EP3017271A1 - Aus einem drallstabilisierten trägergeschoss ausstossbare submunition, insbesondere leuchtmunition - Google Patents
Aus einem drallstabilisierten trägergeschoss ausstossbare submunition, insbesondere leuchtmunitionInfo
- Publication number
- EP3017271A1 EP3017271A1 EP14730896.9A EP14730896A EP3017271A1 EP 3017271 A1 EP3017271 A1 EP 3017271A1 EP 14730896 A EP14730896 A EP 14730896A EP 3017271 A1 EP3017271 A1 EP 3017271A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- submunition
- housing
- parachute
- centrifugal
- spin
- 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
- 230000008878 coupling Effects 0.000 claims abstract description 18
- 238000010168 coupling process Methods 0.000 claims abstract description 18
- 238000005859 coupling reaction Methods 0.000 claims abstract description 18
- 239000003380 propellant Substances 0.000 description 5
- 230000001681 protective effect Effects 0.000 description 4
- 230000004913 activation Effects 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 230000001419 dependent effect Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000003213 activating effect Effects 0.000 description 1
- 210000000078 claw Anatomy 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 230000007257 malfunction Effects 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 230000000452 restraining effect Effects 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
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
- 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
- F42B12/58—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles
- F42B12/62—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile
- F42B12/625—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile a single submissile arranged in a carrier missile for being launched or accelerated coaxially; Coaxial tandem arrangement of missiles which are active in the target one after the other
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
- F42B15/36—Means for interconnecting rocket-motor and body section; Multi-stage connectors; Disconnecting means
Definitions
- the invention relates to a submunition, in particular illuminated ammunition, which can be ejected from a spin-stabilized carrier bullet, comprising a submunition body and a parachute housing arranged on the rear side of the submunition body with a main parachute located therein, in particular a centrifugal clutch system.
- DE 10 2007 057 184 A1 proposes that the fall-speed reduction systems or braking systems, such as parachutes, be made ready for operation only after a predetermined time of flight and stabilization and by a delay element.
- US 2,798,683 A discloses a parachute and a parachute connection for an artillery shell, wherein the opening of the Hauptfailnes is dependent on a falling speed. So that another brake parachute can open, the propellant charge is ignited via a time fuse and a flare material is ignited by the propellant charge. By the gases of the propellant charge pressure is exerted on a plate through which an inner sleeve is pushed with the slip-on sleeve from an outer shell of the shell. In this case, shear bolts, which are integrated in the front region of the outer sleeve and a rope-containing slip sleeve sheared off.
- DE 41 16 191 A1 relates to a spin-stabilized carrier projectile with a jacket which accommodates two submunitions. On the rear side, the submunition has a brake and a main parachute and an antenna at the bow.
- a protective cover In this case, a locking element is provided between the jacket of the submunition and the protective cover, which ensures the positive connection between the jacket and protective cover under the action of the centrifugal force of the carrier projectile. After ejection of the submunition from the carrier level unfolds the Bremsfallwall, whereby the spin of the submunition decreases. Upon reaching a certain speed of the submunition pulls the locking element (a stretchable locking ring) in the groove of the shell of the submunition and releases the protective cover.
- the locking element a stretchable locking ring
- the object of the invention is to disclose a submunition which can be ejected from a spin-stabilized carrier bullet, in which an activation of the main parachute takes place at a predetermined spin of the submunition.
- the invention is essentially based on the idea of releasably connecting the submunition body and the parachute housing with one another via a centrifugal clutch such that the submunition body and the parachute housing are non-positively and / or positively locked to each other due to the centrifugal force occurring when the carrier bullet is fired be connected, and that after reducing the centrifugal force to a predetermined value, the centrifugal clutch eliminates the connection between submunitions and parachute housing.
- three rotationally symmetrically arranged securing bolts are provided which determine the position of the parachute housing relative to the coupling housing and thus also to the submunition body.
- the submunition according to the invention has the advantage that only a small space requirement is required for the centrifugal clutch.
- the activation of the main parachute is purely mechanical and almost independent of storage and temperature. because no pyrotechnics are used.
- the activation of the main parachute is also independent of the propellant charge with which the carrier bullet was fired from the corresponding weapon, and thus independent of the spin of the submunition when leaving the carrier bullet.
- the centrifugal clutch consists of a cylindrical coupling housing which is rotatably connected at one end face with the submunition and the circumference is at least partially covered by the parachute housing.
- at least one centrifugal pin is arranged in the Kuppiungsgephaseuse, which is slidably mounted in a radially outwardly extending guide bore and fixed with its first end via a tension spring in the vicinity of the central axis of the coupling housing.
- the guide bore extends to the outer wall of the coupling housing, so that the centrifugal bolt engages with a corresponding centrifugal force acting on it partially through this opening in an aligned detent opening of the parachute housing and the parachute housing connects to the submunition.
- centrifugal clutch To avoid an imbalance of the centrifugal clutch should be stored in the coupling housing at least two, preferably three, rotationally symmetrical, in guide holes radially outwardly displaceable centrifugal bolts, which engage in the case of sufficient centrifugal force in three correspondingly arranged detent openings of the parachute housing.
- FIG. 1 is a perspective view of a submunition according to the invention with a submunition, a parachute housing with Hauptfalinem and a centrifugal clutch, immediately after leaving a carrier projectile;
- denoted by 1 is a submunition ejected from a spin-stabilized carrier bullet at a predetermined height, which is, for example, a light ammunition flying in the direction of the arrow marked 100.
- the light ammunition 1 comprises a submunition 2 a luminous body, to which the rear side a hood-shaped parachute housing 3 with a main parachute located therein (not shown) is connected.
- the centrifugal clutch 4 consists of a preferably cylindrical coupling housing 5, which is non-positively connected at one end face 6 with the luminous body 2, and which is peripherally surrounded by the outer wall 7 of the parachute housing 3 (see also Fig. 2 and 3).
- centrifugal bolts 8 are arranged, which are displaceably mounted in three radially outwardly extending guide holes 9.
- the guide bores 9 extend through the outer wall 10 of the coupling housing 5, so that corresponding openings 14 are present on the outer wall side.
- the centrifugal bolts 8 are fastened with their first end 11 in each case via a tension spring 12 with the coupling housing 5 in the vicinity of the central axis 13. Due to the centrifugal forces acting on them, the centrifugal bolts 8 are displaced radially outward against the restraining forces of the tension springs 12 and each engage with their second end 17 through the outer wall side openings 14 into corresponding aligned detent opening 15 of the parachute housing 3 (FIG.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102013011219.2A DE102013011219B3 (de) | 2013-07-05 | 2013-07-05 | Aus einem drallstabilisierten Trägergeschoss ausstoßbare Submunition, insbesondere Leuchtmunition |
PCT/EP2014/062629 WO2015000691A1 (de) | 2013-07-05 | 2014-06-17 | Aus einem drallstabilisierten trägergeschoss ausstossbare submunition, insbesondere leuchtmunition |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3017271A1 true EP3017271A1 (de) | 2016-05-11 |
EP3017271B1 EP3017271B1 (de) | 2017-08-09 |
Family
ID=50879065
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP14730896.9A Active EP3017271B1 (de) | 2013-07-05 | 2014-06-17 | Aus einem drallstabilisierten trägergeschoss ausstossbare submunition, insbesondere leuchtmunition |
Country Status (5)
Country | Link |
---|---|
EP (1) | EP3017271B1 (de) |
DE (1) | DE102013011219B3 (de) |
ES (1) | ES2644379T3 (de) |
LT (1) | LT3017271T (de) |
WO (1) | WO2015000691A1 (de) |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR862451A (fr) * | 1939-08-23 | 1941-03-07 | Perfectionnements à la défense contre aéronefs au moyen de mines aériennes | |
US2798683A (en) * | 1952-03-19 | 1957-07-09 | Wayne A Swenson | Delayed release mechanism for parachutes |
US3221656A (en) * | 1964-03-23 | 1965-12-07 | Adrian P Sutten | Apparatus for high-velocity recovery |
DE3046816C2 (de) * | 1980-12-12 | 1982-12-02 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | "Verpackungsbehälter für den Fallschirm einer Abwurflast" |
US4628821A (en) * | 1985-07-05 | 1986-12-16 | The United States Of America As Represented By The Secretary Of The Army | Acceleration actuated kinetic energy penetrator retainer |
DE8711921U1 (de) * | 1987-09-03 | 1989-01-05 | Diehl GmbH & Co, 8500 Nürnberg | Submunition eines Drallgeschosses |
DE4116191A1 (de) * | 1991-05-17 | 1992-11-19 | Rheinmetall Gmbh | Submunition fuer ein drallstabilisiertes traegergeschoss |
DE4124655C2 (de) * | 1991-07-25 | 1995-07-06 | Rheinmetall Ind Gmbh | Bremseinrichtung für Submunition |
US5386781A (en) * | 1992-11-12 | 1995-02-07 | Thiokol Corporation | Parachute deployment system |
DE102007048074A1 (de) * | 2007-10-05 | 2009-04-09 | Rheinmetall Waffe Munition Gmbh | Leuchtmunition zur Gefechtsfeldbeleuchtung |
DE102007057184A1 (de) * | 2007-11-26 | 2009-05-28 | Rheinmetall Waffe Munition Gmbh | Munition oder Geschoss zur Gefechtsfeldbeleuchtung |
DE102008023271A1 (de) * | 2008-05-13 | 2009-11-19 | Rheinmetall Waffe Munition Gmbh | Fallschirmsystem für insbesondere ballistisch ausgebrachte Systeme |
-
2013
- 2013-07-05 DE DE102013011219.2A patent/DE102013011219B3/de not_active Expired - Fee Related
-
2014
- 2014-06-17 EP EP14730896.9A patent/EP3017271B1/de active Active
- 2014-06-17 LT LTEP14730896.9T patent/LT3017271T/lt unknown
- 2014-06-17 ES ES14730896.9T patent/ES2644379T3/es active Active
- 2014-06-17 WO PCT/EP2014/062629 patent/WO2015000691A1/de active Application Filing
Non-Patent Citations (1)
Title |
---|
See references of WO2015000691A1 * |
Also Published As
Publication number | Publication date |
---|---|
LT3017271T (lt) | 2017-09-11 |
DE102013011219B3 (de) | 2014-06-26 |
EP3017271B1 (de) | 2017-08-09 |
ES2644379T3 (es) | 2017-11-28 |
WO2015000691A1 (de) | 2015-01-08 |
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