EP3070429A1 - Projectile destine a intercepter un petit drone - Google Patents

Projectile destine a intercepter un petit drone Download PDF

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Publication number
EP3070429A1
EP3070429A1 EP16000556.7A EP16000556A EP3070429A1 EP 3070429 A1 EP3070429 A1 EP 3070429A1 EP 16000556 A EP16000556 A EP 16000556A EP 3070429 A1 EP3070429 A1 EP 3070429A1
Authority
EP
European Patent Office
Prior art keywords
projectile
net
small drone
network
weights
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP16000556.7A
Other languages
German (de)
English (en)
Other versions
EP3070429B1 (fr
Inventor
Norbert Stelte
Martin Hertel
Harald Schieb
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.)
Diehl Defence GmbH and Co KG
Original Assignee
Diehl BGT Defence GmbH and Co KG
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 Diehl BGT Defence GmbH and Co KG filed Critical Diehl BGT Defence GmbH and Co KG
Publication of EP3070429A1 publication Critical patent/EP3070429A1/fr
Application granted granted Critical
Publication of EP3070429B1 publication Critical patent/EP3070429B1/fr
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H13/00—Means of attack or defence not otherwise provided for
    • F41H13/0006—Ballistically deployed systems for restraining persons or animals, e.g. ballistically deployed nets
    • 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
    • F42B12/56—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 for dispensing discrete solid bodies
    • F42B12/58—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles
    • F42B12/66—Chain-shot, i.e. the submissiles being interconnected by chains or the like
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H11/00—Defence installations; Defence devices
    • F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems

Definitions

  • the invention relates to a projectile for intercepting a small drone.
  • the DE 197 44 742 A1 discloses a device for firing a net at a person.
  • the device is intended to provide a replacement for land mines.
  • the device ejects after a triggering a rotating container upwards.
  • the container detects the distance to objects around it as a function of the ascent.
  • a net is fired in its direction out of the container.
  • the known device is not suitable to intercept a flying object.
  • the object of the aforementioned invention is to provide a device with which a small drone can be intercepted.
  • the projectile comprises an activating agent, an ejection means and a projectile stowed network, wherein the activator time-delayed after firing the projectile from a firing device activates the ejection means by an activation signal, so that thus the network in the direction of flight of the projectile to the small drone is ejected from the projectile.
  • the term "drone” is understood to mean an unmanned aerial vehicle which is either autonomously navigated or remotely controlled.
  • the drone can be an unmanned aircraft or an unmanned helicopter.
  • the drone may be an unmanned helicopter with multiple rotors, such. B. a quadrocopter.
  • small drone is understood to mean a drone having a weight of at most 20 kg, preferably at most 10 kg, in particular at most 5 kg.
  • interception is understood to mean that a flying small drone is prevented from flying by being rendered flightless.
  • the network can be deployed in particular on rotors of the small drone.
  • the small drone thus loses its drive. It can no longer be purposefully navigated or controlled.
  • the small drone is thus unable to fly through the network.
  • the network at least partially wraps around the small drone.
  • the network can completely wrap the small drone.
  • the net can form a kind of Konkon around the small drone.
  • the net can thus dampen the force of impact in case of a crash of the small drone.
  • the network can prevent ammunition from being dropped or fired from the small drone. For example, the dropping of a hand grenade can be prevented. Even the force of an explosion of the small drone or a mounted on this ammunition can be reduced by the network.
  • the activating means comprises a distance sensor which outputs the activation signal upon reaching a predetermined and / or calculated desired distance to the small drone.
  • the distance sensor may be an electro-optical sensor or a radar sensor, for. B. be a signal transit time sensor.
  • B. be a signal transit time sensor.
  • the distance sensor can be provided as a distance sensor known from military technology distance fuse or proximity fuse.
  • the distance sensor has a wide field of view.
  • the distance sensor may comprise evaluation electronics.
  • a specific distance value can be specified.
  • additional sensors and / or further electronics can be provided in the projectile, which allow a calculation of the desired distance. The calculation can be carried out continuously.
  • the desired distance can be calculated, for example, as a function of the projectile speed or the speed of the small drone.
  • the nominal distance is dimensioned so small that the net is deployed immediately before the small drone.
  • the nominal distance is preferably at most 5 m. Particularly preferred is a desired distance of at most 3 m. This can prevent that the small drone still has the opportunity of an evasive maneuver in front of her approaching network and can escape the net.
  • the activating means may comprise, in addition to or as an alternative to the distance sensor, a means for pattern recognition.
  • the means for pattern recognition is designed to detect objects to which the projectile falls, and with typical small drones patterns or for other flying objects, eg. For example, for birds, to compare typical patterns.
  • the activating means may be designed such that the activation signal is output only when the means for pattern recognition has identified an object for which the distance sensor determines the reaching of the desired distance as a small drone. This can be prevented that the network to another flying object, eg. B. on a bird is thrown.
  • the activating means comprises a timing controller which outputs the activation signal at the end of a predetermined and / or calculated period of time.
  • the timing is advantageously designed as an electronic circuit.
  • a predetermined period of time can be entered.
  • a predetermined distance to the small drone can be entered into the timing control.
  • the Time control then calculates the time duration.
  • Other information may also be taken into account in the calculation, for example the ejection speed of the projectile from the firing device and / or the actual projectile velocity measured by a velocity sensor after the projectile has been fired.
  • it can also be given a maximum period of time, with the expiry of the time control outputs the activation signal to prevent collateral damage caused by the projectile.
  • the timing may be provided in addition to the distance sensor. So z. B. when not reaching the desired distance, the activation signal are issued with the expiry of the maximum time.
  • the activating means comprises a receiver for receiving radio signals and / or optical signals, which outputs the activation signal upon receiving a predetermined command signal.
  • the predetermined command signal may thus be a radio signal or an optical signal. It may be delivered by a shooter who fires the projectile by means of the firing device or by an observer watching the flight of the projectile.
  • the optical signal can, for. B. be emitted from the firing device fro light flash, which may be coded to distinguish extraneous light.
  • the receiver may also be provided together with a distance sensor and / or a time control. The receiver may also be configured to receive an abort signal.
  • the termination signal Upon receiving the termination signal, it can be prevented, for example, that the activation signal is output when the nominal distance to the small drone has been reached or when a calculated time has elapsed. This is z.
  • the activation signal is output when the nominal distance to the small drone has been reached or when a calculated time has elapsed. This is z.
  • To prevent collateral damage caused by the projectile may be provided after receiving the abort signal that the activation signal is issued only to the predetermined command signal or expiration of a predetermined time.
  • tensioning weights are mounted on the net for mounting the network after ejection from the projectile.
  • the tension weights may form part of a shell surrounding the projectile.
  • the tension weights can also be provided within the projectile.
  • the tension weights are preferably at the edge of the network with the Network connected.
  • the tension weights each have a through hole through which at least one thread forming the net is guided.
  • two to twelve clamping weights can be provided.
  • four to six clamping weights are provided.
  • the tensioned net preferably has the shape of a rectangle, in particular a square, a pentagon or hexagon, in accordance with the number of tension weights.
  • the spanned network can also have the shape of a circle.
  • the tensioning weights can be arranged, for example, equidistantly on the outer circumference of the net.
  • the tension weights advantageously have a high density. They are z. B. made of steel.
  • the tension weights continue to have a low air resistance. This allows a quick opening of the network.
  • the tension weights and the network are arranged in the projectile such that the network is ejected from the projectile only after the tension weights.
  • the tension weights can first be released from the projectile by the ejection means and subsequently pull the net with it.
  • the network can therefore be ejected from the projectile through the intermediary of the tension weights connected to the network.
  • the ejection means may transmit an additional impulse to the tensioning weights and / or the net, which assists the ejection of the tensioning weights and / or the net from the projectile and the tensioning of the net. On the additional impulse can also be dispensed with, if the projectile with twist, d. H.
  • the ejection means may for example comprise a cutting device which cuts through a holder of the clamping weights, a release device with z. B. springs and / or hooks, which releases the clamping weights, and / or include an opening device which opens a surrounding the clamping weights envelope of the projectile.
  • the ejection means may further comprise, for example, a stepping motor for actuating said devices.
  • the ejection means comprises an ignitable to the activation signal propellant.
  • the ejection means further comprises an igniter for igniting the propellant charge.
  • the detonator receives the activation signal issued by the activator and ignites then the propellant.
  • the propellant may transmit an impulse to the grid and / or to the tensioning weights, which assists the ejection of the tensioning weights and / or the net from the projectile and the tensioning of the net.
  • the tensioning weights are arranged around at least a part of the propellant charge.
  • the propellant charge, the clamping weights and the network can be arranged such that when the ignition of the propellant charge initially the tension weights are ejected from the projectile and pull in the wake of the network with it.
  • the propellant charge can only serve to release the tensioning weights from the projectile.
  • the propellant can destroy a holder of the clamping weights and / or a surrounding the clamping weights enclosure of the projectile.
  • the propellant may alternatively operate, for example, the cutting device which cuts through a holder of the clamping weights. As a result of their rotational energy, the tension weights released by the projectile can then move away from the projectile as well as from each other, thereby expanding the net.
  • the network of aramid fibers, carbon fibers and / or a fabric of nanotubes is formed.
  • the nanotubes are preferably carbon nanotubes.
  • the network thus created is characterized by a low weight with a high strength.
  • the net can have a diameter of between 30 cm and 10 m when clamped. Preferably, the diameter is 1.5 to 8 m. In particular, a mesh diameter of 3 to 5 m is preferred.
  • the mesh size of the net should be such that the air resistance of the net is low, but the small drone can not slip through the net.
  • the mesh size of the mesh is preferably 1 to 20 cm, preferably a mesh size of 4 to 6 cm, more preferably 5 cm mesh size.
  • the projectile comprises a head part and a rear part, wherein the network and the tension weights are accommodated in the head part, and wherein the rear part is constructed such that it can be dismantled into several sections.
  • the tail section may be configured to disassemble into multiple sections during or after ejection of the net.
  • the sections can be fastened by means of a holding device.
  • the holding device can, for. B. be designed as a rope.
  • the propellant and / or another propellant may assist in disassembling the tail section.
  • the propellant charge and / or the further propellant charge the Destroy holding device.
  • the propellant and / or the further propellant may also operate a cutting device. The cutter then cuts the holding device, the z. B. is designed as a rope. Disassembling the projectile into multiple parts can reduce the impact of a projectile impact. Thus, collateral damage can be largely prevented.
  • the projectile from a rifle, a grenade launcher or a pneumatic weapon as Abfeuervorides is fired.
  • the firing device can be a hand-held weapon or a z. B. be by means of a tripod on a surface storable weapon.
  • the rifle, grenade launcher or compressed air weapon may be conventional weapons for firing conventional ammunition.
  • the projectile may have the outer shape of a conventional grenade.
  • the rifle, the grenade launcher or the compressed air weapon can also be specially designed for firing projectiles according to the invention.
  • a compressed air weapon having an opposing piston can be configured in such a way that the projectile, as a piston assigned to the counter piston, can be fired from the compressed air weapon essentially without any recoil.
  • the projectile advantageously has a caliber of at most 100 mm. Most preferably, the projectile caliber has 40mm, 60mm or 90mm.
  • the projectile has a mass of 50 g to 5 kg. Preference is given to projectiles with a mass of 200 g to 700 g.
  • the ejection speed of the projectile from the firing device is advantageously between 50 m / s and 300 m / s. Preferably, the ejection speed is about 100 m / s.
  • the ejection speed can be measured by means of two coils provided in the course of the firing device.
  • the projectile is advantageously suitable to intercept small drones at a distance of 30 m to 500 m.
  • the range of the projectile is preferably 300 m.
  • the required accuracy is advantageously between 2 ° and 10 °. Preferably, the required accuracy is 6 °.
  • the network is clamped immediately before reaching the small drone.
  • the small drone can even be successfully intercepted when the net is not fully deployed. It can even be enough if a tension weight hits the small drone and makes it unable to fly.
  • a leash is attached to the net and / or to a tension weight with a first end, wherein a second end of the leash remains after the firing of the projectile at the firing device.
  • the small drone can be pulled by attaching the line to the firing device after attaching the net to the small drone.
  • the networked small drone can be pulled by means of the leash into a container.
  • the container is preferably designed explosion-proof.
  • the small drone can be controlled destroyed in the container.
  • the small drone can be examined for any danger posed by it. If necessary, the small drone can be defused. Furthermore, by examining the small drone, conclusions can be drawn about the technology used in it and about the persons responsible for it.
  • a parachute may be provided on the net and / or on the tensioning weights.
  • the parachute preferably opens only after the net has made the small drone flightless.
  • Fig. 1 shows a schematic longitudinal section through a first projectile according to the invention 1.
  • the projectile 1 comprises a head part 2 and a rear part 3.
  • the head part 2 is bounded by a sheath 2a and an annular disc 2b.
  • the shell 2a and / or the annular disc 2b are formed, for example, of PVC.
  • a network 4 connected to the net 4 tension weights 5, a propellant 6 and a distance sensor 7 are added.
  • the propellant charge 6 is arranged in the region of a central axis of the projectile 1.
  • the tensioning weights 5 surround the propellant charge 6. For example, eight tensioning weights 5 are provided.
  • the distance sensor 7 is z. B. designed as a laser rangefinder.
  • the distance sensor 7 comprises a laser diode for emitting a laser pulse and a photodiode for receiving the reflected laser pulse.
  • a laser diode for emitting a laser pulse and a photodiode for receiving the reflected laser pulse.
  • photodiode for laser diode and photodiode each provided with a window 2c recess in the shell 2a is provided. In the in Fig. 1 shown sectional view is only one of the two windows 2c recognizable.
  • the rear part 3 is composed of several sections 3a, 3b, 3c, 3d, 3e.
  • an electronics 8 is added in an area adjacent to the head portion 3a.
  • the electronics 8 is connected to the distance sensor 7 via a data line, not shown.
  • the electronics 8 is used to evaluate the data determined by the distance sensor 7.
  • the electronics 8 allows the calculation and / or storage of a desired distance, at the time of reaching the network 4 is to be ejected from the projectile 1.
  • the electronics 8 may also include a timer and means for calculating and / or storing a period of time, at the end of which the network 4 is to be ejected from the projectile 1.
  • the electronics 8 may include a receiver.
  • a command signal can be received, to which the network 4 is to be ejected from the projectile 1.
  • the receiver or another receiver arranged in the electronics 8 can be designed to receive, for example, data transmitted by the firing device.
  • the transmission can also take place, for example, via a transmitting coil arranged on the barrel of the firing device, while the projectile is still located in the firing device.
  • the transmitted data can z. For example, the removal of the small drones to be intercepted just prior to firing the projectile from the firing device, the ejection speed of the projectile from the firing device, and / or the predetermined amount of time computed in the firing device.
  • the section 3a closest to the head part continues to receive a cutting device 9 in the region of a central axis of the projectile 1.
  • the cutting device 9 is connected to a cable 10, which passes through the further sections 3b, 3c, 3d, 3e along the central axis of the projectile 1 and is secured to the head part 2 farthest section 3e.
  • the further sections 3b, 3c, 3d, 3e are preferably made in lightweight construction. For example, they can be constructed in a honeycomb structure. They can also be made of foam.
  • the head portion nearest portion 3a is preferably made of a solid material for the protection of the electronics 8, for. B. of PVC.
  • the individual sections 3a, 3b, 3c, 3d, 3e are firmly against each other.
  • the propellant 6 and the cutting device 9 are configured such that upon ignition of the propellant charge 6, the cutting device 9 is actuated. In this case, the cutting device 9 cuts the rope 10. As a result, lose the individual sections 3a, 3b, 3c, 3d, 3e their connection and fall apart.
  • the projectile 1 is advantageously fired from a specially designed with regard to the projectile 1 pneumatic weapon.
  • the compressed air weapon includes a launch tube into which the projectile 1 is to be inserted from the front. Furthermore, the compressed air weapon has a matched to the projectile 1 opposed piston.
  • the projectile 1 can be fired from the compressed air weapon essentially recoilless.
  • a pressure accumulator can be charged by means of a nitrogen cylinder. Solenoid valve-controlled overflow openings allow the required differential pressure to be directed to the projectile 1.
  • the specially designed compressed air weapon is reloadable.
  • Fig. 2 1 shows an exploded view of a second projectile 11 according to the invention.
  • the second projectile 11 according to the invention differs from the first projectile 1 according to the invention only in that its rear part 3 comprises only four sections 3a, 3b, 3c, 3d.
  • the exploded view illustrates the modular design of the projectile 11. With the ejection of the network 4 and the tension weights 5 due to the ignition of the propellant charge 6 the projectile 11 breaks down into several small parts. The small parts are so small and light that they pose only a small hazard to people. Furthermore, the propellant charge 6 can be designed such that when it is ignited, the casing 2a is blown open.
  • Fig. 3 shows a schematic cross section through a third projectile according to the invention 21.
  • the projectile 21 is a 40 mm cartridge that can be fired by a conventional grenade launcher.
  • the projectile 21 removes a network 4 Carbon fibers on.
  • the network 4 has in the clamped state a diameter of 5 m with a mesh size of 5 cm.
  • the projectile 21 comprises four tension weights 5.
  • the tension weights 5 are made of steel or mineral binder and each form inside with a recess provided quarter circle segments.
  • the recesses taken together form a cylindrical shape which receives a propellant 6.
  • the outer circumference of the tensioning weights 5 forms part of an enclosure of the projectile 21.
  • the tensioning weights 5 can form, for example, the dome-shaped part of the projectile 21 directed in the direction of flight.
  • the tension weights 5 can also be surrounded by an additional enclosure instead.
  • the first 1 and second projectile 11 according to the invention can tensioning weights 5 in the in Fig. 3 illustrated arrangement.
  • the projectile 1, 11, 21 approaches on a ballistic trajectory of the small drone.
  • the tail section 3 of the projectile is used to stabilize the trajectory.
  • At the end of the period transmitted by the electronics 8 timing transmits an activation signal to the propellant 6.
  • the propellant 6 ignites and accelerates the tension weights 5 in the direction of the small drone to be intercepted.
  • the tension weights 5 pull the network 4 attached to them.
  • the tension weights 5 undergo an acceleration in a radial direction with respect to the projectile 1, 11, 21 by the propellant charge 6.
  • the tensioning weights 5 are removed from one another. This leads to a stretching of the network 4.
  • the network 4 is clamped immediately before reaching the small drone.
  • the small drone to be intercepted an obstacle at which the clamped network 4 is stopped.
  • the tension weights 5 continue to fly due to their inertia initially. By tightening the network 4, however, the tension weights 5 are moved towards each other and thrown back. As a result, the small drone is wrapped by the network 4. In particular, the drive of the small drone is blocked by the network 4. The small drone is unable to fly through the net 4 and falls wrapped in the net 4 to the ground.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Toys (AREA)
  • Catching Or Destruction (AREA)
EP16000556.7A 2015-03-17 2016-03-08 Projectile destiné a intercepter un petit drone Not-in-force EP3070429B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102015003324.7A DE102015003324A1 (de) 2015-03-17 2015-03-17 Projektil zum Abfangen einer Kleindrohne

Publications (2)

Publication Number Publication Date
EP3070429A1 true EP3070429A1 (fr) 2016-09-21
EP3070429B1 EP3070429B1 (fr) 2018-09-26

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Family Applications (1)

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EP16000556.7A Not-in-force EP3070429B1 (fr) 2015-03-17 2016-03-08 Projectile destiné a intercepter un petit drone

Country Status (2)

Country Link
EP (1) EP3070429B1 (fr)
DE (1) DE102015003324A1 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106679507A (zh) * 2017-01-23 2017-05-17 芜湖博高光电科技股份有限公司 一种软毁伤弹药
RU2789825C1 (ru) * 2022-10-14 2023-02-10 Федеральное Государственное Бюджетное Образовательное Учреждение Высшего Образования "Новосибирский Государственный Технический Университет" Боеприпас подствольного гранатомета для поражения беспилотных летательных аппаратов

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Publication number Priority date Publication date Assignee Title
DE102016219457A1 (de) * 2016-10-07 2018-04-12 Mbda Deutschland Gmbh Verfahren und System zur Abwehr von Bedrohungsflugkörpern in Form steuerbarer unbemannter Kleinluftfahrzeuge
DE102017105565A1 (de) 2017-03-15 2018-09-20 Rheinmetall Waffe Munition Gmbh Munitions- und Logistikkonzept für insbesondere Artilleriegeschosse
DE102019103148A1 (de) * 2019-02-08 2020-08-13 Andreas Voss Vorrichtung und Verfahren zur Abwehr von Flugkörpern

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DE19744742A1 (de) 1997-10-10 1999-04-15 Lfk Gmbh Nichtletales Personen-Abwehrsystem
US5898125A (en) * 1995-10-17 1999-04-27 Foster-Miller, Inc. Ballistically deployed restraining net
DE10005931A1 (de) 2000-02-10 2001-08-16 Bugiel Horst Georg Netzabschußgerät und dazugehöriges Netz zum Einnetzen von Personen
US6626077B1 (en) * 2002-10-16 2003-09-30 Mark David Gilbert Intercept vehicle for airborne nuclear, chemical and biological weapons of mass destruction
EP1724547A1 (fr) * 2005-05-21 2006-11-22 Diehl BGT Defence GmbH & Co.KG Dispositif de lancement
US20090084284A1 (en) * 2007-08-07 2009-04-02 Martinez Martin A Non-Lethal Restraint Device With Diverse Deployability Applications
US20120210904A1 (en) * 2008-08-11 2012-08-23 Merems Paul A Interceptor projectile and method of use

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FR859282A (fr) * 1939-05-04 1940-12-14 Projectile à filet
DE3146166A1 (de) * 1981-11-21 1983-05-26 Rheinmetall GmbH, 4000 Düsseldorf Wurfkoerper
DE3722420A1 (de) * 1987-07-07 1989-01-26 Deutsch Franz Forsch Inst Geschoss zur bekaempfung eines hubschraubers
DE4409424C1 (de) * 1994-03-18 1995-08-10 Daimler Benz Aerospace Ag Abfangvorrichtung für Flugobjekte
DE19716527C1 (de) * 1997-04-19 1998-10-01 Lfk Gmbh Fangnetz für Personen
EP2042826A1 (fr) * 2006-07-17 2009-04-01 Andrey Evgenievich Nazdratenko Dispositif de projection de filet

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Publication number Priority date Publication date Assignee Title
US5898125A (en) * 1995-10-17 1999-04-27 Foster-Miller, Inc. Ballistically deployed restraining net
DE19744742A1 (de) 1997-10-10 1999-04-15 Lfk Gmbh Nichtletales Personen-Abwehrsystem
DE10005931A1 (de) 2000-02-10 2001-08-16 Bugiel Horst Georg Netzabschußgerät und dazugehöriges Netz zum Einnetzen von Personen
US6626077B1 (en) * 2002-10-16 2003-09-30 Mark David Gilbert Intercept vehicle for airborne nuclear, chemical and biological weapons of mass destruction
EP1724547A1 (fr) * 2005-05-21 2006-11-22 Diehl BGT Defence GmbH & Co.KG Dispositif de lancement
US20090084284A1 (en) * 2007-08-07 2009-04-02 Martinez Martin A Non-Lethal Restraint Device With Diverse Deployability Applications
US20120210904A1 (en) * 2008-08-11 2012-08-23 Merems Paul A Interceptor projectile and method of use

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106679507A (zh) * 2017-01-23 2017-05-17 芜湖博高光电科技股份有限公司 一种软毁伤弹药
RU2789825C1 (ru) * 2022-10-14 2023-02-10 Федеральное Государственное Бюджетное Образовательное Учреждение Высшего Образования "Новосибирский Государственный Технический Университет" Боеприпас подствольного гранатомета для поражения беспилотных летательных аппаратов

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Publication number Publication date
EP3070429B1 (fr) 2018-09-26
DE102015003324A1 (de) 2016-09-22

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