IP Library Granted Patent US 11,498,679
Granted Patent B2
US 11,498,679 · App. 17/316,433 · Granted Nov 15, 2022

System and method of providing a projectile module having a net with a drawstring

Inventors: Robert Edmund Gooch (Orem, UT); Devin Donald Lebaron (Saratoga Springs, UT); Adam Eugene Robertson (Provo, UT)
Assignee: Fortem Technologies, Inc.
B64D7/06B64C39/024F41A19/59F41B11/62F41B11/723F41B11/80F41H13/0006F41H13/0012F41H13/0025B64C2201/121
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Quick Facts
Patent No.
US 11,498,679
App. No.
17/316,433
Granted
Nov 15, 2022
Kind
B2
Abstract

A projectile cartridge that can be removably attached to a flying vehicle is disclosed. A system can include a first flying vehicle, a projectile attachment mechanism configured with the first flying vehicle, a projectile cartridge that contains a projectile, the projectile cartridge being removably attachable to the projectile attachment mechanism, a weight attached to the projectile, the weight being configured in a releasable configuration in the projectile cartridge and a drawstring configured with the projectile. After firing the projectile, when tension is applied to the drawstring as the projectile approaches or envelops a second flying vehicle, the tension can cause the drawstring to close the projectile down to secure the second flying vehicle.

Claims (50)

1. A system comprising:

a first flying vehicle;

a projectile attachment mechanism configured with the first flying vehicle;

a projectile cartridge that contains a projectile, the projectile cartridge being removably attachable to the projectile attachment mechanism;

a weight attached to the projectile, the weight being configured in a releasable configuration in the projectile cartridge; and

a drawstring configured with the projectile, wherein, after firing the projectile, when tension is applied to the drawstring as the projectile approaches or envelops a second flying vehicle, the tension causes the drawstring to close the projectile down to secure the second flying vehicle, wherein at least two of four corners of the projectile have configured thereon a respective attachment guide member through which the drawstring is pulled to close the projectile down to secure the second flying vehicle.

2. The system of claim 1 , wherein the projectile comprises a net having one of a circular shape, a hexagonal shape, a rectangular shape, a square shape, a first shape having four corners, a second shape having six corners or a third shape having eight corners.

3. The system of claim 2 , wherein, when the net comprises the first shape having four corners, the drawstring is attached to at least two of the four corners of the net.

4. The system of claim 2 , wherein weight comprises a first weight and wherein a first string attaches the first weight to a first location of the net, a second string attaches the second weight to a second location of the net, a third string attaches the third weight to a third location of the net, and a fourth string attaches the fourth weight to a fourth location of the net.

5. The system of claim 4 , wherein a first attachment guide member is configured at the first location of the net and a second is configured at the second location of the net.

6. The system of claim 5 , wherein a first portion of the drawstring passes through the first attachment guide member and is attached at the second location of the net, a second portion of the drawstring passes through the first attachment guide member and is attached to the third location of the net, a third portion of the drawstring passes through the second attachment guide member and is attached to the second location of the net and a fourth portion of the drawstring passes through the second attachment guide member and is attached to the third location.

7. The system of claim 2 , wherein a first branch of the drawstring is connected to the a first location of the net via a first mechanism that provides a first ratio of distance pulled to how much the drawstring draws and wherein a second branch of the drawstring is connected to a second location of the net via a second mechanism that provides a second ratio of distance pulled to how much the drawstring draws.

8. The system of claim 7 , wherein the first mechanism and the second mechanism each comprise one of a pulley, a block and tackle and a loop.

9. The system of claim 1 , wherein a first portion of the drawstring passes through a first attachment guide member at a first location of the net, the first portion of the drawstring extending across a center portion of the net to a second location opposite the first location, and wherein a second portion of the drawstring passes through a second attachment guide member at a third location of the net, the second portion of the drawstring extending across the center portion of the net to a fourth location opposite the third location.

10. The system of claim 1 , wherein a first portion of the drawstring passes through a first attachment guide member at a first location of the net, the first portion of the drawstring extending down a first side of the net attaching to a second location adjacent to the first location, and wherein a second portion of the drawstring passes through a second attachment guide member at a third location of the net, the second portion of the drawstring extending down a second side of the net attaching to a fourth location adjacent to the third location.

11. The system of claim 1 , the drawstring comprises a first loop that passes through a first attachment guide member at a first location of the net, the first loop attached to a tether, a second loop that passes through a second attachment guide member at a second location of the net, the second loop attached to the tether, a third loop that passes through a third attachment guide member at a third location of the net, the third loop attached to the tether and a fourth loop that passes through a fourth attachment guide member at a fourth location of the net, the fourth loop attached to the tether.

12. The system of claim 11 , wherein the drawstring further passes through at least a fifth attachment guide member configured at an edge of the net and between any two adjacent attachment guide members of the first attachment guide member, the second attachment guide member, the third attachment guide member and the fourth attachment guide member.

13. The system of claim 1 , the drawstring having a first branch attached to a first location of the net, a second branch attached to a second location of the net, a third branch attached to a third location of the net and a fourth branch attached to a fourth location of the net.

14. The system of claim 13 , wherein the first branch, the second branch, the third branch and the fourth branch each pass across the net and through a central location of the net and connect to a tether.

15. The system of claim 1 , the system further comprising:

a tension-producing mechanism that provided the tension on the drawstring to cause the drawstring to close the projectile down.

16. The system of claim 15 , wherein the tension-producing mechanism comprises one of: a weight that is dropped, a separate weight that is launched, a rewind spool for a tether attached to the drawstring, a parachute attached to the drawstring, a block and tackle structure attached to the drawstring, and a reversal of the first flying vehicle.

17. The system of claim 1 , where the drawstring is attached to a tether which is attached to the first flying vehicle and wherein a momentum of the second flying vehicle upon impacting the projectile causes the tether to pull on the drawstring.

18. A projectile cartridge that is removably attached to a first flying vehicle, the projectile cartridge comprising:

a net;

a first weight attached to a first location of the net, the first weight being configured in a first receiving cavity of the projectile cartridge;

a second weight attached to a second location of the net, the second weight being configured in a second receiving cavity of the projectile cartridge;

a drawstring associated with the first location and the second location of the net; and

a tether that attaches the drawstring to the first flying vehicle, wherein upon firing the net, tension provided to the drawstring causes the drawstring to close down the net and cause the net to capture a second flying vehicle, wherein at least two of four corners of the net have configured thereon a respective attachment guide member through which the drawstring is pulled to close the net down to secure the second flying vehicle.

19. The projectile cartridge of claim 18 , further comprising:

a drawstring mechanism to initiate tension on the drawstring to capture the second flying vehicle.

20. The projectile cartridge of claim 19 , further comprising:

a third weight attached to the net, the third weight being configured in a third receiving cavity of the projectile cartridge that enables the net to capture the second flying vehicle; and

a fourth weight attached to the net, the fourth weight being configured in a fourth receiving cavity the projectile cartridge the net to capture the second flying vehicle.

21. A projectile cartridge configured to be removably attached to a first flying vehicle, the projectile cartridge comprising:

a net;

a weight attached to the net, the weight being configured in a receiving cavity in the projectile cartridge that enables a projection of the weight upon firing via a control system on the first flying vehicle; and

a drawstring configured with the net, wherein the drawstring, after the net being fired to capture a second flying vehicle and upon implementation of a drawing operation, draws in to close the net to enable a capture of the second flying vehicle in the net, wherein at least two of four corners of the net have configured thereon a respective attachment guide member through which the drawstring is pulled to close the net down to secure the second flying vehicle.

22. The projectile cartridge of claim 21 , wherein the weight comprises a first weight attached to a first location of the net, and wherein the projectile cartridge further comprises:

a second weight attached to a second location of the net;

a third weight attached to a third location of the net; and

a fourth weight attached to a fourth location of the net, wherein the drawstring is either attached directly to a respective location of the net or slides by the respective location of the net via a sliding mechanism.

23. A projectile cartridge configured to be removably attached to a first flying vehicle, the projectile cartridge comprising:

a net;

a weight attached to the net, the weight being configured in a receiving cavity in the projectile cartridge that enables a projection of the weight upon firing via a control system on the first flying vehicle; and

a drawstring configured with the net, the drawstring connected to a tether which is anchored to the first flying vehicle, wherein a momentum of a second flying vehicle upon impacting with the net causes the tether to pull the drawstring and close the net on the second flying vehicle thus capturing the second flying vehicle, wherein at least two of four corners of the net have configured thereon a respective attachment guide member through which the drawstring is pulled to close the net down to secure the second flying vehicle.

24. A projectile cartridge configured to be removably attached to a first flying vehicle, the projectile cartridge comprising:

a net;

a weight attached to the net, the weight being configured in a receiving cavity in the projectile cartridge that enables a projection of the weight upon firing via a control system on the first flying vehicle; and

a drawstring configured with the net, the drawstring connected to a tether which is attached to a parachute, wherein a momentum of a second flying vehicle upon impacting with the net causes the tether being resisted by the parachute to pull the drawstring and close the net around the second flying vehicle thus capturing and disabling the second flying vehicle due to the drag of the parachute, wherein at least two of four corners of the net have configured thereon a respective attachment guide member through which the drawstring is pulled to close the net down to secure the second flying vehicle.

Assignments (3)
ASSIGMENT OF SECURITY INTEREST Recorded Mar 26, 2026
From: LAGO EVERGREEN CREDIT, LLC
To: LAGO EVERGREEN CREDIT, A DELAWARE STATUTORY TRUST
Reel/Frame 075244/0175 →
SECURITY INTEREST Recorded Oct 23, 2024
From: FORTEM TECHNOLOGIES, INC.
To: LAGO EVERGREEN CREDIT, LLC, AS AGENT
Reel/Frame 068984/0602 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 30, 2021
From: GOOCH, ROBERT E; LEBARON, DEVIN DONALD; ROBERTSON, ADAM EUGENE
To: FORTEM TECHNOLOGIES, INC.
Reel/Frame 056715/0727 →
Continuity (3)
Continuation In Part 16914640 · Jun 29, 2020
Continuation 16176688 · Oct 31, 2018
Related Publication 20210323672A1 · Oct 21, 2021