Information
-
Patent Grant
-
6349650
-
Patent Number
6,349,650
-
Date Filed
Tuesday, August 29, 200024 years ago
-
Date Issued
Tuesday, February 26, 200222 years ago
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Inventors
-
-
Examiners
- Poon; Peter M.
- Smith; Kimberly S.
Agents
-
CPC
-
US Classifications
Field of Search
-
International Classifications
-
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 |