EP1514072A1 - Nebelwurfkörper - Google Patents
NebelwurfkörperInfo
- Publication number
- EP1514072A1 EP1514072A1 EP03759933A EP03759933A EP1514072A1 EP 1514072 A1 EP1514072 A1 EP 1514072A1 EP 03759933 A EP03759933 A EP 03759933A EP 03759933 A EP03759933 A EP 03759933A EP 1514072 A1 EP1514072 A1 EP 1514072A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- charge
- projectile according
- hollow cylinder
- mist
- stack
- 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
Links
- 239000000779 smoke Substances 0.000 title claims abstract description 12
- 239000003595 mist Substances 0.000 claims description 15
- 239000000443 aerosol Substances 0.000 claims description 8
- 230000000007 visual effect Effects 0.000 claims description 6
- 238000004804 winding Methods 0.000 claims description 3
- 239000002657 fibrous material Substances 0.000 claims description 2
- 239000012188 paraffin wax Substances 0.000 claims description 2
- 230000005855 radiation Effects 0.000 abstract description 6
- 238000005562 fading Methods 0.000 abstract description 3
- 239000007787 solid Substances 0.000 abstract description 3
- 239000011248 coating agent Substances 0.000 abstract 1
- 238000000576 coating method Methods 0.000 abstract 1
- 229910001963 alkali metal nitrate Inorganic materials 0.000 description 4
- 239000011230 binding agent Substances 0.000 description 3
- 239000000470 constituent Substances 0.000 description 3
- 229910052751 metal Inorganic materials 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 238000001514 detection method Methods 0.000 description 2
- 229910052752 metalloid Inorganic materials 0.000 description 2
- 150000002738 metalloids Chemical class 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 229910052723 transition metal Inorganic materials 0.000 description 2
- 150000003624 transition metals Chemical class 0.000 description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- -1 CuO Chemical class 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- 241000475481 Nebula Species 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- 239000013543 active substance Substances 0.000 description 1
- 229910045601 alloy Inorganic materials 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
- 229910052796 boron Inorganic materials 0.000 description 1
- 238000005253 cladding Methods 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 229910000765 intermetallic Inorganic materials 0.000 description 1
- 230000005923 long-lasting effect Effects 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 150000003623 transition metal compounds Chemical class 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
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
- F42B12/56—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
- F42B12/70—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 for dispensing radar chaff or infrared material
-
- 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
- F42B12/46—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 gases, vapours, powders or chemically-reactive substances
- F42B12/48—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 gases, vapours, powders or chemically-reactive substances smoke-producing, e.g. infrared clouds
Definitions
- the invention relates to a smoke impact body with an active charge made of a pyrotechnic active mass for producing an aerosol that emits in the infrared and is impenetrable in the visual.
- Armored and unarmored vehicles are protected against detection, detection and target tracking using aerosol curtains and thus against the threat of missiles.
- DE 199 14 097 AI describes a suitable pyro-technical active substance for producing an aerosol which is highly emissive in the infrared and impenetrable in the visual.
- This active mass develops a camouflage mist that, in addition to being impenetrable in the visible range, also enables long-lasting coverage in the infrared range.
- the main constituents of this active mass are red phosphorus, an alkali metal nitrate or a mixture of Alkali metal nitrates and as secondary components at least one transition metal or a metallic compound or alloy thereof, at least one metalloid and a binder.
- threatening missiles fly at speeds of 200 to 600 m / s, they must be misted very quickly after they are detected.
- Known throwing bodies only develop their effect after a flight time and a time delay of, for example, 2 s. The vehicle is unprotected during this time.
- DE 29 08 217 C2 describes a unit charge for fogging vehicles, which has a sleeve filled with fog bodies.
- the mist bodies have the shape of cylindrical flat discs lying on top of one another with an open center hole.
- the mist bodies are ejected from the sleeve without being covered. A cross-fading of the line of sight in the infrared range is not provided.
- the object of the invention is to propose a simply constructed throwing body which is designed in such a way that when ejecting i ⁇ a solid angle there is a rapid cross-fading of the line of sight in the infrared radiation range and in the visual radiation range.
- the winding charge stack consisting of the hollow cylinder segments is held by the sheath and ejected from a launcher tube, which ensures aerodynamic stability in the initial phase of the flight. This prevents the stack from unfolding directly on the vehicle. Only after a few meters of flight, for example 5 m to 10 m, do the ignited hollow cylinder segments break up the envelope. Due to the lack of aerodynamic cladding, the incoming air reaches into the stack of hollow cylinder segments. As a result, the segments are immediately dispersed, which leads to a large-scale fanning out of the burning hollow cylinder segments in a wide solid angle.
- an aerosol mist distribution is created very quickly, for example within 0.25 s, which covers the vehicle both in the infrared radiation range and in the visual radiation range against missiles approaching horizontally and in gliding flight.
- the vehicle has a long period of time available in order to avoid the time of impact of the approaching missile calculated in the vehicle by driving maneuvers.
- FIG. 1 shows a smoke ejection body with several layers of hollow cylinder segments in an envelope
- FIG. 2b shows a side view in the direction of the arrows IIb-IIb in FIG. 2a
- FIG. 3a shows a single hollow cylinder segment in supervision
- FIG. 3b shows a single hollow cylinder segment in a perspective view
- FIG. 4 shows a perforated disk of the casing
- FIG. 5 a film of the wrapping, unwound
- FIG. 6 shows the smoke ejection body in an ejection device
- FIG. 7 shows an aerosol mist generated by the smoke ejection body
- FIG. 8 shows a time diagram of the development of the aerosol mist.
- a smoke ejection body 1 consists of a hollow cylindrical active charge 2, an ignition charge 3 and an envelope 4 (cf. FIG. 1).
- the active charge 2 is a stack of a plurality of layers 5 of hollow cylinder segments 6.
- Each layer 5 is composed of a plurality of hollow cylinder segments 6; there is a cavity 7 in the interior of the active charge stack.
- each layer 5 is formed by four hollow cylinder segments 6, the segment angle a being 90 °, the individual hollow cylinder segments 6 abutting one another.
- the segment angle a can also be smaller than 90 °, in which case there are correspondingly more hollow cylinder segments 6 in one position.
- the diameter d of the cavity 7 is ⁇ 1/6 D, where D is the outer diameter of the active charge stack (cf. FIGS. 1, 2a, 2b).
- the winding charge stack 2 has a height H which is, for example,> 20 h, where h is the height of a hollow cylinder segment (cf. FIGS. 1, 2b, 3b).
- the height h is preferably> 1/15 D.
- the hollow cylinder segments 6 are compressed from a pyrotechnic heat mass, which produce an aerosol which dampens and emits in the infrared radiation range and is impenetrable in the visual field.
- a pyrotechnic heat mass which produce an aerosol which dampens and emits in the infrared radiation range and is impenetrable in the visual field.
- Such an active mass is described in DE 199 14 097 AI. It has red phosphorus, an alkali metal nitrate or a mixture of alkali metal nitrates as the main constituents and at least one transition metal or a metal-rich compound or alloy thereof and at least one metalloid and a binder as secondary constituents.
- the ignition charge 3, which is used to ignite the hollow cylinder segments 6 via the cavity 7 and can serve as an ejection charge, is a pyrotechnic ignition charge which contains 50 to 80 percent by mass of black powder, 0 to 20% of an organic binder,
- a metal powder from the group of metals, magnesium, aluminum, boron, zirconium, titanium and 0 to 20% of a combustion moderator based on a transition metal compound, such as CuO, K [Fe 2 (CN) 6 ], (C 5 H 5 ) 2 Fe).
- the wrapper 4 has a consumable film 8, which consists, for example, of a paper soaked in paraffin.
- the film 8 holds initially the active charge stack 2 consisting of the hollow cylinder segments 6 together.
- the film 8 envelops the Wixkladungs pile 2 on the top and on its circumference U corresponding to the diameter D in the entire height H.
- FIG. 5 shows the film 8 unwound.
- the film 8 is connected to a disc 9 which rests on the underside of the active charge 2.
- the disk 9 consists of a press fiber material and has a central opening 10.
- the diameter dl of the opening 10 is> the diameter d (cf. FIG. 1, FIG. 4).
- the described smoke ejection body can be inserted into a metallic ejector tube 11 (cf. FIG. 6).
- Figure 6 shows the arrangement in an exploded state.
- an electrical ignition element 13 At the bottom 12 of the ejector tube 11 there is an electrical ignition element 13, the electrical contacts 14 of which can be unlocked via a corresponding switching device of the vehicle.
- the ignition element 13 ignites the ignition charge 3 upon initiation, which can also act as an exhaust charge.
- the hollow cylinder segments 6 are ignited and the smoke nozzle 1 is ejected.
- the hollow cylinder segments 6 remain held together by the film 8 in the range between about 5 to 10 m after the start of the gas evolution of the discharge.
- the active charge stack 2 fuses, separating the hollow cylinder segments 6, and the individual hollow cylinder segments 6 develop after a distance S at a distance from the one to be protected Vehicle F has a fog curtain N, which shields the vehicle F from both missiles K1 threatening in gliding flight and missiles K2 attacking in horizontal flight (cf. FIG. 7).
- the protective nebula N is developed, for example, within 0.25 s after the vehicle F has recognized and evaluated the threat posed by the missiles K1 and K2.
- FIG. 8 shows a comparison of known action times and the action time achievable by the projectile according to the invention.
- t4 is the point in time at which the threatening missile strikes after the calculation of the vehicle F.
- the fog development W counteracting the threat is reached along line a at time t3, whereas the level of effectiveness achieved with the device described is already reached in line b at time t2. It shows that the time period between t3 and r4 is significantly shorter than the time period between t2 and t4. This means that between t2 and t4 in the threatened vehicle there is a significantly longer time available for avoiding driving maneuvers than between the prior art, for avoiding driving maneuvers
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
Description
Claims
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10226507A DE10226507A1 (de) | 2002-06-14 | 2002-06-14 | Nebelwurfkörper |
DE10226507 | 2002-06-14 | ||
PCT/EP2003/006147 WO2003106913A1 (de) | 2002-06-14 | 2003-06-12 | Nebelwurfkörper |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1514072A1 true EP1514072A1 (de) | 2005-03-16 |
EP1514072B1 EP1514072B1 (de) | 2005-11-30 |
Family
ID=29594519
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP03759933A Expired - Lifetime EP1514072B1 (de) | 2002-06-14 | 2003-06-12 | Nebelwurfkörper |
Country Status (9)
Country | Link |
---|---|
US (1) | US20060060103A1 (de) |
EP (1) | EP1514072B1 (de) |
AU (1) | AU2003242677B2 (de) |
BR (1) | BR0311793B1 (de) |
DE (2) | DE10226507A1 (de) |
IL (1) | IL165732A (de) |
MY (1) | MY134363A (de) |
WO (1) | WO2003106913A1 (de) |
ZA (1) | ZA200410264B (de) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7640858B1 (en) * | 2004-01-23 | 2010-01-05 | Kilgore Flares Company, Llc | Stacked pellet flare assembly and methods of making and using the same |
DE102006008309B4 (de) * | 2006-02-23 | 2008-03-27 | Diehl Bgt Defence Gmbh & Co. Kg | Nebelwurfkörper |
DE102008028292B4 (de) | 2008-06-13 | 2021-10-14 | Diehl Defence Gmbh & Co. Kg | Nebelwurfkörper |
DE102008033494A1 (de) | 2008-07-16 | 2010-01-21 | Diehl Bgt Defence Gmbh & Co. Kg | Nebeltopf |
DE102010013110A1 (de) * | 2010-03-26 | 2011-09-29 | Rheinmetall Waffe Munition Gmbh | Gekapselter Wirkkörper für ein IR-Täusch- bzw. Scheinziel |
DE102010026641A1 (de) | 2010-07-09 | 2012-01-12 | Diehl Bgt Defence Gmbh & Co. Kg | Nebelwurfkörper |
DE102011009154A1 (de) | 2011-01-22 | 2012-07-26 | Diehl Bgt Defence Gmbh & Co. Kg | Verfahren zur Abwehr einer Bedrohung durch Ausbringen von Tarnnebel und Einrichtung zum Ausüben des Abwehr-Verfahrens |
DE102014012657B4 (de) * | 2014-08-22 | 2019-12-19 | Diehl Defence Gmbh & Co. Kg | Wirkkörper mit einer Wirkmasse und einer Umhüllung |
DE102015004306A1 (de) * | 2015-04-01 | 2016-10-06 | Diehl Bgt Defence Gmbh & Co. Kg | Nebelwurfkörper |
US10926273B2 (en) | 2019-01-31 | 2021-02-23 | Toyota Motor Engineering & Manufacturing North America, Inc. | Systems and methods for modifying an infrared signature of a vehicle |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3352238A (en) * | 1965-10-12 | 1967-11-14 | Universal Match Corp | Atomizer and method for disseminating toxicants |
US3861880A (en) * | 1973-03-06 | 1975-01-21 | Dow Chemical Co | Oxygen generator cell |
DE2359758C1 (de) * | 1973-11-30 | 1988-07-28 | Buck Chemisch-Technische Werke GmbH & Co, 7347 Bad Überkingen | Infrarot-Störstrahler |
FR2343989A1 (fr) * | 1976-03-09 | 1977-10-07 | Lacroix E | Dispositif de lancement de leurre infra-rouge |
NO142930C (no) * | 1978-03-08 | 1980-11-12 | Raufoss Ammunisjonsfabrikker | Enhetsladning for kjoeretoeysskjerming. |
DE2811016C1 (de) * | 1978-03-14 | 1986-07-17 | Buck Chemisch-Technische Werke Gmbh & Co, 8230 Bad Reichenhall | Wurfkoerper |
US4860657A (en) * | 1978-05-05 | 1989-08-29 | Buck Chemisch-Technische Werke Gmbh & Co. | Projectile |
DE3238455C2 (de) * | 1982-10-16 | 1987-03-05 | Pyrotechnische Fabrik F. Feistel GmbH + Co KG, 6719 Göllheim | Nebelwurfkörper |
US5113765A (en) * | 1990-03-30 | 1992-05-19 | James Carey | Absolute anti-roll emergency road flare |
NO171750C (no) * | 1991-01-21 | 1993-04-28 | Raufoss As | Anordning ved roeykgranat |
DE4125355C1 (de) * | 1991-07-31 | 1993-01-28 | Buck Werke Gmbh & Co, 7347 Bad Ueberkingen, De | |
FR2729749B1 (fr) * | 1993-07-29 | 1997-05-23 | Lacroix Soc E | Cartouche de leurrage infrarouge et dispositif de leurrage comportant une telle cartouche |
DE19756204C1 (de) * | 1997-12-17 | 1999-03-11 | Buck Chem Tech Werke | Folienstreifen für pyrotechnische Effekte sowie Feuerwerkskörper |
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 |
DE10065816B4 (de) * | 2000-12-27 | 2009-04-23 | Buck Neue Technologien Gmbh | Munition zur Erzeugung eines Nebels |
-
2002
- 2002-06-14 DE DE10226507A patent/DE10226507A1/de not_active Withdrawn
-
2003
- 2003-04-21 MY MYPI20031488A patent/MY134363A/en unknown
- 2003-06-12 DE DE50301814T patent/DE50301814D1/de not_active Expired - Lifetime
- 2003-06-12 AU AU2003242677A patent/AU2003242677B2/en not_active Ceased
- 2003-06-12 WO PCT/EP2003/006147 patent/WO2003106913A1/de not_active Application Discontinuation
- 2003-06-12 BR BRPI0311793-6B1A patent/BR0311793B1/pt not_active IP Right Cessation
- 2003-06-12 EP EP03759933A patent/EP1514072B1/de not_active Expired - Lifetime
- 2003-06-12 US US10/517,288 patent/US20060060103A1/en not_active Abandoned
-
2004
- 2004-12-12 IL IL165732A patent/IL165732A/en active IP Right Grant
- 2004-12-21 ZA ZA200410264A patent/ZA200410264B/en unknown
Non-Patent Citations (1)
Title |
---|
See references of WO03106913A1 * |
Also Published As
Publication number | Publication date |
---|---|
EP1514072B1 (de) | 2005-11-30 |
IL165732A (en) | 2010-11-30 |
US20060060103A1 (en) | 2006-03-23 |
IL165732A0 (en) | 2006-01-15 |
BR0311793B1 (pt) | 2013-12-31 |
AU2003242677A1 (en) | 2003-12-31 |
ZA200410264B (en) | 2007-07-25 |
DE10226507A1 (de) | 2003-12-24 |
MY134363A (en) | 2007-12-31 |
DE50301814D1 (de) | 2006-01-05 |
WO2003106913A1 (de) | 2003-12-24 |
BR0311793A (pt) | 2005-03-15 |
AU2003242677B2 (en) | 2009-03-26 |
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