초록 ▼

A sabot projectile with a subcaliber penetrator and a sabot, which has a propulsion element that acts on the rear end of the penetrator, a segmented, essentially cylindrical guide cage, which is connected to the front end of the propulsion element, and a segmented, disk-shaped metal guide element th

A sabot projectile with a subcaliber penetrator and a sabot, which has a propulsion element that acts on the rear end of the penetrator, a segmented, essentially cylindrical guide cage, which is connected to the front end of the propulsion element, and a segmented, disk-shaped metal guide element that extends radially inward in the front area of the guide cage and holds the penetrator. The disk-shaped guide element has a slightly convex contour in the direction of flight of the projectile and the material and the wall thickness of the guide element are chosen in such a way that convex area of the guide element is pushed back slightly when the sabot projectile is fired, so that the outer marginal area of the guide element rests against the inside wall of the gun barrel from which the sabot projectile is fired, and/or the inner marginal area of the guide element, which faces the penetrator, rests against the outer surface of the penetrator.

대표청구항 ▼

The invention claimed is: 1. A sabot projectile, comprising: a subcaliber penetrator; and a sabot, the sabot including a propulsion element that acts on a rear end of the penetrator, a segmented, essentially cylindrical guide cage, which is connected to a front end of the propulsion element, and a s

The invention claimed is: 1. A sabot projectile, comprising: a subcaliber penetrator; and a sabot, the sabot including a propulsion element that acts on a rear end of the penetrator, a segmented, essentially cylindrical guide cage, which is connected to a front end of the propulsion element, and a segmented, disk-shaped metal guide element that extends radially inward in a front area of the guide cage and holds the penetrator, wherein the disk-shaped guide element has a convex contour that extends in a direction of flight of the projectile, wherein the guide element is dimensioned and of a material so that the guide element is pushed back slightly when the sabot projectile is fired, whereby an outer marginal area of the guide element is restable against an inside wall of a gun barrel from which the sabot projectile is fired, and/or an inner marginal area of the guide element rests against an outer surface of the penetrator.