DE1578069B - Feeding device in the form of a magazine drum rotatably arranged inside an armored vehicle for a launching device for missiles with recoil drive - Google Patents

Description

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that the operating personnel open the armored vehicle in opposite directions; the loader therefore needs to exit through the hatches. Since such a diglich the missile handlurig placed on the carrier plate in combat situations certainly leads to death by or launch tubes with their, for example, as the crew and on the other hand, a non-remediation pin formed receiving means in the paralbs of the detected defect to the loss of the Fahr- 5 lel recesses des Kreisririges.der carrier plate stuff and the team, this will roughly align. By closing the shark solution for storing the missiles in the tactical claws, the missile or the shearing requirements are not met; The shot tube is locked in the position that has now been adjusted. ■ object of the invention is, therefore, one for inputs - ¹ Furthermore, it allows formation of the DIE Zubringbau in relatively low on all sides armored io device gemäß.der invention, the space in the interior and NBC weapons protected vehicles suitable supply of ren Armored vehicle optimally: to use, bring device for 'a launcher for without creating the.Accessible missile with recoil drive for the operating personnel ^ the ability to: -; ....: ..:;. ·,

body or ' the ab- 15 The invention is based on hand'.der. subsequent guns are simply designed, an optimal spelling in connection with the drawing closer utilization "and accessibility for the operator explained, on which an" embodiment more or personal of the space available in the vehicle / a less is shown schematically.:. ■ ::.:. ". ■ :: -: · ..;: .1 easy handling as well as an exact allocation- '■ ·' In detail shows ..: /! J. .....; ... ·: .-:

planning the missile with respect to the Aufnahmeör- '20 ■ :. 1 guarantees a longitudinal section through a loading space throughout the launching device. '-' ■ '■'"- a nut partially shown, · sides armored case of a feeding apparatus in the form of a Zubrihgvdrrichtung according to the Neren domestic vehicle; an armored vehicle rotatably Toggle invention, - · · ..... :.: .... '· ... "; ::

The ordered magazine drum of the initially mentioned 'Fig. 2 is a plan view of the feeding device type, this task according to the invention is characterized in accordance with Fig. 1.' ■ -. ■■. . : ..- 0 .. ::; ...:. :: ... ^; . ":. solved that the magazine barrel immediately next to '-"''Although the position of the in-one in.Fig / 1 and 2 only the firing in the retracted state is partially shown, is arranged on all sides armored driving device and on a horizontal Zug 1 mounted missile in adaptation to the carrier plate at the lower end of the magazine drum may be different, hydraulically actuated joints, each 30 is in the embodiment to be described a missile or ", a launch tube partially around a vertical storage the missile ausfassende gone about an axis parallel to the missile axis -... '.::' * ■ '.. axis of rotation of the joints are oppositely pivotable in a so-called battle space 2 of the Fahrzeu-holding claws carry, and saturated at its outer edge 1 based on ari known training areas is provided with a circular ring in which wedge 35 two launching devices 3 and 3 'side by side r ■ shaped, arranged parallel to the axis of rotation of the magazine drum! Each of the recesses on the right and left according to FIG. 2 are arranged, which are located opposite the imaginary longitudinal axis of the vehicle on the missile or, on the launching tube, a connection device is arranged as a magazine drum 5, 6. ^"::. Trained feeding apparatus associated with each 'In such' Zübringvbrrichtung so are the 40 Zubririgvorrichtüng is using, on the one bearing hub 8, paths by which the collated missile or waste of fixed on the vehicle floor 9 Konsoschußrohre ¹ to the Abschußvörrichtung brought up len 10 are held and radial ball bearings 11 are sluggish, must be "rotatably mounted" without the intermediate connection of a loading device and "points" near the vehicle device to an "automatically" executed den9 a horizontally arranged, circular rotary movement "the" Mägäzihtromrhei reduced. After 45 carrier plate 12. On this carrier plate are the removal of a missile or a launcher in the present case eight (see Fig. 2) missile tubes from the magazine barrel through the launcher 13, "which 'also in the packaging-serving device -will through ^; a step-by-step further rotating shot can be ^{found: 14;} They "are also ensured with their hinge of the magazine barrel that longitudinal axes parallel to the vertical axis of rotation of the launching device immediately after each discharge device and - circular; around this - assuming" again ^{: a} missile is assigned, arranged and are held by - "holding claws 15 in their end, the empty Mägaziriplätz in a vertical position! · The holding claws 15 are located far from the shooter and immediately back out! hinges 16 'that can be actuated when filled on missiles are rotatably mounted; Since this type of construction of the sealing element, not shown here, is particularly space-saving, it is also possible for Hälteklaueri when the wing bodies are brought in and out ; "eirie" large number of opened by '.-- ^: " ^: -"-'-:'-'--'—- - ^ ^; · "S -'- jy ^ - · '-' - '.." · ■■■ missiles for the Nächladevorgäng deiÄbschüß ^ - - ^"; Zur- Lägezentrieruhg- the missile or - bereitzühäiten DER down Vörrichtung. ^r "For this purpose" in the ~ -Fähf- schußrohre -in-'Zutiringvorrichtüng are Ausnehzeugihneren, preferably ^: in the direction of travel of the drive-60-effort18-in one on the-TiägeYplatte-12 located "euges ^: seen" ^ behind the Mägäzintrommer more "Ehen circular 19 provided in which the standing in the drift missile are 'stored'. Are "two wedge-shaped noses' 20 of the missile. The missiles and / or directions provided so that a single loading gun can have, in addition to protecting the wedge-shaped nose 20, operate two training devices; the 65 still has a hip! Recess 21, which the axial reloading process will also get it by aligning the missile in the still to be exposed that, through the follow-up peeling gestures! writing launcher 3 is used, ert, the holding claws arranged on the joints' Anr free end of the bearing hubs is a

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via the per se known FoI, not shown here, The mode of action of the above-described

circuit-controlled hydraulic rotary motor 22. Feeding device is the following:
The rotary motor drives the launching device 3 ', for example, in a position not shown here

Instruct the delivery device step by step. Each one of a missile 13 or a: launch tube 14 _: with step here comprises at least three missiles 13, 5 a missile held therein into the launching

The launchers 3 and 3 '(see. Fig. 1) position 4 extended, so is under the control • each consist of a sequential circuit (not shown) lowering in vehicle 1, the feeder right arranged rails 23 running elevator device 6 around a several missiles 24, the closing step, which is not described in detail here, is turned further clockwise, io controlled by the sequence circuit already mentioned. A missile or launch tube is now located Drive means is movable up and down. The elevator is in readiness position again while the loading wagons carries a hydraulically actuated pivot point of the delivery device from which the missile device 28, which was also removed by means of a hydraulic, is now the loader lisch actuated swivel joint 29 with the elevator hoist opposite, and thus the loader a gen is connected. The pivoting device has 15 new launch tube can put on with the hooves two clamp-like retaining claws 31 and 32 (cf. also retaining claws 15 can be locked. ....;:;:

Fig. 3), of which the holding claw 32 around the after the launch of the extended missile

• in the loading position retracted launcher pers. And dropping the launcher tube is under the vertical bearing axis 33 by a hydraulic control of the follow-up peeling the launcher rotary motor 34 is pivotable. The extension and retraction in the direction indicated by dash-dotted lines in FIG. 1 movement of the launcher and the vertical position pivoted and retracted again. The pivoting movement of the holding claw 32 can be controlled by the sequence circuit called the following circuit, which is opened when the launch tube is ejected. The holding claws teklaue 32 and the holding claw 31 are thereby over 31 and 32 are the cross-sectional shape of the missile that is now on the carrier plate 12 of the feeder or adapted to the launch tubes. They have launchers in the loading position in their direction Inner surfaces not shown pressure pieces moved to the pipe; As soon as the launcher has its Recording and has reached a lowest position corresponding to the recess 21 is via the rotary motor Dierendes centering piece, for aligning the missiles 34j of a not shown, with the geper or launch tubes. . : called sequential circuit connected limit switch

The thrust pieces and centering means of the holding 30 can be released, the holding claw 32 in the locked position in the stored position in FIG. moved back and firing device act as shown in Fi g. 2 and 3 at the same time. Holding claws _: 15 of the carrier plate; 12 can be seen with the open in the direction of travel of the vehicle. Thus, a new launch tube or a missile standing in front of the feeder device is verper with the launching device or with its launching tube and 35 and can from this into the launching position in the approximate range of its center of gravity. be moved. Of course, the retaining claws encompass the missile locking device also the electric or launch tube, not shown here, and press with their pressure signal connections between the launching device on the outer wall and the wedge-shaped nose device and launching tube or missile. of the launch tube, so that a 40 and the 'the extension of the. Firing device frictional locking occurs after a possible hatch 44 is opened and closed. γ axial alignment of the missile or the Ab- Since two feeder devices and the associated

Shotguns are provided in the launcher by the renden launchers can. Centering piece 38 has been reached. ,. . - during the remote controlled; Flight. _: a first F, lug-

A second missile is located in the armored body above the loading point in the roof covering 42, one of the ABC levels of a hatch cover 43. Way to be made ready to go. _: . _;
As can be seen from the above, a hatch 44, which can be opened by the mentioned sequential circuit free number - in the present case eight - missiles can be deployed. > ■. - ■■ '■: ■■■ ^■■:;. The delivery device without the help of a loading

. Finally, in the direction of travel of the driver, 50 are protected by the; firing device with. short stuff; loading times taken from behind the feeder devices _; and fired; will. In space (see Fig: 2) on the left and right of the vehicle arrangement of two alternately extendable longitudinal axis a number, here nine each, missile firing devices, of which: a launching tube that is always in or containing missiles, standing firing position can be located, "are sixteen flight-bearings. A 55 body attached to the vehicle floor, automatically magazine-like grid 45 in the launching devices facilitates the reloading. . stockyard It also prevents lateral displacement obligations has a loader, the possibility of using gerutschen the upper at its end with quick ringem labor and 60 missile kleinenNachladewegen circuits 46 against bottom and top wall of the vehicle in _which: reload Zubringyprrichtung tool elastically in which from or can the steering contactor pause in combat If the missiles or launch tubes are not filled in. Filling up the drums so that a dazed space behind: the feeder devices 5 special loaders is superfluous. The space for one and 6 is space for a loader, whose loader required space can then be added to fill up the feeder gates. · ■■ -. ·· 65 borrowed to accommodate additional missiles.

1 sheet of drawings

Claims (1)

1 2 Sliding shoe is provided, which with jaws the fitting surface Claim: Chen encloses and after a stroke in the longitudinal direction of the rails against the limits Feeding device is in the form of an inside bar. of an armored vehicle can be rotated S - This allows the missile to be removed th magazine drum for a launcher from the magazine with; the launcher that facilitates under the control of a subsequent formwork-connecting transport trolley, but none tion in the magazine drum with the vertical possibility of magazining the flight axis stored missile automatically grips bodies inside an armored vehicle to improve and in the direction of the missile longitudinal axis from io and the missile must still from the armored cover executes and there are fed into a hand of the transport trolley. There firing position swivels, thereby marked: this type of reloading at the expense of Schußka draws, Attempts have also been made to eliminate the problem directly, so that the magazine drum (5, 6) goes idle in addition to the firing rate in the retracted state in a vehicle with a Sensitive launching device (3, 3 ') arranged 15 attached to the vehicle upper wall, as a height is and Abam formed on a horizontal support plate (12) and laterally adjustable tube bundle lower end of the magazine drum (5, 6) hydraulic system for recoil-propelled missiles has actuatable joints (16), which can be solved by that in which the launcher system a missile (13) or a launching room with an elevator for the missile The tube (14) partially encompassing a magazine body axis that is rotatably mounted on this elevator for flight 20 parallel axis of rotation of the joints drum was arranged (see. German Patent (16) oppositely pivotable 'holding claws (15) 1 020 547). The ones carried standing in the magazine drum, and the missiles at their outer periphery. be 'by gradual is provided with a circular ring (19) in which wedge pivoting around the vertical axis of rotation of the maga-shaped, brought to the axis of rotation of the magazine drum 25 tin drum in a loading position from which it (5, 6) parallel recesses (18) arranged through the under the magazine drum are each facing the missile lift truck of the elevator vertically upwards into the (13) or on the launch tube (14) arranged vertically pivoted launch tubes brought who-receiving means (20) are located. the. In the case of such a feeding device, that is sufficient 30 Number of missiles that can be automatically reloaded from the magazine drum for one-time reloading only loading the launcher. Also needed this intended for larger watercraft ^Zubringvor-: directionally not much space, so that they land-The invention relates to a feeding apparatus in armored vehicles in 35 of the type mentioned under a form can be brought inside an armored vehicle ... rotatably arranged magazine drum for a shooting device that does not belong to the state of the art and which, under the control of a foil proposal (cf. and in 40 firing devices on: a turret of an armored vehicle that can be rotated about a vertical direction of the missile longitudinal axis from the armor axis extends cover and is arranged there in a firing position, the missile pivoting in a firing position, pipe in the turret on the turret inner circumference armored vertically , are provided with launchers for standing or hanging. Vehicles provided with this shock-powered missile must be a solution. However, it is disadvantageous that the launchers are small and can be built as low as possible from their magazined position, in order to offer little attack surface, and yet an automatic loading device is swiveled out and the launching device retracted into the interior of the turret in a certain relation to the vehicle value Number of missiles with you. need to be implemented. Furthermore, the inside of the armored driver's loading device with the missiles arranged to hold the aircraft must be locked quickly and without a body during the great hindrance of the swiveling required for the operation of the drive, accordingly, an increased tech tool required, Personals as well as .without large. ..ruff. On with himself,., .Der. the operational safety of work of one or more charging protecting such, be fed even in difficult combat situations of the launcher, ~ to \ decreases a 55th fighting armored vehicles,
to enable high rate of fire. At the for? Concentric tower inner circumference It is therefore proposed according to the German patent specification The arrangement of the magazined missiles remains wei-1 137 348, the removal of the missiles automatically for the operating personnel of the vehicle with the aforementioned feed device through only a very small space releasing and engaging 60 launchers is downsized. Apart from automating mounts to a large extent. For this purpose, the operating personnel are also provided by other rail-shaped brackets, the ren sections of which are separated from the armored vehicle. Openings face each other and the corresponding mounts, for example a defect in the twisting device, can be repaired after the magazine has been inserted in the direction of the magazine, so other missiles can rest on limits and between repairs on Agden rails that are not arranged in the tower and the mating surfaces of the holder on the unit, for example on the engine or other missile, a supply system that can be operated in a suitable manner can only be repaired in this way,