably supplied at at least 2,000, 5,000, 10,000, 15,000, or 18,000 psi, or at 5,000 to 10,000 to 15,000 psi. When used to drill laterally from a well, the hose extends about or at least or not more than 7, 10, 50, 100, 200, 250, 300, 350, 400, 500, 1000, or 2000 feet laterally from the original well. In one embodiment the hose extends about 440 feet laterally from the original well.
As illustrated in FIG. 11, in one embodiment a thruster coupling 12 comprises a coupling or fitting, preferably made from metal, preferably steel, most preferably stainless steel, less preferably aluminum. Less preferably, coupling 12 is a fitting made from plastic, thermoset, or polymeric material, able to withstand 5,000 to 10,000 to 15,000 psi of water pressure. Still less preferably, coupling 12 is a fitting made from ceramic material. It is important to note that when a drilling fluid other than water is used, the material of construction of the couplings 12 must be selected for compatibility with the drilling fluid and yet still withstand the desired fluid pressure. Coupling 12 has two threaded end sections 16 and a middle section 14. Preferably, end sections 16 and middle section 14 are formed integrally as a single solid part or fitting. Threaded sections 16 are female-threaded to receive male-threaded pressure fittings 23 which are attached to, preferably crimped within the ends of, hose sections 22 (FIG. 14).
Alternatively, the fittings 23 can be attached to the ends of the hose sections 22 via any conventional or suitable means capable of withstanding the fluid pressure. In the illustrated embodiment, each fitting 23 has a threaded portion and a crimping portion which can be a unitary or integral piece, or a plurality of pieces joined together as known in the art. Alternatively, the threaded connections may be reversed; i.e. with male-threaded end sections 16 adapted to mate with female-threaded pressure fittings attached to hose sections 22. Less preferably, end sections 16 are adapted to mate with pressure fittings attached to the end of hose sections 22 by any known connecting means capable of providing a substantially water-tight connection at high pressure, e.g. 5,000-15,000 psi. Middle section 14 contains a plurality of holes or thruster ports 18 which pass through the thickness of wall 15 of coupling 12 to permit water to jet out. Though the thruster ports 18 are shown having an opening with a circular cross-section, the thruster port openings can be provided having any desired cross section; e.g. polygonal, curvilinear or any other shape having at least one linear edge, such as a semi-circle.
Coupling 12 preferably is short enough to allow hose 310 to traverse the elbow-shaped passage 230 in the alignment member 204. Therefore, coupling 12 is formed as short as possible, preferably having a length of less than about 3, 2, or 1.5 inches, more preferably about 1 inch or less than 1 inch. Hose 310 (and therefore couplings 12 and hose sections 22) preferably has an outer diameter of about 0.25 to about 3 inches, more preferably about 0.375 to about 2.5 inches, and an inner diameter preferably of about 0.5-2 inches. Couplings 12 have a wall thickness of preferably about 0.025-0.25, more preferably about 0.04-0.1, inches.
Optionally, hose 310 is provided with couplings 12 formed integrally therewith, or with thruster ports 18 disposed directly in the sidewall of a contiguous, unitary, non-sectioned hose at spaced intervals along its length (see FIG. 16). A hose so comprised obviates the need of threaded connections or other connecting means as described above.
In the embodiments shown in FIGS. 11 and 17, thruster ports 18 have hole axes 20 which form a discharge angle β with the longitudinal axis of the coupling 12. The discharge angle β is preferably 5° to 90°, more preferably 10° to 90°, more preferably 10° to 80° , more preferably 15° to 70° , more preferably 20° to 60° , more preferably 25° to 55° , more preferably 30° to 50°, more preferably 40° to 50°, more preferably 40° to 45° , more preferably about 45°. The thruster ports 18 are also oriented such that a jet of drilling fluid passing through them exits the coupling 12 in a substantially rearward direction; i.e. in a direction such that a centerline drawn through the exiting jet forms an acute angle (discharge angle β) with the longitudinal axis of the flexible hose rearward from the location of the thruster port, toward the proximal end of the hose assembly. In this manner, high-pressure jets 30 emerging from thruster ports 18 impart forward drilling force or thrust to the blaster nozzle, thus forcing the blaster nozzle forward into the earth strata (see FIG. 14). As illustrated in FIG. 12, a plurality of thruster ports 18 are disposed in wall 15 around the circumference of coupling 12. There are 2 to 6 or 8 ports, more preferably 3 to 5 ports, more preferably 3 to 4 ports. Thruster ports 18 are spaced uniformly about the circumference of coupling 12, thus forming an angle α between them. Angle α will depend on the number of thruster ports 18, and thus preferably will be from 45° or 60° to 180° , more preferably 72° to 120°, more preferably 90° to 120°. Thruster ports 18 are preferably about 0.010 to 0.017 inches, more preferably 0.012 to 0.016 inches, more preferably 0.014 to 0.015 inches in diameter.
As best seen in FIGS. 11-13, thruster ports 18 are formed in the wall 15 of coupling 12, extending in a substantially rearward direction toward the proximal end of the hose assembly 10, connecting inner opening 17 at the inner surface of wall 15 with outer opening 19 at the outer surface of wall 15. The number of couplings 12, as well as the number and size of thruster ports 18 depends on the desired drilling fluid pressure and flow rate. If a drilling fluid source of only moderate delivery pressure is available, e.g. 5,000-7,000 psi, then relatively fewer couplings 12 and thruster ports 18, as well as possibly smaller diameter thruster ports 18 should be used. However, if higher pressure drilling fluid is supplied, e.g. 10,000-15,000 psi, then more couplings 12 and thruster ports 18 can be utilized. The number of couplings 12 and thruster ports 18, the diameter of thruster ports 18, and the initial drilling fluid pressure and flow rate are all adjusted to achieve flow rates through blaster nozzle 300 of 1-10, more preferably 1.5-8, more preferably 2-6, more preferably 2.2-3.5, more preferably 2.5-3, gal/min. It is also to be noted that because larger diameter hose can be used than conventionally was possible, larger diameter or a greater number of thruster ports 18 also can be used to supply greater drilling thrust without adversely impacting the pressure or flow rate of drilling fluid at the blaster nozzle. This is a substantial advancement over the prior art.
In one embodiment illustrated in FIG. 11, the thruster ports 18 are provided as unobstructed openings or holes through the side wall of the thruster coupling 12. The ports 18 are provided or drilled at an angle so that the exiting pressurized fluid jets in a rearward direction as explained above.
In a further embodiment illustrated in FIG. 17, the thruster couplings 12 and thruster ports 18 are similarly provided as described above shown in FIG. 11, except that the thruster ports 18 are adjustable, including a shutter 31. The shutter 31 is preferably an iris as shown in FIG. 17, and shown close-up in FIG. 19. The shutter 31 is actuated by a servo controller 32 (pictured schematically in the figures) which is controlled by an operator at the surface via wireline, radio signal or any other suitable or conventional means. The servo controller 32 is preferably provided in the sidewall of the coupling 12 as shown in FIG. 18, or is mounted on the inner wall surface of the coupling 12. The servo controller 32 has a small stepping motor to control or actuate the shutter 31 to thereby regulate the diameter or area of the opening 34 for the thruster port 18. A fully open shutter 31 results in the maximum possible thrust from the associated thruster port 18 because the maximum area is available for the expulsion of high pressure fluid. An operator can narrow the opening 34 by closing the shutter 31 to regulate the amount of thrust imparted to the hose assembly by the associated thruster port 18. The smaller diameter the opening 34, the less thrust provided by the thruster port 18. Although an iris is shown, it will be understood that other mechanisms can be provided for the shutter 31 which are conventional or which would be recognized by a person of ordinary skill in the art; e.g. sliding shutter, flap, etc. The servo controller 32 is preferably a conventional servo controller having a servo or stepping motor that is controlled in a conventional manner. Servo controllers are generally known or conventional in the art.
In a further preferred embodiment, the thruster ports 18 can be provided so that different ones of them are opened, permitting the jetting of water from those ports, based on the fluid pressure in the high-pressure hose. For example, the thruster ports 18 can be provided as or incorporating fluid check valves or normally-closed relief valves (schematically illustrated at 38—See FIG. 17 a) as known in the art. Such valves prevent the flow of fluid (from the hose, through the valve 38 and into the space surrounding the hose) below a certain ‘cracking pressure,’ which is characteristic of each valve 38. Below the cracking pressure for the valve 38, no flow is permitted; hence that thruster port 18 is off. At the cracking pressure, however, fluid begins to be emitted from the valve 38 and the thruster port 18 is turned on. Above the cracking pressure, the valve opens fully and maximum flow of the fluid jet through that thruster port 18 is achieved.
In an exemplary embodiment, all the thruster ports 18 in the same thruster coupling 12 can be provided as check valves or relief valves having the same cracking pressure. Couplings 12 with valves of successively increasing cracking-pressure valves can be provided along the length of the flexible hose. For example, the lowest-cracking-pressure valves 38 can be provided in the hose proximate the distal end where the blaster nozzle 300 is cutting the strata. This way, the thruster ports 18 nearest the blaster nozzle 300 are always or nearly always open, providing thrust to the blaster nozzle 300 from a position just behind that nozzle. Also, the rearwardly-directed thruster ports 18 nearest the blaster nozzle 300 continuously sweep freshly made cuttings backward so they are less likely to interfere with continued operation of the blaster nozzle. The cracking pressure of more proximally-located thruster ports 18 (in thruster couplings 12) are higher so that they are not opened unless an operator selects a higher operating fluid pressure for the drilling operation. This may provide a more efficient method of operation because the rearward-most thruster ports 18, which are least able to impart useful thrust to the blaster nozzle 300, are only open when sufficient pressure and flow is employed so that the pressure and flowrates at the blaster nozzle 300 do not suffer from significant fluid and pressure exiting through the whole series of thruster ports 18 disposed along the entire length of the high-pressure hose (which can be several hundred feet or yards, or even greater.
Alternatively, other arrangements of pressure-actuated thruster ports 18 also can be used, and the foregoing arrangement with increasing cracking pressures distal-to-proximal in the high-pressure hose merely illustrates a preferred embodiment.
In addition to providing thrust, the thruster ports 18 also provide another desirable function. Thruster ports 18 keep the bore clear behind blaster nozzle 300 as the rearwardly jetting high pressure drilling fluid (water) washes the drill cuttings out of the lateral bore so that the cuttings do not accumulate in the lateral bore. The high pressure drilling fluid forced through the thruster ports 18 also cleans and reams the bore by clearing away any sand and dirt that has gathered behind the advancing blaster nozzle 300, as well as smoothing the wall of the freshly drilled bore.
This is a desirable feature because, left to accumulate, the cuttings and other debris can present a significant obstacle to lateral boring, effectively sealing the already-bored portion of the lateral bore around the advancing hose assembly 10. This can make removal of the hose assembly 10 difficult once boring is completed. In a worst case, the remaining debris can cause the lateral bore to reseal once the hose assembly 10 has been withdrawn. By forcing these cuttings rearward to exit the lateral bore, the rearwardly directed drilling fluid jets 30 ensure the lateral bore remains substantially open and clear after boring is completed and the hose assembly 10 is removed. By providing the thruster ports 18 along substantially the entire length of the hose assembly 10, drill cuttings can be driven out of the lateral bore from great distances, preferably at least 50, 100, 200, 250, 300, 350, 400, 500, 1000, or more, feet.
In one embodiment, adjustable thruster ports 18 are operated sequentially such that when a thruster port or a group of longitudinally aligned thruster ports is closed, the next-most proximal thruster port or group of longitudinally aligned thruster ports is opened, thereby sweeping cuttings in a proximal direction out from the lateral channel and into the existing well. In this method, the benefits of sweeping the cuttings out of the lateral channel are obtained, while only a relatively small number of the thruster ports 18 is open at any one time. The result is that drilling fluid pressure through the blaster nozzle is maximized, while drilling thrust and lateral channel sweeping is provided by the sequentially operated thruster ports.
Blaster nozzle 300 is of any type that is known or conventional in the art, for example, the type shown in FIGS. 15 a-15 b. In the illustrated embodiment, blaster nozzle 300 comprises a plurality of holes 50 disposed about a front portion 46 a which preferably has a substantially domed shape. Holes 50 are positioned to form angle θ with the longitudinal axis of blaster nozzle 300. Angle θ is 10°-30°, more preferably 15°-25°, more preferably about 20°. Blaster nozzle 300 also comprises a plurality of holes 46 b, which are oriented in a reverse or rearward direction on a rear portion 60 of blaster nozzle 300, the direction and diameter of holes 46 b being similar to that of thruster ports 18 disposed around couplings 12. Holes 46 b serve a similar function as thruster ports 18 to impart forward drilling force to blaster nozzle 300 and to wash drill cuttings rearward to exit the lateral bore. Optionally, front portion 46 a is rotatably coupled to rear portion 60, with holes 50 oriented at an angle such that exiting high-pressure drilling fluid imparts rotational momentum to front portion 46 a, thus causing front portion 46 a to rotate while drilling. Rear portion 60 is either fixed with respect to hose 310 unable to rotate, or is rotatably coupled to hose 310 thus allowing rear portion 60 to rotate independently of hose 310 and front portion 46 a. In this embodiment, holes 46 b are oriented at an angle effective to impart rotational momentum to rear portion 60 upon exit of high-pressure drilling fluid, thus causing rear portion 60 to rotate while drilling. Holes 50 and 46 b can be oriented such that front and rear portions (46 a and 60 respectively) rotate in the same or opposite directions during drilling.
The hose assembly 10 may be provided with a plurality of position indicating sensors 35 along its length. Position indicating sensors 35 are shown schematically in FIG. 14 attached to the thruster couplings 12 and blaster nozzle 300. Alternatively, the position indicating sensors 35 can be provided in the coupling walls, or in the hose wall along its length. The position indicating sensors 35 can emit a radio signal or can be monitored by wireline from the surface to determine the location and configuration of the flexible hose. The adjustable thruster ports 18 can be controlled based on position and configuration information received from these position indicating sensors 35. Preferably, a computer receives information from the position indicating sensors 35 and regulates the adjustable thrusters based on that information to achieve the desired position control of the hose assembly 10 as it drills a lateral bore.
Although the hereinabove described embodiments of the invention constitute preferred embodiments, it should be understood that modifications can be made thereto without departing from the spirit and the scope of the invention as set forth in the appended claims.

Claims

1. A well perforating tool having a substantially cylindrical body having a proximal end and a distal end and defining a circumferential wall of the perforating tool, said perforating tool having a longitudinal axis and comprising an axial blind bore open to said proximal end of the perforating tool and defining an axial flow passage within the perforating tool, a hole provided through the distal end of said tool, said hole having a lateral dimensions smaller than the diameter of said blind bore, and at least one lateral port located in the circumferential wall of said perforating tool, said lateral port providing fluid communication between said axial flow passage and a position exterior of said perforating tool, said lateral port being adapted to accommodate a jet of high pressure cutting fluid for perforating a well casing.

2. A well perforating tool according to claim 1, comprising a plurality of said lateral ports.

3. A well perforating tool according to claim 1, comprising upset tubing operatively connected to said tool and being adapted to convey said cutting fluid to said tool.

4. A well perforating tool according to claim 1, said lateral port being provided as a port hole in an abrasion resistant insert, said abrasion resistant insert being disposed within an aperture drilled or punched substantially radially through the circumferential wall of said perforating tool.

5. A well perforating tool according to claim 4, said abrasion resistant insert being made from carbide material.

6. A well perforating tool according to claim 4, said abrasion resistant insert being made from tungsten carbide.

7. A well perforating tool according to claim 4, comprising a plurality of said lateral ports.

8. A well perforating tool according to claim 1, further comprising a chamfered edge provided about the perimeter of said hole located at an interior surface of said distal end of said tool.

9. A well perforating tool according to claim 1, further comprising a plug member that is dimensioned and adapted to close the hole in said distal end of said tool during operation thereof.

10. A well perforating tool according to claim 8, said hole in said distal end of said tool being a circular hole, said tool further comprising a spherical plug member having a diameter that is selected to be received and seated against said chamfered edge to thereby close said hole during operation of said tool.

11. A well perforating tool according to claim 10, said spherical plug member being a steel ball bearing.

12. An apparatus comprising:

a lateral channel alignment tool comprising a substantially elongate basic body having a longitudinal axis, a lateral alignment member pivotally attached to the basic body, and a biasing mechanism effective to bias said lateral alignment member in an angled or laterally engaged position relative to said basic body, said basic body having a longitudinal passage therethrough that is radially offset relative to the longitudinal axis of said basic body and adapted to accommodate a hose therein, said lateral alignment member comprising a first portion that extends generally lengthwise, a terminal portion that extends at an angle relative to the lengthwise direction of the first portion, and an elbow-shaped passage provided within the lateral alignment member, said elbow-shaped passage extending through said respective first and terminal portions of said lateral alignment member from an entrance located in said first portion to an exit located in said terminal portion, said entrance of said elbow-shaped passage being located adjacent a distal end of said longitudinal passage in said basic body and being adapted to receive a blaster nozzle and associated hose therefrom; and

a hose received within both said longitudinal passage and said elbow-shaped passage, said hose comprising a first hose section, a second hose section, and a thruster coupling including a thruster port, wherein said first hose section and said second hose section are operatively connected by said thruster coupling, said thruster port being actuable based on fluid pressure in said hose.

13. An apparatus according to claim 12, said thruster port comprising a valve having a characteristic cracking pressure such that when said fluid pressure is above the cracking pressure, said valve is opened and fluid is permitted to jet out of said thruster port through said valve, and when said fluid pressure is below the cracking pressure, said valve is closed and fluid is not permitted to jet out of said thruster port.

14. A lateral channel alignment tool according to claim 13, comprising a plurality of said thruster couplings provided along the length of said hose, each said thruster coupling having a thruster port including a valve having a characteristic cracking pressure.

15. A lateral channel alignment tool according to claim 14, wherein the thruster couplings and their associated thruster ports are arranged so that their respective valves, at least some of which having different characteristic cracking pressures, are provided at desired locations along the length of said hose.

16. A lateral channel alignment tool according to claim 12, said elbow-shaped passage being adapted to direct said hose, received from said longitudinal passage, out said exit located in said terminal portion to bore a lateral channel in an adjacent formation of earth.

17. A method of completing a lateral channel from an existing oil or gas well having a well casing, comprising the steps of:

providing a well perforating tool having a substantially elongate body defining a circumferential wall of the perforating tool, said perforating tool having a longitudinal axis and comprising an axial blind bore open to a proximal end of said perforating tool and defining an axial flow passage within the perforating tool, and at least one lateral port located in the circumferential wall of said perforating tool, said lateral port providing fluid communication between said axial flow passage and a position exterior of said perforating tool;

suspending said well perforating tool at a selected depth in said existing well; and

pumping a fluid at high pressure through said axial flow passage such that a jet of said high pressure fluid shoots out from said lateral port, said jet perforating said well casing and cutting away a portion of earth strata beyond said well casing.

18. A method according to claim 17, further comprising operating said well perforating tool to produce a perforation in said well casing about the circumference thereof, and further to cut a circular groove in the earth strata beyond said well casing.

19. A method according to claim 18, said perforation in said casing and said groove in the earth strata having approximately the same height and being aligned with one another.

20. A method according to claim 18, wherein said well includes a cement encasement surrounding said well casing, said cutting tool being operated to produce a perforation in said cement encasement about the circumference thereof, in addition to the perforation in said well casing and the circular groove cut in the earth strata.

21. A method according to claim 20, the perforations provided in said well casing and in said cement encasement and the groove cut in said strata all cooperating to provide a composite groove that expands radially outward from said well.

22. A method according to claim 18, further comprising the steps of:

providing a lateral channel alignment tool comprising a substantially elongate basic body having a longitudinal axis, a lateral alignment member pivotally attached to the basic body, and a biasing mechanism effective to bias said lateral alignment member in an angled or laterally engaged position relative to said basic body, said basic body having a longitudinal passage therethrough adapted to accommodate a hose therein, said lateral alignment member comprising a first portion that extends generally lengthwise, a terminal portion that extends at an angle relative to the lengthwise direction of the first portion, and an elbow-shaped passage provided within the lateral alignment member, said elbow-shaped passage extending through said respective first and terminal portions of said alignment member from an entrance located in said first portion to an exit located in said terminal portion, said entrance of said elbow-shaped passage being located adjacent a distal end of said longitudinal passage in said basic body and being adapted to receive a blaster nozzle and associated hose therefrom;

advancing said lateral channel alignment tool in said well until the terminal portion of said lateral alignment member reaches and engages through said perforation and into said groove in the earth strata; and

providing a flexible hose and directing it through said elbow-shaped passage in said lateral alignment member, out through the exit thereof and into engagement with the earth strata to cut a channel through the strata.

23. A method according to claim 22, wherein said hose is a flexible high-pressure hose comprising a plurality of thruster ports disposed at spaced intervals along the length thereof, the method further comprising actuating said thruster ports based on fluid pressure within said flexible high-pressure hose.

24. A method according to claim 22, said lateral channel alignment tool further comprising an extensible hose guide member provided in said lateral alignment member and effective to extend from the distal end of said terminal portion of said lateral alignment member to help guide a high-pressure hose fed through said elbow-shaped passage and exiting therefrom into engagement with the strata.

25. A method according to claim 24, said hose guide member comprising a series of guide sections, each said guide section having a horizontal and two opposing vertical plate portions that cooperate to provide a substantially U-shaped cross-section, wherein each guide section is joined to adjacent guide section(s) via a pivot joint, a first guide section having a locking flange provided extending forward from the underside of a first horizontal plate portion thereof, said flange having an upper surface that extends substantially parallel to the bottom face of said first horizontal plate portion, said flange being effective to prevent a successive, second horizontal plate portion of a successive, second guide section from pivoting below the plane of the first horizontal plate portion of the first guide section.