The invention will be elucidated in more detail in the following on the basis of Figures.
The cartridge 20 shown in
The material of the shotgun-barrel projectile 1 consists of Pb (lead) or of a readily deformable material (see
In the course of firing, the shoulder 4 with the plane face 5 consequently has the advantage that the case 26 is held in place until snapping open, and the projectile 1 is thereby centred in the case 26 and also remains centred until leaving the cartridge case 26 (improved hit pattern).
The intercalation 2 consists of plastic, the front part taking the form of a plunger 21, and in the rear part has an obturation aid 6 which prevents a leakage of the propellant charge 27—or, to be more precise, of the gases thereof—in the direction of the projectile 1 after detonation has taken place. In the front region the intercalation 2—or, to be more precise, the plunger 21—has a shoulder 7 which centres the projectile 1 with the intercalation 2. The adjoining large diameter (projectile diameter) of the ring 8, which in this embodiment is connected to the plunger 21 in one piece via an incorporated predetermined breaking-point 9, serves as an assembly stop in the course of mounting the projectile 1 onto the plunger 21 (projectile seating—retracted case). In the course of firing, the predetermined breaking-point 9 provides for a uniform build-up of pressure. After the ring 8 has been sheared off by the pressure of the propelling gases that builds up, the plunger 21 is pushed into the free space 10 of the projectile 1. The sheared-off ring 8 is pressed rearwards in the direction of the obturation aid 6 by the projectile 1 on the centring diameter 11 or on the plunger 21. In this description, the terms “downwards” and “rearwards” are always understood to mean the end opposed to the direction of firing.
When the projectile 1 is telescoped together with the intercalation 2—or, to be more precise, with the plunger 21—a projectile spigot 12 with incorporated bevel 13 and bore 14 is pushed into the bore 15 in the plunger 21 with incorporated diameter reduction 16 and with a hemisphere 17 at the bottom of the bore 15. Once the plunger 21 has travelled a certain distance in the direction of the projectile 1, the bevel 13 comes into contact with the hemisphere 17. From this time until the abutment of the upper side 18a of the plunger against the bottom 18 of the free space 10 (initial motion of the projectile), the material of the projectile is pressed into the diameter 19 which becomes larger again. In this way, the desired connection arises, which can no longer be released. The projectile spigot 12 with its bore 14, and the bore 15 with the hemisphere 17 are arranged on the axis of symmetry 22. The diameter of the projectile spigot 12 in the region of the bore 14 is somewhat reduced in comparison with the diameter of the bore 15 in the plunger 21 and corresponds approximately to the diameter created by the diameter reduction 16.
The height of the firm connection between the plunger 21 and the ring 8 determines the gas pressure at which the rupture of the ring 8 takes place. The build-up of pressure in the powder chamber, where the propelling charge 27 is located, determines the rupture of the ring 8 at the predetermined breaking-point 9 and consequently releases the intercalation 2 with the plunger 21. The ring 8 is able to move rearwards on the diameter 11 in a centred manner. The plunger 21 is pushed into the projectile 1, which is held in place by the case 26 which is retracted by 180° at the upper end.
After a certain distance, the bevel 13 impinges on the hemisphere 17 and presses the material located on the bevel 13 into the diameter 19 that becomes larger again. In this way, a firm connection arises between the projectile 1 and the plunger 21. If the two faces 18 and 18a abut in a positive manner, the projectile 1 is set in motion contrary to the force of the retracted case 26.
In the process, the case 26 is peeled upwards by the shoulder 4 and by the plane face 5 and additionally centres and stabilises the projectile 1 in the case 26 until said projectile leaves the case 26. This is the prerequisite for a stable flight within and outside the barrel. But only the fully coordinated system guarantees the desired precision.
Advantages of the invention are:
Number | Date | Country | Kind |
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103-47-369.6 | Oct 2003 | DE | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/EP04/11138 | 10/6/2004 | WO | 00 | 1/9/2007 |