IP Library › Granted Patent US 11,378,363
Granted Patent B2
US 11,378,363 · App. 16/973,672 · Granted Jul 5, 2022

Contoured liner for a rectangular slotted shaped charge

Inventors: Liam McNelis (Bonn, DE); Arash Shahinpour (Troisdorf, DE); Joerg Mueller (Bonn-Lengsdorf, DE); Joern Olaf Loehken (Troisdorf, DE)
Assignee: DynaEnergetics Europe GmbH
F42B1/028
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Quick Facts
Patent No.
US 11,378,363
App. No.
16/973,672
Granted
Jul 5, 2022
Kind
B2
Abstract

According to the exemplary disclosed embodiments, contoured, curvilinear liners for a rectangular slotted shaped charge are described. The exemplary curvilinear liners include one or more curvilinear contours. The contoured, curvilinear liners provide improved perforating performance for rectangular slotted shaped charges used in oil and gas wellbore operations such as completion and abandonment.

Claims (48)

1. A contoured liner for a shaped charge, comprising:

a first wing and a second wing, wherein

each of the first wing and the second wing includes an exterior surface that extends from a curvilinear exterior central edge to a curvilinear exterior peripheral edge,

each of the first wing and the second wing includes an interior surface that extends from a curvilinear interior central edge to a curvilinear interior peripheral edge,

the first wing and the second wing converge at an apex of the curvilinear exterior central edge, and

the interior surface is separated from the exterior surface by a thickness t;

a face surface including a first end and a second end that extends away from and is opposite the first end, wherein the face surface spans between the exterior peripheral edge and the interior peripheral edge; and

a curvilinear bottom edge including a first end and a second end that extends away from and is opposite of the first end, wherein the curvilinear bottom edge is defined by the curvilinear interior central edge;

wherein at least one of the exterior peripheral edge and the interior peripheral edge of at least one of the first wing and the second wing is concave or convex with respect to a line or plane that includes the corresponding first end of the face surface and the second end of the fact surface.

2. The contoured liner of claim 1 , wherein a cross section of the exterior surface of each of the first wing and the second wing is substantially straight, extending in one direction.

3. The contoured liner of claim 1 , wherein the curvilinear bottom edge is concave with respect to a line or plane that includes the first end of the curvilinear bottom edge and the second end of the curvilinear bottom edge.

4. The contoured liner of claim 1 , wherein the curvilinear bottom edge is convex with respect to a line or plane that includes the first end of the curvilinear bottom edge and the second end of the curvilinear bottom edge.

5. The contoured liner of claim 1 , wherein at least one of the exterior peripheral edge and the interior peripheral edge of at least one of the first wing and the second wing is concave with respect to a line or plane that includes the corresponding first end of the face surface and the second end of the face surface.

6. The contoured liner of claim 1 , wherein at least one of the exterior peripheral edge and the interior peripheral edge of at least one of the first wing and the second wing is convex with respect to a line or plane that includes the corresponding first end of the face surface and the second end of the face surface.

7. The contoured liner of claim 1 , wherein the exterior surface of each of the first wing and the second wing is curvilinear.

8. The contoured liner of claim 7 , wherein the exterior surface of each of the first wing and the second wing is concave with respect to a line or plane that includes the apex of the curvilinear exterior central edge and the corresponding face surface.

9. The contoured liner of claim 7 , wherein the exterior surface of each of the first wing and the second wing is convex with respect to a line or plane that includes the apex of the curvilinear exterior central edge and the corresponding face surface.

10. The contoured liner of claim 1 , wherein the thickness t varies along a length of at least one of the first wing and the second wing.

11. The contoured liner of claim 1 , wherein the thickness t is substantially constant along a length of at least one of the first wing and the second wing.

12. The contoured liner of claim 1 , wherein the first wing and the second wing are symmetrical about the curvilinear exterior central edge.

13. The contoured liner of claim 1 , wherein the contoured liner is formed from one or more of copper, bronze, lead, aluminum, nickel, titanium, molybdenum, tantalum, graphite, tungsten, glass, cement, high-density composite, or plastic.

14. The contoured liner of claim 1 , wherein the contoured liner is formed from at least one of a solid metal sheet, a compressed powdered metal, and a compressed powered metal alloy.

15. A shaped charge, comprising:

a shaped charge casing;

a contoured liner within the shaped charge casing; and

an explosive load between the contoured liner and the shaped charge casing, wherein the contoured liner includes a first wing and a second wing, wherein

each of the first wing and the second wing includes an exterior surface that extends from a curvilinear exterior central edge to a curvilinear exterior peripheral edge,

each of the first wing and the second wing includes an interior surface that extends from a curvilinear interior central edge to a curvilinear interior peripheral edge,

the first wing and the second wing converge at an apex of the curvilinear exterior central edge, and

the interior surface is separated from the exterior surface by a thickness t,

wherein the contoured liner further includes a face surface including a first end and a second end that extends away from and is opposite the first end, wherein the face surface spans between the exterior peripheral edge and the interior peripheral edge, and

the contoured liner further includes a curvilinear bottom edge including a first end and a second end that extends away from and is opposite of the first end, wherein the curvilinear bottom edge is defined by the curvilinear interior central edge;

wherein at least one of the exterior peripheral edge and the interior peripheral edge of at least one of the first wing and the second wing is concave or convex with respect to a line or plan that includes the corresponding first end of the face surface and the second end of the face surface.

16. The shaped charge of claim 15 , wherein the exterior surface of at least one of the first wing and the second wing is curvilinear.

17. The shaped charge of claim 16 , wherein the first wing and the second wing are symmetrical about the curvilinear exterior central edge.

18. A contoured liner for a shaped charge, comprising:

a first wing and a second wing, wherein

each of the first wing and the second wing includes an exterior surface that extends from a curvilinear exterior central edge to a curvilinear exterior peripheral edge,

each of the first wing and the second wing includes an interior surface that extends from a curvilinear interior central edge to a curvilinear interior peripheral edge,

the first wing and the second wing converge at an apex of the curvilinear exterior central edge, and

the interior surface is separated from the exterior surface by a thickness t;

a face surface including a first end and a second end that extends away from and is opposite the first end, wherein the face surface spans between the exterior peripheral edge and the interior peripheral edge; and,

a curvilinear bottom edge including a first end and a second end that extends away from and is opposite of the first end, wherein the curvilinear bottom edge is defined by the curvilinear interior central edge;

wherein:

the exterior surface of each of the first wing and the second wing is curvilinear; and

the exterior surface of each of the first wing and the second wing is concave or convex with respect to a line or plane that includes the apex of the curvilinear exterior central edge and the corresponding face surface.

19. The contoured liner of claim 18 , wherein the exterior surface of each of the first wing and the second wing is concave with respect to a line or plane that includes the apex of the curvilinear exterior central edge and the corresponding face surface.

20. The contoured liner of claim 18 , wherein the exterior surface of each of the first wing and the second wing is convex with respect to a line or plane that includes the apex of the curvilinear exterior central edge and the corresponding face surface.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 9, 2020
From: MCNELIS, LIAM; SHAHINPOUR, ARASH; MUELLER, JOERG; LOEHKEN, JOERN OLAF
To: DYNAENERGETICS GMBH & CO. KG
Reel/Frame 054597/0001 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 9, 2020
From: DYNAENERGETICS GMBH & CO. KG
To: DYNAENERGETICS EUROPE GMBH
Reel/Frame 054661/0194 →
Continuity (2)
Provisional Application 62683474 · Jun 11, 2018
Related Publication 20210254938A1 · Aug 19, 2021
Cited By (1)
US 12,644,680