EP3091326A1 - Arme sans recul - Google Patents
Arme sans recul Download PDFInfo
- Publication number
- EP3091326A1 EP3091326A1 EP15166220.2A EP15166220A EP3091326A1 EP 3091326 A1 EP3091326 A1 EP 3091326A1 EP 15166220 A EP15166220 A EP 15166220A EP 3091326 A1 EP3091326 A1 EP 3091326A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- shot
- counterweight
- propellant charge
- chassis
- valve
- 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.)
- Granted
Links
Images
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
Definitions
- the invention relates to military technology to the recoilless rifle guns. Can be used in weapons systems for ground and air targets.
- Object of the invention is a device - thermal impulse machine, which provides increased range, minimizes recoil impulse by a constructive solution that includes a two-tier scheme of throwing the shells, submunitions, ready to respond to various challenges including civil use.
- the closest to the invention was a recoilless rifle, the barrel with the breechblock, which performed at the rear of the jet orifice and balancing weight placed in the barrel between the propelling charge and the back part of the breech ring [2].
- the task of the proposed invention is the creations of recoilless rifles are firing range with minimal impact.
- the technical result in the proposed device is achieved by using two-stage scheme of throwing, features shot and counterweight.
- the new combination of components allows to:
- the invention describes a drawing ( fig. 1 ), which described one of the possible technical solutions.
- Recoilless rifle ( fig. 1-a ) consists of a trunk - 1, 2 - shot, 3 - counterweight, electric or other catalyst - 4 and starter propellant charge - 5.
- Shot ( fig. 1-b ), consists: chassis - 6 with the projectile or submunitions - 7 and propelling charge - 8, the rod valve (aka tube) - 9, with the female side of the breech area - 10, that one party, tightly in the building shot, while the other rests, on the counterweight.
- the subsequent initiation of seed propellant charge 5 calls the movement along a trunk in opposite directions, hull 6 shot and valve core 9 and 10, push counterweight - 3 to compensate for the recoil impulse ( fig. 2-b ), when this, outlet valve core axis - 9 from the chassis - 6, lets start a gas propellant charge 5 to penetrate in the chassis 6, through the opening after the release of the core of the valve hole of the transmission detonation time and initiate the propellant charge - 8 ( fig. 2-c ) that, in turn, will cause the increase of pressure in order to obtain the desired initial speed projectile or projectiles elements - 7 ( fig.
- the proposed invention can provide enhanced range and minimal recoil impulse by a constructive solution, that includes a two-tier scheme of throwing a projectile or manufactured submunitions, though simple in terms of technology, that determines it's mass production at low cost and high "efficiency-cost" in solving problems.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Toys (AREA)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES15166220.2T ES2639715T3 (es) | 2015-05-04 | 2015-05-04 | Arma sin retroceso |
EP15166220.2A EP3091326B1 (fr) | 2015-05-04 | 2015-05-04 | Arme sans recul |
CY20171101162T CY1119555T1 (el) | 2015-05-04 | 2017-11-07 | Οπλο ανευ οπισθοδρομησης |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP15166220.2A EP3091326B1 (fr) | 2015-05-04 | 2015-05-04 | Arme sans recul |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3091326A1 true EP3091326A1 (fr) | 2016-11-09 |
EP3091326B1 EP3091326B1 (fr) | 2017-08-09 |
Family
ID=53510570
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP15166220.2A Not-in-force EP3091326B1 (fr) | 2015-05-04 | 2015-05-04 | Arme sans recul |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP3091326B1 (fr) |
CY (1) | CY1119555T1 (fr) |
ES (1) | ES2639715T3 (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2018117941A1 (fr) * | 2016-12-21 | 2018-06-28 | Saab Ab | Procédé et lanceur pour lancer un projectile |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1395630A (en) | 1920-11-18 | 1921-11-01 | Davis Cleland | Non-recoil gun |
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 |
US4050351A (en) * | 1976-05-04 | 1977-09-27 | Societe Anonyme Dite: Societe Europeenne Depropulsion | Assembly for launching a projectile |
US4676136A (en) * | 1985-11-29 | 1987-06-30 | Werkzeugmaschinenfabrik Oerlikon-Buhrle Ag | Apparatus for recoilless firing of projectiles from a lauching tube |
DE102012010142A1 (de) * | 2012-05-24 | 2013-11-28 | Rheinmetall Waffe Munition Gmbh | Waffensystem mit einer rückstoßfreien oder rückstoßarmen Waffe und einer mit der Waffe verschießbaren Granate |
-
2015
- 2015-05-04 EP EP15166220.2A patent/EP3091326B1/fr not_active Not-in-force
- 2015-05-04 ES ES15166220.2T patent/ES2639715T3/es active Active
-
2017
- 2017-11-07 CY CY20171101162T patent/CY1119555T1/el unknown
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1395630A (en) | 1920-11-18 | 1921-11-01 | Davis Cleland | Non-recoil gun |
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 |
US4050351A (en) * | 1976-05-04 | 1977-09-27 | Societe Anonyme Dite: Societe Europeenne Depropulsion | Assembly for launching a projectile |
US4676136A (en) * | 1985-11-29 | 1987-06-30 | Werkzeugmaschinenfabrik Oerlikon-Buhrle Ag | Apparatus for recoilless firing of projectiles from a lauching tube |
DE102012010142A1 (de) * | 2012-05-24 | 2013-11-28 | Rheinmetall Waffe Munition Gmbh | Waffensystem mit einer rückstoßfreien oder rückstoßarmen Waffe und einer mit der Waffe verschießbaren Granate |
Non-Patent Citations (1)
Title |
---|
VICTOR RON: "Panzerfaust», turbulent family", MAGAZINE «WEAPON», 2012, pages 48 - 53 |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2018117941A1 (fr) * | 2016-12-21 | 2018-06-28 | Saab Ab | Procédé et lanceur pour lancer un projectile |
JP2020503486A (ja) * | 2016-12-21 | 2020-01-30 | サーブ エービーSaab Ab | 発射体を発射するための方法および発射筒 |
US10928147B2 (en) | 2016-12-21 | 2021-02-23 | Saab Ab | Method and launcher for launching a projectile |
Also Published As
Publication number | Publication date |
---|---|
EP3091326B1 (fr) | 2017-08-09 |
CY1119555T1 (el) | 2018-03-07 |
ES2639715T3 (es) | 2017-10-30 |
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