GB471165A - Improvements in ammunition and firearms - Google Patents
Improvements in ammunition and firearmsInfo
- Publication number
- GB471165A GB471165A GB32300/35A GB3230035A GB471165A GB 471165 A GB471165 A GB 471165A GB 32300/35 A GB32300/35 A GB 32300/35A GB 3230035 A GB3230035 A GB 3230035A GB 471165 A GB471165 A GB 471165A
- Authority
- GB
- United Kingdom
- Prior art keywords
- projectile
- charge
- gun
- chamber
- piston
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
- F42B5/02—Cartridges, i.e. cases with charge and missile
- F42B5/16—Cartridges, i.e. cases with charge and missile characterised by composition or physical dimensions or form of propellant charge, with or without projectile, or powder
-
- 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
-
- 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
- F41A13/00—Cooling or heating systems; Blowing-through of gun barrels; Ventilating systems
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S102/00—Ammunition and explosives
- Y10S102/702—Compression ignition
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Portable Nailing Machines And Staplers (AREA)
- Toys (AREA)
Abstract
471,165. firearms; ammunition; explosives. ROST, H. Nov. 21, 1935, No. 32300. Void. Convention date, May 25. [Classes 9 (i), 9 (ii), and 92 (ii)] [Also in Group XIII] A projectile is propelled from a gun by the gases generated by the combustion of a liquid fuel with oxygen derived from a solid oxygenliberating charge. The fuel may be gasoline, kerosene, gas oil, crude oil, mononitrotoluene, or mononitrobenzol. The solid oxygen-liberating charge may be potassium chlorate or perchlorate, or sodium or ammonium perchlorate. The projectile may be further propelled by explosive charges contained in the projectile and fired while the projectile is still in the gun or rocket-wise after the projectile has left the gun. As shown in Fig. 1, a cartridge case 14 is 'fitted with a projectile 12 at one end and a perforated disc 17 at the other end, and contains a charge of potassium chlorate 15 formed with channels 16. The cartridge is inserted in the gun through a loading aperture 2, and is pushed into the chamber of the barrel 1 by a cylindrical breech-block 3, which contains a piston 19 with a rod 21 and a handle 23. Springs 29, 32 urge the piston and breech-block forward, but these parts may be drawn back by the handle. The piston is retracted first and held cocked by a spring catch 30; then the piston and breech-block are drawn back together to open the breech. The breechblock may be held open and released automatically if desired. When a trigger is operated, the spring catch 30 releases the piston, which compresses air in the chamber 9 ; a projection 24 on the handle operates a pump 36 with inlet and outlet valves 38, 37 fed with liquid fuel through a filter 40, whereby the fuel is injected into the chamber 9 by a nozzle 11 ; and a sparking plug 10 is set in operation to ignite the charge in the chamber. The compressed air with the injected fuel mix up with the oxygen derived from the solid charge 16 and the gases generated by the combustion, expel the projectile. The barrel chamber may be kept cool by means of aluminium fins 41. In a modification, the barrel chamber is cooled by a surrounding jacket, and the ignition is performed by a percussion cap in the base of the cartridge adapted to be struck by a firing- pin in the piston. In the cartridge, Fig. 5, the projectile 61 contains additional explosive charges 69 fired in succession in the gun or during flight, ignition being derived from a percussion cap 68 fired when the main propellent charge is ignited. In another cartridge, Fig. 6, the solid charge 75 is in the projectile and the liquid combustible in a fragile container 74, which is burst when a percussion cap 73 is fired. In a modification, the solid charge is in the cartridge and the liquid fuel in the projectile. An arrangement for cooling the gun barrel is shown in Fig. 9. The reciprocation of the breech-block 103 in the cylinder 106 sucks in air through a valve 107 and forces it through a valve 108 to a receptacle 109, from which the air passes through an expansion valve 110 to a cooling jacket 111 around the explosion chamber 102 of the gun barrel 100. The air then escapes through an outlet 112. Instead of air, a gas or liquid adapted for refrigeration may be used in a closed system.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US23412A US2129875A (en) | 1935-05-25 | 1935-05-25 | Ammunition and firearm |
Publications (1)
Publication Number | Publication Date |
---|---|
GB471165A true GB471165A (en) | 1937-08-27 |
Family
ID=21814939
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB32300/35A Expired GB471165A (en) | 1935-05-25 | 1935-11-21 | Improvements in ammunition and firearms |
Country Status (2)
Country | Link |
---|---|
US (1) | US2129875A (en) |
GB (1) | GB471165A (en) |
Families Citing this family (41)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2536597A (en) * | 1946-09-05 | 1951-01-02 | Daniel And Florence Guggenheim | Recoil-operated feeding apparatus for a combustion chamber used in aerial propulsion |
US2564189A (en) * | 1948-06-28 | 1951-08-14 | Frank P Daniell | Combination cap and lid for condiment dispensers with sealing means for cap apertures |
US2574147A (en) * | 1949-06-28 | 1951-11-06 | James M Hobbs | Firearm |
US2965000A (en) * | 1951-11-07 | 1960-12-20 | Leslie A Skinner | Liquid propellant, regenerative feed and recoilless gun |
US2780019A (en) * | 1952-02-19 | 1957-02-05 | George C Sullivan | Gun barrel of aluminum alloy with metallic coatings |
US2804804A (en) * | 1952-06-30 | 1957-09-03 | James M Cumming | Apparatus for impelling a projectile |
US2981153A (en) * | 1952-11-14 | 1961-04-25 | Texaco Experiment Inc | Fuel injection device |
US3313208A (en) * | 1953-03-25 | 1967-04-11 | Jr Edward G Dorsey | Liquid propellant for small caliber gun |
US2834245A (en) * | 1954-04-05 | 1958-05-13 | Charles C Osborne | Blast hole loading device |
US2872846A (en) * | 1954-07-07 | 1959-02-10 | William D Crozier | High velocity gun |
US2922341A (en) * | 1955-11-07 | 1960-01-26 | Olin Mathieson | Projectile propelling system |
US2947221A (en) * | 1956-12-10 | 1960-08-02 | Olin Mathieson | Compression ignition gun |
US2926565A (en) * | 1958-03-10 | 1960-03-01 | Rudolph B Thorness | Safety explosive line cutter |
US3115007A (en) * | 1958-09-22 | 1963-12-24 | Phillips Petroleum Co | Self-actuating hybrid rocket motor |
US3017748A (en) * | 1959-01-02 | 1962-01-23 | Phillips Petroleum Co | Combination liquid and solid propellant spin-stabilized rocket motor |
US3022597A (en) * | 1959-02-18 | 1962-02-27 | Richard A Rucker | Electric toy cannon |
US3367268A (en) * | 1959-10-05 | 1968-02-06 | Exxon Research Engineering Co | Hybrid rocket propellent grain |
US3143446A (en) * | 1959-11-27 | 1964-08-04 | Gen Electric | Propellant charge containing fluid encapsulations |
US3097602A (en) * | 1960-10-28 | 1963-07-16 | Olin Mathieson | Liquid propellant cartridge |
US3328963A (en) * | 1962-12-27 | 1967-07-04 | Curtiss Wright Corp | Attitude control device for space vehicles |
US3195407A (en) * | 1963-05-07 | 1965-07-20 | Olin Mathieson | Liquid propellant projectile unit |
US3202055A (en) * | 1963-11-01 | 1965-08-24 | Olin Mathieson | Valve system for compression ignition device |
US3803975A (en) * | 1971-09-13 | 1974-04-16 | Pulsepower Sys Inc | Liquid propellant weapon |
US3881419A (en) * | 1973-11-02 | 1975-05-06 | Us Navy | Pyrotechnic initiator |
DE2518149C1 (en) * | 1975-04-24 | 1985-10-31 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Propellant gas generation system, in particular for firearms |
US3969979A (en) * | 1975-07-29 | 1976-07-20 | Sun Ventures, Inc. | Liquid propellant for a gun |
DE2809410A1 (en) * | 1978-03-04 | 1979-09-06 | Gen Electric | Igniter for gun liquid propellant or jet engine fuel - has outer tubular conductor spaced from inner conductor by irregular granules of insulating material |
EP0030297A3 (en) * | 1979-11-26 | 1981-10-14 | Ulf Höllthaler | Firearm with a gaseous propulsive charge and projectile therefor |
US4336741A (en) * | 1980-01-17 | 1982-06-29 | Ford Motor Company | Liquid propellant velocity assistance system for guns |
US4376406A (en) * | 1981-03-02 | 1983-03-15 | The United States Of America As Represented By The Secretary Of The Navy | Hybrid gun system |
DE3234638C1 (en) * | 1982-09-18 | 1991-01-03 | Diehl Gmbh & Co | Sealing for differential pressure piston combustion chamber systems of barrel weapons |
US4644843A (en) * | 1985-09-10 | 1987-02-24 | The United States Of Amercia As Represented By The Secretary Of The Navy | Gas actuated gun system for launching a projectile |
US4930238A (en) * | 1988-04-21 | 1990-06-05 | Poff Jr Charles R | Rimfire firearm receiver |
US5703322A (en) * | 1995-02-02 | 1997-12-30 | General Dynamics Land Systems Inc. | Cartridge having high pressure light gas |
DE10347372A1 (en) * | 2003-10-11 | 2005-06-09 | Rheinmetall Waffe Munition Gmbh | gun ammunition |
WO2006020861A2 (en) * | 2004-08-12 | 2006-02-23 | Tippmann Sports, Llc. | Apparatus and method for firing a projectile |
US7735408B1 (en) * | 2004-10-14 | 2010-06-15 | The United States Of America As Represented By The Secretary Of The Army | Mortar tube with cooling fin |
HU227997B1 (en) * | 2005-03-16 | 2012-08-28 | Istvan Attila Levai | Gas-expansion chamber for fire-arm having longer barrel and increased propellant charge |
US20150268022A1 (en) * | 2014-03-23 | 2015-09-24 | Blake Van Brouwer | Channel-forming propellant compression die and method |
RU2714956C1 (en) * | 2018-09-10 | 2020-02-21 | Василий Александрович Казаковцев | Operating method of cartridge-free automatic weapon with balanced automation and device for implementation thereof |
US12203714B2 (en) * | 2022-03-08 | 2025-01-21 | Eddie L Brooks | Electrical velocity enhancement assembly |
-
1935
- 1935-05-25 US US23412A patent/US2129875A/en not_active Expired - Lifetime
- 1935-11-21 GB GB32300/35A patent/GB471165A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
US2129875A (en) | 1938-09-13 |
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