US3380383A - Directional dispensing grenade - Google Patents

Directional dispensing grenade Download PDF

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Publication number
US3380383A
US3380383A US459068A US45906865A US3380383A US 3380383 A US3380383 A US 3380383A US 459068 A US459068 A US 459068A US 45906865 A US45906865 A US 45906865A US 3380383 A US3380383 A US 3380383A
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Prior art keywords
grenade
pressure
transducer
shear
chamber
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US459068A
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Jr Robert W Schnepfe
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Textron Systems Corp
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AAI Corp
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Priority to US459068A priority Critical patent/US3380383A/en
Priority to SE6782/66A priority patent/SE322443B/xx
Priority to IL25810A priority patent/IL25810A/en
Priority to GB22698/66A priority patent/GB1124834A/en
Priority to NO163124A priority patent/NO118139B/no
Priority to DK266266AA priority patent/DK128867B/en
Priority to DE19661578059 priority patent/DE1578059A1/en
Priority to FR63126A priority patent/FR1519544A/en
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Publication of US3380383A publication Critical patent/US3380383A/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/36Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
    • F42B12/46Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing gases, vapours, powders or chemically-reactive substances
    • F42B12/50Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing gases, vapours, powders or chemically-reactive substances by dispersion

Definitions

  • This invention relates to grenades or other particle or liquid ejecting devices, and particularly to a grenade arrangement and method which enables the facile ejection and dissemination of particles or liquid material from within an initially closed and sealed canister or the like.
  • a grenade which will enable the full and complete ejection of a tear gas substance such as CN powder or liquid from the grenade into the atmosphere within a short interval of time.
  • a tear gas substance such as CN powder or liquid
  • Such an ejection can be obtained with a grenade employing explosive charge for expelling the tear gas particles or liquid, but when such is attempted with an initially sealed container a difficult problem is encountered in the conflicting requirements of providing a strong enough seal to prevent undesired inadvertent preopening, with a low cost lightweight canister or other container, while providing sufficient initial pressure to cause opening of the seal at the discharge opening to enable ejection of the tear gas granules or liquid.
  • tear gas material such as powder or liquid from which tear gas is generated in the atmosphere
  • Still a further feature of the invention is the provision of an ejection arrangement in which a discharge opening seal is employed, and in which the pressure generated within the device for ejection of material is transmitted in such a manner as to create an increased effective pressure at and eiiective force transmitted to the discharge opening seal to facilitate rupture of the seal and ease of discharge of the material.
  • a further feature of the invention is the provision of a particle ejection device having pressure-transducing means therein which serves the dual functions of transmitting the force resulting from particles ejection pressure thereon to the zone of a seal at the discharge opening for increasing the effective rupture force applied to the seal, and which facilitates the lateral movement toward the discharge opening of the material to be ejected, by transice forming longitudinal ejection forces into radially inwardly directed forces which converge along a line in alignment with the discharge zone.
  • FIGURE 1 is a longitudinal section view of a grenade constructed according to the invention, the grenade being shown in its condition prior to firing;
  • FIGURE 2 is an external perspective view of the grenade of FIGURE 1;
  • FIGURE 3 is a longitudinal section view similar to that of FIGURE 1, illustrating the grenade action during firing;
  • FIGURE 4 is an exploded view in perspective of the transducer and seal parts of this embodiment.
  • the illustrated grenade 11 takes the form of a container or canister 13, which is preferably formed of plastic material such as nylon, Delrin acetal resin, or other suitable relatively lightweight material of good strength.
  • a container or canister 13 which is preferably formed of plastic material such as nylon, Delrin acetal resin, or other suitable relatively lightweight material of good strength.
  • one end 13a of the canister 13 is closed as initially moulded, and over the mouth of the other end of the cylindrical canister 13 is secured a cover 15 which may be of similar material and which is suitably secured to the main body 13 of the canister as by a pressure weld or adhesive along an annular joint line as indicated at 16.
  • the cover 15 of the canister is provided with a shear disc 17 which is formed integrally therewith, there being an annular relatively weaker shear zone 17a formed by a thinner wall zone surrounding the shear disc and connecting with the remaining portion of the cover 15.
  • a flanged cap 23 may be provided over the shear disc to give added protection against undesired rupture from external forces, in which case the cap may be seated in a recess in the cover 15 as shown in FIGURE 1, as by a slight pressure fit or by holding in place with a pressure-sensitive tape or the like (not shown).
  • cap 23 is optional in many instances, as the shear disc shear zone may be made sufiiciently strong with this invention to prevent most accidental or other unwanted rupture of the shear disc without the necessity for the additional cap 23.
  • the cap 23 is of particular use in such instances as where the cover 15 may be subjected to external high pressures, such as explosive propellant pressures, prior to the firing of the grenade itself.
  • Rupture of the shear disc 17 along the shear zone 17a is accomplished by exerting a concentrated force on the shear disc along the annular shear zone through the medium of a funnel-shaped pressure transducer 21 having a central discharge opening 21a at its smaller tapered end 21b.
  • This small open end 21b of the funnel transducer 21 is seated on an annular step seat 19 formed on the inner surface of the shear disc 17 adjacent the annular shear zone, and the larger outer end 21c of the transducer 21 is guided by the cylindrical side wall surface of the canister 13.
  • the transducer 21 is initially spaced from the remaining portion of the cover 15, as shown in FIGURE 1, and upon rupture and expulsion of the shear disc this funnel transducer 21 is moved into abutment with the main body of cover 15 by the forces exerted thereon through the material being discharged, as shown in FIGURE 3.
  • the tear gas powder or liquid or other material 25 which is to be ejected is initially disposed between the funnel-shaped pressure transducer 21 and an o-bturator piston 27 which is initially disposed adjacent the opposite end of canister 13.
  • the obturator piston 27 may be provided with a suitable trailing annular pressure-responsive obturating edge 27a to aid in sealing of the tear gas particle chamber from the propellent gases which are employed to impart longitudinal movement to the obturator piston 27 and thereby effect rupture of the shear zone 17a and the ejection of the tear gas powder or other material through the discharge opening 18 formed upon rupture and ejection of the shear disc 17.
  • a propellent chamber assembly 29 which is disposed in a cup-shaped recess 31 formed in the closed end 13a of the canister 13.
  • the propellent chamber assembly 29 is of self-contained modular construction enabling insertion into the recess 31 either before or preferably after the filling of the canister 13 with tear gas powder or other desired material 25, particularly inasmuch as the recess 31 is also completely sealed from the internal chamber holding the tear gas powder 25. This enables mutual ease and independence of the loading of the tear gas powder and the positioning of the propellent chamber assembly 29.
  • the propellent chamber assembly 29 may be suitably formed with outer and inner main body portions 29a, 2%, which are slidably or press fit together. Suitable sealing against pressure loss may be provided by an annular O- ring seal 37 disposed in an annular groove in the outer body portion 29a, and the entire assembly 29 may be suitably retained in position within the cup-shaped recess 31 as through the medium of a pair of retainer pins which engage complementary transverse locking grooves formed in the adjacent interfacing wall portions of the canister end 13a and the propellent assembly body portion 29a.
  • the propellent chamber assembly 29 includes a propellent charge 39 which is covered by a blowout cover 41 disposed in an annular groove 43 at the inner end of the main body portion of the assembly 29.
  • a blowout cover 41 disposed in an annular groove 43 at the inner end of the main body portion of the assembly 29.
  • Formed at the bottom of the recess 31 of the canister 13 is a shear disc 33 which has an annular thinner wall shear zone 33a, as shown in FIGURE 1.
  • the blowout cover 41 is disposed in facing relation to the shear disc 33, and is adapted to effect blowout of the shear disc 33 upon energization of the explosive propellent charge 39 as shown in FIGURE 3.
  • the propellent charge is fired through the medium of an intermediate pyrotechnic time delay fuze 45 which is in the form of a rod of suitable fuze material such as a powder mixture of ground glass or silica, and zirconium barium chromate, of standard time delay fuze construction, carried within a metallic tube shield 47 and communicating with the propellent charge 39 at its inner end.
  • an apertured metallic shield such as a cover washer 49, on which rests a percussion primer 51 of conventional construction and which is adapted to be fired through the medium of a striker 57.
  • the striker 57 may be of suitable conventional construction and is illustrated as being carried by a pivot pin 59 which also carries an actuating torsion spring 61 which serves to effect the desired actuating movement of the striker 57 into contact with the primer 51.
  • the striker 57 Prior to firing, the striker 57 is held in the ready position as shown in FIGURE 1 through the medium of an L-shaped handle 53 of conventional construction and which is hooked under a lip 291m of the propellent chamber assembly outer body portion 29a, as seen in FIGURES l and 2.
  • the handle may be suitably retained in this initial position through the medium of a releasable retainer pin and pull ring 55a carried in a suitable transverse bore formed in the end wall 13a of the container 13.
  • the grenade 11 may be either hand-held,
  • the handle 53 is conditioned for release by removing the pull ring 55a and the retainer pin 55, and after release of the handle 53 the striker 57 is moved into percussion contact with the primer 51 by action of the spring 61.
  • the primer initiates the burning of the time delay fuze 45 which subsequently initiates the burning of the propellent charge 39 which effects blowout of the blowout cover 41 and shear disc 33 and longitudinal movement of the obturator piston 27 toward the discharge end of the canister 13. Movement of the obturator piston 27 by the pressure of the propellent gases imparts compression pressures to the tear gas powder or other material 25, which pressures are transmitted to both the shear disc -17 directly and the funnel pressure transducer 21.
  • the Wall pressure exerted thereupon is converted into a longitudinal component and a transverse radially-acting component, the longitudinal component being opposed along the relatively much smaller annular end wall section forming the shear disc zone 17a, and thereby increasing the pressure and effective force at this shear zone may fold over what would without transducer 21 be exerted as a result of only the pressure applied by the particles 25 along the face of the shear disc 17, so as to facilitate rapid and facile rupture of shear zone 17a and blowout of the shear disc 17.
  • the radial component forces resulting from the pressure exerted against the transducer funnel 21 effect a radially inward camming motion of the particles which greatly facilitates the movement of the particles from the peripheral portion of the canister chamber toward and through the discharge opening 18, thereby obviating any tendency of the particle material to become compacted and remain in columnar form along the peripheral portion of the container. It will also be apparent that by formation of the transducer 21 in the funnel shape as shown in this embodiment the strength of the transducer is substantially increased over what would otherwise be its strength in a flat or plain apertured disc shape.
  • transducer 21 which is other than funnel-shaped, although the much to be preferred embodiment in particle type material discharge is a funnel shape as shown, with its resultant multiple functions and advantages.
  • a grenade comprising a. container having material-moving means for ejecting particle or fluid material from said container, and
  • said container including a chamber cover spaced from said material-moving means and having a rupturable portion for rupture and ejection of material through the rupture opening,
  • a movable frusto-conical pressure transducer member disposed adjacent one end of said chamber and having a central opening therein, the smaller end of said transducer being disposed for concentration of pressure on said rupturable portion of said cover in response to pressure on said transducer member through pressurized contact thereof by said material.
  • said pressure transducer member is a centrally apertured funnel
  • said cover including a cover disc adapted to be dislodged from a covering position in response to pressurized movement of said material toward said funnel and said cover disc, the small apertured end of said transducer funnel corresponding in approximate size to said cover disc and being disposed in lateral registry therewith for transmitting a concentrated pressure on said cover disc.
  • a grenade according to claim 2 wherein said cover disc is a shear disc having a surrounding annular weakened shear section connecting between said shear disc and the contiguous container wall, said container being cylindrical in shape and said shear disc and annular weakened shear section being disposed at one end of said cylindrical container and being of smaller diameter than the continer body diameter.
  • a grenade according to claim 1 further comprising a charge of particle material disposed within said chamber for ejection.
  • a grenade according to claim 7 wherein said explosive charge has an exteriorly exposed percussion primer for exterior actuation, said explosive charge and primer being disposed at the opposite end of said container from said rupturable chamber cover.
  • An explosive charge actuated grenade dispenser for tear gas or comminuted or liquid material comprising a cylindrical container having a cylindrical chamber formed therein for carrying a charge of material to be ejected,
  • a piston disposed for movement within and along said chamber for causing ejection of material from said chamber
  • said container having an opposite end wall with a shear disc disposed thereon
  • said shear disc being of smaller diameter than said piston and cylindrical chamber
  • transducer having a tapered wall surface and a central thru-opening formed therein in longitudinal registry with said shear disc.
  • a grenade according to claim 9 wherein said shear disc has a surface protruding inwardly from the adjacent surface of said end wall, said pressure transducer being spaced in loaded position away from the adjacent end wall surface to enable ease of transmission of motion by said transducer to said shear disc.
  • a grenade according to claim 11 wherein said pressure transducer is a funnel having a central opening in registry with and smaller than said shear disc.
  • An explosive charge actuated grenade dispenser for tear gas or other comminuted or liquid material comprising a cylindrical container having a cylindrical chamber formed therein for carrying a charge of material to be ejected,
  • a piston disposed for movement within and along said chamber for causing ejection of material from said chamber
  • said container having an opposite end wall with a shear disc disposed thereon
  • said shear disc being of smaller diameter than said piston and cylindrical chamber
  • a movable pressure step-up transducer disposed within said container and adapted to transmit increased pressure to said shear disc upon movement of said charge material theretoward
  • transducer having an opening formed therein in longitudinal registry with said shear disc.
  • a grenade according to claim 13 wherein said shear disc has a surface protruding inwardly from the adjacent surface of said end wall, said pressure transducer being spaced in loaded position away from the adjacent end wall surface to enable ease of transmission of motion by said transducer to said shear disc.

Description

April 30, 1968 R. w. SCHNEPFE, JR 3,
DIRECTIONAL DISPENSING GRENADE Filed. May 26, 1965 9 7 1 5 a 5 a 3 7 9 9 9 9 7 5 2 6 3 4&2 2 h L r a M 3 A fi l 1 1) a) l /U m i 54.2 A m a a 3 9 4 U 3 m1 3 3 M 4. A 2 4 D b A A 4 A a a A a 4 U Ab b A A A 4 A A A A 5 4 A A 44 i 2 U A A p A U A n 4 Q/ A b A 09 m a a A A H A A ,A A u b b A I A p A 3 AM A A a a A0 A A M A A b o 4 v n U A D H h 7 b l H A 1 1| A 2 i 2 A) W A bba W P v 9 k 6 P a 7 3 U 2 Robert W. Schnepfe Jr. INVENTOR Hg. 3
Y a L ATTORN Y United States Patent 3,380,383 DIRECTIONAL DISPENSING GRENADE Robert W. Schnepfe, Jr., Timonium, Mi, assignor to AAI Corporation, Cockeysville, Md., a corporation of Maryland Filed May 26, 1965, Ser. No. 459,068 14 Claims. (Cl. 102-64) This invention relates to grenades or other particle or liquid ejecting devices, and particularly to a grenade arrangement and method which enables the facile ejection and dissemination of particles or liquid material from within an initially closed and sealed canister or the like.
In the riot control field it is often desirable to employ a grenade which will enable the full and complete ejection of a tear gas substance such as CN powder or liquid from the grenade into the atmosphere within a short interval of time. Such an ejection can be obtained with a grenade employing explosive charge for expelling the tear gas particles or liquid, but when such is attempted with an initially sealed container a difficult problem is encountered in the conflicting requirements of providing a strong enough seal to prevent undesired inadvertent preopening, with a low cost lightweight canister or other container, while providing sufficient initial pressure to cause opening of the seal at the discharge opening to enable ejection of the tear gas granules or liquid. Thus, if one employs a heavy walled canister it is quite possible to have a strong seal over the discharge opening and effect adequate breakage of this strong seal with a suiii ciently adequate explosive charge; however, it is desirable on the other hand to employ a lightweight canister in most instances while still having a sufficiently strong seal over the discharge opening, and this presents problems in the accomplishment of rupturing or otherwise opening of the seal with the requisite lesser explosive charge which can be tolerated by the lighter weight canister. It has also been found that in the case of ejecting particle materials from such a grenade through the use of an explosive charge a difiiculty is often encountered with compacting of the particles along the side walls of the grenade canister, and consequent prevention of ejection of these particles, particularly when the discharge or ejection opening is substantially smaller than the cross-section of the chamber formed by the canister side walls.
It is accordingly a major object and feature of this invention to provide a grenade which is useful in the dispensing of tear gas material, such as powder or liquid from which tear gas is generated in the atmosphere, and which is particularly adapted to the expulsion of particle type material, particularly tear-gas-forming material, and which enables the employment of a relatively lightweight canister with a relatively small propellant charge, while still enabling the employment of a relatively rugged discharge opening seal arrangement if desired.
I Still a further feature of the invention is the provision of an ejection arrangement in which a discharge opening seal is employed, and in which the pressure generated within the device for ejection of material is transmitted in such a manner as to create an increased effective pressure at and eiiective force transmitted to the discharge opening seal to facilitate rupture of the seal and ease of discharge of the material.
A further feature of the invention is the provision of a particle ejection device having pressure-transducing means therein which serves the dual functions of transmitting the force resulting from particles ejection pressure thereon to the zone of a seal at the discharge opening for increasing the effective rupture force applied to the seal, and which facilitates the lateral movement toward the discharge opening of the material to be ejected, by transice forming longitudinal ejection forces into radially inwardly directed forces which converge along a line in alignment with the discharge zone.
Still other objects, features and attendant advantages will become apparent to those skilled in the art from a reading of the following detailed description of one physical embodiment constructed in accordance with the invention, taken in conjunction with the accompanying drawings wherein:
FIGURE 1 is a longitudinal section view of a grenade constructed according to the invention, the grenade being shown in its condition prior to firing;
FIGURE 2 is an external perspective view of the grenade of FIGURE 1;
FIGURE 3 is a longitudinal section view similar to that of FIGURE 1, illustrating the grenade action during firing;
FIGURE 4 is an exploded view in perspective of the transducer and seal parts of this embodiment.
Referring now in detail to the figures of the drawing, the illustrated grenade 11 takes the form of a container or canister 13, which is preferably formed of plastic material such as nylon, Delrin acetal resin, or other suitable relatively lightweight material of good strength. In this illustrated embodiment one end 13a of the canister 13 is closed as initially moulded, and over the mouth of the other end of the cylindrical canister 13 is secured a cover 15 which may be of similar material and which is suitably secured to the main body 13 of the canister as by a pressure weld or adhesive along an annular joint line as indicated at 16.
The cover 15 of the canister is provided with a shear disc 17 which is formed integrally therewith, there being an annular relatively weaker shear zone 17a formed by a thinner wall zone surrounding the shear disc and connecting with the remaining portion of the cover 15. If desired, a flanged cap 23 may be provided over the shear disc to give added protection against undesired rupture from external forces, in which case the cap may be seated in a recess in the cover 15 as shown in FIGURE 1, as by a slight pressure fit or by holding in place with a pressure-sensitive tape or the like (not shown). However, the use of the cap 23 is optional in many instances, as the shear disc shear zone may be made sufiiciently strong with this invention to prevent most accidental or other unwanted rupture of the shear disc without the necessity for the additional cap 23. The cap 23 is of particular use in such instances as where the cover 15 may be subjected to external high pressures, such as explosive propellant pressures, prior to the firing of the grenade itself.
Rupture of the shear disc 17 along the shear zone 17a is accomplished by exerting a concentrated force on the shear disc along the annular shear zone through the medium of a funnel-shaped pressure transducer 21 having a central discharge opening 21a at its smaller tapered end 21b. This small open end 21b of the funnel transducer 21 is seated on an annular step seat 19 formed on the inner surface of the shear disc 17 adjacent the annular shear zone, and the larger outer end 21c of the transducer 21 is guided by the cylindrical side wall surface of the canister 13. To enable ease of movement of the funnel transducer 21 in its rupture action on the shear zone 17a the transducer 21 is initially spaced from the remaining portion of the cover 15, as shown in FIGURE 1, and upon rupture and expulsion of the shear disc this funnel transducer 21 is moved into abutment with the main body of cover 15 by the forces exerted thereon through the material being discharged, as shown in FIGURE 3.
The tear gas powder or liquid or other material 25 which is to be ejected is initially disposed between the funnel-shaped pressure transducer 21 and an o-bturator piston 27 which is initially disposed adjacent the opposite end of canister 13. The obturator piston 27 may be provided with a suitable trailing annular pressure-responsive obturating edge 27a to aid in sealing of the tear gas particle chamber from the propellent gases which are employed to impart longitudinal movement to the obturator piston 27 and thereby effect rupture of the shear zone 17a and the ejection of the tear gas powder or other material through the discharge opening 18 formed upon rupture and ejection of the shear disc 17.
In order to provide the desired explosive propellent gas pressures for imparting motion to the obturator piston 27 and tear gas powder 25, there is provided a propellent chamber assembly 29 which is disposed in a cup-shaped recess 31 formed in the closed end 13a of the canister 13. The propellent chamber assembly 29 is of self-contained modular construction enabling insertion into the recess 31 either before or preferably after the filling of the canister 13 with tear gas powder or other desired material 25, particularly inasmuch as the recess 31 is also completely sealed from the internal chamber holding the tear gas powder 25. This enables mutual ease and independence of the loading of the tear gas powder and the positioning of the propellent chamber assembly 29.
The propellent chamber assembly 29 may be suitably formed with outer and inner main body portions 29a, 2%, which are slidably or press fit together. Suitable sealing against pressure loss may be provided by an annular O- ring seal 37 disposed in an annular groove in the outer body portion 29a, and the entire assembly 29 may be suitably retained in position within the cup-shaped recess 31 as through the medium of a pair of retainer pins which engage complementary transverse locking grooves formed in the adjacent interfacing wall portions of the canister end 13a and the propellent assembly body portion 29a.
The propellent chamber assembly 29 includes a propellent charge 39 which is covered by a blowout cover 41 disposed in an annular groove 43 at the inner end of the main body portion of the assembly 29. Formed at the bottom of the recess 31 of the canister 13 is a shear disc 33 which has an annular thinner wall shear zone 33a, as shown in FIGURE 1. In the seated position of the propellent chamber assembly 29 the blowout cover 41 is disposed in facing relation to the shear disc 33, and is adapted to effect blowout of the shear disc 33 upon energization of the explosive propellent charge 39 as shown in FIGURE 3.
In the illustrated embodiment the propellent charge is fired through the medium of an intermediate pyrotechnic time delay fuze 45 which is in the form of a rod of suitable fuze material such as a powder mixture of ground glass or silica, and zirconium barium chromate, of standard time delay fuze construction, carried within a metallic tube shield 47 and communicating with the propellent charge 39 at its inner end. Over the outer end of the tube of the tube shield 47 may be disposed an apertured metallic shield such as a cover washer 49, on which rests a percussion primer 51 of conventional construction and which is adapted to be fired through the medium of a striker 57.
The striker 57 may be of suitable conventional construction and is illustrated as being carried by a pivot pin 59 which also carries an actuating torsion spring 61 which serves to effect the desired actuating movement of the striker 57 into contact with the primer 51. Prior to firing, the striker 57 is held in the ready position as shown in FIGURE 1 through the medium of an L-shaped handle 53 of conventional construction and which is hooked under a lip 291m of the propellent chamber assembly outer body portion 29a, as seen in FIGURES l and 2. The handle may be suitably retained in this initial position through the medium of a releasable retainer pin and pull ring 55a carried in a suitable transverse bore formed in the end wall 13a of the container 13.
In operation, the grenade 11 may be either hand-held,
thrown or shot toward the desired action zone. The handle 53 is conditioned for release by removing the pull ring 55a and the retainer pin 55, and after release of the handle 53 the striker 57 is moved into percussion contact with the primer 51 by action of the spring 61. The primer initiates the burning of the time delay fuze 45 which subsequently initiates the burning of the propellent charge 39 which effects blowout of the blowout cover 41 and shear disc 33 and longitudinal movement of the obturator piston 27 toward the discharge end of the canister 13. Movement of the obturator piston 27 by the pressure of the propellent gases imparts compression pressures to the tear gas powder or other material 25, which pressures are transmitted to both the shear disc -17 directly and the funnel pressure transducer 21. By virtue of the tapered inner surface of funnel transducer 21 the Wall pressure exerted thereupon is converted into a longitudinal component and a transverse radially-acting component, the longitudinal component being opposed along the relatively much smaller annular end wall section forming the shear disc zone 17a, and thereby increasing the pressure and effective force at this shear zone may fold over what would without transducer 21 be exerted as a result of only the pressure applied by the particles 25 along the face of the shear disc 17, so as to facilitate rapid and facile rupture of shear zone 17a and blowout of the shear disc 17. The radial component forces resulting from the pressure exerted against the transducer funnel 21 effect a radially inward camming motion of the particles which greatly facilitates the movement of the particles from the peripheral portion of the canister chamber toward and through the discharge opening 18, thereby obviating any tendency of the particle material to become compacted and remain in columnar form along the peripheral portion of the container. It will also be apparent that by formation of the transducer 21 in the funnel shape as shown in this embodiment the strength of the transducer is substantially increased over what would otherwise be its strength in a flat or plain apertured disc shape. It is to be understood, however, that in some instances, particularly where liquid is to be dispensed, it may be found suitable to employ a transducer 21 which is other than funnel-shaped, although the much to be preferred embodiment in particle type material discharge is a funnel shape as shown, with its resultant multiple functions and advantages.
While the invention has been illustrated and described with respect to a single physical embodiment it will be readily apparent that various modifications and embodiments may be made without departing from the scope and spirit of the invention. Accordingly, it is to be understood that the invention is not to be limited by the specific illustrative embodiment, but only by the scope of the appended claims.
That which is claimed is:
1. A grenade comprising a. container having material-moving means for ejecting particle or fluid material from said container, and
a chamber for containing particle or fluid material to be ejected,
said container including a chamber cover spaced from said material-moving means and having a rupturable portion for rupture and ejection of material through the rupture opening,
and a movable frusto-conical pressure transducer member disposed adjacent one end of said chamber and having a central opening therein, the smaller end of said transducer being disposed for concentration of pressure on said rupturable portion of said cover in response to pressure on said transducer member through pressurized contact thereof by said material.
2. A grenade according to claim 1 wherein said pressure transducer member is a centrally apertured funnel, said cover including a cover disc adapted to be dislodged from a covering position in response to pressurized movement of said material toward said funnel and said cover disc, the small apertured end of said transducer funnel corresponding in approximate size to said cover disc and being disposed in lateral registry therewith for transmitting a concentrated pressure on said cover disc.
3. A grenade according to claim 2 wherein said cover disc is a shear disc having a surrounding annular weakened shear section connecting between said shear disc and the contiguous container wall, said container being cylindrical in shape and said shear disc and annular weakened shear section being disposed at one end of said cylindrical container and being of smaller diameter than the continer body diameter.
4. A grenade according to claim 1 further comprising a charge of particle material disposed within said chamber for ejection.
5. A grenade according to claim 4 wherein said material-moving means includes a movable piston spaced from and movable toward said rupturable cover portion to effect movement of said material and transducer member, rupture of said cover and ejection of said material.
6. A grenade according to claim 5 wherein said material-moving means further includes gas pressure generating means adjacent, andseparated from said charge of particle material by, said piston, said piston being an obturator piston having a pressure-responsive radiallysealing expandable trailing edge.
7. A grenade according to claim 6 wherein said gasgenerating means is an explosive charge.
8. A grenade according to claim 7 wherein said explosive charge has an exteriorly exposed percussion primer for exterior actuation, said explosive charge and primer being disposed at the opposite end of said container from said rupturable chamber cover.
9. An explosive charge actuated grenade dispenser for tear gas or comminuted or liquid material comprising a cylindrical container having a cylindrical chamber formed therein for carrying a charge of material to be ejected,
a piston disposed for movement within and along said chamber for causing ejection of material from said chamber,
an explosive charge disposed adjacent said piston and on the opposite side thereof from said charge chamher,
said container having an opposite end wall with a shear disc disposed thereon,
said shear disc being of smaller diameter than said piston and cylindrical chamber,
and a movable pressure transducer disposed at one end of said chamber adjacent said shear disc and adapted to transmit increased pressure to said shear disc upon movement of said charge material theretoward,
said transducer having a tapered wall surface and a central thru-opening formed therein in longitudinal registry with said shear disc.
10. A grenade according to claim 9 wherein said shear disc has a surface protruding inwardly from the adjacent surface of said end wall, said pressure transducer being spaced in loaded position away from the adjacent end wall surface to enable ease of transmission of motion by said transducer to said shear disc.
11. A grenade according to claim 10 wherein said shear disc has an annular step formed thereon forming a seat for said pressure transducer.
12. A grenade according to claim 11 wherein said pressure transducer is a funnel having a central opening in registry with and smaller than said shear disc.
13. An explosive charge actuated grenade dispenser for tear gas or other comminuted or liquid material comprising a cylindrical container having a cylindrical chamber formed therein for carrying a charge of material to be ejected,
a piston disposed for movement within and along said chamber for causing ejection of material from said chamber,
an explosive charge disposed adjacent said piston and on the opposite side thereof from said charge chamher,
said container having an opposite end wall with a shear disc disposed thereon,
said shear disc being of smaller diameter than said piston and cylindrical chamber,
and a movable pressure step-up transducer disposed within said container and adapted to transmit increased pressure to said shear disc upon movement of said charge material theretoward,
said transducer having an opening formed therein in longitudinal registry with said shear disc.
14. A grenade according to claim 13 wherein said shear disc has a surface protruding inwardly from the adjacent surface of said end wall, said pressure transducer being spaced in loaded position away from the adjacent end wall surface to enable ease of transmission of motion by said transducer to said shear disc.
References Cited UNITED STATES PATENTS 1,039,839 10/ 1912 Sevenson 10243 2,959,127 11/ 1960 Weinert 10265 3,000,304 9/1961 Donaldson 10243 X 1,276,434 8/1918 Steinmetz 102-64 2,146,921 2/ 1939 Temple 222-541 2,925,042 2/ 1960 Schmidt et al. 222389 3,282,477 1/ 1966 Henchert 222541 BENJAMIN A. BORCHELT, Primary Examiner.
W. KUJAWA, Assistant Examiner.
Fletcher, Jr.
UNITED STATES PATENT OFFICE CERTIFICATE OF CORRECTION Patent No. 3,380,383 April 30, 1968 Robert W. Schnepfe, Jr.
It is certified that error appears in the above identified patent and that said Letters Patent are hereby corrected as shown below:
Column 4 line 22 "may"should read many Column 5. line 13, "continer" should read container Column 6 line 51, "2,925,042" should read 2,925,942
Signed and sealed this 9th day of September 1969.
(SEAL) Attest:
Attesting Officer Commissioner of Patents WILLIAM E. SCHUYLER, JR.

Claims (1)

1. A GRENADE COMPRISING A CONTAINER HAVING MATERIAL-MOVING MEANS FOR EJECTING PARTICLE OR FLUID MATERIAL FROM SAID CONTAINER, AND A CHAMBER FOR CONTAINING PARTICLE OR FLUID MATERIAL TO BE EJECTED, SAID CONTAINER INCLUDING A CHAMBER COVER SPACED FROM SAID MATERIAL-MOVING MEANS AND HAVING A RUPTURABLE PORTION FOR RUPTURE AND EJECTION OF MATERIAL THROUGH THE RUPTURE OPENING, AND A MOVABLE FRUSTO-CONICAL PRESSURE TRANSDUCER MEMBER DISPOSED ADJACENT ONE END OF SAID CHAMBER AND HAVING A CENTRAL OPENING THEREIN, THE SMALLER END OF SAID TRANSDUCER BEING DISPOSED FOR CONCENTRATION OF PRESSURE ON SAID RUPTURABLE PORTION OF SAID COVER IN RESPONSE TO PRESSURE ON SAID TRANSDUCER MEMBER THROUGH PRESSURIZED CONTACT THEREOF BY SAID MATERIAL.
US459068A 1965-05-26 1965-05-26 Directional dispensing grenade Expired - Lifetime US3380383A (en)

Priority Applications (8)

Application Number Priority Date Filing Date Title
US459068A US3380383A (en) 1965-05-26 1965-05-26 Directional dispensing grenade
SE6782/66A SE322443B (en) 1965-05-26 1966-05-17
IL25810A IL25810A (en) 1965-05-26 1966-05-18 Grenade
GB22698/66A GB1124834A (en) 1965-05-26 1966-05-20 Grenade arrangement
NO163124A NO118139B (en) 1965-05-26 1966-05-24
DK266266AA DK128867B (en) 1965-05-26 1966-05-24 Garnet with charge of particulate or liquid material.
DE19661578059 DE1578059A1 (en) 1965-05-26 1966-05-26 grenade
FR63126A FR1519544A (en) 1965-05-26 1966-05-26 New ejection device, more particularly for grenades, and its production method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US459068A US3380383A (en) 1965-05-26 1965-05-26 Directional dispensing grenade

Publications (1)

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US3380383A true US3380383A (en) 1968-04-30

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US459068A Expired - Lifetime US3380383A (en) 1965-05-26 1965-05-26 Directional dispensing grenade

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US (1) US3380383A (en)
DE (1) DE1578059A1 (en)
DK (1) DK128867B (en)
GB (1) GB1124834A (en)
IL (1) IL25810A (en)
NO (1) NO118139B (en)
SE (1) SE322443B (en)

Cited By (25)

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Publication number Priority date Publication date Assignee Title
US3460507A (en) * 1967-07-21 1969-08-12 Us Navy Piston expelled chemiluminescent water signal dispenser
US3496906A (en) * 1968-02-02 1970-02-24 Us Navy Day/night bidirectional marine marker
US3504826A (en) * 1968-05-16 1970-04-07 Ewell Lee Carlton Sealant containers and dispensers
US3512480A (en) * 1967-12-04 1970-05-19 Aai Corp Directional dispensing grenade with externally open,integrally formed and internally closed,propellant-charge well
US3512685A (en) * 1968-04-25 1970-05-19 Seaquist Valve Co Aerosol container
US3563258A (en) * 1967-10-26 1971-02-16 Valentine Hechler Disposable hermetically sealed container and method
US3613794A (en) * 1970-08-07 1971-10-19 Robert J Naumann Liquid aerosol dispenser
US3656435A (en) * 1967-12-04 1972-04-18 Aai Corp Directional dispensing grenade with externally open, integrally-formed and internally closed, propellant-charge well and internal frusto-conical material discharge guiding surface
US4444111A (en) * 1978-09-30 1984-04-24 Nico-Pyrotechnik Hanns-Juergen Diederichs Kg Crowd control projectile and method of ejecting same
US4607579A (en) * 1982-02-18 1986-08-26 Stenild Eddie L Apparatus for dispersing a dye over securities in a closed space at attempts at burglary
US6227118B1 (en) * 1968-07-15 2001-05-08 The United States Of America As Represented By The Secretary Of The Navy Vaporizer and aerosol generator
US6484908B1 (en) * 2002-03-21 2002-11-26 Garry Tsaur Pressurized piston pusher
US6553912B2 (en) * 2001-04-09 2003-04-29 Blackpoint Engineering, Llc War games land mine
FR2846698A1 (en) * 2002-11-04 2004-05-07 Pyroalliance Disperser for liquid that destroys valuables in attempted theft has reservoir with piston separating liquid from gas generator
US20070068683A1 (en) * 2005-09-23 2007-03-29 Fireaway Llc Manually activated, portable fire-extinguishing aerosol generator
US20070079972A1 (en) * 2005-09-23 2007-04-12 Fireaway Llc Manually activated, portable fire-extinguishing aerosol generator
US20070235200A1 (en) * 2006-04-10 2007-10-11 Gross Marc V Aerosol fire-retarding delivery device
US20070246229A1 (en) * 2006-04-10 2007-10-25 Gross Marc V Aerosol fire-retarding delivery device
US20070245918A1 (en) * 2006-04-10 2007-10-25 Fireaway Llc Ignition unit for aerosol fire-retarding delivery device
US20090301738A1 (en) * 2006-05-04 2009-12-10 Gross Marc V Portable fire extinguishing apparatus and method
US20100282108A1 (en) * 2008-11-11 2010-11-11 Caldwell Marcus L Replaceable cartridge for diversionary device
US20110017187A1 (en) * 2003-10-27 2011-01-27 Brock Nathan R Non-pyrotechnic explosion device
US20150069091A1 (en) * 2012-04-02 2015-03-12 Kaga Works Co., Ltd. Plunger for pneumatic dispenser
US9046334B1 (en) * 2013-03-15 2015-06-02 The United States Of America As Represented By The Secretary Of The Army Non-lethal obscuration grenade
US20170356707A1 (en) * 2012-09-23 2017-12-14 Lhb Ltd. Clay-pigeon-like projectile for crowd control

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GB2188128B (en) * 1986-02-15 1989-11-08 Royal Ordnance Plc Ejection cartridge
DE9213376U1 (en) * 1992-10-05 1992-12-10 Nico Pyrotechnik Hanns-Juergen Diederichs Gmbh & Co Kg, 2077 Trittau, De
DE9213375U1 (en) * 1992-10-05 1992-12-17 Nico Pyrotechnik Hanns-Juergen Diederichs Gmbh & Co Kg, 2077 Trittau, De
DE102011120420A1 (en) * 2011-12-08 2013-06-13 Rheinmetall Waffe Munition Gmbh Grenade, in particular for the release of irritants
DE102014012226A1 (en) * 2014-08-21 2016-02-25 Hartmut J. Schneider launch device

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US1276434A (en) * 1917-10-09 1918-08-20 Joseph A Steinmetz Grenade.
US2146921A (en) * 1938-08-20 1939-02-14 Victor Metal Products Corp Single-dose tube
US2925042A (en) * 1957-12-09 1960-02-16 Allis Chalmers Mfg Co Intermediate pressure take-off from barrel type boiler feed pumps
US2959127A (en) * 1956-02-16 1960-11-08 Fed Lab Inc Gas grenade
US3000304A (en) * 1955-09-30 1961-09-19 T W Hand Fireworks Co Ltd Container closure
US3282477A (en) * 1961-01-19 1966-11-01 Continental Can Co Plastic dispensing nozzle with removable seal and captive cap

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US1039839A (en) * 1912-10-01 C H Stevenson Paper shell cartridge.
US1276434A (en) * 1917-10-09 1918-08-20 Joseph A Steinmetz Grenade.
US2146921A (en) * 1938-08-20 1939-02-14 Victor Metal Products Corp Single-dose tube
US3000304A (en) * 1955-09-30 1961-09-19 T W Hand Fireworks Co Ltd Container closure
US2959127A (en) * 1956-02-16 1960-11-08 Fed Lab Inc Gas grenade
US2925042A (en) * 1957-12-09 1960-02-16 Allis Chalmers Mfg Co Intermediate pressure take-off from barrel type boiler feed pumps
US3282477A (en) * 1961-01-19 1966-11-01 Continental Can Co Plastic dispensing nozzle with removable seal and captive cap

Cited By (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3460507A (en) * 1967-07-21 1969-08-12 Us Navy Piston expelled chemiluminescent water signal dispenser
US3563258A (en) * 1967-10-26 1971-02-16 Valentine Hechler Disposable hermetically sealed container and method
US3512480A (en) * 1967-12-04 1970-05-19 Aai Corp Directional dispensing grenade with externally open,integrally formed and internally closed,propellant-charge well
US3656435A (en) * 1967-12-04 1972-04-18 Aai Corp Directional dispensing grenade with externally open, integrally-formed and internally closed, propellant-charge well and internal frusto-conical material discharge guiding surface
US3496906A (en) * 1968-02-02 1970-02-24 Us Navy Day/night bidirectional marine marker
US3512685A (en) * 1968-04-25 1970-05-19 Seaquist Valve Co Aerosol container
US3504826A (en) * 1968-05-16 1970-04-07 Ewell Lee Carlton Sealant containers and dispensers
US6227118B1 (en) * 1968-07-15 2001-05-08 The United States Of America As Represented By The Secretary Of The Navy Vaporizer and aerosol generator
US3613794A (en) * 1970-08-07 1971-10-19 Robert J Naumann Liquid aerosol dispenser
US4444111A (en) * 1978-09-30 1984-04-24 Nico-Pyrotechnik Hanns-Juergen Diederichs Kg Crowd control projectile and method of ejecting same
US4607579A (en) * 1982-02-18 1986-08-26 Stenild Eddie L Apparatus for dispersing a dye over securities in a closed space at attempts at burglary
US6553912B2 (en) * 2001-04-09 2003-04-29 Blackpoint Engineering, Llc War games land mine
US6484908B1 (en) * 2002-03-21 2002-11-26 Garry Tsaur Pressurized piston pusher
WO2003080501A1 (en) * 2002-03-21 2003-10-02 Garry Tsaur Pressurized piston pusher
FR2846698A1 (en) * 2002-11-04 2004-05-07 Pyroalliance Disperser for liquid that destroys valuables in attempted theft has reservoir with piston separating liquid from gas generator
US7905179B2 (en) * 2003-10-27 2011-03-15 Brock Nathan R Non-pyrotechnic explosion device
US20110017187A1 (en) * 2003-10-27 2011-01-27 Brock Nathan R Non-pyrotechnic explosion device
US20070079972A1 (en) * 2005-09-23 2007-04-12 Fireaway Llc Manually activated, portable fire-extinguishing aerosol generator
WO2007040561A1 (en) * 2005-09-23 2007-04-12 Fireaway Llc Manually activated, portable fire-extinguishing aerosol generator
US20070068683A1 (en) * 2005-09-23 2007-03-29 Fireaway Llc Manually activated, portable fire-extinguishing aerosol generator
US20070068687A1 (en) * 2005-09-23 2007-03-29 Fireaway Llc Manually activated, portable fire-extinguishing aerosol generator having a plurality of discharge ports circumferentially disposed about the surface of the casing
US7389825B2 (en) 2006-04-10 2008-06-24 Fireaway Llc Aerosol fire-retarding delivery device
US20070246229A1 (en) * 2006-04-10 2007-10-25 Gross Marc V Aerosol fire-retarding delivery device
US7461701B2 (en) 2006-04-10 2008-12-09 Fireaway Llc Aerosol fire-retarding delivery device
US7614458B2 (en) 2006-04-10 2009-11-10 Fireaway Llc Ignition unit for aerosol fire-retarding delivery device
US20070245918A1 (en) * 2006-04-10 2007-10-25 Fireaway Llc Ignition unit for aerosol fire-retarding delivery device
US20070235200A1 (en) * 2006-04-10 2007-10-11 Gross Marc V Aerosol fire-retarding delivery device
US20090301738A1 (en) * 2006-05-04 2009-12-10 Gross Marc V Portable fire extinguishing apparatus and method
US7832493B2 (en) 2006-05-04 2010-11-16 Fireaway Llc Portable fire extinguishing apparatus and method
US20110056711A1 (en) * 2006-05-04 2011-03-10 Fireaway Llc Portable fire extinguishing apparatus and method
US8146675B2 (en) 2006-05-04 2012-04-03 Fireaway Llc Portable fire extinguishing apparatus and method
US20100282108A1 (en) * 2008-11-11 2010-11-11 Caldwell Marcus L Replaceable cartridge for diversionary device
US20150069091A1 (en) * 2012-04-02 2015-03-12 Kaga Works Co., Ltd. Plunger for pneumatic dispenser
US9598223B2 (en) * 2012-04-02 2017-03-21 Kaga Works Co., Ltd. Plunger for pneumatic dispenser
US20170356707A1 (en) * 2012-09-23 2017-12-14 Lhb Ltd. Clay-pigeon-like projectile for crowd control
US10928149B2 (en) * 2012-09-23 2021-02-23 Yariv Ben-Yehuda Clay-pigeon-like projectile for crowd control
US9046334B1 (en) * 2013-03-15 2015-06-02 The United States Of America As Represented By The Secretary Of The Army Non-lethal obscuration grenade

Also Published As

Publication number Publication date
DK128867B (en) 1974-07-15
SE322443B (en) 1970-04-06
NO118139B (en) 1969-11-10
DE1578059A1 (en) 1970-10-15
IL25810A (en) 1970-12-24
GB1124834A (en) 1968-08-21

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