EP2989414A1 - Drallstabilisiertes leuchtgeschoss - Google Patents
Drallstabilisiertes leuchtgeschossInfo
- Publication number
- EP2989414A1 EP2989414A1 EP14722587.4A EP14722587A EP2989414A1 EP 2989414 A1 EP2989414 A1 EP 2989414A1 EP 14722587 A EP14722587 A EP 14722587A EP 2989414 A1 EP2989414 A1 EP 2989414A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- luminous
- projectile
- parachute
- spin
- floor
- 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
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
- F42B4/28—Parachute flares
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
- F42B10/48—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding
- F42B10/56—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding of parachute or paraglider type
-
- 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
- F42B12/42—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 illuminating type, e.g. carrying flares
-
- 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
Definitions
- the invention is concerned with a space-saving 1-stage ejection system for a lightning projectile, in particular for an artillery light projectile.
- Known luminous projectiles for example for illuminating a battlefield, are based on a 2-stage ejection system. In this case, the timing of the application of the projectiles is controlled by pyrotechnic delay elements.
- a lighting projectile describes the DE 10 2007 057 184 A1. It is known that, in particular, environmental influences have a great influence on the pyrotechnic charges. This influence additionally leads to a spread in the delay times.
- a luminous ammunition for battlefield illumination with a parachute is disclosed in WO 2009/0468000 A1.
- light-emitting diodes are used as luminous bodies, which are arranged like an array.
- DE 25 18 645 A1 discloses a luminous projectile with a projectile casing and a packing sleeve.
- the packing sleeve there are an incident shield, a main parachute, a swirl brake and a light pot.
- the projectile hood another twist brake is arranged, which in turn is formed by swinging wings. These open when they have left the projectile casing and serve to reduce the swirl pot's swirl.
- Such a structure requires a relatively large space in the floor.
- the invention takes on the task to show an ejection system, which is constructed to save space.
- the invention is based on the idea of integrating a 1-stage ejection system in the projectile, ie to realize a 1-stage lighting projectile.
- a 1-stage ejection system in the projectile
- the luminaire then sinks at the main parachute at a constant speed to the ground.
- This idea means that the structure for the luminous floor, which is also cheaper, requires less space in the floor. This creates the use for a larger luminous body, which in turn leads to a longer lighting time.
- the structural design is distinguished from known projectiles in that the internal structure of the filament is pushed out of the projectile casing by only one ejection charge. There is no 2nd output. The further activation of the sinking parachute takes place by separation of the packaging line from the latter with the aid of the separating device. The timing takes over a delay unit in a known manner.
- FIG. 1 is an enlarged view of the inner structure of FIG. 1,
- Fig. 3 is an illustration of the device for rope separation of the packaging line
- a designated 1 luminous projectile is shown.
- the projectile 1 comprises a projectile floor 2, a ballute 3 and a parachute support 4.
- the parachute support 4 serves to receive a sinking parachute 5 with swirl brake 6.
- the parachute support 4 is integrated in the rear part of a projectile shell 7 of the projectile 1.
- In the front part of the projectile casing 7 at least one luminous element 8 is integrated, wherein in the exemplary embodiment, three filaments 8 are integrated stacked, which act together.
- a packing sleeve 9 can be provided, which receives the luminous bodies 8.
- the projectile nose is provided with a discharge charge 10 which reaches as far as a plate 11 or, when using a packing sleeve 9, as far as the bottom of the packing sleeve 9.
- the ejection charge 10 is preferably located in a central cavity.
- a packing line 12 for the sinking parachute 5 leads from the rear plate 16 of the parachute support 4 (viewed in the direction of flight of the projectile 1) to the luminous bodies 8. This is separated for the use of the sinking parachute 5.
- the separating device 13 comprises a cutting punch 14.
- the ball 3 unfolds and takes over together with the swirl brake 6, the function of reducing the swirl of the luminous element 8.
- the sinking parachute 5 takes on the task of controlling the lowering of the lighting elements 8, so that the lighting elements 8 on the sinking parachute sink to the ground at a constant speed.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Non-Portable Lighting Devices Or Systems Thereof (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
Description
Claims
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PL14722587T PL2989414T3 (pl) | 2013-04-24 | 2014-04-23 | Pocisk oświetlający o stabilizowanym wirowaniu |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102013007031 | 2013-04-24 | ||
| PCT/EP2014/058170 WO2014173916A1 (de) | 2013-04-24 | 2014-04-23 | Drallstabilisiertes leuchtgeschoss |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP2989414A1 true EP2989414A1 (de) | 2016-03-02 |
| EP2989414B1 EP2989414B1 (de) | 2018-01-31 |
Family
ID=50685879
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP14722587.4A Active EP2989414B1 (de) | 2013-04-24 | 2014-04-23 | Drallstabilisiertes leuchtgeschoss |
Country Status (7)
| Country | Link |
|---|---|
| EP (1) | EP2989414B1 (de) |
| DK (1) | DK2989414T3 (de) |
| ES (1) | ES2665878T3 (de) |
| NO (1) | NO2997483T3 (de) |
| PL (1) | PL2989414T3 (de) |
| TR (1) | TR201802200T4 (de) |
| WO (1) | WO2014173916A1 (de) |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1978641A (en) * | 1923-04-18 | 1934-10-30 | Martin Ralph | Illuminating projectile |
| FR1011556A (fr) * | 1949-07-27 | 1952-06-24 | Fusée éclairante | |
| US3374739A (en) * | 1966-03-16 | 1968-03-26 | Army Usa | Payload recovery system |
| FR2260772B1 (de) * | 1974-02-08 | 1976-06-25 | France Etat | |
| DE2518645C2 (de) * | 1975-04-26 | 1986-07-17 | Rheinmetall GmbH, 4000 Düsseldorf | Drallbremse für eine aus einem Drallgeschoss ausstoßbare Nutzlast |
| DE3618679A1 (de) * | 1986-06-03 | 1987-12-10 | Diehl Gmbh & Co | Munition mit einem fallschirm |
| GB9015445D0 (en) * | 1990-07-13 | 1991-02-20 | Royal Ordnance Plc | Projectile surveillance apparatus |
| US5398614A (en) * | 1994-06-10 | 1995-03-21 | The United States Of America As Represented By The Secretary Of The Army | Ram air inflated decelerator deployment flaps |
| JP3856177B2 (ja) * | 1998-03-31 | 2006-12-13 | 株式会社小松製作所 | 高速飛翔体 |
-
2014
- 2014-04-23 EP EP14722587.4A patent/EP2989414B1/de active Active
- 2014-04-23 PL PL14722587T patent/PL2989414T3/pl unknown
- 2014-04-23 ES ES14722587.4T patent/ES2665878T3/es active Active
- 2014-04-23 DK DK14722587.4T patent/DK2989414T3/en active
- 2014-04-23 WO PCT/EP2014/058170 patent/WO2014173916A1/de not_active Ceased
- 2014-04-23 TR TR2018/02200T patent/TR201802200T4/tr unknown
- 2014-06-28 NO NO14816848A patent/NO2997483T3/no unknown
Non-Patent Citations (1)
| Title |
|---|
| See references of WO2014173916A1 * |
Also Published As
| Publication number | Publication date |
|---|---|
| TR201802200T4 (tr) | 2018-03-21 |
| EP2989414B1 (de) | 2018-01-31 |
| DK2989414T3 (en) | 2018-05-07 |
| NO2997483T3 (de) | 2018-01-20 |
| WO2014173916A1 (de) | 2014-10-30 |
| PL2989414T3 (pl) | 2018-07-31 |
| ES2665878T3 (es) | 2018-04-30 |
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