Launchable flameless expulsion grenade

Information

  • Patent Grant
  • 6349650
  • Patent Number
    6,349,650
  • Date Filed
    Tuesday, August 29, 2000
    24 years ago
  • Date Issued
    Tuesday, February 26, 2002
    22 years ago
Abstract
A tear gas grenade having a pressurized CO2 container oriented with a top in the trajectory direction to a target area and in facing relation to a top-piercing component across a clearance of a tracking compartment therebetween, in the operation of which a fuel-produced gas expands to simultaneously urge the top-piercing component in descending movement puncturing the CO2 container and also sealing the tracking compartment against venting of the fuel-produced gas and, after a time interval of contraction of the fuel-produced gas, the CO2 pressure urges the top piercing component in ascending movement unblocking the puncture opening in a container top and also unsealing the tracking compartment, to thereby correlate the expulsive effect of the CO2 to the time interval of the sealed contraction of the fuel-produced gas contributing to a tear gas consequence adjacent or in the target area.
Description




The present invention relates generally to tear gas grenades and, more particularly, tear gas-type grenades using as the expulsive force compressed gas such as CO


2


which, unlike a pyrotechnic, is flameless and thus provides a correspondingly flameless use.




BACKGROUND OF THE INVENTION




Field of the Invention




The use of expulsive Carbon Dioxide (CO


2


) tear gas grenades are well known because the expulsion is flameless due to the use of CO


2


, as distinguished from a pyrotechnic expulsive fuel which burns hot and may shoot out white hot slag, one such flameless CO


2


tear gas grenade being that described and illustrated in U.S. Pat. No 5,069,134 for “Flameless Expulsive Grenade” issued to Pinkney on Dec. 3, 1991.




The '134 tear gas grenade and all other known similar grenades benefit from a flameless expulsion due to the use of CO


2


for the tear gas formulation which is normally in powder or liquid form, but in the absence of delicate handling prior to use and/or careful control during use, these grenades are vulnerable to premature release of the CO


2


and thus a tear gas consequence at an unwanted non-target area location.




SUMMARY OF THE INVENTION




Broadly, it is an object of the present invention to provide a flameless CO


2


tear gas grenade overcoming the foregoing and other shortcomings of the prior art.




More particularly, it is an object to release the CO


2


for its expulsive effect following a piercing of its storage container caused by use of an expanding and contracting pyrotechnic-produced gas, but under safe and controlled circumstances which maintains its flameless nature, and in which the gas expansion for container piercing and subsequently contraction for CO


2


release from the pierced container entails a time interval which obviates any premature tear gas consequence until completion of the trajectory of the grenade at the target area, all as will be better understood as the description proceeds.











BRIEF DESCRIPTION OF THE DRAWING




The description of the invention which follows, together with the accompanying drawings should not be construed as limiting the invention to the example shown and described, because those skilled in the art to which this invention appertains will be able to devise other forms thereof within the ambit of the appended claims.





FIG. 1

is a front elevational view, partially in longitudinal cross section, of a prior art grenade using pressurized carbon dioxide (CO


2


) as the expulsive force to achieve a tear gas consequence at a target area;





FIGS. 2

,


3


and


4


are front elevational views, in longitudinal cross section, illustrating in sequence an operating mode of a tear gas expulsive grenade addressing the problem of premature release of the CO


2


of the prior art and like grenades of

FIG. 1

, in which more particularly,

FIG. 2

depicts the grenade prior to use;





FIG. 3

depicts the grenade at an initial location in its trajectory to a target area; and





FIG. 4

depicts the grenade subsequently along its trajectory at a location adjacent its target area.











DESCRIPTION OF THE PREFERRED EMBODIMENT




As background, it is noted that tear gas grenades of the flammable or pyrotechnic type have been in use for some time. Pyrotechnic grenades include a fuel used to ignite tear gas pellets which produce a smoke that is expelled through ports in the grenades. A major drawback in using pyrotechnic grenades is that they burn quite hot and can readily start fires. Accordingly, their use is generally limited to locations where there is no fear of igniting combustible materials.




A tear gas grenade having a more desirable flameless explosive force instead of a pyrotechnic fuel uses pressurized carbon dioxide (CO


2


) and in

FIG. 1

is generally designated


10


. The source


12


of the CO


2


is stored for use within a container


14


mounted in relation to the direction of launch or its trajectory


16


, in an upside down orientation in which a bottom closure


18


of the container


14


is in a clearance position below a closure piercing component


20


. In the pre-launch handling of the prior art grenade


10


inadvertent dropping of the unit on its base


22


or, even more significant, a sudden acceleration immediately after launch will cause movement


24


in the housing


26


not also occurring in the CO


2


container


14


, due to its inertia and being held stationary in the housing


26


between spring


28


and rear positioning wad


30


, which will cause premature piercing contact of the piercing component


20


with the bottom closure


18


and thus a corresponding premature release of the CO


2


.




The problem of premature release of the CO


2


is addressed in the operating mode illustrated in sequence in

FIGS. 2

,


3


and


4


to which reference should now be made. The tear gas grenade, generally designated


32


, preparatory to use, is held securely in hand and this results in a lever


34


being restrained by the palm of the hand. A safety pin


36


is removed by pulling on a ring


38


and the grenade


32


is thrown.




Once free, the lever


34


under spring urgency flies off and results in a sequence of occurrences, well understood in the munitions art of:




(1) allowing a striker to hit a primer that initiates a pyrotechnic delay column;




(2) after a prescribed delay (usually 1.5 seconds), a fuse shoots out white hot slag and flame into a baffle cavity;




(3) slag and flame emerging from a small hole in a baffle disc which ignites a propelling charge; and




(4) the stock and expanding gasses from the ignited charge provide the operating mode in the grenade


32


which uses the pressurized CO


2


as the expulsive force in causing a tear gas consequence at a target area.




To advantageously use the aforesaid well known sequence of occurrences to obviate premature release of the CO


2


which provides the expulsive force for grenade


32


, the grenade


32


is constructed, as will now be described in conjunction with

FIGS. 2

,


3


and


4


, with significant differences noted from the construction of prior art tear gas grenades, as exemplified by grenade


10


of FIG.


1


. More particularly, in the housing


40


of the grenade


32


there is provided a source


42


of pressurized CO


2


within a container


44


mounted, relative to its direction of launch


46


, in a right-side up orientation, thereby positioning a top closure


48


of pierceable construction material, from which the container


44


is suspended in descending relation in the housing


40


in a clearance position below a piercing component


50


, or in a reverse relationship of that of the prior art grenade


10


of FIG.


1


.




Piercing component


50


has a circular disc-like body


52


sized to have a friction fit at the interface


54


of its peripheral edge and a cylindrical wall


56


bounding a tracking compartment


58


for the piercing component


50


during descending movement


60


from its clearance position above the container top closure


48


, said descending movement


60


resulting under the urgency of expanding gas, depicted at


62


, dislodging the piercing component from its friction fit


54


into piercing contact of its integral pointed projection


64


into the top closure


48


. The expanding gas


62


, in turn, is the result of ignition of a propelling pyrotechnic charge


66


.




At the base of the tracking compartment cylindrical wall


56


are side venting openings


68


and


70


in communication via an external clearance


72


about the container


44


and spaced from a frangible latex or rubber membrane housing


74


. Housing


74


protects the CO


2


container


44


and internal components from contamination and possible adverse effects of a payload


76


in the grenade housing


40


, such as tear gas-producing powder or the like known to cause oxidation.




It will be noted that the piercing component


50


comes to a full stop against the container top closure


48


and in that position the disc body


52


closes the venting openings


68


and


70


thus preventing any flame or hot gases


62


from escaping through the venting openings


68


and


70


and having flow communication via the clearance


72


causing premature rupturing of the membrane housing


74


.




As the gasses


62


above the piercing component


50


cool and contract, pressure above the piercing component subsides. Simultaneously, pressure released from the pierced CO


2


container


44


builds under the piercing component body


50


eventually forcing it to partake of ascending movement


78


unblocking venting openings


68


and


70


and resulting in the CO


2


pressure blowing through one or more membrane openings, such as opening


80


, as depicted at


82


, with the result of serving as an effective expulsive force expelling, as at discharge openings, such as opening


84


, and as depicted at


86


, as well as through additional openings


88


, the tear gas powder


76


.




In practice, it has been found that the sequence of events initiated by the fuse entails a time interval resulting in the grenade


32


being at a location in its trajectory which is adjacent its intended target area, thus obviating any adverse consequence as might occur upon premature release of the CO


2


being used as the expulsive force of the grenade.




While the apparatus for practicing the within inventive method, as well as said method herein shown and disclosed in detail is fully capable of attaining the objects and providing the advantages hereinbefore stated, it is to be understood that it is merely illustrative of the presently preferred embodiment of the invention and that no limitations are intended to the detail of construction or design herein shown other than as defined in the appended claims.



Claims
  • 1. A tear gas expulsion grenade using pressurized carbon dioxide comprising a housing, a source of pressurized carbon dioxide in a container with a top closure of pierceable construction material from which said container is mounted in descending relation in said housing, a said carbon dioxide container-piercing component in said housing disposed in a clearance position above said container top closure operatively mounted to be urged in descending movement into piercing contact with said carbon dioxide container top closure and in returning ascending movement to said clearance position, wall means bounding a tracking compartment for said opposite direction descending and ascending movement of said piercing component, said tracking compartment having vent openings adjacent a base thereof in communicating relation to said carbon dioxide container, and a propelling charge operatively effective to urge said piercing component in said descending movement with expanding gas and to permit said ascending movement thereof upon contracting of said gas, said piercing component having an operative position after an expanding gas-caused descent simultaneously causing a piercing of said carbon dioxide container top closure and closing said tracking compartment vent openings, whereby passage of released pressurized carbon dioxide is initially confined to said tracking compartment and only subsequently is in communication with said carbon dioxide through said opened vent openings.
US Referenced Citations (5)
Number Name Date Kind
3188954 Roach et al. Jun 1965 A
3795197 Levenson Mar 1974 A
4932328 Pinkney et al. Jun 1990 A
5069134 Pinkney Dec 1991 A
6250226 Leichter et al. Jun 2001 B1