Claims
- 1. A method of manufacturing a gun ammunition multi-component projectile including at least one powder-based core disposed within a jacket of generally cup-shape having a closed end and an open end and a longitudinal centerline comprising the steps ofproviding a spherical member of either a solid metal or a self-supporting pressed compact of at least one metal powder, disposing said spherical member within the jacket and between the core and the open end of the jacket, with the jacket/core/spherical member combination disposed within a first die cavity, applying sufficient pressure to said spherical member in a direction axially along the longitudinal centerline of the jacket to deform said spherical member into a generally flat disc which extends radially across the cross-sectional area of the jacket adjacent the core, disposing said pressed jacket/core/disc combination in a second die cavity suitable for at least partial closing of the open end of the jacket and formation of an ogive on said at least partially closed end of the jacket, including deformation of said disc into a generally hollow hemispherical geometry and disposed in sealing relationship to the at least partially closed end of the jacket, at least a portion f said at least one powder-based core substantially filling said generally hollow hemispherical deformed disc.
- 2. The method of claim 1 wherein said spherical member comprises a solid metal ball.
- 3. The method of claim 1 wherein said spherical member comprises a spherical compact formed from a quantity of pressed metal powder.
- 4. The method of claim 1 wherein said spherical member comprises tin, zinc, copper, iron, magnesium, aluminum, or a mixture or an alloy of two or more of said metals.
- 5. The method claim 4 wherein each of said metals is in its powdered form.
- 6. The method of claim 1 wherein said step of providing a spherical member includes compressing a quantity of metal powder particles into a self-supporting spherical member preparatory to disposition of said spherical member within the jacket.
- 7. The method of claim 1 wherein said core is of generally straight cylindrical geometry and includes a substantially flat face disposed adjacent the open end of the jacket, and including the step of forming a concavity centrally disposed of the flat face of the core.
- 8. The method of claim 7 and including the step of disposing said spherical member within said concavity preparatory to the application of pressure against said spherical member.
- 9. The method of claim 1 wherein the diameter of said spherical member is about 0.002 inch less in diameter than the internal diameter of the jacket at its open end.
RELATED INVENTIONS
The present application is a non-provisional application based on Provisional Application Ser. No. 60/291,173, filed May 15, 2001, entitled: METHOD FOR THE MANUFACTURE OF A SOLID CAP FOR A MULTI-COMPONENT AMMUNITION PROJECTILE AND PRODUCT.
US Referenced Citations (6)
Provisional Applications (1)
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Number |
Date |
Country |
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60/291173 |
May 2001 |
US |