DE2242930C2 - Hollow charge daughter floor - Google Patents

Description

Holes 14 are also provided in all three exemplary embodiments as it is only shown in FIG. 1 are shown.

When using a carrier cover (not shown), from which a respective column of shaped charge daughter projectiles is ejected over a target area, 5 the column at least partially takes on its load-bearing function.

A carrier shell is advantageously unnecessary, the respective column forming a multiple storey, the wing stabilization of which is taken over by the stabilization facility 5 of the respective terminal hollow-charge subsidiary storey G \.

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Claims (5)

1 2 The invention is based on the object of creating a shaped-charge subsidiary projectile according to the design, which is simple in design and which can be opened quickly 1. Hollow charge daughter storey, the front stabilization of the respective hollow charge daughter bullet Ignition spacer tube, on the back a detonator housing s shot on its trajectory the transition of the Stabilimit a wing having stabilization line sierungsflügel from the transport or rest position in plant and at an axial distance from each other in one the operations management at the earliest possible point in time each area close to the timeline has a front and and without obstruction of a neighboring floor / oleine rear support surface is assigned and used to educate aiming a high loading density for transport this object is achieved by the teaching according to the type of stackable that a first floor under claim 1 with the in its characterizing contact corresponding support surfaces a front part specified inventive features.
The invention is explained below with reference to three in the housing of the neighboring floor at least partially drawing shown, preferred Ausführungsbeise in the HohJIadungseinlage of the first floor is play, and the immersed and that when lifting the stacked; according to the design teachings of the further claims, arrangement over a target area, the wings for resulting advantages are obvious. They show
ner space-saving rest position in their effective position Fig. 1, 2 and 3 of the drawing can each be brought in the longitudinal axis, kl which they over the outer circumference of the section and dispensing with the projectile which is not essential to the invention, characterized in that a columnar stack is marked with 20 details that each draws the stabilization tail unit with two shaped-charge subsidiary floors of the respective earth wings (5) as a winding tail unit designed in an inventive design. is that the transition from the rest position to the shape of a hollow charge subsidiary Gi according to FIG. I at Effective action exclusively through a movement in a projectile body 1 with a subordinate in it dialer direction completes 25 brought shaped charge 2, in front of which an insert 3 is arranged 2. Hollow charge daughter projectile according to claim I, net is In the rear end of the projectile body 1 is characterized in that several stacked detonator housing 4 is attached, which form a non-detailed projectile CGi, ...) a self-supporting column, includes detonators shown and on the outside wherein the flight path stabilization of such a nusklappbaren stabilization wing 5 are arranged. Mehrfachgeschf-saes from the wings (5) of the rear 30 The projectile body 1 is limited by a shell 1 ', the first floor (C \) is guaranteed. which are in one piece and with essentially continuous 3. Hohlladihigstochergeschob is formed according to claim 1 of the same wall thickness. On the front side or 2, characterized in that the Zündab- the projectile body 1 is a substantially circular cystic tube (6c) against the force of a spring (12) axially cylindrical and forwardly open ignition spacer tube 6a is designed and thus a space 3s whose inner diameter is larger than the saving, pushed-in transport position can take the outer diameter of the projectile body I and the pin. dergehäuses 4 with wrapped stabilizing wings 5. In front of the terminal shaped charge = daughter floor Gi is to illustrate the columnar structure in 40 dash-dotted lines a second shaped charge poke G2 indicated, the rear end of which The invention relates to a shaped charge daughter located within the ignition spacer tube 6a. shot according to the preamble of claim I. The ignition spacer tube 6.7 is rigid on the projectile body I. A bullet of the same generic type is known from FR-fastened and, in conjunction with PS 20 71 096, ensures a high load-bearing capacity. The stabilization tail unit with ignition spacing has around the circumference tube 6a has an arranged pivot bolt for the arm of a respective front surface 7 and a rear surface 7 'for mutual support of two unevenly distributed and indirectly adjacent shaped charge projectiles transversely to the longitudinal axis of the projectile.
gen profiled stabilizing wing. For the trans- At the hollow charge daughter floor Gi according to FIG. 2 port, the stabilizing wings are forward mutual Abrohres extend. Support of the directly adjacent hollow When lifting the stacked arrangement over loading daughter floors Gi and Gj takes place here through a target area, the transition of the stabilizing shell 1 'delimiting circular ring surfaces 10 and 1J occurs.
wing from the transport or. In the exemplary embodiment according to FIG. The envelope 1 'is circular arc corresponding to its length around which the insert 3 also vei .Jngcrt and takes over in this associated pivot bolt, and this be μ area of a helical spring 12 on. The screwing requires both a considerable amount of space and time. As a result of the space required, it can on the other hand be supported on the ignition spacer tube 6c. In this way, the helical spring 12 can come to the Ziindubdaughter-bullet with the help of different shaped charges; Because of the time required to achieve a space-saving rest position in, the stabilization of the trajectory of each individual is delayed. For guiding the Zündabslunds shaped charge punch. In addition, when shifting from the rest position to the active position, the design of the known stabilizing oil function proves to be a groove 13. It also serves to reduce the amount of material and labor involved. of weight. For the purposes mentioned above,