EP3523595B1 - Granatenhaltevorrichtung und fach zur aufnahme solch einer vorrichtung - Google Patents

Granatenhaltevorrichtung und fach zur aufnahme solch einer vorrichtung Download PDF

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Publication number
EP3523595B1
EP3523595B1 EP17794360.2A EP17794360A EP3523595B1 EP 3523595 B1 EP3523595 B1 EP 3523595B1 EP 17794360 A EP17794360 A EP 17794360A EP 3523595 B1 EP3523595 B1 EP 3523595B1
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EP
European Patent Office
Prior art keywords
shell
rack
intended
lever
chocking
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.)
Active
Application number
EP17794360.2A
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English (en)
French (fr)
Other versions
EP3523595A1 (de
EP3523595B8 (de
Inventor
Christophe Jamet
Philippe Grelat
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nexter Systems SA
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Nexter Systems SA
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Publication date
Application filed by Nexter Systems SA filed Critical Nexter Systems SA
Publication of EP3523595A1 publication Critical patent/EP3523595A1/de
Publication of EP3523595B1 publication Critical patent/EP3523595B1/de
Application granted granted Critical
Publication of EP3523595B8 publication Critical patent/EP3523595B8/de
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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
    • F41A9/61—Magazines
    • F41A9/64—Magazines for unbelted ammunition
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B39/00—Packaging or storage of ammunition or explosive charges; Safety features thereof; Cartridge belts or bags
    • F42B39/28—Ammunition racks, e.g. in vehicles

Definitions

  • the technical field of the invention is that of wedging devices for shells as well as racks with propellant charges.
  • each locker can receive a case or packaging of loads.
  • the shells are also placed in other lockers of a shell magazine.
  • the dimensions of the boxes receiving the shells are smaller than those of the boxes receiving the cases for propellant charges.
  • the patent DE19529914 thus describes a shell magazine and means facilitating the withdrawal of shells from the magazine.
  • These means comprise a drawer which can slide in grooves of the store by means of rollers.
  • the racks of such a store have small dimensions, slightly greater than the diameter of the shell.
  • Such a compartment cannot carry propellant charges whose dimensions, whatever the caliber, always have a diameter much greater than the caliber of the shell.
  • the patent DE2620930 also discloses a store comprising an upper floor made up of charge lockers and a lower floor made up of shell lockers. As in the patent DE19529914 , each shell locker is equipped with a drawer allowing the extraction of the shell
  • the shells are mobile and collide with the walls of the cargo lockers, which can cause damage to the locker but also to the shell and its rocket.
  • the invention proposes to solve this wedging problem by proposing shells wedging devices and load boxes capable of receiving such wedging devices according to the invention.
  • the invention relates to a device for horizontal wedging for a shell intended to be positioned in a propellant charge rack, device comprising a bucket intended to be placed in the rack, the bucket comprising support surfaces intended to support the shell and bearing surfaces comprising uprights intended to be in contact with the side walls of the locker so as to prevent any transverse movement of the device relative to the locker, the support surfaces being moreover arranged in the locker so as to position the longitudinal axis of the shell at a distance R from an upper part of the compartment substantially equal to the radius of the shell so as to prevent upward transverse movements of the shell, device comprising a means for longitudinal locking of the shell 'shell capable of pivoting between a blocking position where it rests on the warhead of the shell and an open position where it is at a distance from the shell, the trough comprising a means of 'stop intended to cooperate with a stop interface integral with the locker.
  • the support surfaces form an angle relative to one another and are able to each be tangent with a separate generator of the shell.
  • the support surfaces form a semi-cylindrical profile intended to correspond with a profile of the shell.
  • the bearing surfaces comprise an antifriction coating so as to allow easy sliding of the shell.
  • the locking means comprises a lever, a first end of which comprises a fork bearing on the ogive at at least two diametrically opposed points thereof when the locking means is in the locking position.
  • the device comprises a lock capable of locking the lever in the blocked position.
  • the second end of the lever is oriented towards the bottom of the device and comprises a pivot axis transverse to the device.
  • the center of gravity of the lever is offset relative to a vertical plane passing through the pivot axis of the lever so as to make it possible to cause the lever to pivot by gravity.
  • the bucket comprises a stopper intended to interfere with the rear of the shell.
  • the invention also relates to a propellant charge container comprising at least one propellant charge box intended to receive a shells wedging device, container characterized in that each box comprises at least one stop interface intended to cooperate with a stop means carried by the bucket so as to prevent the longitudinal translation of the wedging device relative to the rack.
  • the stop interface may include at least one cylindrical boss integral with a side wall of the rack.
  • a wedging device 1 according to the invention comprises a bucket 2 intended to carry a shell 100.
  • This bucket 2 is made for example of folded sheet metal, and it has an M-shaped profile (the M-shaped profile is best seen figure 4 ), profile which extends substantially over the entire length of shell 100.
  • Support surfaces 3 receive the shell 100 to support it and wedge it laterally forming a V under the shell 100. These support surfaces 3 thus form an angle relative to one another and are able to be tangent. each with a generator separate from the shell 100 (tangents T visible at the figure 4 ).
  • the support surfaces 3 are covered with an anti-friction coating which may include, for example, high density polytetrafluoroethylene plates in order to allow easy longitudinal manipulation (introduction / extraction) of the shell 100 by the user.
  • the wedging device 1 comprises bearing surfaces 4 comprising vertical uprights 4 extending over the entire length of the bucket 2.
  • the bearing surfaces 4 are intended to interfere with their flat lateral parts (branches of the M). and vertical and by their lower edge with the walls of a rack as we will see later on figure 4 .
  • the front part AV of the device 1 comprises a locking means 5, intended to prevent the translation of the shell 100 towards the front AV of the device 1.
  • the locking means 5 visible at the figure 1 has a lever 6.
  • the lever 6 comprises at its first end a fork 7 able to correspond with the ogive of the shell 100 providing a semi-circular bearing area offering at least two support points diametrically opposed relative to the longitudinal axis 101 of shell 100.
  • the locking means 5 may be located at a reduced distance D from the warhead ( figure 2 ), the main thing being that it can stop the shell 100 during a possible longitudinal translation of the latter without resting on the rocket 200 of the shell 100.
  • the second end of the lever 6 comprises a pivot link 8 allowing the locking means 5 to pivot between a locked position and an open position.
  • the open position shown in figure 3 , enables the locking means 5 to be released from the longitudinal trajectory of the shell 100 sliding on the support surfaces 3.
  • a locking button 9 forming a stop makes it possible to lock the locking means 5 in the locking position.
  • the lever 6 comprises a weight 10 which shifts the center of gravity of the lever by a vertical plane passing through the axis of the pivot link 8, thus producing a pivoting torque.
  • the lever 5 could not include a weight 10. It will then be necessary to manually tilt the lever 6 in order to extract the shell.
  • the bucket 2 may include a stopper 12 intended to interfere with the rear face of the shell 100 ( figure 1 ).
  • a container 15 or store 15 of charges comprises compartments 11 with contiguous propellant charges.
  • each load bin 11 can contain a device 1 according to the invention.
  • the vertical uprights 4 form bearing surfaces 4 which interfere laterally with the side walls 16 of the load compartment 11. The edge of each of these uprights 4 rests on the lower wall of the bin 11. In this way, the vertical uprights 4 prevent any transverse or horizontal translations of the bucket 2 (arrow H) and any movement of the bucket 2 downward relative to the bin 11 (arrow V).
  • the person skilled in the art will dimension the bearing surfaces 4 and the bearing surfaces 3 so as to position the longitudinal axis of the shell 100 at a distance R from the wall upper compartment 11, distance R which is substantially equal to the maximum radius R of shell 100, so as to prevent vertical upward movements of shell 100.
  • the wedging device 1 makes it possible to compensate for the excessive space offered by the rack 11 alone and it radially blocks the shell 100.
  • a load compartment 11 in the upper part of the container 15 is occupied by a propellant charge 20 contained in its packaging 21.
  • This type of packaging 21 of octagonal section holds the load 20 vertically and horizontally by resting on its upper and lower faces and sideways, on the walls of the compartment 11. It is thus clearly visible that a shell 100 has a diameter D which is clearly less than the width L and the height of a load packaging 21 and therefore requires suitable wedging which is produced by a wedging device according to the invention.
  • the person skilled in the art will position the locking means 5 longitudinally so that the rear face of the shell 100 rests on the bottom of the box 11. It is then the bottom of the box which will limit the longitudinal translation towards the back of the shell in the locker.
  • the device 1 comprises a stop means 13 (here a notch), visible at the bottom. figure 2 which is intended to correspond with a stop interface 14 of the locker 11 visible at the figure 4 (here a boss 14).
  • each upright 4 therefore comprises at its lower edge a notch 13 able to correspond with a cylindrical boss 14 integral with each side wall 16 of the rack 11 by screwing, which has the effect of blocking the translation of the device.
  • the bucket 2 may have a semi-cylindrical shape which will receive the shell at its part of larger diameter.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Details Of Rigid Or Semi-Rigid Containers (AREA)
  • Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
  • Cage And Drive Apparatuses For Elevators (AREA)
  • Laying Of Electric Cables Or Lines Outside (AREA)
  • Warehouses Or Storage Devices (AREA)
  • Packaging Of Machine Parts And Wound Products (AREA)

Claims (11)

  1. Horizontal-Haltevorrichtung (1) für eine Granate (100), die zur Positionierung in einem Treibladungsfach (11) bestimmt ist, dadurch gekennzeichnet, dass die Vorrichtung (1) eine Mulde (2) aufweist, die zum Platzieren in dem Fach (11) bestimmt ist, wobei die Mulde (2) Stützflächen (3) aufweist, die zum Stützen der Granate (100) bestimmt sind, und Auflageflächen (4), die Pfosten aufweisen, die bestimmt sind, mit Seitenwänden des Fachs (11) derart im Kontakt zu sein, dass jedwede transversale Bewegung der Vorrichtung (1) relativ zum Fach (11) untersagt ist, wobei die Stützflächen (3) im Übrigen derart in dem Fach (11) angeordnet sind, dass die Längsachse der Granate (100) in einem Abstand R von einem oberen Teil des Fachs (11) positioniert ist, der etwa dem Radius R der Granate (100) entspricht, so dass die aufsteigenden transversalen Bewegungen der Granate (100) untersagt werden, wobei die Vorrichtung (1) ein Längsblockademittel (5) der Granate (100) aufweist, das imstande ist, zwischen einer Blockadeposition, in der es sich auf dem Sprengkopf der Granate (100) abstützt, und einer offenen Position, in der es von der Granate (100) beabstandet ist, zu schwenken, wobei die Mulde (2) ein Arretierungsmittel (13) aufweist, das zum Zusammenwirken mit einer mit dem Fach (11) fest verbundenen Arretierungsschnittstelle (14) bestimmt ist.
  2. Haltevorrichtung (1) nach Anspruch 1, dadurch gekennzeichnet, dass die Stützflächen (3) einen relativen Winkel zueinander bilden und imstande sind, mit einer Mantellinie, die sich von der Granate (100) unterscheidet, jeweils tangential (T) zu sein.
  3. Haltevorrichtung (1) nach Anspruch 1, dadurch gekennzeichnet, dass die Stützflächen (3) ein halbzylindrisches Profil bilden, das bestimmt ist, mit einem Profil der Granate (100) übereinzustimmen.
  4. Haltevorrichtung (1) nach einem der Ansprüche 1 bis 3, dadurch gekennzeichnet, dass die Stützflächen (3) eine reibungsmindernde Beschichtung aufweisen, so dass das mühelose Gleiten der Granate (100) erlaubt ist.
  5. Haltevorrichtung (1) nach einem der Ansprüche 1 bis 4, dadurch gekennzeichnet, dass das Blockademittel (5) einen Hebel (6) aufweist, von dem ein erstes Ende (7) eine Gabel (7) aufweist, die sich auf dem Sprengkopf an mindestens zwei diametral gegenüberliegenden Punkten desselben abstützt, wenn das Blockademittel (5) in Blockadeposition ist.
  6. Haltevorrichtung (1) nach Anspruch 5, dadurch gekennzeichnet, dass sie einen Riegel (9) aufweist, der imstande ist, den Hebel (6) in Blockadeposition zu verriegeln.
  7. Haltevorrichtung (1) nach einem der Ansprüche 5 oder 6, dadurch gekennzeichnet, dass das zweite Ende des Hebels (7) zum unteren Teil der Vorrichtung (1) zeigt und eine zur Vorrichtung (1) transversale Schwenkachse (8) aufweist.
  8. Haltevorrichtung (1) nach Anspruch 7, dadurch gekennzeichnet, dass das Schwerkraftzentrum des Hebels (6) in Bezug auf eine vertikale Ebene, die durch die Schwenkachse (8) des Hebels (6) verläuft, derart versetzt ist, dass das Verursachen eines Schwenkens des Hebels (6) durch Schwerkraft erlaubt ist.
  9. Haltevorrichtung (1) nach einem der vorangehenden Ansprüche, dadurch gekennzeichnet, dass die Mulde (2) einen Feststeller (12) aufweist, der zum Interagieren mit dem Heck der Granate (100) bestimmt ist.
  10. Treibladungsbehälter (15), aufweisend mindestens ein Ladungsfach (11), das zur Aufnahme einer Haltevorrichtung (1) einer Granate (100) nach einem der vorangehenden Ansprüche bestimmt ist, wobei der Behälter (15) dadurch gekennzeichnet ist, dass jedes Fach (11) mindestens eine Arretierungsschnittstelle (14) aufweist, die zum Zusammenwirken mit einem von der Mulde (2) getragenen Arretierungsmittel (13) bestimmt ist, so dass die Längsverlagerung der Haltevorrichtung (1) relativ zum Fach (11) verhindert wird.
  11. Ladungsbehälter (15) nach Anspruch 10, dadurch gekennzeichnet, dass die Arretierungsschnittstelle (14) mindestens einen zylindrischen Vorsprung (14) aufweist, der mit einer Seitenwand (16) des Fachs (11) fest verbunden ist.
EP17794360.2A 2016-10-04 2017-10-02 Granatenhaltevorrichtung und fach zur aufnahme solch einer vorrichtung Active EP3523595B8 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1601441A FR3057058B1 (fr) 2016-10-04 2016-10-04 Dispositif de calage pour obus et casier apte a accueillir un tel dispositif
PCT/FR2017/052697 WO2018065713A1 (fr) 2016-10-04 2017-10-02 Dispositif de calage pour obus et casier a charges propulsives apte a accueillir un tel dispositif

Publications (3)

Publication Number Publication Date
EP3523595A1 EP3523595A1 (de) 2019-08-14
EP3523595B1 true EP3523595B1 (de) 2020-11-25
EP3523595B8 EP3523595B8 (de) 2021-01-20

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EP17794360.2A Active EP3523595B8 (de) 2016-10-04 2017-10-02 Granatenhaltevorrichtung und fach zur aufnahme solch einer vorrichtung

Country Status (7)

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EP (1) EP3523595B8 (de)
KR (1) KR102241343B1 (de)
DK (1) DK3523595T3 (de)
ES (1) ES2855028T3 (de)
FR (1) FR3057058B1 (de)
IL (1) IL265765B (de)
WO (1) WO2018065713A1 (de)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110160416B (zh) * 2018-04-16 2022-04-12 北京机电工程研究所 托弹架拆卸装置及技术准备车
CN113357978B (zh) * 2021-06-04 2023-01-06 西安昆仑工业装备配套有限公司 密封式快速装取弹丸的包装筒及包装组件

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2620930A1 (de) * 1976-05-12 1977-11-24 Kern & Grosskinsky Magazin bzw. halterung fuer laengliche behaelter, insbesondere geschosskoerper und treibladungsbehaelter
DE19529914C2 (de) * 1994-11-29 2002-07-11 Rheinmetall Landsysteme Gmbh Munitionsmagazin
FR2869681B1 (fr) * 2004-04-29 2006-07-28 Giat Ind Sa Dispositif de separation de modules de charge propulsive

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* Cited by examiner, † Cited by third party
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Also Published As

Publication number Publication date
EP3523595A1 (de) 2019-08-14
ES2855028T3 (es) 2021-09-23
KR20190072538A (ko) 2019-06-25
WO2018065713A1 (fr) 2018-04-12
FR3057058B1 (fr) 2019-03-29
DK3523595T3 (da) 2021-03-01
EP3523595B8 (de) 2021-01-20
KR102241343B1 (ko) 2021-04-16
IL265765A (en) 2019-06-30
IL265765B (en) 2022-02-01
FR3057058A1 (fr) 2018-04-06

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