US3896732A - Multi-section projectile and means for firing the same - Google Patents
Multi-section projectile and means for firing the same Download PDFInfo
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- US3896732A US3896732A US309225A US30922572A US3896732A US 3896732 A US3896732 A US 3896732A US 309225 A US309225 A US 309225A US 30922572 A US30922572 A US 30922572A US 3896732 A US3896732 A US 3896732A
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- Expired - Lifetime
Links
- 238000010304 firing Methods 0.000 title claims description 11
- 239000003380 propellant Substances 0.000 claims description 8
- 239000006185 dispersion Substances 0.000 abstract description 7
- 239000007789 gas Substances 0.000 description 4
- 229910000831 Steel Inorganic materials 0.000 description 3
- 239000010959 steel Substances 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 231100000518 lethal Toxicity 0.000 description 2
- 230000001665 lethal effect Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- JFALSRSLKYAFGM-UHFFFAOYSA-N uranium(0) Chemical compound [U] JFALSRSLKYAFGM-UHFFFAOYSA-N 0.000 description 2
- HRPVXLWXLXDGHG-UHFFFAOYSA-N Acrylamide Chemical compound NC(=O)C=C HRPVXLWXLXDGHG-UHFFFAOYSA-N 0.000 description 1
- 229910001369 Brass Inorganic materials 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 229910052770 Uranium Inorganic materials 0.000 description 1
- 229910001080 W alloy Inorganic materials 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 239000010951 brass Substances 0.000 description 1
- 230000002079 cooperative effect Effects 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 230000000875 corresponding effect Effects 0.000 description 1
- -1 e.g. Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
- 238000000605 extraction Methods 0.000 description 1
- 239000011133 lead Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 239000012188 paraffin wax Substances 0.000 description 1
- 230000000979 retarding effect Effects 0.000 description 1
- 238000009987 spinning Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
- F42B5/02—Cartridges, i.e. cases with charge and missile
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
- F42B5/02—Cartridges, i.e. cases with charge and missile
- F42B5/03—Cartridges, i.e. cases with charge and missile containing more than one missile
Definitions
- a plurality of generally disclike elements are unitarily arranged in stacked, face contacting relation within a [52] US. Cl 102/38; lO2/92.l Cartridge
- the projectile element edges are formed [51] hit. Cl. F421) 5/02 into a Set of teeth or projections for Cooperation with [58] held of Search 102/38 92-6; similarly dimensioned toothed tracks to produce ele- 89/l4 R; 42/78 ment rotation for movement along guide grooves extending longitudinally within a gun barrel.
- the guide grooves are fanned out a predeter- UNITED STATES PATENTS mined amount in the region immediately adjacent the 616,721 12/1898 Muthherr 102/38 m zzl to produce a prescribed element dispersion.
- Another object is the provision of a multi-section projectile, the parts of which on firing are each imparted with rotative as well as translational motion improving dynamic stability.
- a further object is the provision of a multi-part projectile, the parts. of which closely fit within grooves in a gun barrel so that during initial firing stages an effective gas seal is maintained between the projectile and gun barrel.
- a still further object is the provision of gun barrel means for the multi-section projectile described in the above objects in which guiding grooves direct the projectile sections along respective paths producing a wedgelike dispersal pattern at a prescribed distance.
- the multi-sectionprojectile includes a plurality of m stacked, face contacting relation within a cartridge.
- the projectile element edges are formed into a set of teeth orprojections which cooperate with similarly dimensioned toothed tracks for rotative movement along guide grooves extending longitudinally within a gun barrel.
- the cartridge is located within the .gun chamber with the element stack extending transverse of the barrel and the elementsindividually edge-alignedto the guide grooves.
- the guide grooves are fanned out a predetermined amount in the region immediately adjacent the muzzle to produce a prescribed element dispersion.
- FIG. 1 is a perspective view of a cartridge including the multi-section projectile or bullet of the present invention.
- FIG. 2 is a perspective view of one element of the multi-section projectile or bullet of FIG. 1.
- FIG. 3 is a sectional, elevational view taken along line 3-3 of the cartridge in FIG. 1.
- FIG. 4 is an elevational view in section of the cartridge of FIG. 1 within the gun chamber also depicting movement of a projectile element along the gun barrel.
- FIG. 5 is a transverse sectional view taken along line 55 in FIG. 4.
- FIG. 6 is a plan, sectional view of the barrel end portion especially adapted for use in propulsion of the multi-section projectile of this invention.
- a cartridge assembly 10 is seen to include a hollow cartridge case 11 having a primer assembly 12 in its closed end wall, a quantity of propellant 13, amulti-section bullet or projectile 14 to be more .fully described, and an end wad 15.
- the cartridge case 11 can be made of, optionally, brass, steel or aluminum and is of conventional construction other than having a generally rectangular cross-section for accommodating the multi-section projectile.
- the primer may be any one of a number of different commercially or militarily available primers for small arms.
- the propellant 13 may be selected from any number of known substances, and the wad 15 typically may be made of paraffin wax, or the like.
- the multi-section projectile 14 includes a plurality of identical circular disclike elements 16, the peripheries of which are formed into a continuous set of equally spaced teeth 17.
- the elements have their edge margins beveled to a substantial knife edge 18 as seen best in FIGS. 2 and 5. s
- the elements 16 may be constructed of any of the usualgbullet materials, e.g., lead, steel, copper, uranium, tungsten, or any other metal having sufficient strength and rigidity to withstand propulsion. Evaluation tests indicate that depleted uranium is a near opti- -mum material from which to construct elements 16.
- Tungsten alloys closely follow with steel next.
- the elements 16 are stacked in side by side, face contacting relation and inserted into the open end of the cartridge case 11 with the ,edges facing outwardly.
- the case is crimped as at l9 tov secure the projectile elements therewithin and to align the element teeth transversely of the case. End wad 15 then closes the outer case opening.
- the gun chamber 20 is formed to receive the cartridge 10 in a tight fitting relation.
- the upperinner surfaces of the barrel 21 includes a first set of longitudinally extending grooves 22 of transverse dimension and mutual spacing identical to that of theelements 16 forming the projectile 14.
- a second set 23 of similar longitudinal grooves is provided along the lowerinside barrel surface, the grooves of the second set being aligned with and in vertical registry with the grooves 22.
- the leading end of the cartridge 10 abuts against a shoulder- 24 defining the beginning of the gun barrel, and also, the beginning of the two sets 22 and 23 of guide grooves.
- a shoulder- 24 defining the beginning of the gun barrel, and also, the beginning of the two sets 22 and 23 of guide grooves.
- toothlike projections 25 of dimensions for cooperative action with the bullet element teeth 17 in a way that will be described.
- the elements 16 move into the chamber with their upper edges being received in the upper set of grooves 22 (FIG. 4). Also, as the elements 16 leave the cartridge case, rotation is initiated by the crimped portion 19 retarding the elements lower edges. On the elements leaving the cartridge case, the lower element edge teeth engage the projections 25 which continues the rotative motion for each element as it simultaneously moves outwardly along the gun barrel. During such movement along the barrel the grooves 22 and 23 maintain the element upright throughout the barrel length so that they are emitted from the muzzle substantially in a line with their edges facing the target. In addition, since the grooves 22 are 23 are formed to closely match the beveled element edges and teeth a gas seal is achieved enhancing propulsion.
- FIG. 6 An alternate form of gun barrel is that shown in FIG. 6 which obtains a wider dispersion of the bullet elements than that achieved by the first described embodiment.
- the grooves are straight-line throughout the entire barrel length.
- the grooves in the region 26 immediately adjacent the muzzle curve away from each other or fan out a slight amount.
- the propellant gases leak past the elements just before they leave the muzzle.
- each bullet element 16 comprises a disclike body member 0.25 inches in diameter and 0.025 inches thick with 8l0 teeth. Fifty elements stacked in side-by-side relation form a multi-section bullet 1.25 inches by 0.25 inches. It has been found that vertical dispersion, i.e., measured transversely of the element stack, was approximately 1 foot at a distance of 100 feet down range, or substantially 0.5". Lateral dispersion, on the other hand, at the same distance down range was to 10 feet, or 3 to 6. The disc elements spread out generally uniformly and retain their edge forward orientation during flight. In addition, depending on the initial yaw position, some precession of the spinning elements occurs producing a wedgeshaped pattern which may be considered lethal anywhere within the range of 0-300 feet.
- a multi-section projectile or bullet readily adaptable for firing from a number of different kinds of weapons including hand-held and shoulderfired varieties.
- the different bullet sections or parts separate on firing to form a wedge-shaped pattern that is lethal for an extended range.
- each of the bullet sections spins in the plane of the direction of movement, whereby it is gyroscopically stabilized with its momentum vector perpendicular to the line of flight.
- a multisection bullet in which the pattern achieved upon dispersal downrange can be controlled by modifying the rate of gyroscopic precession.
- the angle of dispersion produced at the muzzle of the barrel (FIG. 6) will in turn produce a certain rate of gyroscopic precession effecting a corresponding pattern change.
- bullet elements 16 may be made in a conventional disc of uniform thickness throughout, it is advantageous to bevel the edges as in the described embodiments, not only to produce a gas seal as was described, but also to reduce aerodynamic drag during flight.
- a multi-section bullet and cartridge assembly comprising:
- a cartridge casing including a primer and propellant and having portions thereof defining an opening
- said casing portions defining the opening being formed into at least one line of crimp along one side only of the stack and interacting with said ele' ments to impart a spin to said elements in a common direction as said elements leave said casing.
- a multi-section bullet and easing assembly comprising:
- a multi-section bullet and easing assembly comprising;
- -a casing including a primer and propellant and having portions thereof defining an opening
- said casing portions defining the opening including at least one crimp line extending along one side of the stack of elements and engaging the toothed edges thereof such that on firing spin is imparted to each element.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
Abstract
A plurality of generally disclike elements are unitarily arranged in stacked, face contacting relation within a cartridge. The projectile element edges are formed into a set of teeth or projections for cooperation with similarly dimensioned toothed tracks to produce element rotation for movement along guide grooves extending longitudinally within a gun barrel. As a further aspect, the guide grooves are fanned out a predetermined amount in the region immediately adjacent the muzzle to produce a prescribed element dispersion.
Description
Elnited States Patent Schaffer July 29, 1975 [54] MULTLSECTION PROJECTILE AND 1,302,720 5/1919 Schultz 89/14 R 1,777,519 10/1930 Flowers 42/78 MEANS FOR FIRING THE SAME 2,433,334 12/1947 Birkeland... 102/38 X [75} Inventor: Marvin B. Schaffer, Pacific 2,706,356 4/1955 De Vita l02/38 X Palisades, Calif.
[73] Assignee: R & D Associates, Santa Monica, Primary Examinersamuel Feinberg C lif Assistant Examiner-H. J. Tudor {22] Filed: Nov. 24, 1972 57 ABSTRACT [21] Appl. No.: 309,225
A plurality of generally disclike elements are unitarily arranged in stacked, face contacting relation within a [52] US. Cl 102/38; lO2/92.l Cartridge The projectile element edges are formed [51] hit. Cl. F421) 5/02 into a Set of teeth or projections for Cooperation with [58] held of Search 102/38 92-6; similarly dimensioned toothed tracks to produce ele- 89/l4 R; 42/78 ment rotation for movement along guide grooves extending longitudinally within a gun barrel. As a further [56] References Cned aspect, the guide grooves are fanned out a predeter- UNITED STATES PATENTS mined amount in the region immediately adjacent the 616,721 12/1898 Muthherr 102/38 m zzl to produce a prescribed element dispersion. 694,675 3/1902 Scott 102/38 UX 1,204,282 11/1916 Lake 89/14 R 3 Claims, 6 Drawmg Flgures generally disclike elements unitarily. arranged 1 MULTI-SECTION PROJECTILE AND NEANS FOR FIRING THE SAME FIELD OF THE INVENTION OBJECTS AND SUMMARY It is, therefore, a primary object of this invention to provide an improved multi-part projectile which on firing presents an extended bandlike pattern.
Another object is the provision of a multi-section projectile, the parts of which on firing are each imparted with rotative as well as translational motion improving dynamic stability. 1
A further object is the provision of a multi-part projectile, the parts. of which closely fit within grooves in a gun barrel so that during initial firing stages an effective gas seal is maintained between the projectile and gun barrel. 7 I
A still further object is the provision of gun barrel means for the multi-section projectile described in the above objects in which guiding grooves direct the projectile sections along respective paths producing a wedgelike dispersal pattern at a prescribed distance.
In accordance withthe practice of the present-invention the multi-sectionprojectile includes a plurality of m stacked, face contacting relation within a cartridge. The projectile element edges are formed into a set of teeth orprojections which cooperate with similarly dimensioned toothed tracks for rotative movement along guide grooves extending longitudinally within a gun barrel. The cartridge is located within the .gun chamber with the element stack extending transverse of the barrel and the elementsindividually edge-alignedto the guide grooves. As a further aspect, the guide grooves are fanned out a predetermined amount in the region immediately adjacent the muzzle to produce a prescribed element dispersion.
DESCRIPTION OF THE DRAWINGS I FIG. 1 is a perspective view of a cartridge including the multi-section projectile or bullet of the present invention.
FIG. 2 is a perspective view of one element of the multi-section projectile or bullet of FIG. 1.
FIG. 3 is a sectional, elevational view taken along line 3-3 of the cartridge in FIG. 1.
FIG. 4 is an elevational view in section of the cartridge of FIG. 1 within the gun chamber also depicting movement of a projectile element along the gun barrel.
FIG. 5 is a transverse sectional view taken along line 55 in FIG. 4.
FIG. 6 is a plan, sectional view of the barrel end portion especially adapted for use in propulsion of the multi-section projectile of this invention.
DESCRIPTION OF A PREFERRED EMBODIMENT Turning now to the drawings, and particularly to FIGS. 1 and 3, a cartridge assembly 10 is seen to include a hollow cartridge case 11 having a primer assembly 12 in its closed end wall, a quantity of propellant 13, amulti-section bullet or projectile 14 to be more .fully described, and an end wad 15. The cartridge case 11 can be made of, optionally, brass, steel or aluminum and is of conventional construction other than having a generally rectangular cross-section for accommodating the multi-section projectile. The primer may be any one of a number of different commercially or militarily available primers for small arms. Similarly, the propellant 13 may be selected from any number of known substances, and the wad 15 typically may be made of paraffin wax, or the like.
The multi-section projectile 14 includes a plurality of identical circular disclike elements 16, the peripheries of which are formed into a continuous set of equally spaced teeth 17. The elements have their edge margins beveled to a substantial knife edge 18 as seen best in FIGS. 2 and 5. s
The elements 16 may be constructed of any of the usualgbullet materials, e.g., lead, steel, copper, uranium, tungsten, or any other metal having sufficient strength and rigidity to withstand propulsion. Evaluation tests indicate that depleted uranium is a near opti- -mum material from which to construct elements 16.
Tungsten alloys closely follow with steel next.
In assembly after the propellant is added, the elements 16 are stacked in side by side, face contacting relation and inserted into the open end of the cartridge case 11 with the ,edges facing outwardly. The case is crimped as at l9 tov secure the projectile elements therewithin and to align the element teeth transversely of the case. End wad 15 then closes the outer case opening.
As shown best in FIG. 4, the gun chamber 20 is formed to receive the cartridge 10 in a tight fitting relation. The upperinner surfaces of the barrel 21 includes a first set of longitudinally extending grooves 22 of transverse dimension and mutual spacing identical to that of theelements 16 forming the projectile 14. A second set 23 of similar longitudinal grooves is provided along the lowerinside barrel surface, the grooves of the second set being aligned with and in vertical registry with the grooves 22.
The leading end of the cartridge 10 abuts against a shoulder- 24 defining the beginning of the gun barrel, and also, the beginning of the two sets 22 and 23 of guide grooves. Fora short distance along the lower grooves from the shoulder 24, there are provided toothlike projections 25 of dimensions for cooperative action with the bullet element teeth 17 in a way that will be described.
For satisfactory operation there are also required additional apparatus such as a trigger mechanism, stock or grip, magazine, extraction means and sight, for example. All of these may be of conventional construction and do not form a part of the present invention.
When the cartridge 10 in the chamber 20 is fired, the elements 16 move into the chamber with their upper edges being received in the upper set of grooves 22 (FIG. 4). Also, as the elements 16 leave the cartridge case, rotation is initiated by the crimped portion 19 retarding the elements lower edges. On the elements leaving the cartridge case, the lower element edge teeth engage the projections 25 which continues the rotative motion for each element as it simultaneously moves outwardly along the gun barrel. During such movement along the barrel the grooves 22 and 23 maintain the element upright throughout the barrel length so that they are emitted from the muzzle substantially in a line with their edges facing the target. In addition, since the grooves 22 are 23 are formed to closely match the beveled element edges and teeth a gas seal is achieved enhancing propulsion.
An alternate form of gun barrel is that shown in FIG. 6 which obtains a wider dispersion of the bullet elements than that achieved by the first described embodiment. Thus, whereas in the first barrel form the grooves are straight-line throughout the entire barrel length. in this alternate version the grooves in the region 26 immediately adjacent the muzzle curve away from each other or fan out a slight amount. As the multi-section bullet'reaches the region 26, the propellant gases leak past the elements just before they leave the muzzle. Moreover, since the guide grooves diverge, this effects a dispersal of the elements.
Illustrative of a practical embodiment for use in a hand-held or shoulder-fired weapon, each bullet element 16 comprises a disclike body member 0.25 inches in diameter and 0.025 inches thick with 8l0 teeth. Fifty elements stacked in side-by-side relation form a multi-section bullet 1.25 inches by 0.25 inches. It has been found that vertical dispersion, i.e., measured transversely of the element stack, was approximately 1 foot at a distance of 100 feet down range, or substantially 0.5". Lateral dispersion, on the other hand, at the same distance down range was to 10 feet, or 3 to 6. The disc elements spread out generally uniformly and retain their edge forward orientation during flight. In addition, depending on the initial yaw position, some precession of the spinning elements occurs producing a wedgeshaped pattern which may be considered lethal anywhere within the range of 0-300 feet.
There is provided in accordance with the practice of this invention a multi-section projectile or bullet readily adaptable for firing from a number of different kinds of weapons including hand-held and shoulderfired varieties. The different bullet sections or parts separate on firing to form a wedge-shaped pattern that is lethal for an extended range. Moreover, each of the bullet sections spins in the plane of the direction of movement, whereby it is gyroscopically stabilized with its momentum vector perpendicular to the line of flight.
As a further aspect of the subject invention, a multisection bullet is provided in which the pattern achieved upon dispersal downrange can be controlled by modifying the rate of gyroscopic precession. Thus, the angle of dispersion produced at the muzzle of the barrel (FIG. 6) will in turn produce a certain rate of gyroscopic precession effecting a corresponding pattern change.
Although the bullet elements 16 may be made in a conventional disc of uniform thickness throughout, it is advantageous to bevel the edges as in the described embodiments, not only to produce a gas seal as was described, but also to reduce aerodynamic drag during flight.
What is claimed is:
l. A multi-section bullet and cartridge assembly, comprising:
a cartridge casing including a primer and propellant and having portions thereof defining an opening;
a plurality of flat elements arranged in a face-to-face stack secured within the casing opening with the element edges facing outwardly of the opening; and
said casing portions defining the opening being formed into at least one line of crimp along one side only of the stack and interacting with said ele' ments to impart a spin to said elements in a common direction as said elements leave said casing.
2. A multi-section bullet and easing assembly. comprising:
a casing having portions terminating in an opening;
and
a plurality of bullet sections each clampingly received within said casing opening at one side only such that on firing said bullet sections are each gyroscopically stabilized during flight with the momentum vector of each being substantially'perpendicular to the line of flight and in the same directron.
3. A multi-section bullet and easing assembly, comprising;
-a casing including a primer and propellant and having portions thereof defining an opening;
a plurality of tooth-edged disclike elements of substantially identical geometry stackingly received within said casing opening with the element edges facing outwardly of said casing opening; and
said casing portions defining the opening including at least one crimp line extending along one side of the stack of elements and engaging the toothed edges thereof such that on firing spin is imparted to each element.
Claims (3)
1. A multi-section bullet and cartridge assembly, comprising: a cartridge casing including a primer and propellant and having portions thereof defining an opening; a plurality of flat elements arranged in a face-to-face stack secured within the casing opening with the element edges facing outwardly of the opening; and said casing portions defining the opening being formed into at least one line of crimp along one side only of the stack and interacting with said elements to impart a spin to said elements in a common direction as said elements leave said casing.
2. A multi-section bullet and casing assembly, comprising: a casing having portions terminating in an opening; and a plurality of bullet sections each clampingly received within said casing opening at one side only such that on firing said bullet sections are each gyroscopically stabilized during flight with the momentum vector of each being substantially perpendicular to the line of flight and in the same direction.
3. A multi-section bullet and casing assembly, comprising; a casing including a primer and propellant and having portions thereof defining an opening; a plurality of tooth-edged disclike elements of substantially identical geometry stackingly received within said casing opening with the element edges faciNg outwardly of said casing opening; and said casing portions defining the opening including at least one crimp line extending along one side of the stack of elements and engaging the toothed edges thereof such that on firing spin is imparted to each element.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US309225A US3896732A (en) | 1972-11-24 | 1972-11-24 | Multi-section projectile and means for firing the same |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US309225A US3896732A (en) | 1972-11-24 | 1972-11-24 | Multi-section projectile and means for firing the same |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3896732A true US3896732A (en) | 1975-07-29 |
Family
ID=23197256
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US309225A Expired - Lifetime US3896732A (en) | 1972-11-24 | 1972-11-24 | Multi-section projectile and means for firing the same |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3896732A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4577813A (en) * | 1979-05-07 | 1986-03-25 | Rheinmetall Gmbh | Discus-shaped projectile |
| US4653403A (en) * | 1981-12-28 | 1987-03-31 | Gibbs Robert L | Cartridge-launched, disk-deployed chaff |
| US4683824A (en) * | 1983-01-26 | 1987-08-04 | Gibbs Robert L | Cartridge launched - disk deployed chaff |
| US20050150413A1 (en) * | 2003-12-12 | 2005-07-14 | Lord Steven M. | Firearms cartridge with rectangular, rounded oblong, or elliptical casing |
| US20110185936A1 (en) * | 2010-01-08 | 2011-08-04 | Richardson Matthew D | Shotshell with combination load for personal defense |
| US20230124564A1 (en) * | 2020-06-23 | 2023-04-20 | Diehl Metall Stiftung & Co. Kg | Base part for producing a cartridge case and cartridge case, method for producing a base part for a cartridge case, and method for producing a cartridge case |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US616721A (en) * | 1898-12-27 | Josef mutiiiierr | ||
| US694675A (en) * | 1901-10-24 | 1902-03-04 | Louis N D Williams | Gun-cartridge. |
| US1204282A (en) * | 1916-01-22 | 1916-11-07 | Robert H Lake | Disk-throwing gun. |
| US1302720A (en) * | 1918-04-03 | 1919-05-06 | Karl A Schultz | Projectile. |
| US1777519A (en) * | 1929-09-20 | 1930-10-07 | Thomas E Flowers | Cartridge |
| US2433334A (en) * | 1944-01-11 | 1947-12-30 | Birkeland Leigh Forstner | Ammunition |
| US2706356A (en) * | 1951-04-02 | 1955-04-19 | Vita Victor A De | Multi-bullet machine gun barrel |
-
1972
- 1972-11-24 US US309225A patent/US3896732A/en not_active Expired - Lifetime
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US616721A (en) * | 1898-12-27 | Josef mutiiiierr | ||
| US694675A (en) * | 1901-10-24 | 1902-03-04 | Louis N D Williams | Gun-cartridge. |
| US1204282A (en) * | 1916-01-22 | 1916-11-07 | Robert H Lake | Disk-throwing gun. |
| US1302720A (en) * | 1918-04-03 | 1919-05-06 | Karl A Schultz | Projectile. |
| US1777519A (en) * | 1929-09-20 | 1930-10-07 | Thomas E Flowers | Cartridge |
| US2433334A (en) * | 1944-01-11 | 1947-12-30 | Birkeland Leigh Forstner | Ammunition |
| US2706356A (en) * | 1951-04-02 | 1955-04-19 | Vita Victor A De | Multi-bullet machine gun barrel |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4577813A (en) * | 1979-05-07 | 1986-03-25 | Rheinmetall Gmbh | Discus-shaped projectile |
| US4653403A (en) * | 1981-12-28 | 1987-03-31 | Gibbs Robert L | Cartridge-launched, disk-deployed chaff |
| US4683824A (en) * | 1983-01-26 | 1987-08-04 | Gibbs Robert L | Cartridge launched - disk deployed chaff |
| US20050150413A1 (en) * | 2003-12-12 | 2005-07-14 | Lord Steven M. | Firearms cartridge with rectangular, rounded oblong, or elliptical casing |
| US20110185936A1 (en) * | 2010-01-08 | 2011-08-04 | Richardson Matthew D | Shotshell with combination load for personal defense |
| US20230124564A1 (en) * | 2020-06-23 | 2023-04-20 | Diehl Metall Stiftung & Co. Kg | Base part for producing a cartridge case and cartridge case, method for producing a base part for a cartridge case, and method for producing a cartridge case |
| US12366438B2 (en) * | 2020-06-23 | 2025-07-22 | Diehl Metall Stiftung & Co. Kg | Base part for producing a cartridge case and cartridge case, method for producing a base part for a cartridge case, and method for producing a cartridge case |
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