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 of
providing 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 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.
- 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. In a method of manufacture of a gun ammunition projectile including a jacket having an open end and a closed end, the improvement comprising the step of forming a seal for the open end of the jacket from a spherical member disposed within the jacket.
- 8. The improvement of claim 7 wherein said spherical member comprises either a solid metal or a self-supporting pressed quantity of metal powder particles
- 7. The improvement of claim 7 and including the steps of disposing a powder-based core within the jacket, followed by the disposition of said spherical member within the jacket between the core and the open end of the jacket, disposing the jacket and its contained core and spherical member in a die, applying sufficient pressure against said spherical member, hence against said core, to deform said spherical member into a substantially disc geometry, and thereafter in a different die, applying pressure to the closed end of the jacket having the core and disc disposed therein to at least partially close the open end of the jacket and define an ogive on said partially closed end, said latter pressure being sufficient to also deform said disc into a generally hollow hemispherical geometry which seals the at least partially closed open end of the jacket.
- 8. In a projectile including a powder-based core disposed within a jacket having an open end, a closed end and a longitudinal centerline, the improvement comprising a cap formed by die pressing a spherical member disposed within the jacket between the core and the open end of the jacket into a generally hollow hemispherical geometry which is disposed in sealing relationship to the open end of the jacket.
- 9. The improvement of claim 10 wherein said spherical member is formed from a solid metal or a self-supporting pressed quantity of at least one metal powder.
- 10. 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.
- 11. The method of claim 10 and including the step of disposing said spherical member within said concavity preparatory to the application of pressure against said spherical member.
- 12. 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
[0001] 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.
Provisional Applications (1)
|
Number |
Date |
Country |
|
60291173 |
May 2001 |
US |