IP Library Granted Patent US 12,442,605
Granted Patent B1
US 12,442,605 · App. 19/238,406 · Granted Oct 14, 2025

Barrel cooling block for a semi-automatic rifle

Inventor: Raymond Brien (Scottsdale, AZ)
F41A13/12F41A21/24F41A21/44
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 12,442,605
App. No.
19/238,406
Granted
Oct 14, 2025
Kind
B1
Abstract

The invention is a cooling block that is added to a semi-automatic rifle to improve the cooling of the barrel. The cooling block is designed to fit into an air-cooling shroud and sit tightly against the gun barrel. The tolerances for the contact surface between the cooling block and the outer gun are critical for optimal cooling, and the block is designed for easy replacement to provide more continuous cooling.

Claims (31)

1. A metal block cooling system that improves precision of a semi-automatic rifle comprising:

A) a metal cooling block having a block height, a block width, and a block length,

B) said metal cooling block having a halved cylinder cutout along said block length, said metal cooling block having desirable thermal characteristics for heat transfer and heat absorbing,

C) said metal cooling block having a pin positioning hole on a surface opposite of said halved cylinder cutout,

D) a shroud positioned above said rifle barrel and attached to said rifle barrel by a pair of shroud spring clips,

E) said shroud incorporates a block positioning pin,

G) said metal cooling block is positioned on said rifle barrel according to:

i) being between said pair of shroud spring clips,

ii) by placing said halved cylinder cutout on top of said rifle barrel, and

iii) said block positioning pin being inserted into said pin positioning hole,

H) whereby said metal cooling block provides additional cooling when said semi-automatic rifle is fired and said metal cooling block provides an improvement in shooting precision by 19% to 35% inclusive.

2. The metal block cooling system of claim 1 , wherein said metal cooling block substantially comprises copper or aluminum.

3. The metal block cooling system of claim 2 , wherein said metal cooling block includes alloying metals.

4. The metal block cooling system of claim 1 , wherein said halved cylinder cutout has a radius tolerance of +/− of 0.0005 inches.

5. The metal block cooling system of claim 4 , wherein said halved cylinder cutout has a radius of 0.8750 inches.

6. A method that improves precision of a semi-automatic rifle, comprising:

A) providing:

i) a metal cooling block having a block height, a block width, and a block length,

ii) said metal cooling block having a halved cylinder cutout along said block length, said metal cooling block having desirable thermal characteristics for heat transfer and heat absorbing,

iii) said metal block having a pin positioning hole on a surface opposite of said halved cylinder cutout,

iv) a shroud positioned above said rifle barrel and attached to said rifle barrel by a pair of shroud spring clips,

v) said shroud incorporates a block positioning pin,

B) placing said metal cooling block on said rifle barrel according to:

i) being between said pair of shroud spring clips,

ii) by positioning said halved cylinder cutout on top of said rifle barrel, and

iii) said block positioning pin being inserted into said pin positioning hole,

C) whereby said metal cooling block provides additional cooling when said semi-automatic rifle is fired and said metal cooling block provides an improvement in shooting precision by 19% to 35% inclusive.

7. The method of claim 6 , wherein said metal cooling block substantially comprises copper or aluminum.

8. The method of claim 7 , wherein said metal cooling block includes alloying metals.

9. The method of claim 6 , wherein said halved cylinder cutout has a radius tolerance of +/− of 0.0005 inches.

10. The method of claim 9 , wherein said halved cylinder cutout has a radius of 0.8750 inches.

References Cited (28)
US 7464496B1 · Davies · 2008 [cited by examiner]
US 9207031B2 · Balthaser · 2015 [cited by examiner]
US 9410757B2 · Miller · 2016 [cited by applicant]
US 9796057B2 · Tertin · 2017 [cited by applicant]
US 10161700B2 · Klett · 2018 [cited by examiner]
US 10386146B2 · Spector · 2019 [cited by applicant]
US 10386148B1 · Handrick · 2019 [cited by applicant]
US 10866051B2 · Thompson · 2020 [cited by applicant]
US 11578941B2 · Hart · 2023 [cited by applicant]
US 11635271B2 · Lagenbeck · 2023 [cited by applicant]
US 20030010187A1 · Muirhead · 2003 [cited by examiner]
US 20050262997A1 · Brixius · 2005 [cited by examiner]
US 20140076135A1 · Balthaser · 2014 [cited by examiner]
US 20140082990A1 · Lee · 2014 [cited by examiner]
US 20160273861A1 · Langenbeck · 2016 [cited by examiner]
CN 109084616 · 2018 [cited by applicant]
CN 109084616A · 2018 [cited by examiner]
DE 2001938 · 1970 [cited by applicant]
DE 2001938A1 · 1970 [cited by examiner]
GB 374502 · 1932 [cited by applicant]
GB 374502A · 1932 [cited by examiner]
GB 519070 · 1940 [cited by applicant]
GB 519070A · 1940 [cited by examiner]
GB 2613883 · 2023 [cited by applicant]
GB 2613883A · 2023 [cited by examiner]
KR 20150005738 · 2015 [cited by applicant]
KR 20150005738A · 2015 [cited by examiner]
RU 2689091C1 · 2019 [cited by examiner]