The present disclosure relates to firing heads for actuating downhole tools.
One of the activities associated with the completion of an oil or gas well is the perforation of a well casing. During this procedure, perforations, such as passages or holes, are formed in the casing of the well to enable fluid communication between the wellbore and the hydrocarbon producing formation that is intersected by the well. These perforations are usually made with a perforating gun loaded with shaped charges. The gun is lowered into the wellbore on electric wireline, slickline, tubing or coiled tubing, or other means until it is at a desired target depth; e.g., adjacent to a hydrocarbon producing formation. Thereafter, a surface signal actuates a firing head associated with the perforating gun, which then detonates the shaped charges. Projectiles or jets formed by the explosion of the shaped charges penetrate the casing to thereby allow formation fluids to flow from the formation through the perforations and into the production string for flowing to the surface.
Many oil well tools deployed on tubing or coiled tubing use pressure-activated firing heads to initiate a detonation train during a desired well operation. In certain aspects, the present disclosure provides pressure-activated firing heads for situations where a differential pressure and a flow source is used to activate a well tool.
In aspects, the present disclosure provides a firing head assembly for a well tool. The firing head assembly includes a shaft, a piston head, a biasing member, and a housing. The shaft has a nose and a terminal end. The shaft also includes a first shoulder and a second shoulder formed between the nose and the terminal end. The piston head slides along the shaft and is positioned between the retaining element and the first shoulder. The biasing member is mounted on the shaft and positioned between the piston head and the second shoulder. The housing has a bore in which the shaft, the piston head, and biasing member are disposed. The housing includes an opening allowing fluid communication between the housing bore and the borehole fluid external to the housing.
It should be understood that examples certain features of the disclosure have been summarized rather broadly in order that the detailed description thereof that follows may be better understood, and in order that the contributions to the art may be appreciated. There are, of course, additional features of the disclosure that will be described hereinafter and which will in some cases form the subject of the claims appended thereto.
For detailed understanding of the present disclosure, references should be made to the following detailed description of the preferred embodiment, taken in conjunction with the accompanying drawings, in which like elements have been given like numerals and wherein:
The present disclosure relates to firing heads for detonating downhole tools. The present disclosure also relates to systems and related methods for transferring signals between two or more downhole tools. The transferred signals may be used to activate one or more of these downhole tools. Exemplary signals may be in the form of kinetic energy, thermal energy, pressure pulses, etc. Signal transfer systems according to the present disclosure receive a signal at one downhole location and transfer that signal to another downhole location. The present disclosure is susceptible to embodiments of different forms. There are shown in the drawings, and herein will be described in detail, specific embodiments of the present disclosure with the understanding that the present disclosure is to be considered an exemplification of the principles of the disclosure, and is not intended to limit the disclosure to that illustrated and described herein.
Referring to
In one embodiment, the signal transfer assembly 100 may include a first detonator cord 32, a propellant assembly 34, a piston chamber sub 35, a connector tube 36, a firing head assembly 38, a detonator 40, and a second detonator cord 42. The detonator cords 32, 42 are formed of conventional energetic material used to detonate shaped charges (not shown). It should be noted that in some arrangements, the detonator cords 32, 42 may be a part of the perforating guns 20, 30. The detonator 40 may be formed of one or more high-explosives, such as RDX (Hexogen, Cyclotrimethylenetrinitramine), HMX (Octogen, Cyclotetramethylenetetranitramine), CLCP, HNS, and PYX. Generally, suitable high-explosives generate a supersonic pressure pulse when detonated.
The propellant assembly 34 may include a propellant charge 46 formed of an energetic material that generates a high-pressure gas upon activation (e.g., deflagration). The gas is of sufficient volume and high pressure to break one or more frangible elements 53 that retain the piston 48 and propel a piston 48 into a bore 37 of the piston chamber sub 35. The piston chamber sub 35 is a tubular member configured to “catch” and retain the piston 48. Suitable materials for propellants may be formed of one or more of ammonium perchlorate, ammonium nitrate, black powder, etc. In contrast, to high-explosives, propellant material is formulated to burn, or “deflagrate,” such that the pressure pulse of the generated gas is subsonic.
The bore 50 of the connector tube 36 is in fluid communication with the bore 37 of the piston chamber sub 35 and with wellbore fluids (not shown) surrounding the well tool 10 via ports 52, 54. When in the borehole, wellbore fluids fill the bore 50 and form a liquid column that hydraulically connects the propellant assembly 34 with the firing head assembly 38. Thus, when the piston 48 moves into the bore 37, a pressure pulse is applied via the bore 50 to the firing head assembly 38. Accordingly, the propellant assembly 34 may be considered a fluid mover; e.g., a device configured to displace fluid toward the firing head assembly 38.
Referring to
In one embodiment, the pin assembly 62 includes a shaft 66, a piston head 68, a biasing member 70, and one or more frangible members 72. The shaft 66 may be a solid cylinder having a nose 74, a terminal end 76, and annular first and second shoulders 80, 82. The shoulders 80, 82 may be raised surfaces or projections extending from an outer surface of the shaft 66 that present surfaces that can block axial movement. The axial direction is defined as along the direction the shaft 66 translates. The piston head 68 may be an annular disk shaped body that can slide along the shaft 66 and is retained between a retaining element 78 positioned at the terminal end 76 and the first shoulder 80. The retaining element 78 may be a nut, washer, flange, or other radially enlarged projection formed or attached to the terminal end 76. In some embodiments, the retaining element 78 may be omitted. The biasing member 70, which may be a spring, surrounds the shaft 66 and biases the piston head 68 toward the retaining element 78. In one arrangement, the biasing member 70 is retained between the second shoulder 82 and the piston head 68.
The frangible members 72 may be used to selectively secure the shaft 66 to the outer housing 60. By “selectively,” it is meant that the shaft 66 is stationary relative to the outer housing 60, and therefore does not impact the detonator 40 until a predetermined amount of pressure is applied to the pin assembly 62. The frangible members 72 may be bodies such as shear pins that are intentionally constructed to break when subjected to a predetermined loading. The frangible member(s) 72 may also be formed as shoulders, flanges, or other features that connect, either directly or indirectly, the shaft 66 to the housing 60.
Referring to
Referring to
Referring to
Referring now to
The repeater assembly 130 includes a first propellant assembly 160, a first piston chamber sub 162, a first connector tube 164, and a first firing head 146. The signal transfer assembly 140 includes a second propellant assembly 152, a second piston chamber sub 154, a second connector tube 156, and a second firing head 158. The details of these components have already been discussed above.
During use, firing the first perforating gun 20 initiates the detonator cord 32, which activates the first propellant assembly 160 to generate a high-pressure gas. In a manner previously described, this high-pressure gas enables the propellant assembly 160 to create a pressure pulse in the liquid column in the first connector sub 164. Upon encountering the pressure pulse, the first firing head 146 activates the second propellant assembly 152, which creates another pressure pulse in the second connector tube 156. The second firing head 158 responds to this second pressure pulse by activating the detonator 40. The detonator 40 fires the second perforating gun 30 in a conventional manner.
Thus, in the
In the
Referring to
The firing head assembly 38 may be used to fire a perforating gun as previously described. More generally, the firing head 38 may be used to activate any downhole device 186 that can change operating states in response to an impact or pressure pulse. Illustrative devices include, but are not limited to, perforating guns, power charge activated setting tools, and tubing or casing cutters. If a setting tool is run, then the detonator 40 will be replaced with an igniter.
Referring to
In one embodiment, the well perforating system 190 may include perforating gun sets 200a-e and detonation transfer assemblies 220a-d conveyed by a work string 195. The length of each gun set 200a-e is selected to best match the associated zone 210a-e. The length of each signal transfer assembly 220a-d is selected to position each gun set 200a-e at the associated zone 210a-e. In the formation illustrated, detonation transfer assemblies 220a and 220b each have two repeater units because of the distances separating formations 210a,b,c. The distance separating formation 210c and 210d is relatively shorter. Therefore, the signal transfer assembly 220c has only one repeater unit. The distance separating formation 210d and 210e is the longest and requires the signal transfer assembly 220d to have three repeater units.
The work string 195 may be coiled tubing or drill pipe. In other arrangements, the work string 195 may be electric wireline, slickline, or other rigid or non-rigid carriers.
In an exemplary use, the formation traversed by the wellbore 192 is logged to determine the location of each of the zones 210a-e. Conventionally, the locations are with reference to the “measured depth,” which the distance along the wellbore 192. Thereafter, the perforating system 190 is assembled to position each of the perforating gun sets 200a-e at an associated zone 210a-e. Next, the perforating assembly 190 is conveyed into the wellbore and positioned using the information acquired from the prior logging and information being acquired while conveying. Referring to
Once properly positioned, a firing signal is sent to detonate the first perforating gun 200a. The firing of the first perforating gun 200a is transmitted via the first detonation transfer unit 220a to the second gun set 200b. The firing of the second gun set 200b is transmitted via the second detonation transfer unit 220b to the third gun set 200c. The firing signals are conveyed in this manner until the final gun set 200e is fired. It should be appreciated that the formations 210a-e have all been perforated at the same time and while the perforating system 190 is stationary in the wellbore 192. If present, time delay fuses would have inserted delays between the firings. Thereafter, the entire perforating system 190 may be retrieved from the wellbore 192.
Referring to
Different from the
The shifting sleeve 280 may be a tubular member having an outer circumferential surface 281 and an inner circumferential surface 284 that defines a passage 286. The passage 286 has a sufficiently large diameter to allow the piston head 268 to translate at least partially through the shifting sleeve 280. In a pre-activated position, the frangible member 272 prevents the shaft 266 from sliding axially toward the detonator 40. The frangible member 272 may be a shear flange or other inwardly projecting portion of the shifting sleeve 280. The frangible member 272 may interferingly engage a shoulder 273 formed on the shaft 266 to stop axial movement toward the detonator 40 The outer surface 282 includes sealing members 288.
The sleeve 280 translates within a bore section 290 from a pre-activated position shown in
The shifting sleeve 280 is displaced from the pre-activated position to the activated position using ambient wellbore fluid pressure. In one embodiment, the housing 260 may include a fluid path 300 that connects a bore section 302 in which the pin shaft 266 slides axially. The fluid path 300 is in fluid communication with one or more passages 304, each of which includes a piston 306. Each piston 306 includes a pressure face 308 in fluid communication with the fluid path 300 via the passage 304 and a contact end 310 for physically contacting the shifting sleeve 280. The pistons 306 translates from a pre-activated position shown in
Referring to
It should be noted that the seals 92 disposed on the pin shaft 266 provide selective fluid tight sealing for the fluid path 300. As shown in
Referring to
For brevity, the various details of the response of the pin assembly 262 to an applied pressure pulse will not be described as the response is generally similar to that described in connection with the
Referring to
Referring to
In embodiments, the seal at the shoulder 363 is directionally sensitive. The biasing member 282 provides a biasing force that urges the piston head 268 to the shoulder 262. For a seal to be made, the biasing force combined with the fluid pressure in the bore 264 must be greater than the fluid pressure in the adjacent bore 350 in which the annular shoulder 363 is positioned. Specifically, the pressure differential must be sufficiently large to axially displace the piston head 268 toward the shoulder 363 and activate the sealing member 368. If a pressure differential of sufficient magnitude does not exist, then fluid-tight seal may not be formed. Moreover, if the pressure in the adjacent bore 350 is greater than the pressure in the bore 264 in an amount to overcome the biasing force of the biasing member 282, then the piston head 268 is displaced away from the shoulder 363.
Referring to
In the context of the present disclosure, a detonation is a supersonic combustion reaction. Whereas a burn or deflagration is a subsonic combustion reaction. High explosives (RDX, HMX, etc.) will detonate. Low explosives such as propellant will deflagrate. Therefore, when the propellant burns (deflagrates) it creates a subsonic pressure pulse that may be used to propel the piston and generate a pressure pulse through the tubing to activate the next firing head.
The foregoing description is directed to particular embodiments of the present disclosure for the purpose of illustration and explanation. It will be apparent, however, to one skilled in the art that many modifications and changes to the embodiment set forth above are possible without departing from the scope of the disclosure. It is intended that the following claims be interpreted to embrace all such modifications and changes.
This application claims priority from U.S. Provisional Application Ser. No. 62/674,390, filed May 21, 2018, the entire disclosure of which is incorporated herein by reference in its entirety.
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Entry |
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Owen Oil Tools, Core Lab, “Differential Safety Firing Assembly,” Ball Activated Differential Safety Firing Assembly Low Pressure TC-022-2375-000 R01; pp. 32-34. |
Owen Oil Tools, Core Lab, Differential Filing Head 3-1/8 inch, TC-025-2375-000; MAN-TC-025(R06), 2009, 2014, pp. 1-12. |
Number | Date | Country | |
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20190353015 A1 | Nov 2019 | US |
Number | Date | Country | |
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62674390 | May 2018 | US |