EP3177886B1 - Dispositif pour décharger côté sortie d'un canon - Google Patents

Dispositif pour décharger côté sortie d'un canon Download PDF

Info

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)
Other versions
EP3177886A1 (fr
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/fr
Application granted granted Critical
Publication of EP3177886B1 publication Critical patent/EP3177886B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

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)

Claims (9)

  1. Ensemble (1) pour décharger par l'embouchure une munition (5) chargée erronément dans le canon d'une arme et comprenant une tête de combat (3) et un mécanisme (4) de guidage de vol, et dont le mécanisme (4) de guidage de vol possède des ailes (6-6''') de mécanisme de guidage qui présentent chacune une section (7), et dans lequel :
    a) l'ensemble (1) comporte un corps de base (8) apte à être inséré par l'embouchure dans le canon (2) de l'arme jusque dans une position d'extrémité et apte à tourner autour de son axe longitudinal (100), le corps de base présentant au moins un élément cylindrique de guidage (10) dont le côté extérieur s'appuie sur la surface intérieure (9) du canon (2) de l'arme,
    b) des bras de maintien (12-16) qui s'étendent axialement dans le canon (2) de l'arme sont prévus sur le côté frontal (11) du corps de base (8) tourné vers le mécanisme (4) de guidage de vol de la munition (5) concernée,
    c) les bras de maintien (12-16) sont reliés sur leur côté non tourné vers le corps de base (8) à des griffes de maintien (17) qui accrochent par l'arrière les surfaces frontales des ailes (6-6''') du mécanisme de guidage au niveau de leur section (7) qui de préférence se rétrécit,
    d) au moins un élément (20, 24) d'insertion du l'ensemble (1) dans le canon (2) de l'arme et d'extraction de l'ensemble (1) hors de ce dernier est prévu sur le côté frontal, non tourné vers le mécanisme (4) de guidage de vol, du corps de base (8),
    caractérisé en ce que
    e) chacun des bras de maintien (12-16) présente sur un premier côté frontal (18) qui s'étend dans la direction périphérique une surface de guidage (19) qui se rétrécit en direction de l'extrémité avant du bras de maintien (12-16) et qui est sélectionnée de telle sorte que lors de l'insertion du corps de base (8) dans le canon (2) de l'arme, les surfaces de guidage (19) s'appuient sur une aile (6-6''') du mécanisme de guidage voisine de la surface de guidage (19) et ont pour effet un déplacement de rotation du corps de base (8) autour de son axe longitudinal (100).
  2. Ensemble (1) selon la revendication 1, caractérisé en ce que la section (7) est une section qui se rétrécit en direction de la tête de combat (3).
  3. Ensemble selon l'une des revendications 1 ou 2, caractérisé en ce que lorsque l'ensemble (1) est dans la position complètement insérée, la griffe de maintien (17) associée à chaque bras de maintien (12-16) accroche par l'arrière le côté frontal de l'aile (6'-6''', 6) du mécanisme de guidage voisine dans la direction de rotation au niveau de sa section (7) qui de préférence se rétrécit, les bras de maintien (12) proprement dits restant dans les parties situées entre les ailes (6-6''') du mécanisme de guidage.
  4. Ensemble selon l'une des revendications 1 à 3, caractérisé en ce que les bras de maintien (12-16) sont répartis uniformément à la périphérie et en ce que leur nombre correspond au nombre des ailes (6-6''') du mécanisme de guidage.
  5. Ensemble selon l'une des revendications 1 à 5, caractérisé en ce que sur leur côté tourné vers chaque aile (6-6''') du mécanisme de guidage, les griffes de maintien (17) sont configurées en forme de rainures qui chevauchent l'aile (6-6''') du mécanisme de guidage au niveau de sa section (7) qui de préférence se rétrécit.
  6. Ensemble selon l'une des revendications 1 à 5, caractérisé en ce que la forme de la surface (22) de la griffe de maintien (17) qui accroche par l'arrière chaque aile (6-6''') du mécanisme de guidage correspond à la forme de la partie accrochée par l'arrière de l'aile (6-6''') du mécanisme de guidage, de sorte que lors de l'extraction du l'ensemble (1) hors du canon (2) de l'arme, il existe une liaison en correspondance géométrique entre les griffes de maintien (17) et les ailes (6-6''') du mécanisme de guidage.
  7. Ensemble selon l'une des revendications 1 à 6, caractérisé en ce que le corps de base (8) contient un alésage axial d'évent (25).
  8. Ensemble selon l'une des revendications 1 à 7, caractérisé en ce qu'un câble de retenue (20) est fixé sur le côté frontal, non tourné vers les bras de maintien (12-16), du corps de base (8), pour insérer l'ensemble (1) dans le canon (2) de l'arme et pour l'extraire hors de ce dernier.
  9. Ensemble selon l'une des revendications 1 à 8, caractérisé en ce qu'un oeillet de saisie (24) est disposé sur le côté frontal du corps de base (8) non tourné vers les bras de maintien (12-16).
EP15738933.9A 2014-08-07 2015-07-21 Dispositif pour décharger côté sortie d'un canon Active EP3177886B1 (fr)

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 (fr) 2014-08-07 2015-07-21 Dispositif pour décharger côté embouchure un projectile d'un canon

Publications (2)

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

Family

ID=53673957

Family Applications (1)

Application Number Title Priority Date Filing Date
EP15738933.9A Active EP3177886B1 (fr) 2014-08-07 2015-07-21 Dispositif pour décharger côté sortie d'un canon

Country Status (7)

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

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 (fr) * 1952-07-24
FR1581703A (fr) * 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
WO2016020183A1 (fr) 2016-02-11
DE102014111307B3 (de) 2015-11-26
DK3177886T3 (en) 2019-04-29
PL3177886T3 (pl) 2019-07-31
LT3177886T (lt) 2019-05-10
EP3177886A1 (fr) 2017-06-14
ES2718953T3 (es) 2019-07-05

Similar Documents

Publication Publication Date Title
DE102020113538B3 (de) Auszieher-Vorrichtung zum momentfreien Ziehen einer Patronenhülse
EP3177886B1 (fr) Dispositif pour décharger côté sortie d'un canon
DE2125149A1 (de) Waffe
DE102005006062A1 (de) Vorrichtung zum Entladen einer Mörserpatrone
DE19748829C2 (de) Verpackungsbehälter für großkalibrige Munition
DE19644524C2 (de) Geschützturm für Panzerfahrzeuge
DE4135273C2 (de) Ansetzerkopf mit integriertem Auszieher für Munition
DE60305382T2 (de) Vorrichtung zum Adaptieren eines aus einem Rohr abzuschiessenden Projektils
EP2739931B1 (fr) Dispositif de cartouche à blanc et arme à feu automatique convenant pour ledit dispositif
DE4128050C2 (de) Manöverpatrone
DE102017107442B4 (de) Vorrichtung zum Laden einer Rohrwaffe mit Munitionskörpern
DE102008052074A1 (de) Waffensystem mit einem Trägerfahrzeug und einem fahrzeuggebundenen Mörser
DE3640485C1 (en) Bomblet (submunition)
EP2979055B1 (fr) Dispositif de tir de munitions encartouchées
DE4134603B4 (de) Geschützturm
DE102020211065B3 (de) Torpedokassettenadapter und Torpedokassettenadapterverlängerungsstück
EP0510253B1 (fr) Dispositif de chargement auxiliaire pour le refoulement manuel de munitions
EP1413848A1 (fr) Conteneur pour munitions de gros calibre
DE10005412B4 (de) Übungsgeschoß
DE19852360C2 (de) Vorrichtung zur Ladungsraumbegrenzung einer Waffe
DE1703918A1 (de) Vorrichtung zum Auseinanderziehen rohrfoermiger Koerper
DE102015009823B4 (de) Startsystem für einen Lenkflugkörper sowie Lenkflugkörper für ein derartiges Startsystem
DE10252717B4 (de) Verpackungsbehälter für eine grosskalibrige Patrone
EP3637039A1 (fr) Projectile porteur de charges pour une arme à canon
DE178381C (fr)

Legal Events

Date Code Title Description
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE

PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20170120

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

DAV Request for validation of the european patent (deleted)
DAX Request for extension of the european patent (deleted)
GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

INTG Intention to grant announced

Effective date: 20181105

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 1093627

Country of ref document: AT

Kind code of ref document: T

Effective date: 20190215

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 502015007815

Country of ref document: DE

REG Reference to a national code

Ref country code: DK

Ref legal event code: T3

Effective date: 20190423

REG Reference to a national code

Ref country code: SE

Ref legal event code: TRGR

REG Reference to a national code

Ref country code: EE

Ref legal event code: FG4A

Ref document number: E017171

Country of ref document: EE

Effective date: 20190326

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20190130

REG Reference to a national code

Ref country code: NO

Ref legal event code: T2

Effective date: 20190130

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2718953

Country of ref document: ES

Kind code of ref document: T3

Effective date: 20190705

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190530

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190130

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190501

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190130

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190530

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190430

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190130

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190130

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190130

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190130

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190130

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502015007815

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190130

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20191031

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190130

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190130

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190130

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20190731

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190721

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190731

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190731

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190731

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190721

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190130

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190130

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20150721

REG Reference to a national code

Ref country code: AT

Ref legal event code: MM01

Ref document number: 1093627

Country of ref document: AT

Kind code of ref document: T

Effective date: 20200721

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200721

REG Reference to a national code

Ref country code: DE

Ref legal event code: R082

Ref document number: 502015007815

Country of ref document: DE

Ref country code: DE

Ref legal event code: R082

Ref document number: 502015007815

Country of ref document: DE

Representative=s name: DREISS PATENTANWAELTE PARTG MBB, DE

REG Reference to a national code

Ref country code: DE

Ref legal event code: R082

Ref document number: 502015007815

Country of ref document: DE

Representative=s name: DREISS PATENTANWAELTE PARTG MBB, DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190130

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: NO

Payment date: 20230721

Year of fee payment: 9

Ref country code: IT

Payment date: 20230724

Year of fee payment: 9

Ref country code: GB

Payment date: 20230721

Year of fee payment: 9

Ref country code: FI

Payment date: 20230719

Year of fee payment: 9

Ref country code: ES

Payment date: 20230926

Year of fee payment: 9

Ref country code: EE

Payment date: 20230717

Year of fee payment: 9

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: SE

Payment date: 20230719

Year of fee payment: 9

Ref country code: PL

Payment date: 20230714

Year of fee payment: 9

Ref country code: FR

Payment date: 20230726

Year of fee payment: 9

Ref country code: DK

Payment date: 20230721

Year of fee payment: 9

Ref country code: DE

Payment date: 20230719

Year of fee payment: 9

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: LV

Payment date: 20230719

Year of fee payment: 9

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: LT

Payment date: 20240621

Year of fee payment: 10