US3151412A - Firearm barrel with grooves and projectile with fins fitting in said grooves - Google Patents

Firearm barrel with grooves and projectile with fins fitting in said grooves Download PDF

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US3151412A
US3151412A US163657A US16365762A US3151412A US 3151412 A US3151412 A US 3151412A US 163657 A US163657 A US 163657A US 16365762 A US16365762 A US 16365762A US 3151412 A US3151412 A US 3151412A
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projectile
grooves
bore
barrel
chamber
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US163657A
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Kenneth C Swindle
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    • 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
    • F41A21/18—Grooves-Rifling
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/02—Stabilising arrangements
    • F42B10/04—Stabilising arrangements using fixed fins

Definitions

  • This invention relates to a firearm and has for an object to provide a combination of a barrel and projectile that is efiicient, yet inexpensive to manufacture, and provides for a wide range of design for both long and short propulsion range.
  • Another object of the invention is to provide a combination as above characterized that has accuracy of projectile flight at a flatter than normal trajectory and in which barrel rifling is omitted while still retaining projectile stability during propulsion thereof.
  • a further object of the invention is to provide, in a combination as indicated, a fin-stabilized projectile and a barrel that so guides the fins of the projectile that flight accuracy results.
  • This invention also has for its objects to provide such means that arepositive in operation, convenient in use, easily installed in a Working position and easily disconnected therefrom, economical of manufacture, relatively simple, and of general superiority and serviceability.
  • the invention also comprises novel details of construction and novel combinations and arrangements of parts, which will more fully appear in the course of the following description and which is based on the accompanying drawing.
  • said drawing merely shows, and the following description merely describes, preferred embodiments of the present invention, which are given by way of illustration or example only.
  • FIG. 1 is a broken longitudinal sectional view of a firearm according to the present invention.
  • FIG. 2 is a cross-sectional view as taken on the line 2-2 of FIG. 1.
  • FIG. 3 is a cross-sectional view of the barrel as seen from the right end of FIG. 1.
  • FIG. 4 is a side elevational view, partly broken away, of the projectile shown in FIG. 1.
  • FIG. 5 is a side elevational view of a modification.
  • the firearm that is illustrated comprises, in combination, a barrel it), a projectile 11 cooperatively engaged with the barrel, and a cartridge case 12 into which the projectile is fitted.
  • the barrel may be made of any suitable rigid material, as steel or plastic, depending on the use to which the firearm is to be put.
  • said barrel is provided with a bore 15 from which radiates a plurality of radial grooves 16 that are uniformly circumferentially spaced.
  • the drawing shows four such grooves, but three may be used or a greater number than four.
  • Said bore opens into a cartridge chamber 17, a conical lead-in throat I8 constituting a transition chamber space between the bore and the chamber to guide the projectile 11 into the former.
  • Said lead-in throat 18 is formed to have sloping guide sides 19 that lead from the throat 18 to the grooves 16 for reasons later apparent.
  • the cartridge chamber 17 may be of any conventional design and is preferably as large or larger than the dimension across the outer edges of grooves 16, the chamber, thereby, freely passing the projectile 11 of the present combination.
  • the projectile ll of plastic, metal or any other suitable rigid material, comprises a body 20 with a preferably 3,151,412 Patented 0st. 6, 1964 pointed end 21 and formed of a size and elongated shape to have a sliding fit in the bore 15.
  • Each fin has a rearwardly sloping front edge 23 and rearwardly directed extensions 24 that are spaced from the body 24) and may extend rearwardly beyond the rearward end of said body.
  • Said body may be solid or hollow, as desired. If hollow, the same may be filled with a ballast material or with an explosive charge that is set ofi' on impact.
  • the outer surface of the projectile body is smooth and designed to have ballistic efiiciency and, therefore, the accuracy in flight that is provided by the stabilizing effect of the fins 22.
  • the cartridge case 12 has a rear body 25 that fits the chamber 17 and the same is preferably reducingly tapered toward the muzzle of the barrel 10.
  • said case, or itsequivalent may be percussed by an explosive charge or by compressed air or gas.
  • the body 25 terminates at its forward end in a conical part 26 that fits the lead-in throat 18 of the barrel, said part 26having a tubular extension 27 into which the rear end of the projectile body 20 is tightly fitted so that said body end is aubject to the propulsion forces generated in the cartridge case 12, as above described.
  • Said tubular extension resides in the spaces provided between the body 20 .and the fin extensions 24.
  • FIG. 5 shows the fins 22a on a small or fiat helical pitch, it being understood that the grooves for said fins will be similarly pitched. Thus, propulsion will result in a rotative movement of the projectile in flight, yet rotation-inducing rifting as practiced with malleable bullets is not used.

Description

Oct. 6, 1964 K. c. SWINDLE 3,151,412
EL WITH GROOVES AND PROJ ILE WITH ECT ES FIREARM BARR NS FITTING IN SAID GROOV Filed Jan. 2, 1962 'INVENTOR. Kim/Er firm/01 5 BY 5 g Mme/w? United States Patent l 3,151,412 FIREARM BAL WITH GROOVES AND PRGIEG TILE WITH FINS FITTEJG IN SAID 'GROOVES Kenneth C. Swindle, South El Monte, Califi, assignor to Jack Spencer, Big Bear Lake, Calif. Filed Jan. 2, 1962, Ser. No. 163,657 4- (Ilaims. (CI. 42-76) This invention relates to a firearm and has for an object to provide a combination of a barrel and projectile that is efiicient, yet inexpensive to manufacture, and provides for a wide range of design for both long and short propulsion range.
Another object of the invention is to provide a combination as above characterized that has accuracy of projectile flight at a flatter than normal trajectory and in which barrel rifling is omitted while still retaining projectile stability during propulsion thereof.
A further object of the invention is to provide, in a combination as indicated, a fin-stabilized projectile and a barrel that so guides the fins of the projectile that flight accuracy results.
This invention also has for its objects to provide such means that arepositive in operation, convenient in use, easily installed in a Working position and easily disconnected therefrom, economical of manufacture, relatively simple, and of general superiority and serviceability.
The invention also comprises novel details of construction and novel combinations and arrangements of parts, which will more fully appear in the course of the following description and which is based on the accompanying drawing. However, said drawing merely shows, and the following description merely describes, preferred embodiments of the present invention, which are given by way of illustration or example only.
In the drawing, like reference characters designate similar parts in the several views.
FIG. 1 is a broken longitudinal sectional view of a firearm according to the present invention.
FIG. 2 is a cross-sectional view as taken on the line 2-2 of FIG. 1.
FIG. 3 is a cross-sectional view of the barrel as seen from the right end of FIG. 1.
FIG. 4 is a side elevational view, partly broken away, of the projectile shown in FIG. 1.
FIG. 5, to a smaller scale, is a side elevational view of a modification.
The firearm that is illustrated comprises, in combination, a barrel it), a projectile 11 cooperatively engaged with the barrel, and a cartridge case 12 into which the projectile is fitted.
The barrel may be made of any suitable rigid material, as steel or plastic, depending on the use to which the firearm is to be put. In the present case, said barrel is provided with a bore 15 from which radiates a plurality of radial grooves 16 that are uniformly circumferentially spaced. The drawing shows four such grooves, but three may be used or a greater number than four.
Said bore opens into a cartridge chamber 17, a conical lead-in throat I8 constituting a transition chamber space between the bore and the chamber to guide the projectile 11 into the former. Said lead-in throat 18 is formed to have sloping guide sides 19 that lead from the throat 18 to the grooves 16 for reasons later apparent.
The cartridge chamber 17 may be of any conventional design and is preferably as large or larger than the dimension across the outer edges of grooves 16, the chamber, thereby, freely passing the projectile 11 of the present combination.
The projectile ll, of plastic, metal or any other suitable rigid material, comprises a body 20 with a preferably 3,151,412 Patented 0st. 6, 1964 pointed end 21 and formed of a size and elongated shape to have a sliding fit in the bore 15. A complement of fins 22, either integral or affixed, radiates from said body, said fins being of a depth and thickness to slidingly fit into the grooves 16. The same number of fins as grooves is used. Each fin has a rearwardly sloping front edge 23 and rearwardly directed extensions 24 that are spaced from the body 24) and may extend rearwardly beyond the rearward end of said body.
Said body may be solid or hollow, as desired. If hollow, the same may be filled with a ballast material or with an explosive charge that is set ofi' on impact. In any case, the outer surface of the projectile body is smooth and designed to have ballistic efiiciency and, therefore, the accuracy in flight that is provided by the stabilizing effect of the fins 22. a
The cartridge case 12 has a rear body 25 that fits the chamber 17 and the same is preferably reducingly tapered toward the muzzle of the barrel 10. In any of the usual conventional ways, said case, or itsequivalent, may be percussed by an explosive charge or by compressed air or gas.
The body 25 terminates at its forward end in a conical part 26 that fits the lead-in throat 18 of the barrel, said part 26having a tubular extension 27 into which the rear end of the projectile body 20 is tightly fitted so that said body end is aubject to the propulsion forces generated in the cartridge case 12, as above described. Said tubular extension resides in the spaces provided between the body 20 .and the fin extensions 24.
When a projectile is inserted, with its cartridge, into the barrel It the lead-in throat 18, together with the sloping sides 19, guides the fins 22 into the grooves 16, the sloping fin edges 23 aiding such insertion since the full widths of the fins do not achieve entry into grooves 16 until after the progressive entry of the lead-in ends of the fins.
It will be clear that percussion effective on the rearward end of the projectile body will propel the projectile from the bore 15 with the fins stabilized by their engagement with the grooves 16 to proxide the mentioned accuracy in flight of the projectile.
The modification of FIG. 5 shows the fins 22a on a small or fiat helical pitch, it being understood that the grooves for said fins will be similarly pitched. Thus, propulsion will result in a rotative movement of the projectile in flight, yet rotation-inducing rifting as practiced with malleable bullets is not used.
While the foregoing has illustrated and described what is now contemplated to be the best mode of carrying out the invention, the constructions are, of course, subject to modification without departing from the spirit and scope of the invention. Therefore, it is not desired to restrict the invention to the particular forms of construction illustrated and described, but to cover all modifications that may fall within the scope of the appended claims.
Having thus described this invention, what is claimed and desired to be secured by Letters Patent is:
1. In combination:
(a) a firearm barrel having a cylindrical bore in the wall thereof;
(b) a cylindrical projectile slidingly fitted in said bore;
(a) cartridge means comprising,
(1) a chamber in one end of the barrel wall larger in diameter than the bore thereof, and a conical transition space connecting said bore and chamber, and
(2) a cartridge case fitted into said chamber and provided with an extension into which an end of the projectile is fitted; and
(d) means to stabilize the flight of the projectile upon discharge from the barrel bore comprising,
(1) a plurality of parallel, longitudinal and circumferentially spaced grooves in said barrel wall extending radially from the barrel bore to a diametral size at least as large as the cartridge chamber, and
(2) a similar number of parallel fin extending radially from the portion of the projectile that extends beyond the end of the projectile in the cartridge case extension, said fins being fixed to the projectile and slidingly fitted into said grooves.
2. The combination according to claim 1 provided with a conical lead-in transition throat between the adjacent ends of the bore and cartridge chamber.
3. In combination:
(a) a firearm barrel having a cylindrical bore in the Wall thereof;
(b) a cylindrical projectile slidingly fitted in said bore;
(c) cartridge means comprising,
(1) a chamber in one end of the barrel wall larger in diameter than the bore thereof, and a conical transition space connecting said bore and chamher, and
(2) a cartridge case fitted into said chamber and provided with an extension into which an end of the projectile is fitted; and
(d) means to stabilize the flight of the projectile upon discharge from the barrel bore comprising,
(1) a plurality of parallel, longitudinal and circumferentially spaced grooves in said barrel wall extending radially from the barrel bore to a diametral size at least as large as the cartridge chamber, and
(2) a similar number of parallel fins extending radially from the portion of the projectile that extends beyond the end of the projectile in the cartridge case extension, said fins being fixed to the projectile and slidingly fitted into said grooves, the trailing ends of the fins extending beyond the trailing end of the projectile.
4. The combination according to claim 3 provided with a conical lead-in transition throat between the adjacent ends of the bore and cartridge chamber, the trailing ends of the fins terminating at a midpoint of the transition throat.
References Cited in the file of this patent UNITED STATES PATENTS 40,958 Somes Dec. 15, 1863 868,938 Pufi Oct. 22, 1907 1,546,842 Lafitte July 21, 1925 2,344,957 Anzalone Mar. 28, 1944 2,389,846 Ericson Nov. 27, 1945 2,426,239 Renner Aug. 26, 1947 3,009,393 Lynch Nov. 21, 1961 FOREIGN PATENTS 89,970 Sweden Aug. 10, 1 937

Claims (1)

1. IN COMBINATION: (A) A FIREARM BARREL HAVING A CYLINDRICAL BORE IN THE WALL THEREOF; (B) A CYLINDRICAL PROJECTILE SLIDINGLY FITTED IN SAID BORE; (C) CARTRIDGE MEANS COMPRISING, (1) A CHAMBER IN ONE END OF THE BARREL WALL LARGER IN DIAMETER THAN THE BORE THEREOF, AND A CONICAL TRANSITION SPACE CONNECTING SAID BORE AND CHAMBER, AND (2) A CARTRIDGE CASE FITTED INTO SAID CHAMBER AND PROVIDED WITH AN EXTENSION INTO WHICH AN END OF THE PROJECTILE IS FITTED; AND (D) MEANS TO STABILIZE THE FLIGHT OF THE PROJECTILE UPON DISCHARGE FROM THE BARREL BORE COMPRISING, (1) A PLURALITY OF PARALLEL, LONGITUDINAL AND CIRCUMFERENTIALLY SPACED GROOVES IN SAID BARREL WALL EXTENDING RADIALLY FROM THE BARREL BORE TO A DIAMETRIAL SIZE AT LEAST AS LARGE AS THE CARTRIDGE CHAMBER, AND (2) A SIMILAR NUMBER OF PARALLEL FINS EXTENDING RADIALLY FROM THE PORTION OF THE PROJECTILE THAT EXTENDS BEYOND THE END OF THE PROJECTILE IN THE CARTRIDGE CASE EXTENSION, SAID FINS BEING FIXED TO THE PROJECTILE AND SLIDINGLY FITTED INTO SAID GROOVES.
US163657A 1962-01-02 1962-01-02 Firearm barrel with grooves and projectile with fins fitting in said grooves Expired - Lifetime US3151412A (en)

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3225655A (en) * 1964-05-25 1965-12-28 Gen Dynamics Corp Controlled tip-off launcher
US3302525A (en) * 1965-05-06 1967-02-07 James P Haine Missile loading tray for breech-loaded gun-launchers
US20220307806A1 (en) * 2021-03-24 2022-09-29 Jamie George McWilliam Bullet Stabilization in Subsonic Flight

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US40958A (en) * 1863-12-15 Improvement in projectiles for ordnance
US868938A (en) * 1907-07-25 1907-10-22 Carl Puff Barrel for portable firearms and cannon with deepened grooves.
US1546842A (en) * 1923-01-08 1925-07-21 Lafitte Theodore Shell for infantry use
US2344957A (en) * 1940-01-12 1944-03-28 Aerial Products Inc Pistol rocket
US2389846A (en) * 1941-08-26 1945-11-27 George R Ericson High velocity projectile
US2426239A (en) * 1942-12-28 1947-08-26 Henry M Renner Rocket shell
US3009393A (en) * 1958-12-02 1961-11-21 Gen Dynamics Corp Missile launcher

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US40958A (en) * 1863-12-15 Improvement in projectiles for ordnance
US868938A (en) * 1907-07-25 1907-10-22 Carl Puff Barrel for portable firearms and cannon with deepened grooves.
US1546842A (en) * 1923-01-08 1925-07-21 Lafitte Theodore Shell for infantry use
US2344957A (en) * 1940-01-12 1944-03-28 Aerial Products Inc Pistol rocket
US2389846A (en) * 1941-08-26 1945-11-27 George R Ericson High velocity projectile
US2426239A (en) * 1942-12-28 1947-08-26 Henry M Renner Rocket shell
US3009393A (en) * 1958-12-02 1961-11-21 Gen Dynamics Corp Missile launcher

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3225655A (en) * 1964-05-25 1965-12-28 Gen Dynamics Corp Controlled tip-off launcher
US3302525A (en) * 1965-05-06 1967-02-07 James P Haine Missile loading tray for breech-loaded gun-launchers
US20220307806A1 (en) * 2021-03-24 2022-09-29 Jamie George McWilliam Bullet Stabilization in Subsonic Flight

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