초록 ▼

A projectile for use in firearms and of the type having on one end a hemispherical tip which communicates at its base with a nose segment which then attaches to a cylindrical body terminating in a surface whose width represents the diameter of the aforementioned cylindrical body. One or many parts o

A projectile for use in firearms and of the type having on one end a hemispherical tip which communicates at its base with a nose segment which then attaches to a cylindrical body terminating in a surface whose width represents the diameter of the aforementioned cylindrical body. One or many parts of the projectile are coated or plated in a material that creates a surface featuring recesses when it hardens. This surface acts as an aerodynamic aid when the projectile is in flight. The coating or plating may be applied directly to the projectile or layered on top of a jacket.

대표청구항 ▼

What is claimed is: 1. A munitions projectile comprising a forward portion that includes a nose segment, a jacket that surrounds the nose segment and presents an exterior surface that has a conical or hemispherical shape, and added material provided at a thickness of between about 0.001 and 0. 005

What is claimed is: 1. A munitions projectile comprising a forward portion that includes a nose segment, a jacket that surrounds the nose segment and presents an exterior surface that has a conical or hemispherical shape, and added material provided at a thickness of between about 0.001 and 0. 005 inch in the form of a metal coating, a metal alloy coating, a metal plating or a metal alloy plating provided on the jacket and which defines a pattern of raised surface area portions predominantly covering the exterior surface of the jacket of the projectile to provide improved aerodynamic properties to the projectile compared to munition projectiles that do not include such added material. 2. The projectile of claim 1, wherein the pattern of the added material defines a plurality of uncoated or unplated portions that appear to be recesses. 3. The projectile of claim 2, wherein the pattern of the added material defines recesses in the shape of concave dimples. 4. The projectile of claim 1, wherein the jacket is made of a metal or alloy. 5. The projectile of claim 1, having a hemispherical tip and a rearward cylindrical portion. 6. The projectile of claim 1, wherein the exterior surface of the jacket is made of a metal or alloy. 7. The projectile of claim 1, having a conical nose segment and jacket and a rearward cylindrical portion. 8. In a munitions projectile that has a forward portion that includes a nose segment, a jacket that surrounds the nose segment and presents an exterior surface that has a conical or hemispherical shape, the improvement comprising added material provided at a thickness of between about 0.001 and 0.005 inch in the form of a metal coating, a metal alloy coating, a metal plating or a metal alloy plating provided on the jacket and provided in a pattern of raised surface area portions predominantly covering the exterior surface of the jacket of the projectile to provide improved aerodynamic properties to the projectile compared to munition projectiles that do not include such added material. 9. The projectile of claim 8, wherein the exterior surface of the jacket is made of a metal or alloy. 10. The projectile of claim 8, having a conical nose segment and jacket and a rearward cylindrical portion. 11. The projectile of claim 8, having a hemispherical tip and a rearward cylindrical portion. 12. A method for enhancing aerodynamic properties of a munitions projectile that includes a forward portion that includes a nose segment, a jacket that surrounds the nose segment and presents an exterior surface that has a conical or hemispherical shape, which method comprises providing added material provided at a thickness of between about 0.001 and 0.005 inch in the form of a metal coating, a metal alloy coating, a metal plating or a metal alloy plating provided on the jacket and in a pattern of raised surface area portions predominantly covering the exterior surface of the jacket of the projectile to provide improved aerodynamic properties to the projectile compared to munition projectiles that do not include such added material. 13. The method of claim 12 wherein the pattern is provided by selectively coating the exterior surface. 14. The method of claim 12 wherein the pattern is provided by masking the exterior surface to provide a mask where the raised areas are not desired, coating or plating the surface and then removing the mask. 15. The method of claim 12 wherein the pattern is provided by uniformly coating or plating the exterior surface and then removing portions of the coating or plating where raised areas are not desired. 16. The method of claim 12, wherein the exterior surface of the jacket is made of a metal or alloy. 17. The method of claim 12, having a conical nose segment and jacket and a rearward cylindrical portion. 18. The method of claim 12, wherein the projectile has a hemispherical tip and a rearward cylindrical portion.