US2991718A - Disintegrating ammunition for machine gun and cannon - Google Patents
Disintegrating ammunition for machine gun and cannon Download PDFInfo
- Publication number
- US2991718A US2991718A US820562A US82056259A US2991718A US 2991718 A US2991718 A US 2991718A US 820562 A US820562 A US 820562A US 82056259 A US82056259 A US 82056259A US 2991718 A US2991718 A US 2991718A
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- United States
- Prior art keywords
- disintegrating
- ammunition
- cannon
- weight
- lead
- 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.)
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/72—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material
- F42B12/76—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material of the casing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B8/00—Practice or training ammunition
- F42B8/12—Projectiles or missiles
- F42B8/14—Projectiles or missiles disintegrating in flight or upon impact
- F42B8/16—Projectiles or missiles disintegrating in flight or upon impact containing an inert filler in powder or granular form
Definitions
- This invention relates to disintegrating ammunition for testing fire control systems and more particularly to the construction of the bullet or slug.
- An object of the present invention is to eliminate the necessity for constructing expensive firing butts, wide angle and all angle ranges in order to test fire control systems at both manufacturers plants and military installations.
- a further object of the present invention is to provide disintegrating ammunition for testing machine guns, cannons and accessories thereto such as solenoids, boosters, heaters and chargers without the cost of construction of expensive testing ranges. It is a still further object of the invention to provide disintegrating ammunition that, when fired, will produce identical forces on the structure of the aircraft, gun mounts and other parts of the mounting structure as standard ball or test type ammunition.
- the bullet or slug comprises a thin substantially conically shaped outer shell, weighting means within said outer shell to provide accurate weight for said slug, and means closing the open end of said outer shell to prevent discharge of the weighting means.
- FIG. 1 is a sectional view of the bullet or slug of the present invention
- FIG. 2 is an end vieW of the bullet or slug of the present invention.
- FIG. 1 the bullet or slug of the present invention generally designated having a thin outer shell 12 of approximately of an inch in thickness.
- a driving band 14 is formed integral with said thin outer shell near the trailing end of the slug, said driving band 14 has a shoulder I16 positioned to abut the front edge of the charge containing cartridge casing (not shown).
- the thin outer shell 12 of the slug is filled with loose material 18 which may be any of a number of weighting materials such as powdered lead, lead shot or lead fragments.
- the loose material 18 is retained within the thin Patented July 11, 1961 ice outer shell 12 by means of paper wadding 20 which is inserted into the open end 22 of the shell 12.
- the preferred embodiment of the present invention will comprise a thin outer shell 12, 7 of an inch thick, and constructed in the form of a casted alloy shell consisting of bismuth, 25% lead, 12 /2% tin and 12 /2 cadmium, by weight, which will have a melting point of approximately 149 F.
- a casted alloy shell consisting of bismuth, 25% lead, 12 /2% tin and 12 /2 cadmium, by weight, which will have a melting point of approximately 149 F.
- the weight-producing material (18 is necessary to the proper functioning of the test ammunition since the weight of the test ammunition must be the same as an actual round to produce identical recoil and shock characteristics on the weapon being fired.
- a disintegrating projectile of the type described comprising a thin outer metal shell, said metal shell being a cast alloy of 50% bismuth, 25% lead, l2 /2% tin and 12 /2 cadmium, by weight, approximately of an inch thick, powdered lead disposed within said thin metal shell to approximate the weight of a standard projectile, and means sealing said powdered lead within said thin outer metal shell.
- a disintegrating projectile of the type described com prising a bullet-shaped thin outer metal shell approximately of an inch thick, said metal shell being a cast alloy of 50% bismuth, 25% lead, 12 /z% tin and 12V2% cadmium by weight, and means contained within said thin metal shell to approximate the weight of standard round.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
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- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Toys (AREA)
Description
July 11,
1961 R. M. FERGUSON 2,991,718
DISINTEGRATING AMMUNITION FOR MACHINE GUN AND CANNON Filed June 15, 1959 IN V EN TOR.
RALPH M. FERG USON United States Patent 2,991,718 DISINTEGRATING AMMUNITION FOR MACHINE GUN AND CANNON Ralph M. Ferguson, Dayton, Ohio, assignor t the United States of America as represented by the Secretary of the Air Force Filed June 15, 1959, Ser. No. 820,562 3 Claims. (Cl. 102-91) (Granted under Title 35, US. Code (1952), sec. 266) The invention described herein may be manufactured and used by or for the United States Government for governmental purposes without payment to me of any royalty thereon.
This invention relates to disintegrating ammunition for testing fire control systems and more particularly to the construction of the bullet or slug.
An object of the present invention is to eliminate the necessity for constructing expensive firing butts, wide angle and all angle ranges in order to test fire control systems at both manufacturers plants and military installations.
A further object of the present invention is to provide disintegrating ammunition for testing machine guns, cannons and accessories thereto such as solenoids, boosters, heaters and chargers without the cost of construction of expensive testing ranges. It is a still further object of the invention to provide disintegrating ammunition that, when fired, will produce identical forces on the structure of the aircraft, gun mounts and other parts of the mounting structure as standard ball or test type ammunition.
According to the present invention the bullet or slug comprises a thin substantially conically shaped outer shell, weighting means within said outer shell to provide accurate weight for said slug, and means closing the open end of said outer shell to prevent discharge of the weighting means.
These and other objects and features of the present invention are described below in connection with the accompanying drawings.
In the drawings:
FIG. 1 is a sectional view of the bullet or slug of the present invention;
FIG. 2 is an end vieW of the bullet or slug of the present invention.
Referring now in detail to the drawings wherein like reference numerals disingnate like parts and more particularly to FIG. 1 there is shown the bullet or slug of the present invention generally designated having a thin outer shell 12 of approximately of an inch in thickness. A driving band 14 is formed integral with said thin outer shell near the trailing end of the slug, said driving band 14 has a shoulder I16 positioned to abut the front edge of the charge containing cartridge casing (not shown).
The thin outer shell 12 of the slug is filled with loose material 18 which may be any of a number of weighting materials such as powdered lead, lead shot or lead fragments. The loose material 18 is retained within the thin Patented July 11, 1961 ice outer shell 12 by means of paper wadding 20 which is inserted into the open end 22 of the shell 12.
In operation, the preferred embodiment of the present invention will comprise a thin outer shell 12, 7 of an inch thick, and constructed in the form of a casted alloy shell consisting of bismuth, 25% lead, 12 /2% tin and 12 /2 cadmium, by weight, which will have a melting point of approximately 149 F. When the slug 10 is fired the heat of the exploding charge and barrel friction will cause the thin outer shell 12 to be heated to a temperature near its melting point thus reducing the outer shell 12 to a putty-like consistency. As the slug 10 leaves the gun barrel it will be subjected to approximately 600 p.s.i. of pressure and air friction wich will complete the destruction of the thin outer shell 12, thus permitting the powdered lead or other weight-producing material 18 along with the paper wadding 20 to be scattered over a relatively small area near the barrel of the weapon.
The weight-producing material (18 is necessary to the proper functioning of the test ammunition since the weight of the test ammunition must be the same as an actual round to produce identical recoil and shock characteristics on the weapon being fired.
The present invention has been described in detail above tor the purpose of illustration only and is not intended to be limited by this description or otherwise except as defined in the appended claims.
I claim:
1. A disintegrating projectile of the type described comprising a thin outer metal shell, said metal shell being a cast alloy of 50% bismuth, 25% lead, l2 /2% tin and 12 /2 cadmium, by weight, approximately of an inch thick, powdered lead disposed within said thin metal shell to approximate the weight of a standard projectile, and means sealing said powdered lead within said thin outer metal shell.
2. A distintegrating projectile according to claim 1 wherein said sealing means consists of paper wadding.
3. A disintegrating projectile of the type described com prising a bullet-shaped thin outer metal shell approximately of an inch thick, said metal shell being a cast alloy of 50% bismuth, 25% lead, 12 /z% tin and 12V2% cadmium by weight, and means contained within said thin metal shell to approximate the weight of standard round.
References Cited in the file of this patent UNITED STATES PATENTS 2,782,717 Burri Feb. 26, 1957 2,850,978 Franklin Sept. 9, 1958 FOREIGN PATENTS 5,204 Great Britain AD. 1912 215,008 Great Britain Ian. 8, 1925 OTHER REFERENCES Marks Handbook, third edition, second impression, McGraw-Hill Book Company, Inc., 1930, page 673, Lionel S. Marks, editor in chief. (Copy in Div. 10.)
Claims (1)
1. A DISINTEGRATING PROJECTILE OF THE TYPE DESCRIBED COMPRISING A THIN OUTER METAL SHELL, SAID METAL SHELL BEING A CAST ALLOY OF 50% BISMUTH, 25% LEAD, 12 1/2% TIN AND 12 1/2% CADMIUM, BY WEIGHT, APPROXIMATELY 3/64 OF AN INCH THICK, POWDERED LEAD WITHIN SAID THIN OUTER TO APPROXIMATE THE WEIGHT OF A STANDARD PROJECTILE, AND MEANS SEALING SAID POWDERED LEAD WITHIN SAID THIN OUTER METAL SHELL.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US820562A US2991718A (en) | 1959-06-15 | 1959-06-15 | Disintegrating ammunition for machine gun and cannon |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US820562A US2991718A (en) | 1959-06-15 | 1959-06-15 | Disintegrating ammunition for machine gun and cannon |
Publications (1)
Publication Number | Publication Date |
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US2991718A true US2991718A (en) | 1961-07-11 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US820562A Expired - Lifetime US2991718A (en) | 1959-06-15 | 1959-06-15 | Disintegrating ammunition for machine gun and cannon |
Country Status (1)
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US (1) | US2991718A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3170405A (en) * | 1962-03-17 | 1965-02-23 | Karlsruhe Augsburg Iweka | Disintegrating training ammunition for firearms |
US3216358A (en) * | 1962-07-26 | 1965-11-09 | Mannesmann Ag | Method of making readily disintegrating projectile cores for practice ammunition |
DE1226458B (en) * | 1961-08-12 | 1966-10-06 | Dynamit Nobel Ag | Decay bullet for maneuver cartridges |
US3289585A (en) * | 1964-04-23 | 1966-12-06 | Dynamit Nobel Ag | Shell construction |
EP0007695A1 (en) * | 1978-06-09 | 1980-02-06 | FORD AEROSPACE & COMMUNICATIONS CORPORATION | Frangible projectile body |
US4522126A (en) * | 1984-01-11 | 1985-06-11 | Morton Thiokol Inc. | Gun launched IR cloaking device for vehicles |
US10883786B2 (en) * | 2015-10-18 | 2021-01-05 | William D. Reilly | Sub-mass projectile for a firearm |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB191205204A (en) * | 1911-03-10 | 1912-09-19 | Uldarique Marga | Improvements in Blank Fire Cartridges. |
GB215008A (en) * | 1924-04-25 | 1925-01-08 | Angelo Magistri | Bullet for cartridges for firing practice with fire arms |
US2782717A (en) * | 1952-07-03 | 1957-02-26 | Mach Tool Works Oerlikon Admin | Fuze |
US2850978A (en) * | 1955-03-02 | 1958-09-09 | Philip J Franklin | Safety device for ordnance fuzes |
-
1959
- 1959-06-15 US US820562A patent/US2991718A/en not_active Expired - Lifetime
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB191205204A (en) * | 1911-03-10 | 1912-09-19 | Uldarique Marga | Improvements in Blank Fire Cartridges. |
GB215008A (en) * | 1924-04-25 | 1925-01-08 | Angelo Magistri | Bullet for cartridges for firing practice with fire arms |
US2782717A (en) * | 1952-07-03 | 1957-02-26 | Mach Tool Works Oerlikon Admin | Fuze |
US2850978A (en) * | 1955-03-02 | 1958-09-09 | Philip J Franklin | Safety device for ordnance fuzes |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1226458B (en) * | 1961-08-12 | 1966-10-06 | Dynamit Nobel Ag | Decay bullet for maneuver cartridges |
US3170405A (en) * | 1962-03-17 | 1965-02-23 | Karlsruhe Augsburg Iweka | Disintegrating training ammunition for firearms |
DE1189890B (en) * | 1962-03-17 | 1965-03-25 | Karlsruhe Augsburg Iweka | Maneuver cartridge disintegrating projectile |
US3216358A (en) * | 1962-07-26 | 1965-11-09 | Mannesmann Ag | Method of making readily disintegrating projectile cores for practice ammunition |
US3289585A (en) * | 1964-04-23 | 1966-12-06 | Dynamit Nobel Ag | Shell construction |
EP0007695A1 (en) * | 1978-06-09 | 1980-02-06 | FORD AEROSPACE & COMMUNICATIONS CORPORATION | Frangible projectile body |
US4522126A (en) * | 1984-01-11 | 1985-06-11 | Morton Thiokol Inc. | Gun launched IR cloaking device for vehicles |
US10883786B2 (en) * | 2015-10-18 | 2021-01-05 | William D. Reilly | Sub-mass projectile for a firearm |
US20240060741A1 (en) * | 2015-10-18 | 2024-02-22 | William D. Reilly | Sub-mass projectile for a firearm |
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