Granted Patent B2

US 12,492,617 · App. 17/079,601 · Granted Dec 9, 2025

Inventors: Brenden Grove (Mansfield, TX); Courtney Ann Thain Roberts (Crowley, TX); Jason Karl Cook (Crowley, TX); Christopher C Hoelscher (Arlington, TX)

Assignee: Halliburton Energy Services, Inc.

E21B43/117E21B43/116E21B43/119

Abstract

Claims (32)

1 . A method of perforating a formation surrounding a borehole, comprising:

placing a perforating gun assembly into the borehole, the perforating gun assembly comprising a gun body comprising a gun body wall, a connector, and a shaped charge housed within the gun body wall, the gun body also comprising a longitudinal axis;

detonating the shaped charge thereby producing a shock wave in the gun body; and

attenuating the shock wave propagating through the gun body wall using a shock attenuation feature in the gun body wall, wherein the shock attenuation feature is longitudinally axially positioned intermediate the shaped charge and the connector, and wherein the shock attenuation feature is longitudinally axially spaced from the connector to decrease a stress from the shock wave communicated to the connector,

wherein the shock attenuation feature comprises more than one groove, each groove being located at a longitudinal axial position of the gun body wall and comprising a pattern of groove segments spaced circumferentially around the gun body wall.

2 . The method of claim 1 , wherein the gun body comprises more than one separate piece connected together.

3 . The method of claim 1 , further comprising a material within at least one of the grooves with an impedance different from the gun body wall, wherein the material is a solid.

4 . The method of claim 3 , wherein the at least one groove defines a depth, and wherein the material fills an entirety of the depth of the at least one groove.

5 . The method of claim 1 , wherein the stress from the shock wave comprises a tensile stress.

6 . The method of claim 5 , wherein the tensile stress comprises a peak axial tensile stress, and wherein the shock attenuation feature is configured to attenuate a simulated peak axial tensile stress of the shock wave by at least 1 Gdyn/cm 2 .

7 . The method of claim 1 , wherein placing further comprises connecting a second perforating gun assembly to the perforating gun assembly and attenuating further comprises decreasing the stress communicated from the second perforating gun assembly through the second perforating gun connector.

8 . The method of claim 7 , wherein:

placing further comprises connecting the perforating gun assembly to a conveyance using the connector; and

attenuating further comprises decreasing the stress communicated from the perforating gun assembly to the conveyance through the connector.

9 . The method of claim 1 , wherein placing further comprises connecting the perforating gun assembly to a conveyance using the connector and attenuating further comprises decreasing the stress communicated from the perforating gun assembly to the conveyance through the connector.

10 . A perforating gun assembly for use in a borehole, comprising:

a gun body comprising a longitudinal axis and:

a gun body wall comprising a shock attenuation feature;

a connector;

a shaped charge supported within the gun body wall, detonation of which produces a shock wave that propagates within the gun body;

wherein the shock attenuation feature is longitudinally axially positioned intermediate the shaped charge and the connector,

wherein the shock attenuation feature is longitudinally axially spaced from the connector and configured to attenuate the shock wave within the gun body to decrease a stress communicated to the connector,

wherein the shock attenuation feature comprises more than one groove at longitudinal axial positions of the gun body wall, groove comprising a pattern of groove segments spaced circumferentially around the gun body wall.

11 . The perforating gun assembly of claim 10 , wherein the gun body comprises more than one separate piece connected together.

12 . The perforating gun assembly of claim 10 , further comprising a material within at least one of the grooves with an impedance different from the gun body wall, wherein the material is a solid.

13 . A perforation system for perforating a formation surrounding a borehole, the system comprising:

perforating gun assemblies, each assembly comprising a gun body comprising a longitudinal axis and:

a gun body wall comprising a shock attenuation feature, the shock attenuation feature comprises comprising more than one groove, each groove being located at a longitudinal axial position of the gun body wall and comprising a pattern of groove segments spaced circumferentially around the gun body wall;

a threaded connector, wherein the threaded connector is longitudinally axially spaced from the shock attenuation feature; and

a shaped charge supported within the gun body wall, detonation of which produces a shock wave that propagates within the gun body, wherein the shock attenuation feature is longitudinally axially positioned intermediate the shaped charge and the connector; and

wherein the perforating gun assemblies are connected through the threaded connectors and each shock attenuation feature is located and configured to attenuate the shock waves within each respective gun body to decrease stress communicated from one assembly to another assembly through the threaded connectors.

14 . The perforation system of claim 13 , further comprising a conveyance connected to one of the perforating gun assemblies, wherein the shock attenuation feature of the perforating gun assembly connected to the conveyance is located and configured to attenuate the shock wave and decrease stress communicated to the conveyance through the connector.

Assignments (1)

Continuity (1)

References Cited (31)