Ammunition projectile having enhanced flight characteristics
AssigneeCove Corporation
InventorHarold F. Beal
Life of this patent
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Abstract
An ammunition projectile of enhanced flight characteristics, having a boat tail portion and including a circular land provided on the rear surface of the boat tail portion and concentric with the longitudinal centerline of the projectile, the land having a circular concave wall extending from the flat rear face of the boat tail portion to a circular flat surface of the land. Among other things, the projectile exhibits a lesser rate of velocity deceleration along its flight path to a target than like projectiles that do not include the land.
Claims9
An ammunition projectile having enhanced flight characteristics comprising a cylindrical body portion having a longitudinal centerline, a leading end, and a rear end, a boattail portion including a non-radiussed sharp circumferential edge defining a non-radiussed sharp juncture between said rear end of said body portion of the projectile and said boattail portion, and a truncated frusto-conical wall which tapers from said non-radiussed sharp circumferential edge gradually inwardly toward the longitudinal centerline of the projectile to terminate in a flat rear end surface having a non-radiussed outer sharp circumferential edge, a circular land defined on the rear end of said boattail portion and extending rearward therefrom to define a flat circular surface distally of said land, and a continuous concave arcuate wall connecting said flat rear end surface of said trailing end of said boattail portion to said flat circular surface of said land, the continuous concave arcuate wall of said land subtends an angle of 90 degrees or less, and the area of said flat circular surface of said land being between about 60% and about 90% of the area of the flat rear end surface of said boattail portion whereby said projectile exhibits a lesser rate of velocity deceleration during flight to a target than a like projectile without a land and its accompanying concave arcuate wall fired under like circumstances.
A method for the manufacture of an ammunition projectile having enhanced flight characteristics comprising the steps of
- forming a cylindrical body portion of the projectile, said body portion having a longitudinal centerline and a trailing rear end,
- terminating said trailing rear end of the projectile in a non-radiussed sharp outer circumferential edge of said body portion,
- forming a boattail portion which projects rearwardly of said body portion of the projectile from said non-radiussed sharp outer circumferential edge of said body portion and defines a non-radiussed sharp juncture between said rear end of the projectile and said boattail portion, said
- boattail portion including a truncated frusto-conical wall which tapers from said non-radiussed juncture gradually inwardly toward the longitudinal centerline of the projectile to terminate in a flat rear end surface having an outer sharp circumferential edge,
- providing a circular land on said flat rear end surface of said boattail portion, said circular land extending rearwardly from said flat rear end surface of said boattail portion and terminating in a flat circular surface having an outer sharp circumferential edge,
- interconnecting said outer circular edge of said flat circular surface of said land to said outer circular edge of said flat rear end surface of said boattail portion by a continuous concave arcuate wall which subtends an angle of 90 degrees or less, and the area of said flat circular surface of said land being between about 60% and about 90% of the area of the flat rear end surface of said boattail portion.
Dependencies are inferred from the claim text.