WO2002075099A2 - Heavy metal oil well perforator liner - Google Patents
Heavy metal oil well perforator liner Download PDFInfo
- Publication number
- WO2002075099A2 WO2002075099A2 PCT/US2002/007028 US0207028W WO02075099A2 WO 2002075099 A2 WO2002075099 A2 WO 2002075099A2 US 0207028 W US0207028 W US 0207028W WO 02075099 A2 WO02075099 A2 WO 02075099A2
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- liner
- shaped charge
- charge according
- heavy metal
- mixture
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B1/00—Explosive charges characterised by form or shape but not dependent on shape of container
- F42B1/02—Shaped or hollow charges
- F42B1/032—Shaped or hollow charges characterised by the material of the liner
Definitions
- a shaped charge suitable for use in a perforating tool for a subterranean well is described.
- the invention relates particularly to an improved shaped charge liner constructed from powdered heavy metal and binder material with a high proportion of tungsten or similar heavy metal.
- a subterranean gas or oil well typically begins with a hole bored into the earth, which is then lined with joined lengths of relatively large diameter metal pipe.
- the casing thus formed is generally cemented to the face of the hole to give the well integrity and a path for producing fluids to the surface.
- the casing and cement are subsequently perforated with chemical means, commonly explosives, in one or more locations of the surrounding formation from which it is desired to extract fluids.
- the perforations extend a distance into the formation.
- Explosive shaped charges known in the art generally have a substantially cylindrical or conical shape and are used in various arrangements in perforating tools in subterranean wells.
- a tubular perforating gun adapted for insertion into a well is used to carry a plurality of shaped charges to a subsurface location where perforation is desired.
- explosive jets emanate from the shaped charges with considerable velocity and perforate the well casing and surrounding formation.
- Liners of shaped charges have commonly been designed in an effort to maximize penetration depth.
- Various metals have been used.
- Solid metal liners have the disadvantage of introducing metal fragments into the formation, detracting from the effectiveness of the perforation.
- Compressed powdered metal liners have sometimes been used. Such liners disintegrate upon detonation of the shaped charge, avoiding the problems associated with metal fragments.
- heavy metals are particularly suited for use in liners. Generally, the heavy metal is combined with one or more other metals with suitable binding characteristics to form rigid liners through very high compression of the metal powders.
- One of the principal problems in the art has been the attempt to increase the heavy metal content of liners.
- the inventions provide shaped charge apparatus for use in a subterranean well.
- the inventions contemplate an improved liner for a shaped charge constructed from a combination mixture of a high proportion of powdered heavy metal and selected binder metal.
- a mixture of powdered tungsten and powdered metal binder is formed into a rigid shaped charge liner having a tungsten content in a range of between approximately 90% to 99.98% by weight.
- a liner having a tungsten content in a range of between approximately 90% to 99.98% by weight is constructed of a binder metal-coated heavy metal powder formed into a rigid body.
- a liner for a shaped charge is constructed from a mixture of powdered tungsten and powdered metal binder blended with a binder metal-coated heavy metal powder formed into a substantially conical rigid body.
- the resulting liner having a tungsten metal content in a range of between approximately 93% to 99.98% by weight.
- FIGURE 1 is a side elevation view of an example of an axially symmetrical shaped charge in accordance with the invention
- FIGURE 2 is cross-sectional view taken along line 2-2 of Figure 1 showing an example of an embodiment of a shaped charge in accordance with the inventions.
- FIG. 1 A conically symmetrical shaped charge 10 is shown.
- the shaped charge is sized for a perforating gun commonly used to perforate subterranean wells and formations.
- a plurality of shaped charges are arranged in a substantially helical pattern on the perforating gun assembly.
- the exact size and shape of the shaped charge or the configuration of the perforating gun are not critical to the invention.
- the shaped charge 10 is enclosed by a case 12.
- the case 12 is substantially cylindrical or conical.
- the term "conical” is used to refer to shapes substantially conical or in the form of frustum or truncated cone.
- the perforating gun (not shown) is placed in a subterranean location where perforation of the well casing and/or formation is desired, herein designated the target 14.
- the shaped charge has a muzzle 16, which is oriented toward the target 14, and an opposing closed end 18.
- the case 10 is shown in cross section, revealing that the closed end 18 has a relatively small aperture 20 connected to a detonation cord 22.
- the detonation cord 22 is typically operably connected to a detonation circuit system (not shown) known in the art.
- the case 10 contains a predetermined amount of high explosives 24 generally known in the arts, for example, RDX, HMX, HNS, CL-20, NONA, BRX, PETN, or PYX.
- a substantially conical liner 26 is disposed inside of case 12 between the high explosive 24 and the muzzle 16, preferably such that the high explosive 24 fills the volume between the casing 12 and the liner 26.
- the liner is typically affixed to the case with adhesive (not shown), but a retaining ring or spring may also be used.
- the liner 26 Upon detonation of the high explosive 24, the liner 26 disintegrates and the liner material is propelled through the muzzle 16 into the target 14.
- the liner 26 is preferably constructed by compressing a powdered heavy metal and powdered metal binder material under very high pressure to form a rigid body.
- the process of compressively forming the liner from powdered heavy metal and powdered metal binder is understood by those skilled in the arts. Other methods of fabrication, such as sintering may be used.
- the powdered heavy metal is preferably tungsten, but may be another metal or mixture of metals. Metals with high density, high ductility, and capable of achieving high acoustic velocity are preferred. Metals chosen from the group tungsten, tantalum, hafnium, and copper are particularly suitable. Although other metals may be used, cost is often a major factor.
- the percentage of heavy metal, preferably tungsten, in the liner is within a range of approximately 99.0% to 99.98% by weight.
- percentages within a range of approximately 90.0% to 99.98% may be used.
- the binder metal is chosen for its ability to bind together under high levels of compression. Typically, metals chosen from the group copper, lead, zinc, tin, and bismuth are used.
- the percentage of powdered binder metal, preferably lead, in the mixture is preferably within a range of approximately 0.02% to 1.0% by weight, although percentages within a range of approximately 0.02% to 10.0% may be used.
- mixtures of binder metals or alloys such as those containing relatively high levels of tin or zinc may be used.
- the liner 26 may also contain approximately 0.2% to 1.0% lubricant by weight.
- Powdered graphite is a preferred lubricant known in the arts, although oils may also be used. Some oils such as linseed oil or rung oil, or other unsaturated organic compounds as disclosed in United States Patent Number 4,794,990, which is incorporated in its entirety for all purposes by this reference, are thought to be helpful in preventing corrosion of the liner.
- the presently most preferred embodiment of the invention uses a liner 236 constructed from a heavy metal powder coated with a binder metal, a binder metal-coated heavy metal powder compressively formed into a rigid body. The process of coating the heavy metal powder with a binder metal is understood by those skilled in the arts.
- the heavy metal powder, coated with a binder metal is then compressed under very high pressure into a rigid body.
- tungsten and lead are preferred for the heavy metal and binder metal coating, respectively, although the alternative metals described above may be used. Combinations of metals may also be used.
- the percentage of tungsten in the liner is within a range of approximately 99.0% to 99.98% by weight, although percentages within a range of approximately 90.0% to 99.98% may be used.
- the percentage of led in the mixture is preferably within a range of approximately 0.02% to 1.0% by weight, although percentages within a range of approximately 0.2% to 10.0% may optionally be used.
- An additional alternative embodiment of the invention uses a liner 26, which is construed of a combination of the elements of the first two embodiments described. That is, a mixture of heavy metal powder and powdered binder metal may be used in combination with binder metal-coated heavy metal powder to construct the liner 26. The same proportions and variations in ingredients described with reference to the first two embodiments may be employed with this additional embodiment as well.
- the invention has many advantages attendant with raising the percentage of heavy metal in the liner to higher levels than have been known in the art.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Prevention Of Electric Corrosion (AREA)
- Powder Metallurgy (AREA)
Abstract
Description
Claims
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
MXPA03008304A MXPA03008304A (en) | 2001-03-16 | 2002-03-08 | Oil well perforator liner with high proportion of heavy metal. |
AU2002252234A AU2002252234A1 (en) | 2001-03-16 | 2002-03-08 | Heavy metal oil well perforator liner |
CA002440306A CA2440306A1 (en) | 2001-03-16 | 2002-03-08 | Oil well perforator liner with high proportion of heavy metal |
DE10296518T DE10296518T5 (en) | 2001-03-16 | 2002-03-08 | Oil well borehole feed with a high proportion of heavy metal |
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/810,966 US6588344B2 (en) | 2001-03-16 | 2001-03-16 | Oil well perforator liner |
US09/810,966 | 2001-03-16 | ||
US09/810,792 US20020129726A1 (en) | 2001-03-16 | 2001-03-16 | Oil well perforator liner with high proportion of heavy metal |
Publications (3)
Publication Number | Publication Date |
---|---|
WO2002075099A2 true WO2002075099A2 (en) | 2002-09-26 |
WO2002075099A8 WO2002075099A8 (en) | 2003-01-16 |
WO2002075099A3 WO2002075099A3 (en) | 2003-12-11 |
Family
ID=29587248
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2002/007028 WO2002075099A2 (en) | 2001-03-16 | 2002-03-08 | Heavy metal oil well perforator liner |
Country Status (1)
Country | Link |
---|---|
WO (1) | WO2002075099A2 (en) |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4958569A (en) * | 1990-03-26 | 1990-09-25 | Olin Corporation | Wrought copper alloy-shaped charge liner |
DE3729780A1 (en) * | 1987-09-05 | 1993-05-19 | Battelle Institut E V | Increasing the penetration of projectile shaped charges - involves using tungsten@-based, and therefore denser, projectile casing to give increased projectile kinetic energy and higher penetration capacity |
US5259317A (en) * | 1983-11-12 | 1993-11-09 | Rheinmetall Gmbh | Hollow charge with detonation wave guide |
US5279228A (en) * | 1992-04-23 | 1994-01-18 | Defense Technology International, Inc. | Shaped charge perforator |
US5567906A (en) * | 1995-05-15 | 1996-10-22 | Western Atlas International, Inc. | Tungsten enhanced liner for a shaped charge |
US5656791A (en) * | 1995-05-15 | 1997-08-12 | Western Atlas International, Inc. | Tungsten enhanced liner for a shaped charge |
US5827995A (en) * | 1994-06-20 | 1998-10-27 | The Ensign-Bickford Company | Reactive products having tin and tin alloy liners and sheaths |
US5939664A (en) * | 1997-06-11 | 1999-08-17 | The United States Of America As Represented By The Secretary Of The Army | Heat treatable tungsten alloys with improved ballistic performance and method of making the same |
US6354219B1 (en) * | 1998-05-01 | 2002-03-12 | Owen Oil Tools, Inc. | Shaped-charge liner |
-
2002
- 2002-03-08 WO PCT/US2002/007028 patent/WO2002075099A2/en not_active Application Discontinuation
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5259317A (en) * | 1983-11-12 | 1993-11-09 | Rheinmetall Gmbh | Hollow charge with detonation wave guide |
DE3729780A1 (en) * | 1987-09-05 | 1993-05-19 | Battelle Institut E V | Increasing the penetration of projectile shaped charges - involves using tungsten@-based, and therefore denser, projectile casing to give increased projectile kinetic energy and higher penetration capacity |
US4958569A (en) * | 1990-03-26 | 1990-09-25 | Olin Corporation | Wrought copper alloy-shaped charge liner |
US4958569B1 (en) * | 1990-03-26 | 1997-11-04 | Olin Corp | Wrought copper alloy-shaped charge liner |
US5279228A (en) * | 1992-04-23 | 1994-01-18 | Defense Technology International, Inc. | Shaped charge perforator |
US5827995A (en) * | 1994-06-20 | 1998-10-27 | The Ensign-Bickford Company | Reactive products having tin and tin alloy liners and sheaths |
US5567906A (en) * | 1995-05-15 | 1996-10-22 | Western Atlas International, Inc. | Tungsten enhanced liner for a shaped charge |
US5656791A (en) * | 1995-05-15 | 1997-08-12 | Western Atlas International, Inc. | Tungsten enhanced liner for a shaped charge |
US5567906B1 (en) * | 1995-05-15 | 1998-06-09 | Western Atlas Int Inc | Tungsten enhanced liner for a shaped charge |
US5939664A (en) * | 1997-06-11 | 1999-08-17 | The United States Of America As Represented By The Secretary Of The Army | Heat treatable tungsten alloys with improved ballistic performance and method of making the same |
US6354219B1 (en) * | 1998-05-01 | 2002-03-12 | Owen Oil Tools, Inc. | Shaped-charge liner |
Also Published As
Publication number | Publication date |
---|---|
WO2002075099A3 (en) | 2003-12-11 |
WO2002075099A8 (en) | 2003-01-16 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP1241433B1 (en) | Liner for a shaped charge | |
US11112221B2 (en) | Oil well perforators | |
US5567906A (en) | Tungsten enhanced liner for a shaped charge | |
EP1682846B1 (en) | Apparatus for penetrating oilbearing sandy formations | |
AU2008217645B2 (en) | Improvements in and relating to oil well perforators | |
EP1671013B1 (en) | Improvements in and relating to oil well perforators | |
US5656791A (en) | Tungsten enhanced liner for a shaped charge | |
US5814758A (en) | Apparatus for discharging a high speed jet to penetrate a target | |
EP1812771B1 (en) | Improvements in and relating to oil well perforators | |
CA2334552C (en) | High performance powdered metal mixtures for shaped charge liners | |
CA2409849C (en) | Shaped charges having enhanced tungsten liners | |
US20020129726A1 (en) | Oil well perforator liner with high proportion of heavy metal | |
WO2002075099A2 (en) | Heavy metal oil well perforator liner |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
AK | Designated states |
Kind code of ref document: A2 Designated state(s): AE AG AL AM AT AU AZ BA BB BG BR BY BZ CA CH CN CO CR CU CZ DE DK DM DZ EC EE ES FI GB GD GE GH GM HR HU ID IL IN IS JP KE KG KP KR KZ LC LK LR LS LT LU LV MA MD MG MK MN MW MX MZ NO NZ OM PH PL PT RO RU SD SE SG SI SK SL TJ TM TN TR TT TZ UA UG UZ VN YU ZA ZM ZW |
|
AL | Designated countries for regional patents |
Kind code of ref document: A2 Designated state(s): GH GM KE LS MW MZ SD SL SZ TZ UG ZM ZW AM AZ BY KG KZ MD RU TJ TM AT BE CH CY DE DK ES FI FR GB GR IE IT LU MC NL PT SE TR BF BJ CF CG CI CM GA GN GQ GW ML MR NE SN TD TG |
|
121 | Ep: the epo has been informed by wipo that ep was designated in this application | ||
AK | Designated states |
Kind code of ref document: C1 Designated state(s): AE AG AL AM AT AU AZ BA BB BG BR BY BZ CA CH CN CO CR CU CZ DE DK DM DZ EC EE ES FI GB GD GE GH GM HR HU ID IL IN IS JP KE KG KP KR KZ LC LK LR LS LT LU LV MA MD MG MK MN MW MX MZ NO NZ OM PH PL PT RO RU SD SE SG SI SK SL TJ TM TN TR TT TZ UA UG UZ VN YU ZA ZM ZW |
|
AL | Designated countries for regional patents |
Kind code of ref document: C1 Designated state(s): GH GM KE LS MW MZ SD SL SZ TZ UG ZM ZW AM AZ BY KG KZ MD RU TJ TM AT BE CH CY DE DK ES FI FR GB GR IE IT LU MC NL PT SE TR BF BJ CF CG CI CM GA GN GQ GW ML MR NE SN TD TG |
|
CFP | Corrected version of a pamphlet front page | ||
CR1 | Correction of entry in section i |
Free format text: PAT. BUL. 39/2002 UNDER (30) REPLACE "09/810966" BY "09/810792"; ADD "DECLARATION UNDER RULE 4.17: - OF INVENTORSHIP (RULE 4.17(IV)) FOR US ONLY." |
|
DFPE | Request for preliminary examination filed prior to expiration of 19th month from priority date (pct application filed before 20040101) | ||
WWE | Wipo information: entry into national phase |
Ref document number: 2440306 Country of ref document: CA |
|
WWE | Wipo information: entry into national phase |
Ref document number: PA/a/2003/008304 Country of ref document: MX |
|
REG | Reference to national code |
Ref country code: DE Ref legal event code: 8642 |
|
122 | Ep: pct application non-entry in european phase | ||
NENP | Non-entry into the national phase in: |
Ref country code: JP |
|
WWW | Wipo information: withdrawn in national office |
Country of ref document: JP |