EP3091326B1 - Arme sans recul - Google Patents

Arme sans recul Download PDF

Info

Publication number
EP3091326B1
EP3091326B1 EP15166220.2A EP15166220A EP3091326B1 EP 3091326 B1 EP3091326 B1 EP 3091326B1 EP 15166220 A EP15166220 A EP 15166220A EP 3091326 B1 EP3091326 B1 EP 3091326B1
Authority
EP
European Patent Office
Prior art keywords
piston
shell
propellant charge
counterweight
shell case
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.)
Not-in-force
Application number
EP15166220.2A
Other languages
German (de)
English (en)
Other versions
EP3091326A1 (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, namely to recoilless guns and can be used in armament systems for shootings on ground and air targets.
  • Object of the invention is a device being a thermal impulse machine, which provides for an increased firing range and that minimizes a recoil impulse due to a constructive solution that includes a two-stage scheme of throwing shells, prepared damaging elements, other product mix necessary for solving various challenges including civil use.
  • Document US 4,676,136 refers to an apparatus for recoilless firing of projectiles from a launching tube comprises within the launching tube a forward brake ring, a forward sabot, a propellant charge with an ignition element or screw, a rear sabot, a counter-mass, and a rear brake ring, arranged within the launching tube in the sequence listed.
  • a propellant charge comprising a first cylindrical propellant charge body and a second annular propellant charge body which surrounds this first cylindrical propellant charge body.
  • the closest to the invention is the recoilless gun containing a gun tube with a breech, the rear end of which is provided with a nozzle orifice, and balancing weight placed in the channel of the gun tube between the propellant charge and the rear end of the breech [2].
  • the task of the proposed invention is the creation of a recoilless gun of an increased firing range with minimal recoil.
  • the mentioned technical result in the proposed device is achieved by using a two-stage scheme of throwing, characteristics of the shell construction and the presence of a counterweight.
  • the recoilless gun ( fig. 1-a ) consists of a gun tube 1, a shell 2, a counterweight 3, an electric or other initiator 4 and a starting propellant charge 5.
  • the shell ( fig. 1-b ) consists in turn of a case 6 including a projectile or prepared damaging element 7 and a propellant charge 8, a piston representing a piston rod 9 provided at the breech portion of the gun tube with a piston head 10, the piston rod 9 hermetically entering the shell case, while the piston head 10 rests on the counterweight.
  • the subsequent initiation of the starting propellant charge 5 activates a movement of the shell case 6 and of the piston 9 and 10 in opposite directions along the gun tube, wherein the piston 9 and 10 is adapted to push the counterweight 3 for compensating the recoil impulse ( fig. 2-b ), thereby the exit of the piston rod 9 of the piston from the shell case 6 allows gases of the starting propellant charge 5 to penetrate into the shell case 6 through an opened after the exit of the piston orifice of transmission of the detonation time and to initiate the propellant charge 8 of the shell ( fig. 2-c ) which in turn, causes the increase of pressure in order to obtain the initial exiting speed of the projectile or the prepared damaging elements 7 ( fig.
  • the proposed invention allows to provide an increased firing range and a minimal recoil impulse by a constructive solution, that includes a two-stage scheme of throwing shells or prepared damaging elements, thereby being simple in terms of technology, that determines it's low costs in mass production and high "efficiency-costs" performance when solving problems according to predestination.

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)

Claims (1)

  1. rme sans recul consistant en les éléments suivants :
    - un canon (1),
    - un corps étant un contrepoids (3),
    - une coque (2) consistant en un boîtier (6) comprenant
    - un projectile ou des éléments dommageables préparés (7) et une charge d'agent propulseur (8),
    - un amorceur électrique ou autre (4) et
    - une charge d'agent propulseur de lancement (5),
    dans laquelle la coque (2) comprend en outre un piston comprenant une tige de piston (9) et une tête de piston (10) côté arrière du canon, la tige de piston (9) pénétrant de manière hermétique le boîtier de coque (6), tandis que la tête de piston (10) repose sur le contrepoids (3), dans laquelle la charge d'agent propulseur de lancement (5) peut être disposée dans la zone entre la tête de piston (10) du piston avec le contrepoids (3) et la coque (2), dans laquelle lors de l'actionnement de l'amorceur électrique ou l'autre (4) l'amorçage subséquent de l'agent propulseur de lancement (5) active un mouvement du boîtier de coque (6) et du piston (9, 10) dans des directions opposées le long du canon (1), dans laquelle le piston (9, 10) est adapté afin de pousser le contrepoids (3) pour compenser l'impulsion de recul, la sortie de la tige de piston (9) du piston du boîtier de coque (6) permettant ainsi aux gaz de la charge d'agent propulseur de lancement (5) de pénétrer dans le boîtier de coque (6) et d'amorcer la charge d'agent propulseur (8) de la coque (2), ce qui, à son tour, induit un accroissement de pression afin d'obtenir la vitesse de sortie initiale du projectile ou des éléments dommageables préparés (7), l'impulsion de recul additionnelle étant compensée par le mouvement du boîtier de coque (6) et le flux gazeux de la charge d'agent propulseur (8) dans la zone de basse pression à travers l'orifice généré dans le boîtier de coque (6), ce qui cause une accélération de mouvement du piston et du contrepoids (3).
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 EP3091326A1 (fr) 2016-11-09
EP3091326B1 true 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)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE540531C2 (en) 2016-12-21 2018-09-25 Saab Ab Launcher and method for launching a projectile

Family Cites Families (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
CH668473A5 (de) * 1985-11-29 1988-12-30 Oerlikon Buehrle Ag Vorrichtung zum rueckstossfreien abschiessen von geschossen aus einem abschussrohr.
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
None *

Also Published As

Publication number Publication date
EP3091326A1 (fr) 2016-11-09
CY1119555T1 (el) 2018-03-07
ES2639715T3 (es) 2017-10-30

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