US2742821A - Vent for tapered bore gun - Google Patents
Vent for tapered bore gun Download PDFInfo
- Publication number
- US2742821A US2742821A US588878A US58887845A US2742821A US 2742821 A US2742821 A US 2742821A US 588878 A US588878 A US 588878A US 58887845 A US58887845 A US 58887845A US 2742821 A US2742821 A US 2742821A
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- US
- United States
- Prior art keywords
- bore
- barrel
- tapered
- section
- vent
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 239000000843 powder Substances 0.000 description 4
- 230000003628 erosive effect Effects 0.000 description 2
- 238000010304 firing Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 238000013022 venting Methods 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 238000004513 sizing Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A21/00—Barrels; Gun tubes; Muzzle attachments; Barrel mounting means
- F41A21/16—Barrels or gun tubes characterised by the shape of the bore
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A21/00—Barrels; Gun tubes; Muzzle attachments; Barrel mounting means
- F41A21/28—Gas-expansion chambers; Barrels provided with gas-relieving ports
Definitions
- This invention relates to improvements in tapered bore guns and more particularly to venting means for eliminating the mutilation of the case which invaribly occurs in firing a conventional tapered bore gun.
- Tapered bore guns of large caliber have proven very eifective in anti-tank and armor piercing uses, especially in 57 mm.40 mm. size.
- the advantages of employing a tapered bore together with a deformable projectile are that a projectile of the smaller cross section is obtained, thus having a reduced wind resistance resulting in better stability in range, enabling more favorable types and amounts of powder, relative to the projectile weight to be used, producing greater muzzle velocity; and the life of the barrel is prolonged over that of a barrel of the smaller diameter employing powder in the proportion used in a barrel of the larger diameter.
- the advantage of the tapered bore has been partially lost by the disadvantage of the shell being mutilated, due to the fact that the mutilated shell scores the breech and pre vents re-sizing and re-use of the case as is customary in the Army.
- This mutilation of the case is caused by the formation of a pressure wave in the bore created when the deformable projectile enters the tapered section, producing momentary decrease in velocity thereof. Since the gas pressure is extremely high, approximately 50,000 pounds per square inch, the action of the gas is analogous to the action of liquids under pressure. Since the pressure front is moving toward the muzzle, this momentary deceleration creates a back pressure wave toward the breech which mutilates the case end.
- Still a further aim of the invention is to provide vents so arranged that they will not only function to eliminate the back pressure wave, but will also function as a muz zle brake to reduce the recoil and, in addition, to compensate for the recoil vertical jump of the gun.
- Still another object of the invention is to form the bore with a recessed section into which the vents open so that the projectile skirts will not close the vent openings at the instant that the back pressure wave is created and so that the skirts will not extrude into the vent openings and thereby cause erosion of the bore around the vents.
- FIG. 1 is a longitudinal, substantially central sectional view of a portion of a tapered gun barrel constructed in accordance with the preferred form of the invention
- Figure 2 is a cross sectional view of the barrel taken substantially along a plane as indicated by the line 2-2 of Fig. 1;
- Figure 3 is a fragmentary, longitudinal substantially central sectional view of a slightly modified form of the invention.
- Figure 4 is a view similar to Fig. 3 of another modification thereof.
- Figure 5 is a view similar to Fig. l and showing another embodiment of the invention.
- Figs. 1 and 2 6 designates generally a portion of a gun barrel having a bore including the bore sections 7 and 8.
- Bore section 7 is of the same diameter throughout its length, whereas bore section 8 is tapered and diminishes from a diameter equal to that of bore section 7 to a diameter of a smaller caliber bore section, not shown in Figs. 1 and 2, but illustrated in Figs. 3 and 4.
- the bore section 8, at the end thereof which joins with bore section 7, is recessed at 9 to provide a portion of greater diameter than either of the sections 7 or 8.
- the upper part of the barrel 6 is provided with a plurality of openings or passages 10 which open into the recessed portion 9 at their inner ends and which open outwardly of the barrel 6 at their outer ends.
- the vent openings or passages 10 are inclined to the rear from their inner to their outer ends, for a purpose which will hereinafter become apparent.
- the number and size of the vents 10 will vary depending upon calibers of the barrel, arrived at as a result of test.
- the barrel 11 includes a large caliber bore section 12, a smaller caliber bore section 13 and a tapered bore section 14 therebetween, the rear end of which is of the same caliber as the bore section 12 and the forward end of which is of the same caliber as the bore section 13.
- Barrel 11 is provided with vent openings or passages 15 formed in the forward end of its bore section 12 and which open into said section. Vent openings 15 extend entirely around the barrel 11 and are likewise inclined rearwardly from their inner to their outer ends, and may be of any desired number and size as required.
- vent openings or passages 16 are formed in the rear portion of the tapered, intermediate bore section 17 instead of in the rear bore section 18.
- FIG. 5 Another embodiment of the invention is disclosed in Fig. 5, and is similar to the preferred form as shown in Figs. 1 and 2, in that the tapered bore section 19 is provided with a recessed portion 20, adjacent its rear end, similar to and for the same purpose as the recessed portion 9.
- the vent openings or passages 21 may be formed entirely around the barrel and open into the recessed portion 20 and are inclined outwardly and rearwardly.
- the barrel 22 is formed of sections and the tapered section 19 thereof, at its enlarged end, is provided with an enlarged internally threaded socket 23 for engaging an externally threaded restricted extension 24 of the enlarged straight barrel section 25, for detachably connecting the barrel sections.
- vent means will function acceptably when located in any of the'positions as shown in the drawing, the preferred position is as shown in Figs. '1 and 2 wherein the vent passages are located near the rear .end of the tapered bore section.
- the vent passages By providing the recessed portion 9 or 20,. the skirts of the projectile, not shown, will not extrude into the vent openings to cause erosion of the 'bore therearound and will not impede the release of the excess pressure.
- the vented pressure is additionally utilized to function as a muzzle brake and also to reduce the recoil vertical jump. The grouping of the vents in the upper part of the barrel also prevents an excess amount of flash toward the ground that would reflect against and expose the gun crew.
- vents to atmosphere in the locations illustrated do not afiect the exterior ballistics of the projectile, firstly because gas pressure in the barrel has already reached .a maximum before the vents are reached, and has started to diminish at the time the projectile passes the vents, and secondly because of the fact that muzzle velocity of a projectile is dependent to a very large degree upon the ratio of the weight of the projectile to the type and amount of propellent powder. Firing tests on vented gun barrels, in which the muzzle velocity was measured, indicated that the values obtained were the values .to be expected for the weight of projectiles and type and amount .of propellent powder used.
- a gun barrel having a breech end bore portion of one caliber, a muzzle end bore portion of a lesser caliber, and an intermediate tapered bore portion connecting and merging withthe bores of said end portions to provide a smooth bore surface, there being a cylindrical recess formed in said intermediate portion of the wall of said barrel and adjacent the connection with said breech end bore portion, said recess being of greater diameter than the bore of said breech end portion, there also being a plurality of vents opening outwardly and rearwardly through the top portion of the wall of said cylindrical recess.
- a gun barrel having a breech end portion of one caliber, a muzzle end portion of a lesser caliber, and an intermediate portion connecting the bores of said end portions and having a bore tapered from its breech end to its muzzle end, there being a cylindrical recess in the wall of said barrel between said breech part and said intermediate part .of greater diameter than the bore of said breech portion, said cylindrical recess having a plurality of vents extending through its Wall thereofJ
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
Description
April 24, 1956 L. R. SWEETMAN VENT FOR TAPERED BORE GUN Filed April 17, 1945 Fig]- L ER DY H-5WEET MAN VENT FOR TAPERED BORE GUN Leroy R. Sweetman, Washington, D. C., assignor to the United States of America as represented by the Secretary of War Application April 17, 1945, Serial No. 588,878
2 Claims. (Cl. 89-14) (Granted under Title 35, U. S. Code (E52), sec. 266) The invention described herein may be manufactured and used by or for the Government for governmental purposes without the payment to me of any royalty thereon.
This invention relates to improvements in tapered bore guns and more particularly to venting means for eliminating the mutilation of the case which invaribly occurs in firing a conventional tapered bore gun.
Tapered bore guns of large caliber have proven very eifective in anti-tank and armor piercing uses, especially in 57 mm.40 mm. size. The advantages of employing a tapered bore together with a deformable projectile are that a projectile of the smaller cross section is obtained, thus having a reduced wind resistance resulting in better stability in range, enabling more favorable types and amounts of powder, relative to the projectile weight to be used, producing greater muzzle velocity; and the life of the barrel is prolonged over that of a barrel of the smaller diameter employing powder in the proportion used in a barrel of the larger diameter. However, the advantage of the tapered bore has been partially lost by the disadvantage of the shell being mutilated, due to the fact that the mutilated shell scores the breech and pre vents re-sizing and re-use of the case as is customary in the Army.
This mutilation of the case is caused by the formation of a pressure wave in the bore created when the deformable projectile enters the tapered section, producing momentary decrease in velocity thereof. Since the gas pressure is extremely high, approximately 50,000 pounds per square inch, the action of the gas is analogous to the action of liquids under pressure. Since the pressure front is moving toward the muzzle, this momentary deceleration creates a back pressure wave toward the breech which mutilates the case end.
It is, therefore, a primary aim of this invention to provide means for venting the bore of the barrel to neutralize this back pressure wave and to permit it to escape into the atmosphere.
More particularly, it is an object of this invention to provide vents disposed in the forward end of the enlarged portion of the barrel or adjacent the rear end of the tapered section to eliminate the back pressure wave.
Still a further aim of the invention is to provide vents so arranged that they will not only function to eliminate the back pressure wave, but will also function as a muz zle brake to reduce the recoil and, in addition, to compensate for the recoil vertical jump of the gun.
Still another object of the invention is to form the bore with a recessed section into which the vents open so that the projectile skirts will not close the vent openings at the instant that the back pressure wave is created and so that the skirts will not extrude into the vent openings and thereby cause erosion of the bore around the vents.
Other objects and advantages of the invention will hereinafter become more fully apparent from the following description of the drawing, which illustrates preferred embodiments thereof, and wherein:
2,742,821 Patented Apr. 24, 1956 "ice Figure 1 is a longitudinal, substantially central sectional view of a portion of a tapered gun barrel constructed in accordance with the preferred form of the invention;
Figure 2 is a cross sectional view of the barrel taken substantially along a plane as indicated by the line 2-2 of Fig. 1;
Figure 3 is a fragmentary, longitudinal substantially central sectional view of a slightly modified form of the invention;
Figure 4 is a view similar to Fig. 3 of another modification thereof; and
Figure 5 is a view similar to Fig. l and showing another embodiment of the invention.
Referring more particularly to the drawing, wherein like reference characters designate like or corresponding parts throughout the different views, in Figs. 1 and 2 6 designates generally a portion of a gun barrel having a bore including the bore sections 7 and 8. Bore section 7 is of the same diameter throughout its length, whereas bore section 8 is tapered and diminishes from a diameter equal to that of bore section 7 to a diameter of a smaller caliber bore section, not shown in Figs. 1 and 2, but illustrated in Figs. 3 and 4. In this preferred embodiment of Figs. 1 and 2, the bore section 8, at the end thereof which joins with bore section 7, is recessed at 9 to provide a portion of greater diameter than either of the sections 7 or 8. The upper part of the barrel 6 is provided with a plurality of openings or passages 10 which open into the recessed portion 9 at their inner ends and which open outwardly of the barrel 6 at their outer ends. As seen in Fig. 1, the vent openings or passages 10 are inclined to the rear from their inner to their outer ends, for a purpose which will hereinafter become apparent. The number and size of the vents 10 will vary depending upon calibers of the barrel, arrived at as a result of test. In the modified form disclosed in Fig. 3, the barrel 11 includes a large caliber bore section 12, a smaller caliber bore section 13 and a tapered bore section 14 therebetween, the rear end of which is of the same caliber as the bore section 12 and the forward end of which is of the same caliber as the bore section 13. Barrel 11 is provided with vent openings or passages 15 formed in the forward end of its bore section 12 and which open into said section. Vent openings 15 extend entirely around the barrel 11 and are likewise inclined rearwardly from their inner to their outer ends, and may be of any desired number and size as required.
The embodiment of the invention shown in Fig. 4 varies only from that shown in Fig. 3 in that vent openings or passages 16 are formed in the rear portion of the tapered, intermediate bore section 17 instead of in the rear bore section 18.
Another embodiment of the invention is disclosed in Fig. 5, and is similar to the preferred form as shown in Figs. 1 and 2, in that the tapered bore section 19 is provided with a recessed portion 20, adjacent its rear end, similar to and for the same purpose as the recessed portion 9. In this form of the invention, the vent openings or passages 21 may be formed entirely around the barrel and open into the recessed portion 20 and are inclined outwardly and rearwardly. Also, in this embodiment of the invention, the barrel 22 is formed of sections and the tapered section 19 thereof, at its enlarged end, is provided with an enlarged internally threaded socket 23 for engaging an externally threaded restricted extension 24 of the enlarged straight barrel section 25, for detachably connecting the barrel sections.
From the foregoing, it will be apparent that when a projectile, not shown, of a caliber corresponding to the caliber of the larger bore section of the barrel is fired through any one of the barrels as shown in Figs. 1, 3, 4, and 5, will, 'when it passes from the larger bore section, adjacent the breech end of the barrel, and into the tapered section where it is deformed, create a back pressure wave which will be released through the vents located either at. the rear end of the tapered section or at the forward end of the rear, straight section. This will prevent the back pressure wave from moving back to the breech of the barrel, not shown, and mutilating the open end of the empty shell case, not shown. While the vent means will function acceptably when located in any of the'positions as shown in the drawing, the preferred position is as shown in Figs. '1 and 2 wherein the vent passages are located near the rear .end of the tapered bore section. By providing the recessed portion 9 or 20,. the skirts of the projectile, not shown, will not extrude into the vent openings to cause erosion of the 'bore therearound and will not impede the release of the excess pressure. By grouping the vent passages in the upper portion of the barrel, as shown in Figs. 1 and 2, the vented pressure is additionally utilized to function as a muzzle brake and also to reduce the recoil vertical jump. The grouping of the vents in the upper part of the barrel also prevents an excess amount of flash toward the ground that would reflect against and expose the gun crew.
It is important to note that the provision of vents to atmosphere in the locations illustrated do not afiect the exterior ballistics of the projectile, firstly because gas pressure in the barrel has already reached .a maximum before the vents are reached, and has started to diminish at the time the projectile passes the vents, and secondly because of the fact that muzzle velocity of a projectile is dependent to a very large degree upon the ratio of the weight of the projectile to the type and amount of propellent powder. Firing tests on vented gun barrels, in which the muzzle velocity was measured, indicated that the values obtained were the values .to be expected for the weight of projectiles and type and amount .of propellent powder used.
Various additional modifications and changes are contemplated and may obviously be resorted to, provided that they do not depart from the spirit and scope of the invention as hereinafter defined by the appended claims, as only preferred embodiments have been disclosed.
I claim:
1. In a gun barrel having a breech end bore portion of one caliber, a muzzle end bore portion of a lesser caliber, and an intermediate tapered bore portion connecting and merging withthe bores of said end portions to provide a smooth bore surface, there being a cylindrical recess formed in said intermediate portion of the wall of said barrel and adjacent the connection with said breech end bore portion, said recess being of greater diameter than the bore of said breech end portion, there also being a plurality of vents opening outwardly and rearwardly through the top portion of the wall of said cylindrical recess.
2. In a gun barrel having a breech end portion of one caliber, a muzzle end portion of a lesser caliber, and an intermediate portion connecting the bores of said end portions and having a bore tapered from its breech end to its muzzle end, there being a cylindrical recess in the wall of said barrel between said breech part and said intermediate part .of greater diameter than the bore of said breech portion, said cylindrical recess having a plurality of vents extending through its Wall thereofJ References Cited in the file of this patent UNITED STATES PATENTS 85,949 McKenzie Jan. 1-9, 1869 329,303 Fosbery Oct. 27, 1885 592,437 Oberhammer Oct. 26, 1897 785,975 McClean Mar. 28, 1905 786,230 McClean Mar. 28, 1905 1,082,916 Squire Dec. 30, 1913 1,380,171 Abbot May 31, 1921 1,773,260 Cutts Aug. 19, 1-930 1,944,883 Gerlich Ian. 30, 1934 2,322,370 Lance June 22, 1943 FOREIGN PATENTS 437,027 Great Britain Oct. 23, 1 935
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US588878A US2742821A (en) | 1945-04-17 | 1945-04-17 | Vent for tapered bore gun |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US588878A US2742821A (en) | 1945-04-17 | 1945-04-17 | Vent for tapered bore gun |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2742821A true US2742821A (en) | 1956-04-24 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US588878A Expired - Lifetime US2742821A (en) | 1945-04-17 | 1945-04-17 | Vent for tapered bore gun |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2742821A (en) |
Cited By (30)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2842024A (en) * | 1954-12-07 | 1958-07-08 | John F Mutter | Anti-recoil gun barrels |
| US2916970A (en) * | 1956-02-10 | 1959-12-15 | John F Mutter | Anti-recoil gun barrels |
| US3412641A (en) * | 1966-06-27 | 1968-11-26 | Mb Assoc | Pistol for firing a miniature ballistic rocket |
| US3418741A (en) * | 1965-09-08 | 1968-12-31 | Dynamit Nobel Ag | Firearm |
| US3664052A (en) * | 1970-04-02 | 1972-05-23 | Bruce Mounier | Impact actuated underwater gun |
| US3808943A (en) * | 1972-04-27 | 1974-05-07 | L Kelly | Gun-leveling device |
| US4176487A (en) * | 1970-11-18 | 1979-12-04 | Manis John R | Firearm barrels and projectiles |
| US4379531A (en) * | 1970-11-18 | 1983-04-12 | Manis John R | Projectile |
| US4852460A (en) * | 1988-05-04 | 1989-08-01 | Davidson Windell L | Muzzle brake system |
| US4947729A (en) * | 1989-06-19 | 1990-08-14 | Timothy Downey | Spin stabilizing gun |
| US5249385A (en) * | 1992-03-24 | 1993-10-05 | Vang Hans J | Shotgun barrel |
| US5272827A (en) * | 1992-03-24 | 1993-12-28 | Vang Hans J | Shotgun barrel |
| US5394634A (en) * | 1992-03-24 | 1995-03-07 | Hans J. Vang | Shotgun barrel |
| US20030024377A1 (en) * | 2001-08-03 | 2003-02-06 | Diller E. Wendell | Elongated vented gun barrel |
| US6694887B2 (en) | 2000-06-09 | 2004-02-24 | E. Wendell Diller | Shotgun shell flight path indicator |
| US20050188882A1 (en) * | 2000-06-09 | 2005-09-01 | Diller E. W. | Shotgun shell flight path indicator |
| US20060207154A1 (en) * | 2005-03-19 | 2006-09-21 | Lazor Ernest R | Improved shotgun barrel construction |
| US20090151729A1 (en) * | 2005-11-08 | 2009-06-18 | Resmed Limited | Nasal Assembly |
| US20100269387A1 (en) * | 2006-02-28 | 2010-10-28 | Cornell Drajan | Muzzle Break |
| US20100281743A1 (en) * | 2003-08-28 | 2010-11-11 | Ra Brands, L.L.C. | Modular Barrel Assembly |
| US20120131836A1 (en) * | 2010-08-31 | 2012-05-31 | Smith & Wesson Corp. | Enhanced life barrel |
| CN102519304A (en) * | 2012-01-13 | 2012-06-27 | 内蒙古第一机械集团有限公司 | Gun barrel capable of improving firing precision of gun |
| US9254370B2 (en) | 2006-11-14 | 2016-02-09 | Resmed Limited | Frame and vent assembly for mask assembly |
| US9885533B2 (en) | 2016-03-10 | 2018-02-06 | James Norman Griffitts | Barrel stabalizing and recoil reducing muzzle brake |
| US10422603B2 (en) | 2016-03-10 | 2019-09-24 | James Norman Griffitts | Barrel stabilizing and recoil reducing muzzle brake |
| US10641569B2 (en) * | 2015-08-12 | 2020-05-05 | John Baker | Firearm barrel stiffening and/or cooling systems and methods |
| USD891205S1 (en) | 2016-10-31 | 2020-07-28 | Stego Industries, LLC | Concrete forming stake |
| US10816300B2 (en) * | 2016-03-10 | 2020-10-27 | James Norman Griffitts | Barrel stabilizing and recoil reducing muzzle brake |
| US11280572B2 (en) | 2016-03-10 | 2022-03-22 | James Norman Griffitts | Barrel stabilizing and recoil reducing muzzle brake with guiding ribs |
| US12163750B2 (en) | 2021-02-12 | 2024-12-10 | James Norman Griffitts | Sound suppressor with adapter for use with muzzle accessory |
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| US85949A (en) * | 1869-01-19 | James a | ||
| US329303A (en) * | 1885-10-27 | fosbery | ||
| US592437A (en) * | 1897-10-26 | Peter oberhammer | ||
| US786230A (en) * | 1904-01-26 | 1905-03-28 | Samuel N Mcclean | Recoil-controlling means for guns. |
| US785975A (en) * | 1904-07-01 | 1905-03-28 | Samuel N Mcclean | Means for controlling the recoil and muzzle-blast of guns. |
| US1082916A (en) * | 1912-04-08 | 1913-12-30 | William H Squire | Gas-operated gun. |
| US1380171A (en) * | 1919-01-11 | 1921-05-31 | Charles G Abbot | Ordnance |
| US1773260A (en) * | 1928-04-26 | 1930-08-19 | Richard M Cutts | Compensator device |
| US1944883A (en) * | 1929-12-24 | 1934-01-30 | Gerlich Hermann | Projectile propelling apparatus |
| GB437027A (en) * | 1934-04-23 | 1935-10-21 | Percy Wilderman | Pressure relief chambers, cavities and the like to be used in fire-arms |
| US2322370A (en) * | 1939-08-11 | 1943-06-22 | Robert C Lance | Lift compensator for firearms |
-
1945
- 1945-04-17 US US588878A patent/US2742821A/en not_active Expired - Lifetime
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US85949A (en) * | 1869-01-19 | James a | ||
| US329303A (en) * | 1885-10-27 | fosbery | ||
| US592437A (en) * | 1897-10-26 | Peter oberhammer | ||
| US786230A (en) * | 1904-01-26 | 1905-03-28 | Samuel N Mcclean | Recoil-controlling means for guns. |
| US785975A (en) * | 1904-07-01 | 1905-03-28 | Samuel N Mcclean | Means for controlling the recoil and muzzle-blast of guns. |
| US1082916A (en) * | 1912-04-08 | 1913-12-30 | William H Squire | Gas-operated gun. |
| US1380171A (en) * | 1919-01-11 | 1921-05-31 | Charles G Abbot | Ordnance |
| US1773260A (en) * | 1928-04-26 | 1930-08-19 | Richard M Cutts | Compensator device |
| US1944883A (en) * | 1929-12-24 | 1934-01-30 | Gerlich Hermann | Projectile propelling apparatus |
| GB437027A (en) * | 1934-04-23 | 1935-10-21 | Percy Wilderman | Pressure relief chambers, cavities and the like to be used in fire-arms |
| US2322370A (en) * | 1939-08-11 | 1943-06-22 | Robert C Lance | Lift compensator for firearms |
Cited By (40)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2842024A (en) * | 1954-12-07 | 1958-07-08 | John F Mutter | Anti-recoil gun barrels |
| US2916970A (en) * | 1956-02-10 | 1959-12-15 | John F Mutter | Anti-recoil gun barrels |
| US3418741A (en) * | 1965-09-08 | 1968-12-31 | Dynamit Nobel Ag | Firearm |
| US3412641A (en) * | 1966-06-27 | 1968-11-26 | Mb Assoc | Pistol for firing a miniature ballistic rocket |
| US3664052A (en) * | 1970-04-02 | 1972-05-23 | Bruce Mounier | Impact actuated underwater gun |
| US4176487A (en) * | 1970-11-18 | 1979-12-04 | Manis John R | Firearm barrels and projectiles |
| US4379531A (en) * | 1970-11-18 | 1983-04-12 | Manis John R | Projectile |
| US3808943A (en) * | 1972-04-27 | 1974-05-07 | L Kelly | Gun-leveling device |
| US4852460A (en) * | 1988-05-04 | 1989-08-01 | Davidson Windell L | Muzzle brake system |
| US4947729A (en) * | 1989-06-19 | 1990-08-14 | Timothy Downey | Spin stabilizing gun |
| US5249385A (en) * | 1992-03-24 | 1993-10-05 | Vang Hans J | Shotgun barrel |
| US5272827A (en) * | 1992-03-24 | 1993-12-28 | Vang Hans J | Shotgun barrel |
| US5394634A (en) * | 1992-03-24 | 1995-03-07 | Hans J. Vang | Shotgun barrel |
| US7174833B2 (en) | 2000-06-09 | 2007-02-13 | Diller E Wendell | Shotgun shell flight path indicator |
| US6886468B2 (en) | 2000-06-09 | 2005-05-03 | E. Wendell Diller | Shotgun shell flight path indicator |
| US20050188882A1 (en) * | 2000-06-09 | 2005-09-01 | Diller E. W. | Shotgun shell flight path indicator |
| US20050188881A1 (en) * | 2000-06-09 | 2005-09-01 | Diller E. W. | Shotgun shell flight path indicator |
| US6694887B2 (en) | 2000-06-09 | 2004-02-24 | E. Wendell Diller | Shotgun shell flight path indicator |
| US7171904B2 (en) | 2000-06-09 | 2007-02-06 | Diller E Wendell | Shotgun shell flight path indicator |
| US20030024377A1 (en) * | 2001-08-03 | 2003-02-06 | Diller E. Wendell | Elongated vented gun barrel |
| US20100281743A1 (en) * | 2003-08-28 | 2010-11-11 | Ra Brands, L.L.C. | Modular Barrel Assembly |
| US7866079B2 (en) * | 2003-08-28 | 2011-01-11 | Ra Brands, L.L.C. | Modular barrel assembly |
| US20060207154A1 (en) * | 2005-03-19 | 2006-09-21 | Lazor Ernest R | Improved shotgun barrel construction |
| US20090151729A1 (en) * | 2005-11-08 | 2009-06-18 | Resmed Limited | Nasal Assembly |
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| US10422603B2 (en) | 2016-03-10 | 2019-09-24 | James Norman Griffitts | Barrel stabilizing and recoil reducing muzzle brake |
| US11280572B2 (en) | 2016-03-10 | 2022-03-22 | James Norman Griffitts | Barrel stabilizing and recoil reducing muzzle brake with guiding ribs |
| US10197351B2 (en) * | 2016-03-10 | 2019-02-05 | James Norman Griffitts | Barrel stabilizing and recoil reducing muzzle brake |
| US9885533B2 (en) | 2016-03-10 | 2018-02-06 | James Norman Griffitts | Barrel stabalizing and recoil reducing muzzle brake |
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| US12163750B2 (en) | 2021-02-12 | 2024-12-10 | James Norman Griffitts | Sound suppressor with adapter for use with muzzle accessory |
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