IP Library › Granted Patent US 10,443,970
Granted Patent B2
US 10,443,970 · App. 15/873,694 · Granted Oct 15, 2019

Launch canister to simulate personal and anti-personnel armaments

Inventors: Aaron L Radl (Sandy, UT); Matt Diffley (Salt Lake City, UT)
F41B11/55F41A9/72F41A21/06F41A21/16F41A33/00F42B8/02F42B8/10
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Quick Facts
Patent No.
US 10,443,970
App. No.
15/873,694
Granted
Oct 15, 2019
Kind
B2
Abstract

A launch canister for non-lethal pellets may be used to simulate the use of both personal and anti-personnel weapons. The canister features at least two components, an inner core and outer shell, that are nested and both featuring a plurality of launch bores. Gaskets ring the outside surface of the components, but have slight interface with the internal bores. The gaskets then hold a stack of pellets within each bore until the canister is placed in a launch device and the payload released.

Claims (27)

1. A launch canister for a simulated armament, the canister containing a plurality of non-lethal pellets and comprising:

a. a hollow cylindrical outer canister shell with a length and both outer and inner circumferences, said outer canister shell having a first plurality of cylindrical bores extending through its length and located proximate its outer circumference;

b. a cylindrical inner core with a length, said inner core having an outer circumference and fitting within the hollow canister shell's inner circumference and having a second plurality of cylindrical bores extending through its length and located proximate its outer circumference;

c. means for joining the outer canister shell and the inner core; wherein, each bore of the pluralities of cylindrical bores has a diameter sufficient to accommodate and hold the non-lethal pellets.

2. The launch canister for simulated armament of claim 1 , further comprising a plurality of parallel grooves running the outer circumference of the outer canister shell, said grooves intersecting the first plurality of cylindrical bores; and a plurality of gaskets, one residing in each groove such that at least one portion of each gasket impinges into the cylindrical bores.

3. The launch canister for simulated armament of claim 2 , further comprising a plurality of parallel grooves running the outer circumference of the inner core, said grooves intersecting the second plurality of cylindrical bores; and a plurality of gaskets, one residing in each groove such that at least one portion of each gasket impinges into the cylindrical bores.

4. The launch canister for simulated armament of claim 1 , further comprising a plurality of parallel grooves running the outer circumference of the inner core, said grooves intersecting the second plurality of cylindrical bores; and a plurality of gaskets, one residing in each groove such that at least one portion of each gasket impinges into the cylindrical bores.

5. The launch canister for simulated armament of claim 1 , the means for joining the outer canister shell and the inner core being a threaded interface at an end of the launch canister.

6. The launch canister for simulated armament of claim 5 , further comprising a plurality of parallel grooves running the outer circumference of the outer canister shell, said grooves intersecting the first plurality of cylindrical bores; and a plurality of gaskets, one residing in each groove such that at least one portion of each gasket impinges into the cylindrical bores.

7. The launch canister for simulated armament of claim 6 , further comprising a plurality of parallel grooves running the outer circumference of the inner core, said grooves intersecting the second plurality of cylindrical bores; and a plurality of gaskets, one residing in each groove such that at least one portion of each gasket impinges into the cylindrical bores.

8. The launch canister for simulated armament of claim 5 , further comprising a plurality of parallel grooves running the outer circumference of the inner core, said grooves intersecting the second plurality of cylindrical bores; and a plurality of gaskets, one residing in each groove such that at least one portion of each gasket impinges into the cylindrical bores.

9. A simulated anti-personnel armament comprising:

a. an armament receiver with a barrel;

b. a gas supply in fluid communication with the receiver barrel;

c. a launch canister for containing non-lethal ammunition for the simulated anti-personnel armament, the launch canister fitting within the barrel of the armament receiver and further comprising:

i. a hollow cylindrical outer canister shell with a length, said outer canister shell having a first plurality of cylindrical bores extending through its length and located proximate its outer circumference;

ii. a cylindrical inner core with a length, said inner core fitting within the hollow canister shell and having a second plurality of cylindrical bores extending through its length and located proximate its outer circumference;

iii. means for joining the outer canister shell and the inner core;

iv. the outer canister shell fitting within an interior of the receiver barrel but leaving a space between a bottom of the receiver barrel and a bottom of the outer canister shell into which the gas supply empties;

wherein, each bore of the pluralities of cylindrical bores has a diameter sufficient to accommodate and hold the non-lethal ammunition and the launch canister seals the barrel of the armament so as to allow a build-up of gas pressure which will launch the non-lethal ammunition from the canister.

10. The launch canister for simulated armament of claim 9 , further comprising a plurality of parallel grooves running the outer circumference of the outer canister shell, said grooves intersecting the circumferential cylindrical bores; and a plurality of gaskets, one residing in each groove such that the gaskets seal the launch canister against the barrel and at least one portion of each gasket impinges into the cylindrical bores.

11. The launch canister or simulated armament of claim 10 , further comprising a plurality of parallel grooves running the outer circumference of the inner core, said grooves intersecting the cylindrical bores; and a plurality of gaskets, one residing in each groove such that at least one portion of each gasket impinges into the cylindrical bores.

12. The launch canister for simulated armament of claim 9 , further comprising a plurality of parallel grooves running the outer circumference of the inner core, said grooves intersecting the cylindrical bores; and a plurality of gaskets, one residing in each groove such that at least one portion of each gasket impinges into the cylindrical bores.

13. The launch canister for simulated armament of claim 9 , the means for joining the outer canister shell and the inner core being a threaded interface at an end of the launch canister.

14. The launch canister for simulated armament of claim 13 , further comprising a plurality of parallel grooves running the outer circumference of the outer canister shell, said grooves intersecting the cylindrical bores; and a plurality of gaskets, one residing in each groove such that the gaskets seal the launch canister against the barrel and at least one portion of each gasket impinges into the cylindrical bores.

15. The launch canister for simulated armament of claim 14 , further comprising a plurality of parallel grooves running the outer circumference of the inner core, said grooves intersecting the cylindrical bores; and a plurality of gaskets, one residing in each groove such that at least one portion of each gasket impinges into the cylindrical bores.

16. The launch canister for simulated armament of claim 13 , further comprising a plurality of parallel grooves running the outer circumference of the inner core, said grooves intersecting the cylindrical bores; and a plurality of gaskets, one residing in each groove such that at least one portion of each gasket impinges into the cylindrical bores.

Continuity (2)
Provisional Application 62447317 · Jan 17, 2017
Related Publication 20180202751A1 · Jul 19, 2018
Cited By (1)
US 12,276,474