EP1035401A2 - Dispositif de lancement pour une pluralité de projectiles - Google Patents
Dispositif de lancement pour une pluralité de projectiles Download PDFInfo
- Publication number
- EP1035401A2 EP1035401A2 EP99124646A EP99124646A EP1035401A2 EP 1035401 A2 EP1035401 A2 EP 1035401A2 EP 99124646 A EP99124646 A EP 99124646A EP 99124646 A EP99124646 A EP 99124646A EP 1035401 A2 EP1035401 A2 EP 1035401A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- adapter
- active
- launch tube
- active body
- body package
- 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
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A19/00—Firing or trigger mechanisms; Cocking mechanisms
- F41A19/58—Electric firing mechanisms
- F41A19/64—Electric firing mechanisms for automatic or burst-firing mode
- F41A19/65—Electric firing mechanisms for automatic or burst-firing mode for giving ripple fire, i.e. using electric sequencer switches for timed multiple-charge launching, e.g. for rocket launchers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H9/00—Equipment for attack or defence by spreading flame, gas or smoke or leurres; Chemical warfare equipment
- F41H9/06—Apparatus for generating artificial fog or smoke screens
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
- F42B5/02—Cartridges, i.e. cases with charge and missile
- F42B5/03—Cartridges, i.e. cases with charge and missile containing more than one missile
- F42B5/035—Cartridges, i.e. cases with charge and missile containing more than one missile the cartridge or barrel assembly having a plurality of axially stacked projectiles each having a separate propellant charge
Definitions
- the present invention relates to a device for firing a plurality of active bodies and one using them Throwing system.
- Switching arrangements for firing dummy target sub-bodies in a freely selectable time sequence from a cartridge tube Ignition each with an electric lighter Ignition circuit and each connected to a submunition Ejection charges are also well known. So revealed for example, US 5,429,052 with such a switching arrangement automatic, successive ignition pulse switching.
- the object of the present invention is to launch a Large number of active bodies, regardless of caliber, with simplified To allow contact guidance and reduced installation effort.
- a device for Firing a variety of active bodies solved one Adapter that includes a control unit and in a launch tube a throwing cup is releasably fixable, and an active body package that the active body and detachable with the adapter, mechanically as well as electrically, is connectable, wherein in assembled state, in which the active body package with the The adapter is connected to the active body from the active body package the control unit of the adapter individually in sequence, the Interval between the firing of two consecutive Active bodies is adjustable, or at least partially can be fired at the same time.
- Control unit a battery, contact rings, at least one circuit board for an electronic circuit and, preferably resilient, Includes contact pins and can be used in an adapter housing and there is tightly and releasably attachable.
- Active body package with the adapter mechanically via a Clamp connection, snap connection or the like connectable is, and by mechanically connecting the active body package with the adapter automatically creates an electrical circuit between the Active body package and the adapter is closable.
- the Active body package electrically with the adapter by contacting the Contact pins of the control unit of the adapter by means of this complementary contact points of the active body package can be connected, and the contact points in electrical connection with at least a means of expelling active bodies from the Active body package stand.
- Active body package comprises at least one launch tube, and in each Launch tube two or more active bodies in the launch direction in series are arranged, four active bodies per launch tube preferred are.
- each active body a propellant charge with a lighter, such as a squib or the like, in connection with the control unit of the adapter in assembled condition of active body package and adapter, assigned.
- a lighter such as a squib or the like
- the propellant charges for the Active body of each launch tube within that Launch tube are arranged, and the igniter of the propellant charges are arranged outside the launch tube in question.
- the invention proposed that the propellant charges and igniter for the Active body of each launch tube of the active body package in one common propellant charge bar are arranged, and over the Propellant charge is an electrical contact for the lighter Control unit of the adapter can be built, preferably under Interposition of at least one circuit board for an electronic one Circuit with the contact points.
- the launch tube of the Propellant charge strip associated with the active substance package outside and runs parallel to the longitudinal central axis of this launch tube and is releasably connectable with the same, and propellant gases via lateral holes in the launch tube of the active body package in the same can occur for firing active bodies.
- each lateral bore in the launch tube of the active body package in one Gas space below an active body in this launch tube flows.
- each launch tube a sensor system, preferably in the area of the lastly from this launch tube to be fired active body, arranged and electrically with the control unit of the adapter is connectable.
- two or more Launch tubes parallel to each other in an active body package are arranged, and the launch tubes on a common Plate on which the electrical connection of the launch tubes preferably the at least one circuit board for an electrical one Circuit is located with the contact points, connectable are.
- the active bodies Launch tube can be fired for launch tube.
- the invention provides a throwing system with at least one Throwing cup by using an inventive Device is marked.
- the active body outside the Launch tube of the throwing cup are arranged when the adapter in the throw cup and the active body package on the adapter are attached.
- the Adapter is jammed in the launch tube of the throwing cup, as above a screw connection, and for maintenance purposes or for Firing conventional ammunition from the launch tube of the Throw cup is to be removed.
- the invention is therefore based on the surprising finding that by interposing an adapter between one Throwing cup and an active body package firstly for too available active volumes secondly, a caliber dependency thirdly, no pollution in the area of Contact head occurs within the throwing system and fourth the Handling and wiring is simplified. This leads to overall at considerable cost savings, namely in particular by saving the need for use different throwing cups to fire a certain one Number and / or a certain type of active bodies and by Reduction of maintenance costs.
- the area of application will also be one Throwing system according to the invention due to its modularity enlarges, which is tactically and strategically particularly advantageous.
- the invention includes Device as essential elements an adapter 10 and a Active body package 20, the electrical and mechanical with each other are releasably connectable.
- the adapter 10 according to FIG. 4 is constructed as follows:
- a control unit is located within an adapter housing 11 Fixing screws 17a, 17b, 17c can be fixed, as also in FIG. 3 indicated.
- the control unit in turn consists of resilient Contact pins 12 on a contact pin carrier 13 in contact with an electronic control on boards 14a, 14b, 14c, the are in turn electrically connected to a battery 16.
- the control unit is also via its contact rings 15a, 15b controllable outside via a throwing cup 1.
- the adapter 10 in the launch tube of the throwing cup 1 in such a way usable below that the control unit, apart from the Contact pins 12 on the contact pin carrier 13, within the Launch tube of the throwing cup 1 is arranged, namely in the Area between points A and B of Figure 4.
- the Clamping adapter 10 in the launch tube of the throwing cup 1 fixable, namely via an adapter screw 18.
- the active body package 20 according to the invention is as shown in FIG. 5 constructed as follows:
- An active body package housing 21 has a clamping groove 22 for one mechanical connection with the adapter housing 11, wherein in Figures 1 and 3, the assembled state of adapter 10 and Active body package 20 is shown.
- each launch tube 23 Inside each launch tube 23 are in the launch direction four active bodies 24a, 24b, 24c, 24d, one behind the other gas space 25a, 25b, 25c, 25d arranged underneath.
- the launch tube 23 is below the lowest gas space 25d closed by a bottom cover 26.
- the bottom cover 26 stands with a board 27 in connection on which an electrical Circuit and contact points 28 for electrical contact with the contact pins 12 on the contact pin carrier 13 of the adapter 10 are applied.
- Each launch tube 23 has in the area of the gas spaces 25a, 25b, 25c, 25d a lateral bore 30a, 30b, 30c, 30d to a To provide connection to a propellant charge bar 29 which is parallel to the Launch tube 23 runs and with the same over a variety of Threaded bolt 33a, 33b, 33c, 33d is connected.
- a propellant charge bar 29 which is parallel to the Launch tube 23 runs and with the same over a variety of Threaded bolt 33a, 33b, 33c, 33d is connected.
- Propellant charge strips 29 are for each active body 24a, 24b, 24c, 24d in the launch tube 23 a propellant charge 31a, 31b, 31c, 31d together Primer 32a, 32b, 32c, 32d arranged.
- the squibs 32a, 32b, 32c, 32d are in turn above the board 27 and the contact points 28 of the active body package 20 with the control unit within the Adapters 10 in the assembled state of adapter 10 and Active body package 20 in electrical connection, as in FIG. 3 indicated.
- the active body package 20 also has one Temperature sensor 34 in the area of the last one from the launch tube 23 active body to be fired 24 d.
- This temperature sensor 34 is also on the board 27 together with the contact points 28 with the Control unit in the adapter 10 electrically connectable if that Active body package 20 on the adapter 10 in that shown in Figure 3 Way is set up.
- a throwing system according to the invention with the above is for example as follows for the A variety of active bodies can be built up:
- the control unit 12, 13, 14a, 14b, 14c, 15a, 15b, 16 is in the Figures 3 and 4 from below, inserted into the adapter housing 11 and there by means of the three fastening screws 17a, 17b, 17c fixed.
- the tightness within the adapter housing 10 compared Environmental influences are caused by O-rings, not shown guaranteed.
- the adapter housing 11 is in the launch tube of the Throwing cup 1 inserted and finally the arrangement of the Adapter 10 inside the throwing cup 1 by tightening the Adapter screw 18 fixed.
- the adapter 10 thus assembled must be off the throwing cup 1 only for regular maintenance purposes or Conventional ammunition can be removed again.
- the active body package is placed on the adapter 10 in the throwing cup 1 20, in Figures 1 and 3, from above, until the clamping groove 22 for provides a firm mechanical connection and the contact points 28 of the active body package 20, the contact pins 12 of the adapter 10 to contact.
- the arrangement of the contacts 12, 28 is relative to the Clamping groove 22 selected such that incorrect contacting is not is possible.
- a single throw cup 1 through the enlargement of space for the active bodies 24a, 24b, 24c, 24d due to the Interposition of the adapter 10 now sixteen active bodies 24a, 24b, 24c, 24d from four launch tubes 23, 23 ', 23 ", 23"' selectively lockable to, for example, a desired one Camouflage wall at a selected distance over a selected one Build up time.
- a corresponding signal is the contact rings 15a, 15b of the Adapters 10 supplied and via the electronic control the same and the board 27 of the active body package 20 to the corresponding squibs 32a, 32b, 32c, 32d forwarded.
- a squib for example squib 32a
- a squib 32a can be ignite the corresponding propellant 31a so that propellant gas via the corresponding bore 30a into the associated gas space 25a occurs and an overpressure builds up until finally the Active body 24a in the firing direction above this gas space 25a is fired from the launch tube 23.
- the Charge status of the launch tube 23 is during the firing can be checked via the temperature sensor 34.
- the four launch tubes 23, 23 ', 23 “, 23 “'in succession, at a certain time interval to each other, in groups or simultaneously to fire theirs respective active bodies 24a, 24b, 24c, 24d are controlled, see above that it is possible for the first time, even over several seconds a smoke screen necessary for camouflage or protection build up.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
- Feeding, Discharge, Calcimining, Fusing, And Gas-Generation Devices (AREA)
- Containers And Packaging Bodies Having A Special Means To Remove Contents (AREA)
- Medicines Containing Material From Animals Or Micro-Organisms (AREA)
- Medicines That Contain Protein Lipid Enzymes And Other Medicines (AREA)
- Air Bags (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19910074 | 1999-03-08 | ||
DE19910074A DE19910074B4 (de) | 1999-03-08 | 1999-03-08 | Abschußvorrichtung für das Verschießen einer Mehrzahl von Wirkkörpern sowie diese verwendende Wurfanlage |
Publications (3)
Publication Number | Publication Date |
---|---|
EP1035401A2 true EP1035401A2 (fr) | 2000-09-13 |
EP1035401A3 EP1035401A3 (fr) | 2001-10-17 |
EP1035401B1 EP1035401B1 (fr) | 2005-02-09 |
Family
ID=7900062
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP99124646A Expired - Lifetime EP1035401B1 (fr) | 1999-03-08 | 1999-12-10 | Dispositif de lancement pour une pluralité de projectiles |
Country Status (4)
Country | Link |
---|---|
US (1) | US6659012B1 (fr) |
EP (1) | EP1035401B1 (fr) |
AT (1) | ATE289054T1 (fr) |
DE (2) | DE19910074B4 (fr) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2011101692A1 (fr) * | 2010-02-17 | 2011-08-25 | Wallop Defence Systems Limited | Cartouche de contre-mesure à air |
WO2013178712A1 (fr) * | 2012-05-29 | 2013-12-05 | Rheinmetall Waffe Munition Gmbh, Patente | Munition comprenant des moyens actifs |
WO2013178607A1 (fr) * | 2012-05-29 | 2013-12-05 | Rheinmetall Waffe Munition Gmbh, Patente | Munition à moyens actifs |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2002048641A1 (fr) * | 2000-12-13 | 2002-06-20 | The Secretary Of State For Defence | Fusee-leurre a emission infrarouge |
GB0120181D0 (en) * | 2001-08-17 | 2009-07-22 | Bae Systems Plc | Projectile Storage and Launch Apparatus |
AUPS303702A0 (en) * | 2002-06-20 | 2002-07-11 | Metal Storm Limited | A cartridge assembly for multiple projectiles |
DE10320731B4 (de) | 2003-05-08 | 2005-07-21 | Nico-Pyrotechnik Hanns-Jürgen Diederichs GmbH & Co. KG | Schnellfeuerwaffe |
US8215237B2 (en) * | 2006-07-10 | 2012-07-10 | Raytheon Company | Methods and apparatus for projectile data link system |
EP1962047B1 (fr) * | 2007-02-23 | 2011-06-29 | Clearspark, LLC | Système de lancement pour projectiles pyrotechniques |
DE102008064638A1 (de) | 2008-06-16 | 2009-12-17 | Rheinmetall Waffe Munition Gmbh | Flare mit Flareanzündung sowie Ausstoßsystem dafür |
DE102009020558A1 (de) | 2009-05-08 | 2010-11-18 | Rheinmetall Waffe Munition Gmbh | Aktivierungseinheit für munitionsfreie Scheinziele |
WO2010127762A1 (fr) | 2009-05-08 | 2010-11-11 | Rheinmetall Waffe Munition Gmbh | Unité d'activation pour masses actives ou corps actifs |
DE102009020557B4 (de) * | 2009-05-08 | 2011-03-31 | Rheinmetall Waffe Munition Gmbh | Aktivierungseinheit für Wirkmassen bzw. Wirkkörper |
DE102009030869A1 (de) | 2009-06-26 | 2011-02-10 | Rheinmetall Waffe Munition Gmbh | Wirkkörper |
DE102009030870A1 (de) | 2009-06-26 | 2010-12-30 | Rheinmetall Waffe Munition Gmbh | Wirkkörper |
EP2612101B1 (fr) | 2010-08-31 | 2017-01-11 | Rheinmetall Waffe Munition GmbH | Dispositif et procédé pour générer un mur ou un nuage de brouillard actif |
DE102010036026A1 (de) | 2010-08-31 | 2012-03-01 | Rheinmetall Waffe Munition Gmbh | Vorrichtung und Verfahren zur Bestimmung der Effektivität einer Nebelwand zur Erzeugung einer wirksamen Nebelwolke |
DE102015011058A1 (de) | 2015-08-27 | 2017-03-02 | Rheinmetall Waffe Munition Gmbh | System zur Abwehr von Bedrohungen |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0588015A1 (fr) | 1992-09-15 | 1994-03-23 | Buck Werke GmbH & Co | Méthode et matériaux de camouflage et son application |
Family Cites Families (23)
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US2451981A (en) * | 1939-08-10 | 1948-10-19 | Schermuly Conrad David | Rocket and the like |
US3142959A (en) * | 1959-09-11 | 1964-08-04 | Phillips Petroleum Co | Range control of self propelled missile |
US3013493A (en) * | 1960-06-13 | 1961-12-19 | Thiokol Chemical Corp | Aerial flare |
US3199406A (en) * | 1961-06-21 | 1965-08-10 | Mb Assoc | In-line launching |
AT330030B (de) * | 1973-02-15 | 1976-06-10 | Urbach Ing Erich | Werfer |
SE386735B (sv) * | 1974-11-22 | 1976-08-16 | Philips Svenska Ab | Anleggning for selektiv avfyrning av s k ir-facklor |
FR2294420A1 (fr) * | 1974-12-13 | 1976-07-09 | Lacroix E | Dispositif de lancement de leurres |
FR2383419A1 (fr) * | 1977-03-07 | 1978-10-06 | Lacroix E | Valise lance-leurres pour la deception des systemes de guidage d'armes |
GB2042835B (en) * | 1979-02-03 | 1983-08-17 | Solartron Electronic Group | Pyrotechnic devices and systems and firing circuits therefor |
GB2188920B (en) * | 1980-05-28 | 1988-03-16 | Haley And Weller Limited | Radiation absorbing screen |
US4791870A (en) * | 1983-04-05 | 1988-12-20 | Haley & Weller Limited | Pyrotechnic assembly |
SE8402109L (sv) * | 1983-05-03 | 1984-11-04 | Philips Svenska Ab | Patron for utskjutning av stormedel, vilken patron innehaller flera stormedelsladdningar |
GB2161675B (en) * | 1984-05-10 | 1987-07-01 | Plessey Co Plc | Improvements relating to electrical firing systems |
DE3421708A1 (de) * | 1984-06-12 | 1985-12-12 | Buck Chemisch-Technische Werke GmbH & Co, 7347 Bad Überkingen | Einrichtung zur erzeugung einer scheinzielwolke, insbesondere einer infrarot-scheinzielwolke |
DE3516795A1 (de) * | 1985-05-09 | 1986-11-13 | Wolfgang 8011 Baldham Dahmen | Schlauchbruchsicherungsvorrichtung |
DE3809177C1 (fr) * | 1988-03-18 | 1989-06-22 | Buck Chemisch-Technische Werke Gmbh & Co, 7347 Bad Ueberkingen, De | |
US5157222A (en) * | 1989-10-10 | 1992-10-20 | Joanell Laboratories, Inc. | Pyrotechnic ignition apparatus and method |
FR2683310B1 (fr) * | 1991-11-06 | 1993-12-31 | Giat Industries | Dispositif d'ejection d'elements de charge utile hors de l'enveloppe d'un obus cargo. |
FR2697328A1 (fr) * | 1992-10-23 | 1994-04-29 | Giat Ind Sa | Munition fumigène. |
US5429052A (en) * | 1993-07-30 | 1995-07-04 | Buck Werke Gmbh & Co. | Circuit arrangement for firing dummy target sub-members in a freely selectable chronological sequence |
DE4337680C2 (de) * | 1993-11-04 | 1995-08-24 | Buck Chem Tech Werke | Zweikomponenten-Nebelwurfkörper |
FR2722872B1 (fr) * | 1994-07-19 | 1996-10-04 | Lacroix Soc E | Dispositif pyrotechnique de lancement d'au moins un projectile |
US6279482B1 (en) * | 1996-07-25 | 2001-08-28 | Trw Inc. | Countermeasure apparatus for deploying interceptor elements from a spin stabilized rocket |
-
1999
- 1999-03-08 DE DE19910074A patent/DE19910074B4/de not_active Expired - Fee Related
- 1999-12-10 DE DE59911601T patent/DE59911601D1/de not_active Expired - Lifetime
- 1999-12-10 AT AT99124646T patent/ATE289054T1/de not_active IP Right Cessation
- 1999-12-10 EP EP99124646A patent/EP1035401B1/fr not_active Expired - Lifetime
-
2000
- 2000-03-08 US US09/521,414 patent/US6659012B1/en not_active Expired - Fee Related
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0588015A1 (fr) | 1992-09-15 | 1994-03-23 | Buck Werke GmbH & Co | Méthode et matériaux de camouflage et son application |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2011101692A1 (fr) * | 2010-02-17 | 2011-08-25 | Wallop Defence Systems Limited | Cartouche de contre-mesure à air |
WO2013178712A1 (fr) * | 2012-05-29 | 2013-12-05 | Rheinmetall Waffe Munition Gmbh, Patente | Munition comprenant des moyens actifs |
WO2013178607A1 (fr) * | 2012-05-29 | 2013-12-05 | Rheinmetall Waffe Munition Gmbh, Patente | Munition à moyens actifs |
Also Published As
Publication number | Publication date |
---|---|
ATE289054T1 (de) | 2005-02-15 |
EP1035401A3 (fr) | 2001-10-17 |
US6659012B1 (en) | 2003-12-09 |
EP1035401B1 (fr) | 2005-02-09 |
DE59911601D1 (de) | 2005-03-17 |
DE19910074A1 (de) | 2000-09-21 |
DE19910074B4 (de) | 2005-02-10 |
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