F42B14/00

SUB-MASS PROJECTILE FOR A FIREARM
20170234665 · 2017-08-17 ·

A sub-mass projectile for a firearm includes a core having a relatively lower mass than a standard projectile for the firearm. A force inducer is associated with the core. The force inducer has an interface that interacts with the firearm. The interface includes a bearing surface with a relatively larger outer diameter than a standard projectile for the firearm. The bearing surface bears against a surface of the firearm during operation so as to increase resistive forces between the sub-mass projectile and the firearm to a magnitude sufficient to approximate the kinetic forces of a standard mass projectile on the firearm during operation.

SUB-MASS PROJECTILE FOR A FIREARM
20170234665 · 2017-08-17 ·

A sub-mass projectile for a firearm includes a core having a relatively lower mass than a standard projectile for the firearm. A force inducer is associated with the core. The force inducer has an interface that interacts with the firearm. The interface includes a bearing surface with a relatively larger outer diameter than a standard projectile for the firearm. The bearing surface bears against a surface of the firearm during operation so as to increase resistive forces between the sub-mass projectile and the firearm to a magnitude sufficient to approximate the kinetic forces of a standard mass projectile on the firearm during operation.

Bullet Stabilization in Subsonic Flight

The present invention relates to increasing the flight stability of a bullet in subsonic flight. The bullet may incorporate features that impart additional angular momentum during flight. Helical fins may be configured such that laminar airflow over the bullet during flight causes the bullet to rotate, increasing the angular momentum of the bullet and stabilizing it during flight. The fins may be self-forming during the use of the bullet or may be formed during manufacturing.

Bullet Stabilization in Subsonic Flight

The present invention relates to increasing the flight stability of a bullet in subsonic flight. The bullet may incorporate features that impart additional angular momentum during flight. Helical fins may be configured such that laminar airflow over the bullet during flight causes the bullet to rotate, increasing the angular momentum of the bullet and stabilizing it during flight. The fins may be self-forming during the use of the bullet or may be formed during manufacturing.

TECHNIQUES FOR RELEASE OF MATERIAL INTO AN ENVIRONMENT

Systems and methods for releasing a material into an environment. The material may be encapsulated in a receptacle or otherwise packaged for movement into the environment. The receptacle with the material inside is introduced into the environment. A triggering causes release of the material from the receptacle into the environment.

Entangling Projectiles and Systems for thier Use
20170276460 · 2017-09-28 ·

An entangling projectile for use in a projectile deployment system includes a pair of pellets and a flexible tether connecting the pellets. Each of the pellets includes an outer diameter and at least one recessed portion extending inwardly from the outer diameter, the recessed portion having an inner diameter smaller than the outer diameter of the pellet such that a pocket is formed in the pellet. The pocket provides an area for accumulation of debris and gasses carried by a pressure wave created by the projectile deployment system. One or more engagement hooks can be coupled to one or both the pellets, or to the tether.

Supercharged accelerating projectile fired in a flight trajectory towards a target
11359895 · 2022-06-14 ·

A projectile system has a projectile with a metal body having a first outside diameter, a forward end and a rearward end, a plastic base wad engaged at the rearward end, the plastic base wad of solid plastic having a first length and a second outside diameter, greater than the first outside diameter, and a rifled barrel having a third inside diameter at the tips of the rifling, the third inside diameter greater than the first outside diameter but less than the second outside diameter, and a fourth diameter at the root of the rifling greater than the second outside diameter. With the projectile translating along the rifled barrel, the metal body passes inside the rifling, avoiding metal to metal friction, while the plastic base wad fully engages the rifling, imparting rotation to the metal projectile.

A BULLET
20220163299 · 2022-05-26 ·

A bullet, having a longitudinal body on which is defined a set of radially spaced, longitudinally extending helical grooves corresponding to the rifling of a particular barrel and at least one circumferential drive band which intersects the set of helical grooves, to define a pressure retaining formation with a casing of a cartridge, in use.

Reduced stiffness barrel fired projectile
11333472 · 2022-05-17 · ·

In various embodiments, a projectile includes a projectile body including a tail portion, a nose portion, a barrel engaging portion between the nose portion and the tail portion, and a metal jacket that defines an exterior of the projectile that surrounds an interior solid core. In one or more embodiments the projectile includes one or more circumferential grooves defined in the interior core portion, each of the one or more circumferential grooves covered by and positioned adjacent to the metal jacket and within the barrel-engaging portion. In various embodiments, during firing of the projectile, the one or more circumferential grooves define a void that allows material of one or more of the metal jacket and interior solid core to displace into the void for reduction in radial stiffness to the projectile in the barrel engaging portion.

Reduced stiffness barrel fired projectile
11333472 · 2022-05-17 · ·

In various embodiments, a projectile includes a projectile body including a tail portion, a nose portion, a barrel engaging portion between the nose portion and the tail portion, and a metal jacket that defines an exterior of the projectile that surrounds an interior solid core. In one or more embodiments the projectile includes one or more circumferential grooves defined in the interior core portion, each of the one or more circumferential grooves covered by and positioned adjacent to the metal jacket and within the barrel-engaging portion. In various embodiments, during firing of the projectile, the one or more circumferential grooves define a void that allows material of one or more of the metal jacket and interior solid core to displace into the void for reduction in radial stiffness to the projectile in the barrel engaging portion.