Fin stabilized subcaliber shell of large length to diameter ratio

• US 4,638,738 A
• Filed: 10/29/1984
• Issued: 01/27/1987
• Est. Priority Date: 10/28/1983
• Status: Expired due to Fees

• Current Assignee: Rheinmetall GmbH
• Original Assignee: Rheinmetall GmbH
• Inventors: Bornefeld, Klaus, Bisping, Bernhard
• Primary Examiner(s): Tudor, Harold J.
• Application Number:
  US06/666,181
• Time in Patent Office: 820 Days
• Field of Search: 102/514-523
• US Class Current: 102/516
• CPC Class Codes: F42B 12/06 with hard or heavy core; Kinetic energy penetrators F42B12/16, F42B12/74 take precedence
• CPC Class Codes: F42B 14/061 Sabots for long rod fin stabilised kinetic energy projectiles, i.e. multisegment sabots attached midway on the projectile

Abstract

In a spin stabilized flight shell, a front body and a rear body are attached to each other at a first joint, and a pointed body is attached to the front body at a second joint. The materials of the front and rear bodies contain a high proportion of at least one metallic element having a density of at least 18 g/cm³. The rear body has higher ductility than the front body, which in turn is more brittle, so that it fragments easily.

In one embodiment, a case can be used to protect the first joint and the front body prior to impact. The case is developed in a circumferential region as a form locking zone, for interaction with a drive cage. The front and rear bodies and the case 38 are connected at a contact zone, for example by brazing, and is of circular cylindrical shape with a diameter equal to that of the front and rear bodies. At the rear, the case is developed into a support for the stabilizing fin assembly, and is provided with a internal compartment for a tracer composition.

In another embodiment, a drive cage with front and rear extension supports is provided, and the front and rear bodies are additionally connected to each other by a central pin.

Claims

1. A fin-stabilized subcaliber armor piercing projectile having a large length to diameter ratio comprising

a metallic rear body,

a metallic middle body, and

a pointed front nose body, all of which are operatively joined to each other;

the middle body is made of metal of high density selected from the group of depleted uranium and tungsten of at least a density of 18 gm/cm³, of lower ductility but higher brittleness than the metal of the rear body in a binder phase containing iron and nickel

said rear body is made of metal of high density selected from the group of tungsten and depleted uranium in a binder phase containing iron and nickel, said rear body having a density of at least 18 g/cm³ ;

the volume of the middle body is substantially equal to the rear body;

the pointed front nose body consists of a metal of high ductility and density which has pyrophoric properties;

the rear body and middle body are joined to each other by butt surfaces and a metal sheathing surrounds said rear and middle bodies at these butt surfaces;

said sheathing extends only to about the middle of the middle body and has a front cutting edge;

said sheathing consists of steel;

said steel sheathing has means on its external periphery for connecting it to a sabot;

the rear body coaxially extends into said sheathing and fin-stabilization means are mounted on said steel sheathing; and

said middle body and rear body are joined by hard welding to each other.

2. A fin stabilized subcaliber shell as in claim 1, wherein at least one protecting means surrounds the projectile circumferentially within a region extending away from the first joint towards the front and rear of the shell.

3. A fin stabilized subcaliber shell as in claim 2, wherein at least one protecting means is a segmented drive cage.

4. A fin stabilized subcaliber shell as in claim 2, wherein at least one protecting means is said sheathing having a form locking means for cooperation with another protecting means comprising a drive cage.

5. A fin stabilized subcaliber shell as in claim 4, wherein the sheathing is adapted at least in part to support the stabilizer fin assembly.

6. A fin stabilized subcaliber shell as in claim 5, wherein the wall thickness of the sheathing decreases over a front region down to a front edge having a knife-edge shape.

7. A fin stabilized subcaliber shell as in claim 1, wherein the case is attached to the front and rear bodies by brazing at the first joint and over a contact zone.

8. A fin stabilized subcaliber shell as in claim 7, wherein the rear of the sheathing is adapted to receive a tracer composition.

9. A fin stabilized subcaliber shell as in claim 8, wherein the pointed body comprises a pyrophoric material.

10. A fin stabilized subcaliber shell as in claim 8, wherein the drive cage has front and rear parts;

and the shell additionally comprises a cover, having intended places of breakage, located parallel to the longitudinal axis of the shell and smoothly and circumferentially connecting the front and rear parts of the drive cage.

11. A fin-stabilized subcaliber shell, as defined in claim 1, wherein said metal content of the said middle and rear bodies is at least 90 percent by weight tungsten.

12. A fin-stabilized subcaliber shell, as defined in claim 1, wherein said metal content of the said middle and rear bodies consists essentially of depleted uranium.