Munition with unexploded ordnance limiting

Patent metadata

Field	Value
Publication number	US-9618306-B2
Application number	US-201514878355-A
Country	US
Kind code	B2
Filing date	Oct 8, 2015
Priority date	Oct 9, 2014
Publication date	Apr 11, 2017
Grant date	Apr 11, 2017

Abstract

A munition includes a projectile and a propellant unit. A propellant insert in the propellant unit has at least two propellant chambers each receiving a respective propellant charge. A primer mechanism is actuatable to ignite all of the propellant charges in the propellant insert. The combustion products of a selected one of the propellant charges are directed to the projectile and the combustion products of the non-selected propellant charges are vented.

First claim

The invention claimed is:

1. A munition receivable in a chamber of a projectile launcher, the munition comprising:
a projectile; and
a propellant unit that is actuatable to produce gas under pressure, the projectile being releasably connected with the propellant unit and receiving force of the gas under pressure to cause the projectile to release from the propellant unit and travel from the launcher toward a target, the propellant unit comprising:
a shell;
a cylinder selectively rotatable in the shell between a plurality of firing positions;
the cylinder having at least two propellant chambers each receiving a respective propellant charge;
a primer mechanism for igniting all of the propellant charges in the cylinder;
the shell having a first passage for directing combustion products of a selected one of the propellant charges to the projectile and having a second passage for venting combustion products of all non-selected propellant charges.

2. A munition as set forth in claim 1 further comprising an index assembly acting between the cylinder and the shell for holding the cylinder in a selected firing position in the shell.

3. A munition as set forth in claim 2 wherein the propellant chamber of the selected one of the propellant charges is in fluid communication with the first passage and the propellant chambers of all non-selected propellant charges are in fluid communication with the second passage, when the cylinder is in the selected firing position.

4. A munition as set forth in claim 2 wherein the portion of the shell that is downstream of the cylinder chamber is formed as a manifold that includes one through passage that extends from the downstream end of the cylinder to a projectile chamber and that is circumferentially and radially positioned so that when the cylinder is in the selected firing position one and only one of the propellant chambers opens into the through passage, the through passage constituting the first passage.

5. A munition as set forth in claim 4 wherein the second passage comprises a plurality of vent passages in the manifold that extend from the downstream end of the non-selected propellant chambers to a vent chamber in the manifold, the vent chamber opening on the radially outer side surface of the manifold, upstream of the projectile.

6. A munition as set forth in claim 1 wherein the primer mechanism includes a primer in a primer cavity and a plurality of flow passages directing combustion products of the primer from the primer cavity to all of the propellant charges to ignite all of the propellant charges in the cylinder.

7. A munition as set forth in claim 6 wherein the cylinder has an upstream end surface on which the flow passages are formed.

8. A munition as set forth in claim 1 including a movable member in the cylinder that is selectively movable between a first position that allows flow of combustion products from the primer to the propellant chambers to ignite the propellant charges and a second position that blocks flow of combustion products between the propellant chambers after the propellant charges are ignited.

9. A munition as set forth in claim 8 wherein the movable member is biased to the second position and is moved from the second position to the first position under the influence of the force of the combustion products of the primer.

10. A munition receivable in a chamber of a projectile launcher, the munition comprising:
a projectile; and
a propellant unit that is actuatable to produce gas under pressure, the projectile being releasably connected with the propellant unit and receiving force of the gas under pressure to cause the projectile to release from the propellant unit and travel from the launcher toward a target, the propellant unit comprising:
a shell;
a propellant insert in the shell and having at least two propellant chambers each receiving a respective propellant charge;
a primer mechanism for igniting all of the propellant charges in the propellant insert; and
the shell having a first passage for directing combustion products of a selected one of the propellant charges to the projectile and having a second passage for venting combustion products of all non-selected propellant charges;
wherein the propellant insert is a cylinder rotatably supported in the shell between a plurality of firing positions, and wherein the munition includes an index assembly acting between the cylinder and the shell for holding the cylinder in a selected firing position in the shell.

11. A munition as set forth in claim 10 wherein the propellant chamber of the selected one of the propellant charges is in fluid communication with the projectile and the propellant chambers of all non-selected propellant charges are in fluid communication with a vent chamber when the cylinder is in the selected firing position.

12. A munition as set forth in claim 10 wherein the primer mechanism includes a primer in a primer cavity and a plurality of flow passages directing combustion products of the primer to all of the propellant charges to ignite all of the propellant charges in the propellant insert.

Assignees

• Safariland Llc

Inventors

• Hultman John

Classifications

• F42B5/02

  Cartridges, i.e. cases with charge and missile · CPC title

• F42B15/00 Primary

  Self-propelled projectiles or missiles, e.g. rockets; Guided missiles (F42B10/00, F42B12/00, F42B14/00 take precedence; for practice or training F42B8/12; rocket torpedoes F42B17/00; marine torpedoes F42B19/00; cosmonautic vehicles B64G; jet-propulsion plants F02K) · CPC title

• F42B12/20

  of high-explosive type (F42B12/44 takes precedence) · CPC title

• F42B5/16

  characterised by composition or physical dimensions or form of propellant charge, {with or without projectile,} or powder (chemical composition C06B; {F42B5/24 takes precedence}) · CPC title

• F42B5/025 Primary

  characterised by the dimension of the case or the missile · CPC title