Munition with multiple propellant chambers

US9500451B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9500451-B2
Application numberUS-201514800023-A
CountryUS
Kind codeB2
Filing dateJul 15, 2015
Priority dateJul 16, 2014
Publication dateNov 22, 2016
Grant dateNov 22, 2016

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A munition includes a projectile and a propellant unit. The propellant unit includes a shell having a cylindrical configuration centered on a longitudinal central axis of the munition. The shell has a cylinder opening that receives a cylinder. The cylinder is selectively rotatable in the cylinder opening about a cylinder axis, offset from the munition axis, between a plurality of firing positions. The cylinder has a plurality of propellant chambers each with a respective propellant charge. The propellant chambers are located in the cylinder so that when the cylinder is in a firing position one of the propellant chambers is on munition axis.

First claim

Opening claim text (preview).

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 having a cylindrical configuration centered on a longitudinal central axis of the munition; the shell having a cylinder opening, the cylinder opening having an cylinder axis that is not coincident with the longitudinal central axis of the munition; and a cylinder received in the cylinder opening of the shell and being selectively rotatable in the cylinder opening about the cylinder axis between a plurality of firing positions; the cylinder having a plurality of propellant chambers each receiving a respective propellant charge and a respective primer, the propellant chambers being located in the cylinder so that when the cylinder is rotated to a firing position one of the propellant chambers with the respective propellant charge including the respective primer rotates to and is centered on the longitudinal central axis of the munition. 2. A munition as set forth in claim 1 wherein the propellant chambers are disposed in a circular array centered on the cylinder axis. 3. A munition as set forth in claim 2 wherein the radial distance between the cylinder axis and the propellant chambers is the same as the distance between the cylinder axis and the munition axis. 4. A munition as set forth in claim 3 wherein the cylinder axis is parallel to but spaced apart from the munition axis. 5. A munition as set forth in claim 3 wherein the cylinder axis is perpendicular to the munition axis. 6. A munition as set forth in claim 3 wherein the propellant charges are the same strength as each other. 7. A munition as set forth in claim 3 wherein the propellant charges are different strengths from each other. 8. A munition as set forth in claim 2 further comprising an index assembly acting between the cylinder and the shell for holding the cylinder in a selected firing position in the cylinder opening: the index assembly comprising a pin located on a radially extending end face of the munition, the pin being engageable in a depression in the cylinder, the index mechanism being operable by depressing the pin using a tool.

Assignees

Inventors

Classifications

  • Adjusting the range without varying elevation angle or propellant charge data, e.g. by venting a part of the propulsive charge gases, or by adjusting the capacity of the cartridge or combustion chamber {(adjusting the range by using gas-relieving ports in the barrel F41A21/28)} · CPC title

  • Arrangements of a multiplicity of primers or detonators dispersed within a propellant charge for increased efficiency · CPC title

  • characterised by the shape and configuration of the base element embedded in the cartridge bottom, e.g. the housing for the squib or percussion cap · CPC title

  • F42B5/16Primary

    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

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Frequently asked questions

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What does patent US9500451B2 cover?
A munition includes a projectile and a propellant unit. The propellant unit includes a shell having a cylindrical configuration centered on a longitudinal central axis of the munition. The shell has a cylinder opening that receives a cylinder. The cylinder is selectively rotatable in the cylinder opening about a cylinder axis, offset from the munition axis, between a plurality of firing positio…
Who is the assignee on this patent?
Safariland Llc
What technology area does this patent fall under?
Primary CPC classification F42B5/16. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Nov 22 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 3 related publications on this page (citations in our corpus or others sharing the same primary CPC).