EP1794537B1 - Corps actif - Google Patents
Corps actif Download PDFInfo
- Publication number
- EP1794537B1 EP1794537B1 EP05768690A EP05768690A EP1794537B1 EP 1794537 B1 EP1794537 B1 EP 1794537B1 EP 05768690 A EP05768690 A EP 05768690A EP 05768690 A EP05768690 A EP 05768690A EP 1794537 B1 EP1794537 B1 EP 1794537B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- active
- body according
- active compound
- active body
- pyrotechnic
- 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
- 239000000463 material Substances 0.000 claims abstract description 12
- 239000000126 substance Substances 0.000 claims abstract description 12
- 239000000203 mixture Substances 0.000 claims abstract description 9
- 239000000020 Nitrocellulose Substances 0.000 claims abstract description 4
- 229920001220 nitrocellulos Polymers 0.000 claims abstract description 4
- SNIOPGDIGTZGOP-UHFFFAOYSA-N Nitroglycerin Chemical compound [O-][N+](=O)OCC(O[N+]([O-])=O)CO[N+]([O-])=O SNIOPGDIGTZGOP-UHFFFAOYSA-N 0.000 claims abstract description 3
- LYAGTVMJGHTIDH-UHFFFAOYSA-N diethylene glycol dinitrate Chemical compound [O-][N+](=O)OCCOCCO[N+]([O-])=O LYAGTVMJGHTIDH-UHFFFAOYSA-N 0.000 claims abstract description 3
- 229960003711 glyceryl trinitrate Drugs 0.000 claims abstract description 3
- 230000005855 radiation Effects 0.000 claims description 9
- FGIUAXJPYTZDNR-UHFFFAOYSA-N potassium nitrate Chemical compound [K+].[O-][N+]([O-])=O FGIUAXJPYTZDNR-UHFFFAOYSA-N 0.000 claims description 8
- 239000000843 powder Substances 0.000 claims description 5
- 230000001681 protective effect Effects 0.000 claims description 5
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims description 4
- 235000010333 potassium nitrate Nutrition 0.000 claims description 4
- 239000004323 potassium nitrate Substances 0.000 claims description 4
- 229910052796 boron Inorganic materials 0.000 claims description 3
- 239000013543 active substance Substances 0.000 claims description 2
- 239000008187 granular material Substances 0.000 claims description 2
- 238000004519 manufacturing process Methods 0.000 claims description 2
- 150000001875 compounds Chemical class 0.000 claims 12
- 238000010304 firing Methods 0.000 claims 3
- 239000000006 Nitroglycerin Substances 0.000 abstract description 2
- 239000002360 explosive Substances 0.000 abstract 4
- 239000007789 gas Substances 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 239000011888 foil Substances 0.000 description 3
- 229910021536 Zeolite Inorganic materials 0.000 description 2
- HNPSIPDUKPIQMN-UHFFFAOYSA-N dioxosilane;oxo(oxoalumanyloxy)alumane Chemical compound O=[Si]=O.O=[Al]O[Al]=O HNPSIPDUKPIQMN-UHFFFAOYSA-N 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 229910052744 lithium Inorganic materials 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 238000005457 optimization Methods 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 230000003595 spectral effect Effects 0.000 description 2
- 239000010457 zeolite Substances 0.000 description 2
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 239000011230 binding agent Substances 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 238000006731 degradation reaction Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- 239000003999 initiator Substances 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 239000011872 intimate mixture Substances 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000008188 pellet Substances 0.000 description 1
- 239000004810 polytetrafluoroethylene Substances 0.000 description 1
- 229920001343 polytetrafluoroethylene Polymers 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000002269 spontaneous effect Effects 0.000 description 1
- 230000002123 temporal effect Effects 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
- F42B5/16—Cartridges, i.e. cases with charge and missile characterised by composition or physical dimensions or form of propellant charge, with or without projectile, or powder
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B45/00—Compositions or products which are defined by structure or arrangement of component of product
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06C—DETONATING OR PRIMING DEVICES; FUSES; CHEMICAL LIGHTERS; PYROPHORIC COMPOSITIONS
- C06C15/00—Pyrophoric compositions; Flints
-
- 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
Definitions
- the invention relates to an active body according to the preamble of patent claim 1.
- Active bodies for the protection of military objects, such as aircraft from infrared guided missiles, are well known. In the simplest case, these are pyrotechnically generated heat sources that emit hot radiation.
- An infrared decoy is in the DE 40 07 811 C2 disclosed. This has a spectral distribution of the IR radiation of only very moderately warm targets.
- the fake target zeolite powder is used, which is suitable for absorbing humidity. It can be used as a coating of a body or as a finely divided cloud of powder particles floating in the air. In principle, all zeolite types or powders with zeolite-like crystal structures are suitable.
- Another infrared decoy is also from the JP-A - 20011741 96 known.
- An infrared emitter from incendiary sets describes the DE 26 14 196 A1 , This is in direct contact with a metal foil.
- the fire charge consists in one embodiment of an intimate mixture of potassium nitrate and metallic boron. The fire rate is applied with the aid of a nitrocellulose binder on a metal foil.
- the DE 42 44 682 A1 is a high - intensity infrared pyrotechnic deception torch disclosed. This serves to deflect a projectile which is approaching an aircraft.
- the deceptor flare has a range of compact bubble-free pressed separate pieces of gas-releasing high-intensity infrared-emitting pyrotechnic compositions contained in a rupturable airtight container.
- An infrared decoy for a helicopter also describes the GB 2 327 116 A , From the US 5,343,794 is another infrared decoy known. Possible material compositions Such rogue targets can the US 6,675,719 as well as the US 5,435,224 as well as the US 5,343,794 be removed. Pyrotechnic fog sets are in the WO 00158237 A1 and the WO 00/58238 described.
- Another method for providing a dummy target body is the DE 42 38 038 C1 removable. This is distinguished by the fact that the active masses simulating the dummy target body are brought into the position of the dummy target body to be generated in such a way and decomposed there that a spectral-spatial target signature of the object is generated for a homing head.
- the EP 0 665 415 A (Starting point for claim 1) relates to an igniter, but in particular a method for producing the same. Compared to the prior art, the method is characterized in that the integrated grooves are not milled but are already created when solidifying the compact. To meet the fire requirements, the ten grooves in total have the same surface area as the eight prior art grooves. The position, shape and depth of the groove allows the optimization of the erosion surface shape and thus the optimization of the energy application of the torch compact. The flare pellets are themselves coated with a primer mixture.
- the GB 2 266 944 A describes a torch assembly with pyrotechnic feedstock.
- the housing has a chamber with a trigger, which can be electrical or mechanical. Adjoining this is another chamber with an initiator in the form of a detonator and black powder. However, the larger part takes the pyrotechnic device or feedstock.
- the pyrotechnic feed comprises, in one embodiment, a solid block of lithium metal having a number of cylindrical openings such that the longitudinal axis is aligned parallel to the length of the housing. Each opening is filled with a rod of PTFE.
- the feedstock is a tortuous aperture containing lithium in granular form, the housing being made of aluminum.
- the object of the invention is to provide an active body which has a specific blooming method against modern missiles as an effective IR decoy target, for example for aircraft, an object-like spectral radiation signature with high radiation fraction in the area of plum radiation with the onset of ignition over the entire duration of action with steep Anstlegsflanken and a sufficiently long Wirkzelt fulfilled. Furthermore, the efficacy should also be given at high altitudes with low oxygen and no performance degradation at high ejection speeds (due to flow effects).
- the invention is based on the idea to provide an active body with at least one effective mass block of mono- or polybasic high-energy materials on the surface as well as in the interior with structures. Depending on the pattern (structure) and depth, this requires an enlargement of the surface, as a result of which the burning rate of the active mass block and thus the duration of action of the active body can be controlled.
- the active mass block preferably has one or more channels / cavities in the interior, which allows an inflow-protected initiation of the active mass block in the interior.
- the active mass block In combination with, for example, metallic cover plates and protective foils, it is thus ensured that losses of the IR radiation at high flow velocities, such as occur when the active body (effective mass block) is ejected from the aircraft, are avoided.
- the specific blooming behavior is preferably set by filling the channels with, for example, finely structured material of the same substance but with respect to the active mass block significantly increased surface / mass ratio.
- the steepness of the rising edge can be increased with increasing surface / mass ratio.
- the igniting of the active compositions is carried out in a preferred embodiment within the channels in the active mass block by preferably pyrotechnic ignition charges.
- a spontaneous, flow-dependent ignition is ensured and on the other hand, a radiation originating from the ignition charge is suppressed.
- a active mass block having on its surface 2 structures, for example in the form of grooves.
- the active mass block 1 has inside one or more channels / cavities 3 and filled therein effective mass substances 4.
- This Substance can be a finely structured material of the same substance but compared to the active mass block 1 significantly increased surface / mass ratio.
- a finely structured material are materials with a high radiation content in the wavelength range preferably between 4.1 to 4, 6 microns, for example, a Nitrocellulosengemenge with about 60% nitroglycerin and 40% diethylene glycol dinitrate.
- the active mass block 1 further comprises a flow protection 5, which is formed here from a cover or protective cap 5a and a protective film 5b. With 6 gas and temperature bridges are characterized, which are formed by slots, perforations or holes.
- a pyrotechnic ignition charge 7 is provided, which is preferably formed by powdered boron / potassium nitrate (proportions about 50% boron / 50% potassium nitrate). This primer 7 can be used in a particle size of about 0.2 to 3 mm.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Organic Chemistry (AREA)
- General Engineering & Computer Science (AREA)
- Crystallography & Structural Chemistry (AREA)
- Metallurgy (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Air Bags (AREA)
Abstract
Claims (12)
- Corps pyrotechnique actif pour formation d'une cible apparente, constituée d'au moins un bloc pyrotechnique (1) de masse active dont la surface (2) est dotée de structures spécifiques et présentant à l'intérieur des matériaux (4) finement structurés, en substances de la masse active du bloc (1) de masse active et amorcées par des jeux d'amorce (7),- les structures prévues à la surface (2) étant des rainures ou une rugosité qui ont pour effet une augmentation de la surface (2) en fonction de leur motif et de leur profondeur et- les structures prévues à l'intérieur étant formées par des canaux (3) et/ou des cavités (3), le bloc (1) de masse active possédant à l'intérieur des ponts à gaz et/ou de température entre les canaux (3) et/ou les cavités (3) qui sont formés par des fentes, des perforations et/ou des alésages.
- Corps actif selon la revendication 1, caractérisé en ce qu'à l'intérieur, des matériaux finement structurés en substances de la masse active sont placés dans les structures et présentent un rapport surface/masse nettement plus élevé que le bloc (1) de masse active.
- Corps actif selon les revendications 1 ou 2, caractérisé en ce que le bloc (1) de masse active et les substances (4) de la masse active présentent une proportion élevée de rayonnement dans la plage de longueur d'onde comprise entre 4,1 et 4,6 µm.
- Corps actif selon l'une des revendications 1 ou 2, caractérisé en ce que le bloc (1) de masse active et les substances (4) de la masse active sont constitués de matériaux à haute énergie à base unique ou multiple.
- Corps actif selon la revendication 4, caractérisé en ce qu'il utilise un mélange de nitrocelluloses.
- Corps actif selon la revendication 5, caractérisé en ce que le mélange de nitrocelluloses est constitué de 60 % de nitroglycérine et de 40 % de dinitrate de diéthylèneglycol.
- Corps actif selon l'une des revendications 1 à 6, caractérisé en ce que le bloc (1) de masse active présente une protection anti-souffle (5).
- Corps actif selon la revendication 7, caractérisé en ce que la protection anti-souffle (5) est formée d'un capot de protection (5a) et d'une feuille de protection (5b).
- Corps actif selon l'une des revendications 1 à 8, caractérisé en ce que les substances (4) de la masse active utilisées sont configurées en barres, en flocons, en plaquettes ou en granulés.
- Corps actif selon la revendication 9, caractérisé en ce que les barres ont un diamètre d'environ 0,2 à 1,5 mm.
- Corps actif selon l'une des revendications 1 à 10 qui précèdent, caractérisé en ce que l'allumage des substances (4) de la masse active s'effectue à l'intérieur de la structure interne par les amorces pyrotechniques (7).
- Corps actif selon la revendication 11, caractérisé en ce que les amorces pyrotechniques (7) sont constituées de nitrate de bore et de nitrate de potassium pulvérulents dans un rapport de mélange de 50 % pour l'un et pour l'autre, en grains d'une taille comprise entre 0,2 et 3 mm.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102004047231A DE102004047231B4 (de) | 2004-09-28 | 2004-09-28 | Wirkkörper |
PCT/EP2005/008167 WO2006034746A1 (fr) | 2004-09-28 | 2005-07-28 | Corps actif |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1794537A1 EP1794537A1 (fr) | 2007-06-13 |
EP1794537B1 true EP1794537B1 (fr) | 2012-02-29 |
Family
ID=35106944
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP05768690A Active EP1794537B1 (fr) | 2004-09-28 | 2005-07-28 | Corps actif |
Country Status (4)
Country | Link |
---|---|
US (1) | US8783183B2 (fr) |
EP (1) | EP1794537B1 (fr) |
DE (1) | DE102004047231B4 (fr) |
WO (1) | WO2006034746A1 (fr) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102007040529B4 (de) | 2007-08-28 | 2013-08-01 | Diehl Bgt Defence Gmbh & Co. Kg | Suchkopf |
DE102008017725A1 (de) | 2008-04-07 | 2009-10-08 | Rheinmetall Waffe Munition Gmbh | Scheinziel mit einfacher Sicherheitsvorrichtung |
DE102008017722A1 (de) * | 2008-04-07 | 2009-10-08 | Rheinmetall Waffe Munition Gmbh | Wirkmassenbehälter |
DE102010024848A1 (de) | 2010-06-23 | 2011-12-29 | Rheinmetall Waffe Munition Gmbh | Wurfkörper |
DE102013010266A1 (de) | 2013-06-18 | 2014-12-18 | Diehl Bgt Defence Gmbh & Co. Kg | Scheinzielwirkkörper mit einer pyrotechnischen Wirkmasse |
DE102013108822C5 (de) * | 2013-08-14 | 2017-08-10 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Waffe und Wurfkörper mit RFID-System |
DE102014012657B4 (de) | 2014-08-22 | 2019-12-19 | Diehl Defence Gmbh & Co. Kg | Wirkkörper mit einer Wirkmasse und einer Umhüllung |
DE202014006882U1 (de) | 2014-08-22 | 2014-09-18 | Diehl Bgt Defence Gmbh & Co. Kg | Wirkkörper mit einer Wirkmasse und einer Umhüllung |
DE202015003966U1 (de) | 2015-06-08 | 2015-07-24 | Rheinmetall Waffe Munition Gmbh | Nebelmunition |
DE102019126466A1 (de) | 2019-10-01 | 2021-04-01 | Rheinmetall Waffe Munition Gmbh | Wirkkörper und Verfahren zum Zünden eines Wirkkörpers |
Family Cites Families (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US617738A (en) * | 1899-01-17 | Variable-speed frictional gearing | ||
US2210871A (en) * | 1938-11-23 | 1940-08-06 | Hercules Powder Co Ltd | Process for the manufacture of smokeless powder |
US3938444A (en) * | 1974-07-05 | 1976-02-17 | The United States Of America As Represented By The Secretary Of The Navy | Flare cartridge |
DE2614196A1 (de) * | 1976-04-02 | 1977-10-13 | Dynamit Nobel Ag | Infrarotstrahler |
US5435224A (en) * | 1979-04-04 | 1995-07-25 | The United States Of America As Represented By The Secretary Of The Navy | Infrared decoy |
US6675716B1 (en) * | 1980-08-25 | 2004-01-13 | The United States Of America As Represented By The Secretary Of The Navy | Pyrotechnic pellet decoy method |
DE3402546A1 (de) * | 1984-01-26 | 1985-08-01 | Pyro-Chemie Hermann Weber & Co GmbH, 5208 Eitorf | Pyrotechnischer satz zur erzeugung von lichtblitzen |
US5074216A (en) * | 1987-09-03 | 1991-12-24 | Loral Corporation | Infrared signature enhancement decoy |
DE4007811C2 (de) * | 1990-03-12 | 1994-05-19 | Dornier Gmbh | Infrarot-Scheinziel |
GB9120801D0 (en) * | 1991-10-01 | 1995-03-08 | Secr Defence | Propelled pyrotechnic decoy flare |
GB9120803D0 (en) * | 1991-10-01 | 1995-03-08 | Secr Defence | Pyrotechnic decoy flare |
GB2266944B (en) | 1992-05-12 | 1995-08-02 | Marconi Gec Ltd | Flare arrangements |
DE4238038C1 (de) | 1992-11-11 | 1994-06-16 | Buck Chem Tech Werke | Verfahren zum Bereitstellen eines Scheinzielkörpers |
GB2300035B (en) * | 1993-07-29 | 1997-09-24 | Lacroix Soc E | An infrared decoy cartridge, and decoy apparatus including such a cartridge |
DE4327976C1 (de) * | 1993-08-19 | 1995-01-05 | Buck Chem Tech Werke | Flaremasse zur Scheinzielerzeugung |
US5487851A (en) * | 1993-12-20 | 1996-01-30 | Thiokol Corporation | Composite gun propellant processing technique |
US5456455A (en) * | 1994-02-01 | 1995-10-10 | Thiokol Corporation | Flare pellet and process for making same |
DE19605337C2 (de) * | 1996-02-14 | 1998-12-03 | Daimler Benz Aerospace Ag | Verfahren zur Veränderung der Infrarot-Signatur eines Flugzeuges |
IL121276A (en) * | 1997-07-10 | 2000-01-31 | Israel Military Ind | Decoy flare |
US6427599B1 (en) * | 1997-08-29 | 2002-08-06 | Bae Systems Integrated Defense Solutions Inc. | Pyrotechnic compositions and uses therefore |
DE19914095A1 (de) * | 1999-03-27 | 2000-09-28 | Piepenbrock Pyrotechnik Gmbh | Pyrotechnischer Nebelsatz zur Erzeugung eines im sichtbaren, infraroten und im Millimeterwellen-Bereich undurchdringlichen Aerosols |
DE19914097A1 (de) * | 1999-03-27 | 2000-09-28 | Piepenbrock Pyrotechnik Gmbh | Pyrotechnische Wirkmasse zur Erzeugung eines im Infraroten stark emissiven und im Visuellen undurchdringlichen Aerosols |
JP4276348B2 (ja) * | 1999-12-16 | 2009-06-10 | 日本工機株式会社 | 赤外線デコイフレア飛しょう体 |
-
2004
- 2004-09-28 DE DE102004047231A patent/DE102004047231B4/de not_active Expired - Fee Related
-
2005
- 2005-07-28 WO PCT/EP2005/008167 patent/WO2006034746A1/fr active Application Filing
- 2005-07-28 EP EP05768690A patent/EP1794537B1/fr active Active
-
2007
- 2007-03-28 US US11/727,869 patent/US8783183B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
DE102004047231A1 (de) | 2006-04-06 |
WO2006034746A1 (fr) | 2006-04-06 |
DE102004047231B4 (de) | 2008-08-21 |
US20070266882A1 (en) | 2007-11-22 |
US8783183B2 (en) | 2014-07-22 |
EP1794537A1 (fr) | 2007-06-13 |
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