WO2005116564A1 - Einrichtung zur zuführung von treibladungen zu einer schweren waffe - Google Patents
Einrichtung zur zuführung von treibladungen zu einer schweren waffe Download PDFInfo
- Publication number
- WO2005116564A1 WO2005116564A1 PCT/DE2005/000888 DE2005000888W WO2005116564A1 WO 2005116564 A1 WO2005116564 A1 WO 2005116564A1 DE 2005000888 W DE2005000888 W DE 2005000888W WO 2005116564 A1 WO2005116564 A1 WO 2005116564A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- propellant charge
- propellant
- modules
- magazine
- chain
- Prior art date
Links
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
- F41A9/00—Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
- F41A9/01—Feeding of unbelted ammunition
- F41A9/06—Feeding of unbelted ammunition using cyclically moving conveyors, i.e. conveyors having ammunition pusher or carrier elements which are emptied or disengaged from the ammunition during the return stroke
- F41A9/09—Movable ammunition carriers or loading trays, e.g. for feeding from magazines
- F41A9/10—Movable ammunition carriers or loading trays, e.g. for feeding from magazines pivoting or swinging
- F41A9/13—Movable ammunition carriers or loading trays, e.g. for feeding from magazines pivoting or swinging in a vertical plane
- F41A9/14—Movable ammunition carriers or loading trays, e.g. for feeding from magazines pivoting or swinging in a vertical plane which is transverse to the barrel axis
-
- 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
- F41A9/00—Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
- F41A9/37—Feeding two or more kinds of ammunition to the same gun; Feeding from two sides
- F41A9/375—Feeding propellant charges and projectiles as separate units
-
- 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
- F41A9/00—Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
- F41A9/61—Magazines
- F41A9/64—Magazines for unbelted ammunition
- F41A9/76—Magazines having an endless-chain conveyor
Definitions
- the invention relates to a device for supplying propellant charges to a heavy weapon with at least one propellant charge magazine and a propellant charge supply device, by means of which the propellant charges are removed from the propellant charge magazine and transferred to a propellant charge transfer arm which has a propellant charge supply shell with a propellant charge adapter which can be pivoted into the area behind the weapon ,
- a device for supplying propellant charges to a heavy weapon with at least one propellant charge magazine and a propellant charge supply device, by means of which the propellant charges are removed from the propellant charge magazine and transferred to a propellant charge transfer arm which has a propellant charge supply shell with a propellant charge adapter which can be pivoted into the area behind the weapon ,
- a propellant charge transfer arm which has a propellant charge supply shell with a propellant charge adapter which can be pivoted into the area behind the weapon ,
- Such a device is basically known and described for example in DE 102 58 263.7 AI.
- the invention has for its object to provide a device with the features specified in the preamble of claim 1, which is as compact as possible, so that the often limited interior space inside a tank tower or the turret housing of a shooting module is installed as little as possible and yet the fully automatic feeding of the propellant charges from the propellant charge magazine to the weapon is ensured.
- the device should also be constructed in such a way that it is possible to arrange the propellant charge magazine and at least parts of the propellant charge supply device within an additional housing, which can be arranged on the outer wall of a tower housing in a removable or pivotable manner.
- a basic idea of the invention is to design one or more propellant charge magazines as fixedly arranged magazines, in which the propellant charges are mounted in guides with horizontally oriented longitudinal axes, with several propellant charge modules being arranged axially one behind the other in each guide.
- the guides are arranged parallel to each other and one above the other in horizontal planes.
- an automatic propellant charge is arranged with a propellant charge chain encircling in a vertical plane, on which receptacle elements are arranged, the arrangement of the guides of the propellant charge magazine and the receptacle elements of the propellant charge machine being such that the receptacle elements in a position can be brought in which they are aligned with the guides so that the propellant charge modules can be transferred from the guides of the propellant charge magazine into the receiving elements of the propellant charge chain.
- a portioning unit with means for transferring and joining a predetermined number of propellant charge modules from the receiving element into the portioning unit is provided axially to the uppermost receiving element of the automatic propellant charge. The joined propellant charge modules are then fed from the portioning unit to the propellant charge supply shell on the propellant charge transfer arm.
- FIG. 1 is an isometric illustration of a propellant charge magazine with a propellant charge supply device consisting of an automatic propellant charge and a portioning unit;
- Fig. 2 is a side view of the device of Fig. 1;
- FIGS. 1 and 2A shows an individual illustration of an pick-up tube of the propellant charge magazine and a pick-up element of the propellant charge automat according to FIGS. 1 and 2 in an isometric illustration
- FIG. 3A shows an individual representation of the automatic propellant charge according to FIGS. 1 and 2 in an isometric representation
- 3B and 3C individual representations of receiving elements of the automatic propellant charge according to FIG. 3A;
- FIG. 6 is an isometric illustration of a shooting module with an additional housing which can be pivoted away from the tower housing to accommodate a device for supplying propellant charges to a heavy weapon.
- the propellant charge magazine 2 is designed as a fixedly arranged magazine in which propellant charge modules TM are mounted in guides 2.1 in such a way that their longitudinal axes run horizontally.
- the guides 2.1 are designed as receiving tubes which are shown with a partially cut lateral surface for a clearer illustration.
- other guides for example mounting rails, can also be used at this point.
- a predetermined number of guides 2.1 are arranged parallel to one another and one above the other in horizontal planes.
- an automatic propellant charge 3 is arranged with a propellant charge chain 3.1 rotating in a vertical plane and driven by a motor 3.11, with receiving elements 3.2 for receiving one or two propellant charge modules TM depending on the axial length.
- the transfer of propellant charge modules TM from the receptacle tubes 2.1 into the receptacle elements 3.2 of the automatic propellant charge 3 can, if the receptacle elements are aligned with the receptacle tubes, by supplying excess air pressure via lines 2.2. During loading, air underpressure can be supplied via these lines to feed the propellant charge modules into the receiving tubes 2.1.
- the supply and discharge of propellant charge modules can be carried out in a manner not shown by drivers guided on spindles or rotating chains.
- Locking pawls can also be arranged on the guides 2.1 of the propellant charge magazine 2 in a manner also not shown.
- the receiving elements 3.2 of the propellant charge chain 3.1 are designed as open shells, and each chain link has, in the area of the two ends of a shell, a circular ring section 3.31 and 3.32 which is in contact with one another and is connected at the point of contact
- Bracket on The arrangement is such that one circular ring section 3.31 comprises the shell 3.2 of this chain link on the closed side and the other circular ring section 3.32 comprises the shell of an adjacent chain link on the open side.
- Each bracket is constructed so that the openings of the circular ring sections 3.31 and 3.32 are at an angle of 90 ° to one another, and the holding brackets are arranged and guided in the propellant charge chain 3.1 such that the receiving element 3.2 standing in the removal position at the upper end of the propellant charge chain 3.1 is in the axial direction extending open lead-through area, through which a transfer element 6 designed as a gripping hook and displaceable in the axial direction can be passed such that the propellant charge modules contained in this pick-up element are transferred to a portioning unit 5 arranged above the propellant charge magazine 2 and are joined there.
- the shells on the closed side and on the open side are completely encompassed by the interacting circular ring sections 3.31 and 3.32 of two holding brackets.
- Sensor elements for determining the type of module and the degree of filling are arranged on each receiving element of the propellant charge chain 3.1.
- the sensor elements are designed as spring strips 3.41 to 3.43 guided around the circumference of the shells 3.2, with a scanning element projecting through an opening in the shell, and each spring strip
- 3.41 to 3.43 is assigned a proximity sensor or switch 3.51 to 3.53 on its outside, which is opposite the spring strip.
- three spring strips 3.41 to 3.43 are arranged on each shell at a predetermined axial distance.
- the length of the shells 3.2 is dimensioned such that either two axially successive standard modules TM 1 (FIG. 3B) or a somewhat longer basic module TM 2 (FIG. 3C) can be accommodated, in which case the sensor elements determine exactly can be what type and what number of propellant charge modules are contained in the shell.
- some or all of the spring strips 3.41 to 3.43 are pressed out in the direction of the proximity switches 3.51 to 3.53.
- the propellant charge chain 3.1 is driven by the drive motor 3.11 via a chain wheel 3.12. The deflection takes place in the upper area via a pinion 3.13. In the area of the removal position, further sensors for checking the transfer of the propellant charge modules from the receiving element 3.2 of the propellant charge chain 3.1 into the portioning unit 5 can be arranged.
- the portioning unit 5 has a receiving shell arranged axially to the receiving element 3.2 of the propellant charge chain 3.1 in the removal position, divided in the axial direction, with a large shell portion 5.1, which has a stop 5.3 for the propellant charge modules at the end facing away from the propellant charge chain 3.1, and a small shell portion 5.2 for lateral support of the propellant charge modules.
- the large shell part 5.1 can be pivoted from a receiving position into a delivery position for transferring the joined propellant charge modules TM to a propellant charge supply shell.
- the stop 5.3 arranged at the end of the positioning unit 5 ensures that the propellant charge modules transferred from the gripping hook 6 into the portioning unit 5 are joined there before they are released.
- Fig. 6 shows how the device described above can be arranged on the tower housing of a shooting module.
- Fig. 6 shows a shooting module with an armored turret housing 1, in which a heavy weapon W is pivotally mounted in elevation in a manner not shown, about a shield pin.
- the tower housing 1 can be rotatably supported in azimuth on a support structure, which can be designed, for example, as a chassis of a self-propelled howitzer or as a main battle tank.
- the turret housing contains, in a manner that is not specifically shown and known, at least one projectile magazine from which projectiles are supplied to the weapon W by means of a fully automatic projectile supply device known per se.
- an additional housing 4 is fastened on an outer wall 1.1, which is arranged within a recessed area 1.3 of the contour of the tower housing 1, so that it can pivot about a vertical axis such that, as can also be seen in FIG. 6, the additional housing 4 is made of one can be moved to the tower housing close position in a pivoted outward position.
- the propellant charge magazine 2 and the propellant charge machine 3, with which the propellant charges are removed from the propellant charge magazine 2 and fed to the portioning unit 5, are arranged within the additional housing 4.
- the additional housing 4 has, on the side facing the tower housing 1, a passage opening (not visible in FIG. 1), which is opposite a correspondingly designed passage opening 1.2 in the outer wall 1.1 of the tower housing 1.
- the propellant charge is ejected through the through openings in the additional housing 4 and in the outer wall 1.1 of the tower housing 1.
- the propellant charge is then received within the turret housing 1 by the propellant charge feed shell, which, not shown in FIG. 6, is arranged on the propellant charge transfer arm arranged in the turret housing 1 and can be pivoted into the area behind the weapon W, so that it can be pivoted by means of a at her arranged propellant charge gun can be supplied.
- a propellant charge magazine 2 which has an automatic propellant charge 3 on one end face.
- a propellant charge magazine can be arranged on both sides of the automatic propellant charge, and the portioning unit can be arranged above one of the two propellant charge magazines.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Elimination Of Static Electricity (AREA)
- Warehouses Or Storage Devices (AREA)
- Cosmetics (AREA)
- Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
- Toys (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)
Abstract
Description
Claims
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/597,088 US7475626B2 (en) | 2004-05-26 | 2005-05-14 | Device for feeding propellant charges to a heavy weapon |
CA002567774A CA2567774C (en) | 2004-05-26 | 2005-05-14 | Device for feeding propellant charges to a heavy weapon |
EP05754726A EP1721114B1 (de) | 2004-05-26 | 2005-05-14 | Einrichtung zur zuführung von treibladungen zu einer schweren waffe |
DE502005001021T DE502005001021D1 (de) | 2004-05-26 | 2005-05-14 | Einrichtung zur zuführung von treibladungen zu einer schweren waffe |
IL179556A IL179556A (en) | 2004-05-26 | 2006-11-23 | Device for feeding propelling charges to a heavy weapon |
NO20065698A NO334270B1 (no) | 2004-05-26 | 2006-12-11 | Anordning for tilførsel av drivladninger til et tungt våpen |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102004025742.6 | 2004-05-26 | ||
DE102004025742A DE102004025742A1 (de) | 2004-05-26 | 2004-05-26 | Einrichtung zur Zuführung von Treibladungen zu einer schweren Waffe |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2005116564A1 true WO2005116564A1 (de) | 2005-12-08 |
Family
ID=34971278
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/DE2005/000888 WO2005116564A1 (de) | 2004-05-26 | 2005-05-14 | Einrichtung zur zuführung von treibladungen zu einer schweren waffe |
Country Status (9)
Country | Link |
---|---|
US (1) | US7475626B2 (de) |
EP (1) | EP1721114B1 (de) |
AT (1) | ATE366909T1 (de) |
CA (1) | CA2567774C (de) |
DE (2) | DE102004025742A1 (de) |
ES (1) | ES2289714T3 (de) |
IL (1) | IL179556A (de) |
NO (1) | NO334270B1 (de) |
WO (1) | WO2005116564A1 (de) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8596184B2 (en) | 2009-10-21 | 2013-12-03 | Bae Systems Bofors Ab | Automatic charge magazine |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102004024302B4 (de) * | 2004-05-15 | 2008-04-10 | Kraus-Maffei Wegmann Gmbh & Co. Kg | Gurtkasten für eine lafettierte Granatmaschinenwaffe |
DE102005040407B4 (de) * | 2005-08-26 | 2007-05-16 | Rheinmetall Waffe Munition | Vorrichtung zur Identifizierung des Munitionstyps einer Munition |
IT1404036B1 (it) * | 2010-12-17 | 2013-11-08 | Oto Melara Spa | Veicolo armato con struttura migliorata. |
KR101974079B1 (ko) * | 2014-10-28 | 2019-04-30 | 한화디펜스 주식회사 | 장약 공급 장치 |
DE102022101213B3 (de) | 2022-01-19 | 2023-06-15 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Magazin |
DE102022101219A1 (de) | 2022-01-19 | 2023-07-20 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Verfahren zur Handhabung von Treibladungsmodulen |
DE102022101215A1 (de) | 2022-01-19 | 2023-07-20 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Portioniervorrichtung |
DE102022101216B3 (de) * | 2022-01-19 | 2023-04-27 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Vorrichtung zur Überführung von Treibladungsmodulen, Überführungsbaugruppe mit mindestens zwei Überführungsvorrichtungen, Magazin zur Aufnahme mehrerer Treibladungsmodule und/oder Treibladungsstangen und Verfahren zur Überführung von Treibladungsmodulen und/oder Treibladungsstangen |
EP4215865A1 (de) | 2022-01-19 | 2023-07-26 | Krauss-Maffei Wegmann GmbH & Co. KG | Magazin |
Citations (4)
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EP0493918A2 (de) * | 1990-12-24 | 1992-07-08 | General Electric Company | Magazin und Förderband |
DE4131280A1 (de) * | 1991-09-20 | 1993-03-25 | Wegmann & Co Gmbh | Kampfpanzerturm |
DE4134603A1 (de) * | 1991-10-19 | 1993-04-22 | Rheinmetall Gmbh | Geschuetzturm |
DE10258263A1 (de) | 2002-12-13 | 2004-07-08 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Schießmodul |
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GB1283737A (en) | 1968-09-04 | 1972-08-02 | Nat Distillers Chem Corp | Method of catalyst preparation |
CA1002508A (en) | 1972-11-30 | 1976-12-28 | Takashi Ohara | Method for the production of noble metal catalysts |
US4418607A (en) * | 1977-04-21 | 1983-12-06 | Hughes Helicopters, Inc. | Single barrel externally powdered gun |
DE3931059A1 (de) * | 1989-09-18 | 1991-03-28 | Rheinmetall Gmbh | Treibladungs-portionierer fuer eine mengenvariabel beladbare ladeschale |
DE3932130A1 (de) * | 1989-09-27 | 1991-04-04 | Rheinmetall Gmbh | Ladevorrichtung fuer modulare treibladung |
US5170006A (en) * | 1990-12-24 | 1992-12-08 | General Electric Co. | Propellant magazine for field artillery piece |
FR2682750A1 (fr) * | 1991-10-17 | 1993-04-23 | Giat Ind Sa | Magasin de munitions, en particulier pour char. |
AU668645B2 (en) | 1992-11-12 | 1996-05-09 | Uop | Multimetallic and multigradient reforming catalyst for converting paraffins to aromatics |
FR2702551B1 (fr) * | 1993-03-12 | 1995-05-12 | Giat Ind Sa | Système de stockage et d'alimentation de charges propulsives destinées à être introduites dans la chambre du canon d'une arme de moyen ou de gros calibre d'un véhicule blindé. |
US5456154A (en) * | 1994-03-29 | 1995-10-10 | Western Design Corporation | Compact bustle magazine |
SE503841C2 (sv) * | 1994-09-07 | 1996-09-16 | Bofors Ab | Laddsystem |
DE4443701C1 (de) | 1994-12-08 | 1996-08-29 | Degussa | Schalenkatalysator, Verfahren zu seiner Herstellung und seine Verwendung |
FR2743411B1 (fr) * | 1996-01-05 | 1998-02-27 | Giat Ind Sa | Dispositif de transfert de modules constituant des charges propulsives, entre un magasin de stockage et un systeme de chargement de ces modules dans la chambre d'un canon d'artillerie |
SE507659C2 (sv) * | 1996-12-02 | 1998-06-29 | Bofors Ab | Sätt och anordning för att vid artilleripjäser hantera drivkrutladdningar av olika storlek och laddstyrka |
FR2764055B1 (fr) * | 1997-05-29 | 1999-07-16 | Giat Ind Sa | Systeme de saisie automatique de modules de charge propulsive stockes dans un magasin |
DE19734975A1 (de) | 1997-08-13 | 1999-03-11 | Hoechst Ag | Schalenkatalysator, Verfahren zu dessen Herstellung sowie Verwendung, insbesondere zur Gasphasenoxidation von Ethylen und Essigsäure zu Vinylacetat |
US6073534A (en) * | 1998-01-14 | 2000-06-13 | General Dynamics Armament Systems, Inc. | Transfer mechanism and method for uploading and downloading propellant charges and projectiles |
FR2778235B1 (fr) * | 1998-04-30 | 2000-06-02 | Giat Ind Sa | Dispositif d'alimentation d'un canon d'artillerie en elements de munition |
SE9801601L (sv) * | 1998-05-08 | 1999-06-07 | Bofors Ab | Anordning för hantering av drivkrutladdningar vid hel- och halvautomatiska laddsystem för artilleripjäser |
FR2825144B1 (fr) * | 2001-05-28 | 2003-09-05 | Giat Ind Sa | Magasin de stockage pour modules de charge propulsive |
-
2004
- 2004-05-26 DE DE102004025742A patent/DE102004025742A1/de not_active Withdrawn
-
2005
- 2005-05-14 WO PCT/DE2005/000888 patent/WO2005116564A1/de active IP Right Grant
- 2005-05-14 ES ES05754726T patent/ES2289714T3/es active Active
- 2005-05-14 US US11/597,088 patent/US7475626B2/en not_active Expired - Fee Related
- 2005-05-14 EP EP05754726A patent/EP1721114B1/de active Active
- 2005-05-14 DE DE502005001021T patent/DE502005001021D1/de active Active
- 2005-05-14 AT AT05754726T patent/ATE366909T1/de not_active IP Right Cessation
- 2005-05-14 CA CA002567774A patent/CA2567774C/en not_active Expired - Fee Related
-
2006
- 2006-11-23 IL IL179556A patent/IL179556A/en not_active IP Right Cessation
- 2006-12-11 NO NO20065698A patent/NO334270B1/no not_active IP Right Cessation
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
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EP0493918A2 (de) * | 1990-12-24 | 1992-07-08 | General Electric Company | Magazin und Förderband |
DE4131280A1 (de) * | 1991-09-20 | 1993-03-25 | Wegmann & Co Gmbh | Kampfpanzerturm |
DE4134603A1 (de) * | 1991-10-19 | 1993-04-22 | Rheinmetall Gmbh | Geschuetzturm |
DE10258263A1 (de) | 2002-12-13 | 2004-07-08 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Schießmodul |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8596184B2 (en) | 2009-10-21 | 2013-12-03 | Bae Systems Bofors Ab | Automatic charge magazine |
Also Published As
Publication number | Publication date |
---|---|
ES2289714T3 (es) | 2008-02-01 |
IL179556A (en) | 2011-06-30 |
CA2567774A1 (en) | 2005-12-08 |
IL179556A0 (en) | 2007-05-15 |
DE502005001021D1 (de) | 2007-08-23 |
ATE366909T1 (de) | 2007-08-15 |
US7475626B2 (en) | 2009-01-13 |
EP1721114A1 (de) | 2006-11-15 |
DE102004025742A1 (de) | 2005-12-22 |
EP1721114B1 (de) | 2007-07-11 |
CA2567774C (en) | 2009-06-23 |
NO334270B1 (no) | 2014-01-27 |
NO20065698L (no) | 2007-02-23 |
US20080047417A1 (en) | 2008-02-28 |
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