US1310058A - Ordnance - Google Patents
Ordnance Download PDFInfo
- Publication number
- US1310058A US1310058A US1310058DA US1310058A US 1310058 A US1310058 A US 1310058A US 1310058D A US1310058D A US 1310058DA US 1310058 A US1310058 A US 1310058A
- Authority
- US
- United States
- Prior art keywords
- bore
- projectile
- chambers
- breech
- ordnance
- 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 7
- 239000000843 powder Substances 0.000 description 4
- 230000002459 sustained effect Effects 0.000 description 4
- 238000010276 construction Methods 0.000 description 2
- 235000003197 Byrsonima crassifolia Nutrition 0.000 description 1
- 240000001546 Byrsonima crassifolia Species 0.000 description 1
- 230000003455 independent Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F1/00—Launching apparatus for projecting projectiles or missiles from barrels, e.g. cannons; Harpoon guns
-
- 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
- F41A1/00—Missile propulsion characterised by the use of explosive or combustible propellant charges
- F41A1/04—Missile propulsion using the combustion of a liquid, loose powder or gaseous fuel, e.g. hypergolic fuel
Definitions
- My invention relates to ordnance, and the object of my invention is to increase the effective range of artillery, particularly heavy guns.
- My inventlon comprises means whereby an increased amount of sustained pressure from a charge of powder or other explosive may be provided, with substanially no 11mitation in the magnitude of the explosive charge, and
- Figures 1 and 2 are, respectively, a lontudinal section and a cross section of sufcient of a gun barrel and its breech to illustrate my invention
- Figs. 3 and 4 are similar views illustrati ing a modified construction Within the scope 1 of my invention.
- Ord nance as usually constructed comprises a barrel having a bore of substantially uniform internal diameter throughout, the breech portion of which bore receives acharge of powder or other explosiv'e set behind a projectile which is driven I from the gun by the pressure exerted by the exploding charge.
- a gun oi this type presents the smallest possible space i for the charge of explosive and the shortcast time of sustained pressure, which can only occupy the bore between the breech block and the movin projectile.
- the muzzle velocity of a pro ectile discharged from a gun of this type is such that up to the present time their range has been approximatelv not more than twenty-six miles.
- the breech l of the gun is provided wlth a plu- ORDNANCE.
- Figs. 1 and 2 I have shown'a gun having four chambers for the reception of powder or other explosive charges surrounding the central bore or barrel containing the projectile; "such chambers communicating at suitable points with the central bore to insure the passage of the pressure to the same behind the projectile.
- Figs. 3 and 4 a similar construction is illustrated, but in this arrangement the wall 1* of the breech containing the chambers 2 for the extra powder charges is in the form of a cylinder, instead of the inde pendent semi-cylindrical portions each containing a chamber, as in the structure shown in Figs. 1 and 2.
- Ordnance comprising a barrel having a bore for receiving a projectile and an enlarged breech, a plurality of explosivecharge-receiving chambers formed within said enlarged breech, and gas passages connecting said chambers with the bore of said barrel behind the projectile whereby the force developed in said chambers is directed against the rear of the projectile to drive it from the barrel of the gun.
- Ordnance comprising abarrel having a bore for receiving a projectile and an enlarged breech in which the rear end of said bore is centrally disposed, a plurality of explosive-charge-receiving chambers formed within said enlarged breech, and gas passages disposed at equidistant points and connecting said chambers with the bore of the barrel behind the projectile.
- Ordnance comprising a barrel having a bore for receiving a projectile and an enlarged breech in which the rear end of said bore is centrally disposed, a plurality of explosive-charge-receiving chambers aralleling said bore and formed within said an larged breech,and gas passages disposed at equidistant points and connecting said chambers with the-boreof the barrel be hind the projectile.
- gaunt may be obtained. to; flmcents each, by addressing fl e. ggpig igg lqper qg Xmtsytg chambers is directed against the rearfof the" 1 prcjectile to drive it from thebarrel cf the
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Pyridine Compounds (AREA)
Description
c.H.cAsPAR."
ORDNANCE.
APPLICATION FILED MAR. 28. I918,
Patented July 15, 1919.
w Aw 0.058. I Tasmania-ad 'cba'cem.-' v
. -Be it known that I, CHARLES H. OAsPAn,
1 Philadelphia,
' UNITED STATES PATENT QFFIGE CHARLES H. CASPAR, 0F PHILADELPHIA, rE-NNsY-LvANrA.
a citizen of the United States, residing in Pennsylvania, have invented certain Improvements in Ordnance, of wh1ch the following is a specification.
My invention relates to ordnance, and the object of my invention is to increase the effective range of artillery, particularly heavy guns. My inventlon comprises means whereby an increased amount of sustained pressure from a charge of powder or other explosive may be provided, with substanially no 11mitation in the magnitude of the explosive charge, and
These and other features of my invention are more fully described hereinafter, reference being had to the accompanying drawings, in which:
Figures 1 and 2, are, respectively, a lontudinal section and a cross section of sufcient of a gun barrel and its breech to illustrate my invention, and
Figs. 3 and 4, are similar views illustrati ing a modified construction Within the scope 1 of my invention.
' Ord nance as usually constructed comprises a barrel having a bore of substantially uniform internal diameter throughout, the breech portion of which bore receives acharge of powder or other explosiv'e set behind a projectile which is driven I from the gun by the pressure exerted by the exploding charge. Under ordinary circumstances a gun oi this type presents the smallest possible space i for the charge of explosive and the shortcast time of sustained pressure, which can only occupy the bore between the breech block and the movin projectile. The muzzle velocity of a pro ectile discharged from a gun of this type is such that up to the present time their range has been approximatelv not more than twenty-six miles.
Ordnance experts agree that if the tlme of sustained pressure within the bore of the i gun or the magnitude of the explosive charge could be increased, greater flight of the projectile would be secured. Increase "of the time of sustained pressure within the bore of the gun and provision for increase in the magnitude of the explosive charge is the object of my invention, and
\ in order to provide for such conditions, the breech l of the gun is provided wlth a plu- ORDNANCE.
Specification of Letters mat.
atna Jul .15, 1919.
' Application filed March 28, 1918." Serial no. 225,306.
j'rality "of chambers for the reception of zle velocity of the projectile as to insure a range of substantially any distance desired.
In Figs. 1 and 2, I have shown'a gun having four chambers for the reception of powder or other explosive charges surrounding the central bore or barrel containing the projectile; "such chambers communicating at suitable points with the central bore to insure the passage of the pressure to the same behind the projectile.
In Figs. 3 and 4, a similar construction is illustrated, but in this arrangement the wall 1* of the breech containing the chambers 2 for the extra powder charges is in the form of a cylinder, instead of the inde pendent semi-cylindrical portions each containing a chamber, as in the structure shown in Figs. 1 and 2.
I claim:
1. Ordnance comprising a barrel having a bore for receiving a projectile and an enlarged breech, a plurality of explosivecharge-receiving chambers formed within said enlarged breech, and gas passages connecting said chambers with the bore of said barrel behind the projectile whereby the force developed in said chambers is directed against the rear of the projectile to drive it from the barrel of the gun.
2. Ordnance comprising abarrel having a bore for receiving a projectile and an enlarged breech in which the rear end of said bore is centrally disposed, a plurality of explosive-charge-receiving chambers formed within said enlarged breech, and gas passages disposed at equidistant points and connecting said chambers with the bore of the barrel behind the projectile.
3. Ordnance comprising a barrel having a bore for receiving a projectile and an enlarged breech in which the rear end of said bore is centrally disposed, a plurality of explosive-charge-receiving chambers aralleling said bore and formed within said an larged breech,and gas passages disposed at equidistant points and connecting said chambers with the-boreof the barrel be hind the projectile.
larged breech, a plurality of explosive charge-receiving chambers. formed wit hi ll I 7,;
said enlarged breech, and gaspassa'ges connectlng the rear ends ofsald chambers with the-b'ore -of said bamr'el behind the projectile whereby the force developed in, saldf ,QH LES HQCASLPAR.
Gopiu; 01 this] gauntmay be obtained. to; flmcents each, by addressing fl e. ggpig igg lqper qg Xmtsytg chambers is directed against the rearfof the" 1 prcjectile to drive it from thebarrel cf the
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1310058A true US1310058A (en) | 1919-07-15 |
Family
ID=3377566
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US1310058D Expired - Lifetime US1310058A (en) | Ordnance |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1310058A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1116111B (en) * | 1958-03-29 | 1961-10-26 | Busch Jaeger Duerener Metall | Missile launcher |
-
0
- US US1310058D patent/US1310058A/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1116111B (en) * | 1958-03-29 | 1961-10-26 | Busch Jaeger Duerener Metall | Missile launcher |
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