US3459101A - High velocity weapon - Google Patents

High velocity weapon Download PDF

Info

Publication number
US3459101A
US3459101A US681691A US3459101DA US3459101A US 3459101 A US3459101 A US 3459101A US 681691 A US681691 A US 681691A US 3459101D A US3459101D A US 3459101DA US 3459101 A US3459101 A US 3459101A
Authority
US
United States
Prior art keywords
projectile
weapon
velocity
charge
high velocity
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
Application number
US681691A
Inventor
John J Scanlon Jr
Joseph B Quinlan
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
United States Department of the Army
Original Assignee
United States Department of the Army
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by United States Department of the Army filed Critical United States Department of the Army
Application granted granted Critical
Publication of US3459101A publication Critical patent/US3459101A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A1/00Missile propulsion characterised by the use of explosive or combustible propellant charges
    • F41A1/02Hypervelocity missile propulsion using successive means for increasing the propulsive force, e.g. using successively initiated propellant charges arranged along the barrel length; Multistage missile propulsion
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A1/00Missile propulsion characterised by the use of explosive or combustible propellant charges
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00Rocket or torpedo launchers

Definitions

  • a weapon including a chamber mounted on a gun barrel and containing a caseless charge of propellant therein which partially extends into the path of an oncoming projectile to be ignited thereby.
  • the invention relates to a high velocity Weapon and more particularly to a high velocity weapon utilizing a secondary charge mounted on said weapon for increasing the velocity of a projectile fired from said Weapon.
  • a still further object is to provide a high velocity Weapon utilizing a secondary charge to increase the velocity of a projectile which is initiated by direct contact With said projectile.
  • a gun barrel 10 of a weapon having a plurality of screw threaded, removable chambers 12 and 14.
  • Contained in each of said chambers 12 and 14 is a charge of molded caseless propellant 16 and 18 having a primer composition 20 and 22 attached in a known manner to said molded propellant 16 and 18 at an end extending through orifice 24 and 26 having an annulus and 27 thereon, and into the passageway 28 of the gun barrel 10.
  • the top portions 13 and 15 of each chamber 12 and 14 are screw threaded and removable to allow for the insertion of the charge therein.
  • a standard caseless 7.62 mm. cartridge 30 having attached at its forward end a projectile 32 and inserted in its rearward portion a primer 34. It should be noted that a conventional cased round could also be utilized.
  • the size of the charges 16 and 18 could also be increased if additional velocity was necessary and the number of chambers was limited.
  • a weapon for firing a projectile at increased velocities including a gun barrel having an axial bore therethrough,
  • At least one chamber mounted along the barrel in open communication with said bore and forward of said projectile
  • primer means fixed to said charge and extending within said bore, and explosive means for initially propelling the projectile through said bore whereby the projectile will strike the primer means thus producing a secondary detonation which will increase the velocity of the projectile.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Description

a 5 1969 J. J. SCANLON. JR. Em 3,459,101
HIGH VELOCITY WEAPON Filed Nov. 9, 1967 @M 3 MN a o u ow ON mm R A w O E T N mmm V Q I "H AMP g P w \\\\\\\\\&
United States Patent Oflice 3,459,101 Patented Aug. 1969 y Filed Nov. 9, 1967, Ser. No. 681,691
lnt. Cl. F416 21/00; F41f 1/00 U.S. Cl. 89-8 4 Claims ABSTRACT OF THE DISCLOSURE A weapon including a chamber mounted on a gun barrel and containing a caseless charge of propellant therein which partially extends into the path of an oncoming projectile to be ignited thereby.
The invention described herein may be manufactured, used, and licensed by or for the Government for governmental purposes without the payment to us of any royalty thereon.
The invention relates to a high velocity Weapon and more particularly to a high velocity weapon utilizing a secondary charge mounted on said weapon for increasing the velocity of a projectile fired from said Weapon.
In the past, efforts have been made to increase the velocity of a projectile. Most of these efforts have been directed to the addition of powder to the original charge contained in the cartridge case. It was found, however, that in direct proportion to any increases in the original powder charge, there is a dangerous increase in internal pressures occurring within the firearm on discharge of the projectile.
Other methods for increasing the velocity of a projectile, have included the use of the hot gases of the traveling projectile igniting secondary charges along the path of the barrel. In cases where this method was employed, the increase in velocity was minimal because of the location of the projectile when the secondary charge was ignited.
It is therefore an object of the present invention to provide means for increasing the velocity of the projectile as much as Another object is the provision of a high velocity weapon utilizing secondary charge means to increase the velocity of the projectile.
A still further object is to provide a high velocity Weapon utilizing a secondary charge to increase the velocity of a projectile which is initiated by direct contact With said projectile.
The above objects as well as others together with the benefits and advantages of the invention will be apparent upon reference to the detailed description set forth below, particularly when taken in conjunction with the drawing annexed hereto in which is shown a sectional side view of the present invention.
As can be seen in the drawing, there is shown a gun barrel 10 of a weapon (not shown) having a plurality of screw threaded, removable chambers 12 and 14. Contained in each of said chambers 12 and 14 is a charge of molded caseless propellant 16 and 18 having a primer composition 20 and 22 attached in a known manner to said molded propellant 16 and 18 at an end extending through orifice 24 and 26 having an annulus and 27 thereon, and into the passageway 28 of the gun barrel 10. The top portions 13 and 15 of each chamber 12 and 14 are screw threaded and removable to allow for the insertion of the charge therein.
Shown at the left hand portion of gun barrel 10 is a standard caseless 7.62 mm. cartridge 30 having attached at its forward end a projectile 32 and inserted in its rearward portion a primer 34. It should be noted that a conventional cased round could also be utilized.
In operation, when the weapon (not shown) containing for example the standard caseless 7.62 mm. cartridge 30 is fired, the primer 34 which is ignited in a known fashion, ignites the molded propellant 36 of the cartridge 30 thereby propelling projectile 32 down the passageway 28 of the barrel 10. When said projectile 32 strikes primer portion 20 of charge 16, a secondary detonation is produced thereby giving a boost to the velocity of projectile 32. When projectile 32 strikes primer 22 of charge 18 the same result will occur thereby additionally increasing the velocity of projectile 32. Additional chambers, similar to 12 and 14 could be utilized along the length of the gun barrel if additional increases in velocity were required.
The size of the charges 16 and 18 could also be increased if additional velocity was necessary and the number of chambers was limited.
The standard caseless 7.62 mm. cartridge has been disclosed in the patent application of Quinlan et a1. entitled Uniformed Density Caseless Cartridge, Ser. No. 477,044, filed Aug. 3, 1965, now U.S. Patent No. 3,345,945. The composition of charges 16 and 18 would be the same as the composition of the projectile described in the aforementioned patent application.
Obviously, many modifications and variations of the present invention are possible in light of the above teachings. It is therefore to be understood, that within the scope of the appended claims, the invention may be practiced otherwise than as specifically described.
We claim:
1. A weapon for firing a projectile at increased velocities including a gun barrel having an axial bore therethrough,
at least one chamber mounted along the barrel in open communication with said bore and forward of said projectile,
an explosive charge fixed within said chamber, and
primer means fixed to said charge and extending within said bore, and explosive means for initially propelling the projectile through said bore whereby the projectile will strike the primer means thus producing a secondary detonation which will increase the velocity of the projectile.
2. A weapon of the type described in claim 1 wherein :aid explosive charge includes a molded caseless propelant.
3. A weapon of the type described in claim 1 wherein said primer means includes a primer composition integral with said molded caseless propellant.
4. A weapon of the type described in claim 1 wherein said chamber is removably mounted to said barrel.
References Cited UNITED STATES PATENTS 484,009 10/1892 Haskell 89-8 1,477,078 12/ 1923 Rimailho 898 X 2,360,217 10/ 1944 Francis 898 SAMUEL W. ENGLE, Primary Examiner U.S. Cl. X.R. 89-1
US681691A 1967-11-09 1967-11-09 High velocity weapon Expired - Lifetime US3459101A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US68169167A 1967-11-09 1967-11-09

Publications (1)

Publication Number Publication Date
US3459101A true US3459101A (en) 1969-08-05

Family

ID=24736356

Family Applications (1)

Application Number Title Priority Date Filing Date
US681691A Expired - Lifetime US3459101A (en) 1967-11-09 1967-11-09 High velocity weapon

Country Status (1)

Country Link
US (1) US3459101A (en)

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3613499A (en) * 1968-09-25 1971-10-19 Nat Defence Canada Switch for projectile-accelerating system
FR2352270A1 (en) * 1976-05-17 1977-12-16 Bofors Ab MISSILE NON-RECOIL FIRE DEVICE
US4336741A (en) * 1980-01-17 1982-06-29 Ford Motor Company Liquid propellant velocity assistance system for guns
EP0056789A3 (en) * 1981-01-20 1982-09-08 Treuhand Gmbh Fides Recoilless weapon
US4590842A (en) * 1983-03-01 1986-05-27 Gt-Devices Method of and apparatus for accelerating a projectile
EP0331150A1 (en) * 1988-03-03 1989-09-06 THE STATE of ISRAEL Atomic Energy Commission Soreq Nuclear Research Center A method and apparatus for accelerating projectiles
US5016537A (en) * 1990-03-08 1991-05-21 The Boeing Company Controlled explosive, hypervelocity self-contained round for a large caliber gun
US5097743A (en) * 1990-12-14 1992-03-24 Washington Research Foundation Method and apparatus for zero velocity start ram acceleration
US5233903A (en) * 1989-02-09 1993-08-10 The State Of Israel, Atomic Energy Commission, Soreq Nuclear Research Center Gun with combined operation by chemical propellant and plasma
US5841058A (en) * 1996-01-26 1998-11-24 Manis; John Robert Firearms
RU2154793C1 (en) * 1999-06-22 2000-08-20 Российский Федеральный Ядерный Центр - Всероссийский Научно-Исследовательский Институт Экспериментальной Физики Accelerating device
EP1446626A4 (en) * 2001-11-02 2006-06-07 Poly Systems Pty Ltd DEVICE FOR FIREFIGHTING PROJECTILES USING A LIQUEFIED PROPELLANT GAS
US7775148B1 (en) * 2005-01-10 2010-08-17 Mcdermott Patrick P Multivalve hypervelocity launcher (MHL)
US20150241158A1 (en) * 2013-01-23 2015-08-27 John Arthur Yoakam Projectile launching device
US10767967B2 (en) 2018-08-07 2020-09-08 Thomas Faudree, IV Device for controlling a rate of gas pressure increase in a gun barrel
US20230288154A1 (en) * 2022-03-08 2023-09-14 Eddie L Brooks Electrical velocity enhancement assembly

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US484009A (en) * 1892-10-11 haskell
US1477078A (en) * 1922-02-17 1923-12-11 Rimailho Emile Cannon with multiple powder chambers
US2360217A (en) * 1941-06-20 1944-10-10 Francis Louis Multicharge gun

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US484009A (en) * 1892-10-11 haskell
US1477078A (en) * 1922-02-17 1923-12-11 Rimailho Emile Cannon with multiple powder chambers
US2360217A (en) * 1941-06-20 1944-10-10 Francis Louis Multicharge gun

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3613499A (en) * 1968-09-25 1971-10-19 Nat Defence Canada Switch for projectile-accelerating system
FR2352270A1 (en) * 1976-05-17 1977-12-16 Bofors Ab MISSILE NON-RECOIL FIRE DEVICE
US4336741A (en) * 1980-01-17 1982-06-29 Ford Motor Company Liquid propellant velocity assistance system for guns
EP0056789A3 (en) * 1981-01-20 1982-09-08 Treuhand Gmbh Fides Recoilless weapon
US4590842A (en) * 1983-03-01 1986-05-27 Gt-Devices Method of and apparatus for accelerating a projectile
EP0331150A1 (en) * 1988-03-03 1989-09-06 THE STATE of ISRAEL Atomic Energy Commission Soreq Nuclear Research Center A method and apparatus for accelerating projectiles
US5233903A (en) * 1989-02-09 1993-08-10 The State Of Israel, Atomic Energy Commission, Soreq Nuclear Research Center Gun with combined operation by chemical propellant and plasma
US5016537A (en) * 1990-03-08 1991-05-21 The Boeing Company Controlled explosive, hypervelocity self-contained round for a large caliber gun
US5097743A (en) * 1990-12-14 1992-03-24 Washington Research Foundation Method and apparatus for zero velocity start ram acceleration
US6085630A (en) * 1996-01-26 2000-07-11 Manis; John R. Firearms
US5841058A (en) * 1996-01-26 1998-11-24 Manis; John Robert Firearms
RU2154793C1 (en) * 1999-06-22 2000-08-20 Российский Федеральный Ядерный Центр - Всероссийский Научно-Исследовательский Институт Экспериментальной Физики Accelerating device
EP1446626A4 (en) * 2001-11-02 2006-06-07 Poly Systems Pty Ltd DEVICE FOR FIREFIGHTING PROJECTILES USING A LIQUEFIED PROPELLANT GAS
US7775148B1 (en) * 2005-01-10 2010-08-17 Mcdermott Patrick P Multivalve hypervelocity launcher (MHL)
US20150241158A1 (en) * 2013-01-23 2015-08-27 John Arthur Yoakam Projectile launching device
US9772157B2 (en) * 2013-01-23 2017-09-26 John Arthur Yoakam Projectile launching device
US10767967B2 (en) 2018-08-07 2020-09-08 Thomas Faudree, IV Device for controlling a rate of gas pressure increase in a gun barrel
US11199383B2 (en) 2018-08-07 2021-12-14 Thomas Faudree, IV Device for controlling a rate of gas pressure increase in a gun barrel
US20230288154A1 (en) * 2022-03-08 2023-09-14 Eddie L Brooks Electrical velocity enhancement assembly
US12203714B2 (en) * 2022-03-08 2025-01-21 Eddie L Brooks Electrical velocity enhancement assembly

Similar Documents

Publication Publication Date Title
US3459101A (en) High velocity weapon
US5677505A (en) Reduced energy cartridge
US5492063A (en) Reduced energy cartridge
US4015527A (en) Caseless ammunition round with spin stabilized metal flechette and disintegrating sabot
US5359937A (en) Reduced energy cartridge
US4232468A (en) Combination breech-loading to muzzle-loading firearm converting device and projectile casing
US3956990A (en) Beehive projectile
US3336871A (en) Traveling ignition charge
RU2079096C1 (en) Ammunition for barrel systems
US3726218A (en) Low velocity cartridge having total propellant ignition
ATE250748T1 (en) CANNON WITH AXIAL AMMUNITION FEED, WHICH BREACH CHAMBER IS SEALED BY THE BULLET IN THE BREAKER
US3013495A (en) Spotter-tracer projectile
US2409225A (en) Gas system for firearms
US3345770A (en) Automatic rifle for firing caseless ammunition
US3169333A (en) Projectile for firing a leakproof caseless round
US3815503A (en) Self-propelling ballistic projectiles
US3396658A (en) Small arms cartridge
US2835198A (en) Ammunition for firearms
US3396661A (en) Progressive burning firearm propellant
US3437039A (en) Multicharge cartridge for multibarrel automatic guns
US5639982A (en) Means to fire a fully automatic gun underwater using a special barrel clearance blank round
US3618250A (en) Launching arrangement for sub-caliber projectiles
US3058423A (en) Spin, tangential device for projectiles
ES8309002A1 (en) Gun cartridge for flat trajectory or high angle firing.
US3044363A (en) Propulsion means for projectiles