EP2909569B1 - Cartridge and corresponding method of production - Google Patents
Cartridge and corresponding method of production Download PDFInfo
- Publication number
- EP2909569B1 EP2909569B1 EP13776449.4A EP13776449A EP2909569B1 EP 2909569 B1 EP2909569 B1 EP 2909569B1 EP 13776449 A EP13776449 A EP 13776449A EP 2909569 B1 EP2909569 B1 EP 2909569B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- adhesive
- projectile
- edge contour
- cartridge according
- case cover
- 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
Links
- 238000000034 method Methods 0.000 title claims description 3
- 238000004519 manufacturing process Methods 0.000 title description 2
- 239000000853 adhesive Substances 0.000 claims description 29
- 230000001070 adhesive effect Effects 0.000 claims description 29
- 239000003380 propellant Substances 0.000 claims description 12
- 238000013016 damping Methods 0.000 claims description 7
- 125000006850 spacer group Chemical group 0.000 claims description 7
- 229920001971 elastomer Polymers 0.000 claims description 3
- 229920002379 silicone rubber Polymers 0.000 claims description 3
- 239000007787 solid Substances 0.000 claims description 3
- 239000013013 elastic material Substances 0.000 claims description 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims 4
- 229910052710 silicon Inorganic materials 0.000 claims 4
- 239000010703 silicon Substances 0.000 claims 4
- 239000013464 silicone adhesive Substances 0.000 description 6
- 238000003912 environmental pollution Methods 0.000 description 4
- 230000001419 dependent effect Effects 0.000 description 2
- 239000003292 glue Substances 0.000 description 2
- 229920001296 polysiloxane Polymers 0.000 description 2
- 239000004945 silicone rubber Substances 0.000 description 2
- 229920004482 WACKER® Polymers 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
- F42B5/02—Cartridges, i.e. cases with charge and missile
- F42B5/067—Mounting or locking missiles in cartridge cases
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
- F42B5/02—Cartridges, i.e. cases with charge and missile
- F42B5/18—Caseless ammunition; Cartridges having combustible cases
- F42B5/188—Manufacturing processes therefor
Definitions
- the invention relates to a cartridge having a combustible propellant charge sleeve consisting of a sleeve jacket and a sleeve cover and a stator-stabilized projectile with a solid projectile body and a tail unit adjoining the projectile body, wherein the transitional area between projectile body and tail unit tapers to a rear end of the projectile, having frustoconical outer edge contour, at which the provided with a corresponding inner edge contour sleeve cover is positively connected by means of an adhesive.
- the invention proposes to form the adhesive between the projectile and the sleeve cover of the propellant charge tube as a damping element.
- the invention has for its object to provide a cartridge of the type mentioned, in which the likelihood that it comes due to environmental pollution to damage the propellant sleeve through the full caliber bullet, compared to comparable known cartridges is substantially reduced.
- a method for producing such a cartridge is to be specified.
- the layer thickness (s) themselves is (are) dependent on the bonded surface, so that the preferred layer thickness (s) is (are) only as a guide and empirical value (s) are (are).
- Cartridges with combustible propellant charge sleeve in which the respective sleeve cover is connected to a rear-tapered, frustoconical edge contour of a stabilized missile bullet (eg 120 mm bullet) by means of an adhesive, are known from such projectiles.
- the stabilizer-stabilized projectiles are sub-caliber balancing projectiles in which the sabot identifies the truncated-cone-shaped edge contour (cf., for example, US Pat DE 197 41 842 A1 ).
- the spacers are glued to the frusto-conical inner edge contour of the sleeve cover or on the frustoconical outer edge contour of the projectile. Subsequently, the sleeve cover is then pushed onto the projectile and the remaining space between the sleeve cover and the projectile completely filled with a silicone adhesive. Finally, the silicone adhesive is cured.
- the longitudinal section of a Vollkalibergeunteres is shown, the tail body is connected to the sleeve cover of a (not fully shown) propellant charge sleeve.
- the stabilizer-stabilized full-caliber bullet is designated 1 and comprises a solid projectile body 2 and a tail section 3 adjoining the projectile body 2 Leitwerksnov 3.
- the transition region between bullet body 2 and tail 3 a tapering to the rear end of the projectile, frustoconical outer edge contour 4.
- the projectile 1 is frictionally connected to the sleeve cover 5 of a propellant charge sleeve by means of an adhesive 6, wherein the sleeve cover 5 has a frustoconical inner edge contour 7 corresponding to the outer edge contour 4 of the projectile 1.
- the adhesive 6 causes both a frictional connection between sleeve cover 5 and projectile 1 as well as the function of a damping element takes over damage to the propellant charge through the sleeve Full-caliber bullet 1 to avoid environmental pollution.
- the sleeve cover 5 is then pushed onto the projectile 1 and then the remaining space between the sleeve cover 5 and the projectile 1 is completely filled with a silicone adhesive, preferably a silicone rubber (for example Elastosil E43 from Wacker Chemie, Kunststoff).
- a silicone adhesive preferably a silicone rubber (for example Elastosil E43 from Wacker Chemie, Kunststoff).
- Elastosil silicone adhesives are one-component adhesives that cure by absorbing moisture - from the air.
- the specified curing time for further handling is at least 6 hours. If, on the other hand, two-component adhesives, eg Loctite, are used, the defined curing time is at least 50 minutes. As a result, the curing time can be significantly reduced.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Adhesives Or Adhesive Processes (AREA)
Description
Die Erfindung betrifft eine Patrone mit einer aus einem Hülsenmantel und einem Hülsendeckel bestehenden verbrennbaren Treibladungshülse sowie einem leitwerkstabilisierten Geschoss mit einem massiven Geschosskörper und einem sich heckseitig an den Geschosskörper anschließenden Leitwerksträger, wobei der Übergangsbereich zwischen Geschosskörper und Leitwerksträger eine sich zum heckseitigen Ende des Geschosses verjüngende, kegelstumpfförmige äußere Randkontur aufweist, an welcher der mit einer entsprechenden inneren Randkontur versehene Hülsendeckel mittels eines Klebers kraftschlüssig verbunden ist. Um zu erreichen, dass Beschädigungen der Treibladungshülse durch das Vollkalibergeschoss bei Umweltbelastungen vermieden werden, schlägt die Erfindung vor, den Kleber zwischen dem Geschoss und dem Hülsendeckel der Treibladungshülse als Dämpfungselement auszubilden.The invention relates to a cartridge having a combustible propellant charge sleeve consisting of a sleeve jacket and a sleeve cover and a stator-stabilized projectile with a solid projectile body and a tail unit adjoining the projectile body, wherein the transitional area between projectile body and tail unit tapers to a rear end of the projectile, having frustoconical outer edge contour, at which the provided with a corresponding inner edge contour sleeve cover is positively connected by means of an adhesive. In order to achieve that damage to the propellant charge sleeve by the full-caliber bullet is avoided in environmental pollution, the invention proposes to form the adhesive between the projectile and the sleeve cover of the propellant charge tube as a damping element.
Bei den bekannten Patronen müssen die im Rahmen von Umweltbelastungen (Vibrationen, Herunterfallen der Patrone) auftretenden Massenkräfte der relativ schweren Geschosse im Wesentlichen durch die verbrennbaren Treibladungshülsen aufgenommen werden. Dabei ist es aus innenballistischen Gründen nicht möglich, zur Erhöhung der Festigkeit der Treibladungshülsen deren Wandstärke bei einem vorgegebenen Außendurchmesser wesentlich zu erhöhen.In the case of the known cartridges, the mass forces of the relatively heavy projectiles occurring in the context of environmental pollution (vibrations, dropping of the cartridge) must be absorbed essentially by the combustible propellant charge tubes. It is not possible for internal ballistic reasons, to increase the strength of the propellant charge tubes whose wall thickness at a given outer diameter significantly.
Der Erfindung liegt die Aufgabe zugrunde, eine Patrone der eingangs erwähnten Art anzugeben, bei der die Wahrscheinlichkeit, dass es aufgrund von Umweltbelastungen zur Beschädigung der Treibladungshülse durch das Vollkalibergeschoss kommt, gegenüber vergleichbaren bekannten Patronen wesentlich verringert wird. Außerdem soll ein Verfahren zur Herstellung einer derartigen Patrone angegeben werden.The invention has for its object to provide a cartridge of the type mentioned, in which the likelihood that it comes due to environmental pollution to damage the propellant sleeve through the full caliber bullet, compared to comparable known cartridges is substantially reduced. In addition, a method for producing such a cartridge is to be specified.
Diese Aufgabe wird, ausgehend von der
Die Erfindung beruht im Wesentlichen auf dem Gedanken, zwischen dem Geschoss und dem Hülsendeckel der Treibladungshülse ein Dämpfungselement anzuordnen. Dieses wird auf einfache Weise durch entsprechende Wahl und Anordnung des aus einem elastischen Material bestehenden Klebers realisiert, der den Hülsendeckel mit dem Geschoss verbindet. Gleichzeitig dient der Kleber als Dämpfungsmittel. Dabei hat es sich als vorteilhaft erwiesen, wenn als Kleber ein Silikonkleber, vorzugsweise ein Silikonkautschuk, mit einer Schichtdicke von mindestens 300 µm verwendet wird. Die Schichtdicke(n) selbst ist (sind) jedoch abhängig der verklebten Fläche, sodass die bevorzugte(n) Schichtdicke(n) nur als Richt -und Erfahrungswert(e) zu werten ist (sind).
Patronen mit verbrennbarer Treibladungshülse, bei denen der jeweilige Hülsendeckel mit einer sich heckseitig verjüngenden, kegelstumpfförmigen Randkontur eines leitwerkstabilisierten Geschosses (z.B. 120 mm Panzergeschoss) mittels eines Klebers verbunden ist, sind von derartigen Geschossen bekannt. Dabei handelt es sich bei den leitwerkstabilisierten Geschossen um unterkalibrige Wuchtgeschosse, bei denen der Treibkäfig die kegelstumpfförmige Randkontur ausweist (vgl. z.B.
Der Einsatz von Klebern ist als solches bekannt. So offenbart die
The invention is based essentially on the idea to arrange a damping element between the projectile and the sleeve cover of the propellant charge sleeve. This is realized in a simple manner by appropriate choice and arrangement of the existing of an elastic material adhesive, which connects the sleeve cover to the floor. At the same time, the adhesive serves as a damping agent. It has proven to be advantageous if a silicone adhesive, preferably a silicone rubber, having a layer thickness of at least 300 microns is used as the adhesive. However, the layer thickness (s) themselves is (are) dependent on the bonded surface, so that the preferred layer thickness (s) is (are) only as a guide and empirical value (s) are (are).
Cartridges with combustible propellant charge sleeve, in which the respective sleeve cover is connected to a rear-tapered, frustoconical edge contour of a stabilized missile bullet (eg 120 mm bullet) by means of an adhesive, are known from such projectiles. The stabilizer-stabilized projectiles are sub-caliber balancing projectiles in which the sabot identifies the truncated-cone-shaped edge contour (cf., for example, US Pat
The use of adhesives is known as such. So revealed the
Zur Einhaltung einer definierten Schichtdicke des Klebers - auch mit der Funktion eines Dämpfungsmittels - sind zwischen der kegelstumpfförmigen äußeren Randkontur des Geschosses und der gegenüberliegenden inneren Randkontur des Hülsendeckels umfangseitig mindestens bzw. bevorzugt drei gleichmäßig verteilt angeordnete Abstandsteile vorgesehen, bei denen es sich beispielsweise um Gummiplättchen entsprechender Wandstärke handelt.To maintain a defined layer thickness of the adhesive - even with the function of a damping means - circumferentially at least or preferably three evenly spaced spacers are provided between the frusto-conical outer edge contour of the projectile and the opposite inner edge contour of the sleeve cover, which are, for example, corresponding rubber sheets Wall thickness acts.
Zur Herstellung der erfindungsgemäßen Patrone werden auf die kegelstumpfförmige innere Randkontur des Hülsendeckels oder auf die kegelstumpfförmige äußere Randkontur des Geschosses die Abstandsteile aufgeklebt. Anschließend wird dann der Hülsendeckel auf das Geschoss aufgeschoben und der verbleibende Zwischenraum zwischen dem Hülsendeckel und dem Geschoss vollständig mit einem Silikonkleber ausgegossen. Abschließend wird dann der Silikonkleber ausgehärtet.To produce the cartridge according to the invention, the spacers are glued to the frusto-conical inner edge contour of the sleeve cover or on the frustoconical outer edge contour of the projectile. Subsequently, the sleeve cover is then pushed onto the projectile and the remaining space between the sleeve cover and the projectile completely filled with a silicone adhesive. Finally, the silicone adhesive is cured.
Weitere Einzelheiten und Vorteile der Erfindung ergeben sich aus dem folgenden, anhand einer Figur erläuterten Ausführungsbeispiel.Further details and advantages of the invention will become apparent from the following, explained with reference to a figure embodiment.
In der Figur ist der Längsschnitt eines Vollkalibergeschosses dargestellt, dessen Leitwerkskörper mit dem Hülsendeckel einer (nicht vollständig dargestellten) Treibladungshülse verbunden ist.In the figure, the longitudinal section of a Vollkalibergeschosses is shown, the tail body is connected to the sleeve cover of a (not fully shown) propellant charge sleeve.
Das leitwerkstabilisierte Vollkalibergeschoss ist mit 1 bezeichnet und umfasst einen massiven Geschosskörper 2 sowie einen sich heckseitig an den Geschosskörper 2 anschließenden Leitwerksträger 3. Dabei weist der Übergangsbereich zwischen Geschosskörper 2 und Leitwerksträger 3 eine sich zum heckseitigen Ende des Geschosses verjüngende, kegelstumpfförmige äußere Randkontur 4 auf.The stabilizer-stabilized full-caliber bullet is designated 1 and comprises a solid projectile body 2 and a
Im Bereich dieser Randkontur 4 ist das Geschoss 1 mit dem Hülsendeckel 5 einer Treibladungshülse mit Hilfe eines Klebers 6 kraftschlüssig verbunden, wobei der Hülsendeckel 5 eine der äußeren Randkontur 4 des Geschosses 1 entsprechenden kegelstumpfförmige inneren Randkontur 7 besitzt.In the region of this edge contour 4, the projectile 1 is frictionally connected to the
Erfindungsgemäß ist nun vorgesehen, dass der Kleber 6 sowohl eine kraftschlüssige Verbindung zwischen Hülsendeckel 5 und Geschoss 1 bewirkt als auch die Funktion eines Dämpfungselementes übernimmt, um Beschädigungen der Treibladungshülse durch das Vollkalibergeschoss 1 bei Umweltbelastungen zu vermeiden.According to the invention it is now provided that the adhesive 6 causes both a frictional connection between
Hierzu werden zunächst auf die kegelstumpfförmige innere Randkontur 7 des Hülsendeckels 5 oder auf die kegelstumpfförmige äußere Randkontur 4 des Geschosses 1 Abstandsteile 8 aus Gummi mit einer Wandstärke von 800 µm gleichmäßig über den Umfang des Hülsendeckels 5 bzw. des Geschosses 1 aufgeklebt.For this purpose, first spacers 8 of rubber with a wall thickness of 800 microns evenly glued over the circumference of the
Anschließend wird dann der Hülsendeckel 5 auf das Geschoss 1 aufgeschoben und anschließend der verbleibende Zwischenraum zwischen dem Hülsendeckel 5 und dem Geschoss 1 vollständig mit einem Silikonkleber, vorzugsweise einem Silikonkautschuk (beispielsweise Elastosil E43 der Firma Wacker Chemie, München), ausgegossen.Subsequently, the
Abschließend wird dann der zwischen Hülsendeckel 5 und Leitwerksträger 3 befindliche Silikonkleber 6 ausgehärtet.Finally, the silicone adhesive 6 located between the
Silikonkleber der E-Typen von Elastosil sind Ein-Komponentenkleber, die über die Aufnahme von Feuchtigkeit - aus der Luft - aushärten. Die hierfür festgelegte Aushärtezeit für ein weiteres Handling beträgt mindestens 6 Stunden. Verwendet man hingegen ZweiKomponentenkleber, z.B. Loctite, beträgt die festgelegte Aushärtezeit mindestens 50 min. Dadurch kann die Aushärtedauer deutlich reduziert werden.Elastosil silicone adhesives are one-component adhesives that cure by absorbing moisture - from the air. The specified curing time for further handling is at least 6 hours. If, on the other hand, two-component adhesives, eg Loctite, are used, the defined curing time is at least 50 minutes. As a result, the curing time can be significantly reduced.
- 11
- Geschoss, VollkalibergeschossProjectile, full-caliber bullet
- 22
- Geschosskörperprojectile body
- 33
- Leitwerksträgertail boom
- 44
- äußere Randkonturouter edge contour
- 55
- Hülsendeckelcasing cover
- 66
- Kleber, SilikonkleberGlue, silicone glue
- 77
- innere Randkonturinner edge contour
- 88th
- Abstandsteilspacer
Claims (8)
- Cartridge having a combustible propellant charge case comprising a case sleeve and a case cover (5) and also a fin-stabilized projectile (1) with a solid projectile body (2) and a fin carrier (3) attached to the projectile body (2) at the rear end, wherein the transitional region between the projectile body (2) and the fin carrier (3) has a truncated conical outer edge contour (4) tapering to the rear end of the projectile (1), at which edge contour the case cover (5) provided with a corresponding inner edge contour (7) is connected in a force-fitting manner by means of an adhesive (6), wherein the adhesive (6) is an elastic material, wherein at the same time the adhesive (6) acts as a damping means.
- Cartridge according to Claim 1, characterized in that the layer thickness of the adhesive (6) is between 200 - 800 µm.
- Cartridge according to Claim 2, characterized in that the layer thickness of the adhesive (6) is preferably 300 µm.
- Cartridge according to one of Claims 1 to 3, characterized in that in order to maintain a defined layer thickness of the adhesive (6), at least three uniformly distributed spacer parts (8) are provided between the truncated conical outer edge contour (4) of the projectile (1) and the opposite inner edge contour (7) of the case cover (5) on the circumferential side.
- Cartridge according to Claim 4, characterized in that the spacer parts (8) are rubber discs.
- Cartridge according to one of Claims 1 to 5, characterized in that the adhesive (6) is a silicon adhesive.
- Cartridge according to Claim 6, characterized in that the silicon adhesive (6) is a silicon rubber.
- Method of producing the cartridge according to one of Claims 1 to 7, characterized in that the spacer parts (8) are initially adhered to the truncated conical inner edge contour (7) of the sleeve cover (5) or to the truncated conical outer edge contour (4) of the projectile (1), that the case cover (5) is then slid onto the projectile (1) and that the remaining space between the case cover (5) and the projectile (1) is then completely plugged with a silicon adhesive (6) and the silicon adhesive (6) is then allowed to harden.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PL13776449T PL2909569T3 (en) | 2012-10-19 | 2013-10-07 | Cartridge and corresponding method of production |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE201210020541 DE102012020541A1 (en) | 2012-10-19 | 2012-10-19 | Cartridge and method for its production |
| PCT/EP2013/070855 WO2014060239A1 (en) | 2012-10-19 | 2013-10-07 | Cartridge and corresponding method of production |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP2909569A1 EP2909569A1 (en) | 2015-08-26 |
| EP2909569B1 true EP2909569B1 (en) | 2018-02-21 |
Family
ID=49354641
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP13776449.4A Active EP2909569B1 (en) | 2012-10-19 | 2013-10-07 | Cartridge and corresponding method of production |
Country Status (9)
| Country | Link |
|---|---|
| EP (1) | EP2909569B1 (en) |
| DE (1) | DE102012020541A1 (en) |
| DK (1) | DK2909569T3 (en) |
| ES (1) | ES2667338T3 (en) |
| LT (1) | LT2909569T (en) |
| NO (1) | NO2779572T3 (en) |
| PL (1) | PL2909569T3 (en) |
| PT (1) | PT2909569T (en) |
| WO (1) | WO2014060239A1 (en) |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2323244C3 (en) * | 1973-05-09 | 1979-04-19 | Rheinmetall Gmbh, 4000 Duesseldorf | Wing-stabilized sub-caliber bullet |
| DE3037662A1 (en) * | 1980-10-04 | 1982-05-13 | Rheinmetall GmbH, 4000 Düsseldorf | CARTRIDGED AMMUNITION |
| DK0860682T3 (en) * | 1997-02-25 | 2002-07-29 | Ruag Munition | Device for optical marking of the orbit of missiles accelerated by means of drive devices |
| DE19741842B4 (en) | 1997-09-23 | 2006-09-07 | Rheinmetall Waffe Munition Gmbh | cartridge |
| DE19929915A1 (en) * | 1999-06-29 | 2001-01-18 | Rheinmetall W & M Gmbh | Cartridge for a weapon comprises a cage projectile, a combustible sleeve, a cage with a pressure flange and a seal. |
| DE10055068B4 (en) * | 2000-11-07 | 2006-08-17 | Rheinmetall Waffe Munition Gmbh | cartridge |
| DE102007037741B4 (en) | 2007-08-09 | 2014-01-16 | Rheinmetall Waffe Munition Gmbh | A method for connecting a tubular sleeve sheath and a sleeve cover of a cartridge |
| DE102008015421A1 (en) | 2008-03-20 | 2009-09-24 | Rheinmetall Waffe Munition Gmbh | Method of making a cartridge and cartridge having a sabot projectile made by this method |
| DE102008029397A1 (en) | 2008-06-23 | 2009-12-24 | Rheinmetall Waffe Munition Gmbh | Sabot projectile |
| DE102009009772A1 (en) | 2009-02-20 | 2010-09-02 | Rheinmetall Waffe Munition Gmbh | Method for introducing predetermined breaking points in an annular retaining and sealing strip of a sabot projectile and Laborierwerkzeug for performing the method |
-
2012
- 2012-10-19 DE DE201210020541 patent/DE102012020541A1/en not_active Withdrawn
-
2013
- 2013-10-07 EP EP13776449.4A patent/EP2909569B1/en active Active
- 2013-10-07 DK DK13776449.4T patent/DK2909569T3/en active
- 2013-10-07 WO PCT/EP2013/070855 patent/WO2014060239A1/en active Application Filing
- 2013-10-07 PT PT137764494T patent/PT2909569T/en unknown
- 2013-10-07 ES ES13776449.4T patent/ES2667338T3/en active Active
- 2013-10-07 PL PL13776449T patent/PL2909569T3/en unknown
- 2013-10-07 LT LTEP13776449.4T patent/LT2909569T/en unknown
-
2014
- 2014-03-13 NO NO14159374A patent/NO2779572T3/no unknown
Also Published As
| Publication number | Publication date |
|---|---|
| EP2909569A1 (en) | 2015-08-26 |
| NO2779572T3 (en) | 2018-09-29 |
| LT2909569T (en) | 2018-04-25 |
| DK2909569T3 (en) | 2018-05-22 |
| WO2014060239A1 (en) | 2014-04-24 |
| PL2909569T3 (en) | 2018-07-31 |
| DE102012020541A1 (en) | 2014-04-24 |
| PT2909569T (en) | 2018-05-16 |
| ES2667338T3 (en) | 2018-05-10 |
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