ES8105859A1 - Device for firing a projectile without ejection of gases towards the rear, nor recoil, by means of a launching tube open at both ends. - Google Patents
Device for firing a projectile without ejection of gases towards the rear, nor recoil, by means of a launching tube open at both ends.Info
- Publication number
- ES8105859A1 ES8105859A1 ES495746A ES495746A ES8105859A1 ES 8105859 A1 ES8105859 A1 ES 8105859A1 ES 495746 A ES495746 A ES 495746A ES 495746 A ES495746 A ES 495746A ES 8105859 A1 ES8105859 A1 ES 8105859A1
- Authority
- ES
- Spain
- Prior art keywords
- projectile
- piston
- rod
- launching tube
- propelling charge
- 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
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
Abstract
1. Claims for the Contracting States : SE, IT, CH, LI Device enabling to launch a projectile without backward gas ejection or recoil, using a launching tube (10) open at both ends, which device comprises a projectile (11, 21), a propelling charge (12, 22) situated behind the projectile, an inert mass (14, 24) situated behind the propelling charge and designed to be ejected at the back of the launching tube at firing time, and a piston (13, 23) separating in tight manner the propelling charge from the inert mass band being able to slide backwards after the firing of the propelling charge, along an axially extending portion at the back of the projectile, which portion is provided with means of stopping the piston at its rear end, characterized in that : the projectile (11, 21) is extended at its rear part by at least one rod (15, 25) integral with the projectile and of external diameter smaller than that of the projectile the piston (13, 23) is in direct contact with the propelling charge (12, 22) and the inert mass (14, 24) the means of stopping the piston are means (16, 26) of permanently holding the piston on the rod and means (13a, 27) are provided for aerodynamically stabilizing the projectile in flight with the rod and the piston. 1. Claims for the Contracting States : DE, GB Device enabling to launch a projectile without recoil, using a launching tube (10) open at both ends, which device comprises a projectile (11) extended at its back part by at least a rod (15) which is axially directed and fast with the projectile a propelling charge (12) situated behind the projectile and about the rod (15) an inert mass (14) situated behind the propelling charge and about the rod (15) and designed to be ejected at the back of the launching tube at firing time and a piston (13) separating in tight manner the propelling charge (12) from the inert mass (14) inside the annular space situated between the external surface of the rod (15) and the inner surface of the launching tube (10) when the device is loaded therewith, the piston (13) being able to slide after firing towards the rear end of the rod (15), characterized in that, in order to prevent gas ejection towards the back of the launching tube (10), the rod (15) is provided at its rear end with means (16) of holding back the piston (13) on the rod (15) after firing and in that the face (13a) of piston (13) which is directed towards the projectile (11) is streamlined in order to aerodynamically stabilize the projectile (11) in flight with the rod (15) and piston (13).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7925232A FR2467380B1 (en) | 1979-10-10 | 1979-10-10 | DEVICE FOR SHOOTING WITHOUT EJECTING GAS TO THE REAR, OR BACK-UP |
Publications (2)
Publication Number | Publication Date |
---|---|
ES495746A0 ES495746A0 (en) | 1981-06-16 |
ES8105859A1 true ES8105859A1 (en) | 1981-06-16 |
Family
ID=9230542
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES495746A Expired ES8105859A1 (en) | 1979-10-10 | 1980-10-08 | Device for firing a projectile without ejection of gases towards the rear, nor recoil, by means of a launching tube open at both ends. |
Country Status (5)
Country | Link |
---|---|
EP (1) | EP0027418B1 (en) |
CA (1) | CA1142782A (en) |
DE (1) | DE3070323D1 (en) |
ES (1) | ES8105859A1 (en) |
FR (1) | FR2467380B1 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2558946B1 (en) * | 1984-01-27 | 1988-04-08 | Brandt Armements | LAUNCHING TUBE FOR RECOVERY SHOOTING WEAPON |
FR2602040B1 (en) * | 1986-07-23 | 1988-11-10 | Serat | IMPROVEMENTS IN OR RELATING TO PROJECTILES WITHOUT RECOIL ARMS OR LAUNCHING SYSTEMS |
CN110160396A (en) * | 2019-05-15 | 2019-08-23 | 南京理工大学 | A kind of fire extinguishing bullet launching device and method based on classification coyote hole |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR597391A (en) * | 1924-04-29 | 1925-11-19 | Device and part for non-reactive firing | |
DE1012849B (en) * | 1955-05-20 | 1957-07-25 | Ludger Volpert | Self-propelled projectile |
FR1326176A (en) * | 1961-07-20 | 1963-05-03 | Energa | Projectile |
CH493818A (en) * | 1968-03-07 | 1970-07-15 | Oerlikon Buehrle Ag | Projectile with a hollow explosive charge |
US4012987A (en) * | 1975-09-03 | 1977-03-22 | The United States Of America As Represented By The Secretary Of The Army | Dual combustion missile system |
DE2553201C2 (en) * | 1975-11-27 | 1984-05-10 | Rheinmetall GmbH, 4000 Düsseldorf | Recoil-free and bang-free projectile |
-
1979
- 1979-10-10 FR FR7925232A patent/FR2467380B1/en not_active Expired
-
1980
- 1980-10-08 ES ES495746A patent/ES8105859A1/en not_active Expired
- 1980-10-09 DE DE8080401451T patent/DE3070323D1/en not_active Expired
- 1980-10-09 EP EP19800401451 patent/EP0027418B1/en not_active Expired
- 1980-10-10 CA CA000362148A patent/CA1142782A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
EP0027418B1 (en) | 1985-03-20 |
ES495746A0 (en) | 1981-06-16 |
FR2467380B1 (en) | 1986-04-18 |
DE3070323D1 (en) | 1985-04-25 |
CA1142782A (en) | 1983-03-15 |
EP0027418A1 (en) | 1981-04-22 |
FR2467380A1 (en) | 1981-04-17 |
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