EP3575735B1 - Leuchtspursatz für aus einer rohrwaffe verschiessbare leuchtspurmunition - Google Patents

Leuchtspursatz für aus einer rohrwaffe verschiessbare leuchtspurmunition Download PDF

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Publication number
EP3575735B1
EP3575735B1 EP19187608.5A EP19187608A EP3575735B1 EP 3575735 B1 EP3575735 B1 EP 3575735B1 EP 19187608 A EP19187608 A EP 19187608A EP 3575735 B1 EP3575735 B1 EP 3575735B1
Authority
EP
European Patent Office
Prior art keywords
tracer
projectile
tracer charge
shaped housing
light
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
EP19187608.5A
Other languages
German (de)
English (en)
French (fr)
Other versions
EP3575735A1 (de
Inventor
Torsten Niemeyer
Knut KRÜGER
Christian Baumann
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 PL19187608T priority Critical patent/PL3575735T3/pl
Publication of EP3575735A1 publication Critical patent/EP3575735A1/de
Application granted granted Critical
Publication of EP3575735B1 publication Critical patent/EP3575735B1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
    • F42B12/38—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information of tracer type
    • F42B12/382—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information of tracer type emitting an electromagnetic radiation, e.g. laser beam or infrared emission
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C19/00—Details of fuzes
    • F42C19/04—Protective caps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C11/00—Electric fuzes
    • F42C11/001—Electric circuits for fuzes characterised by the ammunition class or type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C11/00—Electric fuzes
    • F42C11/008—Power generation in electric fuzes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C15/00—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
    • F42C15/40—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein the safety or arming action is effected electrically

Definitions

  • the invention relates to a tracer set for tracer ammunition which can be fired from a barrel weapon with a projectile receiving the tracer set, the tracer set either being integrated directly into the projectile or the tracer set comprising a cup-shaped housing.
  • the known tracer sets are each a pyrotechnic set that is either pressed directly into a recess in the floor of the projectile or into a cup-shaped housing, for example made of steel. If a cup-shaped housing is used, this is usually screwed into a threaded hole in the floor of the projectile.
  • the tracer set When the corresponding projectile is fired, the tracer set is ignited by the propellant charge gases of the corresponding ammunition and then burns down, generating great heat.
  • the disadvantage of the known tracer sets is therefore, inter alia, that they can set the area around the point of impact of the projectile on fire in dry weather, provided that they are not completely burned out when the projectile hits the ground.
  • pyrotechnic tracer sets harbor dangers in the rough handling of the ammunition and, due to the classification according to the Explosives Act, are associated with a relatively high administrative, transport and storage effort.
  • the invention is based on the object of developing a tracer set in which a strong development of heat is reliably avoided when it is used as intended, so that the area around a projectile impact cannot be set on fire by the tracer set.
  • the invention is essentially based on the idea of using an electrical tracer set instead of a pyrotechnic tracer set, in which the tracer is not generated by the burning of a pyrotechnic mixture after the respective projectile has been fired, but rather by the lighting of one or more electrical illuminants, preferably light-emitting diodes, and the bullet tracking is thus carried out by a "cold" light trail.
  • a luminous ammunition for illuminating a battlefield which proposes not to use a pyrotechnic flare for the luminous ammunition, but an electric luminous element which, depending on its intended use, emits light in the visible and / or infrared wavelength range.
  • the light ammunition goes to the ground by means of a parachute and illuminates the battlefield.
  • US2004 / 0099173 A1 and US2005 / 0034627 A1 reveal flares.
  • the tracer set according to the invention essentially comprises an electrical power supply device arranged at the bottom in the cup-shaped housing, a circuit device and a light-emitting diode arrangement which can be supplied with electrical voltage from the power supply device via the circuit device.
  • optics consisting of a lens or a lens system are also provided in the area of the rear opening of the cup-shaped housing. If a lens or a lens system is not used, the focusing is implemented by a reflector. Instead of a cup, the components of the tracer can also be built directly into the projectile body.
  • the tracer set according to the invention is completely inert and can therefore not be implemented unintentionally. Since it is not a dangerous good within the meaning of the Explosives Act, it is also less complicated to send than conventional pyrotechnic tracer sets. In addition, the color of the light track can be achieved in a simple manner by appropriate selection of the light-emitting diode (s).
  • the energy supply device is preferably a bullet-proof battery located in a battery receptacle. Such batteries known from the prior art already have a service life of 10 years and more.
  • At least one capacitor can be integrated in the light ammunition.
  • Further energy supply options are wind turbines, set-back generators, etc.
  • the inner surface of the cup-shaped housing can be made reflective in the area of the light-emitting diode and the optics adjoining it at the rear (for example by means of chrome plating).
  • the optics can be designed as a lens system or as a reflector.
  • the tracer set in particular the optics, is heavily stressed by the high pressure when the projectile is fired and the optical components of the tracer set would also be heavily contaminated by the propellant charge gases, it is advisable to close the rear opening of the cup-shaped housing with a detachable closure part.
  • This closure part can preferably consist of an elastic membrane made of rubber or plastic, which has a contour adapted to the optics of the tracer set in its middle area, and which can be frictionally connected to the projectile receiving the tracer set at the edge (e.g. with the help of screws).
  • the membrane can be reinforced in the axial area of the closure part by a metallic insert with greater strength than the membrane.
  • the metallic insert can be firmly connected to the membrane made of rubber, for example, by vulcanization.
  • the metallic insert, together with the membrane, protects against the propellant gases.
  • the membrane should preferably have an outer diameter that protrudes laterally beyond the projectile receiving the tracer set, so that when the projectile is fired, the membrane is torn off from the open area of the cup-shaped housing by the air flow.
  • the membrane can be connected circumferentially via several valves with blind hole-like bores in the rear outer wall of the projectile, so that the high-tension propellant gases that penetrated the blind bores when the projectile was fired flow out of the bores again as soon as the projectile hits the muzzle of the Weapon barrel has left the corresponding barrel weapon and tear the membrane with it.
  • the switching device can be, for example, a switching element which, due to the high launch acceleration of the projectile containing the respective tracer set, automatically changes from an open to a closed state and then electrically connects the energy supply device to the light-emitting diode arrangement.
  • an electronic circuit device which is connected to a sensor for detecting the launch of the projectile that can be connected to the tracer set.
  • the electronic circuit device comprises a thyristor which supplies the light-emitting diode arrangement with voltage from the energy supply device via a processor only when a voltage value generated by the sensor has exceeded a predetermined voltage value (1st condition) during a predetermined time interval (2nd condition) (similar to a fuse release).
  • the sensor is a piezosensor, preferably a sheet-like piezoceramic, the first surface of which is supported on the electrical energy supply device and the second surface of which is supported on the electronic circuit device.
  • the inert mass of the energy supply device here, for example, the battery
  • the inert mass of the energy supply device can thus exert a high pressure on the piezo element when it is fired by the acceleration forces and meet the two conditions mentioned above.
  • the sensor is a piezoceramic arranged between the bottom of the cup-shaped housing and the adjacent wall of the projectile.
  • the displacement of the cup-shaped housing is exploited by the high pressure of the propellant gases when the corresponding projectile is fired. This is because a displacement of the housing occurs at least in the elastic range at the high gas pressures that occur during firing. Movements of the housing in the elastic range are sufficient to apply considerable pressure to the piezoceramic located between the bottom of the cup-shaped housing and the projectile.
  • the sequence of the light-emitting diode (s) flashing, switching on the light-emitting diodes only after a pre-pipe time has elapsed, switching off after the flight time and a predefinable safety time, etc.
  • the sequence of the light-emitting diode (s) flashing, switching on the light-emitting diodes only after a pre-pipe time has elapsed, switching off after the flight time and a predefinable safety time, etc.
  • the tracer set according to the invention is fireproof, not only must fireproof components be used, but the components of the tracer set should also be fixed fireproof in the cup-shaped housing by means of corresponding potting compounds.
  • the tracer set 1 denotes a tracer set for tracer ammunition that can be fired from a barrel weapon.
  • the tracer set 1 comprises a cup-shaped housing 2 made of steel, in which an electrical power supply device 3 is arranged at the bottom.
  • the energy supply device 3 comprises a battery holder 4 and a battery 5 located therein.
  • the battery holder 4 serves to center the battery 5 and protects against accidental short circuits when the battery 5 comes into contact with the metallic parts of the tracer set 1.
  • Its material is preferably made of a plastic and / or made of a ceramic material. When using metal, a surface treatment (e.g. by anodizing) for electrical passivation is also conceivable.
  • a capacitor can be used as the energy supply device 3, which is charged via an ammunition-internal energy supply (not shown in more detail) and supplies a circuit device 6 with current after the launch signal.
  • An ammunition-internal energy supply can be an RCID chip to which the necessary energy can be coupled in during / after the projectile exit 4 (luminous ammunition) from the weapon barrel (not shown in detail), for example by means of microwaves.
  • An electronic circuit device 6 is axially connected to the energy supply device 3, followed by a light-emitting diode arrangement 7 which can be supplied with electrical energy by the energy supply device 3 with the aid of the electronic circuit device 6.
  • the electronic circuit device 6 comprises a first circuit board 8, which receives first electronic components 9, and a second circuit board 13 with further electronic components 11, which is fixed in a first potting compound 10.
  • the circuit board 8 of the electronic circuit device 6 serves to support a film-shaped piezo sensor 12, which is arranged between the circuit board 8 and the battery holder 4 and is used as a launch sensor.
  • the light-emitting diode arrangement 7 comprises a second circuit board 13 on which one or more light-emitting diodes 14 are arranged (only a single light-emitting diode is shown for reasons of clarity).
  • a lens (optics) 16 is provided for focusing the light generated by the light-emitting diode 14.
  • the optics 16 are designed in such a way that a suitable opening angle is created for the visibility of the light trail.
  • an opening angle of approximately ⁇ 5 ° to ⁇ 10 ° is preferred for large-caliber ammunition.
  • the optics 16 should be crystal clear (completely transparent to the light of the light emitting diodes 14) and as free as possible from inclusions in order to achieve a high light yield and to avoid unintentional scattering. It can be made of glass, plastic (e.g. a silicone elastomer) or other crystal-clear materials.
  • the load can be realized by gluing in a solid body (lens) or pouring a casting compound either in a mold or with subsequent mechanical processing. A combination is also conceivable.
  • FIG. 1 A completely transparent second potting compound 17 was introduced into the cup-shaped housing 2, in which the light-emitting diode arrangement 7 was already located, and the lens 16 was then pressed into the potting compound 17 before the second potting compound 17 finally hardened.
  • the in Fig. 1 Only schematically indicated filling openings 18, 19 are provided in the side wall of the housing 2.
  • the potting compounds 10, 20, 21 for fixing the components of the tracer set 1 between the second board 13 and the bottom 22 of the housing 2 should not have any air pockets in order to intercept the pressure and acceleration forces and enclose all components.
  • the casting compounds which can be epoxy resins, polyurethanes or silicone elastomers, for example, should not be electrically conductive.
  • Fig.1a the rear opening of the tracer is shown with a reflector geometry 15 '.
  • the geometry is designed in such a way that a reflection takes place as far as possible in the range of ⁇ 5 ° to ⁇ 10 ° mentioned above.
  • the potting compound 17 is then only used to protect the LED.
  • FIG. 2 The block diagram shown here explains in more detail the mode of operation of the tracer set 1 described above when a projectile provided with tracer set 1 is fired: How Fig. 2 can be removed, the electronic circuit device 6 is electrically connected to the battery 5, the piezo sensor 12 and the light-emitting diode (LED) 14 via corresponding lines.
  • the electronic circuit device 6 is electrically connected to the battery 5, the piezo sensor 12 and the light-emitting diode (LED) 14 via corresponding lines.
  • the electronic circuit device 6 essentially comprises a thyristor 60 which always supplies the light-emitting diode 14 with power from the battery 5 via a processor 61 which controls the light-emitting diode 14 when a voltage value generated by the piezo sensor 12 reaches a predetermined voltage value (1st condition) during has exceeded a specified time interval (2nd condition).
  • piezo sensor 12 when a projectile containing tracer set 1 is fired, piezo sensor 12 is loaded by the inertial masses of the internal components of tracer set 1, in particular battery 5, and generates a voltage. If a previously set voltage value suitable for the load is exceeded, a field effect transistor 62 is used (FET 1) conductive and the capacitor of an RC timing element 63 charged. The charging process of the capacitor is dependent on the duration of the pressure acting on the piezo sensor 12 and thus on the duration of the permeability of the field effect transistor 62.
  • the thyristor 60 is ignited and the processor 61 is supplied with voltage from the battery 5 via further field effect transistors (FET 2/3) 64 so that the processor 61 can start a corresponding program .
  • the processor 61 supplies the light-emitting diode 14 with the voltage of the battery 5 via the driver circuit (FET 4/5) 65.
  • the light-emitting diode 14 is protected from overload by a current limiting circuit 66.
  • the light-emitting diode 14 can be switched so that it can generate any rhythm, such as “switch-on delay”, “flashing”, “variable flashing rhythm” etc.
  • the processor 61 can be dispensed with.
  • the electrical tracer set 1 has the great advantage over pyrotechnic tracer sets that - controlled by the processor 61 - a flashing tracer can be generated and / or that the tracer is only switched on after a predeterminable lead time has elapsed. In this way, the service life of the battery 5 or the light output of the light-emitting diode 14 (increase in performance) can be increased.
  • the duration of the lighting should be timed in such a way that the tracer can light up over the entire flight time of the respective projectile, including a safety time.
  • Switching off the light-emitting diode 14 after a predetermined period of time can be provided so that if the light-emitting diode 14 is unintentionally switched on, not too much energy is consumed and the tracer set 1 can still be used as intended even after it has accidentally illuminated.
  • a one-time "switch-on" with a subsequent defined discharge of the battery can also be provided.
  • the electronic circuit device 6 is preferably designed in such a way that a long service life can be achieved.
  • the field effect transistor 62 has a very high resistance in the switched-off state and therefore consumes virtually no current in this state.
  • the RC timing element 63 is passive and therefore, just like the subsequent high-resistance thyristor 60, likewise does not consume any current. Finally, the components 65 and 66 connected downstream of the thyristor 60 are also de-energized.
  • the tracer set can comprise a multi-part cup-shaped housing, which can considerably simplify the assembly of the tracer set.
  • a tracer set of this type denoted by 1 '
  • a corresponding housing 2' the thread-cutting areas between the individual housing parts being denoted by the reference numeral 23.
  • the inner jacket surface 25 of the cup-shaped housing 2 ' can be made reflective in the area of the light-emitting diode 14 and the adjoining optics 16 (for example by means of chrome plating).
  • a reflector geometry can be incorporated into the open area 15.
  • a corresponding representation can be found in Fig. 1 a.
  • the piezosensor is a piezoceramic arranged between the bottom of the cup-shaped housing and the rear wall of the corresponding projectile. Such an arrangement is shown in Fig. 4 shown.
  • the tracer set labeled 1 ′′ is located in the rear part of a projectile 26 and the piezoceramic 12 ′ is located between the bottom 22 of the cup-shaped housing 2 ′′ and the adjacent wall 27 of the projectile 26.
  • the tracer set 1 ′′ ′′ located in a floor 26 has a light-emitting diode 14 arranged at an angle to the longitudinal axis 100 of the housing.
  • such a closure part 30 can preferably consist of an elastic membrane 31 made of rubber or plastic, which has a contour adapted to the optics 16 of the tracer set 1 in its middle area, and the edge side with the projectile 26 receiving the tracer set 1 frictionally (e.g. can be connected with the aid of screws 32).
  • the membrane 31 has an outer diameter which protrudes laterally beyond the projectile 26 receiving the tracer set 1, so that when the projectile 26 is fired, the membrane 31 is torn off by the air flow 33 from the opening 15 of the cup-shaped housing 2.
  • the membrane 31 ' ( Fig. 7 ) be reinforced in the middle area of the closure part 30 'by a metallic insert 34 with greater strength than the membrane 31'.
  • the metallic insert 34 can be firmly connected by vulcanization to the membrane 31 ′, which is made of rubber, for example.
  • the metallic insert 34 protects the optics 16 or the reflector coating together with the membrane 31 'from the propellant gases.
  • the membrane 31 ′′ of the closure part 30 ′′ does not protrude beyond the projectile 26 at the edge and is fastened to the projectile 26 in a force-locking manner by means of screws 32.
  • the membrane 31 ′′ additionally has several valves 36 which are inserted into corresponding blind bores 37 of the rear outer wall 38 of the projectile 26 intervene.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Health & Medical Sciences (AREA)
  • Electromagnetism (AREA)
  • Optics & Photonics (AREA)
  • Toxicology (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Toys (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
EP19187608.5A 2014-08-19 2015-07-21 Leuchtspursatz für aus einer rohrwaffe verschiessbare leuchtspurmunition Active EP3575735B1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL19187608T PL3575735T3 (pl) 2014-08-19 2015-07-21 Smugacz do amunicji smugowej wystrzeliwanej z broni lufowej

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE102014111852.9A DE102014111852A1 (de) 2014-08-19 2014-08-19 Leuchtspursatz für aus einer Rohrwaffe verschießbare Leuchtspurmunition
PCT/EP2015/066643 WO2016026640A2 (de) 2014-08-19 2015-07-21 Leuchtspursatz für aus einer rohrwaffe verschiessbare leuchtspurmunition
EP15738939.6A EP3183533B1 (de) 2014-08-19 2015-07-21 Leuchtspursatz für aus einer rohrwaffe verschiessbare leuchtspurmunition

Related Parent Applications (2)

Application Number Title Priority Date Filing Date
EP15738939.6A Division-Into EP3183533B1 (de) 2014-08-19 2015-07-21 Leuchtspursatz für aus einer rohrwaffe verschiessbare leuchtspurmunition
EP15738939.6A Division EP3183533B1 (de) 2014-08-19 2015-07-21 Leuchtspursatz für aus einer rohrwaffe verschiessbare leuchtspurmunition

Publications (2)

Publication Number Publication Date
EP3575735A1 EP3575735A1 (de) 2019-12-04
EP3575735B1 true EP3575735B1 (de) 2021-05-05

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Family Applications (2)

Application Number Title Priority Date Filing Date
EP15738939.6A Active EP3183533B1 (de) 2014-08-19 2015-07-21 Leuchtspursatz für aus einer rohrwaffe verschiessbare leuchtspurmunition
EP19187608.5A Active EP3575735B1 (de) 2014-08-19 2015-07-21 Leuchtspursatz für aus einer rohrwaffe verschiessbare leuchtspurmunition

Family Applications Before (1)

Application Number Title Priority Date Filing Date
EP15738939.6A Active EP3183533B1 (de) 2014-08-19 2015-07-21 Leuchtspursatz für aus einer rohrwaffe verschiessbare leuchtspurmunition

Country Status (6)

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EP (2) EP3183533B1 (es)
DE (1) DE102014111852A1 (es)
DK (2) DK3183533T3 (es)
ES (2) ES2882784T3 (es)
PL (2) PL3575735T3 (es)
WO (1) WO2016026640A2 (es)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102017109627B4 (de) * 2017-05-04 2022-08-04 Rheinmetall Waffe Munition Gmbh Elektronische Sicherungsvorrichtung
CN111595211B (zh) * 2020-06-24 2024-06-04 湖南天合终极防务科技实业有限公司 一种高穿透子弹
CA3189132A1 (en) 2020-07-16 2022-01-20 Bae Systems Plc Non-incendiary tracers
EP3940331A1 (en) * 2020-07-16 2022-01-19 BAE SYSTEMS plc Non-incendiary tracers
GB2597252B (en) * 2020-07-16 2024-02-28 Bae Systems Plc Non-incendiary tracers

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4934273A (en) * 1989-06-20 1990-06-19 Spectra Diode Laboratories, Inc. Laser flare
US6880467B1 (en) * 2002-09-11 2005-04-19 Raytheon Company Covert tracer round
US20040099173A1 (en) * 2002-11-01 2004-05-27 Rector Harry Eugene Non-incendiary directionally illuminated tracer bullet
US20050034627A1 (en) * 2003-03-24 2005-02-17 Manole Leon R. System and method for a flameless tracer/marker utilizing an electronic light source
DE10341713B3 (de) * 2003-09-10 2005-06-09 Diehl Bgt Defence Gmbh & Co. Kg Drallstabilisiertes Artillerieprojektil mit einem Generator
US7421951B2 (en) * 2004-12-01 2008-09-09 Drexel University Piezoelectric stun projectile
WO2006086527A1 (en) * 2005-02-07 2006-08-17 Bae Systems Information And Electronic Systems Integration Inc. Radiation homing tag
US7900619B1 (en) * 2007-02-07 2011-03-08 Sierra Innotek, Inc. System for luminescing and propelling a projectile
DE102007048074A1 (de) 2007-10-05 2009-04-09 Rheinmetall Waffe Munition Gmbh Leuchtmunition zur Gefechtsfeldbeleuchtung

Also Published As

Publication number Publication date
PL3183533T3 (pl) 2020-04-30
EP3183533B1 (de) 2019-09-04
WO2016026640A2 (de) 2016-02-25
ES2757602T3 (es) 2020-04-29
EP3183533A2 (de) 2017-06-28
PL3575735T3 (pl) 2021-11-22
ES2882784T3 (es) 2021-12-02
EP3575735A1 (de) 2019-12-04
DK3183533T3 (da) 2019-12-09
WO2016026640A3 (de) 2016-04-14
DE102014111852A1 (de) 2016-02-25
DK3575735T3 (da) 2021-08-09

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