Ammunition round

• US 4,782,758 A
• Filed: 12/16/1986
• Issued: 11/08/1988
• Est. Priority Date: 02/03/1986
• Status: Expired due to Term

• Current Assignee: Aerojet-General Corporation (L3Harris Technologies, Inc.)
• Original Assignee: Aerojet-General Corporation (L3Harris Technologies, Inc.)
• Inventors: Washburn, William J.
• Primary Examiner(s): Tudor, Harold J.
• Application Number:
  US06/942,553
• Time in Patent Office: 693 Days
• Field of Search: 102/430-434, 102/443, 102/501, 102/439
• US Class Current: 102/434
• CPC Class Codes: F42B 5/045 of telescopic type F42B5/184 takes precedence

Abstract

An improved telescoped ammunition round having a projectile comprising an aft recess to receive a booster tube that is affixed to the cartridge case and which remains stationary relative to the cartridge case throughout the firing sequence. The booster tube is provided with a primer to ignite the booster charge and is positioned within the projectile recess to initially propel the projectile and subsequently ignite the main propellant within the cartridge case after the projectile has been forced at least partially into the gun barrel.

Claims

1. An improved telescoped ammunition round having a projectile and a cartridge case, said cartridge case having a main propellant charge forming an axial bore for receiving said projectile, the projectile having a forward end and an aft end;

the improvement comprising;

an imperforate booster tube having (1) a closed first end affixed to said cartridge case adjacent the aft end of said projectile and extending toward said projectile within said axial bore to an open second end, and (2) a first annular recess formed in an external surface of said booster,

said projectile being contained within said cartridge case and having an axial recess extending from its aft end for receiving said second end of said booster tube, said axial recess including an internal conical portion, a cylindrical portion and a second annular recess interfacing with said conical portion and said cylindrical portion therebetween, where said internal conical portion extends from said projectile aft end toward said second annular recess,

said booster tube including a frangible retaining means for releasably coupling said projectile to said booster tube when each of said respective first and second annular recesses are aligned each to the other, said frangible retaining means being contained at least partially within each of said annular recesses, said booster tube further having means for generating ignition gases within said projectile recess for propelling said projectile away from said booster tube within said bore whereby said gases are exposed to said main propellant charge at said second end of said booster tube for igniting said main propellant charge after predetermined motion of said projectile.

3. The improved round of claim 1 wherein said cartridge case comprises a threaded aperture adjacent the aft end of said projectile and wherein said booster tube comprises a threaded portion for threadably mating said cartridge case within said threaded aperture.

4. The improved round of claim 1 wherein said means for generating ignition gases comprises a booster charge within said booster tube and a primer in communication with said booster charge and accessible external of said cartridge case.

2. The improved round of claim where said frangible retaining means is sheared upon motion of said projectile in response to said ignition gases.