DE1553987A1 - Device for locking a container containing a missile with a launching device - Google Patents

Description

BOLKOV / limited liability company Ottobrunn near Munich

Ottobrunn, May 23, 1967 BP 628

SX-I Pu / Gt ■

Device for locking a missile containing container with a launcher.

The invention relates to a device for locking a container containing at least one recoil-propelled missile and a container that can be adjusted vertically and laterally Closing facility.

Starting from a container, for example a launch tube, and following the so-called target coverage method into their target

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Dirigible missiles are made using a part of a Launching device-forming tracking device steered until it reaches its target. This from a Perj sko.) existing tracking device that contains a tracking device, forms a structural unit with a straightening device, which is only available as Whole can be moved.

With this launching device is a so-called gun carriage forming device rigidly connected, on which the launch tube is locked before the start of the Fliigkörpe'rs and only after the missile has reached its target is removed from it.

Since the detection area of the location device located in the periscope, which forms the guidance signals for the flight of the missile after locating the launched missile, very small the missile must be aligned with the lifter so that that he entered the detection area shortly after the start of the tracking device arrives so that the preconditions for a guided flight are met at all.

As a result of the rigid connection of the mount with the launching device, the missile to be inserted into the mount is irrelevant whether it is in a launch tube or not - precisely set up on this, i.e. to be applied in such a way that the missile longitudinal axis or longitudinal axis of the launch tube and the longitudinal axis of the mount are parallel . The launch tube must therefore be locked after alignment on the mount with this so that the assumed aligned position

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crändort is preserved, while at the same time the necessary oloktx-i see connections for the ignition of the engines, for the commissioning of the gyroscopes, which serve as reference generators during the flight, and for the signal transmission between the Absxisso i. !! direction and the missile si. ad

A \ is logistical reasons, it is finally desired, "the externally mounted on the launcher locking device s in their dimension as possible KLR-1 ^ to hold and to provide especially a self-contained unit, which is insensitive, for example against weather influences. Suitably it also to design the locking device so that it allows the insertion of a launch tube from different sides, the reloading being carried out manually or automatically depending on the type of use and the missile to be used.

The object of the invention is to create a device for locking eixies containing at least one recoil-driven missile container with a vertically and laterally visible launching device, which can be operated manually or using a power amplifier without interference, has a low overall height and self-contained design, and which meets the above mentioned requirements. The container should still be able to be ejected after the missile has been launched.

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Based on a device for locking tines at least one recoil gear containing missiles Container with a height and height adjustable 1 Alischußoinrichtung, with mutually movable chews as Virriogol.ungsorgauen and means for automatically establishing an electrical connection between the missile and the launcher, this object is achieved according to the invention in that two in relation to the longitudinal axis of the container behind <ifiandcr arranged claw pairs are provided, the individual claws mounted resiliently about their respective pivot axis and can be influenced at least temporarily by an energy store Adjusting means are movable such that a. Klauoinartr in a a stop for inserting the container üi1dcude Intermediate position can be automatically transferred before the container is driven differently by the same adjusting means Pairs of claws, which correspond to abutments arranged on the container, in an aligned firing position can be transferred and locked in this. The electrical connection between the missile and the launcher is only after the container has been aligned by the adjusting means the claws can be produced automatically.

In this surprisingly simple way it is achieved that after the container has been placed on, two pairs of claws initially only one, in particular the one at the front in the firing direction, into a stop for the abutment arranged on the container forming position is movable so that the position of the container is securely fixed on the locking device and at the same time an exact assignment of both the actual locking elements on the abutment to the locking device as well

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oa plug to socket in the locking device or in: container for making the electrical connection can be reached. Only when the actuating means are subsequently actuated do both pairs of claws simultaneously engage in the locking elements assigned to them and thus lock the container.

Di. ·; Actuators for the locking system can be used depending on the type the missile used according to a further feature of the invention via eil llan.dstoll member or via At least one hydraulic motor can be operated so that the Operation of the locking device both manually and using a power amplifier is possible.

It is useful here, the device according to a further Design feature of the invention in such a way that the claws in the same direction bfiv.:;gbaren claws of both claw pairs on the end faces of one tub-shaped forming a support surface for the container Recording with the interposition of an eccentric on each of the free ends of itself symmetrically to the longitudinal axis of the recording extending torsion bar springs are arranged. There are those Claws of one pair of claws compared to the claws of the other arranged at different angles on the torsion bar springs. Furthermore, there is a cylinder on each of the two torsion bar springs fixed eccentrically, which can be moved together via axially displaceable adjusting means, depending on an electrical connector can also be actuated by the movement of the actuating means.

The arrangement of the claws on an eccentric also enables

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X3> more simply the holding force of the individual claws a-i dem adjust their associated abutment so that the claws each of a pair evenly virkon. The different V. ' of the claw pairs in the starting position relative to their torsion bar springs allows a different one Temporal engagement of the claw pairs on the Itfiderlager. Uni now too to achieve the same squeezing pressure for all four claws, is the movement of the SteJ! means on the respective fixed Torsion spring connected to it, transferring cylinder off-center arranged on the torsion bar springs, so that the one with the; first engaging pair of claws connected part of the torsion bar spring is softer than that of the other pair of claws shorter part of the torsion bar. In particular, the abutment that interacts with the first engaging Klaluenpaeir on the container and the holding surfaces of the two claws this Pair are those of the respective pen's properties To train torsion bar depending Schwerikwinkel accordingly.

The cylinders are easily movable when each cylinder two diametrically arranged grooves with predetermined has the same and opposite slope and with his Each end is mounted in fixed mounts and the grooves in the cylinders on your axially displaceable adjusting means attached pins are assigned.

The movement of the cylinders and thus the turning of the claws bearing torsion bar springs is therefore dependent on the Movement of the respective adjusting means and according to the slope selected for you grooves.

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The automatic transfer of a stop for the container forming Elaucnpaares in its intermediate position takes place after c-ϊ non! κ!> i doors feature, dor i £ i-finding via compression springs, which the Dr;. "Hs tnbf c-dora to'ischcn one of the permanent camps and one on the assigned face of the mount \ * orges eh (.-new bearing block to encoder., with the interposition of one of the actuating means movable pressure plate on the side facing the bearing. In Your pretensioned ei: The compression springs are located, by eüsc with the rx-ial- displaceable adjusting means connected and with the Ilandstellgli '-.' d hold to be activated notch. In this position they are kli-.uenpanrc fully open. When unlocking the said. Kaste ο ltspainrcii then the compression springs and cause a Closing movement of both clans.ipaires around a small botrag schoi? In the starting position, more closed pairs of claws are prevented uuii s-ij »further shifting of the container.

To actuate the electrical plug "during the locking process". Iig <? S the adjusting means is expedient according to a further feature of the invention verbxmden with guide rods, each at one end have a groove with a slope, in which a connected to the plug Pin engages. The preferably steep and short groove has the effect that the adjusting Jt? J ttcl and the claws of the pin connected to the connector "into the Xu ten engages and the plug from a recessed and thus quickly in an extended, dnc-! electrical connection producing position is raised.

If large operating forces are required or an automatic one or remote-controlled actuation of the locking device is required, a device is expediently used

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used in which the actuating means on a double-sided piston axxfweisenden piston rod are arranged in the middle, which in each a cylinder arranged between the bearing blocks and the bearings in the longitudinal center axis of the v.aimen-shaped receptacle. and can be moved forward, the sides of the cylinders facing the bearing blocks each being connected to a pressure source Line are connected.

Point the guide rods for actuating the electrical connector in this embodiment one cam rail for actuation of microswitches interacting with the pressure source. In addition, ejector levers can be connected to the locking claws, which enable the empty container or in the event of malfunctions, a lit-hältx- with missile throw off.

Correct functioning of the locking device also requires a suitable design of the abutments, which cooperate with the pairs of claws, on the container ei 'containing a missile. In the case of a container for at least one recoil-driven missile with locking elements for connection to a height-adjustable and laterally adjustable launching device, in an advantageous embodiment of the inventive concept, the container is connected to a longitudinal bead protruding from the container configuration and extending from end to end. This has within its cross-section at least the locking elements interrupting its outer surface and ends from a locking element towards one end face in a wedge-shaped part, in such a way that the ¹ } resiliently abutting it, the locking

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associated device, formed by the claws enweit er s Locking elements when sliding the container onto the locking device in the associated locking elements of the container can snap into place.

In addition to its function as an abutment for the locking organs the locking device serves the longitudinal bead after a Another feature of the invention also as a container for all door required for launch and guided flight of the missile Additional equipment, such as a cutting device for the wire connection for steering signal transmission, electrical plug connection, locking devices and a pyrotechnically triggered mechanical unlocking device chtiuig.

In this way, not only are the additional devices protected against damage in a container with a smooth outer contour and low overall height, but also the sensitive connecting organs, for example the electrical plug connections, are sunk into the longitudinal bead and are thus provided for when handling the container Protected against damage until it is locked on the locking device. The longitudinal bead finally represents an orientation problem, which makes it easier for the operator to eirizubringexi the container during manual reloading in the approximately desired assignment in the locking device, so that a rough alignment of the container is already selected.

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The invention is illustrated below using two exemplary embodiments explained. Show it:

Fig. 1 is a perspective and partially shown in section View of the entire locking device, with the locking members locking in their End position are,

2 shows an end view of the locking device with a tubular container,

3 shows a plan view of part of the locking device in an intermediate division,

4 shows an enlarged illustration of a locking member of the Locking device,

5 schematically shows another embodiment of the locking device with hydraulically operated actuators,

Fig. 6 is a plan view of a container with a than

Longitudinal vi.11 s t W "derlager for those serving the Voi'riegoTungsorgano

7 ^a, 7b and 7c are sections along the lines II, 11-11 and III-III from FIG. 6.

The one marked with J ^ and one not shown here Height-adjustable and laterally adjustable launching device to be connected The locking device consists, as shown in FIG. 1, in essentially from a trough-shaped receptacle 2 with a Base plate 3 and a cover plate 4 on their front sides is limited by bearing blocks 8 and 9. These bearing blocks each point outwards at an angle on their Schma3.seiten directed legs 10 to 13, of which in FLg, 1 however

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only the legs 10, 11 and 12 are shown. In In the longitudinal direction of the receptacle 2, the legs are each through a rod 15 which stiffens the structure and serves as a support for a container 1 * 1. In the tub-shaped Recording 2 are the essential elements of the locking device arranged symmetrically to the longitudinal axis. For this include two extending in the longitudinal direction of the receptacle Dreiistabfedc.ru l6, which with their ends in the bearing blocks 8 and and in the area of the first and second third.? their length by one arranged transversely to the longitudinal axis Camps 18 and 20 are held. Between camps 18 and is on each torsion bar spring l6 a cylinder 22 with two Nutetx 23 and 24 opposite each other in the valley

xxoidc attached opposite the same slope. Each cylinder 22 is with its end collars 25, 26 in corresponding recesses 27 and 28 of the bearing lo hzwO 2-J £ '*!' -: g © rt _e

The protruding over the bearing blocks 8 and 9 to the outside Ends of the torsion bar springs l6 each carry a claw, namely the rear torsion bar spring in FIG. 1, the claws 30 and 32, the

order the torsion bar spring the claws 31 and 33 · The respectively on different torsion bar springs l6 rigidly arranged, themselves axially parallel opposite claws, i.e. claws 3O> 31 and 32,335 each form a pair of claws. The pairs of claws are also on their torsion bar springs at different angles arranged. So is the one lying in front in the firing direction, on the dex- in Fig. I right front side, arranged Pair of claws 32,33 in an initial position already in a somewhat more closed position than the opposite

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Claw pair 3Οι31 · The individual claws are on their associated torsion bar springs, as shown in Fig. 2 for the claws 32, 33 can be seen, arranged with the interposition of an eccentric bushing 34, a guide sleeve 35 and a clamping bushing 36. As a result, manufacturing tolerances can be compensated for by adjusting the claws accordingly, and the Holding force assigned to each individual claw on the ihx " Abutments are adjusted.

Between the bearings 18 and 20 there is also provided a bridge 40 which is longitudinally displaceable between them and extends transversely to the longitudinal axis, through which the Zj ^ lindci '22 are passed with play. This bridge carries pins 42 and 44, each of which engages in one of the grooves 23 or 24 of the two cylinders 22. Moreover, the bridge 4θ at its center a pin 45 with an annular collar 46, see. Fig. 3i, which serves for mounting the bridge to an ^<i ;; i Zxigrohr 47, which is part of a still to be described Ilandstellglei edes 62 is. The end of the draw tube 47 cooperating with the bridge is slotted and at the end of the slot 48 has a limiting pin 50 lying parallel to the pins 42, 44 and protruding on both sides beyond the draw tube 47, which is dimensioned so that it is between the cylinders 22 is freely movable. The task of this limiting pin 50 is to limit the movement of the draw tube 47 in the axial direction. As a stop for the limiting pin 50, a pressure plate is provided on the side of the bearing 18 facing away from the cylinders 22, which counteracts the action of compression springs 53

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Is movable. With their one ends these compression springs 53 are supported on shoulders of recesses 55 provided in the pressure plate 52, while they are supported with their other ends on the cylinder bushings 84 of the claws 30 or Ji . The respective associated torsion bar springs l6 are also guided through the recesses 55.

In the container 14 shown in FIG. 1, see FIG. 2, locking end positions are the adjusting means by a cube-shaped Notch 56 with a wedge-shaped beveled recess 57 held on the free end one in one perpendicular to the slot 48 provided further slot 58 held Leaf spring 59 is screwed on and protrudes through an opening 60 in draw tube 47. The leaf spring 59 is approximate cranked twice on half of its length.

In Fig. 3, the limiting pin 50 is shown when it hits the pressure plate 52. S _e ine end position in which the torsion bar springs l6 surrounding compression springs 53 (compressed is the other hand, indicated by dash-dotted lines.

According to FIG. 1, the pairs of claws are actuated via the manual control element designated _6_2, as from a handle 63, exists, which is connected to the draw tube 47 via a handle bracket 64 and is thus also connected to the bridge 40. The draw tube encloses a push rod 66 loaded by a spring 65, which is held in the handle holder via a pressure catch 67. ' In addition, the draw tube 47 is enclosed by a guide tube 68, that with draw tube 47 and push rod 66 via one on the draw tube

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arranged bearing bush 70 is connected. The guide tube also has at its end facing the receptacle 2, but outside this, a guide ring 72, in the mandrel the detent 56 fastened on the leaf spring 59 through an opening 73 in the guide tube 68 in the position of the dash-dotted line in FIG Adjusting means engages · The free end of the push rod 66 finally carries a wedge-shaped beveled pawl 74 corresponding to the catch 56.

To make the electrical connection between the launching device and the one containing a liquid body not shown here To produce container, an electrical connector 75 penetrating the top of the bearing block is provided, which is shown in FIG Depending on the movement of the draw tube 47 over one each on the bridge 40 arranged guide rod 76 from a retracted Position can be converted into an extended position. To this end, each of the guide rods 76, respectively are guided in a recess 77 of the bearing 20, at its free end a groove 78 with a relatively steep slope on. In each of these grooves protrude. 1 the connector 75 receiving bearing piece 80 connected pins 8l.

For releasable temporary locking of the actuating means at Stop of the limiting pin 50 on the pressure plate 5 "according to FIG FIG. 3 is a notch shown schematically in FIG. 4. This consists of one assigned to each guide rod 76 spring-loaded ball 82, each arranged in the bearing 20 are, and when moving the draw tube 47 i'i the position 3 snap into a recess 83 in each case, which at the undersides of which also trigger the movement of the plug 75

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Management staff: ». 76 are provided.

5 shows an embodiment of the Vex locking device in which the actuating means for the claws are actuated hydraulically. The structure and mode of operation of this embodiment is essentially the same as that described above, so that the same parts are identical As can be seen from Fig. 5, the bridge 40, which carries the pins 42, 44 engaging in the grooves 23 and 2k d - The piston rod 89 extending along the longitudinal axis of the receptacle 2 is fixedly connected and each has O-inc-i pistons 90 and 91 at its two ends 9 and the other end of which is arranged in each of the bearings 1.8 and 20. The cylinders 92 and 93 are each connected to a hydraulic pressure source (not shown here) via a line 96 or 97. These lines 90 and 97 each wound in the cylinders 92 and 93 via openings 9k and 95> which are provided on the ends of the cylinders 92 and 93 fixed in the bearing blocks, 8, 9, so that they form two hydraulic actuators that work against one another.

The connectors connected to the bridge 40 and the electrical connector 75 actuating guide rods 76 instruct in this embodiment each of its sides facing the torsion bar spring has a Xockon splint 98.99 for the actuation of attached to the base plate 3 Microswitches 100, 101 and 102 on. Depending on the Paths covered by the piston rod 89 in the direction of the The cam rails 98199

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moved along and actuated, thereby, according to their training, the Microswitch. These microswitches won't work here - MagnetVentilo, which is also not shown, connects the pressure source shown to the lines 96 and 97, which actuates the Block the supply and drainage of pressure medium in and out of the system, so that the position of the actuating means upright remains bright. Via the microswitches 100, 101 and so individual Raststellimgen are defined that the through the Ball 82 and detent 56 have specific positions according to FIG. 1 correspond.

For ejecting the container 14 after the missile has been launched is also an ejector in this embodiment provided, which consists of a lever IO5, each only with claws arranged on the same torsion bar spring, so either the claws 31i33 or the claws 30.32 in is connected in a suitable manner or forms a single part with them. The ejector closes with the respective claw connect that it in the intermediate position of the claws, i.e. when reloading a new container l4, the receiving cross-section the locking device for the container releases, i.e. lies in the plane of the cover plate 4. At the opening movement In this way, the claws also become the container 14 to the outside thrown off. A bracket 103 is also connected to the receptacle 2, with the aid of which the locking device, for example be attached to a straightening and tracking device can. Such a console can of course also be used in the mechanically actuated design of the locking device to be appropriate.

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In FIG. 6, the roller-shaped container 14 is shown in a plan view of the side facing the receptacle 2 when it is locked, which shows a longitudinal bead 120 applied over part of its circumference. The longitudinal bead representing the abutment 120 mentioned in the Z ^ ιsammenhaπ.g with Fig. 2 extends from face to face of the container 14 and is tint place oil t through interruptions in its dumbbell surface in three sections 122, 124 and 126. The part of the longitudinal bead 120 lying in front in the lowering direction of the missile, namely the part 122, has a recess 127 symmetrical to its longitudinal axis in relation to the cross section of the adjoining sections 124 and 126, see FIG 128 serves as a guide for the elastically engaging claws 32 and 331 ^v £ l · Fig. 1, of the front claw egg pair in its intermediate position. The stepped portion 128 ends in a wedge-shaped. Part 121, so that centering surfaces are formed between the front pair of claws and the longitudinal bead 120.

The identically axisgeb i .Identorbrocliuungen along the lines XI-II in the lateral surface of the longitudinal bead 120 form the own borrowed Riegolorgane I30 and 132 for the, claws 32,33 and 30,31 · Oia longitudinal bead has here, as Fig. "? h shows an approximately T-shaped cross-section. lie in its locking end position. see also FIG. 2, the grip of the claws ef laugh on the transverse beams on the T-shaped ridge 131 ·

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The distance between the two locking elements 130, 132 naturally corresponds to the distance between the front and rear <.rcr> Pair of claws on the locking device so that leg: Stop of the longitudinal bead on the front pair of paws i: i its Intermediate position, as will be described in more detail below, Both pairs of claws are precisely assigned to their locking organs are located.

In addition to serving as an abutment for the locking organs, the Longitudinal bead 120 to accommodate sanitizers for the start and the guided flight of the missile required additional equipment. These include those indicated only schematically in the drawing Clipping device 135 for the Leriksignals on the ·. Missile conductive wire connection during its flight, as e.g.

in our patent application BP Gjk (file number B)

is described in more detail; unites socket 1385 with the multipole :! Plug 75 according to Fig. 1 forms an electrical plug-in connection, such as that in our patent application, file number D 92.310

VIIId / 21c, and via which the connection to 0

all signal circles necessary for the launch and guided flight of the missile is established. The Längsulst 120 further comprises a pyrotechnically releasable mechanical unlocking 1 ^ 0 that solves a lock 1 ^ 2 is not closer described here, which in Fig. Fc dot-dash lines missile with respect to the tubular container lk to launch fixed and electrical after release of the missile Circuits operated, (see our patent application BP 632, file number B)

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The Liingswulst 120 also forms over their; entire length one Cable kana.l, in which all the steering wire, the cutting device 135, the socket I38, the mechanical unlocking device τι.id d.i. to c i.iier'i common, central harness I36 in addition, you are allowed to do so.

The .i'.rku Ji jr-si ·; ei s ο the interlocking device is shown below explained in III. of the embodiment shown in Fig. 1:

Boi vol Istjiatd.ig open claw pairs 30,31 and 32,33 are the cleat means, ie the bridge 40 with its pins 42,44 and the one with this over the tap; 45 connected draw tube 47, as shown in FIG. 3 - the position shown in dash-dotted lines - and are held in this position by the catch 56 that engages in the guide ring 72. After placing the container from above or pushing it in from the front side, the pressure razor 67 is actuated so that the pairs of claws can previously be converted into their Zivi division. For this purpose, when the pressure catch 67 is actuated, the IZastc 56 is released from the guide ring 72 and as a result the pressure springs 53 suddenly relax. The moves; previously against the force of the compression spring! "53 pressure plate 32 moved back up to the stop on bearing 18, before then the ball 82 snaps into the recess 83. At the same time, however, the claws of both claw pairs were also pivoted inward 32,33 has been pivoted so far inward into an intermediate position that the wedge-shaped part 121 of the longitudinal bead 120 on the container lh , see FIG.

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Upon further displacement of the container, the claws 32-33 come to the edge 129 of the recess 127 dos subsequent 'nfulstteiles cross-section shown by. In Fig Yes resiliently to the plant, so that tilting of the Läugswulstes and thus inaccurate resting is avoided on the locking device. The container can now be pushed forward on the locking device until the rear edge of the first locking member 130 strikes the inner surfaces of the front pair of claws 32, 33. The aligned position of the container 14 is thereby indicated to the operator. Both the front and the rear pair of claws, which have not yet been in contact with the longitudinal bead, are now in a position that corresponds exactly to their associated locking element I3O or 132, in which, due to the design, the plug 75 of the locking device of FIG socket I38 located in the container l4 is precisely assigned. The pair of claws are still held in this position by the catch consisting of the ball 82 and the recess 83 until the operator pushes the manual control rail 62 in. The only slightly .sperrende detent ball and recess is released during this movement and the bridge 40 connected to the draw tube 47 is pushed forward to the stop on the bearing 20. The pins 42, 44 arranged in the bridge 40 and engaging in the grooves 23, 24 of the cylinders 22 also rotate the cylinders 22 so that both pairs of claws close in their locking members 130, 32. The catch 56 now protrudes, see Fig. 1, into the opening 60 of the draw tube 47 and, held by the pawl 74, locks the claws in their locking position. Towards the end of the locking movement is also

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the plug 75 i * i extended in the manner already described and connected to the socket I38. For this purpose, the pitch of the grooves 78 i * ^{1 of} the guide rods 76 is chosen so that the extension movement of the plug 75 only begins when the beheilt he Ik is already held immovable by the two claw pairs, although the claws are not yet fully closed.

When the container is unlocked, the sequence described takes place in the opposite direction. By actuating the pressure catch 67, the catch 56 is released from the opening 60 and the bridge kO is pulled out via the manual control element 62 until the limiting pin attached to the pin k5 hits the pressure plate, Fig. 3 The ball 82 is now in place again the recess 83 and allows the container lk to be removed from the locking device. The manual control element can then be pulled out until the catch 56 is again in the guide ring 72 and the compression springs 53 for transferring the claws into their intermediate division for reloading a new container lk are pretensioned again.

Patent claims:

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Claims (1)

Claims 1. Device for locking at least one inside recoil-propelled missile containing container with a height-adjustable and laterally adjustable launching device, with £ J ^ mutually movable claws as locking organs and means for the automatic production of an electrical Connection, characterized in that two arranged one behind the other with respect to the longitudinal axis of the container Claw pairs (30,31 and 32,33) are provided, the individual claws resiliently mounted about their respective pivot axis and at least via an energy storage device temporarily influenceable a setting means are movable in such a way, that a pair of claws automatically move into an intermediate division that forms a stop for inserting the container (14) can be transferred before the container (l4) by the claw pairs driven differently by the same actuating means, the correspond to abutments (130, 132) arranged on the container, can be transferred into its aligned firing position and is locked in this position. 109821/0082 2. Device according to claim 1, characterized in that the electrical Ifex connection between the missile and the locking device can only be produced automatically after alignment of the container (lk) by the adjusting means of the claws (30 to 33). 3 · Device according to claim 1, characterized in Ii ii e t that the actuating means can be actuated via a manual actuator (62). k. Device according to Claim 1, characterized in that the actuating means can be actuated by at least one hydraulic motor. 5. Device according to claims 1 to J, characterized in that the claws (30,32 or 31i33) J ^{c of} a pair, which can be moved in the same direction, on the end faces of a horizontal receptacle ( 2) with the interposition of an eccentric (3 ^) on the free ends of torsion bar springs (16) extending symmetrically to the longitudinal axis of the receptacle (2), the claws of one pair of claws opposite the claws of the other at different angles on the Drelistabfedern (l6) are arranged, and that on each of the two torsion bar springs (l6) a cylinder (22) is fixedly arranged eccentrically, which can be moved together via axially advancing cleat means (4θ), with an electrical connector also depending on the movement of the actuating means (75) actuatigbax "is. -3-10 9821/0082 * ^E; "° ^: ''" Vt >. Device according to Claim 5i, characterized in that it is g e k c 11 η zoic hii ο t that each cylinder (22) two diametrically mutually arranged grooves (23,24) with predetermined, opposite and equal slope ntif shows and with its ends (25,26) each in receptacle-proof bearings (l8,20) is mounted, the grooves (23,24) in the cylinders (22) being attached to the axially displaceable actuating means (40) Pins (42,44) are arranged in a row. ^7th Device according to claim 5i, thereby -geke η η ζ cich .n. ο t that the actuator (4θ) influenceable energy storage consists of compression springs (53) that the torsion bar springs (l6) the
between a bearing (l8) that is fixed to the receptacle and a Lugerbock (8) provided on the associated end face of the receptacle (2), with a pressure plate (52) movable by the actuators in between, on which the bearing ( l8) facing side. 8. Apparatus according to claim 7, characterized in that that the compression springs (53) in their vorgespanritcn position by a connected to the axially displaceable adjusting means (4θ) and held with the handset cooperating catch (56) are. 9.Vorrichtung according to one or more of the preceding claims, characterized in that the actuating means (^ 0) for actuating the electrical. Plug (75) Führujigsstäbc (7 ^) sand connected, at one end, $ p have pitch with a groove (78) into which a erbundoncr with Stocker (75) \ pin (81I engages. 109821/0082 BAD OftCEm. __, -4-. 10. The device according to one or 'liiohrcrcn dor preceding claims, characterized gc Ic e η η ζ ο Ii ic et ji that the St el! .In tt i el (4o) to ei. A piston rod (89) having a piston (90 or a piston rod 89) are arranged in the middle on both sides, the one between di: n bearing blocks (8, 9) and the bearings (38, 20) in the longitudinal axis the nanneuf örraigen receptacle (2) arranged Z.lindern (92,93) is movable back and forth, wöbe; which -t Lagerböckea (8,9) facing sides of the cylinder (92.93) J ^{e ini} at a a pressure source connected; line (96,97) are connected. 11. Apparatus according to claim 10, characterized gekennzei not -CH that the guide rods (76) juelle for actuating the plug (75) cam tracks (98,99) for actuating the pressure lifit <cooperating Mikr ο scarf tern (100,101,102). 12. Device according to the preceding claims, characterized in that one claw of the claw pairs, namely only the claws (30,32 or 31,33) arranged on the same lJ torsion bar spring (l6) have a lever (105) for ejecting the Carry container (l ^l i). 13 · Container for at least one recoil-driven. Missile, with locking organs for connection with a height and be a directable launcher, especially after Claim 1, thereby g e k e n η ζ ο i c h 11 e L, that the 1098 21/0082 Container (l4) with one from the Bc-haltorkouf igurc.t Lo.ι iierausragendeii, itself .on Stiruscilc am Stirüscj. t «· c; r- ■ strockenden longitudinal v.ailst (120) '." crbundch is, di ο within its' cross-section at least the transverse lateral surface of the bar orgo.ne (130,132) auiVo.ne (130,132) and> on oiiioii; Ri.cgelorgan ans zu Eiucr end face in a kvj Llfön ,, i ge, i part (121) ends in such a way that the other locking organs (30 to 33) are resiliently adjacent to it and are assigned to the locking system -: Auf.sciiiiifaev: the container (lk) on the locking device in diυ associated locking elements (130,132) eiarasten köüaeu. Container according to claim 13, characterized geke η η ζ calibrated η et that the longitudinal mills (120) as a container for all additional devices required for the launch and the guided flight of the missile, such as Ιίειρρ before device (135) for the wire connection for steering signal transmission, electrical Plug connection (138), locking devices (1 ^ 2) and -sine pyrotechnically triggered mechanical unlocking device (l40), among other things. 109821/0082