US3528512A - Sealing off a firing chamber in a perforating tool - Google Patents
Sealing off a firing chamber in a perforating tool Download PDFInfo
- Publication number
- US3528512A US3528512A US793391*A US3528512DA US3528512A US 3528512 A US3528512 A US 3528512A US 3528512D A US3528512D A US 3528512DA US 3528512 A US3528512 A US 3528512A
- Authority
- US
- United States
- Prior art keywords
- seat
- sealing
- chamber
- projectile
- chambers
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 238000007789 sealing Methods 0.000 title description 43
- 238000010304 firing Methods 0.000 title description 17
- 239000002360 explosive Substances 0.000 description 45
- 239000004020 conductor Substances 0.000 description 28
- 238000005192 partition Methods 0.000 description 16
- 238000005474 detonation Methods 0.000 description 15
- 230000015572 biosynthetic process Effects 0.000 description 12
- 238000005755 formation reaction Methods 0.000 description 12
- 230000000694 effects Effects 0.000 description 11
- 239000000463 material Substances 0.000 description 11
- 239000012530 fluid Substances 0.000 description 9
- 238000004891 communication Methods 0.000 description 6
- 230000006872 improvement Effects 0.000 description 5
- 229910052751 metal Inorganic materials 0.000 description 5
- 239000002184 metal Substances 0.000 description 5
- 238000000034 method Methods 0.000 description 5
- 239000010425 asbestos Substances 0.000 description 3
- 238000010276 construction Methods 0.000 description 3
- 239000000835 fiber Substances 0.000 description 3
- 229910052895 riebeckite Inorganic materials 0.000 description 3
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 230000009545 invasion Effects 0.000 description 2
- 238000002955 isolation Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 229910001369 Brass Inorganic materials 0.000 description 1
- 239000004215 Carbon black (E152) Substances 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 229910001209 Low-carbon steel Inorganic materials 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 229910001347 Stellite Inorganic materials 0.000 description 1
- 230000001154 acute effect Effects 0.000 description 1
- 239000010951 brass Substances 0.000 description 1
- 239000004568 cement Substances 0.000 description 1
- AHICWQREWHDHHF-UHFFFAOYSA-N chromium;cobalt;iron;manganese;methane;molybdenum;nickel;silicon;tungsten Chemical compound C.[Si].[Cr].[Mn].[Fe].[Co].[Ni].[Mo].[W] AHICWQREWHDHHF-UHFFFAOYSA-N 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 229930195733 hydrocarbon Natural products 0.000 description 1
- 150000002430 hydrocarbons Chemical class 0.000 description 1
- 230000002706 hydrostatic effect Effects 0.000 description 1
- 238000011065 in-situ storage Methods 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 150000003839 salts Chemical class 0.000 description 1
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 1
- 229910010271 silicon carbide Inorganic materials 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
-
- E—FIXED CONSTRUCTIONS
- E21—EARTH OR ROCK DRILLING; MINING
- E21B—EARTH OR ROCK DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
- E21B43/00—Methods or apparatus for obtaining oil, gas, water, soluble or meltable materials or a slurry of minerals from wells
- E21B43/11—Perforators; Permeators
- E21B43/116—Gun or shaped-charge perforators
Definitions
- This specification also discloses a specific construction of apparatus in which retaining means is provided behind the projectile and in which a preferred projectile comprises:
- This invention relates to perforating tools. More particularly, it relates to perforating tools such as are employed in establishing communication through casing between a well bore and subterranean formations.
- FIG. 1 is a view partly in section and partly schematic of a down hole perforating tool employing one embodiment of the invention.
- FIG. 2 is a longitudinal cross-section of a sealing partition employed in one embodiment of the invention.
- FIG. 3 is a lateral cross-sectional view along the lines III-III of FIG. 2.
- FIGS. 4 and 5 are side views, partly in section, showing the sealing projectile in place before and after detonation of an explosive charge in accord with one embodiment of the invention.
- the improvement comprises:
- an improvement in a down hole tool for establishing communication through a casing from a Well bore into a subterranean formation by detonating an explosive charge within one of a plurality of chambers in the tool comprises:
- FIG. 1 illustrates apparatus for establishing communication through a casing 11 from a wall bore filled with fluid 13 into subterranean formation 15.
- tool 17 has a plurality of chambers 19 and 21.
- perforating means including explosive charges 23, are set to perforate into the formation.
- perforating means including explosive charges 25, are also set to perforate into the formation.
- Explosive charges 23 are detonated by appropriate detonating means, such as Primacord 27.
- second detonating means such as Primacord 29, serves to detonate explosive charges 25.
- a DC power source 31 may be connected by conductors 33 and 35 via a stepping switch 37 with Primacord 27 and explosive charge 23.
- Conductor means, such as conductors 33 and 35, are carried inside cable 39 which ordinarily has a tensile load bearing member in addition to the conductors. Cable 39 may have an exterior armored portion which will serve as a ground for the conductor means if desired.
- tool 17 is introduced into the well through a lubricator to maintain the well pressure, especially after perforating.
- Cable 39, suspending tool 17, is lowered over a sheave and is lowered into and withdrawn from the well in response to winching means.
- depth measuring means may be employed in connection with cable 39 and its supporting sheave to position tool 17 in order to effect perforations at exactly the desired depth in the subterranean formation 15.
- the lubricator, sheave, winching means and depth measuring means are well known, and do not form any part of this invention and, hence, need not be described herein.
- Partition means 41 is interposed between chamber 19 and chamber 21.
- Partition means 41 is sealingly connected with wall 43 of chamber 19 and with wall 45 of chamber 21.
- the connection may be effected by any means; such as, threaded bolts 47 having countersunk, recessed heads and passing through the respective walls and into the partition means having an aperture 49 tapped with matching threads, shown in greater detail in FIG. 2.
- the sealing may be effected by any means, such as O-rings 51 mounted in grooves 53 and interposed between partition means 41 and the walls 43 and 45 of the respective chambers 19 and 21.
- Passageway 55 penetrates longitudinally through partition means 41.
- the conductor means passing through passageway 55 connects explosive charges 23 with the firing means.
- Seat 57 is formed in the passageway. Ordinarily, seat 57 is formed by reaming to a particular dimension for a depth; for example, about 1 inch; into passageway 55. If desirable, seat 57 may be coated by a hard coating, such as silicon carbide or Stellite.
- Sealing projectile 59 is positioned adjacent seat 57 such that it is between seat 57 and explosive charges 23 (FIG. 1)
- threaded apertures 49 do not penetrate through the sidewall of the partition means to passageway 55;hence, there is no problem of communication of fluids between the well bore and passageway 55 except by way of chamber 19 following detonation of explosive charges 23.
- the components are assembled in tool 17 as described hereinbefore. Thereafter, tool 17 is lowered, via cable 39 into well bore 13 to the depth interval to be perforated.
- Stepping switch 37 is stepped onto conductor 33. This detonates Primacord 27, also detonating explosive charges 23 in chamber 19. The detonation of the explosive charges 23 and Primacord 27 simultaneously perforates through casing 11 into subterranean formation 15, and drives sealing projectile 59 deeply into seat 57 to isolate firing chamber 19. Thereafter, the gases liberated by detonation of explosive charges 23 are dispelled through openings in chamber 19 into well bore 13.
- Sealing projectile 59 in being driven into seat 57, severs conductor 33 and seals against seat 57. In this way, misfiring of explosive charges 25 in chamber 21 is prevented, either by damage from the detonation gases or from subsequent invasion of fluids from the pressurized well bore 13 into chamber 21.
- Stepping switch 37 can be stepped onto conductor 63, which, via its connection with DC power source through conductor 65, detonates Primacord 29; in turn, (1) detonating explosive charges 25, (2) isolating chamber 21 by driving its sealing projectile into its seat, and (3) perforating into the formation.
- any number of chambers may be fired successively to effect perforation over the desired interval by employing this embodiment of the invention.
- Back up material 65 functions to help retain sealing projectile 59 in place adjacent seat 57 and aligned therewith before the detonation of charges 23; helps ensure that a maximum pressure is applied to the frustum base portion of sealing projectile 59 to drive it deeply into seat 57; and disintegrates to fill any voids that might occur, block blow-by of any detonation gasses, and effect complete sealing.
- Back up material 65 is composed of short asbestos fiber formed into a disc. The asbestos fiber withstands high temperature and yet disintegrates readily because of its short fiber to fulfill the desired functions. Because it is asbestos, it may be pressed into retaining means 61 without harming conductors that pass therethrough.
- Sealing projectile 59 may be of any shape that will form a seal with seat 57.
- sealing projectile 59 can be in the form of a sphere or a cone.
- a cone having three sections differing in degree of taper, or slope, from the adjacent section can be employed as the sealing projectile.
- cone-shaped nose portion 69 aids in assembly and alignment, automatically dispersing conductors such as conductor 33 around the sealing projectile.
- Cone-shaped nose portion 69 need not be completed to its apex but can be frusto-conical. Its maximum diameter will be no larger than the diameter of seat 57.
- cone-shaped nose portion has a slope with respect to its longitudinal axis of between 10 and 30 degrees.
- First cylindrical portion 73 contiguous with the base of the cone-shaped nose portion 69, has a diameter substantially equal to the seat diameter.
- Second cylindrical portion 75 contiguous with first cylindrical portion 73 has a diameter slightly larger than the seat diameter.
- the diameter of the second cylindrical portion is at least 0.002 inch, preferably about 0.005
- the second cylindrical portion serves to make the projectile self aligning in order to get seal material all around the seat opening and somewhat cushion the impact of the projectile.
- the amount of metal larger than the seat must not be so great as to diminish the Wall to wall contact penetration into the seat to less than about A; inch.
- the maximum diameter will vary with the materials of construction; ordinarily, the diameter of the second cylindrical portion will be no more than about 0.010 inch larger than the seat diameter.
- a third cylindrical portion 77 contiguous with the second cylindrical portion which has a diameter similarly slightly larger than the diameter of the second cylindrical portion.
- the diameter of the third cylindrical portion is, ordinarily, 0.0020.0l inch, preferably about 0.005 inch, larger than the second cylindrical portion.
- the third cylindrical portion 77 improves the self aligning characteristics of the projectile and by the additional metal around its periphery further cushions the impact of the projectile into seat 57; yet, does not accumulate metal so rapidly as to prevent the projectile from being driven deeply into the seat for a better seal.
- a frustrum base portion 79 adjacent the last cylindrical portion, that has a minimum diameter substantially the same as the last cylindrical portion and sloping to a diameter at its base large enough to ensure that the projectile does not pass completely through the seat under the force of the explosive charge.
- the maximum diameter of the base will depend somewhat upon the material from which sealing projectile 59 is made and on the degree of slope, ordinarily, a maximum diameter of at least 50% more than the diameter of the seat is adequate to ensure that the sealing projectile does not pass completely through the seat.
- the frustum base portion has a slope of between 10 and 30 degrees with respect to its longitudinal axis.
- FIG. 5 illustrates sealing projectile 59 after it has been driven deeply into seat 57 by the detonation of explosive charges 23.
- Conductor 33 is cleanly severed.
- Excess metal 81 is driven onto the reamed seat and into any small openings thereabout to effect a complete seal that is resistant to high temperature and high pressure.
- Sealing projectile 59 may be constructed of any material that will resist the high temperature and high pressure; yet, be malleable enough to be driven deeply into the seat to effect a seal.
- the material of which the sealing projectile is constructed should be lightweight such that it would have little inertia and will be moved into sealing position quickly when the explosive charge is detonated. It should have a uniform density so as to truly align itself and properly seat into seat 57. It should withstand temperature as high as 500 degrees Fahrenheit down hole plus instantaneous temperature as high as 1000 degrees Fahrenheit. It should be capable of shear and flow; i.e., not be frangible; should have less hardness than the seat but should have high enough density and resistance to shear and flow to keep from being forced completely through the seat.
- soft, malleable metals such as, brass, copper, and mild steel may be employed. Aluminum is particularly preferred. Any other material having the desired properties can be employed.
- a specific embodiment that has been found to work well in several different tools having different diameters was the following.
- a passageway inch in diameter was drilled longitudinally through the partition means.
- a retaining means inch in diameter was drilled 1 inch deep into the passageway before the seat was formed.
- a seat inch was reamed 1 inch deeper into the passageway.
- a sealing projectile was fabricated of aluminum. It had a maximum diameter at the base of the frustum base portion of about inch.
- T he'frustum base portion had a slope of about 13 degrees with respect to its longitudinal axis.
- the cone-shaped nose portion had a slope of about 15 degrees with respect to its longitudinal axis and had a maximum diameter of 0.328 inch.
- the first cylindrical portion had a diameter of 0.328 inch and a length of 1.4 inch.
- the second cylindrical portion had a diameter of 0.333 inch and a length of inch.
- the third cylindrical portion had a diameter of 0.338 inch and a length of inch.
- the overall length of the sealing projectile was 1% inch, affording /2 inch each for the cone-shaped nose portion and the frustum base portion.
- the invention provides a method of effecting a seal in situ, using the explosive force of the detonation of an explosive charge, to effect a seal that is resistant to high temperatures and to pressures in excess of 4,500 psi.
- the seal alleviates difiiculties with blow-by of fluid, either during the detonation or from the well bore fluids following the detonation, that could cause misfiring of the explosive charges in the remaining chambers.
- the invention effects a cost reduction by cutting the labor costs on loading and assembling the gun in half, reducing the material cost for the seal itself to about the former cost and reduces the manufacturing cost for the sub-assembly by about 20%.
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- Life Sciences & Earth Sciences (AREA)
- Engineering & Computer Science (AREA)
- Geology (AREA)
- Mining & Mineral Resources (AREA)
- Physics & Mathematics (AREA)
- Environmental & Geological Engineering (AREA)
- Fluid Mechanics (AREA)
- General Life Sciences & Earth Sciences (AREA)
- Geochemistry & Mineralogy (AREA)
- Portable Nailing Machines And Staplers (AREA)
Description
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US79339169A | 1969-01-23 | 1969-01-23 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3528512A true US3528512A (en) | 1970-09-15 |
Family
ID=25159813
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US793391*A Expired - Lifetime US3528512A (en) | 1969-01-23 | 1969-01-23 | Sealing off a firing chamber in a perforating tool |
Country Status (1)
Country | Link |
---|---|
US (1) | US3528512A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4089381A (en) * | 1976-02-26 | 1978-05-16 | Gearhart-Owen Industries, Inc. | Chamber isolator and sealing means for borehole perforating tools |
US20180135389A1 (en) * | 2016-11-17 | 2018-05-17 | Geodynamics, Inc. | Switch sub with two way sealing features and method |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3010396A (en) * | 1957-12-31 | 1961-11-28 | Western Co Of North America | Selective firing apparatus |
US3246707A (en) * | 1964-02-17 | 1966-04-19 | Schlumberger Well Surv Corp | Selective firing system |
US3327792A (en) * | 1965-10-22 | 1967-06-27 | Profitable Resources Inc | Jet perforating gun |
US3441093A (en) * | 1967-06-19 | 1969-04-29 | Profitable Resources Inc | Jet perforating gun arming switch and circuitry |
-
1969
- 1969-01-23 US US793391*A patent/US3528512A/en not_active Expired - Lifetime
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3010396A (en) * | 1957-12-31 | 1961-11-28 | Western Co Of North America | Selective firing apparatus |
US3246707A (en) * | 1964-02-17 | 1966-04-19 | Schlumberger Well Surv Corp | Selective firing system |
US3327792A (en) * | 1965-10-22 | 1967-06-27 | Profitable Resources Inc | Jet perforating gun |
US3441093A (en) * | 1967-06-19 | 1969-04-29 | Profitable Resources Inc | Jet perforating gun arming switch and circuitry |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4089381A (en) * | 1976-02-26 | 1978-05-16 | Gearhart-Owen Industries, Inc. | Chamber isolator and sealing means for borehole perforating tools |
US20180135389A1 (en) * | 2016-11-17 | 2018-05-17 | Geodynamics, Inc. | Switch sub with two way sealing features and method |
US11208873B2 (en) * | 2016-11-17 | 2021-12-28 | Bakken Ball Retrieval Llc | Switch sub with two way sealing features and method |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: MBANK HOUSTON NATIONAL ASSOCIATION Free format text: SECURITY INTEREST;ASSIGNOR:CRUTCHER RESOURCES CORPORATION, A DE. CORP.;REEL/FRAME:004570/0273 Effective date: 19850529 Owner name: PRUDENTIAL INSURANCE COMPANY OF AMERICA THE Free format text: SECURITY INTEREST;ASSIGNOR:CRUTCHER RESOURCES CORPORATION, A DE. CORP.;REEL/FRAME:004570/0273 Effective date: 19850529 Owner name: TEXAS COMMERCE BANK NATIONAL ASSOCIATION, AND Free format text: SECURITY INTEREST;ASSIGNOR:CRUTCHER RESOURCES CORPORATION, A DE. CORP.;REEL/FRAME:004570/0273 Effective date: 19850529 Owner name: CITIBANK, N.A. Free format text: SECURITY INTEREST;ASSIGNOR:CRUTCHER RESOURCES CORPORATION, A DE. CORP.;REEL/FRAME:004570/0273 Effective date: 19850529 Owner name: CHASE MANHATTAN BANK THE (NATIONAL ASSOCIATION) Free format text: SECURITY INTEREST;ASSIGNOR:CRUTCHER RESOURCES CORPORATION, A DE. CORP.;REEL/FRAME:004570/0273 Effective date: 19850529 Owner name: FIRST CITY NATIONAL BANK OF HOUSTON Free format text: SECURITY INTEREST;ASSIGNOR:CRUTCHER RESOURCES CORPORATION, A DE. CORP.;REEL/FRAME:004570/0273 Effective date: 19850529 Owner name: TORONTO-DOMINION ATLANTA AGENCY THE Free format text: SECURITY INTEREST;ASSIGNOR:CRUTCHER RESOURCES CORPORATION, A DE. CORP.;REEL/FRAME:004570/0273 Effective date: 19850529 |
|
AS | Assignment |
Owner name: MBANK HOUSTON NATIONAL ASSOCIATION Free format text: SECURITY INTEREST;ASSIGNOR:CRC WIRELINE, INC., A CORP OF DE.;REEL/FRAME:004573/0123 Effective date: 19850529 Owner name: TEXAS COMMERCE BANK NATIONAL ASSOCIATION Free format text: SECURITY INTEREST;ASSIGNOR:CRC WIRELINE, INC., A CORP OF DE.;REEL/FRAME:004573/0123 Effective date: 19850529 Owner name: FIRST CITY NATIONAL BANK OF HOUSTON Free format text: SECURITY INTEREST;ASSIGNOR:CRC WIRELINE, INC., A CORP OF DE.;REEL/FRAME:004573/0123 Effective date: 19850529 Owner name: PRUDENTIAL INSURANCE COMPANY OF AMERICA THE Free format text: SECURITY INTEREST;ASSIGNOR:CRC WIRELINE, INC., A CORP OF DE.;REEL/FRAME:004573/0123 Effective date: 19850529 Owner name: CHASE MANHATTAN BANK THE (NATIONAL ASSOCIATION) Free format text: SECURITY INTEREST;ASSIGNOR:CRC WIRELINE, INC., A CORP OF DE.;REEL/FRAME:004573/0123 Effective date: 19850529 Owner name: TORONTO-DOMINION BANK ATLANTA AGENCY Free format text: SECURITY INTEREST;ASSIGNOR:CRC WIRELINE, INC., A CORP OF DE.;REEL/FRAME:004573/0123 Effective date: 19850529 Owner name: CITIBANK, N.A. Free format text: SECURITY INTEREST;ASSIGNOR:CRC WIRELINE, INC., A CORP OF DE.;REEL/FRAME:004573/0123 Effective date: 19850529 |