Ammunition round

Claim 2

A fully telescoped ammunition round comprising: a propellant charge means having an axial cavity for supplying firing power for said ammunition round; a projectile means housed within said cavity for being fired from said ammunition round; a control tube means for selectively covering portions of said propellant charge means facing said axial cavity thereby putting selected portions of said propellant charge in communication with said axial cavity and being generally positioned between said propellant charge means and said projectile means, said projectile means extending forward of said control tube means and including coupling means for releasably securing said projectile means to said control tube means; a primer means positioned generally aft of said projectile means for providing a firing force as part of a firing sequence from said ammunition round; said control tube means including a first firing opening for providing an access to said propellant charge means from said axial cavity so that temperature and pressure conditions within said axial cavity adjacent said first firing opening can act on said propellant means thus providing for firing of said propellant charge means; said first firing opening being positioned intermediate the axial ends of said control tube means; said control tube means having a second firing opening circumferentially displaced from said first firing opening; said control tube means including slotted means forward of said first firing opening for providing a communication path between said propellant charge and said axial cavity for reducing the pressure differential across said control tube means when said propellant charge is fired; sealing means for separating said axial cavity into a forward portion and aft portion, said sealing means being conditionable between a first condition separating said primer means and said first firing opening thus providing a barrier between said primer means and said propellant means and a second condition permitting communication between said propellent means and said primer means through said firing opening; said sealing means including a piston means positioned aft of said projectile means so that forward motion of said piston means within said axial cavity causes forward motion of said projectile means within said cavity; and said piston means having a generally cylindrical outer shape, a rearwardly opening recess means for receiving a charge and a skirt means extending circumferentially around said piston means for obstructing the flow of combustion gases between said piston means and said control tube means.

Claim 3

An ammunition round as recited in claim 1 wherein said piston means and said projectile means are integral.

Claim 4

An ammunition round as recited in claim 1 wherein said primer means includes a primer charge positioned aft of said piston means and a booster charge positioned within said rearwardly opening recess, said primer and booster charges being sufficiently close together so that ignition of said primer charge causes ignition of said booster charge and causes a forward movement of said piston means within said axial cavity and thus forward movement of said projectile means within said axial cavity.

Claim 5

An ammunition round as recited in claim 1 wherein said sealing means and said projectile means are integral, said first firing opening is forward of the aft end of said projectile means and forward motion of said projectile means is necessary to put said propellant charge means in communication with said primer means through said first firing opening thus permitting sequential ignition of said propellant charge means and said primer means as a function of the physical position of said projectile means within said axial cavity.

Claim 6

An ammunition round as recited in claim 1 wherein said first firing opening is forward of the aft end of said piston means and forward motion of said piston means is necessary to put said propellant charge means in communication with said primer means through said first firing opening thus permitting sequential ignition of said propellant charge means and said primer means as a function of the physical position of said piston means within said axial cavity.

Claim 7

An ammunition round as recited in claim 5 further comprising an igniter charge positioned adjacent said propellant charge means at said first firing opening, said igniter charge providing for the firing of said propellant charge means.

Claim 8

An ammunition round as recited in claim 5 wherein said control tube means is sufficiently axially elongated so that it can circumferentially surround, in a direction transverse to the longitudinal axis of said axial cavity, said primer means, said piston means and only a portion of said projectile means.

Claim 9

A fully telescoped ammunition round comprising: a propellant charge having an axial cavity for supplying firing power for said ammunition round; a projectile means housed within said cavity for being fired from said ammunition round, said projectile means being elongated in a direction along the axis of said axial cavity; a primer means positioned generally aft of said projectile means for providing a firing force as part of a firing sequence for firing said projectile means from said ammunition round; a piston means positioned aft of said projectile means so that forward motion of said piston means within said axial cavity causes forward motion of said projectile means within said axial cavity and said piston means includes a circumferential, radially extending skirt thereby providing a seal isolating the portion of said axial cavity forward of said skirt from the portion of said axial cavity aft of said skirt, said skirt acting as a seal so a force caused by firing of said primer means is transferred to said piston means thus causing forward motion, and said piston means further including a rearwardly opening recess so that said skirt generally surrounds the periphery of said recess; a primer charge portion of said primer means being positioned aft of said piston means and a booster charge portion of said primer means being positioned within said recess and being positioned sufficiently close so that firing of said primer charge portion causes firing of said booster charge portion and results in forward motion of said piston means and projectile means; a control tube means positioned within said axial cavity and laterally surrounding said primer means and said piston means thereby directing a force from the firing of said primer means along the axis of said axial cavity, said control tube means having a first firing opening extending radially through the wall of said control tube means thereby providing a path of communication between said axial cavity and said propellant charge, said first firing opening being positioned forward of said skirt so that said first firing opening is initially isolated from said primer means by said piston means and is in communication with said primer means after firing of said primer means and movement of said skirt forward of said first firing opening thus causing firing of said piston means along said axial cavity, and said first firing opening being positioned intermediate the axial ends of said control tube means; said control tube means having a second firing opening circumferentially displaced from said first firing opening, said control tube means extending forward over at least a portion of said projectile means and further including coupling means for releasably securing said projectile means to said control tube means; said coupling means includes an inwardly facing circumferential groove within said control tube means, an outwardly facing circumferential groove around said projectile means, said grooves positioned to be aligned when said control tube means and said projectile means are in said ammunition round, and a retainer ring adapted to be positioned within said inwardly and outwardly facing grooves and to shear in response to a predetermined pressure applied to said projectile means thereby releasably securing said projectile means and said control tube means to each other; said control tube means including slotted means forward of said first firing opening for providing a communication path between said propellant charge and said axial cavity and for reducing the pressure differential across said control tube means when said propellant charge is fired; and said control tube means and said piston means being fabricated of a combustibly consumable material having sufficient initial resistance to combustion so that said primer means is isolated from the propellant charge for a period of time after firing of said primer means and so that the piston means can physically cause movement of the projectile means.

Claim 10

A fully telescoped ammunition round comprising: a propellant charge having an axial cavity for supplying firing power for said ammunition round; a projectile means housed within said cavity for being fired from said ammunition round, said projectile means being elongated in a direction along the axis of said axial cavity; a primer means positioned generally aft of said projectile means for providing a firing force as part of a firing sequence for firing said projectile means from said ammunition round; a piston means positioned aft of said projectile means so that forward motion of said piston means within said axial cavity causes forward motion of said projectile means within said axial cavity and said piston means includes a circumferential, radially extending skirt thereby providing a seal isolating the portion of said axial cavity forward of said skirt from the portion of said axial cavity aft of said skirt, said skirt acting as a seal so a force caused by firing of said primer means is transferred to said piston means thus causing forward motion, and said piston means further including a rearwardly opening recess so that said skirt generally surrounds the periphery of said recess; a primer charge portion of said primer means being positioned aft of said piston means and a booster charge portion of said primer means being positioned within said recess and being positioned sufficiently close so that firing of said primer charge portion causes firing of said booster charge portion and results in forward motion of said piston means and projectile means; a control tube means positioned within said axial cavity and laterally surrounding said primer means and said piston means thereby directing a force from the firing of said primer means along the axis of said axial cavity, said control tube means having a first firing opening extending radially through the wall of said control tube means thereby providing a path of communication between said axial cavity and said propellant charge, said first firing opening being positioned forward of said skirt so that said first firing opening is initially isolated from said primer means by said piston means and is in communication with said primer means after firing of said primer means and movement of said skirt forward of said first firing opening thus causing firing of said piston means along said axial cavity, and said first firing opening being positioned intermediate the axial ends of said control tube means; said control tube means having a second firing opening circumferentially displaced from said first firing opening, said control tube means extending forward over at least a portion of said projectile means and further including coupling means for releasably securing said projectile means to said control tube means; said coupling means includes an inwardly facing circumferential groove within said control tube means, an outwardly facing circumferential groove around said projectile means, said grooves positioned to be aligned when said control tube means and said projectile means are in said ammunition round, and a retainer ring adapted to be positioned within said inwardly and outwardly facing grooves and to shear in response to a predetermined pressure applied to said projectile means thereby releasably securing said projectile means and said control tube means to each other; said control tube means including slotted means forward of said first firing opening for providing a communication path between said propellant charge and said axial cavity and for reducing the pressure differential across said control tube means when said propellant charge is fired; and said control tube means and said piston means being fabricated of a combustibly consumable material having sufficient initial resistance to combustion so that said primer means is isolated from the propellant charge for a period of time after firing of said primer means and so that the piston means can physically cause movement of the projectile means.