Method and apparatus for reducing projectile spread
First Claim
1. A method of reducing the spread of shots in a hit pattern for a rotationally-stabilized ammunition unit in the form of a projectile discharged in a ballistic trajectory from a launching device towards a target which is to be combated, by dynamic balancing of a shell in order to reduce the differences in air resistance between different projectile shells and increase hit probability, comprising the steps of:
- measuring the inclination between the main axis of the inertia of said shell and the geometric axis of the shell casesetting said two axes in parallel by providing a weight adjustment on one side of the point of gravity of said shell seen in its longitudinal direction, in the rear region of said shell at the rear plane substantially perpendicular to the longitudinal axis of said shell.
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Abstract
A method and an apparatus for reducing the spread of hit pattern for a rotationally-stabilized ammunition unit such as a projectile, which is discharged in a ballistic trajectory from an artillery piece towards a target which is to be combated including dynamic balancing of the shell (1) to reduce the effect of the air resistance between different shells, and increase hit probability. The inclination between the main axis of inertia of the shell and the geometric axis of the shell case are measured, whereafter these axes are set in parallel in that an adjustment weight (2) is mounted on one side of the point of gravity of the shell seen in its longitudinal direction. The adjustment weight (2) preferably consists of a disk or washer provided with an eccentric recess (4) for suitable weight and mass eccentricity.
15 Citations
8 Claims
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1. A method of reducing the spread of shots in a hit pattern for a rotationally-stabilized ammunition unit in the form of a projectile discharged in a ballistic trajectory from a launching device towards a target which is to be combated, by dynamic balancing of a shell in order to reduce the differences in air resistance between different projectile shells and increase hit probability, comprising the steps of:
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measuring the inclination between the main axis of the inertia of said shell and the geometric axis of the shell case setting said two axes in parallel by providing a weight adjustment on one side of the point of gravity of said shell seen in its longitudinal direction, in the rear region of said shell at the rear plane substantially perpendicular to the longitudinal axis of said shell.
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2. A method of reducing the spread of shots in a hit pattern for a rotationally-stabilized ammunition unit in the form of a projectile discharged in a ballistic trajectory from a launching device towards a target which is to be combated, by dynamic balancing of a shell in order to reduce the differences in air resistance between different shells to increase hit probability, comprising the steps of:
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measuring the inclination between main axis of inertia of said shell and geometric axis of the shell case, setting said two axes in parallel by providing a weight adjustment on one side of the point of gravity of said shell seen in its longitudinal direction, in the rear region of said shell at the rear plane substantially perpendicular to the longitudinal axis of said shell, wherein said adjustment weight is mounted in a tracer cartridge of said shell and may constitute retaining means for an igniter of the tracer cartridge. - View Dependent Claims (3, 4)
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5. An apparatus for reducing the spread of a hit pattern for a rotationally-stabilized ammunition unit in the form of a projectile shell discharged in a ballistic trajectory from a launching device towards a target which is to be combated, by dynamic balancing of a shell in order to reduce the difference in air resistance between different shells to increase hit probability, comprising;
- an adjustment weight located on one side of the point of gravity of said shell, seen in its longitudinal direction, in the rear plane of said shell substantially perpendicular to the longitudinal axis of said shell for parallel setting of the main axis of inerta of said shell and the geometric axis of the shell casing.
- View Dependent Claims (6, 7, 8)
Specification