US1280579A - Non-recoil ordnance. - Google Patents
Non-recoil ordnance. Download PDFInfo
- Publication number
- US1280579A US1280579A US18317517A US18317517A US1280579A US 1280579 A US1280579 A US 1280579A US 18317517 A US18317517 A US 18317517A US 18317517 A US18317517 A US 18317517A US 1280579 A US1280579 A US 1280579A
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- US
- United States
- Prior art keywords
- gun
- projectile
- cup
- recoil
- 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
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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
- F41A1/00—Missile propulsion characterised by the use of explosive or combustible propellant charges
- F41A1/08—Recoilless guns, i.e. guns having propulsion means producing no recoil
-
- 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
- F41A1/08—Recoilless guns, i.e. guns having propulsion means producing no recoil
- F41A1/10—Recoilless guns, i.e. guns having propulsion means producing no recoil a counter projectile being used to balance recoil
Definitions
- recoil can UNITED STATES PATENT OFFICE.
- This invention relates to improvements in non-recoil ordnance, and has reference to guns of that character wherein recoil is minimized or wholly eliminated by the discharge from the gun of an inertia mass in a direction opposite to that in which the main proj ectile is projected.
- Our invention relates especially to ordnance of the non-recoiltype shown, for instance, in the U. S. Patent Number 1,108,716, granted August 25, 191 1, and entitled Apparatus for firing projectiles from air craft.
- the object of the present invention is to provide means whereby this inertia mass can be very much reduced; and the invention consists in providing means whereby friction is utilized to take the place of weight or inertia. That is to say, the inertia effects due'to the weight of the effective projectile are balanced by a small and light inertia mass plus the friction of this mass in the gun barrel. By this means the effects be avoided, although the gun barrel will be necessarily subjected to more or less longitudinal stress, depending upon the pressure of the powder gases in the bore.
- the taper of the passage may be varied to I give a greater or less squeezing action on the Specification of Letters Patent.
- Figure 1 shows the un mounted upon part of the framework 0 an aeroplane.
- Fig. 2 shows a section through the loading chamber of the gun and through the cartridge case and counterpoise cup, the projectile being shown in elevation, the muzzle of the gun being cut away, and the rear end of the gun being broken away; the parts in Fig. 2 being on a larger scale than in Fig. 1.
- the gun body consists of the forward portion or barrel A, which is trunnioned in the yoke 0 carried by the mount D, which mount may be of any suitable or desired construction, and B represents the rear portion of the gun which is detachably connected to the muzzle portion,
- the muzzle portion of the gun is rifled, as at a, to engage the rifling band 6 of the main or effective projectile E, and the rear portion of the gun is tapered, as at b, to compress the cup of copper, or other soft material, F, which forms the closure of the rear end of the cartridge case F.
- the breech portion of the gun B may be also rifled, but in the reverse, direction to the rifling a, so as to compensate in a measure for the twist imparted to the gun barrel as the main projectile leaves the gun, but since the cup F will ordinarily be of comparatively small weight relative to that of the main projectile E, this rifling of the breech portion of the gun may ordinarily be omitted, except in guns of heavy caliber.
- G represents the propelling charge which is carried in the cartridge case F between the cup F and the projectile E.
- This propelling char e may be fired in any convenient way, as y-means of the electric primer H controlled by the switch I in the electric circuit K.
- the breech of the gun may be opened and -the gun may be loaded in the same way as is fully described in the Patent No. 1,108,716,
- this cup-shaped inertia mass also serves as a gas check, to prevent the premature escape rearward of the powder ases; and the eflect of the powder gases wil be to expand the thinwalls of this cup, causing themto bind against the gun, thus still further increasing the frictional resistance against the expulsion rear ward of said inertia mass.
- the cylindrical cartridge case F extracted in the usual way.
- a gun of the type described comprising a front barrel in which the projectile proper is mounted, and a rear barrel having a con- I tinuously tapered bore adapted to compress an inertia mass and to thereby increase the frictional resistance of said mass in passing rearward from the gun, the said gun being provided with a powder chamber located between the projectile seat and the said inertia mass when the gun is loaded, substantially as described.
- a gun of the type described provided with open front and rear barrels in which the projectile is zle of the gun, and an inertia mass in the opposite direction through the open breech thereof, having its rear barrel continuously tapered so that the inertia mass is forced to pass through an orifice less in diameter than its own normal diameter, substantially ANDREW J. STONE. WILLIAM SHUKER.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
Description
A. J. STONE & w. S HUKER.
NON-RECOIL ORDNANCE.
APPLICATION FILED JULY 27.1911.
of recoil can UNITED STATES PATENT OFFICE.
ANDREW J. STONE, OF NEW LONDON, AND WILLIAM SHUKER, OF DERBY, CONNECTICUT;
SAID SHUKER ASSIGNOR T0 SAID STONE.
NON-RECOIL ORDNANCE.
To all whom it may concern:
Be it known that we, ANDREW J. STONE and WILLIAM SHU'KER, citizens of the United States, residing at New London and Derby, respectively, in the counties of New London and New-Haven, respectively, and State of Connecticut, have invented certain new and useful Improvements in Non-Recoil Ord nance; and we do hereby declare the follow ing to be 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 improvements in non-recoil ordnance, and has reference to guns of that character wherein recoil is minimized or wholly eliminated by the discharge from the gun of an inertia mass in a direction opposite to that in which the main proj ectile is projected.
Our invention relates especially to ordnance of the non-recoiltype shown, for instance, in the U. S. Patent Number 1,108,716, granted August 25, 191 1, and entitled Apparatus for firing projectiles from air craft.
Hitherto it has been considered necessary to provide an inertia mass nearlyapproximate in weight to the effective projectile; and the object of the present invention is to provide means whereby this inertia mass can be very much reduced; and the invention consists in providing means whereby friction is utilized to take the place of weight or inertia. That is to say, the inertia effects due'to the weight of the effective projectile are balanced by a small and light inertia mass plus the friction of this mass in the gun barrel. By this means the effects be avoided, although the gun barrel will be necessarily subjected to more or less longitudinal stress, depending upon the pressure of the powder gases in the bore. p
In accordance with the inventionv we propose to provide a cartridge having the usual effective projectile at its forward end, while at the rear end we provide a copper or like disk or cup adapted to fit a tapered passage opening through the breech of the gun.
The taper of the passage may be varied to I give a greater or less squeezing action on the Specification of Letters Patent.
Application filed July 21, 1917. Serial no. 183,175.-
cup, thus increasing or decreasing the force required to propel this cup rearward through the breech of the gun.
In operation the firing of the explosive charge will occur between the efiective projectile and the copper disk or cup with the result that the projectile will be shot out of the gun in one direction while the copper disk or cup will be forced through the tapering passage and out of the gun barrel in the other direction. It will readily be seen that by arranging the copper disk or cup of the proper diameter, weight and thickness, and arranging the tapering passage or passages in accordance, a frictional resistance can be provided for which will have precisely the same effect as a greater weight with less frictional resistance. It will be appreciated that the actuaLmethod of carrying the invention into practice may vary so long as the general principle involved is adhered to. This principle can be stated quite simply as follows: The inertia effects due to the heavy weight of the effective projectile plus the light frictional resistance of the projectile in the gun barrel should equal the inertia effects of the lighter weight of the disk or cup plus the heavier frictional resistance of the disk in the barrel so that if the disk is made lighter the frictional resistance must be increased accordingly to effect the desired balance.
Reference is had to the accompanying drawings, in which:
Figure 1 shows the un mounted upon part of the framework 0 an aeroplane.
Fig. 2 shows a section through the loading chamber of the gun and through the cartridge case and counterpoise cup, the projectile being shown in elevation, the muzzle of the gun being cut away, and the rear end of the gun being broken away; the parts in Fig. 2 being on a larger scale than in Fig. 1.
The gun body consists of the forward portion or barrel A, which is trunnioned in the yoke 0 carried by the mount D, which mount may be of any suitable or desired construction, and B represents the rear portion of the gun which is detachably connected to the muzzle portion,
as fully described in the patent to Cleland Davis aforesaid.
The muzzle portion of the gun is rifled, as at a, to engage the rifling band 6 of the main or effective projectile E, and the rear portion of the gun is tapered, as at b, to compress the cup of copper, or other soft material, F, which forms the closure of the rear end of the cartridge case F.
The breech portion of the gun B may be also rifled, but in the reverse, direction to the rifling a, so as to compensate in a measure for the twist imparted to the gun barrel as the main projectile leaves the gun, but since the cup F will ordinarily be of comparatively small weight relative to that of the main projectile E, this rifling of the breech portion of the gun may ordinarily be omitted, except in guns of heavy caliber.
G represents the propelling charge which is carried in the cartridge case F between the cup F and the projectile E. This propelling char e may be fired in any convenient way, as y-means of the electric primer H controlled by the switch I in the electric circuit K. We have indicated an electric battery L for supplying the source of electricity, but the electricity may be had from anysuitable source.
I The breech of the gun may be opened and -the gun may be loaded in the same way as is fully described in the Patent No. 1,108,716,
aforesaid, and we make 'no special claim in this present application to the breech mechanism or to the firing mechanism, or to the gun mount, the present invention relating entirely to the construction and functioning of the inertia mass.
It will be obvious that fired, the projectile E will fly forward through the muzzle in the usual way, while the cup-shaped inertia mass F will be forced backward and subjected to compressive when the gun is strains as it passes rearward through the breech, with the result that there is very great friction; and it will require great force to force this cup backward, even though it be of light weight compared to that of the projectile.
It will be noted that this cup-shaped inertia mass also serves as a gas check, to prevent the premature escape rearward of the powder ases; and the eflect of the powder gases wil be to expand the thinwalls of this cup, causing themto bind against the gun, thus still further increasing the frictional resistance against the expulsion rear ward of said inertia mass.
After the inertia mass leaves the gun its shape will be such that it will not fall with any great speed through the air, and therefore will not'be seriously dangerous to persons below or in rear who exercise a reasonable amount of caution.
The cylindrical cartridge case F extracted in the usual way.
It will be obvious that with guns of larger caliber,-where the propelling charge is supplied in sections, that the cartridge case may be omitted, and the counterpoise mass cup may be filled with explosive and with its may be contents constitute one of the sections of the propelling charge. V
Having thus described our invention, what we claim and desire to secure .by Letters Patent of the United States is:
1. A gun of the type described comprising a front barrel in which the projectile proper is mounted, and a rear barrel having a con- I tinuously tapered bore adapted to compress an inertia mass and to thereby increase the frictional resistance of said mass in passing rearward from the gun, the said gun being provided with a powder chamber located between the projectile seat and the said inertia mass when the gun is loaded, substantially as described.
2. A gun of the type described, provided with open front and rear barrels in which the projectile is zle of the gun, and an inertia mass in the opposite direction through the open breech thereof, having its rear barrel continuously tapered so that the inertia mass is forced to pass through an orifice less in diameter than its own normal diameter, substantially ANDREW J. STONE. WILLIAM SHUKER.
propelled through the muz-
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US18317517A US1280579A (en) | 1917-07-27 | 1917-07-27 | Non-recoil ordnance. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US18317517A US1280579A (en) | 1917-07-27 | 1917-07-27 | Non-recoil ordnance. |
Publications (1)
Publication Number | Publication Date |
---|---|
US1280579A true US1280579A (en) | 1918-10-01 |
Family
ID=3348172
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US18317517A Expired - Lifetime US1280579A (en) | 1917-07-27 | 1917-07-27 | Non-recoil ordnance. |
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US (1) | US1280579A (en) |
Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2557151A (en) * | 1944-08-24 | 1951-06-19 | Leslie A Skinner | Spring actuated generator for rocket launchers |
US2598256A (en) * | 1945-04-21 | 1952-05-27 | Us Sec War | Recoilless gun |
US2703508A (en) * | 1943-04-02 | 1955-03-08 | Charles C Lauritsen | Rocket projector |
US2919627A (en) * | 1953-05-05 | 1960-01-05 | Mcculloch Motors Corp | Projectile ignition device |
US2919629A (en) * | 1950-08-04 | 1960-01-05 | Abramson Hugo | Powder cases for use in breechless anti-recoil arms |
US2925014A (en) * | 1950-08-04 | 1960-02-16 | Abramson Hugo | Anti-recoil arms |
DE1079993B (en) * | 1957-05-06 | 1960-04-14 | Ludwig Bucklisch | Propellant charge with damper for recoil-free guns |
US2983195A (en) * | 1957-06-07 | 1961-05-09 | Bofors Ab | Non-recoiling gun |
DE1107129B (en) * | 1955-11-29 | 1961-05-18 | Latham Valentine Stewart Black | Shooting device with a front and rear barrel and an intermediate chamber |
US2987965A (en) * | 1958-03-17 | 1961-06-13 | Musser C Walton | Self-locking cartridge case for fixed ammunition |
US3128670A (en) * | 1961-10-09 | 1964-04-14 | Blacker Latham Valenti Stewart | Flashless non-recoil gun and round |
US4050351A (en) * | 1976-05-04 | 1977-09-27 | Societe Anonyme Dite: Societe Europeenne Depropulsion | Assembly for launching a projectile |
US4073213A (en) * | 1975-07-02 | 1978-02-14 | Societe Anonyme Dite : Societe Europeenne De Propulsion | Assembly for launching a projectile |
US7624668B1 (en) * | 2005-06-10 | 2009-12-01 | Sanford Matthew J | Recoilless launching |
US11473861B2 (en) * | 2018-05-08 | 2022-10-18 | Zsolt HEGYESHALMI | Recoilless, slideless repeating magazine-fed weapon |
US11959711B1 (en) * | 2021-10-15 | 2024-04-16 | The United States Of America As Represented By The Secretary Of The Army | Recoilless gun and ammunition |
-
1917
- 1917-07-27 US US18317517A patent/US1280579A/en not_active Expired - Lifetime
Cited By (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2703508A (en) * | 1943-04-02 | 1955-03-08 | Charles C Lauritsen | Rocket projector |
US2557151A (en) * | 1944-08-24 | 1951-06-19 | Leslie A Skinner | Spring actuated generator for rocket launchers |
US2598256A (en) * | 1945-04-21 | 1952-05-27 | Us Sec War | Recoilless gun |
US2919629A (en) * | 1950-08-04 | 1960-01-05 | Abramson Hugo | Powder cases for use in breechless anti-recoil arms |
US2925014A (en) * | 1950-08-04 | 1960-02-16 | Abramson Hugo | Anti-recoil arms |
US2919627A (en) * | 1953-05-05 | 1960-01-05 | Mcculloch Motors Corp | Projectile ignition device |
DE1107129B (en) * | 1955-11-29 | 1961-05-18 | Latham Valentine Stewart Black | Shooting device with a front and rear barrel and an intermediate chamber |
DE1079993B (en) * | 1957-05-06 | 1960-04-14 | Ludwig Bucklisch | Propellant charge with damper for recoil-free guns |
US2983195A (en) * | 1957-06-07 | 1961-05-09 | Bofors Ab | Non-recoiling gun |
US2987965A (en) * | 1958-03-17 | 1961-06-13 | Musser C Walton | Self-locking cartridge case for fixed ammunition |
US3128670A (en) * | 1961-10-09 | 1964-04-14 | Blacker Latham Valenti Stewart | Flashless non-recoil gun and round |
US4073213A (en) * | 1975-07-02 | 1978-02-14 | Societe Anonyme Dite : Societe Europeenne De Propulsion | Assembly for launching a projectile |
US4050351A (en) * | 1976-05-04 | 1977-09-27 | Societe Anonyme Dite: Societe Europeenne Depropulsion | Assembly for launching a projectile |
US7624668B1 (en) * | 2005-06-10 | 2009-12-01 | Sanford Matthew J | Recoilless launching |
US7841267B1 (en) * | 2005-06-10 | 2010-11-30 | The United States Of America As Represented By The Navy | Recoilless launching |
US11473861B2 (en) * | 2018-05-08 | 2022-10-18 | Zsolt HEGYESHALMI | Recoilless, slideless repeating magazine-fed weapon |
US11959711B1 (en) * | 2021-10-15 | 2024-04-16 | The United States Of America As Represented By The Secretary Of The Army | Recoilless gun and ammunition |
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