EP3155346A1 - Appareil de mise à feu comportant une différence de pression réglable dans le tuyau de lancement pour des rockets ou des fusils - Google Patents

Appareil de mise à feu comportant une différence de pression réglable dans le tuyau de lancement pour des rockets ou des fusils

Info

Publication number
EP3155346A1
EP3155346A1 EP15727992.8A EP15727992A EP3155346A1 EP 3155346 A1 EP3155346 A1 EP 3155346A1 EP 15727992 A EP15727992 A EP 15727992A EP 3155346 A1 EP3155346 A1 EP 3155346A1
Authority
EP
European Patent Office
Prior art keywords
pressure chamber
firing
pressure
low
tube
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
EP15727992.8A
Other languages
German (de)
English (en)
Other versions
EP3155346B1 (fr
Inventor
Harald STRUCK
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.)
Dynamit Nobel Defence GmbH
Original Assignee
Dynamit Nobel Defence GmbH
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 Dynamit Nobel Defence GmbH filed Critical Dynamit Nobel Defence GmbH
Priority to PL15727992T priority Critical patent/PL3155346T3/pl
Publication of EP3155346A1 publication Critical patent/EP3155346A1/fr
Application granted granted Critical
Publication of EP3155346B1 publication Critical patent/EP3155346B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F41A1/06—Adjusting the range without varying elevation angle or propellant charge data, e.g. by venting a part of the propulsive charge gases, or by adjusting the capacity of the cartridge or combustion chamber
    • 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
    • F41A21/00—Barrels; Gun tubes; Muzzle attachments; Barrel mounting means
    • F41A21/28—Gas-expansion chambers; Barrels provided with gas-relieving ports
    • 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
    • F41A13/06—Evacuating combustion gas from barrels

Definitions

  • the invention relates to a firing device for firing cartridges, in particular rifle cartridges, with an ammunition storage for receiving the cartridges and a launching tube in the direction of firing in front of the ammunition storage.
  • Such firing devices are, for example, rifles or missile weapons.
  • rifles the problem arises that ammunition for, for example, rabbits for a boar are too weak and would not kill the boar immediately.
  • wild boar ammunition were to be used for hare hunting, it would be too strong and kill the hare immediately, but make it unsuitable for consumption.
  • missile weapons it would be an advantage to practice the ballistic flight with, for example, rifle ammunition.
  • the invention is therefore based on the object to improve a shooting machine according to the preamble of claim 1 so that the pressure difference in the launch tube both in the high pressure region, i. before the ammunition store, as well as in the low pressure area, i. in the weft direction before the high pressure area, the requirements can be easily adjusted.
  • the invention is characterized by a high pressure chamber, which sees the launching tube in the weft direction, at its rear end, a low pressure chamber, which is arranged in the weft direction before the high pressure chamber and surrounds the launch tube, high pressure taps in the launch tube in the high pressure chamber, the Connect the inside of the launch tube to the high-pressure chamber, as seen in the direction of the weft, the back and front low-pressure holes in the discharge tube in the region of the low pressure kamner, which connect the interior of the launch tube with the low-pressure chamber, with a blow-out, which connects the high-pressure chamber with the atmosphere and in the blow-out an adjustable valve is arranged.
  • a high pressure chamber which sees the launching tube in the weft direction, at its rear end
  • a low pressure chamber which is arranged in the weft direction before the high pressure chamber and surrounds the launch tube, high pressure taps in the launch tube in the high pressure chamber, the Connect the inside of the launch tube to the high-pressure chamber, as seen in the
  • the high pressure tappings seen in the weft direction arranged in the front region of the high pressure chamber. This can be done as long as a pressure relief until the cartridge, or its bullet leaves the high-pressure chamber.
  • the rear low pressure taps are seen in the weft direction at the rear end of the low pressure chamber and the front low pressure tappings are arranged at the front end of the low pressure chamber.
  • the entire low-pressure chamber for the pressure difference reduction is utilized.
  • the low-pressure chamber is a rotatable sleeve on the launch tube and has the sleeve on an inner surface and are arranged in the inner circumferential surface to the rear and front low-pressure bores congruent bores and is when turning the sleeve on the launch tube of the gas stream adjustable.
  • the pressure difference in the low-pressure region can be easily adjusted by turning the sleeve.
  • the invention is therefore also the object of producing a system is fired with the rifle ammunition and by gas control by means of discharge before the closure and / or reducing the pressure difference in the pipe Speed can be reduced. This can be adjusted via gas valves.
  • This system allows rifle ammunition to be adapted to fire with similar ballistics such as shoulder-based missile weapons.
  • the extracted gas can be used to simulate a return jet and to minimize recoil.
  • the system has the ability to adjust the external ballistics by means of adjustable gas discharge before a closure or adjustable pressure ratios in front of and behind the projectile in the pipe.
  • This excess of gas also serves to simulate a return beam via a marking compound present in a disposable magazine or marking compound loaded in a capsule in the rear emission tube.
  • the excess gas can be derived without marking but with simultaneous pressure conditions and trigger a marking mass at a blow-out.
  • the system is used with a high hit probability for the most adapted external ballistics of a large caliber weapon system, or for the application of the setting of the projectile - energy in case of firing of the same cartridges. This can then be used, for example, as a component for implementing a training system or a practice shooting machine.
  • an excess amount of gas is withdrawn via predefined bores in a collection container which circulates around the closure or the pipe inlet.
  • this pressure extraction is then finely adjusted via a valve or permanently adjusted by the selected cross section to adjust the ballistics of a standard ammunition of a large caliber ammunition (eg a shoulder-based missile weapon).
  • This pressure or gas failure can then be used to represent reflecting areas by passing this through a powder capsule or chamber, possibly also through a smoke-forming substance, and allowing it to flow out to the rear.
  • ammunition-specific deviations can be compensated by means of gas pressure equalization on the sys- tem adapted and thus optics with a rigid line image can be used.
  • the pressure in the pipe behind the projectile can be brought before the projectile over a second reservoir to achieve with the reduction of the pressure difference before and behind the projectile further speed reduction, this is also adjustable by the controlled discharge of the gases.
  • the system includes the ability to adjust the external ballistics by means of adjustable gas discharge behind the closure / pipe start.
  • the gas pressure is reduced via a high-pressure chamber and adjustable blow-out channel and discharged evenly via a valve.
  • a further reduction in speed can be generated by the reduction in the pressure difference from the overhauling gases, which then leads to a further reduction in speed.
  • the excess gas derived from the valve should also serve, when passed over a marker mass present in a disposable magazine, to simulate the return beam from the rear of the tube.
  • a reloadable magazine can be used, which derives the excess gas without marking but with simultaneous pressure conditions.
  • a capsule with a marking mass for the re fl ection simulation can be introduced into the gas outlet at the end of the gas channel.
  • the system has a high probability of hit with largely adjustable and adjustable outer ballistics by adjusting the gas passage at the valve, and optional representation of a vomstrahlzone the blow-out.
  • the gun with tube and adjustable gas outlet is suitable, for example, for installation in various training systems in which the ballistic trajectory is to be adjusted cost-effectively using standard rifle ammunition.
  • the gas duct with adjustable gas passage to the rear contains a Reflecting simulation.
  • the locking system can be adapted to the geometry of a full-caliber weapon, it is designed so that the reloading of the weapon and the repatriation of the ammunition in the magazine after firing guaranteed. At the same time, the system is suitable for applications where it is necessary to adjust the projectile energy for the same ammunition.
  • a disposable magazine containing a shot of a standard munition e.g., 7.62 x 51 with or without a tracer trace
  • a marker mass may be included. This is initiated by the discharged gas excess and marks or represents the sunlightstrahlzone.
  • a rechargeable magazine can be used without marking mass.
  • the system additionally has the optional capability of receiving a marker mass in the form of a capsule at the rear end of the tube. With pipe here is always meant the launching tube.
  • the front end of the pipe is also provided with a thread (which is protected by a sleeve) on which a maneuver cartridge device can be screwed, which enables the firing of maneuver cartridges with simultaneous display of the return zone to the rear by the gas outlet at the rear end of the pipe.
  • FIG. 1 shows a schematic representation of a shooting device according to the invention.
  • the reference numeral 1 shows a rifle cartridge. This is located in the firing direction in front of the ammunition bearing 2, the launching tube 5.
  • the launching tube 5 is surrounded concentrically by a high-pressure chamber 3.
  • This high-pressure chamber 3 extends axially from the ammunition storage 2 to approximately the end of the first quarter of the launching tube.
  • the high pressure chamber 3 is connected to a blow-out 6, in which a valve 7 is located.
  • a low-pressure chamber 4 surrounds the discharge tube 5 concentrically.
  • the low-pressure chamber 4 is a sleeve which can be rotated on the discharge tube 5 and has an inner lateral surface.
  • rear and front low-pressure bores 5b which connect the interior of the discharge tube 5 to the low-pressure chamber 4, are arranged in the discharge tube 5 in the region of the low-pressure chamber 4.
  • congruent bores are arranged on the rear and front low-pressure bores, whereby upon rotation of the sleeve on the launching tube 5, the gas flow is adjustable.
  • FIG. 2 shows the shooting device according to the invention shortly after the initiation of the cartridge 1. Upon initiation, a pressure is generated which drives the projectile 8 forward by default.
  • Figure 3 shows the shooting machine according to the invention when leaving the projectile 8 from the high pressure chamber 3.
  • the projectile of high pressure taps in the high pressure chamber through the projectile bottom is immediately relieved the pressure peak generated by escape of the gases in the high pressure chamber 3. This is determined on-site by the amount, arrangement and size of the high-pressure taps, as well as the volume of the high-pressure chamber and the cross-section of the Ausblaskanals on the one hand and variable by the adjustment of the valve in the exhaust duct.
  • an adjustable through the valve 7 speed reduction of the ammunition is achieved.
  • Figure 4 shows the course of the projectile 8 in the launch tube in the region of the low pressure chamber 4.

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)

Abstract

L'invention concerne un appareil de mise à feu pour mettre à feu des cartouches (1), en particulier des cartouches de fusil, comportant un dépôt de munitions (2) de réception des cartouches (1) et un tuyau de lancement (5) avant le dépôt de munitions (2 ) dans la direction de lancement. Afin que la différence de pression dans le tuyau de lancement (5) puisse être facilement ajustée aux exigences autant dans la zone à haute pression, à savoir avant le dépôt de munitions (2), que dans la zone à faible pression, à savoir dans la direction de lancement avant la zone à haute pression, l'invention est caractérisée par une chambre à haute pression (3) qui entoure le tuyau de lancement (5) à son extrémité arrière, vue dans la direction de lancement, une chambre à faible pression (4) qui est disposée avant la chambre à haute pression (3), vu dans la direction de lancement, et entoure le tuyau de lancement (5), des alésages à haute pression (5a) dans le tuyau de lancement (5) dans la zone de la chambre à haute pression (3) qui relient l'intérieur du tuyau de lancement (5) avec la chambre à haute pression (3), des alésages à faible pression (5b) arrière et avant, vus dans la direction de lancement, dans le tuyau de lancement (5) dans la zone de la chambre à faible pression (4), qui relient l'intérieur du tuyau de lancement (5) avec la chambre à faible pression (4), comportant un canal de soufflage (6) qui relie la chambre à haute pression (3) avec l'atmosphère et une soupape réglable (7) étant disposée dans le canal de soufflage (6).
EP15727992.8A 2014-06-13 2015-06-11 Appareil de mise à feu comportant une différence de pression réglable dans le tube de lancement pour des lance-roquettes ou des fusils Active EP3155346B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL15727992T PL3155346T3 (pl) 2014-06-13 2015-06-11 Urządzenie strzelające z regulowaną różnicą ciśnień w lufie broni rakietowej albo karabinu

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE102014008415 2014-06-13
DE102014017029 2014-11-19
PCT/EP2015/063003 WO2015189305A1 (fr) 2014-06-13 2015-06-11 Appareil de mise à feu comportant une différence de pression réglable dans le tuyau de lancement pour des rockets ou des fusils

Publications (2)

Publication Number Publication Date
EP3155346A1 true EP3155346A1 (fr) 2017-04-19
EP3155346B1 EP3155346B1 (fr) 2019-08-28

Family

ID=53373465

Family Applications (1)

Application Number Title Priority Date Filing Date
EP15727992.8A Active EP3155346B1 (fr) 2014-06-13 2015-06-11 Appareil de mise à feu comportant une différence de pression réglable dans le tube de lancement pour des lance-roquettes ou des fusils

Country Status (6)

Country Link
EP (1) EP3155346B1 (fr)
BR (1) BR112016029039A2 (fr)
ES (1) ES2759538T3 (fr)
PL (1) PL3155346T3 (fr)
SG (1) SG11201610322XA (fr)
WO (1) WO2015189305A1 (fr)

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1549847A (en) * 1924-04-04 1925-08-18 Charles S Reed Gun
BE447475A (fr) * 1931-01-09
US3611867A (en) * 1969-11-03 1971-10-12 Us Army Emergency weapon for firing high-velocity grenade rounds
GB1547562A (en) * 1976-03-19 1979-06-20 Ilsey H V Guns eg for use in the administration of drugs or medicines to animals
US6065384A (en) * 1997-11-10 2000-05-23 Widlin Corporation Variable velocity weapon system having selective lethality and methods related thereto

Also Published As

Publication number Publication date
WO2015189305A1 (fr) 2015-12-17
EP3155346B1 (fr) 2019-08-28
PL3155346T3 (pl) 2020-02-28
ES2759538T3 (es) 2020-05-11
SG11201610322XA (en) 2017-01-27
BR112016029039A2 (pt) 2017-08-22

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