US2026071859A1PendingUtilityA1

Reduced energy marking cartridges providing a multi-phase firing cycle

60
Assignee: GEN DYNAMICS ORDNANCE & TACTICPriority: Jul 11, 2024Filed: Nov 3, 2025Published: Mar 12, 2026
Est. expiryJul 11, 2044(~18 yrs left)· nominal 20-yr term from priority
F42B 8/10F42B 8/02F42B 12/40F42B 5/045F42B 14/067F42B 14/064
60
PatentIndex Score
0
Cited by
0
References
0
Claims

Abstract

A reduced energy marking cartridge includes a casing supporting a sabot for relative sliding movement and defining a combustion chamber at the breech end of the cartridge and a vent chamber at the muzzle end of the cartridge. An assembly of seals and venting passages in the sabot, which may be in the form of notches, slots or holes, cooperate during the relative movement of the casing and sabot to provide a valving mechanism for controlling the flow of combustion gas from the combustion chamber through the venting chamber and into the acceleration chamber for propelling a projectile from the cartridge.

Claims

exact text as granted — not AI-modified
What is claimed is: 
     
         1 . A reduced-energy cartridge having a multi-phase firing cycle, the cartridge comprising:
 a casing having an axial bore including an aft portion extending from a base at a breech end of the cartridge and a fore portion terminating at a muzzle end of the cartridge;   a sabot including a sabot body, a sabot mouth formed at the muzzle end, a blind bore extending axially from the sabot mouth into the sabot body to form an acceleration chamber, and a vent hole extending through the sabot body into the acceleration chamber, wherein the sabot is telescopically received in the axial bore and coupled to the casing for relative movement from a retracted position to an extended position;   a first seal disposed on the sabot body and engaging the aft portion of the casing to form a combustion chamber between the base and the sabot body;   a second seal disposed on the sabot body between the first seal and the sabot mouth and engaging the fore portion of the casing to form a venting chamber in the fore portion of the casing around the sabot body;   a propellant disposed in the aft portion of the casing and ignitable to produce a combustion gas; and   a projectile releasably disposed in the sabot mouth and configured to be propelled from the sabot;   wherein the multi-phase firing cycle includes:
 a combustion phase, wherein the first seal engages the aft portion to seal the combustion chamber such that combustion gas pressurizes the combustion chamber for sliding the casing relative to the sabot; 
 a firing phase, wherein the first seal disengages the aft portion and fluid communication is established from the combustion chamber for pressurizing the acceleration chamber to propel the projectile from the sabot mouth; and 
 a venting phase, wherein the combustion chamber is in fluid communication with the acceleration chamber through the venting chamber for expelling combustion gas from the casing through the sabot mouth. 
   
     
     
         2 . The reduced-energy cartridge of  claim 1 , wherein the vent hole extends radially through the sabot body into the acceleration chamber. 
     
     
         3 . The reduced-energy cartridge of  claim 1 , wherein the sabot further comprises a diametric slot extending through the breech end of the sabot body to form a sabot chamber, wherein the vent hole extends axially though the sabot body from the sabot chamber to the acceleration chamber. 
     
     
         4 . The reduced-energy cartridge of  claim 1 , further comprising a support element disposed on the sabot body between the first seal and the second seal engaging the fore portion of the casing to support relative movement of the sabot therein. 
     
     
         5 . The reduced-energy cartridge of  claim 4 , wherein the support element comprises at least one protuberance formed on the sabot body. 
     
     
         6 . The reduced-energy cartridge of  claim 1 , further comprising an axially-extending notch at an interface between the first seal and the casing for controlling fluid communication across the first seal. 
     
     
         7 . The reduced-energy cartridge of  claim 1 , wherein the sabot further comprises a blind bore extending into the sabot body from the breech end to form a sabot chamber and a bleed port extending through the sabot body into the sabot chamber;
 the multi-phase firing cycle further comprising an expansion phase after the combustion phase, wherein the bleed port is sealed in the aft portion and the acceleration chamber is in fluid communication with the venting chamber via the vent hole; and   wherein fluid communication is established from the combustion chamber through the bleed port, into the venting chamber, and through the vent hole during the firing phase for pressurizing the acceleration chamber to propel the projectile from the sabot mouth.   
     
     
         8 . The reduced-energy cartridge of  claim 1 , wherein a catch portion of the sabot body is configured to engage the muzzle end of the casing for limiting the sliding of the sabot relative to the casing during the venting phase of the firing cycle. 
     
     
         9 . The reduced-energy cartridge of  claim 1 , wherein the sabot further comprises an axial slot formed in the sabot body and extending from the first seal towards the breech end of the sabot body;
 wherein fluid communication is established from the combustion chamber through the slot, into the venting chamber, and through the vent hole during the firing phase for pressurizing the acceleration chamber to propel the projectile from the sabot mouth.   
     
     
         10 . The reduced-energy cartridge of  claim 1 , wherein the sabot further comprises an annular skirt formed on the breech end of the sabot body, wherein the annular skirt has a reduced outer diameter relative to an outer dimeter of the sabot body. 
     
     
         11 . The reduced-energy cartridge of  claim 1 , wherein a catch portion of the sabot body is configured to engage the muzzle end of the casing for limiting the sliding of the sabot relative to the casing during the venting phase of the firing cycle. 
     
     
         12 . The cartridge case of  claim 11 , wherein the casing comprises a tapered end portion extending from the fore portion to the muzzle end of the casing, wherein the catch portion is configured to engage the casing at an interface between the fore portion and the tapered end portion sabot for limiting the sliding of the sabot relative to the casing during the venting phase of the firing cycle. 
     
     
         13 . The reduced-energy cartridge of  claim 1 , wherein the casing further comprises a primer pocket formed in the base, a flash hole extending through the base from the primer pocket to the combustion chamber, and a primer disposed in the primer pocket for completing the firing sequence. 
     
     
         14 . The reduced-energy cartridge of  claim 1 , wherein the projectile comprises a frangible shell, a marking compound disposed in the frangible shell and a base coupled to the frangible shell for sealing the marking compound therein. 
     
     
         15 . A reduced-energy cartridge having a multi-phase firing cycle comprising:
 a casing having an axial bore including an aft portion extending from a base at a breech end of the cartridge and a fore portion terminating at a muzzle end of the cartridge;   a sabot telescopically received in the axial bore and coupled to the casing for relative movement from a retracted position to an extended position, wherein the sabot includes a sabot body, a sabot mouth formed at the muzzle end, a blind bore extending axially from the sabot mouth into the sabot body to form an acceleration chamber, and a vent hole extending through the sabot body into the acceleration chamber;   a first sealing means forming a combustion chamber at the breech end between the casing and the sabot body;   a second sealing means forming a venting chamber at the muzzle end between the casing and the sabot body;   a propellant disposed in the aft portion of the casing and ignitable to produce a combustion gas; and   a projectile releasably disposed in the sabot mouth and configured to be propelled from the sabot;   wherein the multi-phase firing cycle includes:
 a combustion phase, wherein the sabot is positioned in the casing such that the first sealing means is operable for sealing the vent hole from the combustion chamber for pressurizing the combustion chamber with combustion gas for pushing the sabot forward relative to the casing; 
 a firing phase, wherein the sabot is position in the casing such that the first sealing means and second sealing means are operable for establishing fluid communication from the combustion chamber into the venting chamber through the vent hole and into the acceleration chamber to propel the projectile from the sabot mouth; and 
 a venting phase, wherein the sabot is position in the casing such that the first sealing means and second sealing means are operable for establishing fluid communication from the combustion chamber into the venting chamber through the vent hole and the acceleration chamber and out the sabot mouth for expelling combustion gas from the casing through the sabot mouth. 
   
     
     
         16 . The reduced-energy cartridge of  claim 15 , wherein the vent hole extends radially through the sabot body into the acceleration chamber. 
     
     
         17 . The reduced-energy cartridge of  claim 15 , wherein the sabot further comprises a diametric slot extending through the breech end of the sabot body to form a sabot chamber, wherein the vent hole extends axially though the sabot body from the sabot chamber to the acceleration chamber. 
     
     
         18 . A method for firing a reduced-energy cartridge having a casing, a sabot telescopically received and supported in an axial bore of a casing and for relative axial movement from a retracted position to an extended position, and a projectile releasably disposed in a mouth at a muzzle end of the sabot, the multi-phase firing cycle comprising:
 igniting a propellant in a combustion chamber formed in the casing behind the sabot to generate combustion gas during an ignition phase;   pressurizing the combustion chamber with combustion gas for sliding the casing relative to the sabot during a combustion phase;   positioning the sabot in the casing to direct combustion gas from the combustion chamber through a vent hole formed in the sabot and into an acceleration chamber formed in the sabot for propelling the projectile from the mouth of the sabot during a firing phase; and   positioning the sabot in the casing to direct combustion gas from the combustion chamber into a venting chamber through the vent hole and into the acceleration chamber for expelling the combustion gas from the casing.   
     
     
         19 . The method of  claim 18  further comprising positioning the sabot in the casing to direct combustion gas from the combustion chamber into the venting chamber and through the vent hole for pressurizing the acceleration chamber during the firing phase. 
     
     
         20 . The method of  claim 18  further positioning the sabot in the casing to establish fluid communication from the combustion chamber into the venting chamber during the firing phase; and positioning the sabot in the casing to seal the venting chamber before, during and/or after an expansion phase after the firing phase.

Cited by (0)

No later patents cite this yet.

References (0)

No backward citations on record.