The invention generally relates to firearms. More particularly, the invention relates to a gas block and barrel assembly for regulating gas flow to an autoloading firearm operating system.
Firearms may be operated by energy that is released from the firing of an ammunition cartridge. More particularly, detonation of propellant within an ammunition cartridge may release energy that is transformed into mechanical work to induce a firearm's cycle of operation (feeding, chambering, locking, firing, unlocking, extracting, ejecting, cocking). For instance, a gas system for an autoloading rifle may include a pressure impulse-based system which is driven by a gas port. The gas port may be connected via a gas tube to a bolt carrier group. After the unlocking phase of the cycle of operation, the gas tube interface to the bolt carrier group may begin to move in the direction of extraction, and the interface between the gas tube and the bolt carrier may separate. At this point, energy transferred from pressurized exhaust gases within the gas system may be transformed into potential energy within an energy storage system, such as a buffer spring. Potential energy stored in the buffer spring then may be released to initiate another cycle of operation. The amount of energy that is transferred to the projectile and the stored energy that is available for inducing another cycle of operation may affect firearm operation. Accordingly, a need exists for systems and methods which may efficiently utilize energy released during a firearm's cycle of operation.
Hence, the present invention is generally directed toward a gas block assembly for regulating gas flow to an autoloading firearm operating system. The gas block assembly may include a gas block for collecting discharge gases from a barrel. The gas block may include a first side, a second side spaced from the first side, and a barrel receiving bore extending from the first side to the second side. The barrel receiving bore may include a first longitudinal axis. The gas block further may include a gas tube receiving bore extending from the first side to the second side. The gas tube receiving bore may include a second longitudinal axis, the second longitudinal axis being in substantially parallel alignment with the first longitudinal axis. Also, the gas block may include an intermediate passage extending from the barrel receiving bore to the gas tube receiving bore.
The intermediate passage may include a third longitudinal axis, the third longitudinal axis and the first longitudinal axis defining an oblique angle. The intermediate passage may include a starting gas hole segment adjacent the barrel receiving bore and an exiting gas hole segment adjacent the gas tube receiving bore. The exiting gas hole segment may include a first cross-section perpendicular to the third longitudinal axis. The first cross-section may have a first diameter. The intermediate passage further may include a gas regulator seat between the starting gas hole and the exiting gas hole. The gas regulator seat may include a second cross-section perpendicular to the third longitudinal axis. The second cross-section may have a second diameter. The second diameter may be greater than the first diameter.
The gas block assembly further may include a gas regulator arranged in the gas regulator seat. The gas regulator may include a plug including a fourth longitudinal axis. The plug may include a first end and a second end spaced from the first end along the fourth longitudinal axis. Also, the plug may include a gas regulating hole extending from the first end to the second end. The gas regulating hole may include a nozzle segment facing the starting gas hole segment, a keyed segment facing the exiting gas hole segment, and an intermediate segment. The intermediate segment may be disposed between the nozzle segment and the keyed segment. The intermediate segment may be in fluid communication with the starting gas hole segment and the exiting gas hole segment.
Additionally, the plug further may include an exterior surface between the first end and the second end such that the exterior surface is configured and dimensioned to interlock with the gas regulator seat. The gas regulator seat further may include a first screw thread, and the exterior surface may include a second screw thread. The second screw thread may be configured and dimensioned to mate with the first screw thread. Moreover, the first screw thread and the second screw thread may be interlocked, blocking fluid flow between the exterior surface and the regulator seat. The gas regulating hole may fluidly connect the starting gas hole segment and the exiting gas hole segment. Also, the keyed segment may include a drive slot for rotating the gas regulator with respect to the gas regulator seat. The drive slot may further include a third cross-section perpendicular to the fourth longitudinal axis, the third cross-section having a hexagonal shape.
The intermediate segment may include a fourth cross-section perpendicular to the fourth longitudinal axis. The fourth cross-section may include a first maximum outer dimension, and the starting gas hole segment may include a fifth cross-section perpendicular to the third longitudinal axis. The fifth cross-section may include a second maximum outer dimension. The second outer maximum dimension may be greater than the fourth maximum outer dimension. Additionally, the oblique angle may range from approximately 30 degrees to approximately 90 degrees. More particularly, the oblique angle may be approximately 50 degrees.
Further still, the barrel receiving bore may be configured and dimensioned to form a slip fit with a barrel. Also, the gas block may include an orientation key. The gas block further may include an access portal proximate to the gas receiving tube, the access portal providing access to the exiting gas hole such that a drive tool may be connected to the keyed segment and arranged through the access portal and the gas tube receiving bore.
Another aspect of the present invention is directed to a regulated gas block and barrel assembly.
The regulated gas block and barrel assembly may include a gas block assembly as described herein and a barrel fitted in the barrel receiving bore. The barrel further may include a first gas port. The first gas port may be in fluid communication with the starting gas hole segment. Also, the barrel further may include a gas ring recess. The gas ring recess may be in fluid communication with the starting gas hole segment. The gas ring recess may include a circumferential groove around the barrel. Additionally, the barrel further may include a plurality of gas ports other than the first gas port. The plurality of gas ports may be in fluid communication with the circumferential groove.
Another aspect of the present invention is directed to a method of fabricating a regulated gas block assembly for a firearm. The method may include orienting a blank of material for fabricating a regulated gas block, advancing a barrel receiving bore through the blank, and advancing a gas tube receiving bore through the blank. The method further may include establishing a longitudinal axis extending from the barrel receiving bore to the gas tube bore, and advancing a first bore including a first diameter through the blank from the barrel receiving bore along the longitudinal axis to the gas tube receiving bore to create an intermediate passage such that the intermediate passage defines an exiting gas hole. Moreover, the method may include creating a second bore including a second diameter, the second diameter being greater than the first diameter, the second bore extending from the barrel receiving bore along the longitudinal axis to define an intermediate segment of the intermediate passage such that the second bore defines a seat for a gas regulator. The method may include advancing a third bore including a third outer dimension greater than the second diameter along the longitudinal axis from the barrel receiving bore to the intermediate segment such that the third bore defines an entering gas hole. Also, the method may include removing material from an exterior surface of the blank to create an access portal connecting the exterior surface of the blank to the exiting gas hole, as well as positioning a gas regulator into the seat.
In the accompanying drawings, which form part of this specification and are to be read in conjunction therewith and in which like reference numerals are used to indicate like parts in the various views:
Referring to
Additionally, the barrel 22 further may include a gas port 30. The gas port 30 may be located from the breach face 32 of the barrel 22 by a length L2. The muzzle 34 may be spaced from the gas port 30 by a length L3. Also, the distal end of the barrel 36 may include a threaded segment 38 of length L4. As shown in
Generally, however, the gas block 24 in accordance with the present invention may be used with a barrel having a length of up to 20 inches or greater. Preferably, the firearm 10 is an autoloading firearm and the gas block 24 regulates gas flow from the barrel 22 to the firearm operating system to induce the firearm's cycle of operation. Accordingly, the gas block 24 may be used in carbines, rifles, and other small arms weapons.
As shown in
Also, the gas port 30 may have a longitudinal axis 70. The longitudinal axis 70 of the gas port 30 may be substantially perpendicular to the central axis 68 of the bore. The gas port 30 may have a circular shape perpendicular to the longitudinal axis 70. For example, without limitation, the gas port 30 may have a diameter D3 ranging from approximately 0.01 inches to approximately 0.10 inches. In the exemplary embodiment of
Referring to
The gas block 24 may further include a gas tube receiving bore 80. The gas tube receiving bore 80 may be configured and dimensioned to receive the distal end of the gas tube 52. The gas tube receiving bore 80 may extend from the one side of the gas block 24 to another side of the gas block. The gas tube receiving bore 80 may have a longitudinal axis 82. The gas tube receiving bore 80 may have a circular shape perpendicular to the longitudinal axis 82. For example, without limitation, the gas tube receiving bore 80 may have a diameter D5 ranging from approximately 0.08 inches to approximately 0.30 inches. In the disclosed embodiment, the gas tube receiving bore 80 has a diameter D5 of approximately 0.181 inches. The longitudinal axis 82 of the gas tube receiving bore may be parallel to the central axis 84 of the barrel receiving bore 72.
The gas block 24 may further include an intermediate passage 86 extending between the barrel receiving bore 72 and the gas tube receiving bore 80. The intermediate passage 86 may have a longitudinal axis 88. Preferably, the longitudinal axis 88 of the intermediate passage 86 and the central axis 84 of the barrel receiving bore 72 may define an oblique angle Θ2. For example, the angle Θ2 defined by the longitudinal axis 88 of the intermediate passage 86 and the central axis 84 of the barrel receiving bore 72 may range from approximately 30 degrees to approximately 90 degrees. Most preferably, in the disclosed embodiment the angle Θ2 defined by the longitudinal axis 88 of the intermediate passage and the central axis 84 of the barrel receiving bore is approximately 50 degrees. Still, in some embodiments the angle Θ2 may be a right angle.
The intermediate passage 86 may include a starting gas hole 90 which intersects the barrel receiving bore 72 and extends toward the gas tube receiving bore 80. The starting gas hole 90 may have a cross-section perpendicular to the longitudinal axis 88 of rounded shape. For example, the starting gas hole 90 may have a radius R1 ranging from approximately 0.01 inches to approximately 0.250 inches. In the disclosed embodiment, the starting gas hole 90 may have a radius R1 of approximately 0.125 inches.
The intermediate passage further may include an exiting gas hole 92 which intersects the gas tube receiving bore 80 and extends toward the barrel receiving bore 72. The exiting gas hole 92 may have a cross-section perpendicular to the longitudinal axis 88 of circular shape. For example, the exiting gas hole 92 may have a diameter D6 ranging from approximately 0.02 inches to approximately 0.250 inches. In the disclosed embodiment, the exiting gas hole 92 has a diameter D6 of approximately 0.125 inches.
Further still, the intermediate passage 86 may include a gas regulator seat 94 between the starting gas hole 90 and the exiting gas hole 92. The gas regulator seat 94 may have a cross-section of circular shape perpendicular to the longitudinal axis. For example, the gas regulator seat 94 may have a diameter ranging from approximately 0.05 inches to approximately 0.250 inches. In the disclosed embodiment, the gas regulator seat 94 has a diameter D7 of approximately 0.177 inches. The sidewall of the segment may include a screw thread 96. As shown in
Referring to
As shown in
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Referring to
Accordingly, the intermediate passage 86 may define a volume V4 between the gas port 30 and the gas tube 52 through which discharge gases from the barrel are directed to the gas key 54 of the bolt carrier 48. Similarly, the exiting gas hole 92 and the entering gas hole 90 may have respective volumes V1 and V3 through which discharge gases from the barrel transit as the discharge gases are directed to the gas key 54 of the bolt carrier 48. Also, the gas hole 102 of the gas regulator 98 may have a volume V2 through which discharge gases from the barrel transit as the discharge gases are directed to the gas key 54 of the bolt carrier 48. Accordingly, the volume V4 of intermediate passage 86 may be the sum of exiting gas hole 92 volume V1, the entering gas hole volume V3, and the gas hole 102 volume V2. Exemplary values—in units of cubic inches—for the respective volumes of the segments which form the intermediate passage in an exemplary embodiment of the gas block and barrel assembly 40 of
As previously described, the intermediate segment 112 may be configured and dimensioned to allow a target volume of discharge gases to transit the intermediate passage 86 during each cycle of operation.
Referring to
Further, the regulated gas block 40 may be replaced in its entirety for use with the same barrel 22, and thus may provide enhanced flexibility and potential cost saving in the operation and maintenance of the firearm. Moreover, the regulated gas block assembly 40 preferably incorporates an angled gas port 118 instead of a perpendicular one relative to the bore 46 of the barrel 22. The angled gas port 118 may allow for enhanced change in momentum of the discharge gases per unit time. This may moderate the exchange of energy from the expanding discharge gases into potential energy of the buffer spring 64, and result in less wear on moving components involved in the cycle of operation.
The regulated gas block 40 may be manufactured in an additive or subtractive process. Preferably the gas block 24 may be formed from a blank of suitable material (e.g., a steel alloy, titanium alloy, or other metal alloy). For example, a method 1700 for fabricating the gas block 24 from a blank of suitable material is outlined in
The bore 132 may extend from the chamber 130 to the muzzle end 134. Generally, the bore 132 may include rifling. Also, the barrel 120 may include a tapered segment 138 and a step 140 which may include a key 142 for receiving a gas block assembly. Moreover, the barrel 120 may include a gas ring recess 122 situated between the key 142 and the muzzle end 134 of the barrel 132. For example, referring to
Referring to
Additionally, referring to
Generally, the barrel may range in length L12 from approximately 3 inches to approximately 20 inches, including, without limitation, barrel lengths of approximately 5.5 inches, 10.5 inches, 14.5 inches, 16 inches, and 18 inches. Although the barrel 120 of
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The gas block 24 may further include a gas tube receiving bore 80. The gas tube receiving bore may be configured and dimensioned to receive the distal end of the gas tube 52. The gas tube receiving bore 80 may extend from the one side of the gas block 24 to the other side of the gas block 24. The gas tube receiving bore 80 may have a longitudinal axis 82. The gas tube receiving bore 80 may have a circular shape perpendicular to the longitudinal axis. For example, without limitation, the gas tube receiving bore 80 may have a diameter D5 ranging from approximately 0.08 inches to approximately 0.30 inches. In the exemplary embodiment, the gas tube receiving bore may have a diameter of approximately 0.181 inches. The longitudinal axis 82 of the gas tube receiving bore may be parallel to the central axis of the bore.
Referring to
Moreover, the proximal side of the gas block 24 may include a flange. The flange may surround the circumference of the barrel receiving bore 72. The exterior surface of the flange may include a screw thread. The flange may be configured and dimensioned to seal discharge gases in the gas block, and thus may limit fugitive emissions which can adversely affect performance of the gas system. One or more fasteners may be operatively associated with the flange such that the one or more fasteners cooperate with the flange to achieve a secure and gas tight connection between the barrel and the proximal side of the gas tube receiving bore.
In use, a barrel with a gas ring which includes a number of gas ports in a barrel of a gas driven auto loading firearm, may allow for lower temperature exhaust gases per gas port powering the cycle of operation. This may reduce wear of operating mechanism components, beneficially modulate the cycle of operation, and enable more controllable fire during fully automatic fire. Also, the autoloading firearm may be able to fire subsonic ammunition or supersonic ammunition without adjustment of the gas operating system.
The gas regulators (98a, 98b, 98c) in the kit 400 may be substantially the same, and further may be configured and dimensioned for use with a particular barrel. For example, each of the three gas regulators may be configured and dimensioned for use with a barrel chambered for 5.56 NATO ammunition cartridges and having a length of approximately 5.5 inches, 8.5 inches, or 10.3 inches. In another example, each of the three gas regulators may be configured and dimensioned for use with a barrel chambered for 7.62×39 mm ammunition cartridges and having a length of approximately 5.5 inches, 8.5 inches, or 10.3 inches. In yet another example, each of the three gas regulators may be configured and dimensioned for use with a barrel chambered for BLK 300 ammunition cartridges and having a length of approximately 5.5 inches, 8.5 inches, or 10.3 inches.
Moreover, each of the gas regulators may be configured and dimensioned for use with a different barrel. For example, each of the three gas regulators may be configured and dimensioned for use with a barrel chambered for 5.56 NATO ammunition cartridges and having a respective length of approximately 5.5 inches, 8.5 inches, or 10.3 inches. In another example, each of the three gas regulators may be configured and dimensioned for use with a barrel chambered for 7.62×39 mm ammunition cartridges and having a respective length of approximately 5.5 inches, 8.5 inches, or 10.3 inches. In yet another example, each of the three gas regulators may be configured and dimensioned for use with a barrel chambered for BLK 300 ammunition cartridges and having a respective length of approximately 5.5 inches, 8.5 inches, or 10.3 inches.
In yet another example, each of the three gas regulators may be configured and dimensioned for use respectively with a barrel chambered for 5.56 NATO ammunition cartridges, 7.62×39 mm ammunition cartridges, and BLK 300 ammunition cartridges. The respective barrels may each have substantially the same length, such as without limitation, a barrel length of approximately 5.5 inches, 8.5 inches, or 10.3 inches.
In yet another example, each of the three gas regulators may be configured and dimensioned for use respectively with a barrel chambered for a specific cartridge type but having different performance characteristics. For instance, the gas regulators may be configured and dimensioned for a 5.56 NATO ammunition cartridge, a 5.56 NATO ammunition cartridge having a maxim charge of propellant, and a 5.56 NATO ammunition cartridge having a subsonic charge of propellant, respectively. Accordingly, each of the three gas regulators may be configured and dimensioned for use in a particular operational mode of the firearm (e.g., unsuppressed, suppressed etc.).
While it has been illustrated and described what at present are considered to be preferred embodiments of the present invention, it will be understood by those skilled in the art that various changes and modifications may be made, and equivalents may be substituted for elements thereof without departing from the true scope of the invention. Moreover, features and/or elements from any disclosed embodiment may be used singly or in combination with other embodiments. Therefore, it is intended that this invention not be limited to the features disclosed herein, but that the invention include all embodiments falling within the scope and the spirit of the present invention.
This application claims the benefit of U.S. Provisional Application No. 62/797,923 filed Jan. 28, 2019. Additionally, this application claims the benefit of U.S. Provisional Application No. 62/885,146 filed Aug. 9, 2019. This application is a continuation-in-part of U.S. patent application Ser. No. 29/676,356 filed Jan. 10, 2019. Also, this application is a continuation-in-part of U.S. patent application Ser. No. 16/689,037 filed Nov. 19, 2019, which claims the benefit of U.S. Provisional Application No. 62/777,739 filed Dec. 10, 2018. The entire disclosure of each of the U.S. Patent applications mentioned in this paragraph is incorporated by reference herein.
Number | Date | Country | |
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62797923 | Jan 2019 | US | |
62885146 | Aug 2019 | US | |
62777739 | Dec 2018 | US |
Number | Date | Country | |
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Parent | 29676356 | Jan 2019 | US |
Child | 16747478 | US | |
Parent | 16689037 | Nov 2019 | US |
Child | 29676356 | US |