EP2446219A1 - Corps actif - Google Patents
Corps actifInfo
- Publication number
- EP2446219A1 EP2446219A1 EP10723951A EP10723951A EP2446219A1 EP 2446219 A1 EP2446219 A1 EP 2446219A1 EP 10723951 A EP10723951 A EP 10723951A EP 10723951 A EP10723951 A EP 10723951A EP 2446219 A1 EP2446219 A1 EP 2446219A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- active
- flares
- active body
- container
- body according
- 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.)
- Withdrawn
Links
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 claims abstract description 24
- 239000000020 Nitrocellulose Substances 0.000 claims abstract description 3
- 229920001220 nitrocellulos Polymers 0.000 claims abstract description 3
- 238000010521 absorption reaction Methods 0.000 claims description 3
- 239000008187 granular material Substances 0.000 claims description 2
- 239000000654 additive Substances 0.000 claims 1
- 238000004040 coloring Methods 0.000 claims 1
- 238000004519 manufacturing process Methods 0.000 claims 1
- 230000004913 activation Effects 0.000 description 8
- 239000011149 active material Substances 0.000 description 2
- 239000013543 active substance Substances 0.000 description 2
- 230000007613 environmental effect Effects 0.000 description 2
- 239000002360 explosive Substances 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000001939 inductive effect Effects 0.000 description 1
- 239000004922 lacquer Substances 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B4/00—Fireworks, i.e. pyrotechnic devices for amusement, display, illumination or signal purposes
- F42B4/26—Flares; Torches
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41J—TARGETS; TARGET RANGES; BULLET CATCHERS
- F41J2/00—Reflecting targets, e.g. radar-reflector targets; Active targets transmitting electromagnetic or acoustic waves
- F41J2/02—Active targets transmitting infrared radiation
-
- 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
- F42B12/44—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 incendiary type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B4/00—Fireworks, i.e. pyrotechnic devices for amusement, display, illumination or signal purposes
- F42B4/30—Manufacture
-
- 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
- F42B5/145—Cartridges, i.e. cases with charge and missile for dispensing gases, vapours, powders, particles or chemically-reactive substances
- F42B5/15—Cartridges, i.e. cases with charge and missile for dispensing gases, vapours, powders, particles or chemically-reactive substances for creating a screening or decoy effect, e.g. using radar chaff or infrared material
Definitions
- the invention relates to an active body or effective masses consisting of a plurality of successively arranged or stacked flares for generating decoupling targets.
- Such an active body is briefly described for example in DE 199 51 767 C2 and thereby fulfills the object of a dual-mode decoy.
- the active substance emitting radiation in the IR range is formed here from flares.
- a camouflage and deception ammunition of this type for the protection of objects against guided missiles containing the active substances forming fog and / or dummy targets is furthermore dealt with in DE 10 2005 020 159 B4.
- Red phosphorus has been part of military applications for decades, such as nukes for the protection of infantry, artillery and naval vehicles, or aircraft (IR) -effecting aircraft targets.
- the fog or IR effect unfolds the RP after appropriate ignition by activation by means of burn off.
- the ignition and distribution of the RP unit takes place in turn classically via an igniting or disintegrating charge, which ensures that the active body or active mass is optimally ignited and distributed for the respective purpose, i. that an optimal blossoming of the IR decoy target to a cloud or a surface area target takes place.
- Such a new ignition concept is described in more detail in DE 10 2006 004 912 A1. It is a system known to protect, in particular, large flying platforms, such as aircraft, from IR or radar-directed threats.
- the activation or ignition of the active body preferably takes place without contact. Ejecting the Active body is then performed pneumatically or mechanically.
- the active bodies themselves are ammunition-free packages which are ignited by means of hot air or a laser.
- the invention has the object to further develop an active body of the type described in such a way that a reliable mode of action of the active body or its active masses is ensured to form a decoy target.
- the invention is based on the idea to build up the ammunition-free IR decoy concept on NC (nitrocellulose) and / or RP (red phosphorus) basis and thereby to vary the proportions of NC / RP, wherein the variation between the extrema 0% and 100% can lie.
- NC nitrocellulose
- RP red phosphorus
- the essential parameterization possibilities that are offered by this approach are spontaneity and duration of the IR characteristic, which are reflected in the rising edge and the beam duration, so that the invention enables the parameterization of the beam characteristic of the IR dummy target by the variable components of NC or RP offers.
- the geometric or spatial distribution can be a desired IR curve of the apparent target between the two extrema (100% NC / 0% RP or 100% RP / 0% NC) even infinitely adjustable.
- the NC active materials can in turn be brought under ambient pressure (normal atmosphere) to the reaction, they therefore need no additional activation energy.
- the active compounds are held in shape by a film wrapping or the like.
- a residue combustible active body shell / active body container now better protection against environmental influences during storage, transport and handling is achieved.
- This combustible shell is preferably based on NC. The combustibility ensures that no remains of the remains are left over.
- a kind of ignition transfer layer is incorporated, which serves to optimize the ignition transfer between the active body shell and the active masses.
- Non-pyrophoric and non-pyrophoric IR decoy target based on NC and / or RP, which can be activated by alternative ignition concepts such. Laser, High temperature, inductive etc.
- the stacked Einzelflares decay after activation independently.
- Fig. 1 shows schematically an active body of Einzelflares
- FIG. 3 shows the active body of Fig. 2 with shell
- FIG. 4 shows the active body of FIG. 2 with integrated intermediate layer, FIG.
- Fig. 5 shows the active body of Fig. 3 with predetermined breaking points in the shell.
- FIG. 1 shows a schematic illustration of an active body 1 consisting of so-called individual flares 10.
- FIG. 2 shows active masses 5 of an active body marked 1, which is constructed from stacked flares 2, 3.
- the flares 2, 3 are in this case, for example, or preferably punched NC or RP flare disks, which however do not necessarily have to be circular. Other surface geometries are also possible.
- the flares 2, 3 are put together in variable proportions. The respective proportions can be varied from 0% to 100%. As a result, the IR beam characteristic of the active body 1 can be controlled.
- the stacking of the flares 2, 3 can take place alternately, but need not. As a stacking sequence would be a flare 2, then a flare 3 always alternately or two flare 2 and then only a flare 3, etc. (not shown in detail) adjustable.
- the so-stacked Einzelflarerionn 2, 3 are now introduced into a container or a shell 4.
- This is preferably made of NC material, for.
- NC paper NC lacquer, and protects the actual active mass 5 (Einzelflares 2, 3) in particular from environmental influences.
- the choice of material allows the complete burning of the container 4, which is also lit upon activation of the active body 1.
- the activation of the active body 1 takes place, for example, laser-based, thermal, etc. with the aid of a so-called ejection tube or the like, such as in one of - A -
- the active mass can be blackened, which ensures a higher energy input to the active mass by scattering the degree of absorption (eg., Laser absorption). Also possible is an addition of aggregates.
- an intermediate layer 6 can be incorporated between the container 4 and the active mass 5 (FIG. 3). By this load then control the ignition, for example bescheunigen.
- the intermediate layer 6 should consist of NC and / or RP granules.
- Additional predetermined breaking points 7 in the container 4 likewise serve for the optimal decomposition of the active body 1 to form a decoy target after activation / application and serve to optimize the blooming behavior of the decoy target.
- Such predetermined breaking points are already known by so-called explosive projectiles.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Manufacturing & Machinery (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Lasers (AREA)
- Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
- Investigating Or Analysing Materials By Optical Means (AREA)
- Packages (AREA)
- Refuge Islands, Traffic Blockers, Or Guard Fence (AREA)
Abstract
L'invention concerne un corps actif (1) comportant plusieurs fusées éclairantes (2, 3) disposées les unes derrière les autres ou empilées, servant de masse active, notamment pour la constitution de cibles fictives, les fusées éclairantes (2, 3) étant des fusées individuelles NC (nitrocellulose) ou RP (phosphore rouge). Les fusées individuelles (2, 3) sont empilées de façon régulière ou irrégulière dans leur séquence de telle manière qu'une fusée individuelle RP (3) vient se loger sur la fusée individuelle NC (2), ou plusieurs fusées individuelles NC (2) ou plusieurs fusées individuelles RP (3) se suivent, les quantités de NC et RP dans le corps actif (1) pouvant varier de 0 à 100 %. Un contenant (4) présentant des zones de rupture (7) reçoit la masse active (5).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102009030869A DE102009030869A1 (de) | 2009-06-26 | 2009-06-26 | Wirkkörper |
PCT/EP2010/003567 WO2010149290A1 (fr) | 2009-06-26 | 2010-06-15 | Corps actif |
Publications (1)
Publication Number | Publication Date |
---|---|
EP2446219A1 true EP2446219A1 (fr) | 2012-05-02 |
Family
ID=42668161
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP10723951A Withdrawn EP2446219A1 (fr) | 2009-06-26 | 2010-06-15 | Corps actif |
Country Status (12)
Country | Link |
---|---|
US (1) | US8763533B2 (fr) |
EP (1) | EP2446219A1 (fr) |
KR (1) | KR20120039529A (fr) |
AU (1) | AU2010265108B2 (fr) |
CA (1) | CA2764521A1 (fr) |
DE (1) | DE102009030869A1 (fr) |
IL (1) | IL216906A0 (fr) |
NZ (1) | NZ596612A (fr) |
RU (1) | RU2522200C2 (fr) |
UA (1) | UA91373U (fr) |
WO (1) | WO2010149290A1 (fr) |
ZA (1) | ZA201107924B (fr) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2010093292A1 (fr) * | 2009-02-11 | 2010-08-19 | Saab Ab | Paquet de matériel-leurre, distributeur et procédé de distribution de matériel-leurre |
DE102010013110A1 (de) * | 2010-03-26 | 2011-09-29 | Rheinmetall Waffe Munition Gmbh | Gekapselter Wirkkörper für ein IR-Täusch- bzw. Scheinziel |
DE102013010266A1 (de) | 2013-06-18 | 2014-12-18 | Diehl Bgt Defence Gmbh & Co. Kg | Scheinzielwirkkörper mit einer pyrotechnischen Wirkmasse |
DE102014001866B3 (de) * | 2014-02-06 | 2015-07-02 | Martin Rybol | Aus der Kartusche eines Infrarot-Täuschkörpers ausstoßbarer Wirkkörper |
DE102014012657B4 (de) | 2014-08-22 | 2019-12-19 | Diehl Defence Gmbh & Co. Kg | Wirkkörper mit einer Wirkmasse und einer Umhüllung |
US10267606B2 (en) * | 2017-08-24 | 2019-04-23 | Dmd Systems, Llc | Debris-free combustible aerial shell |
US10962337B2 (en) * | 2019-09-03 | 2021-03-30 | Imi Systems Ltd. | Cartridge for providing delayed chaff for use as a decoy for RF radars |
Family Cites Families (58)
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FR613870A (fr) | 1925-04-06 | 1926-12-01 | Anciens Ets Skoda | Bombe d'avion incendiaire combinée |
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DE3238455C2 (de) * | 1982-10-16 | 1987-03-05 | Pyrotechnische Fabrik F. Feistel GmbH + Co KG, 6719 Göllheim | Nebelwurfkörper |
DE3515166A1 (de) * | 1985-04-26 | 1986-10-30 | Buck Chemisch-Technische Werke GmbH & Co, 7347 Bad Überkingen | Wurfkoerper zur darstellung eines infrarot-flaechenstrahlers |
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DE3835887C2 (de) * | 1988-10-21 | 1997-10-02 | Rheinmetall Ind Ag | Patrone zur Scheinzielerzeugung |
DE4327976C1 (de) | 1993-08-19 | 1995-01-05 | Buck Chem Tech Werke | Flaremasse zur Scheinzielerzeugung |
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CA2546252A1 (fr) | 2005-03-08 | 2006-09-08 | Eugen Nicolae | Distributeur de fusees eclairantes |
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DE102005020159B4 (de) | 2005-04-29 | 2007-10-04 | Rheinmetall Waffe Munition Gmbh | Tarn- und Täuschmunition zum Schutz von Objekten gegen Lenkflugkörper |
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DE102007032112A1 (de) | 2007-07-09 | 2009-01-15 | Rheinmetall Waffe Munition Gmbh | Verfahren und Abschussvorrichtung zum Schutz eines Objektes vor einer Bedrohung, insbesondere einem Flugkörper, sowie Munition |
DE102009020558A1 (de) * | 2009-05-08 | 2010-11-18 | Rheinmetall Waffe Munition Gmbh | Aktivierungseinheit für munitionsfreie Scheinziele |
DE102008064638A1 (de) | 2008-06-16 | 2009-12-17 | Rheinmetall Waffe Munition Gmbh | Flare mit Flareanzündung sowie Ausstoßsystem dafür |
EP3173808B8 (fr) | 2009-03-02 | 2019-08-14 | Diversey, Inc. | Système et procédé de gestion et de contrôle de l'hygiène |
FR2942917B1 (fr) | 2009-03-05 | 2011-04-08 | Valeo Etudes Electroniques | Module electrique d'un vehicule automobile et dispositif electrique correspondant |
WO2010127762A1 (fr) | 2009-05-08 | 2010-11-11 | Rheinmetall Waffe Munition Gmbh | Unité d'activation pour masses actives ou corps actifs |
DE102009030870A1 (de) | 2009-06-26 | 2010-12-30 | Rheinmetall Waffe Munition Gmbh | Wirkkörper |
DE102009030868B4 (de) | 2009-06-26 | 2014-01-16 | Rheinmetall Waffe Munition Gmbh | Anzünd- bzw. Aktivierungseinheit zum Anzünden von Rot-Phosphor-Flares mittels Laser |
-
2009
- 2009-06-26 DE DE102009030869A patent/DE102009030869A1/de not_active Withdrawn
-
2010
- 2010-06-15 RU RU2012102521/11A patent/RU2522200C2/ru not_active IP Right Cessation
- 2010-06-15 NZ NZ596612A patent/NZ596612A/en not_active IP Right Cessation
- 2010-06-15 EP EP10723951A patent/EP2446219A1/fr not_active Withdrawn
- 2010-06-15 CA CA2764521A patent/CA2764521A1/fr not_active Abandoned
- 2010-06-15 KR KR1020117028720A patent/KR20120039529A/ko not_active Application Discontinuation
- 2010-06-15 AU AU2010265108A patent/AU2010265108B2/en not_active Ceased
- 2010-06-15 UA UAA201112666U patent/UA91373U/uk unknown
- 2010-06-15 WO PCT/EP2010/003567 patent/WO2010149290A1/fr active Application Filing
-
2011
- 2011-10-28 ZA ZA2011/07924A patent/ZA201107924B/en unknown
- 2011-12-11 IL IL216906A patent/IL216906A0/en unknown
- 2011-12-27 US US13/337,692 patent/US8763533B2/en not_active Expired - Fee Related
Non-Patent Citations (1)
Title |
---|
See references of WO2010149290A1 * |
Also Published As
Publication number | Publication date |
---|---|
CA2764521A1 (fr) | 2010-12-29 |
US20120174812A1 (en) | 2012-07-12 |
IL216906A0 (en) | 2012-02-29 |
AU2010265108B2 (en) | 2015-04-02 |
DE102009030869A1 (de) | 2011-02-10 |
WO2010149290A1 (fr) | 2010-12-29 |
ZA201107924B (en) | 2012-06-27 |
UA91373U (uk) | 2014-07-10 |
RU2522200C2 (ru) | 2014-07-10 |
KR20120039529A (ko) | 2012-04-25 |
US8763533B2 (en) | 2014-07-01 |
AU2010265108A1 (en) | 2011-12-15 |
NZ596612A (en) | 2014-03-28 |
RU2012102521A (ru) | 2013-08-10 |
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