US2012210856A1PendingUtilityA1
Multi-Shoot Launcher Comprising a Load-Redirecting Pusher Plate
Est. expiryOct 1, 2029(~3.2 yrs left)· nominal 20-yr term from priority
Inventors:Antonio Paulic
F42B 14/00F42B 14/06F42B 5/035F41F 1/00
42
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Claims
Abstract
Stacked munitions are launched at high velocity from a launcher by redirecting, to the barrel of launcher, the static load that would otherwise be borne by the nose the projectile in position three for launch. This is accomplished via a load-redirecting pusher plate comprising a load-receiving surface and a plurality of compression members.
Claims
exact text as granted — not AI-modified1 . A launcher for launching stacked munitions, comprising:
a barrel having a bore, wherein the bore is dimensioned to contain at least a first munition in a first position for launch, a second munition in a second position for launch, and a third munition in a third position for launch, and wherein the munitions are arranged one behind another; and a load redirecting pusher plate, wherein the load-redirecting pusher plate has a load-receiving surface and at least two compression members, and wherein the load-receiving surface is configured to abuts an aft end of the second munition, and further wherein a distal end of each compression member is in physical contact with and supported against the barrel so that a load generated upon launch of the first munition is received by the load-receiving surface and transferred through the compression members to the barrel.
2 . The launcher of claim 1 wherein the load-redirecting pusher plate has three compression members.
3 . The launcher of claim 1 wherein the load-redirecting pusher plate has a body, wherein a forward surface of the body comprises the load-receiving surface and wherein the compression members are pivotally coupled proximal to an aft end of the body.
4 . The launcher of claim 1 wherein the load-redirecting pusher plate is attached to the aft end of the second munition.
5 . The launcher of claim 1 wherein the barrel comprises slots, wherein the distal end of each compression members is disposed in the slots.
6 . The launcher of claim 1 wherein the load-redirecting pusher plate has a body, wherein the compression members are pivotally coupled, at a proximal end thereof, to an aft end of the body, wherein the pivotal coupling enables the distal end of each compression member to move in a radial direction with respect to the barrel.
7 . The launcher of claim 1 wherein a forward end of the launcher comprises a physical adaptation for keeping water out of the bore of the barrel when the launcher is fired underwater.
8 . The launcher of claim 1 wherein a body of the launcher comprises a plurality of flanged portions that are attached, end to end, to each other.
9 . The launcher of claim 8 wherein the flanged portions are identical to each other.
10 . A launcher for launching stacked munitions, comprising:
a barrel having a bore, wherein the bore is dimensioned to contain at least three munitions that are arranged one behind another; and a load-redirecting pusher plate, wherein the load-redirecting pusher plate has a body having a load-receiving surface and wherein the load-redirecting pusher plate has at least two compression members that are pivotally coupled to an aft end of the body, and further wherein:
(i) the load-redirecting pusher plate is dimensioned and arranged so that the load-receiving surface receives a static load generated upon launch of one of the munitions;
(ii) a distal end of each compression member is received by a respective slot on the inside surface of the barrel, the distal end of the compression members thereby extending radially beyond the bore of the barrel into the slots; and
(iii) the pivotal coupling is arranged so that the distal end of each compression member is capable of moving in a radial direction with respect to the barrel.
11 . The launcher of claim 10 wherein the compression members comprise maraging steel.
12 . The launcher of claim 10 wherein a forward end of the launcher comprises a physical adaptation for keeping water out of the bore of the barrel when the launcher is fired underwater.
13 . The launcher of claim 10 wherein there are a number, n, of munitions in the bore, wherein munitions in positions 2 through n−1 for launch comprise a load-redirecting pusher plate.
14 . The launcher of claim 10 wherein each slot is in fluidic communication with a source of propellant.
15 . The launcher of claim 14 wherein the source of propellant is a cartridge filled with propellant.
16 . The launcher of claim 10 wherein the load-redirecting pusher plate abuts an aft end of the munition in the second position for launch.
17 . A method for launching stacked projectiles, the method comprising:
loading at least three projectiles, one after another, into a first launch position, second launch position, and third launch position in a bore of a barrel of a launcher; igniting propellant for the munition in the first launch position; and redirecting, into the barrel, a static load caused by propellant ignition that the projectile in a third launch position would otherwise be exposed to by: providing a load-receiving surface for receiving the static load; and providing at least two compression members, wherein a first end of each of the two compression members is operatively coupled to the load-receiving surface to receive the static load therefrom and wherein a second end of each of the two compression members is operatively coupled to the barrel for transferring the static load thereto.
18 . (canceled)
19 . The A method of claim 17 for launching stacked projectiles, the method comprising:
loading at least three projectiles, one after another, into a first launch position, second launch position, and third launch position in a bore of a barrel of a launcher;
igniting propellant for the munition in the first launch position;
redirecting, into the barrel, a static load caused by propellant ignition that the projectile in a third launch position would otherwise be exposed to; and
preventing water from entering the bore after the munition in the first launch position is fired.Cited by (0)
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