Payload mechanism for low impulse cartridges

Information

  • Patent Grant
  • 6324984
  • Patent Number
    6,324,984
  • Date Filed
    Thursday, August 3, 2000
    24 years ago
  • Date Issued
    Tuesday, December 4, 2001
    23 years ago
Abstract
This low impulse payload cartridge for automatic weapons includes a case, a piston, an ogive, a payload cup, a payload, and a link. The payload cup and payload is seated into the forward portion of the piston. Gas passages permit propellant gases to bleed into the cavity behind the payload and to accelerate the payload upon firing. An alternative to using bleed gases is to use a separate propelling charge behind the payload. The case and piston are assembled and telescopically secured by means of a crimp or other similar feature, to allow relative movement therebetween during chambering and firing. The link may be allowed to move for some portion of the required relative travel between the link and the base of the case. A shoulder on the piston provides a stop through which reaction loads are transmitted to the rear of the barrel during chambering and firing. The piston telescopes over the case during chambering to provide the relative movement between the link and the case base required for weapon function. The relative movement between the piston and the case also allow the payload cup to be forced through the end of the piston. Upon firing, the expanding propellant gases force the case and piston to telescope open. Propellant gases are also used to expel the payload. Reaction loads are applied to the rear of the barrel through the shoulder, and at the same time are applied to a bolt, driving it rearward to cycle the weapon. The cartridge can be used in automatic weapon systems including but not limited to the 40 mm MK19 Grenade Machinegun.
Description




U.S. GOVERNMENT INTEREST




The invention described herein may be manufactured, used, or licensed by or for the U.S. Government for U.S. Government purposes without the payment of any royalties thereon.




BACKGROUND OF THE INVENTION




I. Field of Invention




This invention applies to the field of weapons and cartridges which are capable of firing low impulse non-lethal payloads and other payloads from automatic weapons.




The present invention relates in general to the field of ammunition, and it particularly relates to a payload mechanism for low impulse cartridges used in automatic weapons. More specifically, the present invention relates to a low impulse payload cartridge for use in automatic weapon systems such as the 40 mm MK19 Grenade Machinegun, though the inventive concept is applicable to any caliber of weapon and ammunition. The present invention relates to co-pending U.S. patent application Ser. No. 09/351,978 now patented, U.S. Pat. No. 6,178,889 to Frank Dindl, titled “Low Impulse Telescoping Cartridge”, filed on Jul. 12, 1999, and commonly assigned to the assignee of the present invention, which is incorporated herein in its entirety.




II. Background of the Invention




Payload type munitions (non-lethal multiple rubber balls, bean bags, foam batons, wood batons, etc.) have been mostly limited to single shot or manually operated weapons, with of course the exception of shotguns and other weapons purposely designed to work with shot shell cylindrical cartridges.




The U.S. Military, however, has the need to fire payload type munitions from such automatic weapons as the 40 mm MK19 Grenade Machine Gun. Such weapons fire lethal rounds which use rounded tips to provide reliable weapon function. On the other hand, payload type munitions require an opening in the tip of the cartridges to allow payloads to be launched.




Automatic weapons such as the 40 mm MK19 Grenade Machinegun are designed to use ammunition with a specific external envelope. The external dimensions of a payload cartridge must be compatible with the weapon from which it is fired. The cartridge configuration must also withstand the forces encountered during weapon feeding and cycling.




Additionally, the typical opening for launching a payload can be described as cylindrical. Since a simple cylindrical cartridge tip is normally not reliably compatible with most automatic weapon mechanisms, a cover must be provided to provide the necessary external cartridge dimensions and be robust to withstand the forces encountered during weapon operation. However, the cover must open on firing to allow the payload to be expelled.




In summary, there is a great and still unsatisfied need for a payload mechanism for low impulse cartridges used in automatic weapons. Exemplary payloads include liquids, solids and powders, and include nonlethal payloads such as rubber balls, wood batons, foam batons, and rubber projectiles. A need also exists for firing obscurant payloads, which are typically powdered materials.




Accordingly it is an object of this invention to provide the rounded nose configuration essential for reliable weapon function in weapons such as the 40 mm MK19GMG, while at the same time providing the requisite payload for launch.




Another object is to provide a low impulse payload cartridge with an external configuration which is compatible with conventional automatic weapon systems such as the 40 mm MK19 Grenade Machinegun.




Yet, another feature of the present invention is to provide an ammunition configuration that provides a cylindrical opening for launching the payload where the opening approaches the size of bore of the weapon barrel to allow for the launching of low velocity and/or low mass projectiles or payloads such as non-lethal multiple rubber balls, batons, rubber projectiles, powders, and a variety of other low impulse projectile configurations while functioning the MK19 Grenade Machinegun or other firearms in a fully automatic mode.




Finally, another feature of the present invention is to provide a fully automatic weapon function without requiring changes to the weapon itself, while permitting effective firing of reduced velocity and/or reduced mass projectiles. These and other features and advantages of the invention are achieved by a low impulse payload cartridge. Other objects of this invention will appear hereinafter.




SUMMARY OF INVENTION




It has now been discovered that the above and other objects of the present invention may be accomplished in the following manner. Specifically, the invention provides the rounded nose configuration essential for reliable weapon function with low impulse cartridges. This is accomplished upon chambering of the round of ammunition when the internal payload cup is forced through the nose, exposing the payload, allowing straight forward launch of the payload.




The cartridge configuration includes a payload mechanism which consists of a cup containing the payload. The cartridge nose configuration provides the external shape required for compatibility with the weapon while allowing the payload cup to pierce the cartridge nose upon firing to allow the launching of the payload.




During the operation of the 40 mm MK19 Grenade Machinegun using the cartridge of the present invention, the cartridge travels through the weapon feed mechanism. The outside configuration of the cartridge and the position of the link is preferably constrained to that of conventional ammunition to be compatible with the weapon. The link and cartridge are restrained during the delinking operation and cartridge pickup as the bolt reaches the battery position. As the bolt is returned rearward, the cartridge is cammed down the bolt face into alignment with the barrel. As the bolt moves forward to the battery position, the cartridge is chambered. Upon firing, the payload cup is forced through the nose of the cartridge by either the expanding propellant gases or telescoping action of the cartridge case. Expanding propellant gases from the primary propellant charge in the base of the cartridge case or from a secondary charge in the base of the payload cup propels the payload from the payload cup and launches the payload from the weapon. A shoulder on the outer surface of the payload cup stops against a mating surface on the inside of the piston to prevent the payload cup from being ejected during firing. Reaction loads are applied to the barrel through the shoulder and through the base of the cartridge to the bolt. The energy imparted to the bolt accelerates the bolt rearward and cycles the weapon.




The present invention enables the practical and efficient use of low impulse payload ammunition in an unmodified automatic weapon such as the MK19 Grenade Machinegun.




In one embodiment, the secondary propellant charge can be used as an alternative to bleeding propellant gases from the primary propellant charge, in order to accelerate the projectile.











BRIEF DESCRIPTION OF THE DRAWINGS




The features of the present invention and the manner of attaining them will become apparent, and the invention itself will be understood by reference to the following description and the accompanying drawings. In these drawings, like numerals refer to the same or similar elements. The sizes of the different components in the figures might not be in exact proportion, and are shown for visual clarity and for the purpose of explanation.





FIG. 1

is a side elevational view of a low impulse payload cartridge according to the present invention.





FIG. 2

is a cross-sectional view of the payload cartridge of

FIG. 1

taken along line


2





2


, for illustrating the cartridge configuration during feeding prior to chambering.





FIG. 3

is a side elevational view of the cartridge of

FIGS. 1 and 2

, shown fully chambered where the payload cup has pierced the tip of the cartridge to allow ejection of the payload.





FIG. 4

is a cross-sectional view of the cartridge of

FIG. 3

taken along line


4





4


.





FIG. 5

is a side elevational view of the cartridges of

FIGS. 3-4

, shown after firing;





FIG. 6

is cross-sectional view of the cartridge of

FIG. 5

, shown after firing, taken along line


6





6


.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS




A low impulse, telescoping cartridge


100


according to a first embodiment of the present invention is depicted in

FIGS. 1 through 6

. With particular reference to

FIGS. 1

,


2


and


3


, the cartridge


100


is generally comprised of five main components; a projectile or payload


102


, a cup


122


, a piston


104


, a case


110


, and a link


112


. The cartridge case


110


contains a primer


113


to provide ignition. A propellant


116


provides the required propulsion energy to function a weapon. A crimp


111


or another similar or equivalent feature secures the case


110


relative to the piston


104


in such a manner that allows for the cartridge


100


telescoping function, that prevents the case


110


from separating from the piston


104


, and that further prevents cartridge telescoping during the delinking process while feeding. The overall outer configuration of the cartridge


100


matches the outer configuration of a conventional ammunition where the cartridge interfaces with the weapon, to the extent necessary for reliable weapon operation.




The cartridge case


110


fits into the rear portion


104


R of the piston


104


such that a portion of the outer wall


110


W of the cartridge case


110


mates with the inner wall


117


of the piston


104


to provide a seal for containing the propellant gases. The piston


104


further includes a shoulder


114


that protrudes outwardly from the periphery of the piston


104


to provide a stop for the barrel


118


when the cartridge


100


is fully chambered. The shoulder


114


limits the travel distance of the piston


104


within the barrel


118


. The shoulder


114


also provides a mechanism through which the reaction forces are transmitted from the piston


104


to the rear surface or breech


119


of the barrel


118


.




As

FIGS. 3 and 4

show, during chambering, the case


110


is forced into the piston


104


. The case


110


forces the cup


122


forward and through the end of the piston


104


to create an opening through which the payload


102


may be ejected.




From

FIG. 5

, during firing, the expanding propelling gases force the piston


104


to telescope open relative to the case


110


. Now

FIG. 6

shows the shoulder


114


provides the load path for reacting against the barrel


118


. Simultaneously, the case


110


provides a load path to react against a bolt


145


in order to function the weapon in a fully automated mode.




The expanding propellant gases in this embodiment from the primary propellant charge


116


ignite the secondary propellant charge


157


directly or by initiating a secondary primer


150


. Alternatively, a vent hole


300


may be used in place of the secondary primer


150


to allow ignition of the secondary propellant charge


157


directly. Another alternative uses a vent hole


300


in place of the secondary primer


150


and secondary propellant charge


157


. The propellant gases from the primary propellant charge


116


bleed through the vent hole


300


and act against the wad


160


directly to face the payload


102


from the payload cup


122


.




The cartridge


100


is assembled by inserting the propellant


116


and the primer


113


in the case


110


. The primer


150


, if used is inserted into the payload cup


122


. The propellant


157


, if used, is inserted into the payload cup


122


. The wad


160


is installed over the propellant


157


in the payload cup


122


. The payload


102


is inserted in front of the wad


160


in the payload cup


122


. The payload cup


122


is inserted into the piston


104


. The case


110


is assembled to the piston


104


. The base


111


B of the piston


104


is crimped over a flange


110


F of the case


110


to secure the piston


104


and the case


110


in a telescoping relationship. The link


112


is assembled by sliding it over the piston


104


. The link


112


is fitted over the shoulder


114


.




Having described the general components of the cartridge


100


, its operation or use will now be explained in connection with

FIGS. 1-6

. The use of the cartridge


100


can be separated into three general stages: feeding; chambering; and firing.




Feeding




The feeding stage is illustrated in

FIGS. 1

,


2


. In this stage, the cartridge


100


is in the fully extended or “telescope open” position. A drive spring


131


pushes against a bolt


145


, which, in turn, pushes the cartridge


100


inside the barrel


118


, in the direction of the arrow F.




In the case of the 40 mm MK19 Grenade Machinegun, during the feeding stage the cartridge


100


resists telescoping in the delinking process of the weapon operation. The interface between the piston


104


and the cartridge case


110


provides a crimp


111


, adhesive or other means of preventing the case


110


and piston


104


from telescoping until the cartridge


100


is chambered.




Chambering




The chambering stage is illustrated in

FIGS. 3

, and


4


. As the cartridge


100


is chambered, the shoulder


114


contacts the rear surface or breech


119


of the barrel


118


. The resistance exerted by the crimp


111


at the interface between the piston


104


and the cartridge case


110


is overcome, and the piston


104


and the cartridge case


110


telescope to the closed (or compacted) position.




The case


110


pushes the cup


122


forward. The cup


122


pierces the end of the piston


104


to create an opening expelling the piston cover


161


through which the payload


102


may now be expelled. Alternatively, the gas pressure from firing may be used to force the cup


122


forward to pierce the piston


104


. The cup


122


is prevented from being ejected or expelled by the gases by a flange


162


located on the outer surface of cup


122


. The flange


162


stops against a mating surface


163


on the inside of piston


104


.




Firing




The firing stage is illustrated in

FIGS. 5 and 6

. Upon ignition of the primer


113


, the propellant


116


ignites and pressurizes the cartridge


100


. The shoulder


114


is restrained by the breech


119


of the barrel


118


. The expanding propellant gases force the cartridge case


110


rearward in the direction of the arrow R. This, in turn, accelerates the bolt


145


to the rear and compresses the drive spring


131


for cycling the weapon. Propellant gases bled through vent


300


act on the wad


160


at the base of the payload


102


or a forward propellant charge


157


ignited directly or through a forward primer


150


by the hot, high pressure propellant gases from the primary propellant charge


116


act on the wad


160


to force the payload


102


to be expelled from the cup


122


and to be accelerated along the barrel


118


in the direction of the arrow F.




The embodiments described herein are included for the purposes of illustration, and are not intented to be the exclusive; rather, they can be modified within the scope of the invention. Other modifications may be made when implementing the invention for a particular application.



Claims
  • 1. A low impulse cartridge for use in a weapon including a barrel, wherein the cartridge comprises:a case; a piston slidably disposed relative to said cartridge case; a shoulder protruding outwardly from a periphery of said piston to provide a stop surface for the barrel when the cartridge is chambered; a payload which is projected during firing; means to contain the payload; means to pierce said piston to expel said payload; wherein said piston is in a normally telescoping open position; and wherein said piston telescopes in a closed position during chambering whereupon the barrel is forced against the shoulder, so that said shoulder provides a load path for reacting against the barrel; and wherein said piston telescopes in said open position after firing.
  • 2. A low impulse cartridge, according to claim 1, wherein the means which contains the payload is a cylindrical cup seated within said piston.
  • 3. A low impulse cartridge, according to claim 2, wherein said cylindrical cup also houses a second propellant charge to increase pressure and to better propel payload.
  • 4. A low impulse cartridge according to claim 2, wherein said cylindrical cup is prevented from being ejected by the gases by a flange located in the outer surface of said cup.
  • 5. A low impulse cartridge, according to claim 1, wherein the means to pierce said piston to expel said payload comprisesa. cylindrical cup which pierces the piston cup; and b. a wad, which under gas pressure from propellant pushes out the said payload.
  • 6. A low impulse cartridge according to claim 1, wherein said payload includes a projectile.
  • 7. A low impulse cartridge according to claim 1, wherein said payload includes liquids, solids or powders.
  • 8. A low impulse cartridge according to claim 1, wherein said payload includes a plurality of non-lethal rubber balls.
  • 9. A low impulse cartridge according to claim 1, wherein said payload includes non-lethal wood or foam batons.
RELATED APPLICATIONS

This application claims benefit of filing date Aug. 20, 1999 of provisional application 60/149,859, the entire file wrapper contents of which application are herewith incorporated by reference as though fully set forth herein at length.

US Referenced Citations (9)
Number Name Date Kind
H000114 Quintavalle Aug 1986
3744420 Barr Jul 1973
4686905 Szabo Aug 1987
4862805 Szabo Sep 1989
5359937 Dittrich Nov 1994
5677505 Dittrich Oct 1997
5834681 DuBay Nov 1998
5938773 Dionne Nov 1999
6095051 Saxby Aug 2000
Provisional Applications (1)
Number Date Country
60/149859 Aug 1999 US