US511418A - Projectile - Google Patents
Projectile Download PDFInfo
- Publication number
- US511418A US511418A US511418DA US511418A US 511418 A US511418 A US 511418A US 511418D A US511418D A US 511418DA US 511418 A US511418 A US 511418A
- Authority
- US
- United States
- Prior art keywords
- projectile
- section
- charge
- gun
- hollow
- 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
- 239000002360 explosive Substances 0.000 description 28
- 210000000614 Ribs Anatomy 0.000 description 12
- 238000010276 construction Methods 0.000 description 8
- 230000001808 coupling Effects 0.000 description 6
- 238000010168 coupling process Methods 0.000 description 6
- 238000005859 coupling reaction Methods 0.000 description 6
- 239000000020 Nitrocellulose Substances 0.000 description 4
- FJWGYAHXMCUOOM-QHOUIDNNSA-N [(2S,3R,4S,5R,6R)-2-[(2R,3R,4S,5R,6S)-4,5-dinitrooxy-2-(nitrooxymethyl)-6-[(2R,3R,4S,5R,6S)-4,5,6-trinitrooxy-2-(nitrooxymethyl)oxan-3-yl]oxyoxan-3-yl]oxy-3,5-dinitrooxy-6-(nitrooxymethyl)oxan-4-yl] nitrate Chemical compound O([C@@H]1O[C@@H]([C@H]([C@H](O[N+]([O-])=O)[C@H]1O[N+]([O-])=O)O[C@H]1[C@@H]([C@@H](O[N+]([O-])=O)[C@H](O[N+]([O-])=O)[C@@H](CO[N+]([O-])=O)O1)O[N+]([O-])=O)CO[N+](=O)[O-])[C@@H]1[C@@H](CO[N+]([O-])=O)O[C@@H](O[N+]([O-])=O)[C@H](O[N+]([O-])=O)[C@H]1O[N+]([O-])=O FJWGYAHXMCUOOM-QHOUIDNNSA-N 0.000 description 4
- 230000001066 destructive Effects 0.000 description 4
- 238000004880 explosion Methods 0.000 description 4
- 229920001220 nitrocellulos Polymers 0.000 description 4
- 239000000843 powder Substances 0.000 description 4
- 238000005192 partition Methods 0.000 description 2
Images
Classifications
-
- 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
- F42B10/26—Stabilising arrangements using spin
- F42B10/28—Stabilising arrangements using spin induced by gas action
Definitions
- This invention relates to a novel construction in a projectile, and relates more particularly to a projectile adapted to be charged with a high explosive, oil, doc., the object being to provide such a projectile that can be fired with great accuracy.
- FIG. 1 is a central, longitudinal sectional view of said projectile.
- Fig. 3 is a cross section on the line 3--3 of Fig. 2.
- Fig. 4 is a central, longitudinal section cf a modified form of construction embodying my invention.
- A indicates as a whole the projectile, consisting of two hollow sections 1 and 2, the front section 1 to contain the explosive charge, and the rear section 2 to contain a charge of rocket powder or the like to give an additional impetus to the projectile after being fired from the gun.
- the two sections l and 2 are separable and are joined by a coupling piece 3 having au opening or perforation 4 therethrough so that the explosive charge in the front section 1 can be ignited from said rear section 2.
- the front section can be illed with some explosive, such, for instance as wet gun cotton, so that the high explosive charge can be kept separate from the rest of the projectile and thus reduce the danger from accidental explosion or from fire, which is especially desirable in carrying such charges in vessels.
- the rear section 2 with its charges can be kept separate, and when it is desired to use a projectile, the front end of the coupling 3 can be screwed into the en d of section 1, and before doing so, the cup 5 in the end of such coupling can be illed with dry gun cotton, so that it will be readily exploded and thus explode the large charge in the front section 1.
- rocket powder is, as far as I am informed, preferable, and is packed under pressure therein in av familiar manner, and is conveniently ignited by the burning of the charge from the gun from which the project ile is fired bya fuse, or through an opening 7 in a plug 8 located within the rear end of the said section 2, whereupon said charge in said rear section will force the plug from the end of the section.
- a projectile of this kind can be fired from a smooth bore or a ritled gun, but Ihave arranged the plug 8 a little distance in from the end of the section, so that the explosive charge of the gun will force the shell of the section 2 into the rie grooves of a gun, when the projectile is fired from such a gun, to thereby give the initial rotation to the projection.
- the end portion thereot ⁇ may be provided with spiral wings 9 which will serve to cause the rotation of the same in an obvious manner.
- a projectile having a hollow rear end portion to receive a propelling charge, and a series of interior spirally arranged ribs or flanges located Within said hollow rear end 2.
- a projectile having a hollow rear end portion to receive a propelling charge, a series of interior spirally arranged ribs or flanges, and a perforated plug located within the rear end portion of said projectile and inward of its rear end.
- a projectile having a rear section 2 adapted to enter and tit within the bore of a gun or ordnance piece. and an enlarged front section l provided with a series of exterior 4.
- a projectile having a rearsection adapted to enter and tit within the bore of a gun or ordnance piece, and an enlarged hollow front section 1 provided with a series of exterior spirally arranged wings.
- a projectile having a hollow rear section 2, adapted to enter and t within the bore of a gun or ordnance piece and to contain apropelling charge and an enlarged hollow front section 1 to contain au explosive charge to be ignited by said propelling charge.
- a projectile having a hollow rear section 2 adapted to enter and tit within the bore of a. gun or ordnance piece and to contain a propelling charge, an enlarged hollow'front section 1 adapted to contain an explosive charge, and a perforated partition separating said front and rear sections.
- a projectile having a hollow rear section 2 adapted to enter and lit .within the bore of a gun or ordnance piece end to contain a propelling charge, an enlarged hollow front section 1 adapted to contain an explosive charge to he ignited by said propelling charge, and a series of spirally arranged wings upon said enlarged front section 1.
- a projectile having a hollow rear end portion to receive a propelling charge, a series of interior spirally arranged ribs or flanges located within said hollow rear end portion, and a series of exterior spirally arranged wings on the front end portion of said projectile.
- a projectile having a hollow rear section 2 adapted to enter and fit within the bore of a gun or ordnance piece and to contain a propelling charge, a series of interior spirally arranged ribs or dangeslocated within said hollow rear end portion, an enlarged hollow front. section 1 adapted to contain an explosive charge to be ignited by said propelling charge, and a series of spirall'y arranged wings upon said enlarged front section Y In testimony whereof I ax my signature in presence of twov witnesses.
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- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Portable Nailing Machines And Staplers (AREA)
Description
V(No Model.)
L. GATHMANN.
PROJEGTILE.
Patented Deo. 26, 1893.
UNITED STATES PATENTN OFFICE.
A LOUIS GA'II'IMANN, OF CHICAGO, ILLINOIS.
PROJECTILE.
SPECIFICATION forming part of Letters Patent No. 511,418, dated December 26, 1893.
Application tiled April 19, 1892. Serial No. 429,810. (No model.)
T 0 all whom, it may concern:
Beit known that I, LOUIS GATHMANN, a citizen of the United States, residing at Chicago, in the county of Cook and State of Illinois, have invented certain new and useful Improvements in Project-iles; and I do hereby declare the following to he a full, clear, and exact description of the invention, such as will enable others skilled in the art to which it appertains to make and use the same.
This invention relates to a novel construction in a projectile, and relates more particularly to a projectile adapted to be charged with a high explosive, oil, doc., the object being to provide such a projectile that can be fired with great accuracy.
The invention consists in the novel features of construction hereinafter fully described and specifically claimed.
In the accompanying drawings illustrating my invention,-Figure lis a side elevation of a projectile constructed in accordance with `my invention in place in a gun, which latter is shown partly in section and in side elevation. Fig. 2 is a central, longitudinal sectional view of said projectile. Fig. 3 is a cross section on the line 3--3 of Fig. 2. Fig. 4 is a central, longitudinal section cf a modified form of construction embodying my invention.
Referring to said drawings, A indicates as a whole the projectile, consisting of two hollow sections 1 and 2, the front section 1 to contain the explosive charge, and the rear section 2 to contain a charge of rocket powder or the like to give an additional impetus to the projectile after being fired from the gun. The two sections l and 2 are separable and are joined by a coupling piece 3 having au opening or perforation 4 therethrough so that the explosive charge in the front section 1 can be ignited from said rear section 2. By making such sections of the projectile separable, it will be noted that the front section can be illed with some explosive, such, for instance as wet gun cotton, so that the high explosive charge can be kept separate from the rest of the projectile and thus reduce the danger from accidental explosion or from fire, which is especially desirable in carrying such charges in vessels. The rear section 2 with its charges can be kept separate, and when it is desired to use a projectile, the front end of the coupling 3 can be screwed into the en d of section 1, and before doing so, the cup 5 in the end of such coupling can be illed with dry gun cotton, so that it will be readily exploded and thus explode the large charge in the front section 1.
In a projectile of this kind it is of course obvious that there is a liability that during its flight the projectile will turn over and thus spoil the aim, and to prevent such a l'esult, I have provided means for imparting a rotation to the same and for maintaining such rotation during its Hight. To this end a series of spirally arranged ribs or Bauges 6 are located within the rear end portion of the rear section 2, and it will be noted that the force ot the burning charge, within said rear section against such ribs or flanges, and also the twisting motion given to the charge as it emerges from the end of such section will serve to impart such rotation to the projectile and maintain thesame during its flight. Various charges could be used within the rear section, but rocket powder is, as far as I am informed, preferable, and is packed under pressure therein in av familiar manner, and is conveniently ignited by the burning of the charge from the gun from which the project ile is fired bya fuse, or through an opening 7 in a plug 8 located within the rear end of the said section 2, whereupon said charge in said rear section will force the plug from the end of the section. It is ,of course understood that a projectile of this kind can be fired from a smooth bore or a ritled gun, but Ihave arranged the plug 8 a little distance in from the end of the section, so that the explosive charge of the gun will force the shell of the section 2 into the rie grooves of a gun, when the projectile is fired from such a gun, to thereby give the initial rotation to the projection.
To further increase the rotation given to the projectile, the end portion thereot` may be provided with spiral wings 9 which will serve to cause the rotation of the same in an obvious manner.
As a further and separate improvement in projectiles, I make the front section 1 of greater diameter than the rear section 2, and am thus enabled to fire a large amount of explosive IOC ' which it strikes.
portion.
` spirally arranged wings.
takes place nearer the object, as
that will have a maximum destructive effect upon the object against which it is exploded. By this construction it will be further noted that the explosive charge carried in the enlarged end of a projectile of comparatively small caliber will be rendered much more destructive than if it was confined with the shell o f such caliber, because the explosion the explosive, being contained in a shell-of large diameter, is therefore nearer the object against And further, projectiles of a given caliber can carry a greater amount of explosive, and yet be propelled to 'the same extent by reason of the auxiliary propelling charge.
I do not, in this application, claim certain features shown herein, but which are claimed in another application tiled by myself in the United States Patent Olice April 19, 1892, Serial No. 429,809.
I claim as my invention- 1. A projectile having a hollow rear end portion to receive a propelling charge, and a series of interior spirally arranged ribs or flanges located Within said hollow rear end 2. A projectile having a hollow rear end portion to receive a propelling charge, a series of interior spirally arranged ribs or flanges, and a perforated plug located within the rear end portion of said projectile and inward of its rear end.
3. A projectile having a rear section 2 adapted to enter and tit within the bore of a gun or ordnance piece. and an enlarged front section l provided with a series of exterior 4. A projectile having a rearsection adapted to enter and tit within the bore of a gun or ordnance piece, and an enlarged hollow front section 1 provided with a series of exterior spirally arranged wings.
5. A projectile having a hollow rear section 2, adapted to enter and t within the bore of a gun or ordnance piece and to contain apropelling charge and an enlarged hollow front section 1 to contain au explosive charge to be ignited by said propelling charge.
6. A projectile having a hollow rear section 2 adapted to enter and tit within the bore of a. gun or ordnance piece and to contain a propelling charge, an enlarged hollow'front section 1 adapted to contain an explosive charge, and a perforated partition separating said front and rear sections.
7. A projectile havinga hollow rear section 2 adapted to enter and lit .within the bore of a gun or ordnance piece end to contain a propelling charge, an enlarged hollow front section 1 adapted to contain an explosive charge to he ignited by said propelling charge, and a series of spirally arranged wings upon said enlarged front section 1.
8. A projectile having a hollow rear end portion to receive a propelling charge, a series of interior spirally arranged ribs or flanges located within said hollow rear end portion, and a series of exterior spirally arranged wings on the front end portion of said projectile.
9. A projectile having a hollow rear section 2 adapted to enter and fit within the bore of a gun or ordnance piece and to contain a propelling charge, a series of interior spirally arranged ribs or dangeslocated within said hollow rear end portion, an enlarged hollow front. section 1 adapted to contain an explosive charge to be ignited by said propelling charge, and a series of spirall'y arranged wings upon said enlarged front section Y In testimony whereof I ax my signature in presence of twov witnesses.
LoUIs GATHMANN.
Witnesses:
' HARRY CoBB- KENNEDY,
RUDOLPH W. Louez.
Publications (1)
Publication Number | Publication Date |
---|---|
US511418A true US511418A (en) | 1893-12-26 |
Family
ID=2580241
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US511418D Expired - Lifetime US511418A (en) | Projectile |
Country Status (1)
Country | Link |
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US (1) | US511418A (en) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2421522A (en) * | 1944-08-23 | 1947-06-03 | Winslow B Pope | Rocket projector and projectile |
US2457839A (en) * | 1941-09-08 | 1949-01-04 | Leslie A Skinner | Rocket |
US2470120A (en) * | 1943-05-06 | 1949-05-17 | Walker Brooks | Method of bombing from fast moving planes |
US2821137A (en) * | 1952-04-12 | 1958-01-28 | Lyon George Albert | Military rocket structure |
US2944261A (en) * | 1954-07-08 | 1960-07-12 | Schulz | Method of driving studs into bodies by high pressure gases |
US3095694A (en) * | 1959-10-28 | 1963-07-02 | Walter Hermine Johanna | Reaction motors |
US3127691A (en) * | 1962-06-27 | 1964-04-07 | Cyril A Moore | Gas control means for grenade launching attachments |
DE977712C (en) * | 1957-03-03 | 1968-08-08 | Franz Rudolf Dipl-Ing Thomanek | A missile-powered missile equipped with a lined shaped charge |
US4010688A (en) * | 1972-11-17 | 1977-03-08 | Smith Matthew S | Weapon arrangement |
-
0
- US US511418D patent/US511418A/en not_active Expired - Lifetime
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2457839A (en) * | 1941-09-08 | 1949-01-04 | Leslie A Skinner | Rocket |
US2470120A (en) * | 1943-05-06 | 1949-05-17 | Walker Brooks | Method of bombing from fast moving planes |
US2421522A (en) * | 1944-08-23 | 1947-06-03 | Winslow B Pope | Rocket projector and projectile |
US2821137A (en) * | 1952-04-12 | 1958-01-28 | Lyon George Albert | Military rocket structure |
US2944261A (en) * | 1954-07-08 | 1960-07-12 | Schulz | Method of driving studs into bodies by high pressure gases |
DE977712C (en) * | 1957-03-03 | 1968-08-08 | Franz Rudolf Dipl-Ing Thomanek | A missile-powered missile equipped with a lined shaped charge |
US3095694A (en) * | 1959-10-28 | 1963-07-02 | Walter Hermine Johanna | Reaction motors |
US3127691A (en) * | 1962-06-27 | 1964-04-07 | Cyril A Moore | Gas control means for grenade launching attachments |
US4010688A (en) * | 1972-11-17 | 1977-03-08 | Smith Matthew S | Weapon arrangement |
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