EP3775755A1 - Projectile explosif - Google Patents
Projectile explosifInfo
- Publication number
- EP3775755A1 EP3775755A1 EP19711054.7A EP19711054A EP3775755A1 EP 3775755 A1 EP3775755 A1 EP 3775755A1 EP 19711054 A EP19711054 A EP 19711054A EP 3775755 A1 EP3775755 A1 EP 3775755A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- projectile
- explosive charge
- protective layer
- explosive
- layer
- 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
- 239000002360 explosive Substances 0.000 title claims abstract description 58
- 239000010410 layer Substances 0.000 claims abstract description 23
- 239000011241 protective layer Substances 0.000 claims abstract description 19
- 238000004519 manufacturing process Methods 0.000 claims description 5
- 239000004570 mortar (masonry) Substances 0.000 claims description 2
- 230000000977 initiatory effect Effects 0.000 description 4
- 238000005422 blasting Methods 0.000 description 3
- 238000005266 casting Methods 0.000 description 3
- 230000006835 compression Effects 0.000 description 3
- 238000007906 compression Methods 0.000 description 3
- 238000013016 damping Methods 0.000 description 2
- 238000009413 insulation Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 229920001296 polysiloxane Polymers 0.000 description 2
- 239000003795 chemical substances by application Substances 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 229920001903 high density polyethylene Polymers 0.000 description 1
- 239000011796 hollow space material Substances 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 238000007493 shaping process Methods 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
- F42B12/20—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
- F42B12/207—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type characterised by the explosive material or the construction of the high explosive warhead, e.g. insensitive ammunition
Definitions
- the invention relates to a warhead, in particular an explosive projectile, in which an explosive charge is received, which is introduced from behind into the warhead.
- EP 1 338 860 B1 describes a method for producing a large-caliber explosive projectile, in which initially a shell made of an elastic plastic (liner) is introduced through the mouth hole in the interior of the projectile casing and then the explosive charge is poured into the liner.
- liner an elastic plastic
- a liner is necessary in explosive projectiles to decouple due to the different volume expansion coefficients of the explosive charge and the projectile casing material, the explosive charge to the inner wall of the projectile casing with temperature fluctuations.
- the silicone intermediate layer is arranged in the region of the inner surface of the cavity facing the projectile nose of the blasting projectile and / or in the region of the inner surface of the hollow space facing the explosive projectile.
- the invention addresses the problem of avoiding unwanted implementation of an explosive charge by heated at launch air in particular in the bottom of the projectile to avoid.
- the invention is based on the idea to introduce an adjustable protective layer in projectiles filled from behind.
- This idea allows a simple series production while maintaining the required security.
- the introduced layer which can also be referred to as silvering, is firmly connected to the explosive charge without air layer. This ensures that sufficient thermal insulation is achieved. Furthermore, it is considered that an initiation of the explosive charge is not affected stronger by a Zündver.
- the layer thickness can be determined for each type of blasting site.
- the determined layer thickness is ensured by a contouring tool, for example by means of a casting tool.
- the compatible with the explosive charge elastic layer is applied evenly by means of the casting tool on the explosive surface.
- the resulting advantages include the fact that a cost-effective and reproducible at any time introducing the heat-insulating layer is shown.
- the layer serves as a damping element against unwanted implementation of the explosive charge at loading load, but not as a seal of an exposed explosive charge.
- the spatial order of the damping mass or the layer introduced is in the bottom of the Ge fencing head. Proposed is a projectile or a warhead with a projectile casing, an explosive charge therein and a closure part, which closes the projectile casing from behind ver.
- a protective layer is applied at least on a rear explosive charge surface of the explosive charge.
- the layer thickness of the protective layer is variable.
- the layer thickness must sufficiently reduce the heat input from the compressed air into the explosive, do not interfere with the initiation of the explosive charge by the ignition amplifier of the ignition chain.
- the layer is independent of geometry, it should as far as possible be contour-matched to the contour of the explosive charge.
- the present idea serves as protection against friction and excessive heat input into the explosive charge by compression of the residual air after closing the warhead.
- FIG. 1 It shows the only figure a projectile 1 with a projectile casing 2.
- An explosive charge 3 can here completely, partially or without wall adhesion with the projectile casing 2 ver prevented.
- a rear floor opening 4 is closed by a closure part 5.
- the explosive charge 3 is introduced in this embodiment from behind in the projectile 1 and the Ge shot casing 2.
- In the projectile 1 is the projectile head of an unspecified tank mortar or artillery ammunition.
- the projectile head or the projectile 1 is filled from behind with the explosive or explosive charge 3. This is poured into the projectile casing 2. The amount of Sprengla tion 3 is given. The explosive charge 3 assumes its position within the projectile casing 2 a. Thereafter, a protective layer 6 tion against heat in the Sprengla 3 introduced into the projectile casing 2.
- the protective layer 6 can also be referred to as silvering.
- the layer thickness 6 is to be dimensioned so that a sufficient heat insulation is achieved, an initiation of the explosive charge 3 by an unspecified Darge presented ignition amplifier of a detonating chain is not affected.
- the compatible with the explosive charge 3 protective layer 6 is preferably elastic. This is preferably applied uniformly to a rear explosive charge surface 7.
- the contours of the explosive charge 3 and the protective layer 6 can be inexpensively manufactured or created in a series production by a shaping casting tool.
- the projectile 1 is closed by means of closure part 5. There remains only a residual trapped thin layer of air. This air layer is significantly lower than an air layer without an introduced protective layer 6.
- the protective layer 6 prevents the initiation of heat from the compressed residual union air in the explosive charge 3 and thus an unwanted implementation of the projectile.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102018108766.7A DE102018108766A1 (de) | 2018-04-12 | 2018-04-12 | Sprenggeschoss |
PCT/EP2019/056005 WO2019197095A1 (fr) | 2018-04-12 | 2019-03-11 | Projectile explosif |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3775755A1 true EP3775755A1 (fr) | 2021-02-17 |
EP3775755B1 EP3775755B1 (fr) | 2024-05-01 |
Family
ID=65767009
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP19711054.7A Active EP3775755B1 (fr) | 2018-04-12 | 2019-03-11 | Projectile explosif |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP3775755B1 (fr) |
DE (1) | DE102018108766A1 (fr) |
WO (1) | WO2019197095A1 (fr) |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1396279A (en) * | 1966-01-26 | 1975-06-04 | Cross C S | Projectile |
US4365556A (en) * | 1980-10-06 | 1982-12-28 | The United States Of America As Represented By The Secretary Of The Army | Method and system for preventing base separation of cast explosives in projectiles |
AU602870B2 (en) * | 1985-10-22 | 1990-11-01 | Bae Systems Plc | Explosive projectiles |
DE10207209A1 (de) * | 2002-02-21 | 2003-09-11 | Rheinmetall W & M Gmbh | Verfahren zur Herstellung eines großkalibrigen Sprenggeschosses und Sprenggeschoß, hergestellt nach diesem Verfahren |
GB2433579B (en) * | 2004-03-15 | 2007-09-26 | Alliant Techsystems Inc | Reactive material enhanced projectiles and related methods |
DE102005050973A1 (de) | 2005-10-25 | 2007-04-26 | Rheinmetall Waffe Munition Gmbh | Sprenggeschoss |
FR2953587B1 (fr) * | 2009-12-04 | 2016-12-23 | Tda Armements Sas | Munition comportant un corps, un chargement explosif et des moyens de calage entre le corps et le chargement explosif |
DE102009022495A1 (de) | 2009-05-25 | 2010-12-02 | Rheinmetall Waffe Munition Gmbh | Verfahren zur Herstellung eines großkalibrigen Sprenggeschosses und Sprenggeschoss, hergestellt nach diesem Verfahren |
FR3002627A1 (fr) * | 2013-02-25 | 2014-08-29 | Nexter Munitions | Projectile explosif |
ITBS20130145A1 (it) * | 2013-10-16 | 2015-04-17 | Rwm Italia S P A | Metodo di caricamento di un dispositivo esplosivo avente capacita' distruttiva controllata e relativo dispositvo esplosivo |
-
2018
- 2018-04-12 DE DE102018108766.7A patent/DE102018108766A1/de active Pending
-
2019
- 2019-03-11 WO PCT/EP2019/056005 patent/WO2019197095A1/fr active Application Filing
- 2019-03-11 EP EP19711054.7A patent/EP3775755B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
DE102018108766A1 (de) | 2019-10-17 |
WO2019197095A1 (fr) | 2019-10-17 |
EP3775755B1 (fr) | 2024-05-01 |
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