EP3091326A1 - Arme sans recul - Google Patents

Arme sans recul Download PDF

Info

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
Application number
EP15166220.2A
Other languages
German (de)
English (en)
Other versions
EP3091326B1 (fr
Inventor
Anton Alexandrovich Shchukin
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.)
SHCHUKIN, ANTON ALEXANDROVICH
Original Assignee
Shchukin Anton Alexandrovich
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 Shchukin Anton Alexandrovich filed Critical Shchukin Anton Alexandrovich
Priority to ES15166220.2T priority Critical patent/ES2639715T3/es
Priority to EP15166220.2A priority patent/EP3091326B1/fr
Publication of EP3091326A1 publication Critical patent/EP3091326A1/fr
Application granted granted Critical
Publication of EP3091326B1 publication Critical patent/EP3091326B1/fr
Priority to CY20171101162T priority patent/CY1119555T1/el
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • 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)
EP15166220.2A 2015-05-04 2015-05-04 Arme sans recul Not-in-force EP3091326B1 (fr)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Patent Citations (5)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
Title
VICTOR RON: "Panzerfaust», turbulent family", MAGAZINE «WEAPON», 2012, pages 48 - 53

Cited By (3)

* Cited by examiner, † Cited by third party
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
ES2639715T3 (es) 2017-10-30
CY1119555T1 (el) 2018-03-07

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