EP3177886B1 - Vorrichtung zum mündungsseitigen entladen eines geschosses aus einem waffenrohr - Google Patents

Vorrichtung zum mündungsseitigen entladen eines geschosses aus einem waffenrohr Download PDF

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Publication number
EP3177886B1
EP3177886B1 EP15738933.9A EP15738933A EP3177886B1 EP 3177886 B1 EP3177886 B1 EP 3177886B1 EP 15738933 A EP15738933 A EP 15738933A EP 3177886 B1 EP3177886 B1 EP 3177886B1
Authority
EP
European Patent Office
Prior art keywords
tail unit
barrel
main body
retaining
fin
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.)
Active
Application number
EP15738933.9A
Other languages
German (de)
English (en)
French (fr)
Other versions
EP3177886A1 (de
Inventor
Ole Dau
Alfons Sackarndt
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.)
Rheinmetall Waffe Munition GmbH
Original Assignee
Rheinmetall Waffe Munition 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 Rheinmetall Waffe Munition GmbH filed Critical Rheinmetall Waffe Munition GmbH
Priority to PL15738933T priority Critical patent/PL3177886T3/pl
Publication of EP3177886A1 publication Critical patent/EP3177886A1/de
Application granted granted Critical
Publication of EP3177886B1 publication Critical patent/EP3177886B1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00—Rocket or torpedo launchers
    • F41F3/04—Rocket or torpedo launchers for rockets
    • F41F3/058—Means for removing duds or misfires
    • 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
    • F41A15/00—Cartridge extractors, i.e. devices for pulling cartridges or cartridge cases at least partially out of the cartridge chamber; Cartridge ejectors, i.e. devices for throwing the extracted cartridges or cartridge cases free of the gun
    • F41A15/22—Tools for extracting cartridges

Definitions

  • the invention relates to a device for the discharge-side unloading a wrong in the barrel of a weapon loaded weapon, a warhead and a wing assembly comprising projectile whose wing has control wing, each having a warhead towards the preferably tapered portion.
  • the DE 10 2005 006 062 A1 deals with this problem and proposes a device for unloading an accidentally incorrectly loaded mortar cartridge comprising a pull-out rod, at the first end of which a holder device insertable into the weapon barrel with finger-shaped pull-out parts and at the second end of a handle part are attached.
  • the invention has for its object to provide a further device with a simple way quickly and safely a falsely loaded wing-stabilized projectile, in particular a mortar shell, discharge side can be discharged from the barrel of a corresponding weapon.
  • the device comprises a base element which can be introduced into the weapon barrel into an end position and rotatable about its longitudinal axis, which has at least one cylindrical guide element supporting the outside surface of the weapon barrel.
  • On the main body axially extending into the gun barrel support arms are provided on the side facing the wing of the corresponding projectile, which are connected on their side facing away from the base body with retaining claws for engaging behind the projectile wing leading edges in the region of their preferably tapered sections.
  • the holding arms are each formed so wound that they remain both during insertion and when pulling out of the device in the space between the two adjacent tail wings.
  • at least one element for inserting and removing the device according to the invention in the weapon barrel and out of this is provided on the base body on the side facing away from the wing saddle.
  • the unloading device according to the invention is simple and compact, relatively light in weight and robust against external influences.
  • the holding arms of the device each have on a circumferentially extending first end face a to the front end of the retaining arm tapered guide surface, which are selected in that, when the base body is introduced into the weapon barrel, the respective guide surface is supported on an adjacent tail wing and causes a rotational movement of the base body about its longitudinal axis.
  • the support arms slide helically into the free spaces between the tail wings, wherein in the inserted end position of the device according to the invention the retaining claw associated retaining claw engages behind the tube wall side end of the adjacent tail in the direction of rotation in the region of its preferably tapered portion and the subsequent withdrawal of the device a positive position is achieved.
  • the retaining arms are arranged circumferentially evenly distributed and their number corresponds to the number of tail wings, so that when pulling out the device according to the invention from the gun barrel each tail wing with a retaining claw is positively connected.
  • the retaining claws may be formed groove-shaped on its side facing the respective tail wings for embracing the tail wing in the region of the preferably tapered region.
  • the base body contains an axial vent hole for the escape of pent-up air, which arises during the discharge process during insertion and withdrawal of the device according to the invention in the gun barrel.
  • On the main body can be attached to the side facing away from the wing panel end for insertion and withdrawal of the device in the gun barrel and out of this a tether.
  • a handle eye can be arranged on the base body on the side facing away from the wing saddle.
  • Divisible number of vanes also works well with a smaller number of jaws a further weight saving can be achieved.
  • 6-wing tail 3 or 2 appropriately trained claws would be possible and useful.
  • Fig.1 1 is a device according to the invention for unloading a wrong way around in the gun barrel 2 ( Fig.2 ) of a front loader mortar loaded mortar shell 5.
  • the mortar shell 5 includes a warhead 3 and a rear side arranged on the warhead 3 wing assembly 4.
  • the wing assembly 4 has five circumferentially, uniformly distributed tail wings, of which Fig.2 only four tail wings 6-6 '''are shown. Each of the tail wings 6-6 ''''has a section 7 which preferably tapers towards the warhead 3.
  • the device 1 comprises a base body 8, which can be inserted into the weapon barrel 2 and is rotatable about its longitudinal axis 100, which is supported on the outside on the inner surface 9 of the weapon barrel 2 via two cylindrical guide elements 10.
  • Each of the five retaining arms 12-16 is connected on its side facing away from the main body 8 with retaining claws 17.
  • the holding arms 12-16 each have a guide face 19, which tapers towards the front end of the holding arm, on a first end face 18 extending in the circumferential direction.
  • These guide surfaces 19 are selected such that when inserting the base body 8 into the weapon barrel 2 by means of a tether 20 (FIG. Fig.3-6 ) support the guide surfaces 19 each at one of the guide surfaces 19 adjacent tail wings 6-6 '''(from the Fig.3-6 Above all, the support of the guide surface 19 of the holding arm 13 on the tail wing 6 'can be seen).
  • a rotational movement of the main body 8 about its longitudinal axis 100 is automatically effected, so that an independent alignment of the device 1 takes place within the weapon barrel 2.
  • the device 1 or the main body 8 is inserted into the weapon barrel 2 and let down until just before the cartridge or mortar shell 5 on tether 20. Then the device 1 is "dropped" on the mortar shell 5 (about 10 cm in height). As a result, an independent alignment or screwing in of the holding arms 12-16 takes place on the tail unit 4 of the mortar shell 5.
  • the holder arms 12-16 snap through the inertia of the rotational movement of the device in its end position (FIG. Fig. 6 ) on. The actual "detent position" is reached when the device is pulled up again after reaching the end position and the wings "lock".
  • a grip eyelet 24 is further arranged, which makes it possible, the device 1 at the end of the discharge at the mouth end of the gun barrel 2 to grab and pull out of the barrel 2.
  • the main body 8 includes an axial vent hole 25 for the escape of pent-up air, which arises during the discharging process during insertion and withdrawal of the device 1 according to the invention in the gun barrel 2.
  • the device 1 can after the successful unloading of the mortar cartridge from the gun barrel by an upward pulling rotational movement from its locking (locking position 26) and thus from the tail 4 (retaining claws 17) are released.
  • wing-stabilized mortar shells can be unloaded from a Vorderladermörser with the device according to the invention, but it can be unloaded with the device according to the invention in the same way also wrong wing-stabilized projectiles from corresponding weapons tubes (for example, from weapons tubes of Schuladerwaffen).
  • the retaining arms it is not absolutely necessary for the retaining arms to be forcedly guided by the tail wings. Rather, the guide arms need only be formed so twisted that they remain in the final position of introduced into the gun device according to the invention in the spaces between adjacent tail wings and the holding claws connected to them are arranged on the support arms that they, for example, by a rotation of the body slide under the preferably tapered portions of the tail wings.
  • the device is not limited to the aforementioned embodiment.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
EP15738933.9A 2014-08-07 2015-07-21 Vorrichtung zum mündungsseitigen entladen eines geschosses aus einem waffenrohr Active EP3177886B1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL15738933T PL3177886T3 (pl) 2014-08-07 2015-07-21 Urządzenie do rozładowywania broni przez wyjmowanie pocisku z lufy od strony wylotu lufy

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102014111307.1A DE102014111307B3 (de) 2014-08-07 2014-08-07 Vorrichtung zum mündungsseitigen Entladen eines Geschosses aus einem Waffenrohr
PCT/EP2015/066612 WO2016020183A1 (de) 2014-08-07 2015-07-21 Vorrichtung zum mündungsseitigen entladen eines geschosses aus einem waffenrohr

Publications (2)

Publication Number Publication Date
EP3177886A1 EP3177886A1 (de) 2017-06-14
EP3177886B1 true EP3177886B1 (de) 2019-01-30

Family

ID=53673957

Family Applications (1)

Application Number Title Priority Date Filing Date
EP15738933.9A Active EP3177886B1 (de) 2014-08-07 2015-07-21 Vorrichtung zum mündungsseitigen entladen eines geschosses aus einem waffenrohr

Country Status (7)

Country Link
EP (1) EP3177886B1 (lt)
DE (1) DE102014111307B3 (lt)
DK (1) DK3177886T3 (lt)
ES (1) ES2718953T3 (lt)
LT (1) LT3177886T (lt)
PL (1) PL3177886T3 (lt)
WO (1) WO2016020183A1 (lt)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3055955B1 (fr) * 2016-09-13 2021-12-03 Etat Francais Represente Par Le Delegue General Pour Larmement Dispositif d'extraction de munition pour vehicule equipe d'un systeme d'artillerie
US10890393B1 (en) 2018-08-21 2021-01-12 David Schoettle Firearm cartridge extraction tool

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2397554A (en) * 1944-12-13 1946-04-02 Dudley M Lontz Handling device
FR923289A (fr) * 1946-01-31 1947-07-02 Brandt Edgar Ets écouvillon
BE521299A (lt) * 1952-07-24
FR1581703A (lt) * 1968-07-18 1969-09-19
US5987799A (en) * 1998-03-12 1999-11-23 Dedeaux; Tina M. Primitive weapon muzzle loader/unloader device
US6257636B1 (en) * 2000-06-02 2001-07-10 The United States Of America As Represented By The United States Department Of Energy Self-actuating mechanical grapple for lifting and handling objects
DE102005006062A1 (de) * 2005-02-10 2006-08-24 Rheinmetall Waffe Munition Gmbh Vorrichtung zum Entladen einer Mörserpatrone
DE102005016879A1 (de) * 2005-04-13 2006-10-19 Rheinmetall Waffe Munition Gmbh Vorrichtung zum Entladen einer Mörserpatrone

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Also Published As

Publication number Publication date
LT3177886T (lt) 2019-05-10
ES2718953T3 (es) 2019-07-05
DE102014111307B3 (de) 2015-11-26
DK3177886T3 (en) 2019-04-29
EP3177886A1 (de) 2017-06-14
PL3177886T3 (pl) 2019-07-31
WO2016020183A1 (de) 2016-02-11

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