IP Library › Granted Patent US 12,638,260
Granted Patent B2
US 12,638,260 · App. 19/218,431 · Granted May 26, 2026

Systems and methods for enhanced firearm suppression

Inventors: Nick Ryan Johnson (Gillette, WY); Kirt James Jensen (Sheridan, WY)
Assignee: North Country Armory
F41A21/30
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Quick Facts
Patent No.
US 12,638,260
App. No.
19/218,431
Granted
May 26, 2026
Kind
B2
Abstract

A firearm suppressor. In an embodiment, the suppressor includes an outer tube and a baffle core disposed within the outer tube. The baffle core includes a body having an exterior surface spaced from the inside surface of the outer tube. A bore extends through the body from an inlet to an outlet permitting a bullet to pass through the baffle core. A plurality of slots or through holes extend through the body between the bore and the external surface of the body permitting gases to expand outward toward the outer tube. A plurality of blind cavities are formed into the external surface of the body and extending into the body without penetrating the bore. These blind cavities provide additional surface area and slow the exit of gases from the suppressor and further cool the gases.

Claims (31)

1 . A firearm suppressor, comprising:

a tube;

a baffle core disposed within the tube, the baffle core including:

a body, wherein an external surface of the body is spaced from an internal surface of the tube;

a bore extending through the body from an inlet opening to an outlet opening;

a plurality of through holes extending through the body between the bore and the external surface of the body; and

a plurality of blind cavities formed into the external surface of the body and extending into the body without penetrating the bore.

2 . The suppressor of claim 1 , wherein the plurality of through holes comprises at least a first row of through holes formed along a length of the body.

3 . The suppressor of claim 2 , further comprising at least two sets of rows of through holes located at different radial locations along the length of the body relative to a long axis of the bore.

4 . The suppressor of claim 2 , wherein the plurality of blind cavities comprises at least a first row of blind holed formed along the length of the body.

5 . The suppressor of claim 4 , further comprising at least two sets of rows of blind cavities located at different radial locations along the body relative to a long axis of the bore.

6 . The suppressor of claim 4 , wherein a first row of blind cavities formed along the length of the body is disposed between first and second rows of through holes formed along the length of the body.

7 . The suppressor of claim 1 , wherein an open end of each of the plurality of through holes on the exterior surface of the body is adjacent to at least one blind cavity.

8 . The suppressor of claim 1 , further comprising a blast chamber configured to connect to an inlet end of the baffle core.

9 . The suppressor of claim 8 , wherein the blast chamber is a hollow element having an annular sidewall extending between an inlet opening and an outlet opening, wherein the inlet opening is configured for attachment to firearm and an outlet opening is configured to connect to the baffle core, wherein the outlet opening is larger than the inlet opening.

10 . The suppressor of claim 8 , wherein the tube is disposed between the blast chamber and a flange on an outlet end of the baffle core.

11 . The suppressor of claim 1 , wherein the is an inner tube and further comprising an outer tube disposed around the inner tube, wherein an inside surface of the outer tube is spaced from an outside surface of the inner tube.

12 . The suppressor of claim 11 , wherein one of:

the inner tube comprises a plurality of grooves formed on its outside surface;

the inner tube comprises a plurality of grooves formed on its inside surface;

the outer tube comprises a plurality of grooves formed on its inside surface.

13 . The suppressor of claim 12 , further comprising a blast chamber configured to connect to an inlet end of the baffle core, wherein the blast chamber is a hollow element having an annular sidewall extending between an inlet opening and an outlet opening, wherein the inlet opening is configured for attachment to firearm and an outlet opening is configured to connect to the baffle core, wherein the outlet opening is larger than the inlet opening.

14 . The suppressor of claim 13 , wherein the blast chamber comprises at least one port fluidly connecting an interior of the blast chamber to a space between the inner tube and the outer tube.

15 . The suppressor of claim 1 , wherein a ratio of an internal surface area to an internal volume exceeds 14.

16 . A method for suppressing sounds generated by the discharge of a firearm generating propellant gases, comprising:

receiving a bullet through an inlet end of a suppressor, wherein the suppressor includes a hollow blast chamber attached to a baffle core, and an outer tube, wherein the baffle core has a body having a bore therethrough;

expanding the propellant gases through a plurality of through holes extending through the body of the baffle core from the bore to an external surface of the baffle core spaced from an inside surface of the outer tube; and

expanding the propellant gases exiting the plurality of through holes on the external surface of the baffle core into blind cavities formed into the external surface of the body and extending into the body without penetrating the bore.

17 . The method of claim 16 , further comprising at least partially blocking the expanding gasses expanding through the through holes within the suppressor using an outer tube disposed around the baffle core.

18 . The method of claim 17 , further comprising disposing an inner tube between the outer tube and the baffle core, wherein expanding the propellant gases includes expanding the gases into a space between the inner tube and the outer tube.

19 . The method of claim 18 , wherein the propellant gases are ported through passages in the blast chamber onto the space between the inner tube and outer tube.

Continuity (2)
Provisional Application 63651845 · May 24, 2024
Related Publication 20250362101A1 · Nov 27, 2025
References Cited (4)
US 7207258B1 · Scanlon · 2007 [cited by examiner]
US 11268776B1 · Noonan · 2022 [cited by examiner]
US 20240367294A1 · Geissele · 2024 [cited by examiner]
US 20250207883A1 · Escalier · 2025 [cited by examiner]