EP1286129A1 - Munition incendiaire pour un projectile pénétrant stabilisé par empennage - Google Patents

Munition incendiaire pour un projectile pénétrant stabilisé par empennage Download PDF

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Publication number
EP1286129A1
EP1286129A1 EP02012954A EP02012954A EP1286129A1 EP 1286129 A1 EP1286129 A1 EP 1286129A1 EP 02012954 A EP02012954 A EP 02012954A EP 02012954 A EP02012954 A EP 02012954A EP 1286129 A1 EP1286129 A1 EP 1286129A1
Authority
EP
European Patent Office
Prior art keywords
fire
projectile
target
titanium sponge
weight
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
EP02012954A
Other languages
German (de)
English (en)
Other versions
EP1286129B8 (fr
EP1286129B1 (fr
Inventor
Stefan Dr. Thiesen
Hendrik Lips
Dr. Börngen
Dieter Jungbluth
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rheinmetall Waffe Munition GmbH
Original Assignee
Rheinmetall W&M GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Rheinmetall W&M GmbH filed Critical Rheinmetall W&M GmbH
Publication of EP1286129A1 publication Critical patent/EP1286129A1/fr
Application granted granted Critical
Publication of EP1286129B1 publication Critical patent/EP1286129B1/fr
Publication of EP1286129B8 publication Critical patent/EP1286129B8/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B45/00Compositions or products which are defined by structure or arrangement of component of product
    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06CDETONATING OR PRIMING DEVICES; FUSES; CHEMICAL LIGHTERS; PYROPHORIC COMPOSITIONS
    • C06C15/00Pyrophoric compositions; Flints

Definitions

  • the invention relates to an incendiary device for a wing stabilized balancing projectile, which in the Rearward area of the projectile can be arranged and when hitting a target behind the projectile Penetrator of the bullet as a separate unit penetrates into the target.
  • Wing stabilized balancing projectiles in which incendiary devices in the rear area of the Bullet are arranged, for example, in the German patent applications DE 199 48 708.1 and DE 199 48 710.3.
  • balancing bullets is replaces the commonly used tracer set with the set of flames to achieve that the bullet when hitting on semi-hard targets (for example, with a relative thin armor provided infantry fighting vehicles) unfolds a considerable fire effect. Because without such a fire sentence of the penetrator of the bullet would be the fly through a semi-hard target and have no significant destructive effect on it, but only a maximum projectile diameter corresponding hole in create the armor.
  • DE-AS 29 01 517 are incendiary, consisting of a metal sponge and an organic Binders are known.
  • these known incendiary are not optimal can be initiated by shock waves, especially not if only relatively small Quantities of the corresponding fire rate can be used, as this at the Tracer replacing lightning incendiaries of balancing bullets is the case.
  • the invention is based on the object, incendiary for wing-stabilized balancing projectiles which despite a relatively small volume and a low mass cause a large destructive effect within a target and upon impact a target can be safely ignited by the resulting shockwaves.
  • the invention is based on the idea, as fire set a titanium sponge to use, as an epoxy or polyester resin binder used becomes. Since the incendiary contains no oxygen carrier, it is relatively insensitive.
  • the titanium sponge particles are then heated up to the ignition temperature and continue to burn intensively with release of the particles with the atmospheric oxygen.
  • incendiary invention Another advantage of the incendiary invention is that they are normal Condition behave like an inert material and only with a very strong impact can be brought to inflammation. It is therefore also in case of missing the goal one Safe handling of the projectile possible if the fire is not damaged.
  • the fire set consists of a mixture of 85 to 96% by weight titanium sponge and 4 to 15% by weight of the epoxy or polyester resin and has a density of between 1.7 and 2.8 g / cm 3 is located.
  • the grain size of the boron powder should preferably be ⁇ 10 microns.
  • the fire rate therefore consists of a mixture of 65 to 86 wt .-% titanium sponge, 4 to 15 wt .-% of an epoxy or polyester resin and 10 to 20 wt .-% boron powder, the density of the fire rate turn between 1.7 and 2.8 g / cm 3 .
  • the grain size range of the titanium sponge to be chosen such that 30% of titanium sponge particles have a particle size greater than 450 microns and 70% have a particle size less than 450 microns.
  • balancing projectile 1 denotes a large-caliber wing-stabilized balancing projectile, as it is for example, from tank cannons is fired.
  • the balancing projectile 1 comprises a Penetrator 2 and attached to the penetrator tail 3. This consists essentially from a sleeve-shaped tail boom 4 with stabilizing wings arranged on the outside 5 and in the direction of the longitudinal axis 6 of the balancing projectile 1 extending and on the penetrator 2 side facing by this closed Recess 7.
  • the rear-side area 8 of the penetrator 2 extends into a second partial area 9 of the recess 7 and is connected to the tail unit 4, e.g. via a threaded connection 10 positively connected.
  • the Fire sentence 14 is in the recess 7 in the direction of the longitudinal axis 6 of the balancing projectile 1 arranged displaceably.
  • the stabilizing wings 5 of the tail unit 3 splinter and the capsule 12 of the fire sentence 14 at least in some areas tears.
  • the torn capsule 12 flies due to their inertia from the released Opening 16 of the recess 7 of the tail boom 4 behind the penetrator 2 ago and shattered e.g. on the back wall or on items in the tank and gives it the fire sentence free. This reacts with the atmospheric oxygen, so that a hot, beausprühender Sparks rain with considerable fire effect arises.
EP02012954A 2001-08-18 2002-06-12 Munition incendiaire pour un projectile pénétrant stabilisé par empennage Expired - Lifetime EP1286129B8 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE10140600A DE10140600A1 (de) 2001-08-18 2001-08-18 Brandsatz für ein flügelstabilisiertes Wuchtgeschoß
DE10140600 2001-08-18

Publications (3)

Publication Number Publication Date
EP1286129A1 true EP1286129A1 (fr) 2003-02-26
EP1286129B1 EP1286129B1 (fr) 2007-09-26
EP1286129B8 EP1286129B8 (fr) 2007-10-31

Family

ID=7695900

Family Applications (1)

Application Number Title Priority Date Filing Date
EP02012954A Expired - Lifetime EP1286129B8 (fr) 2001-08-18 2002-06-12 Munition incendiaire pour un projectile pénétrant stabilisé par empennage

Country Status (4)

Country Link
US (2) US6849140B2 (fr)
EP (1) EP1286129B8 (fr)
DE (2) DE10140600A1 (fr)
IL (1) IL151292A (fr)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007021451A1 (de) 2007-04-05 2008-10-09 Rwm Schweiz Ag Subprojektil mit energetischem Inhalt
US8518197B2 (en) 2005-11-29 2013-08-27 Rwm Schweiz Ag Incendiary compound comprising a combustible from group IVb of the period table, and projectile containing said incendiary compound
EP2770294A3 (fr) * 2013-02-26 2014-10-29 Diehl BGT Defence GmbH & Co.KG Masse active d'explosif pour une munition de combat
WO2016120605A1 (fr) * 2015-01-27 2016-08-04 Bae Systems Plc Matériaux réactifs

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10140600A1 (de) * 2001-08-18 2003-03-06 Rheinmetall W & M Gmbh Brandsatz für ein flügelstabilisiertes Wuchtgeschoß
US6945175B1 (en) * 2003-06-18 2005-09-20 The United States Of America As Represented By The Secretary Of The Navy Biological and chemical agent defeat system
FR2895497B1 (fr) * 2005-12-23 2008-02-08 Tda Armements Sas Soc Par Acti Dispositif de neutralisation et de destruction de batiments de stockage de substances nocives.
IL189612A (en) * 2008-02-19 2012-10-31 Rafael Advanced Defense Sys Flammable arrowhead
US8485099B2 (en) * 2008-07-10 2013-07-16 Nammo Talley, Inc. Mine defeat system and pyrotechnic dart for same
RU2655338C1 (ru) * 2017-03-31 2018-05-25 Акционерное общество "Центральный научно-исследовательский институт точного машиностроения" (АО "ЦНИИТОЧМАШ") Патрон с бронебойно-зажигательной пулей

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3865035A (en) * 1969-01-16 1975-02-11 Thiokol Chemical Corp Multi-use munition
US4381692A (en) * 1977-05-11 1983-05-03 Quantic Industries, Inc. Method of making an incendiary munition
US5076169A (en) * 1989-12-06 1991-12-31 Schweizerische Eidgenossenschaft Vertreten Durch Die Eidg Munitionsfabrik Thun Der Gruppe Fur Rustungsdienste Incendiary fragmentation particle, a method for its production, as well as the use thereof
FR2664039A1 (fr) * 1990-07-02 1992-01-03 Sauvestre Jean Claude Alliages mixtes organiques-metalliques pour realisation de projectiles.
DE19948710A1 (de) * 1999-10-09 2001-04-12 Rheinmetall W & M Gmbh Flügelstabilisiertes Wuchtgeschoß

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3927993A (en) * 1973-11-21 1975-12-23 Ronald W Griffin Fire starter and method
US4131498A (en) 1978-01-25 1978-12-26 Teledyne Industries, Inc. Metallic sponge incendiary compositions
US4374760A (en) * 1980-09-12 1983-02-22 Harold Charles Electro conductive polymer compositions and new materials found useful in their preparation
DE3164190D1 (en) * 1980-10-31 1984-07-19 Oerlikon Buehrle Ag Incendiary compound comprising a metallic fuel from group iva of the periodic system
US4978400A (en) * 1989-11-17 1990-12-18 General Sciences, Inc. Synergistic composite pyrotechnic material
US5780765A (en) * 1997-02-18 1998-07-14 Dyben; Jerry F. Pyrogen compound kit for an electrical model rocket ignitor
FR2764687B1 (fr) * 1997-06-16 1999-08-27 Ruggieri Projectile pyrotechnique pour la realisation dans le ciel de motifs d'aspect continu
DE19948708A1 (de) 1999-10-09 2001-04-12 Rheinmetall W & M Gmbh Flügelstabilisiertes Wuchtgeschoß
US6354222B1 (en) * 2000-04-05 2002-03-12 Raytheon Company Projectile for the destruction of large explosive targets
US6409854B1 (en) * 2000-10-27 2002-06-25 The United States Of America As Represented By The Secretary Of The Navy Low burning rate, reduced hazard, high temperature incendiary
US6402864B1 (en) * 2000-10-27 2002-06-11 The United States Of America As Represented By The Secretary Of The Navy Low slag, reduced hazard, high temperature incendiary
DE10140600A1 (de) * 2001-08-18 2003-03-06 Rheinmetall W & M Gmbh Brandsatz für ein flügelstabilisiertes Wuchtgeschoß

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3865035A (en) * 1969-01-16 1975-02-11 Thiokol Chemical Corp Multi-use munition
US4381692A (en) * 1977-05-11 1983-05-03 Quantic Industries, Inc. Method of making an incendiary munition
US5076169A (en) * 1989-12-06 1991-12-31 Schweizerische Eidgenossenschaft Vertreten Durch Die Eidg Munitionsfabrik Thun Der Gruppe Fur Rustungsdienste Incendiary fragmentation particle, a method for its production, as well as the use thereof
FR2664039A1 (fr) * 1990-07-02 1992-01-03 Sauvestre Jean Claude Alliages mixtes organiques-metalliques pour realisation de projectiles.
DE19948710A1 (de) * 1999-10-09 2001-04-12 Rheinmetall W & M Gmbh Flügelstabilisiertes Wuchtgeschoß

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8518197B2 (en) 2005-11-29 2013-08-27 Rwm Schweiz Ag Incendiary compound comprising a combustible from group IVb of the period table, and projectile containing said incendiary compound
DE102007021451A1 (de) 2007-04-05 2008-10-09 Rwm Schweiz Ag Subprojektil mit energetischem Inhalt
EP2770294A3 (fr) * 2013-02-26 2014-10-29 Diehl BGT Defence GmbH & Co.KG Masse active d'explosif pour une munition de combat
WO2016120605A1 (fr) * 2015-01-27 2016-08-04 Bae Systems Plc Matériaux réactifs

Also Published As

Publication number Publication date
US6849140B2 (en) 2005-02-01
EP1286129B8 (fr) 2007-10-31
DE10140600A1 (de) 2003-03-06
EP1286129B1 (fr) 2007-09-26
DE50210961D1 (de) 2007-11-08
IL151292A (en) 2006-10-05
IL151292A0 (en) 2003-04-10
US20030034102A1 (en) 2003-02-20
US20050230016A1 (en) 2005-10-20

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